AD 91-10-07

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AD Number:
91-10-07
Document Type:
AD Final Rules
Docket Number:
91-NM-02-AD
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-10 Series Airplanes
Subject:
Cargo Door Bolts
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/11/1991
Make:
The Boeing Company
Model:
DC-10-10 | DC-10-10F | DC-10-15 | DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40 | DC-10-40F
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Superseded AD: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Superseded By: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: 91-10-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   91-NM-02-AD

AMENDMENT:   39-6991

AD NUMBER:   91-10-07

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-10 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 11, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-10-07 MCDONNELL DOUGLAS: Amendment 39-6991. Docket No. 91-NM-02-AD.

Applicability: All McDonnell Douglas Model DC-10 series airplanes, manufacturer's fuselage numbers 1 through 379, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent inadvertent opening of a cargo door in flight, a condition which could result in loss of pressurization and reduced controllability of the aircraft, accomplish the following:

A. Within 16 months after performing the torque test required by AD 90-19-12, Amendment 39-6735, perform magnetic particle inspections on the H-11 cargo door latch spool fitting attach bolts or replace the H-11 cargo door latch spool fitting attach bolts with new bolts and associated hardware, in accordance with the Accomplishment Instructions for Phase 2 of McDonnell Douglas DC-10 Alert Service Bulletin A52-212, Revision 1, dated September 14, 1990 (hereafter referred to as the "Service Bulletin").

1. If a bolt does not pass the magnetic particle inspection, prior to further flight, replace it with a new bolt and seal in accordance with Figure 1 of the Service Bulletin.

2. If a bolt passes the magnetic particle inspection, prior to further flight, reinstall the bolt and seal in accordance with the Service Bulletin.

B. Within 16 months after accomplishment of the inspections required by paragraph A. of this AD, and at intervals not to exceed sixteen months, replace the H-11 cargo door latch spool fitting attach bolts with new bolts and associated hardware or perform either a magnetic particle or ultrasonic inspection on the H-11 cargo door latch spool fitting attach bolts in accordance with the Accomplishment Instructions for Phase 2 of the Service Bulletin.

1. If a bolt does not pass the magnetic particle/ultrasonic inspection, prior to further flight, replace it with a new bolt and seal in accordance with Figure 1 of the Service Bulletin.

2. If a bolt passes the magnetic particle/ultrasonic inspection, prior to further flight, reinstall the bolt and seal in accordance with the Service Bulletin.

C. The inspections required by paragraphs A. and B. of this AD are not required for Inconel bolts, part numbers RA21026-7, 77711-7, and 3D0031-7.

D. Within five years after the effective date of this AD, replace all H-11 cargo door latch spool fitting attach bolts with Inconel bolts, part numbers RA21026-7, 77711-7, and 3D0031-7 (grip lengths as applicable per location as specified in Figure 1 sheets 3 and 4 of the Service Bulletin) in accordance with the Accomplishment Instructions for Phase 3 of the Service Bulletin. Installation of Inconel bolts constitutes terminating action for the requirements of paragraphs A. and B. of this AD.

E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes unpressurized to a base for the accomplishment of the requirements of this AD.

F. An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA Transport Airplane Directorate.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Los Angeles ACO.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, P.O. Box 1771, Long Beach, California 90846-0001, Attention: Business Unit Manager, Technical Publications, C1-HDR (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6991, AD 91-10-07) becomes effective on June 11, 1991.

FOOTER: