AD 75-17-32

final rule

DETROIT DIESEL ALLISON Model 501-D13 Series Engines

AD Number
75-17-32
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation 501-D13 DETROIT DIESEL ALLISON Model 501-D13 Series Engines
engine Rolls-Royce Corporation 501-D13A DETROIT DIESEL ALLISON Model 501-D13 Series Engines
engine Rolls-Royce Corporation 501-D13D DETROIT DIESEL ALLISON Model 501-D13 Series Engines
engine Rolls-Royce Corporation 501-D13E DETROIT DIESEL ALLISON Model 501-D13 Series Engines
engine Rolls-Royce Corporation 501-D13H DETROIT DIESEL ALLISON Model 501-D13 Series Engines

Unsafe Condition

Second stage turbine wheels with part number 6829072 may develop cracks due to fatigue, leading to engine failure.

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

Required Actions

Remove from service turbine wheels based on inspection history and cycle counts as specified in the schedules outlined in sections I, II, III. Inspections must be performed using the fluorescent penetrant method FP-30A/ZL-30A.

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

Compliance Time

Compliance required as indicated in the schedules (e.g., within 100 cycles from the effective date or prior to exceeding specified cycle limits).

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

Affected Aircraft

Rolls-Royce Corporation Model 501-D13 series engines with second stage turbine wheels part number 6829072 and serial numbers listed in the AD (e.g., KK14208 to KK15500), including wheels with R1-R5 suffixes.

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

Federal Register Abstract

Second Stage Turbine Wheels

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-17-32.html
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AD Number:
75-17-32
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DETROIT DIESEL ALLISON Model 501-D13 Series Engines
Subject:
Second Stage Turbine Wheels
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/14/1975
Make:
Rolls-Royce Corporation
Model:
501-D13 | 501-D13A | 501-D13D | 501-D13E | 501-D13H
Product Type:
Engine
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: 75-17-32
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2336

AD NUMBER:   75-17-32

SUBJECT HEADING:   DETROIT DIESEL ALLISON Model 501-D13 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 14, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-32 DETROIT DIESEL ALLISON: Amendment 39-2336. Applies to Detroit Diesel Allison Model 501-D13 series engines which incorporate P/N 6829072 second stage turbine wheels with the following serial numbers:


KK14208	KK14421	KK14443	KK14460	KK15456	KK15484
KK14210	KK14422	KK14445	KK14461	KK15457	KK15485
KK14211	KK14423	KK14446	KK14463	KK15471	KK15486
KK14403	KK14424	KK14447	KK14464	KK15472	KK15487
KK14405	KK14427	KK14448	KK14465	KK15473	KK15489
KK14406	KK14428	KK14449	KK14817	KK15474	KK15490
KK14407	KK14430	KK14450	KK14819	KK15475	KK15492
KK14408	KK14431	KK14451	KK14821	KK15476	KK15493
KK14409	KK14432	KK14452	KK14822	KK15477	KK15494
KK14413	KK14434	KK14453	KK14823	KK15478	KK15495
KK14414	KK14435	KK14454	KK14825	KK15479	KK15496
KK14416	KK14436	KK14455	KK15451	KK15480	KK15497
KK14417	KK14437	KK14456	KK15452	KK15481	KK15498
KK14418	KK14440	KK14457	KK15453	KK15483	KK15500
KK14420	KK14442	KK14459	KK15454		

Note: At time of overhaul, some wheels have R1, R2, R3, R4 or R5 added as a suffix to the wheel serial number. The suffix should be disregarded in determining the applicability of this airworthiness directive.

Compliance required as indicated.

I. Remove from service wheels which have not been inspected since installation as new wheels, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 6900 cycles.

(b) Remove from service prior to exceeding 7000 cycles, wheels with not more than 6900 cycles, on the effective date of this Airworthiness Directive.

II. Remove from service wheels which have been inspected by fluorescent penetrant method FP- 30A/ZL-30A at last inspection, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 3900 cycles since last inspection or more than 9400 total cycles, whichever occurs first.

(b) Remove from service prior to exceeding 4000 cycles since last inspection or 9500 total cycles, whichever occurs first, wheels with not more than 3900 cycles since last inspection or not more than 9400 total cycles on the effective date of this Airworthiness Directive.

Note: If the method of fluorescent penetrant inspection used at last inspection cannot be determined, it must be assumed that FP-30A/ZL-30A was not used.

III. Remove from service wheels which have been inspected by a fluorescent penetrant method other than FP-30A/ZL-30A at last inspection, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 2400 cycles since last inspection, or more than 9400 total cycles, whichever occurs first.

(b) Remove from service prior to exceeding 2500 cycles since last inspection or 9500 total cycles, whichever occurs first, wheels with not more than 2400 cycles since last inspection or not more than 9400 total cycles on the effective date of this Airworthiness Directive.

IV. or the purposes of this airworthiness directive, a cycle is defined as one takeoff.

V. Detroit Diesel Allison Commercial Service Letter 501D13 CSL-234 pertains to this subject.

This amendment is effective August 14, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-17-32.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-17-32
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DETROIT DIESEL ALLISON Model 501-D13 Series Engines
Subject:
Second Stage Turbine Wheels
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/14/1975
Make:
Rolls-Royce Corporation
Model:
501-D13 | 501-D13A | 501-D13D | 501-D13E | 501-D13H
Product Type:
Engine
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: 75-17-32
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2336

AD NUMBER:   75-17-32

SUBJECT HEADING:   DETROIT DIESEL ALLISON Model 501-D13 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 14, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-32 DETROIT DIESEL ALLISON: Amendment 39-2336. Applies to Detroit Diesel Allison Model 501-D13 series engines which incorporate P/N 6829072 second stage turbine wheels with the following serial numbers:


KK14208	KK14421	KK14443	KK14460	KK15456	KK15484
KK14210	KK14422	KK14445	KK14461	KK15457	KK15485
KK14211	KK14423	KK14446	KK14463	KK15471	KK15486
KK14403	KK14424	KK14447	KK14464	KK15472	KK15487
KK14405	KK14427	KK14448	KK14465	KK15473	KK15489
KK14406	KK14428	KK14449	KK14817	KK15474	KK15490
KK14407	KK14430	KK14450	KK14819	KK15475	KK15492
KK14408	KK14431	KK14451	KK14821	KK15476	KK15493
KK14409	KK14432	KK14452	KK14822	KK15477	KK15494
KK14413	KK14434	KK14453	KK14823	KK15478	KK15495
KK14414	KK14435	KK14454	KK14825	KK15479	KK15496
KK14416	KK14436	KK14455	KK15451	KK15480	KK15497
KK14417	KK14437	KK14456	KK15452	KK15481	KK15498
KK14418	KK14440	KK14457	KK15453	KK15483	KK15500
KK14420	KK14442	KK14459	KK15454		

Note: At time of overhaul, some wheels have R1, R2, R3, R4 or R5 added as a suffix to the wheel serial number. The suffix should be disregarded in determining the applicability of this airworthiness directive.

Compliance required as indicated.

I. Remove from service wheels which have not been inspected since installation as new wheels, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 6900 cycles.

(b) Remove from service prior to exceeding 7000 cycles, wheels with not more than 6900 cycles, on the effective date of this Airworthiness Directive.

II. Remove from service wheels which have been inspected by fluorescent penetrant method FP- 30A/ZL-30A at last inspection, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 3900 cycles since last inspection or more than 9400 total cycles, whichever occurs first.

(b) Remove from service prior to exceeding 4000 cycles since last inspection or 9500 total cycles, whichever occurs first, wheels with not more than 3900 cycles since last inspection or not more than 9400 total cycles on the effective date of this Airworthiness Directive.

Note: If the method of fluorescent penetrant inspection used at last inspection cannot be determined, it must be assumed that FP-30A/ZL-30A was not used.

III. Remove from service wheels which have been inspected by a fluorescent penetrant method other than FP-30A/ZL-30A at last inspection, according to the following schedule:

(a) Remove from service within 100 cycles from the effective date of this Airworthiness Directive, wheels with more than 2400 cycles since last inspection, or more than 9400 total cycles, whichever occurs first.

(b) Remove from service prior to exceeding 2500 cycles since last inspection or 9500 total cycles, whichever occurs first, wheels with not more than 2400 cycles since last inspection or not more than 9400 total cycles on the effective date of this Airworthiness Directive.

IV. or the purposes of this airworthiness directive, a cycle is defined as one takeoff.

V. Detroit Diesel Allison Commercial Service Letter 501D13 CSL-234 pertains to this subject.

This amendment is effective August 14, 1975.

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.