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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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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