SEA08CA009

NTSB accident investigation · Piper PA-22/20 · Townsend, MT · October 10, 2007

Accident · No injuriesData collectionFinal report
Date
October 10, 2007, 10:50 local (16:50 UTC)
Place
Townsend, MT
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N1139CPiper PA-22/20
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2007
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20071010022229A
Case key
66881

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 private pilot/student failed to maintain directional control during the landing roll, and remedial action was not possible by the flight instructor which resulted in an inadvertent ground loop.

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.

Loss of control - on ground/waterLanding - roll
Directional control - not maintainedDual studentCause
Remedial action - not possiblePilot in command(cfi)Cause
Ground loop/swerve - inadvertentPilot in command(cfi)
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - ground

Analysis

The flight instructor stated that the purpose of the flight was for the private pilot/owner to receive instruction for the tailwheel endorsement. After practicing several successful takeoffs and landings, the flight instructor had the private pilot set-up for a full stop wheel landing to runway 16, which had a six knot, 45 degree crosswind. While in ground effect, the private pilot reduced the throttle too fast, which increased the sink rate and the aircraft touched down firmly on the mains. The private pilot arrested the bounce with forward pressure before the aircraft lifted off, and applied some power to maintain directional control. The aircraft then began to make an excursion from the runway centerline and the private pilot lowered the tail which made the aircraft unstable. The flight instructor then assisted the private pilot and stabilized the aircraft. The private pilot then indicated that he could handle the situation, and the flight instructor returned control back to the private pilot. The flight instructor stated that he may have returned control back to the private pilot too quickly, as the situation degraded to large excursion from centerline, and the aircraft diverted from normal track. The flight instructor was not able to regain directional control and the aircraft ground looped to the left. During the ground loop, the right wing and elevator contacted the ground and were structurally damaged.

Factual narrative

The flight instructor stated that the purpose of the flight was for the private pilot/owner to receive instruction for the tailwheel endorsement. After practicing several successful takeoffs and landings, the flight instructor had the private pilot set-up for a full stop wheel landing to runway 16, which had a six knot, 45 degree crosswind. While in ground effect, the private pilot reduced the throttle too fast, which increased the sink rate and the aircraft touched down firmly on the mains. The private pilot arrested the bounce with forward pressure before the aircraft lifted off, and applied some power to maintain directional control. The aircraft then began to make an excursion from the runway centerline and the private pilot lowered the tail which made the aircraft unstable. The flight instructor then assisted the private pilot and stabilized the aircraft. The private pilot then indicated that he could handle the situation, and the flight instructor returned control back to the private pilot. The flight instructor stated that he may have returned control back to the private pilot too quickly, as the situation degraded to large excursion from centerline, and the aircraft diverted from normal track. The flight instructor was not able to regain directional control and the aircraft ground looped to the left. During the ground loop, the right wing and elevator contacted the ground and were structurally damaged.

Aircraft

Registration
N1139C
Reported as
Piper PA-22/20
Category
Airplane
Serial number
22-975
Engine
Lycoming O-320, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Douglas S. Cairns
Airworthiness certificate
Standard, Normal
Departed
8U9 · Canyon Ferry, MT
Destination
8U8 · Townsend, MT
Airport
8U8 · Townsend, runway 16, 4,000 × 60 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
0
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2
Flight hours
5,942 total · 10 in this make and model · 121 in the last 90 days · 34 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 6 knots
Visibility
30 statute miles
Lowest ceiling
None

FAA reports on this event · 1

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