AD 54-22-01

final rule

LOCKHEED Models 49, 649, 749, and 1049 Airplanes

AD Number
54-22-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Aircraft Corporation 1049-54 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 1049B-55 (Navy R7V-1) LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 1049C-55 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 1049D-55 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 1049E-55 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 649-79 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 649A-79 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 749-79 LOCKHEED Models 49, 649, 749, and 1049 Airplanes
aircraft Lockheed Aircraft Corporation 749A-79 LOCKHEED Models 49, 649, 749, and 1049 Airplanes

Unsafe Condition

Premature failure of flexible hose in the feathering line and penetration of fire from zone 1 into zone 2 due to engine fire.

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

Required Actions

Replace flexible hose assemblies with those meeting current fire resistance requirements per specified service bulletins. Install steel plates over lower engine cowling longerons adjacent to the diaphragm per service bulletins.

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

Compliance Time

April 1, 1955

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

Affected Aircraft

Lockheed Models 49, 649, 749, and 1049 airplanes as noted in referenced service bulletins.

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

Federal Register Abstract

Flexible Hose Replacement

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_54-22-01.html
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Details
AD Number:
54-22-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Models 49, 649, 749, and 1049 Airplanes
Subject:
Flexible Hose Replacement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 49-46 | 649-79 | 649A-79 | 749-79...Show more
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: 54-22-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   54-22-01

SUBJECT HEADING:   LOCKHEED Models 49, 649, 749, and 1049 Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
54-22-01 LOCKHEED: Applies to Models 49, 649, 749, and 1049 Airplanes as Noted in Referenced Service Bulletins.

Compliance required by April 1, 1955.

A recent engine fire resulted in a premature failure of a flexible hose in the feathering line and in penetration of fire from zone 1 into zone 2.

1. To increase the fire resistance integrity of the propeller feathering line between the pump and the governor, replace the existing flexible hose assemblies meeting current fire resistance requirements. The following Lockheed Service Bulletins cover this subject: No. 49/SB-786 for Model 049 through 749 airplanes and No. 1049/SB-2195 for Model 1049 airplanes. The following hose assemblies may also be considered acceptable for this application:

(a) Aeroquip 680-10S hose assemblies with Aeroquip 304 protective sleeves over end fittings.

(b) Resistoflex - SSFR-3800-10 hose assemblies.

2. To increase the fireproof integrity of the zone 1 fire seal diaphragm against burn-through into zone 2 in the event of a power section fire install steel plates over the lower engine cowling longerons adjacent to the diaphragm. The following Lockheed Service Bulletins cover this subject: No. 49/SB-760 for Model 649/749 airplanes and No. 1049/SB-2115 for Model 1049 airplanes.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_54-22-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
54-22-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Models 49, 649, 749, and 1049 Airplanes
Subject:
Flexible Hose Replacement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Lockheed Aircraft Corporation
Model:
1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 49-46 | 649-79 | 649A-79 | 749-79...Show more
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: 54-22-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   54-22-01

SUBJECT HEADING:   LOCKHEED Models 49, 649, 749, and 1049 Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
54-22-01 LOCKHEED: Applies to Models 49, 649, 749, and 1049 Airplanes as Noted in Referenced Service Bulletins.

Compliance required by April 1, 1955.

A recent engine fire resulted in a premature failure of a flexible hose in the feathering line and in penetration of fire from zone 1 into zone 2.

1. To increase the fire resistance integrity of the propeller feathering line between the pump and the governor, replace the existing flexible hose assemblies meeting current fire resistance requirements. The following Lockheed Service Bulletins cover this subject: No. 49/SB-786 for Model 049 through 749 airplanes and No. 1049/SB-2195 for Model 1049 airplanes. The following hose assemblies may also be considered acceptable for this application:

(a) Aeroquip 680-10S hose assemblies with Aeroquip 304 protective sleeves over end fittings.

(b) Resistoflex - SSFR-3800-10 hose assemblies.

2. To increase the fireproof integrity of the zone 1 fire seal diaphragm against burn-through into zone 2 in the event of a power section fire install steel plates over the lower engine cowling longerons adjacent to the diaphragm. The following Lockheed Service Bulletins cover this subject: No. 49/SB-760 for Model 649/749 airplanes and No. 1049/SB-2115 for Model 1049 airplanes.

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.