AD 69-25-08

Airworthiness directive · Reduction Gear Assemblies · Lycoming Engines GO-435-C2A, GO-435-C2A2, GO-480-A1A and 61 more

Effective
February 19, 1970
Models
GO-435-C2A, GO-435-C2A2, GO-480-A1A, GO-480-B, GO-480-B1A6, GO-480-B1B and 58 more
Registered aircraft
400 matched by model
Product
Engine
Amendment
39-938

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.

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The airworthiness directive

69-25-08 LYCOMING ENGINES: Amdt. 39-892 as amended by Amendment 39-938. Applies to Lycoming GO-435-C2A, GO-480, GSO-480 and IGSO-480 type engines using spline type reduction gear assemblies 72875 and 72879, GO-480 and GSO-480 type engines using flange type reduction gear assemblies 69346, 70412 and 71803 and IGO-540 and IGSO-540 type engines using reduction gear assemblies 72782, 74900, 75679, 76494 and 77731.

Compliance required unless already accomplished prior to the accumulation of six hundred (600) hours in service or 100 hours after the effective date of this AD whichever comes later for the GO-435, IGO-540 and IGSO-540 type engines and prior to the accumulation of seven hundred (700) hours in service or 100 hours after the effective date of this AD whichever comes later for GO-480, GSO-480 and IGSO-480 type engines. To prevent failure of the reduction gear assembly a one time inspection is to be accomplished as follows:

a. Check torque on reduction gearing pinioncage attaching nut.

1. If found to be in excess of 50 ft.-lbs. remove, inspect for damage and replace the oil retaining housing if necessary. During assembly comply with part (b) using a new lockplate and a pinion cage attaching nut torque of 400 ft.-lbs. When the assembly is disassembled replace thrust bearing oil slinger P/N 68319 with P/N 77454.

2. If found to be less than 50 ft.-lbs. disassemble the assembly and insure that all components meet approved specifications and replace the thrust bearing oil slinger P/N 68319 and P/N 77454 and the oil retaining housing. During assembly comply with part (b) using a new lockplate and a pinion cage attaching nut torque of 400 ft.-lbs.

b. If the pinion cage is secured with a spline nut it must be replaced with an approved hexagonal nut.

c. If the assembly has been rebuilt using thrust bearing oil slinger P/N 77454, stamp the suffix (-1) to the part number on the reduction gear housing.

Lycoming Service BulletinNo. 319A and Lycoming Service Instruction No. 1210A pertain to this subject.

Amendment 39-892 effective December 17, 1969.

This Amendment (39-938) is effective February 19, 1970.

Affected TCDS · 5

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

Registered aircraft · 400

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
  • Beech135 aircraft
  • Helio73 aircraft
  • Aero Commander53 aircraft
  • Grumman26 aircraft
  • Republic19 aircraft
  • Other makers3094 aircraft
By year built
19242023
Registered aircraft by year built: 329 aircraft
19241
19414
19421
19434
19442
19454
194610
194711
19481
19504
19512
19521
19531
19545
195524
195624
195715
195813
195920
196028
196112
196222
19639
19645
196511
196613
196710
19688
196910
19708
19714
19722
19735
197414
19754
19762
19775
19923
19991
20001
20011
20022
20151
20231

71 with no year recorded

By model

See all 18 models

Aircraft

See all 400 aircraft