SEA93FA094

NTSB accident investigation · Grumman A6E · Steptoe, WA · April 14, 1993

Accident · Serious injuriesField investigationFinal report
Date
April 14, 1993, 15:24 local (22:24 UTC)
Place
Steptoe, WA
Injuries
2 serious, 1 minor
Phase of flight
Maneuvering
Aircraft
USNGrumman A6EN8630HGrumman-Schweizer G-164A
Weather
Visual (VMC) · Day
Status
Completed · report March 18, 1994
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19930414017212A
Case key
42938

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The inherent limitations of the see-and-avoid concept of separation of aircraft operating under visual flight rules that precluded the crew of the A6E and the pilot of the agcat from recognizing a collision hazard and taking actions to avoid a midair collision.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Midair collisionManeuvering
Visual separation - not possiblePilot in commandCause
Visual separation - not possiblePilot of other aircraftCause
Midair collisionCruise
Visual separation - not possiblePilot in commandCause
Visual separation - not possiblePilot of other aircraftCause

Analysis

The A6E was tracking 033 deg level at 200 ft AGL at 468 KTS VFR in published route VR-1354. The agcat was tracking 334 deg level at 200 ft AGL at 96 KTS VFR across the route to his destination spray field. The two aircraft converged on a 59 deg collision angle with a closure speed of 429 KTS. The A6E notified fss that he was entering the route late and projected exiting 8 minutes after the published closure of the route. The agcat pilot reported he was unaware of any information/publications regarding the operation of military aircraft in the area. The local fss was in the habit of reporting the route 'hot' 24 hrs a day rather than the precise schedule. The convergence angle of the A6E was 111 deg (8 o'clock position & behind the agcat's left wing). The convergence angle of the agcat was 10 deg. At the projected closure speed the agcat would have subtended an angle of 0.2 deg 8.6 secs before impact; the A6E 19.2 secs.

Aircraft · 2

Registration
USN
Reported as
Grumman A6E
Category
Airplane
Serial number
155665
Airframe hours
4,784
Engine
P&W J52P-8B, 8,700 lbs thrust, turbo jet
Damage
Destroyed
Fire
In-Flight
Flight
Armed forces
Operator
United States Navy
Registered owner
United States Navy
Last inspection
Continuous airworthiness · November 28, 1992 · 131 hours before
Departed
NUW · Nas Whidbey Is, WA
Destination
NUW
Flight plan
IFR
Registration
N8630H
Reported as
Grumman-Schweizer G-164A
Category
Airplane
Serial number
1439
Airframe hours
5,014
Engine
P&W R-1340, 600 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Aerial application · Part 137
Operator
Fender, Darrell
Registered owner
Fender, Darrell
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · February 4, 1993 · 94 hours before
Departed
0WA0 · Colfax, WA
Destination
0WA0

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot, aircraft 1
Age
31
Certificates
Commercial, Military
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,814 total · 201 in this make and model · 93 in the last 90 days · 26 in the last 30 days · 1 in the last 24 hours
Role
Pilot, aircraft N8630H
Age
40
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Front
Flight hours
2,231 total · 1,460 in this make and model · 2,200 as pilot in command · 50 in the last 90 days · 50 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
20 statute miles
Lowest ceiling
2,500 ft broken
Temperature
45 °F, dew point 37 °F
Altimeter
30.00 inHg
Observed at
PUW, 18 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.