AD 78-10-04

final rule

Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's)

AD Number
78-10-04
Status
final_rule
Effective Date
Product Category
appliance
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Airesearch Auxiliary Power Units Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's)
appliance Airesearch Auxiliary Power Units Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's)

Unsafe Condition

High energy release of first stage compressor blades and disk parts due to possible fatigue failure of the disk.

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

Required Actions

Remove the first stage disk from the compressor section of the APU and replace with a like serviceable part. Operators must track cycles using defined parameters, including cycle definitions and approved ratios for unrecorded data.

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

Compliance Time

Before accumulating a total of more than 3000 cycles on the first stage compressor disks, or within the next 300 cycles after the effective date of this AD, whichever occurs later.

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

Affected Aircraft

AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's) with first stage compressor disks P/N's 969600-1 or -2 and the listed serial numbers.

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

Federal Register Abstract

Auxiliary Power Units

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_78-10-04.html
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AD Number:
78-10-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model...Show more
Subject:
Auxiliary Power Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/30/1978
Make:
Airesearch
Model:
Auxiliary Power Units
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 78-10-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3216

AD NUMBER:   78-10-04

SUBJECT HEADING:   Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's)

ACTION:  

SUMMARY:  

DATES:   Effective May 30, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-10-04 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-3216. Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's) which have first stage compressor disks P/N's 969600-1 or -2 installed, of the serial numbers listed.

Disk Serial No.


7-03501-2503
	7-03501-2531

7-03501-2504
	7-03501-2532

7-03501-2506
	7-03501-2538

7-03501-2507
	7-03501-2545

7-03501-2510
	7-03501-2546

7-03501-2511
	7-03501-2548

7-03501-2513
	7-03501-2549

7-03501-2514
	7-03501-2558

7-03501-2519
	7-03501-2582

7-03501-2522
	7-03501-2588

7-03501-2523
	7-03501-2599

7-03501-2526
	7-03501-2606

7-03501-2527
	7-03501-2619
	7-03501-2718

7-03501-2529
	7-03501-2743

Compliance required before accumulating a total of more than 3000 cycles on the first stage compressor disks, or within the next 300 cycles after the effective date of this AD, whichever occurs later, unless already accomplished:

To prevent a high energy release of first stage compressor blades and disk parts due to the possible fatigue failure of the disk, accomplish the following:

(a) Remove the first stage disk from the compressor section of the APU and replace with like serviceable part.

(b) For the purposes of this AD:

(1) A cycle is defined as a start and acceleration to at least 95% high pressure spool (N2) rpm followed by a shutdown, during which low pressure spool (N1) rpm reaches, or exceeds, 97% rpm nominal. If, in any start, operating and shutdown sequence, the low pressure spool (N1) is prevented from exceeding 91% rpm nominal, only one half of a cycle must be recorded.

(2) Operators who have not kept a record of operating starts on individual disks may assume two starts have occurred for each recorded APU operating hour of service, or any other cycle per hour ratio approved by the operators' assigned FAA maintenance inspector, provided the request contains substantiating data to justify the alternative ratio.

(3) Operators who have not kept a record of APU operating hours of service shall estimate hours of APU operation equating APU operation to airplane hours time in service using a ratio approved by the operator's assigned FAA maintenance inspector and justified by substantiating data.

NOTE: AiResearch Service Bulletin TSCP700-49-5016 dated April 25, 1978 refers to the same subject.

This amendment becomes effective May 30, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_78-10-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-10-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model...Show more
Subject:
Auxiliary Power Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/30/1978
Make:
Airesearch
Model:
Auxiliary Power Units
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 78-10-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3216

AD NUMBER:   78-10-04

SUBJECT HEADING:   Airworthiness Directives; AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's)

ACTION:  

SUMMARY:  

DATES:   Effective May 30, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-10-04 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA: Amendment 39-3216. Applies to AiResearch Model TSCP700-4B and -5 Auxiliary Power Units (APU's) which have first stage compressor disks P/N's 969600-1 or -2 installed, of the serial numbers listed.

Disk Serial No.


7-03501-2503
	7-03501-2531

7-03501-2504
	7-03501-2532

7-03501-2506
	7-03501-2538

7-03501-2507
	7-03501-2545

7-03501-2510
	7-03501-2546

7-03501-2511
	7-03501-2548

7-03501-2513
	7-03501-2549

7-03501-2514
	7-03501-2558

7-03501-2519
	7-03501-2582

7-03501-2522
	7-03501-2588

7-03501-2523
	7-03501-2599

7-03501-2526
	7-03501-2606

7-03501-2527
	7-03501-2619
	7-03501-2718

7-03501-2529
	7-03501-2743

Compliance required before accumulating a total of more than 3000 cycles on the first stage compressor disks, or within the next 300 cycles after the effective date of this AD, whichever occurs later, unless already accomplished:

To prevent a high energy release of first stage compressor blades and disk parts due to the possible fatigue failure of the disk, accomplish the following:

(a) Remove the first stage disk from the compressor section of the APU and replace with like serviceable part.

(b) For the purposes of this AD:

(1) A cycle is defined as a start and acceleration to at least 95% high pressure spool (N2) rpm followed by a shutdown, during which low pressure spool (N1) rpm reaches, or exceeds, 97% rpm nominal. If, in any start, operating and shutdown sequence, the low pressure spool (N1) is prevented from exceeding 91% rpm nominal, only one half of a cycle must be recorded.

(2) Operators who have not kept a record of operating starts on individual disks may assume two starts have occurred for each recorded APU operating hour of service, or any other cycle per hour ratio approved by the operators' assigned FAA maintenance inspector, provided the request contains substantiating data to justify the alternative ratio.

(3) Operators who have not kept a record of APU operating hours of service shall estimate hours of APU operation equating APU operation to airplane hours time in service using a ratio approved by the operator's assigned FAA maintenance inspector and justified by substantiating data.

NOTE: AiResearch Service Bulletin TSCP700-49-5016 dated April 25, 1978 refers to the same subject.

This amendment becomes effective May 30, 1978.

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.