87-24-05: Rear Pressure Bulkhead
FAA order 87-24-05 is an airworthiness directive in force since December 24, 1987. The FAA's subject line: Rear Pressure Bulkhead. It names Airbus A300: about 120 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Airbus
- Models
- A300 B2-1A, A300 B2-1C, A300 B2-203, A300 B2K-3C, A300 B4-103, A300 B4-203, A300 B4-2C
- On this site
- Airbus A300 120 registered
Dates and paperwork
- In force since
- December 24, 1987
- 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 (2,128 characters)
87-24-05 AIRBUS INDUSTRIE: Amendment 39-5770. Applies to all Model A300 series airplanes, certificated in any category. Compliance required as indicated, unless previously accomplished.
To detect corrosion in the area of the rear pressure bulkhead, accomplish the following:
A. Perform a visual inspection for corrosion in the lower rim area of the rear pressure bulkhead, and repair, if necessary, prior to further flight, in accordance with Airbus Industrie Service Bulletin A300-53-213, dated November 18, 1986, as follows:
1. On airplanes with less than 4.5 years since the first flight in revenue service as of the effective date of this AD: inspect within 6 months after the airplane has reached 4.5 years since the first flight in revenue service.
2. On airplanes with 4.5 years or more, but less than 6 years since the first flight in revenue service: inspect within the next 6 months after the effective date of this AD.
3. On airplanes with 6 years or moresince the first flight in revenue service: inspect within the next 3 months after the effective date of this AD.
B. An alternate means of compliance or adjustment of the compliance time, which provide an acceptable level of safety and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.
C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.
All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Airbus Industrie, Airbus Support Division, Avenue Didier Daurat, 31700 Blagnac, France. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or atthe Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.
This amendment becomes effective December 24, 1987.
Related safety bulletins advice on the same designs, not orders
2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2008-07-02NM-08-31 · Equipment/Furnishings: Non-Textile Floors
2006-12-11SW-07-13 · Oxygen Reserve Cylinder
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.
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/87-24-05.json · aircraft systems.
