Federal Aviation Administration, DOT

Pt. 27

(3) For alteration data developed
after January 11, 2008, the DT data required by paragraph (c)(2) of this section must be submitted before approval
of the alteration data and making it
available to persons required to comply
with SectionSection 121.1109 and 129.109 of this chapter.
(4) For repair data developed and approved 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 approved 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 SectionSection 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]

spaschal on DSK3GDR082PROD with CFR

Section 26.49

(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 submitted 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 STANDARDS:
NORMAL
CATEGORY
ROTORCRAFT
Subpart A - General
Sec.
27.1 Applicability.
27.2 Special retroactive requirements.

Subpart B - Flight

Compliance plan.

GENERAL

(a) Compliance plan. Except for applicants for type certificates and supplemental type certificates whose applications are submitted after January 11,
2008, each person identified in SectionSection 26.43,
26.45, and 26.47, must submit a compliance plan consisting of the following:
(1) A project schedule identifying all
major milestones for meeting the compliance times specified in SectionSection 26.43(f),
26.45(e), and 26.47(e), as applicable.
(2) A proposed means of compliance
with SectionSection 26.43, 26.45, and 26.47, as applicable.
(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 applicable compliance date.
(b) Compliance dates for compliance
plans. The following persons must submit the compliance plan described in
paragraph (a) of this section to the responsible 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.

27.21 Proof of compliance.
27.25 Weight limits.
27.27 Center of gravity limits.
27.29 Empty weight and corresponding center of gravity.
27.31 Removable ballast.
27.33 Main rotor speed and pitch limits.
PERFORMANCE
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-speed envelope.
FLIGHT CHARACTERISTICS
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.
GROUND AND WATER HANDLING
CHARACTERISTICS
27.231
27.235

General.
Taxiing condition.

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