Controlled Flight Into Terrain · NTSB CEN14FA414

PIPER PA 28R-201 — Steamboat Springs, CO

2 fatal Low-time pilot
DateAugust 9, 2014
LocationSteamboat Springs, CO
AircraftPIPER PA 28R-201
Purpose of flightInstructional
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceEnroute Controlled flight into terr/obj (CFIT)
Pilot age60
Pilot total time134 hrs · Low time
Time in type32 hrs
Fatalities2

Probable cause

The pilot’s inability to maintain a climb while attempting to cross over a mountain pass in high-density altitude conditions that degraded the airplane’s climb performance. Contributing to the accident was the pilot’s decision to attempt the flight in mountainous terrain and to enter the pass in such a way that an escape maneuver was not possible.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not attained/maintained - C
  • Aircraft-Aircraft oper/perf/capability-Aircraft capability-Climb capability-Capability exceeded - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Effect on equipment - C
  • Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - F
  • Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Decision related to condition - F
  • Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Response/compensation
  • Environmental issues-Physical environment-Terrain-Mountainous/hilly terrain-Ability to respond/compensate

What happened

The flight instructor and private pilot-rated student were flying a five-leg, cross-country flight to conclude a mountain flying training course. The final leg of the flight was intended to cross over the mountains near a popular mountain pass, which was frequented by local pilots because of the landmarks and highway below. When the flight was overdue, a search was conducted. The wreckage was located in a mountain pass about 2 miles south of the mountain pass that the pilots had intended to cross during the final leg. A postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation.

The density altitude around the time of the accident was calculated to be about 11,200 ft, which would have degraded the airplane's performance. According to the Pilot's Operating Handbook, at a density altitude of 11,200 ft with the landing gear and flaps retracted, the airplane would have had an expected climb rate of between 175 and 200 ft per minute (fpm). Documents about mountain flying found onboard the airplane stated that flight in mountains should not be attempted unless a climb rate of at least 200 ft per nautical mile (300 fpm) is available. Therefore, it is likely that the airplane could not attain a sufficient climb rate to clear mountainous terrain and that the pilot did not enter the pass at an appropriate entrance angle, which reduced the possibility of a successful escape maneuver.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →