AD 76-24-01

Airworthiness directive · Eighth Stage Compressor Disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-1A and 6 more

Effective
June 22, 1977
Models
JT8D-1, JT8D-11, JT8D-1A, JT8D-1B, JT8D-7, JT8D-7A and 3 more
Data sheet
TCDSE2EA
Registered aircraft
105 matched by model
Product
Engine
Amendment
39-2910

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

76-24-01 PRATT & WHITNEY AIRCRAFT: Amendment 39-2775 as amended by Amendment 39-2910. Applies to all Pratt & Whitney Aircraft JT8D-1, -1A, -1B, -7, -7A, -7B, -9, -9A, and -11 turbofan engines containing eighth stage compressor disk, P/N 496908.

Compliance required as indicated.

To prevent possible failure, remove from service the eighth stage compressor disk, P/N 496908 in accordance with the following schedule:

A. After June 30, 1977, remove disks prior to accumulating 8,000 cycles since new. In lieu of removal, disks may be continued in service until December 31, 1977, if inspected in accordance with Pratt & Whitney Aircraft Special Instruction No. SI-10F-77 by June 30, 1977, and every 120 cycles thereafter. Cracked disks shall be replaced prior to further flight. The established life limit of 11,000 cycles shall not be exceeded.

B. After September 30, 1977, remove disks prior to accumulating 6,000 cycles since new. In lieu of removal, disks may be continued in service until December 31, 1977, if inspected in accordance with Pratt & Whitney Aircraft Special Instruction No. SI-10F-77 by September 30, 1977, and every 120 cycles thereafter. Cracked disks shall be replaced prior to further flight. The established life limit of 11,000 cycles shall not be exceeded.

After December 31, 1977, P/N 496908 compressor disk retirement life is 6,000 cycles since new.

Upon request of the operator, an FAA Maintenance Inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA, New England Region, may adjust the inspection intervals specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for that operator.

The manufacturer's Special Instruction No. SI-10F-77 identified and described in this directive is 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 Pratt & Whitney Aircraft, Division of United Technologies Corporation, 400 Main Street, East Hartford, Connecticut 06108. These documents may also be examined at Federal Aviation Administration, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803, and at FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. A historical file on this AD which includes the incorporated material in full is maintained by the FAA at its Headquarters in Washington, D.C., and at New England Region.

Amendment 39-2775 became effective 30 days after publication in the FEDERAL REGISTER.

This amendment 39-2910 becomes effective on June 22, 1977.

Affected TCDS · 1

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

Registered aircraft · 105

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
  • Mcdonnell Douglas80 aircraft
  • Boeing22 aircraft
  • Douglas3 aircraft
By year built
19631999
Registered aircraft by year built: 92 aircraft
19631
19661
19674
19693
19701
19721
19741
19753
19762
19771
19781
19791
19822
19841
19874
19883
19891
19903
199121
19927
19931
19961
19977
19985
199916

13 with no year recorded

By model

Aircraft

See all 105 aircraft