20010827025879A

Accident · No damage

FAA accident report · Cessna R172K · Valdosta, GA · August 27, 2001

Date
August 27, 2001 · 10:44 local
Place
Valdosta, GA
Airport
Valdosta Regional Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N758BW
NTSB investigation
NTSBATL01LA096
Reported as
Cessna R172K

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.

(-23) The instructor pilot was attempting to demonstrate engine failure after takeoff. At approximately 100 feet AGL, after a short field takeoff, the throttle was retarded to simulate the engine failure. The instructor, wiht assist from the student, lowered the nose to maintain approach speed. The initial effort was not sufficient and a correction was made so that the aircraft was diving toward the ground. The flare was initiated, but the descent was not arrested, and the aircraft struck the ground, left main, nose, right main, in that order. Additional power was not added during this approach. The left main strut bent and the wheel cambered toward the fuselage. The nose gear collapsed forward and right into the engine mount area. The fire wall buckled and the fuselage was damaged aft of the firewall. The left door frame is sprung and the door will not close. According to the IA who examined the aircraft, this airframe is totaled.

As the FAA filed it

(-23) THE INSTRUCTOR PILOT WAS ATTEMPTING TO DEMONSTRATE ENGINE FAILURE AFTER TAKEOFF. AT APPROXIMATELY 100 FEET AGL, AFTER A SHORT FIELD TAKEOFF, THE THROTTLE WAS RETARDED TO SIMULATE THE ENGINE FAILURE. THE INSTRUCTOR, WIHT ASSIST FROM THE STUDENT, LOWERED THE NOSE TO MAINTAIN APPROACH SPEED. THE INITIAL EFFORT WAS NOT SUFFICIENT AND A CORRECTION WAS MADE SO THAT THE AIRCRAFT WAS DIVING TOWARD THE GROUND. THE FLARE WAS INITIATED, BUT THE DESCENT WAS NOT ARRESTED, AND THE AIRCRAFT STRUCK THE GROUND, LEFT MAIN, NOSE, RIGHT MAIN, IN THAT ORDER. ADDITIONAL POWER WAS NOT ADDED DURING THIS APPROACH. THE LEFT MAIN STRUT BENT AND THE WHEEL CAMBERED TOWARD THE FUSELAGE. THE NOSE GEAR COLLAPSED FORWARD AND RIGHT INTO THE ENGINE MOUNT AREA. THE FIRE WALL BUCKLED AND THE FUSELAGE WAS DAMAGED AFT OF THE FIREWALL. THE LEFT DOOR FRAME IS SPRUNG AND THE DOOR WILL NOT CLOSE. ACCORDING TO THE IA WHO EXAMINED THE AIRCRAFT, THIS AIRFRAME IS TOTALED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.