86-05-05 R1: Battery Vent System
FAA order 86-05-05 R1 is an airworthiness directive in force since January 19, 1988. The FAA's subject line: Battery Vent System. It names Learjet 23, Learjet 24, Learjet 25, Learjet 35: about 206 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: electrical power.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Learjet Inc.
- Models
- 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
- On this site
- Learjet 23 6 registered
Learjet 24 16 registered
Learjet 25 23 registered
Learjet 35 161 registered
Dates and paperwork
- In force since
- January 19, 1988
- 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 (2,188 characters)
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.
Related safety bulletins advice on the same designs, not orders
2026-03-192026-07 · MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins
2016-09-15NM-16-24 · Fuselage: Main Plate/Skin
2013-06-24NM-13-38 · Flight Controls Control Column Section
2011-08-22NM-11-48 · Ice and Rain Protection: Wing Transverse Duct Assembly
2004-05-06CE-04-67 ·
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 October 26, 2026. Connections as data: /graph/directive/86-05-05 R1.json · aircraft systems.
