Federal Aviation Administration December 8, 2016 – Federal Register Recent Federal Regulation Documents

Type Certificates 3A2 and A-772
Document Number: 2016-29432
Type: Notice
Date: 2016-12-08
Agency: Federal Aviation Administration, Department of Transportation
This notice requests that the current holder(s) (or their heirs) of TCs 3A2 and A-772 come forward and identify themselves; otherwise, the FAA will declare the TCs as abandoned. This notice is issued in accordance with Sec. 302 of the FAA Modernization and Reform Act of 2012,\1\ partially codified as Title 49 of the United States Code (49 U.S.C.) Sec. 44704(a)(5).
Special Conditions: Bell Helicopter Textron, Inc. (BHTI), Model 525 Helicopters; Interaction of Systems and Structures.
Document Number: 2016-29431
Type: Rule
Date: 2016-12-08
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the BHTI Model 525 helicopter. This helicopter will have a novel or unusual design feature associated with fly-by-wire flight control system (FBW FCS) functions that affect the structural integrity of the rotorcraft. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; M7 Aerospace LLC
Document Number: 2016-29242
Type: Rule
Date: 2016-12-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. This AD was prompted by corrosion and stress corrosion cracking of the pitch trim actuator upper attach fittings of the horizontal stabilizer front spar. This AD requires repetitive inspections with replacement of fittings as necessary. We are issuing this AD to correct the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2016-28602
Type: Rule
Date: 2016-12-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes, Model DHC- 8-200 series airplanes, and Model DHC-8-300 series airplanes. This AD was prompted by several occurrences of loss of airspeed data on both pilot and co-pilot air speed indicators due to the accumulation of ice on the pitot probes caused by inoperative pitot probe heaters. This AD requires replacing the existing circuit breakers in the pitot heater system. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2016-28210
Type: Rule
Date: 2016-12-08
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of cracked and corroded barrel nuts found at the mid-spar location of the horizontal-stabilizer-to-vertical-stabilizer attachment joint. This AD requires repetitive detailed inspections of each barrel nut and cradle, a check of the bolt torque of the preload indicating (PLI) washers, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products.