FTW98LA124

NTSB accident investigation · Piper PA-22-108 · Frederick, OK · February 3, 1998

Accident · No injuriesLimited investigationFinal report
Date
February 3, 1998, 09:00 local (15:00 UTC)
Place
Frederick, OK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N4654ZPiper PA-22-108
Weather
Visual (VMC) · Day
Status
Completed · report December 8, 1998
Report
Approved by Office Director
FAA report
19980203003589A
Case key
20535

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 loss of wheel brakes due to the failure of the brake actuating cable. A factor was the tailwind.

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.

Airframe/component/system failure/malfunctionLanding - roll
Landing gear,normal brake system - failureCause
OverrunLanding - roll
Weather condition - tailwindFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - dirt bank/rising embankment

Analysis

The 35-hour student pilot stated that he was aware that he was landing downwind, but feared that he might have lost visual contact with the airport due to the fog that was forming, if he had attempted to circle the airport to land on runway 3. The pilot reported the winds from 030 degrees at 15 knots and stated that he touched down midfield on the 4,800-foot runway. During the landing roll, he started to apply the wheel brakes as he approached the departure end of the runway. While applying brake pressure with the brake lever, the cable to the brakes snapped resulting in the total loss of braking action. The airplane overran the departure end of the runway, and the nose wheel impacted a ridge/terrace in the wheat field adjacent to the airport. The 1961 model 'Colt' had accumulated a total of 1,715 airframe hours. According to the manufacturer's illustrated parts catalog, the failed cable assembly for the brake control, part number 40123-91, is a condition item without a specific replacement or retirement time. The cable separated at the point where it makes a sharp turn over a pulley (part number 11200-00).

Factual narrative

On February 3, 1998, at 0900 central standard time, a Piper PA-22-108 airplane, N4654Z, was substantially damaged during a runway overrun while landing near Frederick, Oklahoma. The student pilot, sole occupant of the airplane, was not injured. The airplane was owned and operated by the pilot under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the instructional flight for which a flight plan was not filed. The local flight originated from the Frederick Municipal Airport at approximately 0800.

The student pilot reported that the flight departed from Runway 35 at the Frederick Municipal Airport "for some upper air work in the local practice area." The pilot further stated that fog started to form in the vicinity of the airport, so he elected to proceed direct to the airport to avoid the inclement weather. The pilot stated that he was aware that he was landing downwind on runway 21, but feared that he might have lost visual contact with the airport if he had attempted to circle the airport to land on runway 03. The pilot reported the winds from 030 degrees at 15 knots.

The pilot stated that he made a normal touchdown midfield on the 4,800 foot concrete runway. During the landing roll, he started to apply the wheel brakes as he approached the departure end of the runway. While applying brake pressure with the brake lever, the cable to the brakes snapped, resulting in the total loss of braking action. The airplane overran the departure end of the runway, and the nose wheel impacted a ridge/terrace in the wheat field adjacent to the airport.

The student pilot had accumulated a total of 35 hours, of which 28 were in the accident airplane. He reported that he purchased the airplane in September from its second owner. The airplane had accumulated 12 hours since it's last annual inspection, which was completed in November 1997. The pilot suspected that the cable that failed was the one that came with the airplane when it was manufactured.

The nose gear dug into the soft ridge, and the airplane nosed over coming to rest in the inverted position. The vertical fin, rudder, the struts for the right wing, and the main spar for the left wing sustained structural damage. The leading edge of the right wing was also damaged.

The 1961 model "Colt" had accumulated a total of 1,715 airframe hours. According to the manufacturer's illustrated parts catalog, the failed brake cable assembly, part number 40123-91, is a condition item without a specific replacement or retirement time. The cable separated at the point where it makes a sharp turn over a pulley (part number 11200-00).

Aircraft

Registration
N4654Z
Reported as
Piper PA-22-108
Category
Airplane
Serial number
22-8177
Airframe hours
1,715
Engine
Lycoming O-235-A, 115 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Jimmy Craig Ripley
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 30, 1997 · 12 hours before
Departed
FDR
Airport
FDR · Frederick Municipal, runway 21, 4,800 × 150 ft, concrete

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
Certificate
Student
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
35 total · 28 in this make and model · 12 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 15 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F

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 N4654Z · 1

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