85-24-02: Air Conditioning Ram Air Plenum Chamber
FAA order 85-24-02 is an airworthiness directive in force since December 23, 1985. The FAA's subject line: Air Conditioning Ram Air Plenum Chamber. It names Boeing 727: about 37 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: heating, ice protection and utility systems.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- The Boeing Company
- Models
- 727-200 Series
- On this site
- Boeing 727 37 registered
Dates and paperwork
- In force since
- December 23, 1985
- 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 (2,345 characters)
85-24-02 BOEING: Amendment 39-5170. Applies to all Model 727-200 series airplanes, certificated in any category. Compliance is required as indicated, unless previously accomplished. \n\n\tTo detect corrosion of the wing lower skin that could result in fuel entering the ram air plenum chamber accomplish the following: \n\n\tA.\tOn airplanes with more than 10,000 hours time-in-service or 4 years since date of manufacture, accomplish the following within the next 3,000 hours time-in-service or 1 year, whichever occurs first after the effective date of this AD: \n\n\t\t1.\tVisually inspect the upper wall of the air conditioning ram air plenum chamber for corrosion in accordance with Part II of Boeing Service Bulletin 727-51-17, dated April 26, 1974, or later FAA approved revision. \n\n\t\t2.\tIf corrosion is detected, repair and refinish in accordance with Figure 3 of the Boeing Service Bulletin 727-51-17 dated April 26, 1974, or later FAA-approved revision, or in a manner approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tB.\tRepeat the procedures required in paragraph A., above, at intervals not to exceed either 8,000 hours time-in-service or 4 years, whichever occurs first. \n\n\tC.\tInspections accomplished in accordance with Part II of Boeing Service Bulletin 727-51-17 prior to the effective date of this AD satisfy the initial inspection requirements of this AD. \n\n\tD.\tAlternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tE.\tSpecial 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. \n\n\tAll persons affected by this proposal who have not already received these documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis amendment becomes effective December 23, 1985.
Related safety bulletins advice on the same designs, not orders
2014-11-24NM-15-03 · Flight Controls
2014-11-06NM-15-02 · Cabin Equipment/Furnishings
2010-01-07NM-10-13 · Navigation: Flight Management System
2006-07-19NM-06-56 ·
2002-03-13NE-02-18 · Air Cruisers Company Evacuation Slide and Slide/Raft Systems
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/85-24-02.json · aircraft systems.
