AD 99-02-51

Superseded

Starter Shaft Seal

Key Information
99-02-51
Superseded
April 20, 1999
Not specified
99-NE-01-AD
39-11108
Applicability
["Engine"]
Not specified
Not specified
AE 3007A AE 3007A1 AE 3007A1P AE 3007A1/1 AE 3007A1/2 AE 3007A1/3 AE 3007A3 AE 3007C
Summary

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 99-02-51 that was sent previously to all known U.S. owners and operators of Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines by individual telegrams. This AD prohibits, prior to further flight, all engine ground starts at oil temperatures below 32 deg. F (0 deg. C) unless preflight operational procedures ensure that engine oil temperature is maintained at or above 32 deg. F (0 deg. C). This amendment is prompted by reports of in-flight engine shutdowns. The in-flight engine shutdowns have been attributed to loss of engine oil from the starter shaft seal. The actions specified by this AD are intended to prevent an in-flight engine shutdown due to loss of engine oil from the starter shaft seal.

Action Required

Final rule, request for comments.

Regulatory Text

99-02-51 Allison Engine Company, Inc.: Amendment 39-11108: Docket 99-NE-01-AD.
Applicability: Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines, installed on but not limited to Embraer EMB-145 and Cessna 750 series airplanes.
Note 1: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
Compliance: Required as indicated, unless accomplished previously.
To prevent an in-flight engine shutdown due to loss of engine oil from the starter shaft seal, accomplish the following:
(a) Prior to further flight, all ground engine starts at engine oil temperatures below 32 deg. F (0 deg. C) are prohibited except as provided in paragraphs (a) (1) and (a) (2) of this AD.
(1) For Allison Engine Company engine models AE 3007A, AE 3007A1, AE 3007A1/1, and AE 3007A1/2, if the engine oil temperature has dropped below 32 deg. F (0 deg. C) prior to flight, perform a high-power leak check on each engine (at least three minutes at takeoff power, reference Allison Engine Company AE 3007A series maintenance manual, section 72-00-00, page 505, subtask 72-00-00-790-002). No leaks above serviceable limits are permitted (0.21 quarts/hour, 200 cc/hour per Allison Engine Company AE 3007A, Fault Isolation Manual, section 79-37-00, page 212, allowable leakage).
(2) ForAllison Engine Company engine model AE 3007C, if the engine oil temperature has dropped below 32 deg. F (0 deg. C) prior to flight, monitor the engine oil level using the following procedures:
(i) Operate engine at maximum continuous power for 10 minutes. Monitor the engine oil level.
(ii) If an oil level decrease of greater than 1.0 quarts occurs, maintenance is required before further flight.
(b) 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, Chicago Aircraft Certification Office. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Chicago Aircraft Certification Office.
Note 2: Information concerning the existence of approved alternative methods of compliance with this airworthiness directive, if any, may be obtained from the Chicago Aircraft Certification Office.
(c) This amendment becomes effective April 20, 1999, to all persons except those persons to whom it was made immediately effective by telegraphic AD 99-02-51, issued January 8, 1999, which contained the requirements of this amendment.

Supplementary Information

On January 8, 1999, the Federal Aviation Administration (FAA) issued telegraphic airworthiness directive (TAD) 99-02-51, applicable to Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines that prohibits, prior to further flight, all engine ground starts at oil temperatures below 32 deg. F (0 deg. C), unless preflight operational procedures ensure that engine oil temperature is maintained at or above 32 deg. F (0 deg. C). That action was prompted by reports of three in-flight engine shutdowns since January 4, 1999. The FAA has determined that engine starting in cold temperatures can cause the starter shaft seal to become unseated, allowing oil to exit the accessory gearbox. This condition, if not corrected, could result in an in-flight engine shutdown due to loss of engine oil from the starter shaft seal.
Since the unsafe condition described is likely to exist or develop on other engines of the same type design, the FAA issued telegraphic AD 99-02-51 to prevent an in-flight engine shutdown due to loss of engine oil from the starter shaft seal. This AD prohibits all engine ground starts at oil temperatures below 32 deg. F (0 deg. C) unless preflight operational procedures ensure that engine oil temperature is maintained at or above 32 deg. F (0 deg. C). This AD is considered an interim action, and as the investigation continues, further rulemaking may be necessary. The actions are required to be accomplished in accordance with the compliance section of this AD.
Since it was found that immediate corrective action was required, notice and opportunity for prior public comment thereon were impracticable and contrary to the public interest, and good cause existed to make the AD effective immediately by individual telegrams issued on January 8, 1999, to all known U.S. owners and operators of Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines. These conditions still exist, and the AD is hereby published in the Federal Register as an amendment to Section 39.13 of part 39 of the Federal Aviation Regulations (14 CFR part 39) to make it effective to all persons.

Comments Invited
Although this action is in the form of a final rule that involves requirements affecting flight safety and, thus, was not preceded by notice and an opportunity for public comment, comments are invited on this rule. Interested persons are invited to comment on this rule by submitting such written data, views, or arguments as they may desire. Communications should identify the Rules Docket number and be submitted in triplicate to the address specified under the caption "ADDRESSES." All communications received on or before the closing date for comments will be considered, and this rule may be amended in light of the comments received. Factual information that supports the commenter's ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether additional rulemaking action would be needed.
Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report that summarizes each FAA-public contact concerned with the substance of this AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this notice must submit a self-addressed, stamped postcard on which the following statement is made: "Comments to Docket Number 99-NE-01-AD." The postcard will be date stamped and returned to the commenter.
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.
The FAA has determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and is not a "significant regulatory action" under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket. A copy of it, if filed, may be obtained from the Rules Docket at the location provided under the caption "ADDRESSES." List of Subjects in 14 CFR Part 39
Airtransportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: PART 39 - AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 39.13 [Amended]
2. Section 39.13 is amended by adding the following new airworthiness directive:
U.S. Department of Transportation Federal Aviation Administration The following Airworthiness Directive issued by the Federal Aviation Administration in accordance with the provisions of Federal Aviation Regulations, Part 39, applies to an aircraft model of which our records indicate you may be the registered owner. Airworthiness Directives affect aviation safety and are regulations which require immediate attention. You are cautioned that no person may operate anaircraft to which an Airworthiness Directive applies, except in accordance with the requirements of the Airworthiness Directive (reference FAR Subpart 39.3).

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
Related ADs
2007-24-05 Replaced by the above
Contact Information

John Tallarovic, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 East Devon Ave., Des Plaines, IL 60018; telephone (847) 294-8180, fax (847) 294-7834.

References
Federal Register: April 05, 1999 (Volume 64, Number 64)
--- - Part 39 [64 FR 16339 NO. 64 04/05/99]
Page 16339
FAA Documents