AD 94-01-02

Airworthiness directive · Ram Air Turbine · Boeing 767-200 Series, 767-300 Series and 767-300F Series

Effective
February 14, 1994
Models
767-200 Series, 767-300 Series, 767-300F Series
Data sheet
TCDSA1NM
Registered aircraft
402 matched by model
Product
Aircraft · Large airplane
Amendment
39-8784
Docket
93-NM-127-AD

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

94-01-02 BOEING: Amendment 39-8784. Docket 93-NM-127-AD.

Applicability: Model 767 series airplanes; as listed in Boeing Service Bulletin 767-29- 0021, Revision 4, dated May 12, 1988; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent the inability to maintain hydraulic system power in the event that power is lost in both engines, accomplish the following:

(a) Within 4,000 hours time-in-service or 15 months after the effective date of this AD, whichever occurs later, replace the ram air turbine (RAT) airspeed switch; cap and stow the wire between the RAT airspeed switch and the air/ground relay; and perform a functional test of the RAT deployment system; in accordance with Boeing Service Bulletin 767-29-0021, Revision 4, dated May 12, 1988.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager,Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The modification shall be done in accordance with Boeing Service Bulletin 767-29-0021, Revision 4, dated May 12, 1988, which contains the following list of effective pages:

Page Number Revision Level Shown on Page Date Shown on Page 1-4, 6, 10 4 May 12, 1988 5, 7-9, 11-14 1 August 10, 1984

This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on February 14, 1994.

Affected TCDS · 1

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

Registered aircraft · 402

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
  • Boeing402 aircraft
By year built
19822026
Registered aircraft by year built: 363 aircraft
19824
19837
19849
19854
19861
19871
19884
19895
19909
199115
199221
199313
19946
199511
19969
199712
199819
199915
20009
20019
20022
20031
20042
20051
20064
20081
20105
20111
20124
20166
201710
201817
201920
202020
202118
202216
202317
202410
202515
202610

39 with no year recorded

By model

See all 35 models

Aircraft

See all 402 aircraft