Investigation Summary
Flight 779 was transporting 25,999 pounds of military cargo from Travis Air Force Base to Tachikawa, Japan, with a scheduled refueling stop at Shemya. During the approach to Runway 10, the aircraft was operating under GCA guidance due to a 200-foot ceiling and restricted visibility in fog. Radar contact was established 18 miles out at 5,500 feet. As the aircraft neared the threshold, the GCA controller observed it slipping below the ideal glidepath. At two miles out, the aircraft was 10 to 25 feet low; at one mile, it was 30 to 40 feet low. Although the controller advised the crew to 'ease the aircraft up,' the crew did not correct the descent. The controller later stated he assumed the pilots had transitioned to a visual approach when the aircraft began to descend more rapidly. However, the lack of functional approach and threshold lighting likely deprived the crew of the visual cues necessary to judge their height above the terrain, leading to the impact 200 feet short of the runway.
Final Conclusions
The Civil Aeronautics Board (CAB) determined the probable cause was the absence of approach and runway lights, combined with the failure of the GCA controller to provide more positive guidance to the pilot during the final stages of the approach. The board noted that the lighting deficiencies were not reported to the crew at Anchorage or during the approach, and the GCA transmissions were not recorded, in violation of standing instructions.
Photographic Evidence (1)
Video Analysis
No video analysis linked for this case file yet.
Airframe & Maintenance
Systems & Failure Modes
Ground Controlled Approach (GCA)
A radar-based landing system where a ground controller provides verbal instructions to the pilot to maintain the correct glidepath and centerline.
Runway Lighting
A system of approach, threshold, and runway edge lights; in this case, the red approach lights and initial runway pairs were non-functional, hindering visual transition.
Interesting Facts
- 01The aircraft was in full working order with all four engines running at the time of impact.
- 02The red runway approach lights and the first four pairs of runway lights were inoperative.
- 03The crew was not notified of the lighting deficiencies during their weather briefing in Anchorage.
- 04The GCA controller failed to use emergency frequencies or provide urgent corrections as the aircraft deviated below the glidepath.
- 05The flight was carrying 25,999 pounds of military cargo.
- 06Weather at the time included a 200-foot variable ceiling and 3/4 mile visibility in fog.
- 07GCA radio transmissions were not recorded, in direct violation of standing instructions.
Safety Actions & Advisories
GCA Standards Recommendation
The CAB recommended that the FAA Administrator take action to ensure personnel and equipment used in GCA approaches meet pertinent safety and operational standards.