JANUARY 4, 2010
DATES Effective date: The effective date of these amendments is January 4, 2010. Applicability date: These amendments are applicable beginning January 1, 2010.
49 CFR Part 175 — Hazardous Materials: Carriage by Aircraft
In Section 175.10, paragraphs (a)(15)(iv)(B) and (a)(18)(ii) are revised to read as follows:
§175.10 Exceptions for passengers, crewmembers, and air operators.
(a)
* * *
(15)
* * *
(iv)
* * *
(B)
Is removed and placed in a strong, rigid packaging marked “NONSPILLABLE BATTERY” (unless fully enclosed in a rigid housing that is properly marked); or * * * * *
(18)
* * *
(ii)
The maximum water capacity of a fuel cell cartridge for hydrogen in a metal hydride may not exceed 120 mL (4 .uid ounces). The maximum quantity of fuel in all other fuel cell car-tridge types may not exceed:
(A)
200 mL (6.76 ounces) for liquids;
(B)
120 mL (4 .uid ounces) for lique.ed gases in non-metallic fuel cell cartridges, or 200 mL (6.76 ounces) for lique.ed gases in metal fuel cell cartridges; or
(C)
200 g (7 ounces) for solids. * * * * * [Docket Nos. PHMSA–2007–0065 (HM-224D) and PHMSA–2008–0005
(HM-215J), 75 FR 73, Jan. 4, 2010]
DECEMBER 1, 2009
Effective date: February 1, 2010
Part 91—General Operating and Flight Rules
Amend Section 91.527 by revising paragraphs (a) and (b) to read as follows:
§91.527 Operating in icing conditions.
(a)
No pilot may take off an airplane that has frost, ice, or snow adhering to any propeller, windshield, stabilizing or control sur-face; to a powerplant installation; or to an airspeed, altimeter, rate of climb, or .ight attitude instrument system or wing, except that takeoffs may be made with frost under the wing in the area of the fuel tanks if authorized by the FAA.
(b)
No pilot may .y under IFR into known or forecast light or moderate icing conditions, or under VFR into known light or mod-erate icing conditions, unless—
(1)
The aircraft has functioning deicing or anti-icing equipment protecting each rotor blade, propeller, windshield, wing, stabilizing or control surface, and each airspeed, altimeter, rate of climb, or .ight attitude instrument system;
(2)
The airplane has ice protection provisions that meet section 34 of Special Federal Aviation Regulation No. 23; or
(3)
The airplane meets transport category airplane type certi.-cation provisions, including the requirements for certi.cation for .ight in icing conditions. * * * * * [As amended by Amdt. 91–310, 74 FR 62696, Dec. 1, 2009]
Part 135 — Operating Requirements: Commuter and On Demand Operations and Rules Governing Persons On Board Such Aircraft
Amend Section 135.227 by revising paragraphs (a) and (c) to read as follows:
§135.227 Icing conditions: Operating limitations.
(a)
No pilot may take off an aircraft that has frost, ice, or snow adhering to any rotor blade, propeller, windshield, stabilizing or control surface; to a powerplant installation; or to an airspeed, altimeter, rate of climb, .ight attitude instrument system, or wing, except that takeoffs may be made with frost under the wing in the area of the fuel tanks if authorized by the FAA. * * * * *
(c)
No pilot may .y under IFR into known or forecast light or moderate icing conditions or under VFR into known light or mod-erate icing conditions, unless—
(1)
The aircraft has functioning deicing or anti-icing equipment protecting each rotor blade, propeller, windshield, wing, stabilizing or control surface, and each airspeed, altimeter, rate of climb, or .ight attitude instrument system;
(2)
The airplane has ice protection provisions that meet section 34 of appendix A of this part; or
(3)
The airplane meets transport category airplane type certi.-cation provisions, including the requirements for certi.cation for .ight in icing conditions. * * * * * [As amended by Amdt. 135–119, 74 FR 62696, Dec. 1, 2009]
OCTOBER 16, 2009
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本文鏈接地址：ASA’s FAR/AIM and Flight Crew 2010 Update(47)
