Federal Aviation Administration October 24, 2016 – Federal Register Recent Federal Regulation Documents
Results 1 - 4 of 4
Eighth RTCA SC-233 Addressing Human Factors/Pilot Interface Issues for Avionics Plenary
The FAA is issuing this notice to advise the public of a meeting of Eighth Plenary of RTCA SC-233 Addressing Human Factors/Pilot Interface Issues for Avionics.
Ninth RTCA SC-229 406 MHz ELT Plenary Joint With EUROCAE WG-98 10th Plenary
The FAA is issuing this notice to advise the public of a meeting of Ninth RTCA SC-229 406 MHz ELT Plenary Joint with EUROCAE WG-98 10th Plenary.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to supersede Airworthiness Directive (AD) 2014-23- 06, for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. AD 2014-23-06 currently requires modifying the main landing gear (MLG) by installing a new bracket on the left and right lower aft-wing planks. Since we issued AD 2014-23-06, we have determined that it is necessary to require a different modification of the MLG. This proposed AD would require modification of the MLG with an improved design. We are proposing this AD to prevent incorrect installation of the brake hydraulic lines, which could cause the brakes and the anti-skid system to operate incorrectly, and result in catastrophic failure of the airplane during a high-speed rejected takeoff.
Airworthiness Directives; Honeywell International Inc. Turboprop Engines
We are superseding airworthiness directive (AD) 2015-12-04 for all Honeywell International Inc. (Honeywell) TPE331-1, -2, -2UA, -3U, - 3UW, -5, -5A, -5AB, -5B, -6, -6A, -10, -10AV, -10GP, -10GT, -10P, -10R, -10T, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, -11U, -12JR, -12UA, - 12UAR, and -12UHR turboprop engines with certain Woodward fuel control unit (FCU) assemblies, installed. AD 2015-12-04 required initial and repetitive dimensional inspections of the affected fuel control drives and insertion of certain airplane operating procedures into the applicable flight manuals. This AD corrects the compliance requirements and relaxes the inspection interval. This AD was prompted by a request to change compliance time from 50 hours to 100 hours for affected fuel controls. We are issuing this AD to prevent failure of the fuel control drive, damage to the engine, and damage to the airplane.
This site is protected by reCAPTCHA and the Google
Privacy Policy and
Terms of Service apply.
