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349 

Federal Aviation Administration, DOT 

§ 125.223 

the seat in front of the user, or in an-
other approved stowage location so 
that it does not block the aisle way or 
the entryway to the row. If the device 
is to be operated by the user, it must 
be operated only at a seat location that 
does not restrict any passenger’s access 
to, or use of, any required emergency 
or regular exit, or the aisle(s) in the 
passenger compartment. 

[Docket No. 19779, 45 FR 67235, Oct. 9, 1980, as 
amended by Docket FAA–2014–0554, Amdt. 
125–65, 81 FR 33119, May 24, 2016; Docket 
FAA–2018–0119, Amdt. 125–68, 83 FR 9173, Mar. 
5, 2018] 

§ 125.221 Icing conditions: Operating 

limitations. 

(a) No pilot may take off an airplane 

that has frost, ice, or snow adhering to 
any propeller, windshield, stabilizing 
or control surface; to a powerplant in-
stallation; or to an airspeed, altimeter, 
rate of climb, flight attitude instru-
ment system, or wing, except that 
takeoffs may be made with frost under 
the wing in the area of the fuel tanks 
if authorized by the FAA. 

(b) No certificate holder may author-

ize an airplane to take off and no pilot 
may take off an airplane any time con-
ditions are such that frost, ice, or snow 
may reasonably be expected to adhere 
to the airplane unless the pilot has 
completed the testing required under 
§ 125.287(a)(9) and unless one of the fol-
lowing requirements is met: 

(1) A pretakeoff contamination 

check, that has been established by the 
certificate holder and approved by the 
Administrator for the specific airplane 
type, has been completed within 5 min-
utes prior to beginning takeoff. A pre-
takeoff contamination check is a check 
to make sure the wings and control 
surfaces are free of frost, ice, or snow. 

(2) The certificate holder has an ap-

proved alternative procedure and under 
that procedure the airplane is deter-
mined to be free of frost, ice, or snow. 

(3) The certificate holder has an ap-

proved deicing/anti-icing program that 
complies with § 121.629(c) of this chap-
ter and the takeoff complies with that 
program. 

(c) No pilot may fly under IFR into 

known or forecast light or moderate 
icing conditions, or under VFR into 

known light or moderate icing condi-
tions, unless— 

(1) The aircraft has functioning deic-

ing or anti-icing equipment protecting 
each propeller, windshield, wing, stabi-
lizing or control surface, and each air-
speed, altimeter, rate of climb, or 
flight attitude instrument system; 

(2) The airplane has ice protection 

provisions that meet appendix C of this 
part; or 

(3) The airplane meets transport cat-

egory airplane type certification provi-
sions, including the requirements for 
certification for flight in icing condi-
tions. 

(d) Except for an airplane that has 

ice protection provisions that meet ap-
pendix C of this part or those for trans-
port category airplane type certifi-
cation, no pilot may fly an airplane 
into known or forecast severe icing 
conditions. 

(e) If current weather reports and 

briefing information relied upon by the 
pilot in command indicate that the 
forecast icing condition that would 
otherwise prohibit the flight will not 
be encountered during the flight be-
cause of changed weather conditions 
since the forecast, the restrictions in 
paragraphs (b) and (c) of this section 
based on forecast conditions do not 
apply. 

[45 FR 67235, Oct. 9, 1980, as amended by 
Amdt. 125–18, 58 FR 69629, Dec. 30, 1993; Amdt. 
125–58, 74 FR 62696, Dec. 1, 2009] 

§ 125.223 Airborne weather radar 

equipment requirements. 

(a) No person may operate an air-

plane governed by this part in pas-
senger-carrying operations unless ap-
proved airborne weather radar equip-
ment is installed in the airplane. 

(b) No person may begin a flight 

under IFR or night VFR conditions 
when current weather reports indicate 
that thunderstorms, or other poten-
tially hazardous weather conditions 
that can be detected with airborne 
weather radar equipment, may reason-
ably be expected along the route to be 
flown, unless the airborne weather 
radar equipment required by paragraph 
(a) of this section is in satisfactory op-
erating condition. 

(c) If the airborne weather radar 

equipment becomes inoperative en 

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350 

14 CFR Ch. I (1–1–24 Edition) 

§ 125.224 

route, the airplane must be operated 
under the instructions and procedures 
specified for that event in the manual 
required by § 125.71. 

(d) This section does not apply to air-

planes used solely within the State of 
Hawaii, within the State of Alaska, 
within that part of Canada west of lon-
gitude 130 degrees W, between latitude 
70 degrees N, and latitude 53 degrees N, 
or during any training, test, or ferry 
flight. 

(e) Without regard to any other pro-

vision of this part, an alternate elec-
trical power supply is not required for 
airborne weather radar equipment. 

§ 125.224 Collision avoidance system. 

Effective January 1, 2005, any air-

plane you operate under this part 125 
must be equipped and operated accord-
ing to the following table: 

C

OLLISION

A

VOIDANCE

S

YSTEMS

 

If you operate any 

. . . 

Then you must operate that airplane 

with: 

(a) Turbine-powered 

airplane of more 
than 33,000 
pounds maximum 
certificated take-
off weight.

(1) An appropriate class of Mode S 

transponder that meets Technical 
Standard Order (TSO) C–112, or a 
later version, and one of the fol-
lowing approved units: 

(i) TCAS II that meets TSO C–119b 

(version 7.0), or a later version. 

(ii) TCAS II that meets TSO C–119a 

(version 6.04A Enhanced) that was 
installed in that airplane before May 
1, 2003. If that TCAS II version 
6.04A Enhanced no longer can be 
repaired to TSO C–119a standards, 
it must be replaced with a TCAS II 
that meets TSO C–119b (version 
7.0), or a later version. 

(iii) A collision avoidance system equiv-

alent to TSO C–119b (version 7.0), 
or a later version, capable of coordi-
nating with units that meet TSO C– 
119a (version 6.04A Enhanced), or a 
later version. 

(b) Piston-powered 

airplane of more 
than 33,000 
pounds maximum 
certificated take-
off weight.

(1) TCAS I that meets TSO C–118, or 

a later version, or 

(2) A collision avoidance system equiv-

alent to TSO C–118, or a later 
version, or 

(1)(3) A collision avoidance system and 

Mode S transponder that meet para-
graph (a)(1) of this section. 

[Doc. No. FAA–2001–10910, 68 FR 15903, Apr. 1, 
2003] 

§ 125.225 Flight data recorders. 

(a) Except as provided in paragraph 

(d) of this section, after October 11, 
1991, no person may operate a large air-
plane type certificated before October 

1, 1969, for operations above 25,000 feet 
altitude, nor a multiengine, turbine 
powered airplane type certificated be-
fore October 1, 1969, unless it is 
equipped with one or more approved 
flight recorders that utilize a digital 
method of recording and storing data 
and a method of readily retrieving that 
data from the storage medium. The fol-
lowing information must be able to be 
determined within the ranges, accura-
cies, resolution, and recording inter-
vals specified in appendix D of this 
part: 

(1) Time; 
(2) Altitude; 
(3) Airspeed; 
(4) Vertical acceleration; 
(5) Heading; 
(6) Time of each radio transmission 

to or from air traffic control; 

(7) Pitch attitude; 
(8) Roll attitude; 
(9) Longitudinal acceleration; 
(10) Control column or pitch control 

surface position; and 

(11) Thrust of each engine. 
(b) Except as provided in paragraph 

(d) of this section, after October 11, 
1991, no person may operate a large air-
plane type certificated after September 
30, 1969, for operations above 25,000 feet 
altitude, nor a multiengine, turbine 
powered airplane type certificated 
after September 30, 1969, unless it is 
equipped with one or more approved 
flight recorders that utilize a digital 
method of recording and storing data 
and a method of readily retrieving that 
data from the storage medium. The fol-
lowing information must be able to be 
determined within the ranges, accura-
cies, resolutions, and recording inter-
vals specified in appendix D of this 
part: 

(1) Time; 
(2) Altitude; 
(3) Airspeed; 
(4) Vertical acceleration; 
(5) Heading; 
(6) Time of each radio transmission 

either to or from air traffic control; 

(7) Pitch attitude; 
(8) Roll attitude; 
(9) Longitudinal acceleration; 
(10) Pitch trim position; 
(11) Control column or pitch control 

surface position;