19970222006479I

Incident · Minor damage

FAA incident report · Cessna 152 · Provo, UT · February 22, 1997

Date
February 22, 1997 · 16:00 local
Place
Provo, UT
Airport
Provo Municipal Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N108ES
Reported as
Cessna 152
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,350 total300 in this make and model75 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Narrative: aircraft was on departure climb from cedar valley airport with pilot under instruction at the flight controls. Engine began to run rough and lose power so flight instructor took control of the aircraft and applied carburetor heat. Engine did not immediately regain power so the flight instructor pushed the carburetor heat control back in to the off position. Instructor executed an emergency landing to a nearby dirt strip. Upon landing the propellor contacted the surface in that it was very soft and muddy. The crew waited approximately two hours, restarted the aircraft and executed a takeoff and flew the aircraft to the home base at Provo, Utah without further incident. Damage was sustained to the propeller with a number of nicks being made in the propellor blades from contacting the mud on the runway. The nose wheel shock strut was bent slightly aft, right hand upper and left hand lower vertical engine mounts were slightly bent. This investigation is final and closed.

As the FAA filed it

NARRATIVE: AIRCRAFT WAS ON DEPARTURE CLIMB FROM CEDAR VALLEY AIRPORT WITH PILOT UNDER INSTRUCTION AT THE FLIGHT CONTROLS. ENGINE BEGAN TO RUN ROUGH AND LOSE POWER SO FLIGHT INSTRUCTOR TOOK CONTROL OF THE AIRCRAFT AND APPLIED CARBURETOR HEAT. ENGINE DID NOT IMMEDIATELY REGAIN POWER SO THE FLIGHT INSTRUCTOR PUSHED THE CARBURETOR HEAT CONTROL BACK IN TO THE OFF POSITION. INSTRUCTOR EXECUTED AN EMERGENCY LANDING TO A NEARBY DIRT STRIP. UPON LANDING THE PROPELLOR CONTACTED THE SURFACE IN THAT IT WAS VERY SOFT AND MUDDY. THE CREW WAITED APPROXIMATELY TWO HOURS, RESTARTED THE AIRCRAFT AND EXECUTED A TAKEOFF AND FLEW THE AIRCRAFT TO THE HOME BASE AT PROVO, UTAH WITHOUT FURTHER INCIDENT. DAMAGE WAS SUSTAINED TO THE PROPELLER WITH A NUMBER OF NICKS BEING MADE IN THE PROPELLOR BLADES FROM CONTACTING THE MUD ON THE RUNWAY. THE NOSE WHEEL SHOCK STRUT WAS BENT SLIGHTLY AFT, RIGHT HAND UPPER AND LEFT HAND LOWER VERTICAL ENGINE MOUNTS WERE SLIGHTLY BENT. THIS INVESTIGATION IS FINAL AND CLOSED.

Other reports on N108ES · 2

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