AD: McDonnell Douglas | 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-04.01.24

Airborne-Unlimited-04.16.24

Airborne-FlightTraining-04.17.24 Airborne-Unlimited-04.11.24

Airborne-Unlimited-04.12.24

Join Us At 0900ET, Friday, 4/10, for the LIVE Morning Brief.
Watch It LIVE at
www.airborne-live.net

Mon, Mar 21, 2005

AD: McDonnell Douglas

AD NUMBER: 2005-06-05
MANUFACTURER: McDonnell Douglas
SUBJECT: Airworthiness Directive 2005-06-05
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all McDonnell Douglas Model DC-8 airplanes. This AD requires an inspection of the pushrod assemblies for the left and right elevator control tabs to determine if the pushrod assemblies are made of aluminum or steel, replacing any assembly made of aluminum with an assembly made of steel or modifying existing steel assemblies, and other specified actions. This AD also requires an inspection of the crank assemblies for the inboard and outboard geared tabs of the elevator to determine if the crank assemblies are made of aluminum or steel, replacing any assembly made of aluminum with an assembly made of steel, and other specified actions.

This AD is prompted by an accident involving a DC-8 airplane. The probable cause of the accident was a loss of pitch control resulting from the disconnection of the pushrod for the right elevator control tab. The pushrod dropped down and jammed in front of the control tab crank, causing a large deflection of the control tab. We are issuing this AD to minimize the possibility of a control tab offset. A control tab offset could cause elevator deflection, an elevator airplane-nose-up condition, and reduced controllability of the airplane. This AD is also prompted by a report that the elevator on a McDonnell Douglas Model DC-8 airplane did not respond to command inputs from the flightcrew. We are also issuing this AD to minimize the possibility of crank assembly failure when the assembly is exposed to abnormal load conditions. Failure of a crank assembly could result in a jammed elevator and consequent reduced controllability of the airplane.

FMI: www.airweb.faa.gov

Advertisement

More News

ANN's Daily Aero-Linx (04.15.24)

Aero Linx: International Flying Farmers IFF is a not-for-profit organization started in 1944 by farmers who were also private pilots. We have members all across the United States a>[...]

Classic Aero-TV: 'No Other Options' -- The Israeli Air Force's Danny Shapira

From 2017 (YouTube Version): Remembrances Of An Israeli Air Force Test Pilot Early in 2016, ANN contributor Maxine Scheer traveled to Israel, where she had the opportunity to sit d>[...]

Aero-News: Quote of the Day (04.15.24)

"We renegotiated what our debt restructuring is on a lot of our debts, mostly with the family. Those debts are going to be converted into equity..." Source: Excerpts from a short v>[...]

Airborne 04.16.24: RV Update, Affordable Flying Expo, Diamond Lil

Also: B-29 Superfortress Reunion, FAA Wants Controllers, Spirit Airlines Pulls Back, Gogo Galileo Van's Aircraft posted a short video recapping the goings-on around their reorganiz>[...]

ANN's Daily Aero-Term (04.16.24): Chart Supplement US

Chart Supplement US A flight information publication designed for use with appropriate IFR or VFR charts which contains data on all airports, seaplane bases, and heliports open to >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC