Federal Register / Vol. 62, No. 63 / Wednesday, April 2, 1997 / Notices 15743

Thomas Boudreau, Engine and Propeller

Standards Staff, ANE–110, 12 New

England Executive Park, Burlington,

MA, 01803, telephone (617) 238–7117,

fax (617) 238–7199.

SUPPLEMENTARY INFORMATION:

Background

This AC is on the subject of vibration

tests and surveys, and was identified as

one where differences existed between

the Joint Aviation Requirements—

Engines, and part 33 of the Federal

Aviation Regulations (FAR’s). A study

group composed of representatives of

the Federal Aviation Administration,

the Joint Aviation Authorities,

Transport Canada and industry worked

to produce a set of improved and

harmonized requirements that was

subsequently incorporated into part 33

of the FAR.

Interested parties were given the

opportunity to review and comment on

the draft AC during the proposal and

development phases. Notice was

published in the Federal Register on

April 18, 1995 (60 FR 19442), to

announce the availability of, and

comment to the draft AC.

This advisory circular, published

under the authority granted to the

Administrator by 49 U.S.C. 106(g), 4113,

44701–44702, 44704, provides guidance

for these new requirements that were

published in the Federal Register on

June 4, 1996 (61 FR 28430).

Issued in Burlington, Massachusetts, on

March 25, 1997.

James C. Jones,

Acting Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 97–8278 Filed 4–1–97; 8:45 am]

BILLING CODE 4910–13–M

Advisory Circular; Continued Rotation

and Rotor Locking

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Notice of issuance Advisory

Circular (AC) on turbine engine

continued rotation and rotor locking.

SUMMARY: This notice announces the

issuance of Advisory Circular (AC), No.

33.74/92, Turbine Engine Continued

Rotation and Rotor Locking. This AC is

combining part 33 sections 33.74 and

33.92. This AC is on the subject of

continued rotation and rotor locking

tests. A set of improved and harmonized

requirements were incorporated into

part 33 of the Federal Aviation

Regulations (FAR’s), and this AC is

meant to provide information and

guidance concerning an acceptable

method, but not the only method, for

complying with those new harmonized

requirements.

DATES: Advisory Circular No. 33.74/92,

was issued by the new England Aircraft

Certification Service, Engine and

Propeller Directorate on February 14,

1997.

FOR FURTHER INFORMATION CONTACT:

Marc Bouthillier, Engine and Propeller

Standards Staff, ANE–110, 12 New

England Executive Park, Burlington,

MA, 01803, telephone (617) 238–7117,

fax (617) 238–7120.

SUPPLEMENTARY INFORMATION:

Background

This AC is on the subject of turbine

engine continued rotation and rotor

locking tests that were identified as one

where differences existed between the

Joint Aviation Requirements—Engines,

and part 33 of the Federal Aviation

Regulations (FAR’s). A study group

composed of representatives of the

Federal Aviation Administration, the

Joint Aviation Authorities, Transport

Canada and industry worked to produce

a set of improved and harmonized

requirements that was subsequently

incorporated into part 33 of the FAR.

Interested parties were given the

opportunity to review and comment on

the draft AC during the proposal and

development phases. Notice was

published in the Federal Register on

April 18, 1995 (60 FR 19442), to

announce the availability of, and

comment to the draft AC.

This advisory circular, published

under the authority granted to the

Administrator by 49 U.S.C. 106(g), 4113,

44701–44702, 44704, provides guidance

for these new requirements that were

published in the Federal Register on

June 4, 1996 (61 FR 28430).

Issued in Burlington, Massachusetts, on

March 26, 1997.

James C. Jones,

Acting Manager, Engine and Propeller

Directorate, Aircraft Certification Service.

[FR Doc. 97–8372 Filed 4–1–97; 8:45 am]

BILLING CODE 4910–13–M

[Summary Notice No. PE–97–18]

Petitions for Exemption; Summary of

Petitions Received; Dispositions of

Petitions Issued

AGENCY: Federal Aviation

Administration (FAA), DOT.

ACTION: Notice of petitions for

exemption received and of dispositions

of prior petitions.

SUMMARY: Pursuant to FAA’s rulemaking

provisions governing the application,

processing, and disposition of petitions

for exemption (14 CFR Part 11), this

notice contains a summary of certain

petitions seeking relief from specified

requirements of the Federal Aviation

Regulations (14 CFR Chapter I),

dispositions of certain petitions

previously received, and corrections.

The purpose of this notice is to improve

the public’s awareness of, and

participation in, this aspect of FAA’s

regulatory activities. Neither publication

of this notice nor the inclusion or

omission of information in the summary

is intended to affect the legal status of

any petition or its final disposition.

DATES: Comments on petitions received

must identify the petition docket

number involved and must be received

on or before April 22, 1997.

ADDRESSES: Send comments on any

petition in triplicate to: Federal

Aviation Administration, Office of the

Chief Counsel, Attn: Rule Docket (AGC–

2000), Petition Docket No. lllll,

800 Independence Avenue, SW.,

Washington, D.C. 20591.

Comments may also be sent

electronically to the following internet

address: 9–NPRM–CMTS@faa.dot.gov.

The petition, any comments received,

and a copy of any final disposition are

filed in the assigned regulatory docket

and are available for examination in the

Rules Docket (AGC–200), Room 915G,

FAA Headquarters Building (FOB 10A),

800 Independence Avenue, SW.,

Washington, D.C. 20591; telephone

(202) 267–3132.

FOR FURTHER INFORMATION CONTACT:

Fred Haynes (202) 267–3939 or Angela

Anderson (202) 267–9681 Office of

Rulemaking (ARM–1), Federal Aviation

Administration, 800 Independence

Avenue, SW., Washington, DC 20591.

This notice is published pursuant to

paragraphs (c), (e), and (g) of § 11.27 of

Part 11 of the Federal Aviation

Regulations (14 CFR Part 11).

Issued in Washington, D.C., on March 28,

1997.

Donald P. Byrne,

Assistant Chief Counsel for Regulations.

Petitions for Exemption

Docket No.: 28696.

Petitioner: Federal Express

Corporation.

Sections of the FAR Affected: 14 CFR

25.857(e) and 25.1447(c)(1).

Description of Relief Sought: To

provide accommodation for up to 24

supernumeraries at the aft portion of

DC–10/11 main deck Class E cargo

compartments, to accompany the

carriage of both live animal and

inanimate cargo.

Docket No.: 28822.

Petitioner: Lynx Air International.