Cessna Safety Record

THE PILOT'S INADVERTENT STALL DURING THE PULL UP. FACTORS WERE THE LOW PASS, HIS OSTENTATIOUS DISPLAY, AND HIS INABILITY TO RECOVER FROM THE STALL DUE TO INSUFFICIENT ALTITUDE.

FAILURE OF THE LOCAL TOWER CONTROLLER TO ADEQUATELY CONTROL THE ARRIVAL OF THE AIRPLANES, AND INADEQUATE VISUAL LOOKOUT BY THE PIPER PA-24 PILOT. A FACTOR RELATED TO THE ACCIDENT WAS: THE LOCAL CONTROLLER'S IMPROPER PHRASEOLOGY IN SEQUENCING THE AIRPLANES.

the failure of the pilot to apply carburetor heat as appropriate while conducting flight in conditions conducive for carburetor icing. A factor in the accident was the unsuitable steep mountainous terrain for a forced landing.

the pilot's intentional VFR flight into known adverse IMC weather conditions. Inadequate preflight planning, dark night operations, and weather conditions that included low ceilings and mountain obscuration were factors in the accident.

THE PILOT'S FAILURE TO MAINTAIN A PROPER ALTITUDE WHILE IN THE VFR TRAFFIC PATTERN, RESULTING IN A COLLISION WITH TREES. FACTORS WERE; HIS FAILURE TO COMPLY WITH SCHOOL DIRECTIVES BY NOT OBTAINING A WEATHER BRIEFING PRIOR TO THE ACCIDENT FLIGHT, AND THE RAIN, GUSTING WINDS, AND DARK NIGHT CONDITIONS AT TIME OF THE ACCIDENT.

the pilot's failure to maintain control of the aircraft's flight path while maneuvering after takeoff in an area of no ground reference lights. Factors in the accident were the pilot's lack of instrument flight experience and the dark nighttime lighting conditions.

The pilot's inadequate inflight decision which resulted in ice accretion on the aircraft, degradation of aircraft performance, an aerodynamic stall, loss of control and inflight collision with the ground. Factors were icing conditions.

WAS THE LOSS OF CONTROL DUE TO THE PILOT'S SPATIAL DISORIENTATION FOLLOWING A COMPLETE ELECTRICAL SYSTEM FAILURE. FACTORS WERE THE DARK NIGHT AND THE ELECTRICAL FAILURE AS RESULT OF BURNED OUT WIRING TERMINAL.

FAILURE OF THE PILOT TO MAINTAIN CONTROL OF THE AIRCRAFT, WHILE MANEUVERING TO LAND. FACTORS RELATED TO THE ACCIDENT WERE: DARKNESS AND POSSIBLE SPATIAL DISORIENTATION.

THE PILOT'S FAILURE TO MAINTAIN CONTROL OF THE AIRCRAFT DUE TO SPATIAL DISORIENTATION, AND EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRCRAFT. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S FLIGHT INTO KNOWN ADVERSE WEATHER CONDITIONS, OVERCONFIDENCE IN HIMSELF AND THE AIRPLANE, FAILURE OF THE LEFT VACUUM PUMP, PARTIAL LOSS OF THE VACUUM SYSTEM, AND AN INOPERATIVE ATTITUDE INDICATOR.

FAILURE OF THE PILOT TO MAINTAIN PROPER ALTITUDE DURING A MISSED APPROACH. FACTORS RELATED TO THE ACCIDENT WERE: THE UNFAVORABLE WEATHER AND SNOW COVERED TERRAIN.

THE PILOT'S IMPAIRMENT OF JUDGMENT AND PERFORMANCE DUE TO ALCOHOL AND DRUGS, WHICH LED TO HIS IMPROPER PLANNING/DECISION, AND HIS FAILURE TO MAINTAIN ALTITUDE/CLEARANCE FROM MOUNTAINOUS TERRAIN, WHILE MANEUVERING AT LOW ALTITUDE.

THE PILOT'S IMPAIRMENT OF JUDGMENT AND PERFORMANCE DUE TO ALCOHOL, WHICH LED TO HIS INTENTIONAL BUZZING, AND HIS FAILURE TO MAINTAIN SUFFICIENT ALTITUDE (OR CLEARANCE) FROM OBSTACLES. FACTORS RELATED TO THE ACCIDENT WERE: DARKNESS AND THE UNLIGHTED TOWER.

The pilot-in-command's failure to maintain a visual lookout and altitude while maneuvering after becoming lost/disoriented, resulting in an in-flight collision with trees and terrain. Contributing to the accident was the pilot's physical impairment due to prescription drugs, and self-induced anxiety and apprehension due to becoming lost and disoriented.

IMPROPER SERVICING OF THE AIRPLANE WITH JET FUEL, WHICH RESULTED IN PREIGNITION AND/OR DETONATION AND SUBSEQUENT FAILURE OF PISTONS IN BOTH ENGINES. A FACTOR RELATED TO THE ACCIDENT WAS: THE LACK OF A RESTRICTIVE MATING NOZZLE ON THE REFUELING TRUCK.

the pilot-in-command's continued operation with known deficiencies in equipment. Factors were ice on the windshield and the pilot-in-commands visual outlook not possible.