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347 

Federal Aviation Administration, DOT 

§ 125.219 

(c) Each emergency cockpit checklist 

required by paragraph (a)(2) of this sec-
tion must contain the following proce-
dures, as appropriate: 

(1) Emergency operation of fuel, hy-

draulic, electrical, and mechanical sys-
tems. 

(2) Emergency operation of instru-

ments and controls. 

(3) Engine inoperative procedures. 
(4) Any other emergency procedures 

necessary for safety. 

§ 125.217 Passenger information. 

(a) Except as provided in paragraph 

(b) of this section, no person may oper-
ate an airplane carrying passengers un-
less it is equipped with signs that meet 
the requirements of § 25.791 of this 
chapter and that are visible to pas-
sengers and flight attendants to notify 
them when smoking is prohibited and 
when safety belts must be fastened. 
The signs must be so constructed that 
the crew can turn them on and off. 
They must be turned on during air-
plane movement on the surface, for 
each takeoff, for each landing, and 
when otherwise considered to be nec-
essary by the pilot in command. 

(b) No passenger or crewmember may 

smoke while any ‘‘No Smoking’’ sign is 
lighted nor may any passenger or crew-
member smoke in any lavatory. 

(c) Each passenger required by 

§ 125.211(b) to occupy a seat or berth 
shall fasten his or her safety belt about 
him or her and keep it fastened while 
any ‘‘Fasten Seat Belt’’ sign is lighted. 

(d) Each passenger shall comply with 

instructions given him or her by crew-
members regarding compliance with 
paragraphs (b) and (c) of this section. 

[Doc. No. 26142, 57 FR 42675, Sept. 15, 1992] 

§ 125.219 Oxygen and portable oxygen 

concentrators for medical use by 

passengers. 

(a) Except as provided in paragraphs 

(d) and (f) of this section, no certificate 
holder may allow the carriage or oper-
ation of equipment for the storage, 
generation or dispensing of medical ox-
ygen unless the conditions in para-
graphs (a) through (c) of this section 
are satisfied. Beginning August 22, 2016, 
a certificate holder may allow a pas-
senger to carry and operate a portable 
oxygen concentrator when the condi-

tions in paragraphs (b) and (f) of this 
section are satisfied. 

(1) The equipment must be— 
(i) Of an approved type or in con-

formity with the manufacturing, pack-
aging, marking, labeling, and mainte-
nance requirements of title 49 CFR 
parts 171, 172, and 173, except 
§ 173.24(a)(1); 

(ii) When owned by the certificate 

holder, maintained under the certifi-
cate holder’s approved maintenance 
program; 

(iii) Free of flammable contaminants 

on all exterior surfaces; 

(iv) Constructed so that all valves, 

fittings, and gauges are protected from 
damage during that carriage or oper-
ation; and 

(v) Appropriately secured. 
(2) When the oxygen is stored in the 

form of a liquid, the equipment must 
have been under the certificate holder’s 
approved maintenance program since 
its purchase new or since the storage 
container was last purged. 

(3) When the oxygen is stored in the 

form of a compressed gas as defined in 
title 49 CFR 173.115(b)— 

(i) When owned by the certificate 

holder, it must be maintained under its 
approved maintenance program; and 

(ii) The pressure in any oxygen cyl-

inder must not exceed the rated cyl-
inder pressure. 

(4) The pilot in command must be ad-

vised when the equipment is on board 
and when it is intended to be used. 

(5) The equipment must be stowed, 

and each person using the equipment 
must be seated so as not to restrict ac-
cess to or use of any required emer-
gency or regular exit or of the aisle in 
the passenger compartment. 

(b) No person may smoke or create 

an open flame and no certificate holder 
may allow any person to smoke or cre-
ate an open flame within 10 feet of oxy-
gen storage and dispensing equipment 
carried under paragraph (a) of this sec-
tion or a portable oxygen concentrator 
carried and operated under paragraph 
(f) of this section. 

(c) No certificate holder may allow 

any person other than a person trained 
in the use of medical oxygen equip-
ment to connect or disconnect oxygen 

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348 

14 CFR Ch. I (1–1–24 Edition) 

§ 125.219 

bottles or any other ancillary compo-
nent while any passenger is aboard the 
airplane. 

(d) Paragraph (a)(1)(i) of this section 

does not apply when that equipment is 
furnished by a professional or medical 
emergency service for use on board an 
airplane in a medical emergency when 
no other practical means of transpor-
tation (including any other properly 
equipped certificate holder) is reason-
ably available and the person carried 
under the medical emergency is accom-
panied by a person trained in the use of 
medical oxygen. 

(e) Each certificate holder who, under 

the authority of paragraph (d) of this 
section, deviates from paragraph 
(a)(1)(i) of this section under a medical 
emergency shall, within 10 days, ex-
cluding Saturdays, Sundays, and Fed-
eral holidays, after the deviation, send 
to the responsible Flight Standards of-
fice charged with the overall inspec-
tion of the certificate holder a com-
plete report of the operation involved, 
including a description of the deviation 
and the reasons for it. 

(f) 

Portable oxygen concentrators

—(1) 

Acceptance criteria. 

A passenger may 

carry or operate a portable oxygen con-
centrator for personal use on board an 
aircraft and a certificate holder may 
allow a passenger to carry or operate a 
portable oxygen concentrator on board 
an aircraft operated under this part 
during all phases of flight if the port-
able oxygen concentrator satisfies all 
of the requirements in this paragraph 
(f): 

(i) Is legally marketed in the United 

States in accordance with Food and 
Drug Administration requirements in 
title 21 of the CFR; 

(ii) Does not radiate radio frequency 

emissions that interfere with aircraft 
systems; 

(iii) Generates a maximum oxygen 

pressure of less than 200 kPa gauge 
(29.0 psig/43.8 psia) at 20 

°

C (68 

°

F); 

(iv) Does not contain any hazardous 

materials subject to the Hazardous Ma-
terials Regulations (49 CFR parts 171 
through 180) except as provided in 49 
CFR 175.10 for batteries used to power 
portable electronic devices and that do 
not require aircraft operator approval; 
and 

(v) Bears a label on the exterior of 

the device applied in a manner that en-
sures the label will remain affixed for 
the life of the device and containing 
the following certification statement 
in red lettering: ‘‘The manufacturer of 
this POC has determined this device 
conforms to all applicable FAA accept-
ance criteria for POC carriage and use 
on board aircraft.’’ The label require-
ments in this paragraph (f)(1)(v) do not 
apply to the following portable oxygen 
concentrators approved by the FAA for 
use on board aircraft prior to May 24, 
2016: 

(A) AirSep Focus; 
(B) AirSep FreeStyle; 
(C) AirSep FreeStyle 5; 
(D) AirSep LifeStyle; 
(E) Delphi RS–00400; 
(F) DeVilbiss Healthcare iGo; 
(G) Inogen One; 
(H) Inogen One G2; 
(I) Inogen One G3; 
(J) Inova Labs LifeChoice; 
(K) Inova Labs LifeChoice Activox; 
(L) International Biophysics 

LifeChoice; 

(M) Invacare Solo2; 
(N) Invacare XPO2; 
(O) Oxlife Independence Oxygen Con-

centrator; 

(P) Oxus RS–00400; 
(Q) Precision Medical EasyPulse; 
(R) Respironics EverGo; 
(S) Respironics SimplyGo; 
(T) SeQual Eclipse; 
(U) SeQual eQuinox Oxygen System 

(model 4000); 

(V) SeQual Oxywell Oxygen System 

(model 4000); 

(W) SeQual SAROS; and 
(X) VBox Trooper Oxygen Concen-

trator. 

(2) 

Operating requirements. 

Portable 

oxygen concentrators that satisfy the 
acceptance criteria identified in para-
graph (f)(1) of this section may be car-
ried or used by a passenger on an air-
craft provided the aircraft operator en-
sures that all of the conditions in this 
paragraph (f)(2) are satisfied: 

(i) 

Exit seats. 

No person operating a 

portable oxygen concentrator is per-
mitted to occupy an exit seat. 

(ii) 

Stowage of device. 

During move-

ment on the surface, takeoff and land-
ing, the device must be stowed under 

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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