IAD03LA026

NTSB accident investigation · Piper PA-28-140 · New Middleton, OH · January 11, 2003

Accident · Minor injuriesLimited investigationFinal report
Date
January 11, 2003, 11:30 local (16:30 UTC)
Place
New Middleton, OH
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N573PAPiper PA-28-140
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 2003
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20030111002709A
Case key
56319

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

A jammed throttle control assembly for undetermined reasons.

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 engine powerManeuvering
Throttle/power lever - jammedCause
Forced landingManeuvering
In flight collision with objectEmergency descent/landing
Object - tree(s)

Analysis

The flight instructor and commercial pilot were practicing flight maneuvers, which required full and idle power settings. At the completion of one of the reduced power maneuvers, when the commercial pilot tried to apply power, the throttle was "completely jammed" in the idle position. The flight instructor was unable to maintain altitude, and elected to land at a private airstrip. In preparation to land, the pilot extended the flaps to 40 degrees, and maintained an approach speed of approximately 80 mph. Prior to reaching the end of the runway, the airplane encountered a high sink rate and collided with trees located about 50 feet from the end of the runway. Examination of the airplane revealed that the throttle bracket was crushed from the impact, and the throttle linkage was kinked. The linkage was still intact at the carburetor. The carburetor was removed to help free the throttle linkage. Once removed, the throttle linkage moved freely, and fuel sprayed from the accelerator pump. No fretting or rubbing of the throttle linkage was noted. The throttle quadrant was removed and examined, and no discrepancies were noted.

Factual narrative

On January 11, 2003, at 1130 eastern standard time, a Piper PA-28-140, N573PA, was substantially damaged during a forced landing to a private airstrip near New Middletown, Ohio. The certified flight instructor and the certificated commercial pilot sustained minor injuries. No flight plan was filed for the flight that originated at New Castle Municipal Airport (UCP), New Castle, Pennsylvania, about 1050. Visual meteorological conditions prevailed for the local instructional flight, conducted under 14 CFR Part 91.

Prior to departure, the commercial pilot informed the flight instructor that there had been a discrepancy with the throttle, and the cable was replaced. During the pre-flight inspection, engine start, taxi, and engine run-up, there were no discrepancies with the throttle.

The flight instructor and commercial pilot flew to the practice area and practiced flight maneuvers which required low and high power settings. According to the flight instructor, at the completion of one of the reduced power maneuvers, at an altitude of 2,500 feet msl (1,500 feet agl), the commercial pilot went to apply power, but the throttle was "completely jammed."

The flight instructor was unable to maintain altitude due to the idle power setting, and elected to land at a private airstrip. While he flew the airplane, the commercial pilot made several attempts to move the throttle, but without any success. The mixture and carburetor heat controls worked normally.

In preparation to land, the flight instructor extended the flaps to 40 degrees, and maintained an approach speed of approximately 80 mph. Prior to reaching the end of the runway, the airplane encountered a high sink rate, and collided with trees.

Two Federal Aviation Administration (FAA) inspectors performed an on-scene examination. According to one of them, the airplane clipped a tree that was located about 50 feet from the end of the runway. After it clipped the tree, the nose of the airplane hit the ground, and airplane flipped over.

Examination of the airplane revealed that the throttle bracket was crushed from the impact, and the throttle linkage was kinked. However, the linkage was still intact at the carburetor. The inspectors removed the carburetor to help free the throttle linkage. Once removed, the throttle linkage moved freely, and fuel sprayed from the accelerator pump. No fretting or rubbing of the throttle linkage was noted. The throttle quadrant was removed and examined. No discrepancies were noted with the system.

Fuel was present in the carburetor, main fuel line, and both wing tanks.

New Middleton Airport was a private airport that was oriented North and South. The snow covered, turf runway was approximately 3,000 feet long and 50 feet wide, with a field elevation of 1,000 feet msl.

The certified flight instructor reported 3,073 flight hours, of which, 522 hours were in make and model.

The commercial pilot reported a total of 435 flight hours, of which, 60 hours were in make and model.

Weather at Youngstown Airport (YNG), Youngstown, Ohio, about 15 miles north, at 1151, was reported as winds from 230 degrees at 15 knots gusting to 20 knots, visibility 10 statute miles, scattered clouds 2, 800 feet, broken clouds at 3, 500 feet, temperature 46 degrees F, dewpoint 57 degrees F, and barometric pressure setting 30.01 inches HG.

Aircraft

Registration
N573PA
Reported as
Piper PA-28-140
Category
Airplane
Serial number
28-7525328
Airframe hours
7,141
Engine
Lycoming O-320, 180 hp, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Haski Aviation Of Pennsylvania Inc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 26, 2002 · 5 hours before
Departed
UCP · New Castle, PA
Airport
NONE · New Middletown, runway 36, 3,000 × 50 ft, grass/turf

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
Age
63
Injuries
Minor
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
September 1, 2002
Seat
Left
Flight hours
3,073 total · 522 in this make and model · 2,975 as pilot in command · 14 in the last 90 days · 9 in the last 30 days
Role
Other flight crew
Age
41
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
September 28, 2002
Seat
Right
Flight hours
435 total · 60 in this make and model · 341 as pilot in command · 9 in the last 90 days · 4 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
230° at 15 knots, gusting 20
Visibility
10 statute miles
Lowest ceiling
3,500 ft broken
Temperature
46 °F, dew point 57 °F
Altimeter
30.01 inHg
Observed at
YNG, 15 nm away

Docket · 5

The files NTSB released with the investigation on June 24, 2003, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 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 N573PA · 1

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