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485 

Federal Aviation Administration, DOT 

§ 26.47 

this section must be submitted by June 
30, 2009. 

(3) For alteration data approved on 

or after January 11, 2008, DT data re-
quired by paragraph (c)(2) of this sec-
tion must be submitted before initial 
approval of the alteration data. 

(4) For repair data developed and ap-

proved before January 11, 2008, the DT 
data required by paragraph (d)(2) of 
this section must be submitted by June 
30, 2009. 

(5) For repair data developed and ap-

proved after January 11, 2008, the DT 
data required by paragraph (d)(2) of 
this section must be submitted within 
12 months after initial approval of the 
repair data and before making the DT 
data available to persons required to 
comply with §§ 121.1109 and 129.109 of 
this chapter. 

[Doc. No. FAA–2005–21693, 72 FR 70505, Dec. 
12, 2007, as amended by Amdt. 26–4, 75 FR 
11734, Mar. 12, 2010; Doc. No. FAA–2018–0119, 
Amdt. 26–7, 83 FR 9170, Mar. 5, 2018] 

§ 26.47

Holders of and applicants for a 

supplemental type certificate—Al-
terations and repairs to alterations. 

(a) 

Applicability.  This section applies 

to transport category airplanes subject 
to § 26.43. 

(b) 

Fatigue critical alteration structure. 

For existing structural alteration data 
approved under a supplemental certifi-
cate, the holder of the supplemental 
certificate must— 

(1) Review the alteration data and 

identify all alterations that affect fa-
tigue critical baseline structure identi-
fied under § 26.43(b)(1); 

(2) For each alteration identified 

under paragraph (b)(1) of this section, 
identify any fatigue critical alteration 
structure; 

(3) Develop and submit to the respon-

sible Aircraft Certification Service of-
fice for review and approval a list of 
the structure identified under para-
graph (b)(2) of this section; and 

(4) Upon approval, make the list re-

quired in paragraph (b)(3) of this sec-
tion available to persons required to 
comply with §§ 121.1109 and 129.109 of 
this chapter. 

(c) 

DT Data. For existing and future 

alteration data developed by the holder 
of a supplemental type certificate that 
affect fatigue critical baseline struc-

ture identified under § 26.43(b)(1), unless 
previously accomplished, the holder of 
a supplemental type certificate must— 

(1) Perform a DTE and develop the 

DTI for the alteration and fatigue crit-
ical baseline structure that is affected 
by the alteration; 

(2) Submit the DT data developed in 

accordance with paragraphs (c)(1) of 
this section to the responsible Aircraft 
Certification Service office or its prop-
erly authorized designees for review 
and approval; and 

(3) Upon approval, make the DTI 

available to persons required to comply 
with §§ 121.1109 and 129.109 of this chap-
ter. 

(d) 

DT Data for Repairs Made to Alter-

ations.  For existing and future repair 
data developed by the holder of a sup-
plemental holder of a supplemental 
type certificate, the holder of a supple-
mental type certificate must— 

(1) Review the repair data, and iden-

tify each repair that affects any fa-
tigue critical alteration structure iden-
tified under paragraph (b)(2) of this sec-
tion; 

(2) For each repair identified under 

paragraph (d)(1) of this section, unless 
previously accomplished, perform a 
DTE and develop DTI; 

(3) Submit the DT data developed in 

accordance with paragraph (d)(2) of 
this section to the responsible Aircraft 
Certification Service office or its prop-
erly authorized designees for review 
and approval; and 

(4) Upon approval, make the DTI 

available to persons required to comply 
with §§ 121.1109 and 129.109 of this chap-
ter. 

(e) 

Compliance times. Holders of sup-

plemental type certificates must sub-
mit the following to the responsible 
Aircraft Certification Service office or 
its properly authorized designees for 
review and approval by the specified 
compliance time: 

(1) The list of fatigue critical alter-

ation structure required by paragraph 
(b)(3) of this section must be submitted 
no later than 360 days after January 11, 
2008. 

(2) For alteration data developed and 

approved before January 11, 2008, the 
DT data required by paragraph (c)(2) of 
this section must be submitted by June 
30, 2009. 

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486 

14 CFR Ch. I (1–1–24 Edition) 

§ 26.49 

(3) For alteration data developed 

after January 11, 2008, the DT data re-
quired by paragraph (c)(2) of this sec-
tion must be submitted before approval 
of the alteration data and making it 
available to persons required to comply 
with §§ 121.1109 and 129.109 of this chap-
ter. 

(4) For repair data developed and ap-

proved before January 11, 2008, the DT 
data required by paragraph (d)(2) of 
this section must be submitted by June 
30, 2009. 

(5) For repair data developed and ap-

proved after January 11, 2008, the DT 
data required by paragraph (d)(2) of 
this section, must be submitted within 
12 months after initial approval of the 
repair data and before making the DT 
data available to persons required to 
comply with §§ 121.1109 and 129.109 of 
this chapter. 

[Docket No. FAA–2005–21693, 72 FR 70505, Dec. 
12, 2007, as amended by Doc. No. FAA–2018– 
0119, Amdt. 26–7, 83 FR 9170, Mar. 5, 2018] 

§ 26.49

Compliance plan. 

(a) 

Compliance plan. Except for appli-

cants for type certificates and supple-
mental type certificates whose applica-
tions are submitted after January 11, 
2008, each person identified in §§ 26.43, 
26.45, and 26.47, must submit a compli-
ance plan consisting of the following: 

(1) A project schedule identifying all 

major milestones for meeting the com-
pliance times specified in §§ 26.43(f), 
26.45(e), and 26.47(e), as applicable. 

(2) A proposed means of compliance 

with §§ 26.43, 26.45, and 26.47, as applica-
ble. 

(3) A plan for submitting a draft of 

all compliance items required by this 
subpart for review by the responsible 
Aircraft Certification Service office 
not less than 60 days before the appli-
cable compliance date. 

(b) 

Compliance dates for compliance 

plans.  The following persons must sub-
mit the compliance plan described in 
paragraph (a) of this section to the re-
sponsible Aircraft Certification Service 
office for approval on the following 
schedule: 

(1) For holders of type certificates, 

no later than 90 days after January 11, 
2008. 

(2) For holders of supplemental type 

certificates no later than 180 days after 
January 11, 2008. 

(3) For applicants for changes to type 

certificates whose application are sub-
mitted before January 11, 2008, no later 
than 180 days after January 11, 2008. 

(c) 

Compliance Plan Implementation. 

Each affected person must implement 
the compliance plan as approved in 
compliance with paragraph (a) of this 
section. 

[Docket No. FAA–2005–21693, 72 FR 70505, Dec. 
12, 2007, as amended by Doc. No. FAA–2018– 
0119, Amdt. 26–7, 83 FR 9170, Mar. 5, 2018] 

PART 27—AIRWORTHINESS STAND-

ARDS: NORMAL CATEGORY 
ROTORCRAFT 

Subpart A—General 

Sec. 
27.1

Applicability. 

27.2

Special retroactive requirements. 

Subpart B—Flight 

G

ENERAL

 

27.21

Proof of compliance. 

27.25

Weight limits. 

27.27

Center of gravity limits. 

27.29

Empty weight and corresponding cen-

ter of gravity. 

27.31

Removable ballast. 

27.33

Main rotor speed and pitch limits. 

P

ERFORMANCE

 

27.45

General. 

27.49

Performance at minimum operating 

speed. 

27.51

Takeoff. 

27.65

Climb: all engines operating. 

27.67

Climb: one engine inoperative. 

27.71

Autorotation performance. 

27.75

Landing. 

27.87

Height-velocity envelope. 

F

LIGHT

C

HARACTERISTICS

 

27.141

General. 

27.143

Controllability and maneuverability. 

27.151

Flight controls. 

27.161

Trim control. 

27.171

Stability: general. 

27.173

Static longitudinal stability. 

27.175

Demonstration of static longitudinal 

stability. 

27.177

Static directional stability. 

G

ROUND AND

W

ATER

H

ANDLING

 

C

HARACTERISTICS

 

27.231

General. 

27.235

Taxiing condition. 

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