Section 121.1117

14 CFR Ch. I (1-1-19 Edition)
TABLE 2 - AIRPLANES EXCLUDED FROM Section 26.21 - Continued
Default LOV
[flight cycles (FC)
or flight hours (FH)]

Airplane model
Boeing 720 .......................................................................................................................
Bombardier:
CL-44D4 and CL-44J .....................................................................................................
BD-700 ............................................................................................................................
Bristol Aeroplane Company:
Britannia 305 ....................................................................................................................
British Aerospace Airbus, Ltd.:
BAC 1-11 (all models) .....................................................................................................
British Aerospace (Commercial Aircraft) Ltd.:
Armstrong Whitworth Argosy A.W. 650 Series 101 ........................................................
BAE Systems (Operations) Ltd.:
BAe 146-100A (all models) .............................................................................................
BAe 146-200-07 .............................................................................................................
BAe 146-200-07 Dev ......................................................................................................
BAe 146-200-11 .............................................................................................................
BAe 146-200-07A ...........................................................................................................
BAe 146-200-11 Dev ......................................................................................................
BAe 146-300 (all models) ...............................................................................................
Avro 146-RJ70A (all models) ..........................................................................................
Avro 146-RJ85A and 146-RJ100A (all models) .............................................................
D Section R Nevada, LLC:
Convair Model 22 .............................................................................................................
Convair Model 23M ..........................................................................................................
deHavilland Aircraft Company, Ltd.:
D.H. 106 Comet 4C .........................................................................................................
Gulfstream:
GV ....................................................................................................................................
GV-SP .............................................................................................................................
Ilyushin Aviation Complex:
IL-96T ..............................................................................................................................
Lockheed:
300-50A01 (USAF C 141A) ............................................................................................

30,000 FC
20,000 FC
15,000 FH
10,000 FC
85,000 FC
20,000 FC
50,000
50,000
50,000
50,000
47,000
43,000
40,000
40,000
50,000

FC
FC
FC
FC
FC
FC
FC
FC
FC

1,000 FC/1,000 FH
1,000 FC/1,000 FH
8,000 FH
40,000 FH
40,000 FH
10,000 FC/30,000 FH
20,000 FC

[Doc. No. FAA-2006-24281, 75 FR 69785, Nov. 15, 2010, as amended by Amdt. 121-360, 77 FR 30878,
May 24, 2012; Admt. 121-360A, 77 FR 55105, Sept. 7, 2012]

Section 121.1117 Flammability
means.

reduction

(a) Applicability. Except as provided
in paragraph (o) of this section, this
section applies to transport category,
turbine-powered airplanes with a type
certificate issued after January 1, 1958,
that, as a result of original type certification or later increase in capacity
have:
(1) A maximum type-certificated passenger capacity of 30 or more, or
(2) A maximum payload capacity of
7,500 pounds or more.
(b) New Production Airplanes. Except
in accordance with Section 121.628, no certificate holder may operate an airplane
identified in Table 1 of this section (including all-cargo airplanes) for which
the State of Manufacture issued the
original certificate of airworthiness or
export airworthiness approval after December 27, 2010 unless an Ignition Mitigation Means (IMM) or Flammability

Reduction Means (FRM) meeting the
requirements of Section 26.33 of this chapter is
operational.
TABLE 1
Model - Boeing
747
737
777
767

Series
Series
Series
Series

Model - Airbus
A318, A319, A320, A321 Series
A330, A340 Series

(c) Auxiliary Fuel Tanks. After the applicable date stated in paragraph (e) of
this section, no certificate holder may
operate any airplane subject to Section 26.33
of this chapter that has an Auxiliary
Fuel Tank installed pursuant to a field
approval, unless the following requirements are met:
(1) The certificate holder complies
with 14 CFR 26.35 by the applicable
date stated in that section.
(2) The certificate holder installs
Flammability
Impact
Mitigation

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