Aviation Accident Summaries

Aviation Accident Summary ANC02LA009

ANCHORAGE, AK, USA

Aircraft #1

N9908D

Piper PA-18

Analysis

The certificated flight instructor was providing instruction to the private pilot/new owner of a tundra tire-equipped, tailwheel airplane. The flight instructor occupied the rear seat of the airplane. The pilot/owner had accrued 66 total flight hours, 14 hours as pilot-in-command, and .5 hours in the accident airplane. Five minutes after takeoff, the student was performing a landing on an asphalt surface runway that had areas of ice along the edges. During the landing roll the airplane began to drift to the right. The instructor applied left rudder, but the airplane departed the right side of the runway into an area of snow. The airplane nosed over and received damage to the propeller, fuselage, and wing lift struts. The right master brake cylinder, installed in the front seat area, was serviced before the flight. A heater hose was installed in the cabin to direct heat into the rear seat area. The instructor reported that the airplane's right brake felt as if it was locked, which she said may have been due to overfilling the brake reservoir, and heating of the brake cylinder by the heater. The instructor cited two previous NTSB reports of brake cylinder locking after extended flight with a heater hose blowing hot air on a brake reservoir. A review of the two previous accidents disclosed airplanes had locked brakes during landing, both within five days of each other in 1997. The previous NTSB accident reports involved two aircraft where a heater hose was directed onto the master brake cylinders after the brake cylinders were serviced. One of the accidents involved 1.5 hours of flight time before landing. The second accident involved 3 hours of flight time before landing. The accident airplane's brake system was not examined postaccident.

Factual Information

On January 12, 2002, about 1332 Alaska standard time, a tundra tire-equipped Piper PA-18 airplane, N9908D, sustained substantial damage during landing at Merrill Field, Anchorage, Alaska. The airplane was being operated as a visual flight rules (VFR) local area instructional flight when the accident occurred. An airline transport certificated pilot/flight instructor, and the private certificated pilot/owner, were not injured. Visual meteorological conditions prevailed. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on January 12, the flight instructor reported that she occupied the rear of the airplane, and was providing instruction to the airplane's new owner, who occupied the front seat. The pilot/owner had accrued 66 total flight hours, 14 hours as pilot-in-command, and .5 hours in the accident airplane. The instructor said that following a "three point landing" on the asphalt surface of runway 06, the airplane began to drift to the right. The instructor said she told the pilot to apply left rudder. At the same time, the instructor applied left rudder, but the airplane departed the right side of the runway into an area of snow. The airplane nosed over and received damage to the propeller, fuselage, and wing lift struts. The instructor reported the accident flight departed Lake Hood Strip, Anchorage, and landed at Merrill Field about five minutes later. The flight was the pilot/owner's first flight in a tailwheel airplane. The instructor said that the middle of the runway at Merrill Field was sanded, but the edges of the runway were icy. At 1335, an Aviation Routine Weather Report (METAR) at Merrill Field was reporting, in part: Wind, 050 degrees (true) at 3 knots; visibility, 10 statute miles; clouds and sky condition, 2,400 feet overcast; temperature, 25 degrees F; dew point, 19 degrees F; altimeter, 29.92 inHg. In the Pilot/Operator report (NTSB form 6120.1/2) submitted by the instructor pilot, the instructor reported the airplane's right hydraulic brake reservoir was serviced before the flight. In addition, the instructor reported that a heater hose, routed to the rear seat, was installed the day before the accident flight. In the Pilot/Operator report, the instructor indicated the right brake felt as if it was locked. She included two previous NTSB reports containing references to locked brakes in the accident airplane make and model where the brake system was serviced before flight, and the utilization of a rear seat heater hose. A review of the two previous accidents by the NTSB IIC disclosed State of Alaska PA-18 airplanes had locked brakes during landing, both within five days of each other in 1997. The previous NTSB accident reports involved two aircraft where a heater hose was directed onto the master brake cylinders after the brake cylinders were serviced. One of the accidents involved 1.5 hours of flight time before landing. The second accident involved 3 hours of flight time before landing. The accident airplane's master brake cylinders are installed on the forward cockpit floor, adjacent to the front seat rudder pedals. The rear seat position does not have brake cylinders installed. Following the accident, the airplane was recovered from the accident scene. No postaccident inspection of the brake system was conducted.

Probable Cause and Findings

The flight instructor's inadequate supervision of the flight. Factors in the accident were the student's failure to maintain directional control of the airplane during the landing roll, icy runway conditions, and snow-covered terrain along the runway edges.

 

Source: NTSB Aviation Accident Database

Get all the details on your iPhone or iPad with:

Aviation Accidents App

In-Depth Access to Aviation Accident Reports