The International Air Transport Association (IATA) released data for the 2017 safety performance of the commercial airline industry showing continued strong improvements in safety.
IATA - IATA Releases 2017 Airline Safety Performance
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NTSB Reports on Dreamliner Battery Fire in Boston

We no longer have to conjecture about the Japan Airlines 787 battery fire in Boston because the National Transportation Safety Board has released an interim factual report with nearly 500 pages of related documentation.
A live webcast forum is scheduled for April in Washington to investigate the design, technology and certification lithium-ion batteries.
Attached is the report which contains the details of what happened, and examination findings to date.

Interim Report on Battery
DETERIORATED PARTS ALLOWED FLUTTER WHICH LED TO FATAL CRASH AT 2011 RENO AIR RACES

August 27, 2012
WASHINGTON – The National Transportation Safety Board determined today that deteriorated locknut inserts found in the highly modified North American P-51D airplane that crashed during the 2011 National Championship Air Races in Reno, Nevada, allowed the trim tab attachment screws to become loose, and even initiated fatigue cracking in one screw. This condition, which resulted in reduced stiffness in the elevator trim system, ultimately led to aerodynamic flutter at racing speed that broke the trim tab linkages, resulting in a loss of controllability and the eventual crash.
On September 16, 2011, as the experimental single-seat P-51D airplane “The Galloping Ghost,” traveling about 445 knots, or 512 mph, in the third lap of the six-lap race, passed pylon 8, it experienced a left-roll upset and high-G pitch up. During the upset sequence, the airplane’s vertical acceleration peaked at 17.3 G, causing incapacitation of the pilot. Seconds later, a section of the left elevator trim tab separated in flight. The airplane descended and impacted the ramp in the spectator box seating area, killing the pilot and 10 spectators and injuring more than 60 others.
“In Reno, the fine line between observing risk and being impacted by the consequences when something goes wrong was crossed,” said NTSB Chairman Deborah A. P. Hersman. “The pilots understood the risks they assumed; the spectators assumed their safety had been assessed and addressed.”
Contributing to the accident were the undocumented and untested major modifications made to the airplane, as well as the pilot’s operation of the airplane in the unique air racing environment without adequate flight testing.
The nearly 70-year-old airplane had undergone numerous undocumented modifications. The modifications, designed to increase speed, included shortening of the wings, installation of a boil-off cooling system for the engine, increasing the elevator counterweights, modification of the pitch trim system, and changing the incidence of the horizontal and vertical stabilizers.
Although the Federal Aviation Administration required that a flight standards district office be notified in writing of any major changes made to The Galloping Ghost before it could be flown, investigators could find no records that such notifications were made except for the installation of the boil-off cooling system. The undocumented major modifications were identified through wreckage examinations, photographic evidence, and interviews with ground crewmembers.
In April, while the investigation was ongoing and after the NTSB’s investigative hearing in January on air race and air show safety, the NTSB issued 10 safety recommendations to the Reno Air Racing Association, the National Air racing Group Unlimited Division, and the FAA. These recommendations addressed:
- requiring engineering evaluations for aircraft with major modifications;
- raising the level of safety for spectators and personnel near the race course;
- improving FAA guidance for air race and course design;
- providing race pilots with high-G training and evaluating the feasibility of G-suit requirements for race pilots; and
- tracking the resolution of race aircraft discrepancies identified during prerace technical inspections.
Although no additional safety recommendations were issued today, the Board reclassified nine existing recommendations as described below:
- Eligibility Requirements for Aircraft with Major Modifications – recommendations A 12 9 and A-12-13 classified “Open—Acceptable Response”
- Prerace Technical Inspection Discrepancy Tracking – recommendation A 12 10, classified “Closed—Acceptable Action”
- Spectator Safety – recommendations A 12 14 and 15, classified “Closed—Acceptable Action”
- High G Training, G-Suit Feasibility for Pilots – recommendations A 12 11, -12, -16, and -17, classified “Closed—Acceptable Action”
A tenth safety recommendation, issued to the FAA, which addressed air race and course design guidance was reclassified as “Open—Acceptable Response” on July 25, 2012.
“It’s good news for the air races that so many of our recommendations have been addressed,” said Chairman Hersman. “We will continue to push for the full implementation of all of our safety recommendations.”
- Public Meeting
- NTSB opens docket on Reno Air Races crash
http://www.ntsb.gov/news/2012/120821b.html - NTSB to issue safety recommendations on air races and provide investigative update on 2011 crash at the Reno Air Races http://www.ntsb.gov/news/2012/120405.html
- NTSB January 10, 2012, hearing on Air Race and Air Show Safety http://www.ntsb.gov/news/events/2012/air_show/index.html
- NTSB Provides Investigative Update and Issues Recommendations to Increase Safety at Air Races
http://www.ntsb.gov/news/2012/120410.html
Release: NTSB Urges Changes
The National Transportation Safety Board today issued two urgent safety recommendations to the Federal Aviation Administration (FAA) regarding two recent occurrences in which the fan midshaft on General Electric GEnx-1B engines fractured or exhibited crack indications; and a GEnx -2B incident that appears similar in nature. The recommendations are: (1) Issue an airworthiness directive to require, before further flight, the immediate ultrasonic inspection of the fan midshaft in all GEnx-1B and -2B engines that have not undergone inspection, and (2) Require repetitive inspections of the fan midshaft at a sufficiently short interval that would permit multiple inspections and detection of a crack before it could reach critical length and the fan midshaft fractures.
On July 28, 2012, the NTSB initiated an investigation of an engine failure that occurred on a Boeing 787 during a pre-delivery taxi test in Charleston, South Carolina. This investigation is ongoing.
“The parties to our investigation — the FAA, GE and Boeing — have taken many important steps and additional efforts are in progress to ensure that the fleet is inspected properly,” said NTSB Chairman Deborah A.P. Hersman. “We are issuing this recommendation today because of the potential for multiple engine failures on a single aircraft and the urgent need for the FAA to act immediately.”
In addition, on August 31, 2012, a GEnx-1B engine installed on a Boeing 787 that had not yet flown was found to have an indication of a similar crack on the fan midshaft. The fan midshaft was removed from the engine for further inspection and examination. As a result of the investigative work to date, the NTSB has determined that the fan midshafts on the GEnx engines fractured or cracked at the forward end of the shaft where the retaining nut is installed.
GE developed a field ultrasonic inspection method to inspect the fan midshaft in the area where the fracture and crack occurred that can be accomplished with the engine still installed on the airplane. To date, all in-service and spare GEnx-1B engines have been inspected. In addition, all GEnx-2B engines on passenger airplanes have been inspected. However, the NTSB is aware of approximately 43 GEnx-2B engines on 747-8F cargo airplanes that have not yet been inspected and is concerned that they are potentially susceptible to a fan midshaft failure.
More recently, a Boeing 747-8F cargo flight, operated by Air Bridge Cargo, equipped with General Electric GEnx-2B turbofan engines, experienced a loss of power in one of the engines during the takeoff roll in Shanghai, China. The airplane had accelerated through 50 knots when the engine’s low pressure rotor speed dropped. The pilot rejected the takeoff and returned to the ramp. Photographs of the low pressure turbine show damage similar to the GEnx-1B engine from the Charleston incident. The NTSB will continue to coordinate with our investigative counterparts in China.
Read the Recommendation Letter:
NTSB BRIEFING TODAY AT 4:00 PM (ADT) ON AIRCRAFT ACCIDENT IN ALASKA
The National Transportation Safety Board will hold a press
briefing on its investigation into last night’s airplane
crash near Dillingham, Alaska.
The briefing will take place today at 4:00 p.m. Alaska
Daylight Time (ADT) at the Signature Flight Support
Building, 2nd floor conference room, 6231 South Airpark
Place, Anchorage, Alaska.
NTSB Chairman Deborah A.P. Hersman will conduct the
briefing.
FAA Pilot Training
The Federal Aviation Administration’s new pilot training rule has been a long time coming, like the recommendation for simulator training for pilots in using TCAS that dates back to 1993, remedial training from 2005 for pilots with bad track records and training in aerodynamic stall recovery from the Colgan accident, and pilot monitoring. Just read FAA Administrator Michael Huerta’s discussion of the new Pilot training rule.
I look forward to safer skies from the implementation of this additional training. Hopefully operators in foreign countries will follow the FAA’s suit and ramp up their pilot training. It will be interesting to hear what pilots think of the new pilot training rule.
Mozambique Plane Crash Final Report

On Jan 9th 2014 Namibia’s Accident Investigation Commission released the preliminary report of the LAM E190 crash over Botswana/Namibia on Nov 29th 2013. The conclusion at that time was that the captain intentionally crashed the aircraft. On November 29, 2013, there were 28 passengers and 6 crew aboard the Embraer ERJ-190 flown by LAM Linhas Aereas de Mocambique, and it was enroute at FL380 over northern Botswana when the flight descended and radio contact was lost. The burned out wreckage was located by villagers in Bwabwata National Park (Sambesi Region) on Nov 30. A news article on April 15 2016 indicated that the final report was released, although we have not verified it.
The captain in charge of the aircraft, Herminio dos Santos Fernandes, was alone in the cockpit at the time of the crash. The copilot had left for the lavatory.
The unverified article says that the final report was compiled by Theo Shilongo, deputy director of the directorate of aircraft accident investigations, who was the investigator in charge, and Hafeni Mweshixwa as the co-investigator. It was signed off by works and transport minister Alpheus Naruseb. When it is available to the public, it should be available at the Directorate of Aircraft Accident Investigations Namibia (DAAI).
An interim report of the accident is below. The interim report indicates “The DAAI will provide updates on the investigation and safety recommendations as they become available until completion of the final report” in accordance with the provisions of ICAO Annex 13.
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