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ETL 13-3 - The Whole Building Design Guide

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4. 5 22 98 gt 79 ON IH9I3A ZTI 41 Cd OST lt 424 2993 0945 1 993 HIDON 3 inal Weight Landi F 117 Nom Chart A2 79 Atch 2 98 of 101 4893 NDIIVOU1 H319d 0009 0005 006 000 005 0006 0052 0008 0051 0001 005 0 DZ P Ulet TT AE Aa E 2202202 m on Fi Fj Fi F SS AAA A EAA d SS is utet NENNT atat EN 5422 m W OQ W P a Pa Pt k Pa PL Cae Cu M DM a ux M X DE XU WE u c m dodo eg 5 ode dde de eoe E 1 alata Dx wx X4 L 6 ee 8 PU LUN LEA w ou u Par u cut b 555555000705 EIS EM ET SY sl Saad 1 Mn m una y 9 d ST De 0 m ar CM DON NA WE spunod 2 9
5. i Sedii u po Ll a OTT ul D ld H EH d E gor EES 2 at os sss T EUBERAY URE Bi 30 40 cua 20 10 0 10 20 30 40 20 60 TEMPERATURE uu 55222 cipem 1 Sees EE LL Figure A2 3 Density Ratio Table Example A2 4 3 5 Request the ranges of the RSC and expected for the day Select the highest RSC or icy is higher than wet wet is higher than dry Record these values on Worksheet 1 A2 4 3 6 Using the RQC Chart Figure Number summary Table A2 2 find the chart number for the aircraft and operation combinations recorded on Worksheet 1 Record these numbers on Worksheet 1 If there is some uncertainty as to the procedures used during aircraft operations select charts for all possible variations Atch 2 8 of 101 Table 2 2 Chart Figure Number A2 Landing Amesmen 6 F 4 C D Chute amp L A5 4 Ce Landing Aerobraking 16 _ Ce lamig WheeBrkng 17 C4 Landing Arresiment 18 _ L Gi tm m 2t Q8 Landing Wheel Braking 22 _ e umm 24 25 oe landing 2 613 Landng Amesmen 27 Qu Evacuation
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8. X os bees 6 NANANA SSO LQG 5 ESSEE gt AD 293 NUIL99D 71 HILYd 009 0005 000 000 000 0001 0 06 0008 000 0 CN AMD T MNT E F QUE a SS SS SSS SS 0007 0056 A cen 11 2 me 232 2018 90 8 1070 9 tete tet NN E H oy N MM Se et SILI OSCE SSS RASA MA 133H pm a S t tote A ONIGNY 4 9 o e sC ge oo o eo e c a a k EEE LOC OC Ma RSX SAA P 90555605 NN ACC TI 6 0 13 NEC NGG br 1I t UWE o 006 009 008 006 0001 OT gt lt aa doe 953 DNIOVdS HJlVd 993 H21Vd Chart A2 17 F 15 A B Landing Wheel Braking Atch 2 36 of 101 993
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11. J E IN 55 seunOgd 00G 22gE gt 3303891 IHDIJA 4 61 34 JS 48835 DNI 11 Alive 24 HLONG k Chart 2 60 KC 135 R Heavy Weight Takeoff Atch 2 79 of 101 39935 Hol ed 0002 0009 0005 000 DO 0001 0 en E UGE 00 E AN MS ND UNA Pim LAN S UNS gt le Z 01 pepe AAT TE LEES DO Z cu gt 7 O Cl VL VWIV V Ill 0001 WE Ee E 0002 _ 0052 000 lt 43303841 LHOIJA 4561 29 1 12945 2194 ISA Chart A2 61 KC 135 R Nominal Weight Takeoff 10943 HION ST R31 48234 Atch 2 80 of 101 aa H31 Wd 00001 0006 0068 000 0009 0005 0002 0001 OGLE mA pur E RR ET ACE CRT pur EDIT ET OC era cT D se tu B l fast ty x 92 OR V B a o S S S 2 060200777771 aM BE BR IS SEE
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13. 4 ld 051 051 lt ad Mr 7993 9 29215 HILV d 33993 HLON31 HILVed F 117 Heavy Weight Landing No Chute Chart A2 81 Atch 2 100 of 101 9933 NOILYIO 1 2194 0059 0009 0066 0005 QOS 000 0055 0005 0052 0002 001 0001 005 0 fp hh th H n r r OL BF 372 Cz P A iia a dE SSAC ETT PE VA AY YV UT WISE T gel at RRR RENN tt ttt NN atat utut uut tutt ung SIS IURE E O Se 2 ne gt w LR qu x S P w W N IR OC RA RU 4 CALI penes k at of UM P Psl RT Ii rs le spunog 00002 gt 9 2 ONIGNY 1 1 Qc OEI 051 424 9942 9 15 HJIVd 49635 HIDN31 21 94 Chute ing F 117 Heavy Weight Land 82 Chart A2 Atch 2 101 of 101 DISTRIBUTION LIST Information Handling Services 1 Construction Criteria Base 1 15 Inverness Way East National Institu
14. Pu ah a abe e d a au ate XJ Pata 4 a m e LM d deo ate MS RP E 7 E M aLL lt 5 M y CAE i 2 125 S NS uid Seer z S x HAAS an lt 4 3 HII in ITT EM SH ts Mb 5252 E Set 14 LLL br sass Li BSS Le gt 1 130 LILES 3994 HIONT H21V4 227 NIJA HOIVA m Figure 2 1 Sample Chart 2 3 Assumptions 2 3 1 Users are familiar with the functions of damage assessment and MOS selection This assumption includes the reporting of airfield damage nomenclature 2 3 2 represent the maximum allowable repair height in inches for all values except flush F and flush repair followed by a flush repair FF 2 3 3 Allowable sag depth 15 2 0 inches for except F and FF 2 3 4 Allowable repair slope is 5 0 for all RQC except in a landing touchdown zone Allowable ramp slope is 3 4 in landing touchdown zones Atch 2 2 of 101 2 3 5 Aircraft contact the entire length of each repair the 5 Lateral repair location does not affect RQC A2 3 6 spalls are repaired to flush criteria A2 3 7 Aircraft operation leng
15. V AJI 0 A EES EEE E A E A IR ER Pee 001 Sata sire ba aina a MEME ta 566655000056 002 A Poda P UR SUUM ETE rt tad me e ad Sy mei 6 oos d M 009 aset 004 sasa 9 NNN N NN ES Bs Em 006 pe 000 OQTI 0021 0081 OOST lt OT gt 0 02 06 ET OST lt ad ae 943 ONIDVdS 194 2883 HIDN31 2194 43 F 111 A E Landing Short Field Chart A2 Atch 2 62 of 101 293 001 19 0022 00902 0081 0091 9021 0007 rigg asldavd 0621 ear Oa EEA E SA t Ls aat Kar P asr a EE Um ps N LONDON wO 7 I3 A 11 selIVd3s EBLE JI eg ama c a ARSE 0 9 gt 009 00 00 0 uM E LOL vie Pd d q j d bd dido 41 NASA IS NSIMSAAA SSO 293 DNIOUdS HILVd ad 1883 H15N31 Arrestment Chart
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17. eet NS AS NS SSS E S 4 SS E UNE WEB ee ee SANG NE m ZZ A AA E l s Too LEE EFL LE y Iy SP yC wU sa AC M X OX XX Ck X X OCDE Chie see 0 52052505050 552525 E a a a E AJI SOE ES CENIA WN 00 d SSS t SSS lt aa S 72 008 006 AG O lt WSS SSS 05 maka E BE e mm n ee a E 0 0001 lt ad 424 243 DNIOVdS HILVd 4943 HION31 19 Chart A2 21 F 15 C D Landing Aerobraking Atch 2 40 of 101 00021 00011 00001 ss lt NES d SSSSSSSSS SSS spunog 16GE gt AD E as OU O O AO WSK NVQ AN SSSR tet d UNT RM y SEO um S CS D RORY ES SS OR EIER ES mer eee ee a M CX LX x X ca T a C P we g WN 3 2 AWN SS 3 293
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21. SSS AS SSS MODEL CO ae RT bod de 0 i 556055696 552505 555509 55995 x 6000 505 5 at 0 Qe 0 aded eO XC OC EES 001 47 E K SS Dom aa ES AAN SSE 5 e W pope EMEN t ee 1133 3 4 3 1 55 7 NMENGENSESM IENNENMENMNNEN Edo Ll uw dq Tou i 0001 lt T yg CIL LTT ITT 1 13 05 apa 06 OST lt 50 9NIJVdS HILVd 223 HL9N31 HILVd Chart A2 14 F 4 E Evacuation Atch 2 33 of 101 993 1 1 2194 0091 OOFI 0001 008 009 OF 00 06 1 E SILLS Ty SSE T F I VPS a 0 Parere iret res lt MM 6422502222 xa o ese assess eee EE 1 005 CET EE NNN 00 SEES DILE PD w 005 009 004 008 005 gt Of 05 0 06 spunog 08 gt AD 1303891 901 1 0007 lt lt ad 4903 DNIJVdS HILVd
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23. DEPARTMENT OF THE AIR FORCE AIR FORCE CIVIL ENGINEER CENTER TYNDALL AIR FORCE BASE FLORIDA 25 EN A R 2 s Q 18 Jan 2013 FROM AFCEC DD 139 Barnes Drive Suite 1 Tyndall AFB FL 32403 5319 SUBJECT Engineering Technical Letter ETL 13 3 Minimum Airfield Operating Surface Selection and Repair Quality Criteria 1 Purpose Establish approved Air Force procedures for Minimum Airfield Operating Surface MAOS selection and determining Repair Quality Criteria 2 Application All Air Force organizations responsible for airfield recovery operations 2 1 Authority Air Force Policy Directive 32 10 Installations and Facilities 2 2 Effective Date Immediately 2 3 Intended Users Air Force Prime Base Engineer Emergency Force Prime BEEF and Rapid Engineer Deployable Heavy Operational Repair Squadron Engineers RED HORSE units 2 4 Coordination Major command MAJCOM A7s 3 Referenced Publications Insert URLs 3 1 Air Force Instructions 10 209 RED HOHSE Program 10 210 Prime Base Engineer Emergency Force BEEF Program 3 2 Air Force Pamphlet AFPAM 10 219 Volume 4 Airfield Damage Repair Operations 3 3 Unified Facilities Criteria UFC 3 270 07 Airfield Damage Repair 4 Acronyms Note The acronyms and terms shown below may not always agree with Joint Publication 1 02 DoD Dictionary of Military and Associated Terms or Air Force Doctrin
24. 5 _ LSS S WS SSE RUND Z Z Z Z Z 77 7 7 Z ees i sss RRR RY 7 V 7 7 17 7 1 7 JU 1 11 145 TL L3 0097 5 7 44 XC COGO O6 0 6 at CC Ct OE 60 06 X PC w SA SESS SBA E oo ld RX ORS RAGA SSS os EM NS en SSSSSSSSSSSSNSSSNSSEUNSSSSESSNWNSINNSSNSN SY YY YmZKYIHSI R I I I IIIG II IRRIK I lt I IQI I IIIILSO UII AX 594 oo SS SS cr G d RSE REREAD Bm NSSSSSSSSSSSSSSSSSSSSSSSANSSSS SAAS SN SEIS if 00069 gt 1 gS E 3393 9NIJVdS H319d 19 31 219 333 Chart A2 47 C 5 B Landing Atch 2 66 of 101 3993 40119207 Hoivd 000 00 0005 0052 0002 0061 0001 00 0 9209 0 3 aaa SS AAA 2 o EC ME y 525252 SAWN S SSS s 4 SS SS ASSIS SSS IN St un 5555 RR lt 3 lt NANA Ep ug cdd n FE e EO E
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26. B TE F 5 ILAE HH i WY ws v 3 la Y s Z i x _ L J x x 4 lt 000 55 30 000 TEMPERATURE OF DENSITY RATIO Figure A2 2 Worksheet 1 Example Atch 2 6 of 101 2 4 3 Collecting Environmental Data A2 4 3 1 Contact the WOC If the WOC does not have the environmental data contact Base Weather A2 4 3 2 Request the expected range of DRs for the day Select the lowest DR expected and record the value on Worksheet 1 A2 4 3 3 If the DR is unavailable request the runway pressure altitude and the expected temperature range Select the highest temperature and record it and the pressure altitude on Worksheet 1 A2 4 3 4 Determine the from the temperature and pressure altitude using the DR chart Figure A2 3 The example uses 59 degrees and sea level A2 4 3 4 1 Enter the DR chart with the temperature value A2 4 3 4 2 Draw a vertical line to the correct altitude line A2 4 3 4 3 Draw a horizontal line to the DR axis and read DH A2 4 3 4 4 Record DR on Worksheet 1 Atch 2 7 of 101 Pup EE ee x ii i a gt HL HHI ms M AEN HE TEETE NE inm HHH 1 0 Hr SERE gt 0 2 Hi 4 ma n TH
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28. A2 4 4 1 Once the proper charts are selected determine the operation length for each combination of aircraft configuration and operation Chart F 111A E Landing Short Field Figure A2 4 shows an example of operations length calculation for an F 111 landing operations with DR 1 0 RCR WET and RSC 0 3 A2 4 4 2 RQC Charts with RCR or RSC A2 4 4 2 1 Draw a horizontal line across the DR section corresponding to the DR recorded on Worksheet 1 A2 4 4 2 2 Draw horizontal line across the RCH HSC section corresponding to the RCR or RSC recorded on Worksheet 1 A2 4 4 2 3 From the intersection of the DR line with the shaded section draw a vertical line up to the bottom of the RCR or RSC section A2 4 4 3 4 Follow the guidelines until the line intersects with the current RCR or RSC Stay between the guidelines in proportion to the starting location A2 4 4 2 5 Draw a vertical line to the location baseline and read the operation length A2 4 4 2 6 Record the length in the space provided on Worksheet 1 A2 4 4 3 RQC Charts without RCR or RSC A2 4 4 3 1 Draw a horizontal line across the DR section corresponding to the DR recorded on Worksheet 1 Atch 2 11 of 101 2 4 4 3 2 From the intersection of the DR line and the shaded section draw a vertical line down to the location baseline and read the operation length A2 4 4 3 3 Record this value on Worksheet 1 A2 4 4 4 The final operati
29. E E Ea X X u 4 x X EK Xx X ce wol Wai I Jm E LA US d E 0 4 5 i i DOT 47867874767 COI d p dh d qd b OO p k B OSO E A A utu m up ep uw ow ww www e PSAL eee IMS Po ao d 1 sss spunod 226 gt 33039591 IHOI3A WNIWON 20 3 d 051 lt ad 44935 ONIDVdS 1 3463 H19N31 Atch 2 Chart 2 77 117 Nominal Weight Takeoff 96 of 101 4994 NOILYIO H319d 0055 00085 DOG 000 0055 0005 0052 0002 0051 9001 005 0 0066 DOZE SKIL ZZ HI a SES S SS SES E SS ML Fa 5506 A etate Och e ee on ata a 2 05 Of 06 gri 01 061 E NE ee E E Hm Loue c quse lx Esacus E lt m EN aru ER sss BS Ty spunod 0009 gt AD LHY9II L 4 Vd Ol g
30. E dd INA A US UR US LR UN 8 NR 0 9 09 0 0 4 9 4 49 9 249 TEES TE TTL a AN NS M TEILE SLES 4 0 SOLS 9 0 9 0 0 0 0 9 OSHS 4 9 OATS 0 0 0 9 9 0 9 0 9 4 0 VARINA 9 0 9 0 0 9 AS XXE 001 LI T or E RUNE 2 if ih e e PERGA ra S es Rut OS iater s NS 5 S 2 gt NS A e E abe cli e d g Ae TT da T LT T E4444 474440474 44 HC on pA 4474744449 4 4 974 4 4 4 4 ETEA ded dede oed dd odd ww Oe HDI HUE WN ie C a s RS 00 25526 NN D SEEN w SS s 3 RAN SR 00b FP 5 OI gt 05 02 06 Jel 051 19 Weight Takeoff 99 Ina t 2 9 Nom Atch 2 86 of 101 Chart A2 67 C H1DN3 7 S E 428835 119000 HEYA 006 000 DOSE DOO UGE 000 OOS OOO 005 OBc LEC 7 7 7 m
31. EEN eee tiim ei E aee 4 E E 7 AR KE A NRK IK ORK OR ME ee Sen 1 aaa SCR UR MES S aS AS SSE iW s _ _ Meet P p pec mani wa GU ss ws isa UK sa Sui ss EE Otto ILLITE ESE Wil SK IEEE Spunog v 0 8 gt AD ONIGNY 3 3 OT 6 0 Aaa 13 8 AJI 0 001 00 00 005 009 00 008 006 0101 lt OT gt 05 Ol 06 ost lt ad 429 4283 10945 219 499 1 Chart 2 12 F 4 E Landing With Chute Atch 2 31 of 101 00 228835 NOILVIOT 21 4 000 010084 00002 0008 0009 00071 00027 00001 0008 0009 000 0002 0 0005 0017 7 OAT BE OT E puer e A p cu OOS e cu pu e cu ap Ge A T SESS SENSN SS S NS SNP Se ES NT RN ANT NU RN Ns NNN AU RUN UN CR NN NN 6 0 S gm
32. Min Wa gr 50 m High Speed Surface Route LoR Constrmints Launch Taxiway Access Point Recovery Taxmay Egress Point Less Than 10008 Less Than 10008 Routing Weights Damage 5 Minimum LOR gt Figure A1 29 Add MOS Routing A1 6 4 6 MOS MAOS Placement An ADR Status Tool Group reports the MAOS MOS criteria and intersecting damage as the MOS template is moved around the surface The Appr Light and MAAS will be Green if the criteria are applied or Red if not Either Uni or Bi will be reported to reflect the applicable operation Craters and spalls will be reported if the MOS physically intersects them Camouflets and UXOs will be reported if the MOS intersects the safety cordons All items will also be highlighted on the map as they are intersected The Est Spalls and Est Camouflets will be calculated if the criteria were selected POL Craters reports those craters intersecting POL lines this count is not a duplicate of the Crater report UXOs reports both Surveyed actually identified and Potential calculated LoR Actual 90 is the actual calculation of the placed MAOS The LoR Constraint 96 is the criterion selected during the Add MOS process If the LoR is critical during placement ensure the lock is locked Ed Finally the Repair Score Index is reported This index rating is used when comparing candidates against another typ
33. T Po ite A Ss AA eee eee ee c u LG KREE F F Pw s a a Re SSS S 8 8 8 8 788 3983 HION31 2194 923 45 Chart A2 56 7 D Landing Arrestment Atch 2 75 of 101 4293 119001 2194 0055 0005 0057 000 005 000 0052 0002 JOST 0001 005 0 0095 i l L 7 77 V gt WC gl ae V v LXX EEEE EEEE EEEE 0 e ata DUK xS Ss XE e ate bes eo ee gei 2 4709 470 49 94 9 0 0 4 0 4 9 4 9 e S 66 5005 4 Soo 5 525 554 558 2 t attinet DEE EEEE EESE EEEE pA e quada d x ettet Deo aco sate 5 264505060 4605060646060054606060 5 0606 Se e Se 22505250 XL ata eae 25526 55 001 SSA 40 YASS SSS gt 008 00E 00 4 9 ad SNIOVdS Chart A2 57 A 7 D Evacuation 993 HLINA Atch 2 76 of 101 3 83 NDILVOD 2
34. S ORO NS owe TEF Fa TT d de le Wc pes SENSN SSS OEE 25222 05557 m m cum RAR 49 tote eae fate 552 06 ten BR See SIS a I LAC ME n psi dia RR RQ RRS RFR NS spunog 00056 gt H3VD3ddV WKRONONTQNY 1 LHOIJ3 A 7 9 1 0 r1 ol 3 go AAT 13 AJI 001 002 006 OOF 005 009 00 008 006 0001 DOT 001 0081 0061 01 Qe 0 04 06 OTI 051 oSI M ad ed ONIOVdS 1 994 4993 HIDN31 H21Vd Normal Approach ing Weight Landi ina 17 Nom Chart A2 74 C Atch 2 93 of 101 enjeA zuana By pjeiury ey InsuoS suonipuoo JO eAnejuesoJdoJ 1 80 JO e pue jo 9AnejuesoJdoi SI gy JO enjeA e Aemun e eAnejueseudau 1 Z jo n A V 80 pue 9 EZ JO 5 esn Seu y 10 eu BunueseudeJ si quinu seyd Burpue JOY 2 3 84 uo pesn 2 eu AJl pue LIM AYO 449 jo SLON SLYVHO ONIONYT 211 54 3
35. SANTIVA ONIGVSY NOILIGNOO L d Chart A2 75 RCR Information Atch 2 94 of 101 GW lt 52 200 Pounds 2 F 117 HEAVY WEIGHT TAKEOFF 993 19 31 HOLVd SIDS aly L s P e m te k ah ne ta a Ae ik 2 2525 x F x fete E qe d ttes hub db db db d a h d d dis pw AK R X X X E U Nate 488 SS 225050506 eate aaa SNNT a ace 3883 9413945 21 94 Chart 2 76 117 Heavy Weight Takeoff Atch 2 95 of 101 N ian t SSS MG 5 SS SSS SS SS ss D ono S WWW ss AS MASA 9200 32300 2000 3000 4000 2000 6000 7000 8000 9000 PATCH LOCATION Feet 1000 yaad NOILVYIU 1 HJ1Vd 0008 0007 0009 0005 000 0200 0002 0001 0 00F8 00 v cs ESS NN NEN SS ERN aa RSS T E F A cec
36. Taxiway RLIRK Taxiway MAAS 12 Months Base Flowable Fill i 12 Months Extreme Weather O 30 Months CBRN Back Next gt Einish Cancel Figure A1 28 Add MOS ADR A1 6 4 5 Add MOS Routing Routing determines the requirements for MAOS selection Route Operation defines the requirement for threshold and departure taxi routes The Minimum Aircraft Width is the width of the required taxiway Checking the High Speed Taxiway box limits the amount of swerving the aircraft is allowed during taxiing Parking Surface to Route To is the primary surface to taxi from additional route selections are available after a MOS has been placed The LoR Constraints sets the requirement for the taxiway location in relation to the existing surface threshold and departure The LoR may or may not be constrained for this requirement during MOS placement to be discussed further in paragraph A1 6 4 6 The Routing Weights can also be set to override the default values as set in the Settings Dialog oelecting Finish at anytime begins the MOS placement activities Be patient there is lot of geoprocessing so it is a bit slow the first time If you are not ready to place a MOS hitting ESC will end the MOS placement session and place the MOS in TOC for future placement Atch 1 22 of 30 Aarcraft Operations WS1 Options ADR Routng Route Operation s Threshold Departure
37. 101 12383 DNIOVdS HILVd Chart A2 50 C 141 A B Heavy Weight Takeoff 9835 HIBN31 H31Vd 993 119301 HILYd 0057 000 0058 0008 0052 000 0001 0101 005 0 0 25 rE2 NVQ S Cy TZ BAVA ZIT Yr SS a ss SG sss 4740 LZ yA RTA iw Audi ALAVA UL AJI gt CMU Z n LLL dem TNZ 00 12 A 2 bes 08 ll Rea TON e 22 4 9NI2VdS 1 Atch 2 70 101 DONIGNV1 LHOISM AAYAH 8 VIvI 29 HLON3 Chart 2 51 141 A B Heavy Weight Landing 993 901193907 HILFE 0005 0057 000 0055 000E 0052 0002 0051 0001 005 0 Sree Orie NGG WD SA SS Z 7 ZV Z22272 A SSS 15 Sree TSS Z lt ZzZV VAT ALL x a m q FF gt L 2 Y Y ri _ 402974797 IC ACACACACACACACA ORAS UO w a LU 070 9 s 545552252555 N OEP e E 00 J 00 Jus
38. 2 5 5 994 NIIN 00655 0055 3 m ie Es 2 Em y e XN xe d E DENN as A a IE ART VT A OT E An AN NKT AQ OD A AMT A a pe WEE dent s UNT E NWO e RR e AE P I i Wow WoW Ww o ps gt 25 550600666060 E hts CO a DP MODO SEN T tete i AE h al h S S Sr SSSA NER ROSS ASAE SS haee 559 SS 328 NN S UNS b ONIGONV 01 33 0 1 60 A ert 00 01 gt US Of 06 tl UNITAS 21 4 ide 4 LENA 1883 H Chart A2 65 KC 10 Landing Atch 2 84 of 101 323233 0119209 H21Vd 006 700 0055 0005 oosa 0002 0051 1001 00G 0 pes AY Y LAG fit 7 gman E nd xd Xs hy LU wd Cats 2 C w C vw Lo Lu WO LU WB X KW Gor XU s Ct 0 ed bo eee lt
39. 5 s SN 1 0051 lt z gt gc ES ds MEE Em Nm Mm lt spunog 007206 gt AD d33is DNIINV 1 1 0 C lt In 3883 HION31 H31Vdg Chart A2 72 C 17 Heavy Weight Landing Steep Approach Atch 2 91 of 101 2393 NUIIV2U 2194 00011 00001 0006 0008 0004 0009 000 000 0006 0002 0001 0 0097 0085 T T ESS ANS SENS SSS BERR ESS E 5 ONU NN NS ANE ANE AO NE SES eS a i us rr f f LLLI NNNM RENT MX CNN ANT T AND Se Se SS d 3 s L s Eu m AZAS IN AT A IO ANN Dur LP RO S RM NR ANON MSS ANS XN Se ot UE SS 55 e Nw MS XXX NS 00 1 ZEAL SSS lt lt ete 275008 ae et eee Cee ee Eat at VT WS VS SII P arde 5 d dd rd 005 tette 0 00 0 00 8 e 525262
40. AJ d SO EAE 473 44 4 4 9 4 4 4 4 4 4 949 9 9 4 wc wow WC OO XC MCOXCOCOQ XX XXX CE VE XE ee q ox e od tor oat ue a iiia X a e S S I P e a Cae AIS 2 525055502655 ERROR RR A n Y y xw a E wc ey 001 rats e r QUE n N x 4 0 02 LN de 5252 maaan a ba 00 SE El I BE i 002 008 006 0001 lt 01 spunod 08 gt TE DONIGNV 1 3 vH ad 424 S9NI2VdS HILYd 493 HLON31 1 4 E Landing Without Chute Chart A2 13 F Atch 2 32 of 101 19235 19 HIL d 0072 0022 0002 0081 0091 DOT 0007 008 009 002 0 00 08091 vene 2 2
41. asan N ELS N T V re ee ee E pat Tm a N T P lente IEEE 5 sr p 8 aa ha LI T 1 01 0E 0S 0 06 OTI QET OST lt ad JS Feds DNIJVdS 48835 HLIDN3 1 Chart 2 52 141 A B Medium Weight Takeoff Atch 2 71 of 101 4993 NOILYIOT 2194 ogot 0055 0005 0062 0002 00S1 0001 005 0 0082 Nore 7 7 7 T T T T 7 um S A87 Ay AV LUN ERO Z 3 ss AAT TAAT AJI 27 wu R yr ur 42 a UR MS X X E aS CORO Ep e toC COGN GOL oes ES 002 O 006 M M M 9 0 MI a Som eC oc on ge my M MC Ue E n aic ao a
42. t Tat Pa Tg E SAIS 5 RASS ess PE I UBF 0096 WSS s APA Ap AA Pie Pee IT HLI SEER CAA NS Ne NN NN NS T LT LT L3 LT MANI lt p 22209 rz lf A LE Tsm EN i VS ANN Xxx 3 IE LLC VV ALG VA 3 E lla bb 6 b LRL 2555652 52525505 5 25 5252525252 ob ob q rer 55500 Xs 1 scie eie ta Ne att NOM XM X NOH e S atari 086746 oe 036300 aal Pat w A 55 E rA UT Dm X GS E X 2 ate UE w w NONO Sane Wess sss 554 I 2 ee ar u ua m a 3 4303 91 1 2 Vi 1 60 000 Se0 DET 061 lt 39235 ONI2V
43. Name Name of the resource Propert Figure A1 3 Properties Tool Group Atch 1 3 of 30 1 2 4 Layer Manager Layer Manager displays currently loaded data GeoExPT required layers are grayed out and cannot be removed The standard Esri layer management tools are available by double clicking the layer name Selectable Layer Non selectable Layer perl Def Quy Inm Plum Tee Popup n ize m9 9 nn communicati n fiber 1 communicatio ns cor ductb An compressed air pepe wwe Crede 5 9 1 7 9 e 9 e e conduit centerline ctrical ca amp electrical du a Fuel line 4 heat cool hr natural gat storm sewe I wastewater water hne d gt surf 8 we e 4 tos can the range of scies W weh thet vd be dew Show wre Dant laper mien Qat tevoret Nore I Figure A1 4 Layer Manager A1 3 Scenario Settings 1 3 1 Airfield Damage Folder This 15 a system folder containing airfield damage shapefiles These files are generated from external sources such as RADAS More details on using these files is in paragraph A1 6 3 3 Checking the Enable Airfield Damage Monitoring turns a simple folder
44. the lowest value intersection on a boundary line between two regions in the uncorrected RQC or correction factor areas must be treated as though it falls in the region with the lowest value A2 6 3 2 Finding Uncorrected RQC Atch 2 15 of 101 2 6 3 2 1 Draw horizontal line across the DR section corresponding to the DR recorded on Worksheet 1 If there is or RSC section draw a horizontal line across that section corresponding to the RCR or RSC recorded on Worksheet 1 A2 6 3 2 2 Draw vertical lines from the patch locations on the location baseline until they intersect with the current DR A2 6 3 2 3 From each intersection follow the guidelines to the top of the DR section Stay between the guidelines in proportion to the starting location A2 6 2 3 4 From the top of the DR section draw a vertical line until it Intersects with the current RCR or RSC then follow the guidelines to the top of that section From this point draw a vertical line to the top of the chart A2 6 2 3 5 If there is or RSC section draw a vertical line from the top of the DR section to the top of the RQC chart A2 6 2 3 6 Draw a horizontal line from each repair patch spacing on the vertical axis to the uncorrected area Continue each line until it intersects the vertical line for that patch A2 6 2 3 7 intersections in the various regions of the uncorrected RQC area The number in each re
45. 993 ONIJVdS 219 993 19 31 H21Vd Chart 2 23 15 C D Landing Arrestment Atch 2 42 of 101 994 119007 2194 OOET O0eT OTT 0001 006 008 G el SeOl i ede dede bab ub odd e Bede ddr de dd dde Poo Mate EEEIEE F Tafa A ITI eee 2 Miao a TATA I RE ETEN WNW 555 TAN tut EC MORD UE F ant S SSS AIO E 004 009 006 00 008 002 001 gt ii dt gt 3 4 SS lt ad 493 DNIOVdS 29235 Chart A2 24 F 15 C D Evacuation Atch 2 43 of 101 GW lt 72 871 Pounds 11 15 TAKEOFF m x a w d od d ue e rete C uode dco LOC a oc x CX M De M LO 55 N 550 M Ad eM ii die 5 ata x NN 6 42 4 e A aie x5 ut x te os X Se i EA de V x s 12 CX ata ut qe v ose ode ded de 252565555
46. MGRS Damage i C382MB28 5981935D1 z Reported By Imported Damage itr Feature Type of Feature POLYGON General Allocation Placed Crater Imported 4 Layer Utility Damage List any utilities intersected by the crater La Properties MEO Figure A1 24 Intersecting Water Line A1 6 3 5 Damage Repair Actions The Airfield Damage Repair dialog can be launched by right clicking a damage item in the TOC and selecting Repair selecting either Permanent or Cleared will remove the item from the map other selections change the features symbologies a Airfield Damage Repair 2 Airfield Damage Repair Base Repair Material Wrepareo Base Repair Material Expedient Cleared Cap Repair Material Permanent Cap Repair Material Verified Sorties Verified Sorties Actual RQC ROC 0 Inspection Date 11 18 2011 Inspection Date 11 1872011 Repair Date 11 18 2011 Repair Date 11 18 2011 8 Figure A1 25 Damage Repair Actions Atch 1 19 of 30 1 6 4 Add Minimum Operating Surface MOS Minimum Airfield Operating Surface MAOS A1 6 4 1 MAOS MOS candidates are added to the scenario by either right clicking the appropriate runway and selecting Add MOS right clicking an existing MOS in the TOC and selecting Duplicate or by highlighting the appropriate runway and selecting Add MOS from the Tools Tool Group The wizard steps through the criteria to d
47. Record these patch lengths on Worksheet 2 A2 6 2 6 Measure in the direction of operation the distance in feet from the center of each patch to the center of the next patch If there is not a next patch Atch 2 13 of 101 1 the patch is the last one use the maximum value on the spacing axis of the chart Record these repair patch spacings on Worksheet 2 A2 6 2 7 Mark the repair patch locations lengths and spacings on the RQC charts If the value for any length or spacing is greater than the maximum or less than the minimum shown on the RQC chart mark the maximum or minimum E 25 g I ME S I CHRR 3838 lt Skee 9 j 5655 E 9 i of i OPERATION THRESHOLD L JL 8c 4 Figure A2 5 TOL Map Atch 2 14 of 101 WORKSHEET was THRESHOLD reer 3000 DEPARTURE END ix 7980 oa HEEE PATCH LOCATION LENGTH SPACING I FEET FEET 4535 130 Im C Cn uc n 83 A Figure A2 6 Worksheet 2 Example A2 6 3 Finding Repair Quality Criteria RQC A2 6 3 1 Incorrect RQC can result in aircraft damage that may cause death Uncertainty of any value uncorrected or correction factor shall be resolved by using the most conservative value 1
48. a i A e e LE ee i Fr Lad L j _ sg TIT TT LLLLILLLLIILILLLTLLLS E E 11 IS T T m c 40 30 20 10 0 10 20 30 40 20 60 50 TEMPERATURE C Chart A2 1 Density Ratio Atch 2 20 of 101 dee TOW HOS lea mai GO MS ML SOM Mj UN3 WS 35H SOM msi 3 1 SDM HOW ONJ MON 3 1 SUM N3 SOM HO 0 3 HOA CHS SD bend 3S0042 NOLL 4320 NOLL 7912345 350062 332 NOLL vasd0 Oliva ALISN3Q Dp m 132 Cdo 4 Chart 2 2 Worksheet 1 Atch 2 21 of 101 Lo emm 8 m amp UNCORRECTED CORREC m RQ CHART d 5 85 i 4 1 Chart 2 3 Worksheet 2 Atch 2 22 of 101 Gi pi EI 2194 Et ol OL L d 21 4 0 50
49. would work together until all the FOD is removed from the MOS At this time GeoExPT assumes all repair teams will start repairs at the same time with an additional assumption that they will start at different locations on the MOS This method will provide the greatest flexibility in team scheduling to be discussed further in paragraph A1 6 5 5 NOTE The tactics techniques and procedures TTP for the aforementioned repair methods are being developed modified by AFCEC CX The GeoExPT time accounting is therefore still a work in progress and the reported time estimates are not 10096 accurate However they are representative and adequate to support comparative decisions when selecting the MAOS MOS candidates Atch 1 21 of 30 Damage Repair Teams designate the available repair teams The Environment applies appropriate time multipliers to the repair time estimates The Crater Repair Zone Size details the area where each repair team will concentrate their efforts only applicable for the Concurrent method The Silver Flag Training options apply time multipliers to the repair time estimates based on team training The Default Repair Material is the default crater repair method for the MAOS and MOS Aircraft Operations W51 Options ADR Routing Repair Methodology Concurrent Time assesment and scheduling based on zones Sequential Time assesmentand scheduling based on linear repairs MOS Base Flowable Fill
50. 0 DORE t E No e CM HHH H 2 S Z HE QAYNA SS M RS SES NS ANN EA _ SPSS SANS SS Sa Ses O HIH s sss s sss DN See SEES SEES SSS SSS EE GSS 706 SESS pun __ t ed ER ul alt Wai Mah dag dei 1 i N a A wS NEA Nate ete state SCE de ae gt S 9 Sn 5550 en t at OF NO o Or OX CEES ORC COE AN x ES ee Wii Ww tt OUR UR tt ama At 224 atte 0000004000 Mt oO ox ERRA 5 52522545050550 0 040 Rise 24 525 5 595250552509 STA a CO Pes a niata ata TAN CAES
51. 1 2192 e td Xx IS GG EEFERUT cde ce c NR I RT ee cee XU XC KO he SO TW XX VNDE TENIS E X X C C COR Re he POCO LOCOS ACE OR sS ede ete 22505245506 VERNIS NUNNA NNN Ws SSSSS 0006 0008 000 0009 0005 0002 0005 0002 NNNNA Run CRT SSS WIN SSE 0001 0 SAWN sss anann AN 109 LAX NAN NN d 133H 0 261 3 TI TTT A 13 001 OOF lt ej JM 4993 SNIOVdS 194 493 31 2194 Chart 2 22 15 C D Landing Wheel Braking Atch 2 41 of 101 993 NOILYIOT H319d ee 0002 0081 0091 OFT 00 1 0001 008 009 00 00 0 622 82189494 0621 28880089 Ce S 5 lt nn a 5 NN 5 lt RF SS SR ux SSS 00 WWW NANA ANN lt _ 2 1 O I3AU T1V 41934 005 008 004 4 ad
52. 2 44 111 Landing Atch 2 63 of 101 005 000 0055 005F _ Pere NT ya 455 5250550 NOS he a 5521 NN L SPS i W x uus x 59 spunog 66 18 gt AD 2222 ZzZZ Ti 293 NOILVIOT 2194 000 0052 0002 0061 0001 005 0 y yif ZZ X X mM E Cm m E I X X X x wW a a a a a a a a aa a eee ELSE p ww c 000 30 30030 ORO OE m era 22252552505 x e OX AR SEAR aa Xm ccm m c X mam UNE NL UNE mam Yami uds mus mama mam ns amana usa una WANS m man mi wana wansi wanni ilis Ss OUI 002 00 OOF 005 009 QU 008 006 0001 lt gt ad HJiVd 993 DNIJVdS H3J1 Vd 4994 HIDN3I Chart A2 45 F 111 A E Evacuation Atch 2 64 of 101 9932 NOILYIOT HILYd 000 7 00051 00081 00011 00007 0006 0008 et aay at e A 5 enn E s m SSS SSSR w spunog 00069 gt AB E
53. 28 Di 29 F 16 AB BLOCK 02 ao ons pg Laning Amesmen L ar D4 Evacuaion 09 a F 16 CID BLOCK De 34 253032 DZ Landing Arrestmem 35 _ Evacuation Do y 3 F 16 C D BLOCK 010 3 _ 042 Dil landmg Amesmem 39 Atch 2 9 of 101 Table 2 2 Chart Figure Number a EP landing FAMAE andmg ShotFeld 43 _ E4 landmg Amesmen 4 _ pes evacuation 48 e Ep lang a med ee taig a49 cast AB HEAVY Hi Heavy Weg Takeoll 5 _ C141 AB MEDIUM Medium Weight Takeo 52 L Medium eightLanding 5 _ Tae _ M mede pen E lani 8 Li T heavy Weight Taket o KC 135R 12 Normal Weight Takeo 6t _ 13 handing 6 _ Mt T heavy Weight Takeo 68 NomalWeghtTakeof 64 Ls 6 _ Ni Heavy Weight Takeo 6 _ w Normal Weight 67 _ aim 01 ge e Heavy Weight Takeo 7 _ O Heavy Weight Landing Steep a Approach EI suu a Approach 74 Atch 2 10 of 101 Q Table 2 2 Chart Figure Number P2 P3 5 Normal Weight Landing Chute 79 P Normal Weight Landing Chute 80 _ cM OM LX A2 4 4 Finding Operational Lengths
54. 4 If DR is unavailable record the temperature and pressure altitude Using DR 112 1 1 3 Operation takeoff landing or evacuation EE EI Chart draw a vertical line from the temperature axis until it intersects with the pressure altitude then draw a horizontal line to the DR axis Record the DR on Worksheet 1 Record the RSC 0 0 1 0 for C 5 or C 141 aircraft 0 0 10 0 for 130 aircraft Record the RCR dry wet or icy Atch 2 3 of 101 Table 2 1 Instructional Guidelines 1 2 If there is an RCR or RSC section draw a horizontal line corresponding to the current RCR or RSC across that section 1 3 From the intersection of the DR line and the shaded section draw a vertical line to the bottom of the RCR or RSC section Then follow the guideline until the line intersects with the correct RCR or RSC From this intersection draw a vertical line down to the location baseline and read the operational length Hecord the length on Worksheet 1 If there is no RCR or RSC section locate the intersection of the DR line with the shaded section From this point draw a vertical line down to the location baseline and read the operational length Record the length on Worksheet 1 3 1 Draw lines perpendicular to the sides of the MOS at the beginning and end of each crater on the MOS Shade the area between the lines for each crater If two shaded areas are within 25 feet of each other shade the ar
55. 993 NOILVIOT 2194 00 2 0002 0081 0091 0021 0001 008 009 00 002 0 4314498 0621 Te q x 2 E T c 1 a T q x m mo Ww uw v EP e MACC OC C D C e E e e ss 3 SOP 0 s E M48 88 6 04 2 878 statuta 001 BOOK OOOO IK ial 55 CR 5256 TANNY 03 SIV 2 009 DN e N 006 0001 lt 01 gt 06 Of 06 OST lt spunod EBP EG gt 415348 351 3 ad 1383 ONTDVdS HOlVd 42883 HION31 21 Chart A2 27 F 15 E Landing Arrestment Atch 2 46 of 101 993 40119207 21 94 9002 0081 0091 Oe 0001 008 009 00 002 0 0502 019 mee a gt 2 7 27 7 v I EE T LL a OO 3 2 29 Qd ECC X uA M M UA 0 aate deor yC N OR M DC XXX E ES a a LOCO 2525940 HIE EMI 55550 001 ROS RC OLX Seer eee
56. A1 4 2 Zoom to Feature Right clicking features in the TOC enables Zoom to Feature es and Pan to Feature Atch 1 5 of 30 It has no effect when manually plotting BIAP Master Add Prioribze Damage 4 Edit Shape p Select Features E to Selection m Man FD Selectii Pan to Faatura E Table of Contents 25 25 ES ES 5 t crease Iecresse X Delete Figure A1 6 Zoom to Feature A1 4 3 Finding a Feature Right clicking over a map feature regardless of what tool is selected and selecting Show Hesources will show a list of all features occupying that location Selecting the feature of interest will highlight the feature in the TOC Figure A1 7 Show Resources 1 4 4 Data Frame Rotation with all geographic information system GIS applications map data is defaulted with North being up While placing assets it may be easier to rotate the data frame than rotate each feature as it is placed Selecting the Rotate Data Frame from the Edit Tool Group rotates the data frame Atch 1 6 of 30 Holding down the A key enables the user to enter rotation angle Selecting Clear Map Rotation po on the Edit Tool Group returns the map orientation to North being up A1 4 5 Map Views A1 4 5 1 Bookmarks are a method to save a current view extent to quickly return to Selectin
57. CUNT UT LN Aa ood ge tette LOLOLO LOLOL a a TIED 005 nana M eee se taa uto S AE ANN MG GEE SS SIS SESS MA www wk ERROR E 002 008 0001 lt gt 06 0 oz 06 O11 OST lt ne SNITNV1 WnIT34 8 VIPT 2 aoa ONIJVdS 2194 993 19 21 HJ1Vd ht Landing Chart A2 53 C 141 A B Medium Weig Atch 2 72 of 101 993 NDILVOD 19 000 0009 0005 000 0008 0002 00DT 068 008 ihr se RC LP Lr nr ur We Rr Wu ce da Cas CA hs aM CLP Tor s LP EDEN CURT GE RT RC URL ee CHR at 4 9 49 e etel ete e eli Y z k ht intet 001 E 7070 0 0 4 4 9 9 9 S 5252525252 EEE 222 i OT eee 00 KAA atate tens PE lt I niger RW 2 SSS S y NN oL pL op o eese aa a 00 NE on _ 00F 005 009 Peake PB 00029 AD 43039141 04 9 ad taap ONIDVdS HOL d 993 HLONS 1 HOLVd Chart A2 54 A7 D Takeoff Atch 2 73 of 101 I 909 NOILYIOT H3193 00001 0006 0008 0004 0009 00
58. E EEO EEO OE OE UE ES leto 5 25 5 55 k CAD Hate a a etat w e Seda ade 20 X Ses dt 009 EEE eee NA L TI OTI P spunod 86 92 gt AD NDOILIVOVA3 OL HD SI 4 OST lt 4393 ONIJVdS HOIVd 993 H1DN31 HILYA ion F 16 A B Block 10 and 15 Evacuat Chart A2 32 Atch 2 51 of 101 293 19001 000 0055 000 0052 0002 0061 0001 005 0 00 cc2 2 37 22 wv viu 2225 e pem yy ae NOI oe 1 S l 0 001 00 O ROX mE CN WE sc se DW cun um k c SM EES ios n S 006 562555965905 NN QT gt OF 05 02 06 E a EE aa ENA e RN yp 55 _ E 33033891 Cat oE c2 HA 4 2 9 4 C spunogd 0 gt AD ce 009 004 008 0007 lt OST lt ad 9932 DNIDVdS 1 993 HIDN31 HILVd Chart A2 33 F 16 C D Block 25 30 32 Takeoff A
59. Planning Tool GeoExPT is not available for use The methods described in this attachment are those described in the to be rescinded TO 35E2 4 1 Repair Quality System for Rapid Runway Repair A2 2 Chart Description A2 2 1 Figure A2 1 is an example of a chart used to determine the MOS requirement for a given aircraft and aircraft operation The chart has four areas 1 the location baseline shift area 2 the environmental shift area 3 the uncorrected and 4 correction factor area 2 2 2 Location Base Line The location baseline is the starting point for calculations This area is used to determine the MOS requirement as well as mark the repair patch locations when determining the RQC requirement A2 2 3 Environmental Shift This area compensates for aircraft performance variations due to weather and runway conditions These include the Density Ratio DR the Runway Condition Reading RCR and the Runway Surface Condition RSC A2 2 4 Uncorrected RQC This area determines the initial RQC for individual repairs A2 2 5 Correction Factor This area provides RQC correction factors based on the repair location on the MOS and its proximity to other repairs Atch 2 1 of 101 6500 4 NOM w ey 4 2 GV lt 54176 E LI NN ams 2 E P RK ONA N X LN cw c LN
60. UXO Explosive ordnance which has been primed fused armed or otherwise prepared for action and which has been fired dropped launched projected or placed in such a manner as to constitute a hazard to operations installations personnel or material and remains unexploded either by malfunction or design gt Figure 4 Unexploded Background 6 1 Airfield Damage Repair encompasses all actions required to rapidly prepare airfield operating surfaces and infrastructure to establish or sustain operations at new Forward Operating Locations FOLs or recover operations at a Main Operating Base MOB Some key components of ADR are e Airfield damage assessment Locating classifying and measuring the damage camoulflet crater spall and UXO on the airfield operating surfaces Minimum Operating Strip MOS Minimum Airfield Operating Surface MAOS selection Analyzing damage and available airfield surfaces to locate the minimum pavement requirement for takeoff landing and evacuation operations and the minimum taxiway and MOS combinations to most efficiently support aircraft operations e UXO clearance Performing render safe operations on unexploded ordnance Damage repair Rapidly repairing camouflets craters and spalls e Aircraft arresting systems Installing mobile aircraft arresting systems MAAS and Mobile Runway Edge Sheaves MRES e Marking a
61. WDa 3 NOIIVAM HU NOLI23MIQ NOILVN3eU Chart A2 4 Worksheet 3 Atch 2 23 of 101 493 9901 2194 0005 005 OCOFr 0052 000E 0052 0002 00S1 0001 005 0 0015 00 ES S 3 IT FFHHE3 a 3 BS V V 7 E O E KORA OND 0 E SS ONDE n d 4 e e ee x x i oe oo 6 0 0 0 oe Seat SR EAE bis 49 479 474 9 4 4 EEE Cee 4 9 499 9199 P CACACE S ACA ACACAC ACA aca A A RN i Mi M Tie 0E GE Eg RATE Eae aa S ES arta ama w r a us TA are DC X eC D ROG OLE EEL O E E E same ira SSN S T E 2 Wo dq T T as nus E pes ME v Lope Eu E EJ OOST lt OT gt qq i 1 1L Lois da ee 084 SEE E ES ESE SSE e E hi OST lt spunog bbb G gt 43033191 2 3 V ad 449 4993 1 H21Vd Chart A2 5 F4 C D Takeoff Atch 2 24 of 101 3993 NOILYIOT 21 94 0022 000
62. baseline to intersect with the current DR Then follow the guidelines to the top of the DR section From this point draw a vertical line to intersect with the current RCR or RSC Then follow the guidelines to the top of the section From this point draw a vertical line to the top of the chart If there is no RCR or RSC section draw a vertical line from the top of the DR section to the top of the RQC chart 5 5 For each patch draw a horizontal line corresponding to the spacing for that patch until the line intersects with the vertical line from step 5 4 Determine the uncorrected from the region of the intersection and record on Worksheet 2 f the intersection falls within a shaded region a correction factor is not required 5 6 For each patch draw a horizontal line corresponding to the length of that patch until the line intersects with the vertical line from step 5 4 Determine the correction factor from the region of the intersection and record on Worksheet 2 Perform all of step 5 for each operation Pe Add the correction factor to the uncorrected RQC and record on Worksheet 2 If the result is a negative number record an F If the uncorrected RQC for a repair is FF record an F for both that patch and the patch immediately following it Calculate the RQC for each patch for each operation List each operation from the MOS threshold on the top half of Worksheet 3 7 2 List each operation from the MOS depar
63. bi Nt 0 4 222 MM cn owe o e Le xe ee e rt a au 1 00E o0 X 788 8 64797679 9 849 4 9 471 E de 2 qo e e at ua tu un a P 1 Sd d dod rd dq e mo iq de d 005 basan oes 225225220220 sh 008 006 01 0E 06 of 06 OST spunogd gt AD 33033891 gr gr AIH 0 2 9T 4 6 O00I lt ad 293 DNIOVdS 2194 993 HLONAT H21Vd 16 C D Block 40 42 Takeoff 37 F Chart A2 Atch 2 56 of 101 993 19001 HILA Pa eR a Sar 0695 WM SN SK VU E QS SNP SNP SME TT i ER TTT TT TT TT Te BORIS ZT TT TT TT TTT ot ott s us ANN qu a NN CNN MN NE NS ANT NT DEL LN PE aN uu am am a aat A N Li ss e c eu 3 3 i ra Sa _ 222 AG 13 AJI m 0 42 CX y Oe m Far p e NONE CP e 4 aa
64. ded de de 4d 4 qd d ee ee PS PU 2 SOS SS LOCUS ut e e OES 2259509 i m T E 2 2 2 Ji SNLIMS SS ROLY So LOS 3 gt 2196 gt a Chart A2 63 KC 10 Heavy Weight Takeoff Atch 2 82 of 101 3883 119201 19 0000 0006 0008 0004 0009 0005 000 0005 0002 0001 0 0065 GEF i D NEN SS NN A pus SS iR r i vetrine 7 z D p EEE EEE EN EO AA A 00001 p uu UU APP Bl AUT CAN NAR NE CAMCN NR RC C EARRA AAA AAA A oppo cp wp a v J 945 EE x 4 4 lt 2 A SS SSS 0 JS a aaj UNIOVdS 1 4 8845 HLUMJ Chart A2 64 KC 10 Nominal Weight Takeoff Atch 2 83 of 101 00001 0006 000 RN DNE MP OU RP QU AD OO RD OS RET NOV RNV RN MO T Cw Pu y y Pu Pf tg S e a Su su EE x X22652 552525 0500056 569559500 spuno 00096 gt AD B 0004 0009 000 000 0005 VOU 0 e s
65. following the directions in Attachment 2 Legacy Manual Method 7 3 The Air Force s intent is to migrate to semi automated automated MOS MAOS selection method using GeoExPT GeoExPT should replace graphical interpolation of the charts in TO 35E2 4 1 as the primary method for MOS MAOS selection upon publication of this ETL The process is faster and more accurate and integrates with other automated tools such as EOD s Tarantula Hawk remotely piloted aircraft where fielded future tools such as the Rapid Airfield Damage Assessment System RADAS and other business mission systems e g Theater Battle Management Core Systems TBMCS Units should posture to enable this capability within the EOC linked to the Civil Engineer Unified Combat Command CE UCC to enable better planning and preparation for post attack recovery 8 Repair Quality Criteria RQC calculations are only required for expedient repair methods e g crushed stone with FOD cover The new ADR repair methods 0 rapid setting concrete are considered a semi permanent repair GeoExPT makes use of the algorithms in TO 35E2 4 1 for RQC calculations 9 Point of Contact Recommendations for improvements to this are encouraged and should be furnished to the Director Readiness AFCEC CX 139 Barnes Drive ouite 1 Tyndall AFB FL 32403 5319 DSN 523 6123 commercial 850 283 6123 or email AFCEC RBC tyndall af mil DAVID L REYNOLDS Colonel USAF
66. management practices draw order stylization etc can be applied Select Add Data S from the Scenario Tool Group and navigate to the applicable data layer If you do not see the data you are looking for ensure the proper file type is selected on the left side of the dialog Add bata Lookin Chi transportation aie Shapes Belal Figure 1 12 Data Atch 1 9 of 30 1 6 Airfield Damage Repair A1 6 1 Grids Grids are required prior to placing any airfield damage Pavement Reference Marking System PRMS grids will be used to track damage on the takeoff and landing surfaces a PRMS is required for each surface The Crash Grid will track all other damage After creating the appropriate grids it is usually best to turn the layers off to simplify the map display A1 6 1 1 PRMS To create a PRMS right click the appropriate Surface or Surface Centerline if a centerline is not present you will be prompted to create one in the TOC and select Add Pavement Reference Marking System 22 The grid will be generated from threshold to departure and the width of the surface 1 Add gt 4 gt BP PavementReference Marking System e 7 l 4 Figure 1 13 Pavement Reference Marking System Atch 1 10 of 30 A1 6 1 2 Crash Grid The Crash Grid is a representation of the Military Grid Reference System MGRS To place a crash grid right click
67. on the Scenario in the TOC and select Add Crash Grid When the cursor changes to a cross hair drag a marquee box around the area of interest The grid will automatically expand to next full grid line L UT n BIAP Maste MP 1 F 15E St M Prioritize Damage aP Airfield Damage 2 eras a pa Select Feature s Route Network biiy Houseke 1 oom ta Selection L gt Houseke e Industriz Pan to Selection Surface Id Ai Zoom to Feature unis Pan to Featur gt Sets Table of Contents k Components i 77777 A 3 8 8 t f s h 1 a ms Fu Figure A1 14 Crash Grid Atch 1 11 of 30 1 6 2 Taxi Routes Entry Control Points A1 6 2 1 ECPs are not for security but designate the points of entry onto a surface Each surface must have at least one ECP to be connected to the taxi network this includes runways not the MOS Most surfaces will have more than one Add an ECP by selecting ECP ESP from the MAOS Tool Group Single click along the surface edge for the first point then single click for the second point The actual width of the ECP is not critical Figure 1 15 Creation 1 6 2 2 Route Network route network is comprised of the connecting line segments As with traditional network routes p
68. perde pue M DE m M T UN GM E RR RR V J IL s A mm INS NEN ON RON 2 ES Say HHHH SS pA TIT 5 l oe de di P a a LL o I Ed ker st f D 1 rq Ce tiger S ene E l Sd bote ot RAE Those oS Sad 260500606682 b O i lt 2 7 y x LUE UE X X XX XU SSS L SSS SSS BE SE BR in SX SB SE SE ES BN 50 Www t 00091 000 00021 00001 0008 0009 000 000 0 0005 00 6 0 AMT 13 AJI 001 002 0 DOT 005 009 008 006 0001 lt au qa 989 SNIOVdS HILVd 883 HL9N31 Chart A2 8 F 4 C D Landing Without Chute Atch 2 2 of 101 393 19201 21 94 082 0092 0072 00252 0002 0081 DOSI DOTT 0041 0001 008 009 007 00 0 0583 0081 SS SS z X 3 0
69. right click the Crash Gird areas off the runways or the appropriate Runway to launch the Airfield P Damage a dialog box It is then a matter of supplying the appropriate information The Damage Code can be entered as a string or in segments in the lower portion of the dialog Atch 1 14 of 30 Type Crater Logout Coda Crash Grid Reported By Damage Code L EPOD A Ai PENES DO EL GT EG ash edd amp G Er Code he Hehe F Add k a Damage 007 50000000000 Figure 1 19 Code 1 6 3 2 Manually Plotting Damage Digitizing Damage plotting tools located on the Damage Tool Group Damage items are automatically assigned to the appropriate grid when digitized the Team Name defaults to Digitized To digitize a bomblet field select Add Bomblet It is then a matter of drawing the polygon Upon completion a dialog pops up to select the Munitions Type This then draws the appropriate safety cordon and prompts for the Number of Bomblets To digitize camouflet select Add Camouflet First click for the center point of the penetration hole then you are prompted to provide the Diameter of the penetration Next you are prompted to provide the Blast Radius actually the expected resulting crater This is a hanging tool so unless the Add Camouflet tool is pushed again you can digitize camouflets wi
70. sniffer to notify the user when new files are added 1 3 2 Airfield Damage Archive Folder This is a system folder containing archived damage shapefiles It copies the data in the Airfield Damage Folder typically GeoExPT does not control this folder so archiving the data ensures no data loss Files are only archived if the Enable Airfield Damage Archiving is checked A1 3 3 Route Weights The Routing Weights is the criteria used when selecting the taxi routes as part of the Minimum Airfield Operating Surface MAOS High Distance looks for the shortest route while high Damage avoids the maximum amount of damage Atch 1 4 of 30 1 3 4 Factor Upheaval Factor is the multiplier applied to craters when imported into a GeoExPT scenario damage Kai General Scenario Navigation 95 General Ci Users Lance riller Desktop se Enable Airfield Damage Monitoring Airfield Damage Archive Folder C Users Lance Filler Desktop Ge 56 Enable Airfield Damage Archiving Routing Weights Distance Damage 5 Upheaval Factor 200 5napping Tolerance Figure A1 5 Scenario Settings A1 4 Useful General Tools 2 4 1 Tools standard navigation tools of Zoom In Zoom Out Pan Zoom to Full Extents and Zoom to Previous available Navigation Tool Group as well as the Quick Assess Toolbar which also includes a Flash Feature Tool
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75. 3 Atch Deputy Director 1 Geospatial Expeditionary Planning Tool GeoExPT 2 Legacy Manual Method 3 Distribution List GEOSPATIAL EXPEDITIONARY PLANNING TOOL GEOEXPT A1 1 Introduction A1 1 1 This attachment addresses only the tools necessary to create a GeoExPT scenario plot and manage airfield damage select a Minimum Operating Strip MOS and Minimum Airfield Operating Surface MAOS and print plot operations A1 1 2 The application is constantly being upgraded modified users should refer to the GeoExPT User Manual for the latest updates and procedures A1 1 3 Documentation Conventions Items in bold represent the name of GeoExPT items such as the Table of Contents or Dialog Boxes Items in italics are tool names such as Add Runway Centerline Tool icons are displayed where applicable such as Add Segment Tool A1 2 User Interface A1 2 1 Overview The GeoExPT user interface contains menus tabs toolbars and dockable panels lt 3 k gt Ribbon Tabs Table of Contents Cn N Map Display in Properties Pane Notification Panel Figure A1 1 User Interface A1 2 2 Table of Contents TOC The TOC is a tree view that enables management of all resources within a scenario As items are selected in the TOC the feature properties are displayed in the Properties Pane Right clicking features Atch 1 1 of 30 the enables applicable tools only some of th
76. 493 31 Chart A2 15 F 15 A B Takeoff Atch 2 34 of 101 38835 NDIILVOU 2194 0008 0006 0009 0005 000 000 0002 0001 0 0075 109 ee Pe PAPA YUU ARRAN GME ae alee aiia NUI SKIES rr TI ZZ ZS 2 RUPEE ZZ AA AU A AVAV AV AW AW INE UN 00 F G Al k 21 0 x X m b x i OUT eR ER ED RN Mann N 7 002 NE RRL 00 3 gt SN SA iG s S Sets sak Wika aan summe kN A I NN 01 gt 0 0 04 06 OST lt _ spunod gt AD 94 0939 amp S WVSI 4 J ad ady Atch 2 35 of 101 4244 9 12945 2194 16 F 15 Landing Aerobraking 2 44953 HION31 2194 00011 00001 00 DOZTI de dodi
77. 5 ms E E Pia Ph F Pa T X sue sss asss ee 5 alates OS SEE OC ORO a a saus uud s m m ae oa ey P 4 se hee icd DXX CERE SQ ML VE F x y ss rw k jt 525 P p C bb d d d dd d d d dd d d dd d diri dd ded dd ttt t 5552560 tete atat areae Kanan SNNT em e 2229 e X 7 50520 eas ARAS SS een tieu Ea ttt o MOI MH NO CS ERE MODE d D ORO EODD DOOR LOO ORO OCC GC ORO MS A aU E CORO EEEE EEE EEEE E E RRRS t 5 2 SES seen EATA a s 22 NS S lt NS 3 spunod 000586 AD WOVOMddv 1 5 HI o l 60 A al 13 AJI 002 OOF 009 008 0001 0021 OOF 0091 0081 000 OI 05 05 Z 06 OTI 051 051 lt ad 424 28235 45 3443 H1DN31 Chart 2 73 17 Heavy Weight Landing Normal Approach Atch 2 92 101 1282835 NDIIVOD 219 00001 0006 0008 000 0009 0005 000 000 0002 0001
78. 6 gt AD 9NIGNV1 LHOISM JVNINUN 1 3 01 Ol OST lt dle Joes DNIOVdS HOJlIVd 993 19 31 Chute ing inal Weight Landi F 117 Nom Chart A2 80 Atch 2 99 of 101 199845 NOILVIO H31Vd 000r 1 00021 00001 0008 0009 000 0002 0 AE A pl fs f RL Of SS gt RS ate LI E Ec atta Matte DO E oa ain gales EEOC Fio a h u 55560 atetetctatstatatateletitatatatetel itatetatatel stetatatats E OR RI II ELLE gt RE OC X XIX X OX OX X ado E RA E AS I peres ipse eme mni spunod 00009 gt 9 ON 9 0 1
79. 6 3 5 4 Patch numbering patch lengths remain constant Remember the operation threshold is now at the departure end 2 6 3 5 5 The final for each patch is the lowest calculated for all the operations intersecting that patch Atch 2 19 of 101 2 7 Blank Charts For Reproduction I I belt T e dE HH E pt II I J III II L IT FF i HN l III L l ll lI III PI TT es 1 1 IN ee L L L I I F B E E E E E r7 DILYa ALISN3T Se iS TIT T l ul LI U a L F TI T LL T ee 7 TFT T I lI l i ty L K SSE L T LI II TI I II E I T P EE ee a a a LLL TILT J 7 50 08 8 0 eu L gx CO
80. OILVIOT 2194 0022 0004 0081 0091 0007 008 ailaavd 0521 wo ow T Mote Ka LI TESS SERE MAN 3ADTIV 5419434 009 00 leo Se XIX M 906 auta tates aa ama re Ss D 002 lt 9989 45 H31Vd 1 Arrestment Chart 2 11 F 4 E Landing Atch 2 30 of 101 OEI OST lt I spunog 88 pb gt IN3WIS3eHBNV 3 3 taag H15N371 00 4 93 NULLYIU 1 H31Vd DOcT 0000 00207 0006 0008 0002 0009 0005 000 GOCE 0002 oont 009 SS AS ZL7 V Y 22222 1 E RSS DEES V f L JPLZLI Ty IE mee ut Kcd Se P 2 d dd O B obli b d ED E BO ILO E ood of Cat CEU CIR UNT WW UR e egi pl gh ie a og a i egi e te te ae fc SES 41 T ten a oS o Pate EU EE CEE a atat
81. SSG So TRES A BRRR RRR NNN NT mom SST seek DOC Dr ees OON ID NS SW SS ce pi 008 006 09001 GT gt 05 OS 0 06 Spend feces erm NOILYNIYA v3 J 1 OST lt ad 394 DNIOVdS HOLVd 293 HIDN31 H21Vd Chart A2 40 F 16 C D Block 40 42 Evacuation Atch 2 59 of 101 993 40149307 21 4 0009 0055 000 0052 000 0056 0006 005 000 0051 0001 005 0 0009 SLB8E SEE omer PS xs ETT Se e s 7 F eaten Mode d ode Wane eee eee JE x ME een eee hehe hee lt lt Ne S C M Li ls UB ine 22 Z 755 Z 9 s Z T Ye m ZAZA n alate ah CE 4 Hi 2 et spunog 00626 gt AD 43039191 3 WITTI ata 4294 ONIJVdS 2194 282843 H1DN31 Chart A2 41 F 111 A E Takeoff Atch 2 60 of 101 4993 NOILVIO 219 00001 0006 0008 Q00 0009 0006 000 0005 0002 0001 0 0009 DY 772 4 5 67 7 AD AV AV AV gt i m EE 1 ao
82. a JUS n A an S RUN UK OC OK UM X N A Race 00 loce nene stata 00 m eol dod dd odd d ird d iod ded d d d d P rd d a NAE E SEER ENE NENNEN NNN ep 00S 109 00 008 006 0001 lt OT gt 05 OL 06 spunog GOE 2 gt AD OST lt 434 2932 JNIJVdS HOIVd 993 HION31 H21Vd ing 16 C D Block 40 42 Landi Chart A2 38 F Atch 2 57 of 101 993 H31Vd 902 000 0081 0091 OFT 0021 0001 008 009 00 002 0 3314494 UST 3AD TIV E SAAN SSS ESS SS 41993 NAGI OT gt t 05 0 06 OEI 110 62457 34 eC at 883 gt ONIDWdS aa HIDN31 HOL d F 16 C D Block 40 42 Landing Arrestment Chart A2 39 Atch 2 58 of 101 Feed 9001 0002 0081 0091 0021 0001 008 009 00 002 0 00 OSET gt gt e a gt S S OO SS y 7 777 3 Dx Cbs la tert 0 555545656 ma PATE LL Um mp WOW Ng rode e SP N 001 5505925 L di V il V an T n ZI Pl ul d i al nd e a RAK ORR Bee ann eass o N 552505056 SE UNS S a e ate v 2 z s ets
83. arrier option is only available if the MOS is Bi Directional Making changes on this panel affects the repair time estimates more on this to follow Atch 1 20 of 30 Aircraft WS1 5 ADR Routing Um Direcbonal 1st Barrier s 5rDirecbonal From MOS Threshold Leveling Required Deadman Required None Hard DCP gt 40 Marking Marking amp Panting 2nd Barrier None PAPI AF Lighbng amp PAPI Figure A1 27 Add MOS Options A1 6 4 4 Add MOS ADR This tab has the greatest impact on the 5 5 repair time calculations Other than the Repair Methodology the options that apply various time multipliers are fairly generic Concurrent time assessment and scheduling based on zones method is based on a repair team consisting of FOD Removal Upheaval Removal Saw Cutting Excavation Backfilling and Capping teams working in a single crater field before moving to the next This method is commonly known as the leap frog method For example if there were five repair teams and six crater fields the first team finishing their repairs would leap frog to the sixth area At this time GeoExPT assumes all repair teams will start repairs at the same time Sequential time assessment and scheduling based on linear repairs method is based on individual sub teams working from one end of the MOS to the other For example if there were five repair teams then all five FOD removal teams
84. ation Atch 1 25 of 30 i IL ann Wired 9 9 335 4 Figure A1 33 ADR Wizard ADR Wizard A1 6 5 3 ADR Wizard Select MOS Candidate This panel presents a dashboard style summation of the candidates The first column Estimated Repair Time is the total time to repair the MAOS It is color coded based on an eight hour repair requirement If the time is less than eight hours the box is highlighted GREEN if it exceeds eight hours it is RED The Operation column summarizes the MAOS criteria If the LoR is achieved the box is highlighted GREEN if not itis RED The Damage Summation column is just that a summation of the intersecting damage At this point there is no distinction between actual or estimated damage since it would all be repaired and must be accounted for in the time estimations The remaining information details the repair time estimates for each repair team The Crater Repair MOS and Crater Repair Apron Taxi is also color coded based on an overall time of 4 5 hours Select the radio button next to the final candidate Atch 1 26 of 30 B rima POF Cand uama Fe Fert bus m mk aa Cte mM 9 Z Dum pri Figure A1 34 ADR Wizard Choose the MOS Candidate for Finalization A1 6 5 4 ADR Wizard Repair Materials per Zone This panel
85. ction factor results in negative number the for that repair patch is A2 6 3 4 4 Record the RQC values on Worksheet 2 and in the spaced proved on Worksheet 3 Figure 2 7 Atch 2 17 of 101 PATCH 13 PATCH 14 PATCH I gt 11 PATCH 10 19 3 3 PATCH PATCH PATCH FATIH 2 PATCH PATCH PATCH FATEH PATCH PATH PATCH pe sa I PATCH PATCH 5 4 4 3 FROM MOS THRESHOLD PATCH PATCH e i r ai u F TION DIRECTION ERATION DIRECTION FROM DEPARTURE Fr ie la F z E LI i E d i amp LE ba i 1 Li B Li Figure A2 7 Worksheet 3 Example A2 6 3 5 Additional Operations A2 6 3 5 1 Repair patch locations and spacing are a function of operating direction RQC values must be found for each operation in each required direction A2 6 3 5 2 Repeat the instruction for paragraph A2 6 2 for every operation in the same direction Patch numbering and patch spacing remain constant A2 6 3 5 3 f bidirectional operations are required repeat the instructions for paragraph A2 6 2 for each operation in the opposite direction Atch 2 18 of 101 2
86. dS 2194 25 HILVd 8835 H1DN31 ight Takeoff We ina 71 C 17 Nom Chart A2 Atch 2 90 of 101 993 NOILYOO 0008 0004 0009 0005 000 000 0002 0001 0 0085 0025 a NOV Y NOLO ACA PN DEN IE NN N S AAHH ASSESS S s mec USES 5 pope x ON SSSR l Z aa Z E LIA 42 3 lt z PER RRR 050505 saa E R NN 5 255552 555 600650 00 _ 555555552220 wx ur up e a 2 WIS lt o Res Ae AS GG atate afa ata tatit 55505 OO CE MR 5554 OOS Dem SR lt 55954 AA MAT See trt reae CERTA 6424 S SOS QE LOSS E AA 009 Ne 1810167 ote Seen MS 3 o ag ataata Ea xh tate s 0 T rr aerei oS NS 002 P ses NN S N RSS EEN WS SS 006 6 WI SSH SSSSSSSSS gt NN Ctt ttt ttt NS Stt Stt 0001 O OO AIAG AC 0021
87. der 2 trans_133213 FrameGrab shp e pcm meom ra 11 AM C Documents and Settings geoexpt user Desktop RADAS 2 trans_133448_FrameGrab shp C Documents and Settings gecexpt user Desktop Figure A1 20 Damage File Notification If you used the Notification Balloon the files will be populated the Shapefile area you then can check the files you want to import You can also manually navigate to the files by selecting the Browse button The tool does several things behind the scenes First it ensures the damage items are converted to the appropriate shape craters and camouflets to normalized circles and UXOs to points It then parses the data to the appropriate GeoExPT feature classes Lastly it performs archiving if selected in the Settings Additional geoprocessing is done by selecting the appropriate criteria Items changed in this dialog overrule default values The Crater Upheaval is the amount of compensation added to the actual crater size for analysis The UXO Operational Radius is the explosive safety cordon distance for an un typed UXO The Spall Depth and Diameter provide default spall values The Camouflet Operational Radius is the explosive safety cordon associated with the camouflet The Crater Diameter is the expected damage size and the Penetration Diameter is the size of the puncture hole Atch 1 16 of 30 When the Estimate Damage box is checked GeoExPT will build craterfields to
88. e Document AFDD 1 2 Air Force Glossary but are common to the engineering community as a whole APPROVED FOR PUBLIC RELEASE DISTRIBUTION UNLIMITED ADR AFDD AFPD ATO BEEF DR GeoExPT EALS ECP EOD ETL FOD FOL GIS kg Kip LoR MAAS MAJCOM MAOS MGRS MOB MOS MRES NAVAID PRMS psi RADAS RCR RED HORSE RSC SPRO TBMCS TOC TOL TTP UFC UXO WOC Airfield Damage Repair Air Force Civil Engineer Center Air Force Doctrine Document Air Force Instruction Air Force Manual Air Force Pamphlet Air Force Policy Directive Air Tasking Order Base Engineer Emergency Force Civil Engineer Unified Combat Command Community of Practice Density Ratio Geospatial Expeditionary Planning Tool Emergency Airfield Lighting System Entry Control Point Emergency Operations Center Explosive Ordnance Disposal Engineering Technical Letter foreign object damage Forward Operating Location Geographic Information System kilogram kilo pound level of repair Mobile Aircraft Arresting System major command Minimum Airfield Operating Surface Military Grid Reference System Main Operating Base Minimum Operating Strip Mobile Runway Edge Sheave Navigational Aid Pavement Reference Marking System pounds per square inch Rapid Airfield Damage Assessment System Runway Condition Reading Rapid Engineer Deployable Heavy Operational Repair Squadron Engine
89. e tools can be found on the Ribbon t is best to filter the TOC display based on the operations being performed Unibet Set 550 Perton Harvest Didier Fuel 12002 0 Ervirenmerntal Uret EC Generator 50k 0 2 0 Power Plant ESC PDC SDC Prenary Cable Sheds D of 2 Remote Aree RAL See 3 Secondary Distribution Center oF houte D ampi Ramp 2 1 Runway 1 gt 1 gt Runway 1ECP 3 D Runway 1 PCP 4 gt Suis 1 5 Rutreay 2 TOC Filter gt TOL a ar Figure 1 2 Table of Contents Atch 1 2 of 30 A1 2 3 Properties Tool Group GeoExPT does not expose the standard feature attribute table The Properties Tool Group displays the properties for resources selected in the TOC some information is read only and grayed out Reminder When in doubt look for information in the Properties Tool Group For example when changing the aircraft parking angle look in the Properties Tool Group not in the AutoPark dialog B Aircraft Jet Blast Lengt 152 Parking Angle 0 Parking Order 1 Buffers turcratt Stando False Jet Blast False 5 General Quantity 1 Service USAF Ej Munitions Net Explosive 1 0 Fl Wingtip Clearances certerime 9 Interior t Parked 3 9
90. ea between them From the MOS threshold number each shaded area as a patch Draw double lines perpendicular to the sides of the MOS marking the operation threshold and operation length For each patch within the two sets of double lines record the operation number EE and patch number on Worksheet 2 for Operations 2 Patch 3 enter 23 4 3 For each patch measure the distance from the operation threshold to the center of the patch and record the Patch Location on Worksheet 2 If the distance is greater than the operation length record the operation length Measure the length of each patch and record on Worksheet 2 4 5 For each patch measure the distance from the center of the patch to the center of the next patch in the operation direction and record this distance as Patch Spacing on Worksheet 2 For the last patch record the maximum spacing value from the RQC chart Repeat all of step 4 for each operation using the MOS Mark the location of each patch on the location baseline Mark the spacing and length for each patch on their respective axes 5 3 Draw a horizontal line corresponding to the current DR across the section If there is an RCR or RSC section draw a horizontal line corresponding to the current RCR or RSC across that section Atch 2 4 of 101 Table 2 1 Instructional Guidelines 5 4 For each patch draw a vertical line from the location
91. enables you to tailor the repair materials per repair team Because we used the Concurrent Repair Method there is only one repair zone per surface However if the Sequential Repair Method was chosen each could be tailored Realize this does affect the total repair time estimate but does not dynamically update the graphic on this panel More about time estimations follows in paragraph A1 6 5 5 Figure A1 35 ADR Wizard Repair Materials per Zone Atch 1 2 of 30 1 6 5 5 ADR Wizard Timeline The panel is work progress Ideally it will replicate the capabilities in MS Project providing the opportunity to realize as many time saving opportunities as possible Howeve r the implement plug in has limited capabilities The data can be printed by selecting Print and exported to Excel by selecting Export Selecting ADR Repair Options Eel launches the Add MOS ADR Tab Changing criteria in this tab has an immediate effect on the timeline Figure A1 36 ADR Wizard Timeline A1 6 5 6 ADR Wizard Summary This final panel is again a summation of the MAOS MOS candidate Selecting Back Back allows going back to tweak any portion of the Wizard Selecting Finish prompts that all other candidates on that surface will be erased and launches the Airfield Damage Repair ADR Report dialog Atch 1 28 of 30 1 Figure 1 37 Wizard Summa
92. ere are no reutable surfaces in this scemanao Routing is disabled Figure A1 311 MOS Warnings Atch 1 24 of 30 After MAOS is placed as candidate or as finalized selection additional taxi routes can be added by right clicking the MOS candidate in the TOC and selecting Add gt Secondary Routes Ta Although these additional routes are not included in the overall MOS scores details are provided in the TOC and Properties Pane on the intersecting damage MOS 1 0 0 44f MOS 2 2739 60 4 Ai Routes E Departure Route 430 5 m Threshold Route 839 a gg A13 Routes E Departure Route 419 5 i Threshold Route 564 5 GPR Figure A1 32 Additional MAOS Routes A1 6 5 ADR Wizard A1 6 5 1 Once multiple MAOS MOS candidates are placed on a single or multiple surfaces it is time to select the final candidate A wizard had been created to step through this process If you know the candidate you would like as the final right click the item in the TOC and select Accept MOS v This will launch the ADR Wizard but starts at panel 3 Repair Materials per Zone to be discussed paragraph A1 6 5 2 Selecting the ADH Wizard on the ADR Tab launches the wizard A1 6 5 2 ADR Wizard The panel provides a summary of the MAOS MOS candidates grouped by surface Select which candidates you would like to include in the MAOS brief by checking the appropriate box Typically three candidates are presented for consider
93. ers Repair Quality Criteria Runway Surface Condition oemi prepared Runway Operations Theater Battle Management Core Systems Table of Contents takeoff or landing tactics techniques and procedures Unified Facilities Criteria unexploded ordnance Wing Operations Center 5 Definitions 5 1 Actual Crater Diameter diameter across the crater after heaved pavement has been removed in other words the actual size of the required repair In most cases the actual crater diameter is significantly larger than the apparent diameter 5 2 Apparent Crater Diameter The visible diameter of the crater inside edge to inside edge at the original surface level prior to debris being removed In actual practice this can be measured from pavement edge to pavement edge Apparent diameter is the information forwarded to the Emergency Operations Center EOC by the damage assessment teams 5 3 Apron Hamp defined area on an airfield intended to accommodate aircraft for the purposes of loading or unloading passengers or cargo refueling parking or maintenance 5 4 Bomblet Field cluster of sub munitions within a defined area 5 5 Camouflet Craters with relatively small apparent diameters but deep penetration and subsurface voids created by the munition puncturing through the pavement surface and exploding in the base material Munitions that penetrate the surface but do not explode are treated as a camouflet Figure 1 Camoufl
94. estimate the additional damage The Crater Buffer Distance Criteria is the edge to edge measurement for locating the craters to be included in a single craterfield The Expected Munitions Dud Rate 96 is the expected UXO rate normally gleaned from intelligence reports The Estimated vs Surveyed Threshold 96 determines at what point the estimated UXO count is used or the actual UXO is used during MAOS placement For example a setting of 50 means that if GeoExPT estimates five 5 UXOs within a craterfield it will report 5 the calculated number if it only finds two 2 UXOs However if it finds more than three 3 UXOs it will report the actual number found The Run Utility Wizard compares the airfield damage against available utility features Intersecting items are noted the Properties Pane as well as the ADR Status Tool Group when the MOS is plotted Damage Importer Airfield Damage Importer mgart airfiald damage nite thi scies Crater Upheaval ux c Factor Fa 201 Spalls Depth Gamer Operational Radiuz 20 Crater m Diameter Deamaetar 1 00 J Estimate Damage Crmter Suffer Distance Crtenas Expected Hunsitionz Dud Rate Ya i Estimated vs Surveyed Cancel Figure A1 21 Damage Import
95. et in Concrete 5 6 Crater The pit depression or cavity formed in the surface of the earth by an explosion It may range from saucer shaped to conical depending largely on the depth of burst diameter Apparent Crater diameter lt 20 EM R ANNE SMALL CRATER ASS gt Pavement damage from munitions which penetrate disturb the subgrade and result in an apparent crater diameter less than 20 feet LARGE CRATER Pavement damage from munitions which penetrate disturb the subgrade and result in an apparent crater diameter greater than or equal to 20 feet DEBRIS s DEFORMED eps FALLBACK SN SOIL Figure 2 Typical Crater Configurations Figure 3 Crater in Concrete 5 7 Ejecta The debris and other material ejected from a crater during detonation of a munition 5 8 Expedient Airfield Repair Airfield pavement repairs to create an initial operationally capable launch and recovery surface known as the minimum operating strip MOS based on projected mission aircraft requirements These repairs are conducted in the most expeditious manner possible Ideally where sufficient equipment and materials are available individual crater repairs should be completed within four 4 hours When required equipment and materials are not readily available as in austere locations additional time for crater repairs will be required Previously established criteria for expedient repairs provide an accessible and functio
96. etermine the MAOS MOS requirement A1 6 4 2 Add Aircraft Operations The data captured in this panel is similar to the traditional Worksheet 1 found in Attachment 2 The Altitude and Temperature are entered and the Density Ratio is calculated The RSC and RCR values are entered Each aircraft operation is listed to determine the MOS length Although the length is calculated from the most restrictive operation a length and width can be manually entered Additional aircraft can be added by selecting Add Aircraft These aircraft do not have worksheets so 10 000 x 50 fighters or 150 heavies MOS will be established Selecting Recalculate Length will recalculate the measurements based the chart data data from this form can be saved to an XML file by selecting Save Configuration Data can be imported by selecting Open Saved Configuration Altitude 10 ft Aircraft Weight Operation Special Landing Direction Chart Length 130 155000 LANDING lt gt From G2 2955 F 15E 72871 TAKEOFF From MO C11 3675 F 1SE 53483 LANDING ARRESTMENT From C13 o zMane zMane z Back Next gt Einish Figure A1 26 Add MOS Aircraft Operations A1 6 4 3 Add MOS Options This panel allows configuration of the Runway Operation MOS Marking Airfield Lighting and MAAS requirements The 279 B
97. f aircraft along its length 5 13 Semi Prepared Runway Operation SPRO A takeoff and landing TOL surface consisting of stabilized material aggregate or soil as well as unimproved surfaces such as dry lake beds and grass strips 5 14 Shoulders Prepared paved or unpaved areas adjacent to the edge of an operational pavement 5 15 Spall Pavement damage that does not penetrate through the pavement surface to the underlying soil layers A spall damage area could be up to 1 5 meters 5 feet in diameter 5 16 Spall Field A cluster spalls within a defined area 5 17 Sustainment Airfield Repair Repairs that upgrade expedient repairs for increased aircraft traffic These repairs are conducted as soon as the operational tempo permits and are expected to support the operation of 5 000 passes of a C 17 aircraft with a gross weight of 227 707 kg 502 kip a C 130 aircraft with a gross weight of 79 380 kg 175 kip or an F 15E aircraft with a gross aircraft weight of 36 741 kg 81 kip Repairs should support the expected number of passes with only routine maintenance minimize maintenance and maintain operational 6 tempo quality control is more important than construction time for sustainment repairs 5 18 Taxiway specially prepared or designated path airfield or heliport other than apron areas on which aircraft move under their own power to and from landing takeoff service and parking areas 5 19
98. g Bookmarks on the Map Views Tool Group allows you to add a New Bookmark and Manage Bookmarks Manage Bookmarks Bookmark E Figure A1 8 Bookmarks A1 4 5 2 Views are a method to quickly group layers for visualization Selecting Views from the Map Views Tool Group launches the wizard to build the views amp View Manager Vieu Manager Define custom scenario layer views IX 4 Layers future prajects annotation future projects point future prajects line airfield aircraft area airfield surface centerline airfield surface marking line Cancel Figure A1 9 View Manager A1 4 6 Map Graphics The tools on the Graphics Tool Group allow placement of annotation items on the map These are essentially tools to help produce more user friendly presentations The tools include Text Point Line and Polygon tools a Atch 1 7 of 30 Dimension Line Feature Tags a Feature Pallet push pin symbols a Buffer true shape and a simple Cordon simple arc A1 5 Creating a Scenario A1 5 1 New Scenario Dialog A scenario is simply an ArcGIS file geodatabase While it can be manipulated outside GeoExPT it is not advisable due to the internal connections and implemented business logic Typically a single scenario is created per site installation not per operation aircraft parking force beddown or airfield operation New Scenario Marne C Documents and Setti
99. gion indicates the uncorrected for intersections in that region Record the uncorrected RQC values for each repair patch on Worksheet 2 A2 6 2 3 8 A value of F indicates a flush repair A value of FF indicates flush repair that must be followed by another flush repair A2 6 3 3 Finding Correction Factor A2 6 3 3 1 If the uncorrected is in a region shaded with diagonal lines a correction factor is not calculated and RQC equals the uncorrected RQC F and FF regions are shaded with diagonal lines FF regions are crosshatched to contract with regions A2 6 3 3 2 Draw a horizontal line from each patch length to intersect the appropriate vertical line A2 6 3 3 3 intersections of these lines are in the various regions of the correction factor The number in each region indicates the correction factor for intersections in that region Atch 2 16 of 101 2 6 3 3 4 Record the values Worksheet 2 These the correction factors A2 6 3 3 5 The correction factor is always negative or zero A2 6 3 4 Calculating RQC A2 6 3 4 1 A patch with an uncorrected RQC of F or FF has an RQC of The patch following a patch with an uncorrected of FF also has of F A2 6 3 4 2 Add the uncorrected RQC and correction factor RQC is always less than or equal to the uncorrected RQC A2 6 3 4 3 If the uncorrected plus the corre
100. ically the lower the score the better the solution The MOS candidate with the Repair Score Index and LoR Actual 90 is added to TOC The tool hangs so multiple MOS candidates can be added quickly If MOS candidates in the TOC have different criteria you can right click the MOS you would like to duplicate and select Duplicate Atch 1 23 of 30 MOS 1 0 0 Craters Spall Fields Bornblet Field Camauflets P Est Spalls 4 P R1 ee ss p Centerline gt a R1 Grid POL Craters Eo q ECF 2 Ri ECP 3 Surveyed gt R1 ECP 4 Potential gt 5 Expected UXO Dud Rate 95 gt Ri ECP 6 LoR Actual a gt ECP 7 gt MOS 1 2625 5 100 gt MOS 2 2639 60 Threshold Departure 4 R2 Repair Score Index Groups LoR Constraint 90 Z Figure A1 30 ADR Status and Score Holding the C Key during placement constrains the MOS candidate to the existing surface centerline If the interface is jumpy during placement hold the Key to suspend the calculations count so the template moves more smoothly Instant feedback is provided if there is a problem with the placed candidate Hemember during placement only the actual MOS not the approach lighting must be on the existing surface MOS candidate does not meet LOR you want ta accept placement MOS candidate is off the surface Retry placement Th
101. ing Damage can also be estimated by selecting Estimate Damage i on the Tools Tool Group This tool can be used either to analyze selected data or reanalyze imported data without having to re import damage items Atch 1 17 of 30 Damage Estimation Select options far estimating damage Use craters selected map Crater Buffer Distance Criteria Expected Munitions Dud Rate 95 Estimated vs Surveyed Threshold 95 Help Figure A1 22 Damage Estimating A1 6 3 4 GeoExPT has the capability to analyze airfield damage against loaded utility layers The Utility Wizard d reports the utility layers available for analysis Craters intersecting utilities will be annotated in the Properties Pane Utility Wizard Cs Utility Wizard Codes all damage craters with the type of utility that the crater intersects The utility layers that checked those that currently existin the scenario Note List 15 readonly and for informational purposes only Utilities In Scenario Layer Mame Utility Code No communications fiberoptic line Comm compressed air pipe line conduit centerline HVAC electrical cable line Elec No electrical ductbank line Elec fuel line heat cool line natual gas line POL storm sewer line Wtr wastewater line Wtr Figure 1 23 Utility Wizard Atch 1 18 of 30 I me TES 4 Damage Damage Type Crater Description
102. j Abo CO dan P db edid bcd b db e d d d dO b b e E OR e URN Ya sayana Bele MEET REOR ET SER a i 1 So Kn cae A SOOO bm SSE NNE ME spunogd 99 pg gt AT ONICINV 7 I OL a a y 9I J 1 1 6 0 Aet 13 0 001 002 00E 00 00 009 00 008 006 00071 Q ET O0FT 00 1 lt OT gt 0E 0S Oz 06 OST lt ej dod 993 ONIDVdS 219 993 3 21 94 Chart A2 30 F 16 A B Block 10 and 15 Landing Atch 2 49 of 101 993 NDILVOD 219 0002 0081 0091 00 0001 008 009 00 0 OSel 4 I3A 119 00 2 222 seIVd3sl N 293 DNIOVdS HILVd 443 HLONAT HILYd Chart A2 31 F 16 A B Block 10 and 15 Landing Arrestment Atch 2 50 of 101 993 NOILYOO 21 4 0081 0091 09 1 OOet 0001 008 009 00 002 0 0561 0021 Ee sii LA b ll p Ce RC 0 4 4 Oe wwe P ROO GEOP OC OR 4587878 OO
103. l Pate et NET lt 111 TE F 51 3 n seen rn lt EE RH ls ai 8112111 era a u E 18 xD m gt gt a 8 A eem BE pa us Lil gt 150 130 109 90 70 50 30 lt 10 gt 1000 900 800 700 600 500 400 300 00 100 g amp wt DR 0 1 EI 3993 H19N31 31 4 1884 9NIOVdS H21Vd Figure 2 4 Chart 111 Landing Short Field A2 5 Damage Plotting Runway damage is plotted Takeoff and Landing TOL map at a 1 1200 scale 1 inch equals 100 feet The TOL map should utilize the same Pavement Reference Marking System PRMS as the grid overlay The MOS selection team uses the TOL map located in the EOC to select MOS candidates Damage is Atch 2 12 of 101 initially plotted on the TOL map with estimated repair diameters double the apparent diameter All other damage items not located on the runway utilize the 1 4800 1 inch equals 400 feet Crash Grid Map This map should utilize the Military Grid Reference oystem MGHS as the grid overlay Following completion of runway repairs RQC must be refigured using the actual repair lengths A2 6 RQC Calculations A2 6 1 Define Repair Patches A2 6 1 1 For each repair at least partially on the MOS draw lines perpendicular to the side of the MOS through the first and last point withi
104. l on the ADR Tool Group checks for crossing route segments without nodes disconnected routes and self intersecting routes Checking the box next to each error will zoom into the applicable segment Route Analyzer Tanalogv Trace Segment 15 disconnects Figure 1 17 Route Analyzer A1 6 2 4 The Route Analyzer also has the ability to trace all the routes from a given ECP Check the box next to the appropriate Surface ECP and select Trace After the tool has run be patient on large networks select a Route Atch 1 13 of 30 Surface and GeoExPT will display that route the symbology will be blue and difficult to see Route Analyzer Route Analyzer Trace Trace a a 1 A1 ECP 2 4 7 1 ECP 2 ajd A13 Full Route 1 A13 ECP 2 Route A13 A13 ECP 2 5 16 Route A16 ECP 3 I A16 ECP 2 Route 16 16 ECP 4 1 A16 ECP Route A17 A17 ECP 2 1 A16 ECP 4 Route A17 A17 ECP 3 a A17 fl Route A2 A2 ECP 2 gt A17 ECP 2 Route A2 A2 ECP 3 1 A17 ECP fol Route A2 A2 ECP 4 gt A17 ECP 4 Route 2 A2 ECP 5 Fighter Attack 50 Ft S Fighter Attack 50 Ft QHeavy 75 Ft Heavy 75 Ft Figure A1 18 Route Tracing 1 6 3 Airfield Damage A1 6 3 1 Manually Plotting Damage by PRMS Code Damage items can be plotted using the traditional PRMS coordinates In the TOC
105. n the MOS width A2 6 1 2 Shade the areas on the MOS between the lines for each repair A2 6 1 3 If two or more shaded areas overlap or are within 25 feet of each other shade the area or areas between them A2 6 1 4 From the MOS threshold number each shaded area as a repair patch For operations on bidirectional MOSs do not renumber the patches when the operation direction changes Once a patch is numbered it should not be changed A2 6 2 Finding Repair Patch Location Length and Spacing A2 6 2 1 Once the repair patches have been numbered determine the location length and spacing for each Figure A2 5 TOL shows examples of patch locations lengths and spacings Figure A2 6 Worksheet 2 Example shows examples of entering the data on Worksheet 2 A2 6 2 2 Draw double lines perpendicular to the sides of the MOS marking the operations threshold and operation length A2 6 2 3 For each patch within the two sets of double lines record the operation number and patch on Worksheet 2 Figure A2 6 Worksheet 2 Example A2 6 2 4 Find the center of each repair patch Measure the distance in feet from this point back to the operation threshold If the distance is greater than the operation length use the operation length If the patch center is in front of the operation threshold use zero Record these repair locations on Worksheet 2 A2 6 2 5 Measure each patch length parallel to the side of the MOS in feet
106. nal MOS that will sustain 100 passes of a 17 aircraft with gross weight of 227 707 kilograms kg 502 kilo pounds kip C 130 aircraft with a gross weight of 79 380 kg 175 kip or an F 15E aircraft with a gross aircraft weight of 36 741 kg 81 Expedient repairs the MAOS for mission aircraft requiring foreign object damage FOD cover are not approved for most non fighter aircraft Refer to UFC 3 270 07 Airfield Damage Repair Table 2 1 to determine repair Suitability for specific aircraft 5 9 Infield Areas paved or unpaved on the airfield encompassed or surrounded by other operational surfaces 5 10 Pavement Upheaval The vertical displacement of the airfield pavement around the edge of an explosion produced crater The pavement upheaval is within the crater damage diameter but is outside the apparent crater diameter In other words it is that part of the pavement out of flush tolerance that is elevated above the adjacent undamaged surface 5 11 Permanent Airfield Repair This repair increases the MAOS to sustain 50 000 or more C 17 passes with a gross weight of 263 008 kg 580 000 Ib or 50 000 C 130 passes with a gross weight of 79 380 kg 175 kip or to support a Service defined airfield design type depending upon mission aircraft in accordance with UFC 3 260 02 Pavement Design for Airfields 5 12 Runway A defined rectangular area of an airfield prepared for the landing and takeoff run o
107. nd striping the MAOS Restoration of airfield markings and pavement striping e Airfield lighting Installing emergency airfield lighting EALS for low visibility operations 6 2 entire ADR process is allocated eight hours from last munition impact to support the Air Tasking Order ATO Damage assessment and MOS MAOS selection will need to be completed as quickly as possible to meet ATO requirements 7 MOS MAOS Selection 7 1 MOS MAOS selection can be accomplished using the Geospatial Expeditionary Planning Tool GeoExPT This application runs on an existing license of Esri software It performs contingency beddown planning aircraft parking airfield damage plotting and MAOS selection and produces a variety of reports and maps GeoExPT may be downloaded from the 3E5X1 Engineering Community of Practice CoP https wwwd my af mil afknprod ASPs docman DOCMain asp Tab 0 amp FolderlD O O EN CE 48 22 5 amp FilterZDO EN CE 48 You can also request a copy from the AFCEC Reachback Center at AFCEC RBC tyndall af mil DSN 312 523 6995 or commercial 850 283 6995 The MAOS selection process and algorithms in GeoExPT are the same as those in Technical Order 35E2 4 1 Repair Quality Criteria System for Rapid Runway Repair to be rescinded Instructions for the use of the ADR tools in GeoExPT are detailed in Attachment 1 Geospatial Expeditionary Planning Tool GeoExPT 7 2 MOS selection can be manually performed by
108. ngssLab7 7d sDeslktopxyGeaExPT Training amp BIAP Master gdb Projected Coordinate System World Miller Cylindrical Author 4 Creation Date 1171372011 10 37 42 AM Primary Service USAF Construction Standard Initial Open Planning Wizard Help Figure A1 10 New Scenario The most import item to remember when creating a scenario is to properly project it This is critical since so many operations require accurate measurements As usual It is best to import the projection data from data you will use within the scenario Atch 1 8 of 30 Spatial Reference Larisa WS LM oe Fee DOOR sisa Picrthing D DDDDDO Contra Pecan 75 PFactor D EO Oen 0 000000 Lirik Fleber DODODIT 03 Jalat a predafined cz irade costam Yurt cease andxf E doresine cun an evicting Feature Pastena clan raster Create arena coordinate Hun of ha selected Sore rhe pst enn bo Linker Pel enamine r s Figure 1 11 Data Projection A1 5 2 Adding Map Data All external data added to the scenario is for reference only there is no capability to edit it However standard layer
109. onal length is the longest calculated length for the aircraft operations to be performed on the MOS LA aw 6500 3 T nx mume JS SED ueg men u E coc ope GW lt 56 176 Pounds axe h 3 ow gt a y y Ag ZEA a v we a ES ON p o w 47 sed PEP PAS 2 a a a 4 4747 PS S e NS fetes atate data tutu La 5 Z 4 T nor h OS E AS Ue Bs Ay OS 7 13 di RAD M Ls J _ eee x x ise x x C e gem NS 41422044 eset AU ORO ORO DuC ON 4500 5000 5500 6000 ai d e Lu Z i 49 So fata ta NOS 52 Mn uem 542 82 7 9 auiem s NES 9 VA i 1222 5 I 55 or INS E ML lt NEE um 7 21 En bt Y aas 2 9173 2 He NE amp 2 SH d ons ore es
110. roper node connectivity is critical Although the segments are drawn as lines they are symbolized as polygons to get a sense of their functionality Right click the scenario name in the and select Add gt Route Network PR Next ensure the network is highlighted in the TOC and select Add Segment from the 5 Tool Group Digitize the line as you would normally single click the first and all vertex points and double click the end point Finally Name and correct the Width in the Properties Pane When digitizing crossing routes the crossed route is automatically split Ensure the Name and Width is correct Within surface routing operations will follow two rules 1 the proposed taxi routes will either be parallel or perpendicular to the digitized route line 2 within a surface other than a runway routing will go directly from ECP to ECP regardless of parked aircraft The workaround is to digitize a smaller surface to account for the taxiway and remove the applicable segments when autoparking Routes are only considered during analysis if Active is set to True in the Properties Pane Atch 1 12 of 30 Properties E Feature E General Allocation Placed Name Name of the resource _ 4 Properties z Coordinate Tool Figure A1 16 Adding Route Segments A1 6 2 3 Routing Quality Control As stated earlier the integrity of the routing network is critical to its performing correctly The Houte Analyzer Too
111. ry A1 6 6 Repair Quality Criteria operations are not applicable to the new repair methods but can still be accomplished by right clicking the MOS in the and selecting This area of the application has been updated some time and presents issues A1 6 7 Reports The reports are a work in progress and there are known issues There are a variety of reports for ADR on the Reports Tab Some reports may be more usable to save as a text file to be able to clip out features and coordinates A1 7 Print Plot A1 7 1 Layout Manager The Layout Manager is accessed by selecting Layout Manager 22 on the View Tab Five pre configured layouts are available with GeoExPT Currently there is limited capability to create new layouts configurations A1 7 2 Printing Printing is launched either from the Layout Manager or selecting Print on the File tab The Print Properties dialog enables you to select the Layout enter the Title Description and any Additional Comments The standard Esri print plot interface enables you to customize your map Atch 1 29 of 30 Figure 1 38 Print Dialog Atch 1 30 of 30 LEGACY MANUAL METHOD A2 1 Purpose The manual method of determining the Minimum Operating Strip MOS and Minimum Airfield Operating Surface MAOS should be used only if Geospatial Expeditionary
112. t lt Jd 1223 ONIDVdS HILVd 9984 HLONS 1 HOLVd Chart A2 78 F 117 Light Weight Takeoff Atch 2 97 of 101 239635 119001 194 000 1 000 00021 000011 0006 0008 0007 1009 0 0005 0 000 00085 902 0001 0 ULL 0055 i s e AJ ANE A YE x 00571 0 59 gl 2 m NN _ 22 eec 22 4 PS 2 E aT Mat Mar Sa as an ma ooh X x XT m XC pi oC x P m UH P UM UN vr M Me vete T 1 ox po eoo e CROP a S S ie EN X ee ata E de E x x 4 gt a e 26 He M 5 dos HH ee nee LLLA P _ OL gt w oc ENE SEEN TM 06
113. tch 2 52 of 101 00001 0006 999 19001 21944 2008 000 0009 0005 000 0008 0002 1001 0 a a t ati S S rs E To T m ANE n m Pet a m Du ca a ri ND RP t m ult NAE LO R F ce cp oin cm gn e e gno Ez ud Man an g EE 52 08 76767874 atat P es eee eee tae iie PIT P TTTO TT FTT RTT T CU CN NEN MOS CC ROC OC COCA 97 bg lt eee eee ee oS Eee CUES CU OATES EEEIEE ESEE EEEE EEE EEA e gt s SEK nea Cw Ew s dts NE ok 4 e t NS rrr eee teen BG TVA 4 7 777 HHHH ue uae pu pu m m mn mar a ESERE SSS SEIA A N eee DET SS Al LL LLL ITT VT pios T ae er ani atte ante a M 0057 y gr EIN CHR
114. te of Bldg Sciences Englewood CO 80150 Washington DC 20005 Atch 3 1 of 1
115. th the same characteristics To digitize a crater select Add Crater First click the center of the crater Quickly releasing the mouse button will launch the Diameter dialog If the mouse button is held you can drag out the diameter of the crater This is a hanging tool so unless the Add Crater tool is pushed again you can digitize craters with the same characteristics To digitize a crater field select Add Crater Field la i It is then a matter of drawing the polygon and providing the Number of Craters To digitize a spall field select Add Spal It is then a matter of drawing the polygon and providing the Number of Spalls To digitize a UXO select Add Click the location of the provide the Munitions Type This is a hanging tool so unless the Add UXO tool Is pushed again you can digitize UXOs with the same characteristics Atch 1 15 of 30 To digitize an area of unknown damage select Add Unclassified It is then a matter of drawing the polygon around the area of interest A1 6 3 3 Importing Damage from RADAS RADAS currently produces shapefiles of airfield damage These can either be accessed by clicking on the balloon pop up if enabled in the Settings or accessing mport Damage on the Tools Tool Group i Airfield Damage Shapefile Monitor Airfield damage shapefile s are available GeoExPT C Documents and Settings gecexptuser Desktop RADAS 12 damage shapefile s exist in fol
116. ths are defined as takeoff or landing distance in the aircraft s performance manual Since the MOS length is specified by the Wing Operations Center WOC and the commander it may be longer than the longest operation length Any repair in a section of the MOS beyond the longest operation length has an RQC equal to flush F A2 3 8 All aircraft are maintained in accordance with the relevant technical orders and service manuals The exception is the A 7D nose gear tire which is serviced to 235 psi A2 3 9 If taxiway repairs are required the following caution will be relayed to the wing operation All operations on taxiway repairs are limited to 5 knots Taxiway repairs may have up to 6 inches of upheaval and up to 2 inches of sag Braking in the vicinity of repairs on taxiway surfaces must be avoided A2 4 Step by step Directions for Minimum Operating Strip MOS Lengths A2 4 1 Instructional Guideline Table A2 1 provides a step by step checklist of the process It is recommended the user follow these steps to ensure accuracy and quality of the process Table A2 1 Instructional Guidelines 1 1 Record data for aircraft operation expected on the MOS Aircraft model Gross weight pounds 1 1 1 Vee 1 1 3 Special operation procedures for landing aero braking wheel braking short field arrestment with chute without chute or normal 1 2 Record the RQC chart number for each operation 1 3 Record the Density Ratio DR
117. ture end on the bottom half of Worksheet 3 7 3 Mark each patch number from the MOS on both the top and bottom of Worksheet 3 For each operation and patch record the from Worksheet 2 onto Worksheet 3 For patches that are on the MOS but are not within the length of any operation record an F 7 5 For each repair patch and each operation direction record the lowest in the summary lines on Worksheet 3 7 6 For each repair patch record the lower summary value in the combined line on Worksheet 3 7 7 Transfer the combined to the TOL map and brief the Base Civil Engineer and or wing commander A2 4 2 Collecting Operational Data A2 4 2 1 Contact the WOC usually collocated with the Emergency Operations Center EOC Atch 2 5 of 101 2 4 2 2 Request the mix of aircraft types configurations operations expected on the MOS Aircraft configuration data consists of the aircraft gross weight Operation data should indicate if the aircraft will take off land or evacuate and any special landing procedures arrested landings aerodynamic braking etc A2 4 2 3 Request the direction for operations from the MOS threshold from the MOS departure end or both A2 4 2 4 Record each combination of aircraft model operation and direction on a separate line on Worksheet 1 Figure A2 2 MA v 2 0213 TIFT i gt 7 Q 3 D 5 1
118. vacuation Atch 2 38 of 101 994 1 19001 2194 0002 0081 0091 0001 008 009 OOF 002 0 QUOTE n B TI gt 15 552405060504 cie l 1 WP p iei grum o i 225555505506 n so oat ue a En ak PE s OM i P See tty tS NT b SENN CNN me VGL ERR CA UR CUR n OA T ss ENN RSs qw SS N SR 52000 LL UT 670 009 002 008 006 0001 gt 05 04 06 OTI Q amp T spunod 81226 gt AD 3303991 261 3 OST lt lt ad 824 9 948 2194 993 19 41 1 Chart A2 20 15 C D Takeoff Atch 2 39 of 101 0006 999 19001 0008 0004 0009 0005 00D0 0006 000 0001 0 SS 0065 00165 wey 7 7 PI Ig O 7726 SS MMSE T x DOC X teat 52020 se ORO ORO ORO ROS E 1 Usa i E erai ia E e LUN VEU TTE SA OE O S a LOC OCC OC ORC 255150006 deor a arae ae 525255526905 GRO M Deo QR OQ Pd o USt URS IS
119. vu 5 4 0 tS EE EEE RS viste eiat ww MS Kw NY e in mx 7772 d N 4 gt i W rZ E JJ 3850 3010 2000 2500 3000 3200 PATCH LOCATION feet 1500 1000 300 se eee Se es mi i vo p 9 nr e F993 HIUN31 42935 DNIOVdS H31Vd ad Chart A2 25 F 15 E Takeoff Atch 2 44 of 101 993 1 H319d 00021 00011 00001 0006 0008 0002 0009 0005 000 000 00 0862 0083 ASS SQW i iS Cl y A Z T AT 4 V A GF AV AU AT 00821 5 w 13 55564 detinet ht Vn 40404 EE LEED 225005500 OOS Y MONS Se x 00 lt S O ETE IOS Sn cae MISI E Nau era atu raram Eu EN ENS ASS DIDA SS SAS 22 908 9 2 5 om of 21251220552 spunod ESPES NIN 31 3 Z C t tt eee us LE 4 et 994 DNIJVdS 21 993 HLUN31 Chart A2 26 F 15 E Landing Atch 2 45 of 101

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