AD 84-13-05

Airworthiness directive · Redesigned Crankshaft · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 19 more

Effective
July 16, 1984
Models
AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C, AEIO-360-A1D, AEIO-360-A1E and 16 more
Data sheet
TCDS1E10
Registered aircraft
952 matched by model
Product
Engine
Amendment
39-4886

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

84-13-05 AVCO LYCOMING: Amendment 39-4886. Applies to engine models AIO-360-A1A, -A2A, -A1B, -A2B, -B1B, all with serial numbers up to and including L-257-63A, engine models AEIO-360-A1A, -A1B, -A1B6, -A2A, -A1C, -A2C, -A1D, -A1E, -A2B, -B1B, -B1D, -B1F, -B1F6, -B2F, -B2F6, -B4A, -H1A, all with serial numbers up to and including L-23521-51A. Also all of the above models, remanufactured by Lycoming which were shipped before June 1, 1983, regardless of serial numbers. Engine models above, the affected serial numbers and remanufactured engines shipped on or after June 1, 1983, incorporate a redesigned crankshaft and are not subject to this AD. Compliance is required as indicated unless already accomplished: To preclude the possibility of in-flight propeller flange separation, accomplish either (a) or (b) or (c). (a) Within the next 25 hours time in service and every 25 hours time in service thereafter, visually inspect the crankshaft flange in accordance with Inspection Procedure I specified in AVCO Lycoming Service Bulletin No. 465A, or FAA approved equivalent. Use a 10 power magnifying glass for the inspection procedure. (b) Within the next 25 hours time in service and every 100 hours time in service thereafter, comply with Magnaflux Inspection Procedure II specified in AVCO Lycoming Service Bulletin No. 465A or FAA approved equivalent. (c) The inspections required under (a) or (b) may be discontinued when the crankshaft is replaced with a redesigned crankshaft in accordance with Procedure III specified in AVCO Lycoming Service Bulletin No. 465A or FAA approved equivalent. (d) An equivalent method of compliance with this AD may be used if approved by the Manager, New York Aircraft Certification Office, FAA, New England Region. (e) Upon submission of substantiating data by an owner or operator through an FAA maintenance inspector, the Manager, New York Aircraft Certification Office, may adjust the compliance time specified in this AD. (f)In accordance with FAR 21.197 and 21.199, the aircraft may be flown to a location where the inspections or alterations required by this AD can be performed. AVCO Lycoming S/B No. 465A identified in this directive is incorporated herein and made by reference a part hereof pursuant to 5. U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents may obtain copies upon request to AVCO Lycoming Williamsport Division, 652 Oliver Street, Williamsport, Pennsylvania 17701. These documents may also be examined at the Office of Regional Counsel, FAA New England Regional Office, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD is maintained at the New England Regional Office. This amendment becomes effective on July 16, 1984.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 952

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • American Champion274 aircraft
  • Bellanca176 aircraft
  • Great Lakes84 aircraft
  • Aerotek50 aircraft
  • Mooney35 aircraft
  • Other makers252333 aircraft
By year built
19592026
Registered aircraft by year built: 833 aircraft
19592
19661
19671
19681
19712
19731
19743
197510
197630
197782
197867
197963
198023
198132
198224
198313
198432
198511
19869
198711
198812
19898
199010
199112
199239
199329
199415
199528
199612
199728
199825
199930
200023
200116
200213
200327
200429
200531
20063
20071
20082
20101
20112
20122
20132
20143
20152
20171
20192
20202
20221
20253
20261

119 with no year recorded

By model

Aircraft

See all 952 aircraft

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 84-13-05, often to say whether the aircraft complied with it.