# AD 91-16-02: Shut-Off Valve Actuator

- Type: Airworthiness directive
- Status: Current
- Products: Airbus A320-111, A320-211, A320-212, A320-214, A320-231, A320-232 and A320-233
- Effective: September 11, 1991
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- Amendment: 39-7092
- Docket: 91-NM-59-AD
- Registered aircraft: 563 may be affected, by airframe or engine model (OpenAirDocs)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/855EA94A92F5E04B8625695E006F2408.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/91-16-02

## The airworthiness directive

91-16-02 AIRBUS INDUSTRIE: Amendment 39-7092. Docket No. 91-NM-59-AD.

Applicability: Model A320 series airplanes, on which Modification 22039 has not been accomplished, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To ensure complete closure of the low pressure fuel fire shut-off valve, accomplish the following:

A. Within 350 hours time-in-service after the effective date of this AD, and thereafter at intervals not to exceed 350 hours time-in-service, perform a functional check of the low pressure fuel fire shut-off valve actuator, in accordance with Airbus Industrie All Operators Telex (AOT) 28-01, dated October 8, 1990.

B. If any valve fails or indicates failure to open or close correctly, prior to further flight, replace the low pressure fuel fire shut-off valve actuator with either P/N HTE 190001 (PRE Airbus Industrie Service Bulletin A320-28-1028), or P/N HTE 190001-1 (POST Airbus Industrie ServiceBulletin A320-28-1028), in accordance with Airbus Industrie Service Bulletin A320-28-1028, Revision 1, dated November 23, 1990. Following actuator replacement, perform a functional test in accordance with AOT 28-01, dated October 8, 1990. Accomplishment of Modification 22039 (Service Bulletin A320-28-1028) constitutes terminating action for the repetitive functional checks required by paragraph A. of this AD.

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.

E. The repetitive functional check requirements shall be done in accordance with Airbus Industrie All Operators Telex (AOT) 28-01, dated October 8, 1990. The replacement requirements shall be done in accordance with Airbus Industrie Service Bulletin A320-28-1028, Revision 1, dated November 23, 1990. 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 Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. Copies may be inspected at the FAA, Transport Airplane Directorate, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

This amendment (39-7092, AD 91-16-02) becomes effective on September 11, 1991.

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS A28NM](https://openairdocs.org/tcds/A28NM): Airbus SAS; names 7 of 50 models: A320-111, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233

## Registered aircraft it may apply to (OpenAirDocs)

Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment.

- Aircraft: 563 (563 by airframe model, 0 by engine model)
- Makers: Airbus 377, Airbus Industrie 184, Airbus S A S 2

Models with the most aircraft:

- [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232): 189 aircraft (airframe model)
- [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214): 160 aircraft (airframe model)
- [Airbus Industrie A320-232](https://openairdocs.org/model/airbus-industrie-a320-232): 109 aircraft (airframe model)
- [Airbus Industrie A320-212](https://openairdocs.org/model/airbus-industrie-a320-212): 39 aircraft (airframe model)
- [Airbus Industrie A320-214](https://openairdocs.org/model/airbus-industrie-a320-214): 26 aircraft (airframe model)
- [Airbus A320-233](https://openairdocs.org/model/airbus-a320-233): 21 aircraft (airframe model)
- [Airbus Industrie A320-211](https://openairdocs.org/model/airbus-industrie-a320-211): 6 aircraft (airframe model)
- [Airbus A320-211](https://openairdocs.org/model/airbus-a320-211): 3 aircraft (airframe model)
- [Airbus Industrie A320-231](https://openairdocs.org/model/airbus-industrie-a320-231): 2 aircraft (airframe model)
- [Airbus A320-212](https://openairdocs.org/model/airbus-a320-212): 2 aircraft (airframe model)
- [Airbus S A S A320-214](https://openairdocs.org/model/airbus-s-a-s-a320-214): 2 aircraft (airframe model)
- [Airbus A320-231](https://openairdocs.org/model/airbus-a320-231): 2 aircraft (airframe model)
- [Airbus Industrie A320-233](https://openairdocs.org/model/airbus-industrie-a320-233): 1 aircraft (airframe model)
- [Airbus Industrie A320-111](https://openairdocs.org/model/airbus-industrie-a320-111): 1 aircraft (airframe model)

All 15 models: https://openairdocs.org/ad/91-16-02/models.md
Every aircraft: https://openairdocs.org/ad/91-16-02/aircraft.md

Its text cites no advisory circulars or STCs.

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