Code of Federal Regulations - Title 14

898

14 CFR Ch. I (1–1–14 Edition)

§ 34.61–31.71

LTO T

EST

YCLES AND

IME IN

ODE

Mode

Class

TF, T3, T8

TSS

TIM (min)

% of rO

TIM (min)

% of rO

TIM (min)

% of rO

Taxi/idle .................................................

26.0 7

26.0

5.8

Takeoff ..................................................

0.5 100 0.7 100 1.2 100

Climbout ................................................

2.5 90 2.2 85 2.0 65

Descent .................................................

NA NA NA NA 1.2 15

Approach ...............................................

4.5 30 4.0 30 2.3 34

(g) Engines comply with an applica-

ble standard if the testing results show
that the engine type certificate fam-
ily’s characteristic level does not ex-
ceed the numerical level of that stand-
ard, as described in the applicable ap-
pendix of Annex 16.

(h) The system and procedure for

sampling and measurement of gaseous
emissions shall be as specified by in
Appendices 2, 3, 4, 5 and 6 to the Inter-
national Civil Aviation Organization
(ICAO) Annex 16, Environmental Pro-
tection, Volume II, Aircraft Engine
Emissions, Third Edition, July 2008.
This incorporation by reference was ap-
proved by the Director of the Federal
Register in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. This docu-
ment can be obtained from the ICAO,
Document Sales Unit, 999 University
Street, Montreal, Quebec H3C 5H7, Can-
ada, phone +1 514–954–8022, or
www.icao.int or sales25icao.int. Copies
can be reviewed at the FAA New Eng-
land Regional Office, 12 New England
Executive Park, Burlington, Massachu-
setts, 781–238–7101, or at the National
Archives and Records Administration
(NARA). For information on the avail-
ability of this material at NARA, call
202–741–6030, or go to:

http://

www.archives.gov/federal

lregister/

code

loflfederallregulations/

ibr

llocations.html.

[Doc. No. FAA–2012–1333, 77 FR 76853, Dec. 31,
2012]

§ 34.61–31.71

[Reserved]

PART 35—AIRWORTHINESS

STANDARDS: PROPELLERS

Subpart A—General

Sec.
35.1

Applicability.

35.2

Propeller configuration.

35.3

Instructions for propeller installation

and operation.

35.4

Instructions for Continued Airworthi-

ness.

35.5

Propeller ratings and operating limita-

tions.

35.7

Features and characteristics.

Subpart B—Design and Construction

35.11

[Reserved]

35.13

[Reserved]

35.15

Safety analysis.

35.16

Propeller critical parts.

35.17

Materials and manufacturing methods.

35.19

Durability.

35.21

Variable and reversible pitch propel-

lers.

35.22

Feathering propellers.

35.23

Propeller control system.

35.24

Strength.

Subpart C—Tests and Inspections

35.31

[Reserved]

35.33

General.

35.34

Inspections, adjustments and repairs.

35.35

Centrifugal load tests.

35.36

Bird impact.

35.37

Fatigue limits and evaluation.

35.38

Lightning strike.

35.39

Endurance test.

35.40

Functional test.

35.41

Overspeed and overtorque.

35.42

Components of the propeller control

system.

35.43

Propeller hydraulic components.

35.45

[Reserved]

35.47

[Reserved]

PPENDIX

ART

35—I

NSTRUCTIONS FOR

ONTINUED

IRWORTHINESS

UTHORITY

: 49 U.S.C. 106(g), 40113, 44701–

44702, 44704.

OURCE

: Docket No. 2095, 29 FR 7458, June

10, 1964, unless otherwise noted.

VerDate Mar<15>2010

10:12 Mar 18, 2014

Jkt 232046

PO 00000

Frm 00908

Fmt 8010

Sfmt 8010

Y:\SGML\232046.XXX

232046

pmangrum on DSK3VPTVN1PROD with CFR