Federal Aviation Administration, DOT

Section 91.611

kpayne on VMOFRWIN702 with $$_JOB

by April 7, 2012, have a cockpit voice
recorder that also - 
(1) Meets the requirements of
Section 23.1457(d)(6) or Section 25.1457(d)(6) of this
chapter, as applicable; and
(2) If transport category, meets the
requirements of Section 25.1457(a)(3), (a)(4),
and (a)(5) of this chapter.
(i) All airplanes or rotorcraft required by this section to have a cockpit
voice recorder and flight data recorder,
that are manufactured on or after
April 7, 2010, must have a cockpit voice
recorder installed that also - 
(1) Is installed in accordance with the
requirements of Section 23.1457 (except for
paragraphs (a)(6) and (d)(5)); Section 25.1457
(except for paragraphs (a)(6) and (d)(5));
Section 27.1457 (except for paragraphs (a)(6)
and (d)(5)); or Section 29.1457 (except for paragraphs (a)(6) and (d)(5)) of this chapter,
as applicable; and
(2) Retains at least the last 2 hours of
recorded information using a recorder
that meets the standards of TSO-C123a,
or later revision.
(3) For all airplanes or rotorcraft
manufactured on or after April 6, 2012,
also meets the requirements of
Section 23.1457(a)(6) and (d)(5); Section 25.1457(a)(6)
and (d)(5); Section 27.1457(a)(6) and (d)(5); or
Section 29.1457(a)(6) and (d)(5) of this chapter,
as applicable.
(j) All airplanes or rotorcraft required by this section to have a cockpit
voice recorder and a flight data recorder, that install datalink communication equipment on or after April 6,
2012, must record all datalink messages
as required by the certification rule applicable to the aircraft.
(k) An aircraft operated under this
part under deviation authority from
part 125 of this chapter must comply
with all of the applicable flight data
recorder requirements of part 125 applicable to the aircraft, notwithstanding
such deviation authority.
[Doc. No. 18334, 54 FR 34318, Aug. 18, 1989, as
amended by Amdt. 91-226, 56 FR 51621, Oct.
11, 1991; Amdt. 91-228, 57 FR 19353, May 5,
1992; Amdt. 91-300, 73 FR 12564, Mar. 7, 2008;
Amdt. 91-304, 73 FR 73178, Dec. 2, 2008; Amdt.
91-300, 74 FR 32800, July 9, 2009; Amdt. 91-313,
75 FR 17045, Apr. 5, 2010]

Section 91.611 Authorization for ferry flight
with one engine inoperative.
(a) General. The holder of an air carrier operating certificate or an operating certificate issued under part 125
may conduct a ferry flight of a four-engine airplane or a turbine-engine-powered airplane equipped with three engines, with one engine inoperative, to a
base for the purpose of repairing that
engine subject to the following:
(1) The airplane model has been test
flown and found satisfactory for safe
flight in accordance with paragraph (b)
or (c) of this section, as appropriate.
However, each operator who before November 19, 1966, has shown that a model
of airplane with an engine inoperative
is satisfactory for safe flight by a test
flight conducted in accordance with
performance data contained in the applicable Airplane Flight Manual under
paragraph (a)(2) of this section need
not repeat the test flight for that
model.
(2) The approved Airplane Flight
Manual contains the following performance data and the flight is conducted in accordance with that data:
(i) Maximum weight.
(ii) Center of gravity limits.
(iii) Configuration of the inoperative
propeller (if applicable).
(iv) Runway length for takeoff (including temperature accountability).
(v) Altitude range.
(vi) Certificate limitations.
(vii) Ranges of operational limits.
(viii) Performance information.
(ix) Operating procedures.
(3) The operator has FAA approved
procedures for the safe operation of the
airplane, including specific requirements for - 
(i) Limiting the operating weight on
any ferry flight to the minimum necessary for the flight plus the necessary
reserve fuel load;
(ii) A limitation that takeoffs must
be made from dry runways unless,
based on a showing of actual operating
takeoff techniques on wet runways
with one engine inoperative, takeoffs
with full controllability from wet runways have been approved for the specific model aircraft and included in the
Airplane Flight Manual:

781

VerDate Sep<11>2014

16:30 Jun 25, 2019

Jkt 247047

PO 00000

Frm 00791

Fmt 8010

Sfmt 8010

Q:\14\14V2.TXT

PC31