GAA17CA093

NTSB accident investigation · Piper PA 34 · Denton, TX · December 7, 2016

Accident · No injuriesData collectionFinal report
Date
December 7, 2016, 11:45 local (17:45 UTC)
Place
Denton, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N2844TPiper PA 34
Defining event
Taxi-from runway: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report July 20, 2017
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20161207024701A
Case key
94495

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

On this page

Probable cause

The flight instructor’s decision to continue to taxi the airplane to the parking area with a known brake malfunction, which resulted in a loss of directional control and subsequent impact with a parked airplane.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Info processing/decision: decision making/judgmentPersonnel issues › Action/decision · Instructor/check pilotPiper PA-34-200: 2 casesAll aircraft: 3,098 casesProbable cause
Landing gear system: brakeAircraft › Aircraft systems · FailurePiper PA-34-200: 2 casesAll aircraft: 297 casesProbable cause
Object/animal/substance: aircraftEnvironmental issues › Physical environment · Effect on operationPiper PA-34-200: 1 caseAll aircraft: 116 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

According to the flight instructor in the multiengine airplane, he occupied the right seat during the instructional flight. The flight instructor reported that, during the landing roll, the brakes on his side were inoperative, but the brakes used by the pilot under instruction appeared to function normally. The flight instructor allowed the pilot under instruction to taxi to parking. During the right turn in the parking area, the pilot under instruction was told to apply both brakes, and the airplane started to "pull left." The flight instructor attempted to use differential thrust to arrest the left pull by increasing the right engine speed, but the attempt had no effect. The flight instructor shut down both engines; however, the left wing struck a parked airplane and came to a stop. The airplane sustained substantial damage to the left wing. The flight instructor reported that the accident could have been prevented if he had stopped on the taxiway and not entered the parking ramp. A postaccident examination of the brake assembly revealed that the right brake actuator piston "o" ring had failed, which decreased hydraulic brake pressure and prevented proper brake function of the airplane.

Factual narrative

According to the flight instructor in the multi-engine airplane, he occupied the right seat during the instructional flight. The flight instructor reported that during the landing roll, the brakes on his side were inoperative, but the brakes used by the pilot under instruction appeared to function normally. The flight instructor allowed the pilot under instruction to taxi to parking. During the right turn in the parking area, the pilot under instruction was told to apply both brakes, and the airplane started to "pull left". The flight instructor attempted to use differential thrust to arrest the left pull by increasing the right engine speed, but the attempt had no effect. The flight instructor shut down both engines, however, the multi-engine airplane's left wing struck a parked single-engine airplane and came to a stop. The multi-engine airplane sustained substantial damage to the left wing. The flight instructor reported that the accident could have been prevented if he would have stopped on the taxiway and not entered the parking ramp. The brake assembly was examined to determine the scope of pre-accident mechanical malfunctions or failures with the airplane's brake system, that would have precluded normal operation. It was determined that the right side brake actuator piston "o" ring failed, which decreased hydraulic brake pressure, preventing proper brake function of the airplane.

Aircraft

Registration
N2844T
Reported as
Piper PA 34 (200)
Category
Airplane
Serial number
34-7250174
Built
1972
Airframe hours
10,733.6
Engines
Lycoming LIO-360, 200 horsepower, reciprocatingLycoming IO-360-CEI6, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
U S Aviation Group LLC
Registered owner
U S Aviation Group LLC
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · October 17, 2016
Departed
KDTO · Denton, TX
Destination
KDTO · Denton, TX
Flight plan
VFR
Airport
DTO · Denton Enterprise, runway 36, 7,002 × 150 ft, asphalt
Equipment
Stall warning system, Electronic primary flight display, ADS-B

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
Flight instructor
Age
24
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
February 26, 2016
Seat
Right
Restraint
3-point
Flight hours
657.4 total · 248.5 in this make and model · 585 as pilot in command · 204.1 in the last 90 days · 51.2 in the last 30 days
Role
Student pilot
Age
23
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
July 22, 2016
Seat
Left
Restraint
3-point
Flight hours
227.8 total · 13.1 in this make and model · 124.6 as pilot in command · 13.1 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
48 °F, dew point 39 °F
Altimeter
30.11 inHg
Observed at
DTO

Docket · 3

The files NTSB released with the investigation on June 21, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.9 MB in all.

FAA reports on this event · 1

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