ERA13CA280

NTSB accident investigation · Piper PA-25-260 · Hollywood, FL · May 31, 2013

Accident · No injuriesData collectionFinal report
Date
May 31, 2013, 18:36 local (22:36 UTC)
Place
Hollywood, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N169ABPiper PA-25-260
Defining event
Landing-landing roll: Loss of control on ground
Weather
Visual (VMC) · Dusk
Status
Completed · report July 29, 2013
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20130531011109A
Case key
87172

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 pilot's failure to maintain directional control during the landing roll.

Findings · 2

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.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedPiper PA-25-260: 2 casesAll aircraft: 3,958 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotPiper PA-25-260: 5 casesAll aircraft: 9,295 casesProbable cause

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 operator, the pilot performed several practice banner pick-ups in the tailwheel equipped airplane prior to joining the traffic pattern to land. The final approach was uneventful, the tailwheel contacted the runway first, and then the airplane settled onto the runway. During the landing roll, the airplane veered to the right, and the pilot applied full power in an attempt to "fly out of the ground loop." As the airspeed of the airplane increased, it departed the runway, struck a taxiway sign, and came to rest inverted, which resulted in substantial damage to the fuselage. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Factual narrative

According to the operator, the pilot performed several practice banner pick-ups in the tailwheel equipped airplane prior to joining the traffic pattern to land. The final approach was uneventful, the tailwheel contacted the runway first, and then the airplane settled onto the runway. During the landing roll, the airplane veered to the right, and the pilot applied full power in an attempt to "fly out of the ground loop." As the airspeed of the airplane increased, it departed the runway, struck a taxiway sign, and came to rest inverted, which resulted in substantial damage to the fuselage. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Aircraft

Registration
N169AB
Reported as
Piper PA-25-260
Category
Airplane
Serial number
25-4517
Airframe hours
6,636
Engine
Lycoming O-540 SERIES, 250 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Aerial Banners North Inc
Registered owner
Aerial Banners North Inc
Airworthiness certificate
Standard, Utility
Last inspection
100 hour · May 28, 2013
Departed
HWO · Hollywood, FL
Destination
HWO · Hollywood, FL
Airport
HWO · North Perry Airport, runway 10L, 3,240 × 100 ft, asphalt

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
24
Injuries
Minor
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
August 29, 2012
Seat
Single
Flight hours
621 total · 2 in this make and model · 440 as pilot in command · 10 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Dusk
Wind
100° at 10 knots
Visibility
10 statute miles
Lowest ceiling
10,000 ft broken
Temperature
81 °F, dew point 72 °F
Altimeter
30.03 inHg
Observed at
HWO

Docket · 6

The files NTSB released with the investigation on July 16, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.1 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.

Other investigations on N169AB · 1

Matched to the same aircraft by N-number and date.