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Aviation safety reports, made easier to study

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July 28, 1988 · Fairchild SA227-AT · N482SA

Anchorage, AK

Overview

Report Status
Preliminary report
Event Type
Accident
Date
July 28, 1988
Injury Outcomes
No injuries (8 uninjured)
Location
Anchorage, AK
Aircraft
Fairchild SA227-AT
Tail Number
N482SA
Operator
Peninsula Airways
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC88FA100

During the taxi to the runway, the flight crew noted a vibration in the airplane and stopped to check the tires, thinking that they were underinflated. No obvious problem was seen, and they elected to takeoff. Shortly after takeoff, a fire erupted in the left main gear wheelwell. The pilot returned to the airport and landed safely. However, the airplane sustained extensive damage to the left wing and aileron control system. Examination of the brakes revealed a cocked thermal insulator in the piston bore. There was evidence that the brakes were worn, had been dragging, then overheated; and that the tires had exploded prior to the fire. The fire damage indicated that the fire had started near the brakes. An aluminum fitting was used as part of the hydraulic brake system on the steel brake housing. The exam indicated that the fitting had been installed but could not be found after the fire. The crew said that they delayed lowering the gear, in contradiction to the checklist requirement when the wheelwell and wing overheat light is on.

Full Narrative

DURING THE TAXI TO THE RUNWAY, THE FLIGHT CREW NOTED A VIBRATION IN THE AIRPLANE AND STOPPED TO CHECK THE TIRES, THINKING THAT THEY WERE UNDERINFLATED. NO OBVIOUS PROBLEM WAS SEEN, AND THEY ELECTED TO TAKEOFF. SHORTLY AFTER TAKEOFF, A FIRE ERUPTED IN THE LEFT MAIN GEAR WHEELWELL. THE PILOT RETURNED TO THE AIRPORT AND LANDED SAFELY. HOWEVER, THE AIRPLANE SUSTAINED EXTENSIVE DAMAGE TO THE LEFT WING AND AILERON CONTROL SYSTEM. EXAMINATION OF THE BRAKES REVEALED A COCKED THERMAL INSULATOR IN THE PISTON BORE. THERE WAS EVIDENCE THAT THE BRAKES WERE WORN, HAD BEEN DRAGING, THEN OVERHEATED; AND THAT THE TIRES HAD EXPLODED PRIOR TO THE FIRE. THE FIRE DAMAGE INDICATED THAT THE FIRE HAD STARTED NEAR THE BRAKES. AN ALUMINUM FITTING WAS USED AS PART OF THE HYDRAULIC BRAKE SYSTEM ON THE STEEL BRAKE HOUSING. THE EXAM INDICATED THAT THE FITTING HAD BEEN INSTALLED BUT COULD NOT BE FOUND AFTER THE FIRE. THE CREW SAID THAT THEY DELAYED LOWERING THE GEAR, IN CONTRADICTION TO THE CHECKLIST REQUIREMENT WHEN THE WHEELWELL AND WING OVERHEAT LIGHT IS ON.

Flight

Event TypeAccident
Event Time18:17 AKDT
Nearest AirportAnchorage Int'L (0nm N)
Runway14
Runway Length10496 ft
Runway Width150 ft
Flight Plan FiledIFR
Aircraft FireIflt
Aircraft ExplosionNo

Aircraft

AircraftFairchild SA227-AT
Tail NumberN482SA
Aircraft CategoryAir
DamageSubstantial
OperatorPeninsula Airways
Operating RulePart 135
Engines2
Engine TypeTurboprop
Engine DetailsGarrett · TPE-331-1146 · Turboprop · 1000
Seats20

People & Injuries

Injury SummaryNo injuries (8 uninjured)
Fatal0
Serious0
Minor0
Uninjured8
Total8
Crew 1Age 39 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind170° @ 16 kt, gusting 23 kt
Visibility60 sm
CeilingNone
Temperature / Dew Point63 F / 46
Altimeter29.00 inHg
Observation Time21:20
Weather SourceWFAC

Appendix: Source Data