AD 80-01-04

Airworthiness directive · Cylinder Holddown Flange Assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 44 more

Effective
January 25, 1980
Models
IO-520-A, IO-520-B, IO-520-BA, IO-520-BB, IO-520-C, IO-520-CB and 41 more
Data sheets
TCDSE8CETCDSE5CE
Registered aircraft
14,256 matched by model
Product
Engine
Amendment
39-3647

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

80-01-04 TELEDYNE CONTINENTAL MOTORS: Amendment 39-3647. Applies to Continental IO-520 and TSIO-520 series engines incorporating cylinder assemblies which have been rebarrelled by Airmotive Engineering Corporation. Compliance is required within the next 50 hours time in service after the effective date of this AD, unless already accomplished, except aircraft may be flown in accordance with FAR 21.197 to a base where the maintenance required by this AD may be performed. To prevent failure of cylinder holddown flanges, accomplish the following: Inspect to determine if Airmotive Engineering Corporation rebarreled cylinders, Part Numbers AE-C- 631397 T.T., AE-C-639272 T.T., and AE-C-639274 T.T., are installed. If installed, inspect cylinders for .050 inch minimum corner radius in the area spot faced for installation of holddown nuts. Airmotive Engineering Corporation Service Alert dated September 28, 1979, covers this also. Replace all cylinders found without the proper radius. The cylinder part numbers are marked on the flat area of the cylinder holddown flanges on the intake valve side. These cylinder assemblies may have been installed during overhaul or unscheduled maintenance. Airmotive Engineering Corporation Service Alert dated September 28, 1979, pertains to and provides instructions for accomplishing the intent of this AD. The manufacturer's procedures identified and described in this directive are incorporated herein and made 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 from the manufacturer may obtain copies upon request to Airmotive Engineering Corporation, 9131 Directors Row, Dallas, Texas 75247. These documents may also be examined at Office of the Regional Counsel, Southwest Region, Federal Aviation Administration, 4400 Blue Mound Road, Fort Worth, Texas. Equivalent means of compliance with the modification prescribed by this AD may be approved by the Chief, Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, Federal Aviation Administration, Post Office Box 1689, Fort Worth, Texas 76101. This amendment becomes effective January 25, 1980.

Affected TCDS · 2

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

Registered aircraft · 14,256

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
  • Cessna7,278 aircraft
  • Beech6,053 aircraft
  • Bellanca469 aircraft
  • Piper194 aircraft
  • Raytheon69 aircraft
  • Other makers48193 aircraft
By year built
19182022
Registered aircraft by year built: 12,793 aircraft
19181
19441
19464
19475
19487
19492
19508
19522
19534
19545
19558
195611
19575
19582
19594
19606
196112
196222
196346
1964433
1965338
1966587
1967456
1968481
1969399
1970298
1971242
1972422
1973610
1974649
1975805
1976862
1977883
19781,064
19791,128
1980788
1981718
1982316
1983165
1984164
1985136
198689
198787
198896
198967
199078
199163
199240
199342
199423
19958
19969
19979
199815
199917
200012
200118
20024
20032
20044
20051
20072
20082
20091
20131
20141
20151
20171
20221

1,463 with no year recorded

By model

See all 43 models

Aircraft

See all 14,256 aircraft