365 

Federal Aviation Administration, DOT 

Pt. 125, App. A 

(2) Deactivate or remove an IMM or 

FRM once installed unless it is re-
placed by a means that complies with 
paragraph (d) of this section. 

(g) 

Inspection Program Revisions. 

No 

person may operate an airplane for 
which airworthiness limitations have 
been approved by the responsible Air-
craft Certification Service office in ac-
cordance with §§ 26.33, 26.35, or 26.37 of 
this chapter after the airplane is modi-
fied in accordance with paragraph (d) 
of this section unless the inspection 
program for that airplane is revised to 
include those applicable airworthiness 
limitations. 

(h) After the inspection program is 

revised as required by paragraph (g) of 
this section, before returning an air-
plane to service after any alteration 
for which airworthiness limitations are 
required by §§ 25.981, 26.33, 26.35, or 26.37 
of this chapter, the person must revise 
the inspection program for the airplane 
to include those airworthiness limita-
tions. 

(i) The inspection program changes 

identified in paragraphs (g) and (h) of 
this section must be submitted to the 
operator’s assigned Flight Standards 
office responsible for review and ap-
proval prior to incorporation. 

(j) The requirements of paragraph (d) 

of this section do not apply to air-
planes operated in all-cargo service, 
but those airplanes are subject to para-
graph (f) of this section. 

(k) After the date by which any per-

son is required by this section to mod-
ify 100 percent of the affected fleet, no 
person may operate in passenger serv-
ice any airplane model specified in 
Table 2 of this section unless the air-
plane has been modified to comply 
with § 26.33(c) of this chapter. 

T

ABLE

2 

Model—Boeing Model—Airbus 

747 Series ..................

A318, A319, A320, A321 Series. 

737 Series ..................

A300, A310 Series. 

777 Series ..................

A330, A340 Series. 

767 Series.
757 Series.

(l) No person may operate any air-

plane on which an auxiliary fuel tank 
is installed after December 26, 2017 un-
less the FAA has certified the tank as 

compliant with § 25.981 of this chapter, 
in effect on December 26, 2008. 

(m) 

Exclusions. 

The requirements of 

this section do not apply to the fol-
lowing airplane models: 

(1) Convair CV–240, 340, 440, including 

turbine powered conversions. 

(2) Lockheed L–188 Electra. 
(3) Vickers VC–10. 
(4) Douglas DC–3, including turbine 

powered conversions. 

(5) Bombardier CL–44. 
(6) Mitsubishi YS–11. 
(7) BAC 1–11. 
(8) Concorde. 
(9) deHavilland D.H. 106 Comet 4C. 
(10) VFW—Vereinigte Flugtechnische 

VFW–614. 

(11) Illyushin Aviation IL 96T. 
(12) Bristol Aircraft Britannia 305. 
(13) Handley Page Herald Type 300. 
(14) Avions Marcel Dassault—Breguet 

Aviation Mercure 100C. 

(15) Airbus Caravelle. 
(16) Fokker F–27/Fairchild Hiller FH– 

227. 

(17) Lockheed L–300. 

[Doc. No. FAA–2005–22997, 73 FR 42502, July 
21, 2008, as amended by Amdt. 125–57, 74 FR 
31619, July 2, 2009; Docket FAA–2018–0119, 
Amdt. 125–68, 83 FR 9174, Mar. 5, 2018] 

A

PPENDIX

A 

TO

P

ART

125—A

DDITIONAL

 

E

MERGENCY

E

QUIPMENT

 

(a) 

Means for emergency evacuation. 

Each 

passenger-carrying landplane emergency exit 
(other than over-the-wing) that is more that 
6 feet from the ground with the airplane on 
the ground and the landing gear extended 
must have an approved means to assist the 
occupants in descending to the ground. The 
assisting means for a floor level emergency 
exit must meet the requirements of 
§ 25.809(f)(1) of this chapter in effect on April 
30, 1972, except that, for any airplane for 
which the application for the type certificate 
was filed after that date, it must meet the 
requirements under which the airplane was 
type certificated. An assisting means that 
deploys automatically must be armed during 
taxiing, takeoffs, and landings. However, if 
the Administrator finds that the design of 
the exit makes compliance impractical, the 
Administrator may grant a deviation from 
the requirement of automatic deployment if 
the assisting means automatically erects 
upon deployment and, with respect to re-
quired emergency exits, if an emergency 
evacuation demonstration is conducted in 

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