Previous Page Page 637 Next Page  
background image

628 

14 CFR Ch. I (1–1–14 Edition) 

§ 26.35 

Office not less than 60 days before the 
compliance times specified in those 
paragraphs. 

(4) A proposal for how the approved 

service information and any necessary 
modification parts will be made avail-
able to affected persons. 

(i) Each affected type certificate 

holder must implement the compliance 
plans, or later revisions, as approved 
under paragraph (g) and (h) of this sec-
tion. 

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

§ 26.35

Changes to type certificates af-

fecting fuel tank flammability. 

(a) 

Applicability. This section applies 

to holders and applicants for approvals 
of the following design changes to any 
airplane subject to 14 CFR 26.33(a): 

(1) Any fuel tank designed to be Nor-

mally Emptied if the fuel tank instal-
lation was approved pursuant to a sup-
plemental type certificate or a field ap-
proval before December 26, 2008; 

(2) Any fuel tank designed to be Nor-

mally Emptied if an application for a 
supplemental type certificate or an 
amendment to a type certificate was 
made before December 26, 2008 and if 
the approval was not issued before De-
cember 26, 2008; and 

(3) If an application for a supple-

mental type certificate or an amend-
ment to a type certificate is made on 
or after December 26, 2008, any of the 
following design changes: 

(i) Installation of a fuel tank de-

signed to be Normally Emptied, 

(ii) Changes to existing fuel tank ca-

pacity, or 

(iii) Changes that may increase the 

flammability exposure of an existing 
fuel tank for which FRM or IMM is re-
quired by § 26.33(c). 

(b) 

Flammability Exposure Analysis—(1) 

General. By the times specified in para-
graphs (b)(1)(i) and (b)(1)(ii) of this sec-
tion, each person subject to this sec-
tion must submit for approval a flam-
mability exposure analysis of the aux-
iliary fuel tanks or other affected fuel 
tanks, as defined in the type design, to 
the FAA Oversight Office. This anal-
ysis must be conducted in accordance 
with Appendix N of part 25 of this chap-
ter. 

(i) Holders of supplemental type cer-

tificates and field approvals: Within 12 
months of December 26, 2008, 

(ii) Applicants for supplemental type 

certificates and for amendments to 
type certificates: Within 12 months 
after December 26, 2008, or before the 
certificate is issued, whichever occurs 
later. 

(2) 

Exception. This paragraph does not 

apply to— 

(i) Fuel tanks for which the type cer-

tificate holder, supplemental type cer-
tificate holder, or field approval holder 
has notified the FAA under paragraph 
(f) of this section that it will provide 
design changes and service instructions 
for an IMM meeting the requirements 
of § 25.981(c) in effect December 26, 2008; 
and 

(ii) Fuel tanks substantiated to be 

conventional unheated aluminum wing 
tanks. 

(c) 

Impact Assessment. By the times 

specified in paragraphs (c)(1) and (c)(2) 
of this section, each person subject to 
paragraph (a)(1) of this section holding 
an approval for installation of a Nor-
mally Emptied fuel tank on an airplane 
model listed in Table 1 of this section, 
and each person subject to paragraph 
(a)(3)(iii) of this section, must submit 
for approval to the FAA Oversight Of-
fice an assessment of the fuel tank sys-
tem, as modified by their design 
change. The assessment must identify 
any features of the design change that 
compromise any critical design con-
figuration control limitation (CDCCL) 
applicable to any airplane on which the 
design change is eligible for installa-
tion. 

(1) Holders of supplemental type cer-

tificates and field approvals: Before 
June 26, 2011. 

(2) Applicants for supplemental type 

certificates and for amendments to 
type certificates: Before June 26, 2011 
or before the certificate is issued, 
whichever occurs later. 

T

ABLE

Model—Boeing 

747 Series 
737 Series 
777 Series 
767 Series 

VerDate Mar<15>2010 

10:12 Mar 18, 2014

Jkt 232046

PO 00000

Frm 00638

Fmt 8010

Sfmt 8010

Y:\SGML\232046.XXX

232046

pmangrum on DSK3VPTVN1PROD with CFR

  Previous Page Page 637 Next Page