AD 91-26-08

Airworthiness directive · Generator Control Units (GCU) and AC Electrical Power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 11 more

Effective
February 14, 1992
Models
A300 B4-601, A300 B4-603, A300 B4-605R, A300 B4-620, A300 B4-622R, A300 F4-605R and 8 more
Data sheet
TCDSA35EU
Registered aircraft
122 matched by model
Product
Aircraft · Large airplane
Amendment
39-8121
Docket
91-NM-87-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

91-26-08 AIRBUS INDUSTRIE: Amendment 39-8121. Docket No. 91-NM-87-AD.

Applicability: Model A310 and A300-600 series airplanes, on which Modification 7769 has not been accomplished, certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless accomplished previously.

To prevent loss of the Generator Control Units (GCU) and AC electrical power, accomplish the following:

(a) Remove the three currently installed GCU's and replace them with three modified GCU's having protective covers, in accordance with Airbus Industrie Service Bulletins A310-24-2040, Revision 1, dated January 28, 1991 (for Model A310); A300-24-6029, Revision 1, dated February 22, 1991 (for Model A300-600); and Sundstrand Service Bulletin 735226/740206/740120-24-9 (for Models A310 and A300-600), dated June 15, 1989 (Modification 7769); as applicable.

(b) 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. The request shall be forwarded through an FAA Principal Avionics Inspector, who may concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

(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 installation required by this AD shall be done in accordance with Airbus Industrie Service Bulletin A310-24-2040, Revision 1, dated January 28, 1991 (for Model A310); Airbus Industrie Service Bulletin A300-24-6029, Revision 1, dated February 22, 1991 (for Model A300-600); and Sundstrand Service Bulletin 735226/740206/740120-24-9 (for Models A310 and A300-600), dated June 15, 1989 (Modification 7769). This incorporation by reference was approved by the Director of the Federal Registerin accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

(e) This amendment (39-8121, AD 91-26-08) becomes effective on February 14, 1992.

Affected TCDS · 1

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

Registered aircraft · 122

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
  • Airbus Industrie74 aircraft
  • Airbus48 aircraft
By year built
19832007
Registered aircraft by year built: 120 aircraft
19832
19841
19851
19881
19892
19905
19913
19927
19935
19945
19958
19965
19975
19986
19996
20007
200111
20026
20038
20047
20057
20066
20076

2 with no year recorded

By model

Aircraft

See all 122 aircraft