AD 52-12-01

final rule

BOEING Model 377 Aircraft

AD Number
52-12-01
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 Aero Spacelines Incorporated 377 BOEING Model 377 Aircraft
aircraft Aero Spacelines Incorporated 377MG BOEING Model 377 Aircraft
aircraft Aero Spacelines Incorporated 377SGT BOEING Model 377 Aircraft

Unsafe Condition

Overheating of the freon compressor motors could result in fire.

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

Required Actions

Replace magnesium parts with aluminum parts (P/N P14A9709 to P35A9046, P14A9712 to P35A9044, A14B3724 to P35A9042) or install a temperature sensing switch actuating at 100 degrees or less with associated circuits and equipment. Alternatively, operate the aircraft with refrigeration systems inoperative.

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

Compliance Time

Before any installation of overhauled or new compressor motor after October 1, 1952 (for item A) or prior to October 1, 1952 (for item B).

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

Affected Aircraft

Aero Spacelines Incorporated Model 377, 377MG, 377SGT aircraft.

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

Federal Register Abstract

Compressor Motors

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_52-12-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
52-12-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 377 Aircraft
Subject:
Compressor Motors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
12/04/1956
Effective Date:
Make:
Aero Spacelines Incorporated
Model:
377 | 377MG | 377SGT
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
Unable to find issue date
AIRWORTHINESS DIRECTIVES FINAL RULES: 52-12-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-12-01

SUBJECT HEADING:   BOEING Model 377 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   52-12-01 BOEING: Applies to all Model 377 Aircraft.
Compliance required as specified below.
In order to reduce the hazard of fire resulting from overheating of the freon compressor motors, compliance with the following is required:
A. Compliance required before any installation of overhauled or new compressor motor after October 1, 1952. (Not required if item B accomplished or airplane operated in accordance item C.)
Replace the following Westinghouse compressor motor magnesium parts with corresponding aluminum parts:


. . . . . . . . . . . . . . . . . P/N (Mg.) P/N (AL.)
Inlet Cooling Cap P14A9709 P35A9046
Front Bearing Bracket P14A9712 P35A9044
Fan A14B3724 P35A9042


B. Compliance required prior to October 1, 1952. (Not required if both motors previously modified in accordance item A or if airplane operated in accordance item C.)
Install a temperature sensing switch, adjusted to actuate at 100 degrees or less, in the cooling air outlet of each freon compressor motor. Install circuits and equipment so that this overheat switch, as well as the motor thermoguard switch, will illuminate a cockpit warning light or will open the compressor motor power circuit, or both.
C. In the event the modifications outlined in A or B are not completed in accordance with the above requirements, aircraft may be operated with the refrigeration systems made inoperative.



FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_52-12-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
52-12-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 377 Aircraft
Subject:
Compressor Motors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
12/04/1956
Effective Date:
Make:
Aero Spacelines Incorporated
Model:
377 | 377MG | 377SGT
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
Unable to find issue date
AIRWORTHINESS DIRECTIVES FINAL RULES: 52-12-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-12-01

SUBJECT HEADING:   BOEING Model 377 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   52-12-01 BOEING: Applies to all Model 377 Aircraft.
Compliance required as specified below.
In order to reduce the hazard of fire resulting from overheating of the freon compressor motors, compliance with the following is required:
A. Compliance required before any installation of overhauled or new compressor motor after October 1, 1952. (Not required if item B accomplished or airplane operated in accordance item C.)
Replace the following Westinghouse compressor motor magnesium parts with corresponding aluminum parts:


. . . . . . . . . . . . . . . . . P/N (Mg.) P/N (AL.)
Inlet Cooling Cap P14A9709 P35A9046
Front Bearing Bracket P14A9712 P35A9044
Fan A14B3724 P35A9042


B. Compliance required prior to October 1, 1952. (Not required if both motors previously modified in accordance item A or if airplane operated in accordance item C.)
Install a temperature sensing switch, adjusted to actuate at 100 degrees or less, in the cooling air outlet of each freon compressor motor. Install circuits and equipment so that this overheat switch, as well as the motor thermoguard switch, will illuminate a cockpit warning light or will open the compressor motor power circuit, or both.
C. In the event the modifications outlined in A or B are not completed in accordance with the above requirements, aircraft may be operated with the refrigeration systems made inoperative.



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.