[email protected] +1 (817) 925-0047

Airworthiness Directive 20-24-05 Wing Spar Inspection on certain PA-28's

This AD was prompted by reports of corrosion found in an area of the main wing spar not easily accessible for inspection. The FAA is issuing this AD to detect and correct corrosion in the wing root area of the left and the right main wing spars. Corrosion of the main wing spar, if not detected and corrected, could cause the main wing spar to fail with consequent loss of control of the airplane.

Models Affected

    PA-28-140 28-20001 through 28-26946, and 28-7125001 through 28-7725290
    PA-28-150 and PA-28-160 28-1 through 28-4377, and 28-1760A
    PA-28-180 28-671 through 28-5859, 28-7105001 through 28-7205318, and 28-7305001 through 28-7505261
    PA-28-235 28-10001 through 28-11378, 28-7110001 through 28-7710089, and 28E-11
    PA-32-260 32-04, 32-1 through 32-1297, and 32-7100001 through 32-7800008
    PA-32-300 32-15, 32-21, 32-40000 through 32-40974, and 32-7140001 through 32-7840222

AD 20-24-05 PA-28 Wing Spar Inspection

Complete text of AD and applicable aircraft can be found here: Link to AD 20-24-05 For those of you that have an aircraft affected by the AD 20-24-05 this is an extreme example of why it is so important to know this ad has been complied with properly. This particular aircraft had been practicing manuevers and stalls the week before this inspection was done. Obviously no one would want to fly this aircraft after seeing these photos of the spar. Stay tuned to this blog for more things we find weekly at DJS during our inspections.

This is a good example of why the FAA issues Airworthiness Directives. Had it not been for the required inspection this defect could have easily been missed as it takes specialized equipment and inspection in areas that are not easily accessible and most probably would have een missed on an ordinary annual inspection.

This AD could be catastrophic in nature and should not be taken lightly!

Stay tuned for more interesting things we find during our weekly inspections!

Airworthiness Directive 2023-04-08 Continental Motors

Continental discovered a potential assembly error affecting approximately 2000 crankshaft assemblies. It is possible one or more counterweight retaining rings were not properly seated in the crankshaft counterweight groove. This condition could allow the counterweight to depart from the crankshaft during engine operation resulting in catastrophic engine damage.

Models Affected

Continental Aerospace Technologies, Inc. (Continental) GTSIO-520-C, -D, -H, -K, -L, -M, -N, and -S; IO-360-A, -AB, -AF, -C, -CB, -D, -DB, -E, -ES, -G, -GB, -H, -HB, -J, -JB, -K, and -KB; IO-470-D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, -V, and -VO; IO-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, and -MB; IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, and -R; LTSIO-360-E, -EB, -KB, and -RB; LTSIO-520-AE; O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -R, -S, -T, and -U; TSIO-360-A, -AB, -B, -BB, -C, -CB, -D, -DB, -E, -EB, -G, -GB, -H, -HB, -JB, -KB, -LB, -MB, -RB, and -SB; TSIO-520-A, -AE, -AF, -B, -BB, -BE, -C, -CE, -D, -DB, -E, -EB, -G, -H, -J, -JB, -K, -KB, -L, -LB, -M, -NB, -P, -R, -T, -UB, -VB, and -WB; TSIO-550-A, -B, -C, -E, -G, -K, and -N; TSIOF-550-K; and TSIOL-550-A, -B, and -C model reciprocating engines.

AD 2023-04-08 Continental Motors

This AD affect those who have had a recent overhaul of the above listed engines and is a big deal in that it can cause a catastrophic failure destroying your engine and causing a forced landing. The AD requires the removal of cylinders and inspecting the counterbalance weights retaining clips. This AD was caused by whoever at Continental Motors who was responsible for installing the counter balance weights did not make sure the retaining rings were installed correctly.

If your engine falls under this AD you must not fly it again until this AD has been accomplished although the FAA has given consent for a one time ferry flight to a facility for inspection under the following conditions

(k) Special Flight Permit

Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to permit a one-time, non-revenue ferry flight to operate the aircraft to a location where the maintenance actions can be performed, provided that:

    (1) The engine oil filter pleats or screen are first inspected and there is no evidence of metal contamination; or
    (2) An oil change has been done within the previous 5 flight hours, and there was no evidence of metal contamination in the oil filter pleats or screen.

The full text of this ad is available here: AD 2023-04-08

This is a another great example of why the FAA issues Airworthiness Directives.

Stay tuned for more interesting things we find during our weekly inspections!

David Johnson

David is the owner and founder of DJS Aviation LLC. His experience and guidance has grown DJS from a small one man operation into what it is today. David has experience with just about all piston aircraft in use today. He is a pilot and avid aviation enthusiast! His favorite make of aircraft is Beech and he is an expert on the older V-tails! He currently does all of DJS logbook and AD research and helps in all the day to day activities! He is our go to person when we have questions or need advice with our inspections or repairs.