AD 67-29-03

final rule

Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft

AD Number
67-29-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft Maryland Air Industries, Inc. F-27J Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
aircraft Maryland Air Industries, Inc. FH-227 Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
aircraft Maryland Air Industries, Inc. FH-227B Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
aircraft Maryland Air Industries, Inc. FH-227C Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
aircraft Maryland Air Industries, Inc. FH-227D Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
aircraft Maryland Air Industries, Inc. FH-227E Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft

Unsafe Condition

The APU fire detection system may have inadequate reliability and sensitivity due to insufficient fire detectors and non-fire resistant wiring in the fire detection circuit.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install an additional fire detector (Solar P/N 7447-2) within 100 operational APU hours. Install MIL-W-25038B fire resistant wire in the fire detection circuit within 100 operational APU hours. Replace existing 700 degree fire detectors (Solar P/N 7447-1) with 400+25 degree F detectors (Solar P/N 7447-2) within 200 operational APU hours.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 100 operational APU hours following the effective date of this AD (for paragraphs (a) and (b)), and within the next 200 operational APU hours for paragraph (c).

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Fairchild-Hiller Models F-27J and FH-227 aircraft with installed Solar Auxiliary Power Unit Model T-62T-25, Serial Nos. S-408000 to S-408099 inclusive.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

APU Fire Detection System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_67-29-03.html
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AD Number:
67-29-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
Subject:
APU Fire Detection System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/27/1967
Make:
Maryland Air Industries, Inc.
Model:
F-27J | FH-227 | FH-227B | FH-227C | FH-227D | FH-227E
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 67-29-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-499

AD NUMBER:   67-29-03

SUBJECT HEADING:   Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 27, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-29-03 FAIRCHILD-HILLER: Amdt. 39-499 Part 39 Federal Register October 25, 1967. Applies to all F-27J and FH-227 aircraft with installed Solar Auxiliary Power Unit Model T-62T-25, Serial Nos. S-408000 to S-408099 inclusive.

Compliance required as indicated unless already accomplished, or unless APU is rendered electrically inoperative and APU controls are placarded to prohibit operation.

To provide adequate APU fire detection system reliability and sensitivity, accomplish the following modifications:

(a) Within the next 100 operational APU hours following the effective date of this AD, install an additional fire detector, Solar P/N 7447-2, (set at 400 25 degrees F) in accordance with Fairchild-Hiller Service Bulletin Nos. F-27-49-4 Revision 3, dated Sept. 25, 1967 or FH-227-49-4 Revision 3 dated Sept. 25, 1967 as applicable, or later FAA approved revision, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(b) Within the next 100 operational APU hours following the effective date of this AD, install MIL-W-25038B fire resistant wire in the fire detection circuit in accordance with Fairchild-Hiller Service Bulletin Nos. F27-49-6 dated July 10, 1967 or FH227-49-6 dated July 10, 1967 as applicable, or later FAA-approved revision, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(c) Within the next 200 operational APU hours following the effective date of this AD, replace the two existing 700 degree fire detectors, Solar P/N 7447-1 with two 400 + 25 degree F Fire detectors Solar P/N 7447-2.

NOTE. - Compliance with paragraph (c) may be accomplished by arranging for the detector manufacturer, Fenwal, Inc. of 900 Main Street, Ashland, Massachusetts 01721, Solar P/N 7447-1 with two 400+25 degree F fire and reidentify the detector by P/N 7447-2.

(d) Upon the effective date of this AD, APU operational hours will be logged until such time as the entire AD has been complied with.

This amendment effective October 27, 1967.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_67-29-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-29-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft
Subject:
APU Fire Detection System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/27/1967
Make:
Maryland Air Industries, Inc.
Model:
F-27J | FH-227 | FH-227B | FH-227C | FH-227D | FH-227E
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 67-29-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-499

AD NUMBER:   67-29-03

SUBJECT HEADING:   Airworthiness Directives; Fairchild-Hiller Models F-27J and FH-227 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 27, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-29-03 FAIRCHILD-HILLER: Amdt. 39-499 Part 39 Federal Register October 25, 1967. Applies to all F-27J and FH-227 aircraft with installed Solar Auxiliary Power Unit Model T-62T-25, Serial Nos. S-408000 to S-408099 inclusive.

Compliance required as indicated unless already accomplished, or unless APU is rendered electrically inoperative and APU controls are placarded to prohibit operation.

To provide adequate APU fire detection system reliability and sensitivity, accomplish the following modifications:

(a) Within the next 100 operational APU hours following the effective date of this AD, install an additional fire detector, Solar P/N 7447-2, (set at 400 25 degrees F) in accordance with Fairchild-Hiller Service Bulletin Nos. F-27-49-4 Revision 3, dated Sept. 25, 1967 or FH-227-49-4 Revision 3 dated Sept. 25, 1967 as applicable, or later FAA approved revision, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(b) Within the next 100 operational APU hours following the effective date of this AD, install MIL-W-25038B fire resistant wire in the fire detection circuit in accordance with Fairchild-Hiller Service Bulletin Nos. F27-49-6 dated July 10, 1967 or FH227-49-6 dated July 10, 1967 as applicable, or later FAA-approved revision, or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

(c) Within the next 200 operational APU hours following the effective date of this AD, replace the two existing 700 degree fire detectors, Solar P/N 7447-1 with two 400 + 25 degree F Fire detectors Solar P/N 7447-2.

NOTE. - Compliance with paragraph (c) may be accomplished by arranging for the detector manufacturer, Fenwal, Inc. of 900 Main Street, Ashland, Massachusetts 01721, Solar P/N 7447-1 with two 400+25 degree F fire and reidentify the detector by P/N 7447-2.

(d) Upon the effective date of this AD, APU operational hours will be logged until such time as the entire AD has been complied with.

This amendment effective October 27, 1967.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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