AD 85-24-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-8-71 | Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes |
| aircraft | The Boeing Company | DC-8-72 | Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes |
| aircraft | The Boeing Company | DC-8-73 | Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes |
Unsafe Condition
Potential APU exhaust door failures and resulting wiring and structural damage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Complete modifications defined in McDonnell Douglas DC-8-70 Service Bulletin 49-2 within six months after the effective date. Modifications include removal of the APU, modification of the APU module and control boxes, revision of the APU control system sensing and firex control wiring, replacement of three generator phase circuit breakers and APU control and fuel supply circuit breakers, inspection of wire routing, and reinstallation of the APU.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within six (6) months after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-8-70 series airplanes equipped with an auxiliary power unit in accordance with STC SA1387NM
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Modifications In SB 49-2
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_85-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes Subject: Modifications In SB 49-2 Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/19/1985 Make: The Boeing Company Model: DC-8-71 | DC-8-72 | DC-8-73 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 85-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5169 AD NUMBER: 85-24-01 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes ACTION: SUMMARY: DATES: Effective December 19, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-24-01 MCDONNELL DOUGLAS: Amendment 39-5169. Applies to McDonnell Douglas Model DC-8-70 series airplanes, equipped with an auxiliary power unit in accordance with STC SA1387NM. Compliance is required as indicated. To preclude potential APU exhaust door failures and resulting wiring and structural damage, accomplish the following, unless already accomplished: A. Within six (6) months after the effective date of this AD, complete the modifications defined in McDonnell Douglas DC-8-70 Service Bulletin 49-2, dated May 16, 1985, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. The modifications involve removal of the APU; modification of the APU module and control boxes; revision of the APU control system sensing and firex control wiring; replacement of three generator phase circuit breakers; and the APU control and fuel supply circuit breakers; inspection of the wire routing; and reinstallation of the APU. 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 which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective December 19, 1985. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_85-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes Subject: Modifications In SB 49-2 Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/19/1985 Make: The Boeing Company Model: DC-8-71 | DC-8-72 | DC-8-73 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 85-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5169 AD NUMBER: 85-24-01 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-8-70 Series Airplanes ACTION: SUMMARY: DATES: Effective December 19, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-24-01 MCDONNELL DOUGLAS: Amendment 39-5169. Applies to McDonnell Douglas Model DC-8-70 series airplanes, equipped with an auxiliary power unit in accordance with STC SA1387NM. Compliance is required as indicated. To preclude potential APU exhaust door failures and resulting wiring and structural damage, accomplish the following, unless already accomplished: A. Within six (6) months after the effective date of this AD, complete the modifications defined in McDonnell Douglas DC-8-70 Service Bulletin 49-2, dated May 16, 1985, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. The modifications involve removal of the APU; modification of the APU module and control boxes; revision of the APU control system sensing and firex control wiring; replacement of three generator phase circuit breakers; and the APU control and fuel supply circuit breakers; inspection of the wire routing; and reinstallation of the APU. 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 which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective December 19, 1985. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.