AD 86-05-05 R1

Active

Battery Vent System

Key Information
86-05-05 R1
Active
January 19, 1988
Not specified
Unknown
39-5792
Applicability
["Aircraft"]
["Small/Large Airplane"]
Learjet Inc.
23 24 24A 24B 24B-A 24C 24D 24D-A 24E 24F 24F-A 25 25A 25B 25C 25D 25F 28 29 35 35A (C-21A) 36 36A
Regulatory Text

86-05-05 R1 GATES LEARJET CORPORATION: Amendment 39-5248 as amended by Amendment 39-5792. Applies to the following Gates Learjet models and serial numbers, equipped with a "flow through" battery vent system with the inlet located on the bottom (belly) of the airplane:

MODEL
SERIAL NUMBERS
23 series
003 thru 099
24, 24A, 24B, 24B-A,
100 thru 357
24C, 24D, 24D-A,

24E, 24F, 24F-A

25, 25A, 25B, 25C, 25D, 25F
003 thru 061; 066 thru 373
28
001 thru 005
29
001 thru 004
35,35A
001 thru 570; 589 thru 600
36, 36A
001 thru 053; 055

Compliance required as indicated, unless previously accomplished.

To eliminate the potential for a fire and explosion within the battery, caused by leaking fuel entering the battery vent, accomplish the following within the next 200 flight hours:

A. Relocate the battery inlet vent in accordance with instructions contained in Gates Learjet Corporation Service Bulletin (SB) 23/24/25-334B, dated February 19, 1987, for Models 23, 24, and 25 series airplanes; SB 28/29-24-5A, dated October 7, 1985, for Models 28 and 29 series airplanes; or SB 35/36-24-10, dated July 18, 1987, for Models 35 and 36 series airplanes; or later FAA-approved revisions.

B. 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.

C. Alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety may be used when approved by the Manager, Wichita Aircraft Certification Office, FAA, Central Region.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Gates Learjet Corporation, P.O. Box 7707, Wichita, Kansas 67277. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or FAA, Central Region,Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid- Continent Airport, Wichita, Kansas

Amendment 39-5248 became effective April 11, 1986.

This amendment, 39-5792, becomes effective January 19, 1988.

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References
This information is not available.
--- - Part 39
FAA Documents