Previous Page Page 638 Next Page  
background image

629 

Federal Aviation Administration, DOT 

§ 26.35 

T

ABLE

1—Continued 

757 Series 

Model—Airbus 

A318, A319, A320, A321 Series 
A300, A310 Series 
A330, A340 Series 

(d) 

Design Changes and Service Instruc-

tions. By the times specified in para-
graph (e) of this section, each person 
subject to this section must meet the 
requirements of paragraphs (d)(1) or 
(d)(2) of this section, as applicable. 

(1) For holders and applicants subject 

to paragraph (a)(1) or (a)(3)(iii) of this 
section, if the assessment required by 
paragraph (c) of this section identifies 
any features of the design change that 
compromise any CDCCL applicable to 
any airplane on which the design 
change is eligible for installation, the 
holder or applicant must submit for ap-
proval by the FAA Oversight Office de-
sign changes and service instructions 
for Flammability Impact Mitigation 
Means (FIMM) that would bring the de-
sign change into compliance with the 
CDCCL. Any fuel tank modified as re-
quired by this paragraph must also be 
evaluated as required by paragraph (b) 
of this section. 

(2) Applicants subject to paragraph 

(a)(2), or (a)(3)(i) of this section must 
comply with the requirements of 14 
CFR 25.981, in effect on December 26, 
2008. 

(3) Applicants subject to paragraph 

(a)(3)(ii) of this section must comply 
with the requirements of 14 CFR 26.33. 

(e) 

Compliance Times for Design 

Changes and Service Instructions. The 
following persons subject to this sec-

tion must comply with the require-
ments of paragraph (d) of this section 
at the specified times. 

(1) Holders of supplemental type cer-

tificates and field approvals: Before De-
cember 26, 2012. 

(2) Applicants for supplemental type 

certificates and for amendments to 
type certificates: Before December 26, 
2012, or before the certificate is issued, 
whichever occurs later. 

(f) 

Compliance Planning. By the appli-

cable date specified in Table 2 of this 
section, each person subject to para-
graph (a)(1) of this section must submit 
for approval by the FAA Oversight Of-
fice compliance plans for the flamma-
bility exposure analysis required by 
paragraph (b) of this section, the im-
pact assessment required by paragraph 
(c) of this section, and the design 
changes and service instructions re-
quired by paragraph (d) of this section. 
Each person’s compliance plans must 
include the following: 

(1) A proposed project schedule for 

submitting the required analysis or im-
pact assessment. 

(2) A proposed means of compliance 

with paragraph (d) of this section. 

(3) For the requirements of paragraph 

(d) of this section, a proposal for sub-
mitting a draft of all design changes, if 
any are required, and Airworthiness 
Limitations (including CDCCLs) for re-
view by the FAA Oversight Office not 
less than 60 days before the compliance 
time specified in paragraph (e) of this 
section. 

(4) For the requirements of paragraph 

(d) of this section, a proposal for how 
the approved service information and 
any necessary modification parts will 
be made available to affected persons. 

T

ABLE

2—C

OMPLIANCE

P

LANNING

D

ATES

 

Flammability exposure anal-

ysis plan 

Impact assessment plan 

Design changes and service 

instructions plan 

STC and Field Approval Hold-

ers.

March 26, 2009 ......................

February 26, 2011 ..................

August 26, 2011. 

(g) Each person subject to this sec-

tion must implement the compliance 

plans, or later revisions, as approved 
under paragraph (f) of this section. 

[Doc. No. FAA–2005–22997, 73 FR 42499, July 
21, 2008, as amended by Amdt. 26–3, 74 FR 
31619, July 2, 2009] 

VerDate Mar<15>2010 

10:12 Mar 18, 2014

Jkt 232046

PO 00000

Frm 00639

Fmt 8010

Sfmt 8010

Y:\SGML\232046.XXX

232046

pmangrum on DSK3VPTVN1PROD with CFR

  Previous Page Page 638 Next Page