AD 94-06-10

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AD Number:
94-06-10
Document Type:
AD Final Rules
Docket Number:
93-NM-163-AD
Subject Heading:
Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes
Subject:
Main Landing Gear Brakes
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/15/1994
Make:
The Boeing Company
Model:
DC-8-11 | DC-8-12 | DC-8-21 | DC-8-31 | DC-8-32 | DC-8-33 | DC-8-41 | DC-8-42 | DC-8-43 | DC-8-51 | ...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
93-09-10
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39 (59 FR 12158 NO. 51 03/16/94)
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 94-06-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   93-NM-163-AD

AMENDMENT:   39-8857

AD NUMBER:   94-06-10

SUBJECT HEADING:   Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes

ACTION:   Final rule.

SUMMARY:   This amendment supersedes an existing airworthiness directive (AD), applicable to all McDonnell Douglas Model DC-8 series airplanes, that currently requires the incorporation of specific maximum brake wear limits into the maintenance inspection program. That action was prompted by an accident in which a transport category airplane executed a rejected takeoff (RTO) and was unable to stop on the runway due to worn brakes. The actions specified by that AD are intended to prevent loss of braking effectiveness during a high energy RTO. This amendment requires that a new part number be permanently marked on certain brakes when modified to meet the new brake wear limits.

DATES:   Effective April 15, 1994.

ADDRESSES:   Information concerning this amendment may be obtained from or examined at the Federal Aviation Administration (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

FOR FURTHER INFORMATION CONTACT:   Andrew Gfrerer, Aerospace Engineer, Systems and Equipment Branch, ANM-131L, FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California 90806-2425; telephone (310) 988-5338; fax (310) 988-5210.

SUPPLEMENTARY INFORMATION:   A proposal to amend part 39 of the Federal Aviation Regulations by superseding AD 93-09-10, Amendment 39-8576 (58 FR 29347, May 20, 1993), which is applicable to all McDonnell Douglas Model DC-8 series airplanes, was published in the Federal Register on December 22, 1993 (58 FR 67723). That action proposed to require that a new part number be permanently marked on certain brakes when modified to meet the new brake wear limits.

Interested persons have been afforded an opportunity to participate in the making of this amendment. Due consideration has been given to the three comments received.

All commenters support the proposed rule.

After careful review of the available data, including the comments noted above, the FAA has determined that air safety and the public interest require the adoption of the rule as proposed.

There are approximately 337 McDonnell Douglas Model DC-8 series airplanes of the affected design in the worldwide fleet. The FAA estimates that 222 airplanes of U.S. registry were affected by AD 93-09-10, and would continue to be affected by this supersedure of that AD. It takes approximately 80 work hours per airplane to accomplish the actions currently required by AD 93-09-10, and the average labor rate is $55 per work hour. (There are 8 brakes per airplane.) The cost of required parts to accomplish the change in wear limits for these airplanes (that is, the cost resulting from the requirement to change the brakes before they are worn to their previously approved limits for a one-time change) is approximately $5,600 per airplane. Based on these figures, the current cost impact of the AD 93-09-10 on U.S. operators is estimated to be $2,220,000, or $10,000 per airplane.

The total cost figure indicated above is presented as if no operator has yet accomplished the requirements of AD 93-09-10 (or this supersedure of that AD). However, because AD 93-09-10 was effective on June 21, 1993, and operators were given 180 days to comply with it, the FAA assumes that the majority of affected operators have already accomplished the requirements of that AD.

The only foreseeable additional costs that may be imposed by this supersedure of AD 93-09-10 would be the cost of reidentifying (permanently marking) any modified brakes that were previously marked by a color code marking. The costs associated with that procedure are expected to be minimal.

The regulations adopted herein will not have substantial direct effects on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, in accordance with Executive Order 12612, it is determined that this final rule does not have sufficient federalism implications to warrant the preparation of a Federalism Assessment.

For the reasons discussed above, I certify that this action (1) is not a "significant regulatory action" under Executive Order 12866; (2) is not a "significant rule" under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption "ADDRESSES."

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends 14 CFR part 39 of the Federal Aviation Regulations as follows:

PART 39 - AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. App. 1354(a), 1421 and 1423; 49 U.S.C. 106(g); and 14 CFR 11.89.

§ 39.13 - [Amended]

2. Section 39.13 is amended by removing amendment 39-8576 (58 FR 29347, May 20, 1993), and by adding a new airworthiness directive (AD), amendment 39-8857, to read as follows:

REGULATORY TEXT:   94-06-10 MCDONNELL DOUGLAS: Amendment 39-8857. Docket 93-NM-163-AD. Supersedes AD 93-09-10, Amendment 39-8576.

Applicability: All Model DC-8 series airplanes, certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent the loss of main landing gear braking effectiveness, accomplish the following:

(a) Within 180 days after June 21, 1993 (the effective date of AD 93-09-10, Amendment 39-8576), inspect the main landing gear brakes having the part numbers indicated below to determine wear. Any brake worn more than the maximum wear limit specified below must be replaced, prior to further flight, with a brake that is within this limit.

Douglas Brake
Part Number	
Bendix
Part Number
	
Maximum Wear
Limit (inches)

		
5610206-5001	
150787-1
	
0.7

	
150787-2
	
0.7

		
5713612-5001	
151882-1
	
0.7

	
151882-2
	
0.7

		
5773335-5001	
154252-1
	
0.5

5773335-5501	
154252-2
	
0.5

		
5759262-5001	
2601412-1
	
0.5

	
2601412-2*
	
0.75

* Brakes having this part number include part number 2601412-1 brakes that have been modified and permanently marked in accordance with McDonnell Douglas Service Bulletin 32-181, Revision 2, dated August 25, 1993.

(b) Within 180 days after June 21, 1993, incorporate the maximum brake wear limits specified in paragraph (a) of this AD into the FAA-approved maintenance inspection program.

(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO.

(d) Special flight permits may be issued in accordance with Federal Aviation Regulations (FAR) 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(e) This amendment becomes effective on April 15, 1994.

FOOTER: