AD: The Boeing Company Airplanes | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.10.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-Unlimited-11.06.25

AirborneUnlimited-11.07.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Mon, Aug 15, 2022

AD: The Boeing Company Airplanes

AD 2022-15-07 Requires Revising The Existing Airplane Flight Manual (AFM)

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 747-400 series airplanes.

This AD was prompted by a report that after a certain circuit breaker tripped, power to the two pitot-static (P/S) probe heaters on the right-hand side was lost, and the flightcrew discovered conflicting procedures in the flightcrew operations manual/quick reference handbook (FCOM/QRH). This AD requires revising the existing airplane flight manual (AFM) to incorporate procedures to be applied during P/S probe heater failure conditions. The FAA is issuing this AD to address the unsafe condition on these products. This AD is effective September 15, 2022. 

Supplementary Information: The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain The Boeing Company Model 747-400 series airplanes. The NPRM published in the Federal Register on December 28, 2021 (86 FR 73694). The NPRM was prompted by a report that after a certain circuit breaker tripped, power to the two P/S probe heaters on the righthand side was lost, and the flightcrew discovered conflicting procedures in the FCOM/QRH. In the NPRM, the FAA proposed to require revising the existing AFM to incorporate procedures to be applied during P/S probe heater failure conditions. The FAA is issuing this AD to address the conflicting procedures, which could result in the transmission of potentially inaccurate pitot static pressure data to the air data computer (ADC), resulting in erroneous or misleading air data being displayed, which, in combination with a stall, overspeed, overrun, or short/hard landing condition, could result in reduced ability of the flightcrew to maintain continued safe flight and landing of the airplane.

FMI: www.regulations.gov

Advertisement

More News

NTSB Final Report: Piper PA-44-180

While On The Base Leg Of The Airport Traffic Pattern The Right Main Landing Gear Did Not Fully Extend Analysis: Both pilots reported that after performing airwork they returned to >[...]

Classic Aero-TV: The Bizarre Universe of Klyde Morris Cartoons

From 2023 (YouTube Edition): Putting the ANT in Antihero A Beech Starship speeds along at altitude. “Deflectors on!” a voice from within the aircraft cries. “Look>[...]

ANN's Daily Aero-Term (11.09.25): Minimum Friction Level

Minimum Friction Level The friction level specified in AC 150/5320-12, Measurement, Construction, and Maintenance of Skid Resistant Airport Pavement Surfaces, that represents the m>[...]

Aero-News: Quote of the Day (11.09.25)

“Beginning this aircraft subsystem testing is the culmination of more than a decade of focused engineering and certification refinements. This is the moment where our intende>[...]

Classic Aero-TV: Falling for Para-Phernalia’s Softie Emergency Parachutes

From 2023 (YouTube Edition): The Best Option for A Pilots’ Worst Days Since its 1979 founding, Para-Phernalia, Inc. has designed and manufactured the Softie line of pilot eme>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC