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Last updated: 25 June 2021
Datum:vrijdag 4 juni 1976
Tijd:14:47 UTC
Type:Silhouette image of generic L188 model; specific model in this crash may look slightly different
Lockheed L-188A Electra
Luchtvaartmaatschappij:Air Manila International
Registratie: RP-C1061
Constructienummer: 1007
Bouwjaar: 1958-09-17 (17 years 9 months)
Motoren: 4 Allison 501-D13
Bemanning:slachtoffers: 12 / inzittenden: 12
Passagiers:slachtoffers: 33 / inzittenden: 33
Totaal:slachtoffers: 45 / inzittenden: 45
Slachtoffers op de grond:slachtoffers: 1
Schade: Afgeschreven
Gevolgen: Written off (damaged beyond repair)
Plaats:1,5 km (0.9 mijl) NE of Guam-Agana NAS (NGM) (   Guam)
Fase: InitiŽle klim (ICL)
Soort vlucht:Internationale charter
Vliegveld van vertrek:Guam-Agana NAS (NGM), Guam
Vliegveld van aankomst:Manila International Airport (MNL/RPLL), Filippijnen
Vluchtnummer: 702
At 21:09 GMT Air Manila flight 702 departed Wake Island for Manila, with an enroute stop at Agana Naval Air Station (NAS). The aircraft arrived at 02:11 GMT. After offloading the passengers maintenance was performed on the no. 2 propeller feathering mechanism. Shortly after the work was completed, the passengers boarded and the flightcrew started all four engines without difficulty. The flightcrew taxied the aircraft to the end of runway 06L, made a right turn onto the runway, and executed a rolling takeoff. The aircraft lifted off the 10,015-foot runway about 7500 feet down the runway. During or just after liftoff the No. 3 propeller was feathered. The aircraft climbed to 100 feet while yawing to the right. The crew retracted the landing gear and flaps before the aircraft reached the apex of the climb. It then rotated to a nose-high attitude, appeared to become laterally unstable, and struck the rising terrain in a tail-low attitude. Impact was about 4,300 feet beyond the end of the runway. The aft portion of the aircraft fuselage dragged along the ground for 220 feet in a right wing down attitude, after which the aircraft slid off the brow of a 13-foot embankment, crashed through the chain link perimeter fence at Agana NAS, crossed a highway, and burst into flames. The aircraft came to rest in an open area between residential areas, about 4,900 feet beyond the end of runway 06L. As the aircraft slid across the highway, it struck an automobile on the highway; the driver of the car was killed. A woman and her son, who were standing outside their residence just south of the impact site, were seriously burned by the heat of the burning fuel and were seriously injured by flying debris.

Probable Cause:

PROBABLE CAUSE: "The loss of climb capability after the crew retracted the flaps at too low an altitude to clear the rising terrain. The flaps were retracted after the no.3 propeller feathered as the aircraft lifted off the runway. Contributing to the accident was the captain's decision to continue the take-off after an engine failed before reaching the rotation speed."

Accident investigation:
Investigating agency: NTSB
Status: Investigation completed
Duration: 1 year and 4 months
Accident number: NTSB/AAR-77-06
Download report: Final report

» Aviation News 25.06.1976
» NTSB-AAR-77-6



photo of Lockheed-L-188A-Electra-RP-C1061
accident date: 04-06-1976
type: Lockheed L-188A Electra
registration: RP-C1061

Deze kaart geeft het vliegveld van vetrek weer en de geplande bestemming van de vlucht. De lijn tussen de vliegvelden geeft niet de exacte vliegroute weer.
De afstand tussen Guam-Agana NAS en Manila International Airport bedraagt 2553 km (1595 miles).
Accident location: Approximate; accuracy within a few kilometers.

This information is not presented as the Flight Safety Foundation or the Aviation Safety Networkís opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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Lockheed L-188

  • 222 built
  • 26e ongeval
  • 15e dodelijk ongeval
  • 8e zwaarste ongeval (toen het plaatsvond)
  • 10e zwaarste ongeval (op dit moment)
» safety profile

  • 2e zwaarste ongeval (toen het plaatsvond)
  • 3e zwaarste ongeval (op dit moment)
» safety profile