83-23-01: Wing Tank Fuel System Modification
FAA order 83-23-01 is an airworthiness directive in force since December 8, 1983. The FAA's subject line: Wing Tank Fuel System Modification. It names Britten-Norman BN-2, Pilatus Britten-Norman Ltd. BN-2: about 67 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: fuel system.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- B-N Group Ltd.
- Models
- BN-2, BN-2A, BN-2A-2, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3
- On this site
- Britten-Norman BN-2 54 registered
Pilatus Britten-Norman Ltd. BN-2 13 registered
Dates and paperwork
- In force since
- December 8, 1983
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (2,458 characters)
83-23-01 PILATUS BRITTEN-NORMAN LTD: Amendment 39-4764. Applies to Models BN-2, BN-2A and BN-2B Islander Series Airplanes equipped with wing tip tanks (Mod NB/M/364) certificated in any category except BN-2A MKIII Series Trislander Airplanes.
Compliance: Required within 100 hours time-in-service after the effective date of this AD, but no later than December 31, 1983, unless already accomplished.
To preclude fuel mismanagement and possible fuel starvation, accomplish the following:
a) Modify the wing tip tank fuel management system in accordance with steps 1. through 12. of the ACTION section of Pilatus Britten-Norman Ltd. Service Bulletin No. BN- 2/SB.157, dated March 14, 1983.
1) Upon completion of the modification described in paragraph a) update and annotate the appropriate airplane flight manual as follows:
i) BN-2A-3 Model: insert Issue 4 of Supplement No. 8 to Section 7 of Flight Manual FM/10 dated March 4, 1983;
ii) BN-2A-9 Model: insert Issue 2 of Supplement No. 16 to Section 7 of Flight Manual FM/2 dated March 4, 1983;
iii) BN-2A-21 Model: insert Issue 4 of Supplement No. 8 to Section 7 of Flight Manual FM/10 dated March 4, 1983;
iv) BN-2A-27 Model: insert Issue 2 of Supplement No. 1 to Section 7 of Flight Manual FM/20 dated March 4, 1983;
v) BN-2B-21 Model: insert Issue 3 of Supplement No. 1 to Section 7 of Flight Manual FM/43 dated March 4, 1983;
vi) BN-2B-27 Model: insert Issue 5 of Supplement No. 1 to Section 7 of Flight Manual FM/42 dated March 4, 1983.
NOTE: The requirement for insertion of specific revisions in the affected Airplane Flight Manuals does not prohibit incorporation of later revisions containing the same information.
2) The requirement of paragraph a)1) of this AD may be accomplished by the holder of a pilot certificate issued under Part 61 of the Federal Aviation Regulations (FAR) on any airplane owned or operated by him. The person accomplishing this action must make the appropriate aircraft maintenance record entry as prescribed by FAR 91.173.
b) Aircraft may be flown in accordance with FAR 21.197 to a location where this AD can be accomplished.
c) An equivalent method of compliance with this AD, if used, must be approved by the Manager, Aircraft Certification Staff, AEU-100, Europe, Africa and Middle East Office, FAA, c/o American Embassy, 1000 Brussels, Belgium.
This amendment becomes effective on December 8, 1983.
Related safety bulletins advice on the same designs, not orders
2015-04-15CE-15-12 · Flight Controls; Control System Interference with Access Panel Fasteners
2007-02-06CE-07-15 · FHL landing gear and components
1999-04-29ACE-99-20 ·
1999-04-29ACE-99-21 ·
1998-07-06ACE-98-38 ·
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/83-23-01.json · aircraft systems.
