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        Aeronca Oil Sumps rev8
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1.   wired to the tab on the drain hub  Each time the oil level is checked  verify that the cap is  secure and tight on the filler neck  If the cap should come loose while the aircraft is in flight you  will most likely end up with a couple quarts of oil coating the firewall and belly of the aircraft     It is important to remember that all inspection  maintenance  alterations  and documentation  should be done in accordance with Part 43 of the Federal Aviation Regulations  FAR         Revision   8 Jan 2  2013  Written by John Propst  Reviewed by Bill Pancake    
2. 0   3577  Model  codes    La   C75 12  C75 12F J  C85 8  C85 8F  C85 8FJ  C85 12  C90 8F  C90 12F  C75 12F    C85 12 with dual fuel pump equipment    C90 14F      C90 14F o  Table 1     Continental Oil Sumps A50 through O 200       1d     90 8F  C90 8Fu    Likewise  often when an aircraft experienced a nose over wreck  the oil sump was one of the  lowest points on the front of the aircraft resulting in the sump being damaged or destroyed  This  often resulted in the most convenient    spare    oil sump being reinstalled on the repaired engine     Revision   8 Jan 2  2013 2  Written by John Propst  Reviewed by Bill Pancake    All this is to say that when swapping an engine from one aircraft to another  the accessories   including the oil sump  approved for one aircraft may not be suitable for other aircraft     In the photo to the left Bill  Pancake is holding an A50331 oil  Sump used on an Aeronca A 65    engine in his right hand  and an oil   Sump used on a Cub with a similar    A65 engine in his left hand  Note  the difference in the length and  position of the filler neck  It  should also be noted that the  Aeronca sump was made from  much heavier steel and weighed  considerably more than the Cub  sump     In Table 1  the O 200 sump is  highlighted on the table only  because it is a 6 quart sump that  was common on Cessna 150   s   When  Aeronca aircraft are  updated with the Aeronca 26  gallon fuel system kit  192  FAA   s  oil to onboard fuel Capacity  specification requ
3. Aeronca Oil Sumps  By John Propst with technical overview by Bill Pancake    Abstract This article covers oil sumps used on post war Aeronca Champs and Chiefs     Before addressing the topic of oil sumps  a few words are in order to discuss aircraft and engine  specifications as they relate to Aeronca airplanes  There are two primary documents that define  the requirements and specifications for an airplane  The first is the aircraft Type Certificate and  the second is the engine Type Certificate  These documents are filed with the FAA by the  aircraft manufacturer and the engine manufacturer and are updated from time to time to reflect  updated and revised specifications     As it relates to the oil sumps  the engine type certificate specifies the oil sump capacity and type  of engine lubricant  As it relates to the oil sumps  the aircraft type certificate specifies the engine  manufacturer and engine model  and the oil sump capacity     In general it is the aircraft manufacturer s responsibility to specify and define all the engine     accessories    including the air box  starter  generator  magnetos  exhaust system  propeller   filters  fuel pump  and oil sump  Most of these accessories are fabricated and sold by third party  manufacturer  Oil Sumps are an exception in that most oil Ssumps are manufactured by the  engine manufacture in accordance with the aircraft manufacturer s specifications  This is done  to assure the sump will fit within the confines of the engine mo
4. LOO 7  caps that contain a  leaf spring use P N 533355 gaskets  1 8    thk X 2 5 16    X 1 7      Caps that contain a coil spring  use P N 633240 gaskets  1 16    thk X 2 5 16    X 1 1       Bill Pancake indicated that none of the  Aeronca Champ and Chief engines used the cap with the leaf spring  Therefore  the correct cap  gasket for an Aeronca with a Continental engine is P N 633240  1 16    thick X 2 5 16    X 1  2     Google    633240 gasket    for sources for buying fuel cap gaskets         Oil Sump Repair   Often when an aircraft has a nose over incident  the engine airbox will be forced back into the oil  sump  This will result in a creased dent in the tank  often accompanied by other dents from other  objects  One practice sometimes used for removing dents both from oil sumps as well as  motorcycle fuel tanks is the use of air pressure and heat  The photo on the next page displays  some of the fixtures that Bill has used in the past for removing unwanted dents and creases  from oil sumps  The pipe fittings are sized to screw into the oil sump drain plug opening  The  rubber cork is sized to fit into the oil filler neck  The cork is placed in the neck opening from the  inside of the sump  The flange and gasket are fitted to the top opening on the oil sump  The  repair is made by applying air pressure to the sump while carefully applying heat to the dented    Revision   8 Jan 2  2013 4  Written by John Propst  Reviewed by Bill Pancake    area  Bill indicated that the a
5. for smaller engines are no longer available from TCM  This document is  available on the Aeronca com website  All sumps have the same drain plug part number 2265  and use gasket AN900 10  These gaskets are relatively inexpensive and it is highly  recommended that they be replaced each time the plug is removed  If you go to the Continental     Service Parts Catalog    to try and figure out which sump and gauge rod is applicable for your  engine you ll probably become more confused as you browse the catalog  There are two  different part numbers listed in my manual in addition to an additional entry indicating that the oil  sump does not have a part number  The service letter listed above seems to be the best source  for matching sumps and rods with engines and aircraft     The photo on the left shows a  disassembled A35919 dipstick for an  A50331 oil sump off of an Aeronca  A65 engine  Note that the cap part  number is stamped on the shaft of the  dipstick  It is important that the cap fit  tightly on the sump  If the gasket in the  cap is worn or cracked it should be  replaced  This is not a vented cap  The  oil cap can be disassembled by  pushing and rotating the dipstick  portion into the cap  Be sure to note  how the cap comes apart so that you  can reassemble it  Sometimes the  metal insert with the two ears that  engage the neck needs to be adjusted to assure the cap fits tight and cannot vibrate loose   According to the footnotes in the TCM Service Information Letter SI
6. ires increasing  the oil sump capacity to at least 5 quarts  While there is a Continental 5 quart sump used on the  C90 7EC and 7FC  the 6 quart sump from the O 200 engine is often easier to find and  commonly used with this conversion  Additional information related to oil sump capacity as it  relates to aircraft fuel capacity and horsepower can be found in the Civil Air Regulations  CAR   part 4  section 621  CAR part 4 is referenced in the aircraft type certificate        Another issue related to oil sumps is that it is not  easy to determine which sump is installed on your  engine just by looking at it  The sump part number  shown on table 1 is usually stamped on the face of  the flange of the oil sump  as shown on the photo to  the left  Therefore you can only see the part number  when the sump is removed  If the sump is removed  from your engine for any reason  be sure to record  the part number for the oil sump  Note that many of  the 6 quart oil sumps do not have a part number  stamped on the flange  The part number for the cap  should be stamped on the dipstick portion of the cap        Revision   8 Jan 2  2013 3  Written by John Propst  Reviewed by Bill Pancake    Teledyne Continental Service Information Letter SIL 00 7A covers the subject of    Oil Gauge Rod  Application     The document lists the part number of the oil gauge rod for various engine and  aircraft applications  The footnotes also provide a listing of the sump part number  Many of the  oil gauge rods 
7. mount of air pressure varies  depending upon the weight of the tank material  As noted earlier   a tank for an Aeronca A65 engine is fabricated from much heavier  steel than a similar Piper Cub tank  In general  Bill indicated that  he would use between 10 and 20 psig as a Starting point  After  pressurizing the tank with air  it is then slowly heated in the  dented area with a soft torch flame  Care must be taken not to  overpressure or overheat the tank as this may result in rupturing  the tank        Oil Level   Issues related to false oil level indication on the dip stick often surface in hangar discussions   Several different theories are typically presented  First  some say that the oil will    wick    up the  dipstick while the engine is at rest   While the capillary action of oil with the  stick certainly does exist  it does not  account for the one to two quart  discrepancies sometimes reported   False level indications can occur when  the engine is in operation and the  normal oil level is above the bottom of  the filler neck  On most oil sumps the  filler neck actually extends down into the  Sump as shown on the photo to the left   lf the oil level is above the base of the  filer neck  when the engine is  shutdown  the air in the filler neck will  cool and draw the oil up into the neck a  considerable distance  There are a  couple ways to circumvent this problem   The first is to remove and wipe down  the dipstick before checking the oil level   This is a good and 
8. recommended  practice for all aircraft  A second method is to obtain a field approval and install a fill neck vent  from near the top of the filler neck back to either the oil sump or to the crankcase  This is one of  the many modifications and field approvals that Bill Pancake has applied to his Champ NC  1890E        The question sometimes comes up asking if the numbers on the dipstick are correct  An easy  way to check the accuracy of your dipstick is to add one quart of oil at a time during an oil  change and then check the calibration on the dipstick  It is important that you Know how much  oil is in your engine     Revision   8 Jan 2  2013 5  Written by John Propst  Reviewed by Bill Pancake    Installing Oil Sumps   Oil sumps are attached to the crankcase with six 1 4    studs  Gasket 3577 is installed between  the sump and the crankcase  The sump is secured with plain AN4 washers and 1 4  28 elastic  stop nuts   elastic stop nuts should be used rather than metallic stop nuts or castle nuts because  elastic stop nuts are specified on the Continental parts list   It may be necessary to equally  tighten the elastic stop nuts from time to time to prevent oil leakage     Preventive Maintenance   During routine maintenance and annual or 100 hour inspections  it is important to visually  inspect the oil sump  especially around the neck that attaches to the crankcase for cracks    After changing oil  confirm that the sump drain plug has a new gasket and that the plug is safety
9. unt  aircraft cowling  and other  physical constraints     The oil sumps for Aeronca aircraft are generally specified on Aeronca aircraft engine assembly  and installation drawings  For example  Aeronca drawing 7 446 specifies an A50331 sump for  the 7AC aircraft with an A65 engine  Likewise Aeronca drawing 7 502 specifies the same sump  for the 11AC aircraft with the A65 engine    It would seem that there would not be any issues related to the oil sump for Aeronca aircraft     The problem that arises is that Continental manufactures seven different oil sumps for the A65  engine  There are at least twelve additional sumps manufactured for C75  C85  C90  and O 200  engines  There are also equal numbers of different caps for the oil sumps  This results in over  300 different possible combinations of sumps and oil caps available for installation on the  Continental engine in your Champ and Chief     Table 1 on the next page displays all the  Continental oil sumps for engines A50 through  O 200  Several lines in the table are highlighted  for Aeronca applications     The drawing to the left is a portion of Aeronca  drawing 4 613  This drawing specifies the exact  length and location of the filler neck with respect  to the tank for the A50331 sump for the A65  engine on the 7AC and 11AC aircraft  Likewise it  shows the markings on the A35919 cap        Revision   8 Jan 2  2013 1  Written by John Propst  Reviewed by Bill Pancake    Other sumps shown in table 1 may well have been de
10. veloped by Continental for other makes  and models of aircraft and may have the filler neck located in a different position and different  angle than the sump for Aeronca airplanes  Over the years it was not at all that uncommon for  an engine from one make and model of aircraft to be removed and reinstalled on an Aeronca  aircraft  Often when the engine swaps were being made many of the engine accessories  including the sump  air box  mags  and propeller were also included in the swap  As a case in  point  when purchased  the authors 7AC Champ with a C85 12 engine had an oil sump  manufactured for an Aircoupe with the filler neck located on the left side of the engine     Paimo a   maei   piap   uaust   amate  n  Part No Part No  Model Plug Gasket Qt  A5479   A35017   A50  A65  A75  A80   2265   AN900 10   3577  4      7AC and 11AC per dwg 7 446  A50331 a a A65  A75  A80 AN900 10 some eo a 7 502    A3966     lab  2265     3577     fee   O l 3577  raseso   36026  oe  2265   ANGO0 10   3577 x  530091   A36026   be  2265   AN900 10   3577  A5460   A36036  b  2265   AN900 10   3577  A5373   A36037  B  2265   AN900 10   3577  3577  3577 48   Asoaet__  saga _  p__  2268_AN900 10 3577    a _  96408 _  2285   AN900 10_ 10   3577 a a 7BCM ECM per owg 7599 _ dwg 7 599      A50351   A361141   11   2265   AN900 10   10 3577      SoA 7FC per Aeronca aa  and Service Manual   530473 530475 c d 2265 AN900 10   3577 For 7CCM per dwg 7 599                           A5230 530667 2265   AN900 1
    
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