N630PA

MINR
None

SWEARINGEN SA227 S/N: AC463

Accident Details

Date
Tuesday, November 30, 1993
NTSB Number
ANC94IA020
Location
KING SALMON, AK
Event ID
20001211X13673
Coordinates
58.750202, -156.540237
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
11
Total Aboard
11

Probable Cause and Findings

THE PILOT-IN-COMMAND DID NOT MAINTAIN CONTROL OF THE AIRPLANE AND DID NOT PERFORM THE APPROPRIATE PROCEDURES FOR AN ABORTED TAKEOFF. A FACTOR IN THE INCIDENT WAS THE ASYMMETRY IN POWER BETWEEN THE PLANE'S TWO ENGINES FOR UNDETERMINED REASONS.

Aircraft Information

Registration
N630PA
Make
SWEARINGEN
Serial Number
AC463
Year Built
2022
Model / ICAO
SA227

Registered Owner (Historical)

Name
AMAZON.COM SERVICES LLC
Address
ATTN: LEGAL DEPT
410 TERRY AVE N
Status
Deregistered
City
SEATTLE
State / Zip Code
WA 98109-5210
Country
United States

Analysis

On November 30, 1993, at 1858 Alaska standard time, a wheel equipped Fairchild (formerly Swearingen) SA227 Metroliner airplane, N630PA, registered to and operated by Peninsula Airways Inc. dba PENAIR, flight 4028, ran off the south side of runway 11 at the King Salmon Airport, King Salmon, Alaska during an aborted takeoff. The airline transport certificated pilot-in-command and first officer (both captains) and the nine revenue passengers were not injured. The airplane sustained minor damage. The 14 CFR Part 135 scheduled commuter flight originated at King Salmon and the intended destination was Anchorage, Alaska. Visual meteorological conditions prevailed and an instrument flight plan was in effect.

Telephone interviews were conducted with the captain and first officer by the NTSB investigator-in-charge. The captain reported that he aligned the airplane with the runway centerline using the plane's nose wheel steering, then, per the PENAIR airplane checklist, he disconnected the nose wheel steering. The captain said that he called for speeds high (96% to 97%) on both power levers. The first officer said that in order to prevent any adverse yaw during the initial stages of the takeoff run, he adjusted the power levers, advancing the left engine throttle ahead of the right by approximately 1 inch because the left engine was historically slower to respond. The captain said that the power from the right engine stopped advancing, "perhaps" halfway into the throttle run, and the plane began diverging to the right. The captain said that he glanced at the engine instruments and observed, albeit, to an unknown degree, an asymmetry in torque between the No.1 and 2 engines. The plane's ground speed at the time was between 20 and 30 knots. The captain said that he immediately attempted to bring both engine power levers back to their flight idle stops then up and over the gate to the ground idle position. The captain said that in his haste to accomplish the abort, he was not able to get the left power lever back to ground idle before the impact. The captain said that he attempted to keep the airplane on the runway with differential braking but was not successful. The plane's nose landing wheel collided with the northwest arresting barrier pit resulting in extensive damage to the nose gear assembly. Both crewmembers said that during the rejected takeoff (RTO) sequence no verbal communication transpired between them and that at the time of the RTO, the surface condition of the runway, for the most part, was clear and dry.

The director of airport operations for the King Salmon Airport examined the area of the incident shortly after it occurred. The director reported that the airplane did not leave heavy rubber reversion deposits on the surface of the runway.

The results of the toxicological examinations conducted on the flightcrew were negative.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC94IA020