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CFR Citation: 14 CFR Part 39

Docket ID: [Docket No. 2001-NE-21-AD]

RIN ID: RIN 2120-AA64

NOTICE: PROPOSED RULES

ACTION: Airworthiness directives:

DOCUMENT ACTION: Notice of proposed rulemaking (NPRM).

SUBJECT CATEGORY: Airworthiness Directives; General Electric Company CF34-3A1, -3B, and -3B1 Turbofan Engines

DATES: Comments must be received by September 8, 2003.

DOCUMENT SUMMARY: The Federal Aviation Administration (FAA) proposes to revise an existing airworthiness directive (AD) applicable to General Electric Company (GE) CF343A1, 3B, and 3B1 turbofan engines with scavenge screens part numbers (P/Ns) 4047T95P01 and 5054T86G02 installed in the Bsump oil scavenge system. That AD currently requires initial and repetitive visual inspections and cleaning of the Bsump scavenge screens until a screenless fitting is installed. This proposal requires the same initial and repetitive visual inspections and cleaning of the Bsump scavenge screens until a screenless fitting is installed. This proposal also corrects a typographical error, and introduces a less restrictive terminating action schedule. This proposal is prompted by the need to correct a typographical error and by the need to introduce a less restrictive terminating action schedule. The actions specified by the proposed AD are intended to prevent Bsump scavenge screen blockage due to coking which could result in ignition of Bsump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure.

SUMMARY: General Electric Co.,

SUPPLEMENTAL INFORMATION

Interested persons are invited to participate in the making of the [[Page 40574]]
proposed 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 above. All communications received on or before the closing date for comments, specified above, will be considered before taking action on the proposed rule. The proposals contained in this action may be changed in light of the comments received.

Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the proposed 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 summarizing each FAApublic contact concerned with the substance of this proposal will be filed in the Rules Docket.

Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this action must submit a selfaddressed, stamped postcard on which the following statement is made: ``Comments to Docket Number 2001NE21AD.'' The postcard will be date stamped and returned to the commenter.

Availability of NPRM's

Any person may obtain a copy of this NPRM by submitting a request to the FAA, New England Region, Office of the Regional Counsel, Attention: Rules Docket No. 2001NE21AD, 12 New England Executive Park, Burlington, MA 018035299.

Discussion

On March 6, 2003, the FAA issued AD 20030510, Amendment 3913086 (68 FR 12806, March 18, 2003), to require initial and repetitive visual inspections and cleaning of the Bsump scavenge screens until a screenless fitting is installed. That action was prompted by six reports of Bsump oil scavenge system failure causing engine inflight shutdowns. That condition, if not corrected, could result in ignition of Bsump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure.

Since AD 20030510 was issued, the FAA has recognized that a typographical error needs to be corrected in the Differences Between This AD and the Manufacturer's Service Information paragraph, and that a less restrictive terminating action schedule needs to be established. Manufacturer's Service Information

The FAA has reviewed and approved the technical contents of GE Aircraft Engines (GE) Alert Service Bulletin (ASB) CF34AL S/B 79 A0014, Revision 3, dated January 31, 2003; and ASB CF34BJ S/B 79 A0015, Revision 3, dated January 31, 2003; that describe procedures for initial and repetitive visual inspections and cleaning of the Bsump scavenge screens. The FAA has also reviewed and approved GE ASB CF34AL S/B 79A0016 and ASB CF34BJ S/B 79A0017, both dated June 17, 2002. These ASBs describe the procedures for introducing the screenless B sump scavenge fittings and for reworking to eliminate the screens from the existing scavenge screen fittings located at the forward and aft end of the lube and scavenge pump assembly, thereby terminating the repetitive inspections.
Differences Between This Proposed AD and the Manufacturer's Service Information

GE ASB CF34AL S/B 79A0014, Revision 3, dated January 31, 2003, recommends for engines with more than 4,000 hours timesincenew (TSN) or more than 1,000 hours timesincelastshopvisit (TSLSV), initial visual inspections and cleaning of the Bsump scavenge screens ``by the next Acheck''. GE ASB CF34BJ S/B 79A0015, Revision 3, dated January 31, 2003, recommends for engines with more than 4,000 hours TSN or more than 1,000 hours TSLSV, initial visual inspections and cleaning of the Bsump scavenge screens within 300 hours for the CF343A1 engine model or within 400 hours for the CF343B engine model. However, this proposed AD would require initial visual inspections and cleaning of the Bsump scavenge screens within 500 hours after the effective date of this proposed AD. The time intervals have been changed from those cited in the ASBs to provide consistency for all engine models and to eliminate the use of aircraft maintenance terminology. The times are approximately equivalent to the Acheck intervals.

GE ASBs CF34AL S/B 79A0016, dated June 17, 2002; and CF34BJ S/B 79A0017, dated June 17, 2002; recommend for engines with more than 4,000 hours TSN or more than 1,000 hours TSLSV, replacement of existing scavenge screens P/Ns 4047T95P01 and 5054T86G02, installed in the B sump oil scavenge system, with screenless fittings ``by the next A check''. However, this proposed AD would require installation of screenless fittings, or fittings that have been reworked to remove the screens, in the Bsump oil scavenge system within 500 hours after the effective date of this proposed AD. The installation requirement has been changed from that cited in the ASBs to eliminate the use of aircraft maintenance terminology. The time is approximately equivalent to the Acheck interval.
FAA's Determination of an Unsafe Condition and Proposed Actions

Since an unsafe condition has been identified that is likely to exist or develop on other GE CF343A1, 3B, and 3B1 turbofan engines of the same type design, this proposed AD is being issued to prevent B sump scavenge screen blockage due to coking, which could result in ignition of Bsump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure. This proposed AD would require:
[sbull] Initial visual inspection and cleaning of the scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump oil scavenge system.
[sbull] Repetitive visual inspection and cleaning of the scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump oil scavenge system, within 200 hours timesincelast inspection (TSLI) if no coking is found.
[sbull] Repetitive visual inspection and cleaning of the scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump scavenge system, within 100 hours TSLI if any coking is found. [sbull] Replacement of existing scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump oil scavenge system, with screenless fittings.

The actions must be done in accordance with the service bulletins described previously.

Economic Analysis

There are approximately 940 engines of the affected design in the worldwide fleet. The FAA estimates that 576 engines installed on aircraft of U.S. registry would be affected by this proposed AD. The FAA also estimates that it would take approximately 10.0 work hours per engine to perform the proposed actions, and that the average labor rate is $65 per work hour. Required parts would cost approximately $1,050 per engine. Based on these figures, the total cost of the proposed AD to U.S. operators is estimated to be $979,200.

Regulatory Analysis

This proposed rule does not have federalism implications, as defined in Executive Order 13132, because it
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would not have a substantial direct effect 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. Accordingly, the FAA has not consulted with state authorities prior to publication of this proposed rule.

For the reasons discussed above, I certify that this proposed regulation (1) is not a ``significant regulatory action'' under Executive Order 12866; (2) is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) if promulgated, 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 copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting 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. The Proposed Amendment

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

PART 39AIRWORTHINESS DIRECTIVES

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

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

2. Section 39.13 is amended by removing Amendment 3913086 (68 FR 12806, March 18, 2003), and by adding a new airworthiness directive, to read as follows:
General Electric Company: Docket No. 2001NE21AD. Revises AD 2003 0510, Amendment 3913086.

Applicability: This airworthiness directive (AD) is applicable to General Electric Company (GE) CF343A1, 3B, and 3B1 turbofan engines with scavenge screens part numbers (P/Ns) 4047T95P01 and 5054T86G02 installed in the Bsump oil scavenge system. These engines are installed on, but not limited to, Bombardier Inc. (Canadair) Model CL6002A12, CL6002B16, and CL6002B19

airplanes.

Note 1: This 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 (d) 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: Compliance with this AD is required as indicated, unless already done.

To prevent Bsump scavenge screen blockage due to coking, which could result in ignition of Bsump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure, do the following:
Initial Inspection and Cleaning of BSump Screens
(a) Perform an initial visual inspection and cleaning of scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump oil scavenge system, in accordance with Paragraphs 3A through 3B of the Accomplishment Instructions of GE Aircraft Engines (GE) Alert Service Bulletin (ASB) CF34AL S/B 79A0014, Revision 3, dated January 31, 2003; or ASB CF34BJ S/B 79A0015, Revision 3, dated January 31, 2003; and the following table:
Initial Inspection and Cleaning Schedule
Engine hours timesincenew (TSN) or time
sincelastshopvisit (TSLSV) Inspect and clean (1) Fewer than 4,000 hours TSN or fewer than Before 4,000 hours TSN or 4,000 hours TSLSV if it can be confirmed TSLSV.
that both the Bsump scavenge screens were
cleaned and the Bsump and combustor frame
(strut tubes) were removed from the engine
and cleaned at that prior shop visit.
(2) Fewer than 1,000 hours TSLSV if it can Before 1,000 hours TSLSV. NOT be confirmed that both the Bsump
scavenge screens were cleaned and the Bsump
and combustor frame (strut tubes) were
removed from the engine and cleaned at that
prior shop visit.
(3) 4,000 hours or greater TSN or 4,000 hours Within 500 hours timein or greater TSLSV if it can be confirmed that service (TIS) after the both the Bsump scavenge screens were effective date of this cleaned and the Bsump and combustor frame AD.
(strut tubes) were removed from the engine
and cleaned at that prior shop visit, or
1,000 hours or greater TSLSV if it can NOT
be confirmed that both the Bsump scavenge
screens were cleaned and the Bsump and
combustor frame (strut tubes) were removed
from the engine and cleaned at that prior
shop visit.
Repetitive Inspections and Cleaning
(b) Perform repetitive visual inspections and cleaning of scavenge screens, P/Ns 4047T95P01 and 5054T86G02, installed in the Bsump oil scavenge system, in accordance with Paragraphs 3A through 3B of the Accomplishment Instructions of GE ASB CF34AL S/B 79 A0014, Revision 3, dated January 31, 2003; and ASB CF34BJ S/B 79 A0015, Revision 3, dated January 31, 2003; and the following: (1) At intervals not to exceed 200 hours timesincelast
inspection (TSLI), if no coke is found in screens during initial or any prior inspections, or
(2) At intervals not to exceed 100 hours TSLI, if coke is found in screens during initial or any prior inspections.
Terminating Actions
(c) Install new screenless fittings or fittings that have been reworked to remove the screens, in the Bsump oil scavenge system, in accordance with GE ASB CF34AL S/B 79A0016, dated June 17, 2002; or ASB CF34BJ S/B 79A0017, dated June 17, 2002, and the following schedule:
(1) For engines with more than 4,000 hours TSN, within 500 hours TIS after the effective date of the AD, or within 1,000 hours TSLSV, whichever occurs first.
(2) For engines with less than or equal to 4,000 hours TSN, prior to 4,500 hours TSN.

This constitutes terminating action to the inspections required in paragraph (b) of this AD.
Alternative Methods of Compliance
(d) 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, Engine Certification Office (ECO). Operators must submit their request through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, ECO.

Note 2: Information concerning the existence of approved alternative methods of compliance with this airworthiness directive, if any, may be obtained from the ECO.
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Special Flight Permits
(e) Special flight permits may be issued in accordance with Sec. Sec. 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be done.

Issued in Burlington, Massachusetts, on June 30, 2003. Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.
[FR Doc. 0317178 Filed 7703; 8:45 am]
BILLING CODE 491013P

FOR FURTHER INFORMATION CONTACT Barbara Caufield, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 018035299; telephone (781) 2387146; fax (781) 2387199.