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Printed page 6. PDF page 6.
aircraft and a helicopter (see Figure 1). In addition, at the time of the accident, all exterior lights on Aircraft A that were visible from the rear were white. The area where Aircraft A was stopped was illuminated with whiteOpen interim report at PDF page 6JTSB Haneda collision: second interim report
Printed page 25. PDF page 32.
estimated to have been 28.0% MAC18 , both of which were estimated to have been within allowable range (the maximum take-off weight of 43,000lb and CG of 20.3 to 40.0% MAC corresponding to the weight at the time of theOpen official document at PDF page 32JTSB Haneda collision: first interim report
Printed page 26. PDF page 33.
Bombardier DHC-8-315Exterior Lighting Locations Inspections of external lights are normally performed at the time of external, scheduled and annual inspections prior to each flight, and inspections of anti-collision light covers are performed at intervals of 5,000 flightOpen official document at PDF page 33JTSB Haneda collision: first interim report