AD 77-09-08

Airworthiness directive · Bleed Valve Diaphragm · Rolls-Royce 250-B17, 250-B17B, 250-C20 and 2 more

Effective
July 18, 1977
Models
250-B17, 250-B17B, 250-C20, 250-C20B, 250-C20C (T63-A-720)
Registered aircraft
1,062 matched by model
Product
Engine
Amendment
39-2907

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

77-09-08 DETROIT DIESEL ALLISON: Amendment 39-2889 as revised by Amendment 39-2907. Applies to 250-C20, C20B, C20C, B17, B17B engines. Compliance required within the next 30 calendar days after the effective date of this AD, unless already accomplished. To prevent engine power loss resulting from bleed valve diaphragm failure, accomplish the following: Clip lockwire and remove the exit nozzle P/N 6874818 from the bleed valve cover. Using a small screwdriver install strainer assembly P/N 6896347 in the valve cover exit port until it is fully seated. Install the exit nozzle in the bleed valve cover. Tighten to 35-45 lb. in. CAUTION: DO NOT EXCEED 45 LB. IN.; OVERTIGHTENING MAY DAMAGE THE STRAINER. Approximately 2-3 threads of the exit nozzle will be visible when the strainer assembly is seated fully in the bleed valve. If more than three threads are visible this modification must not be accomplished and bleed valve must be removed for overhaul. To clear the bleed valvecover passages of burrs and other particles, again remove the exit nozzle and strainer assembly from the valve cover. With the throttle at IDLE CUT OFF, motor the engine in excess of 10% rpm. Using a small screwdriver, reinstall the strainer in the valve cover exit port until it is fully seated. Reinstall the exit nozzle in the bleed valve cover. Tighten to 35-45 lb. in. CAUTION: DO NOT EXCEED 45 LB. IN.; OVERTIGHTENING MAY DAMAGE THE STRAINER. Approximately 2-3 threads of the exit nozzle will be visible when the strainer is fully seated in the bleed valve. Secure the exit nozzle with lockwire. (Detroit Diesel Allison Commercial Engine Bulletins No. 1116 for the 250-C20 series and No. 1071 for the 250-B17 series engines also pertain to this subject.) Amendment 39-2889 became effective June 10, 1977. This amendment 39-2907 becomes effective July 18, 1977.

Affected TCDS · 2

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

Registered aircraft · 1,062

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
  • Bell565 aircraft
  • Hughes Helicopters145 aircraft
  • Mcdonnell Douglas Helicopter79 aircraft
  • MD Helicopters44 aircraft
  • Hughes35 aircraft
  • Other makers40194 aircraft
By year built
19472021
Registered aircraft by year built: 935 aircraft
19471
19581
19602
19611
19625
19631
19641
19653
19664
19676
196811
19699
197014
197119
197223
197321
197430
197523
197634
197743
197842
197959
198064
198174
198251
198314
198414
198515
198612
19878
198822
198926
199017
199121
199220
199324
199434
199543
199617
199718
19989
19996
200017
200115
20028
20032
20042
20053
20072
20089
20094
20123
20132
20143
20181
20201
20211

127 with no year recorded

By model

Aircraft

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