AD 91-09-51

Airworthiness directive · Oxygen Lines · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 4 more

Effective
July 29, 1991
Models
DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-301, DHC-8-311, DHC-8-315
Data sheet
TCDSA13NM
Registered aircraft
33 matched by model
Product
Aircraft · Large airplane
Amendment
39-7026
Docket
91-NM-101-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

91-09-51 BOEING OF CANADA, LTD., DE HAVILLAND DIVISION: Amendment 39- 7026. Docket No. 91-NM-101-AD. Final Rule of Telegraphic AD T91-09-51.

Applicability: de Havilland Model DHC-8-100 and -300 series airplanes, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent an oxygen-fed, in-flight fire under the flight compartment floor, accomplish the following:

(a) Within 24 hours after the effective date of this amendment, perform a visual inspection of the flight crew oxygen lines and adjacent electrical feeder cables in accordance with Boeing of Canada de Havilland Division Alert Service Bulletin A8-35-5, Revision A, dated April 5, 1991.

(b) If evidence of chafing is found in the crew oxygen lines or adjacent electrical feeder cables, prior to further flight, repair or replace damaged lines or cables, in accordance with Boeing of Canada de Havilland Division Alert Service Bulletin A8-35-5, Revision A, dated April 5, 1991.

(c) An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

(d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

The inspection and repair or replacement requirements shall be done in accordance with Boeing of Canada de Havilland Division Alert Service Bulletin A8-35-5, Revision A, dated April 5, 1991. 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 of Canada, Ltd., de Havilland Division, Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada. Copies may be inspected at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington; at the FAA, New England Region, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

This amendment (39-7026, AD 91-09-51) becomes effective on July 29, 1991, as to all persons, except those persons to whom it was made immediately effective by telegraphic AD T91-09-51, issued April 25, 1991, which contained this amendment.

Affected TCDS · 1

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

Registered aircraft · 33

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
  • Bombardier15 aircraft
  • Dehavilland9 aircraft
  • Boeing Of Canada/Dehav Div6 aircraft
  • Boeing3 aircraft
By year built
19852009
Registered aircraft by year built: 16 aircraft
19851
19881
19891
19901
19915
19921
19942
19951
19971
20092

17 with no year recorded

By model

Aircraft

See all 33 aircraft