343
Federal Aviation Administration, DOT
§ 125.227
number of correlation points to accu-
rately establish the conversion from
the recorded values to engineering
units or discrete state over the full op-
erating range of the parameter. Except
for airplanes having separate altitude
and airspeed sensors that are an inte-
gral part of the flight data recorder
system, a single correlation may be es-
tablished for any group of airplanes—
(1) That are of the same type;
(2) On which the flight recorder sys-
tem and its installation are the same;
and
(3) On which there is no difference in
the type design with respect to the in-
stallation of those sensors associated
with the flight data recorder system.
Documentation sufficient to convert
recorded data into the engineering
units and discrete values specified in
the applicable appendix must be main-
tained by the certificate holder.
(k) Each flight data recorder required
by this section must have an approved
device to assist in locating that re-
corder under water.
(l) The following airplanes that were
manufactured before August 18, 1997
need not comply with this section, but
must continue to comply with applica-
ble paragraphs of § 125.225 of this chap-
ter, as appropriate:
(1) Airplanes that meet the Stage 2
noise levels of part 36 of this chapter
and are subject to § 91.801(c) of this
chapter, until January 1, 2000. On and
after January 1, 2000, any Stage 2 air-
plane otherwise allowed to be operated
under Part 91 of this chapter must
comply with the applicable flight data
recorder requirements of this section
for that airplane.
(2) British Aerospace 1–11, General
Dynamics Convair 580, General Dynam-
ics Convair 600, General Dynamics
Convair 640, deHavilland Aircraft Com-
pany Ltd. DHC–7, Fairchild Industries
FH 227, Fokker F–27 (except Mark 50),
F–28 Mark 1000 and Mark 4000, Gulf-
stream Aerospace G–159, Jetstream 4100
Series, Lockheed Aircraft Corporation
Electra 10–A, Lockheed Aircraft Cor-
poration Electra 10–B, Lockheed Air-
craft Corporation Electra 10–E, Lock-
heed Aircraft Corporation Electra L–
188, Lockheed Martin Model 382 (L–100)
Hercules, Maryland Air Industries, Inc.
F27, Mitsubishi Heavy Industries, Ltd.
YS–11, Short Bros. Limited SD3–30,
Short Bros. Limited SD3–60.
(m) All aircraft subject to the re-
quirements of this section that are
manufactured on or after April 7, 2010,
must have a flight data recorder in-
stalled that also—
(1) Meets the requirements in
§ 25.1459(a)(3), (a)(7), and (a)(8) of this
chapter; and
(2) Retains the 25 hours of recorded
information required in paragraph (f)
of this section using a recorder that
meets the standards of TSO–C124a, or
later revision.
(n) In addition to all other applicable
requirements of this section, all Boeing
737 model airplanes manufactured after
August 18, 2000 must record the param-
eters listed in paragraphs (a)(88)
through (a)(91) of this section within
the ranges, accuracies, resolutions, and
recording intervals specified in Appen-
dix E to this part. Compliance with
this paragraph is required no later
than February 2, 2011.
[Doc. No. 28109, 62 FR 38387, July 17, 1997; 62
FR 48135, Sept. 12, 1997, as amended by Amdt.
125–42, 68 FR 42937, July 18, 2003; 68 FR 50069,
Aug. 20, 2003; Amdt. 125–54, 73 FR 12568, Mar.
7, 2008; Amdt. 125–56, 73 FR 73179, Dec. 2, 2008;
Amdt. 125–54, 74 FR 32801, 32804, July 9, 2009]
§ 125.227
Cockpit voice recorders.
(a) No certificate holder may operate
a large turbine engine powered airplane
or a large pressurized airplane with
four reciprocating engines unless an
approved cockpit voice recorder is in-
stalled in that airplane and is operated
continuously from the start of the use
of the checklist (before starting en-
gines for the purpose of flight) to com-
pletion of the final checklist at the ter-
mination of the flight.
(b) Each certificate holder shall es-
tablish a schedule for completion, be-
fore the prescribed dates, of the cock-
pit voice recorder installations re-
quired by paragraph (a) of this section.
In addition, the certificate holder shall
identify any airplane specified in para-
graph (a) of this section he intends to
discontinue using before the prescribed
dates.
(c) The cockpit voice recorder re-
quired by this section must also meet
the following standards:
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