19990728010059A

Accident · Substantial damage

FAA accident report · Beech C-45H · Grain Valley, MO · July 28, 1999

Date
July 28, 1999 · 10:42 local
Place
Grain Valley, MO
Airport
East Kansas City Airport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N72409
NTSB investigation
NTSBCHI99LA262
Reported as
Beech C45H
Reported engine
Pratt & Whitney R985*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
666 total80 in this make and model37 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.

Acft lost control on take-off and sustained substantial damage. (.19) on July 28, 1999, at 1042 central daylight time, a Beech C-45H, N72409, piloted by a private pilot, sustained substantial damage after a loss of directional control on takeoff roll, on runway 27 (4,400 feet by 44 feet, dry asphalt), at the East Kansas City Airport, Grain Valley, Missouri. The personal flight was being conducted under the provisions of 14 CFR part 91 and was not on a flight plan. The pilot, who was the sole occupant, reported no injuries. The flight was originating at the time of the accident and was en route to the Kansas city international airport, Kansas city, Missouri. (-23)the PIC stated he lost directional control during takeoff. At a point approximately 500' into the takeoff roll the aircraft departed from centerline and exited the runway on the left side and then crossed the runway and exited on the right side of the runway and approximately 1500' west of the departure end of runway 27. This operation resulted in substantial damage to the aircraft. All three landing gear had separated from the aircraft, both propellers were damaged, right engine had broken loose from the mounts and damage to the wing spar, and stabilizer as well as other airframe damage. (.4) during takeoff, the aircraft departed the prepared runway surface and impacted a ditch adjacent to the runway. During a post accident examination, a federal aviation administration inspector noted that the tailwheel was not in the locked position. No anomalies were found that could be associated with a preexisting condition.

As the FAA filed it

ACFT LOST CONTROL ON TAKE-OFF AND SUSTAINED SUBSTANTIAL DAMAGE. (.19) ON JULY 28, 1999, AT 1042 CENTRAL DAYLIGHT TIME, A BEECH C-45H, N72409, PILOTED BY A PRIVATE PILOT, SUSTAINED SUBSTANTIAL DAMAGE AFTER A LOSS OF DIRECTIONAL CONTROL ON TAKEOFF ROLL, ON RUNWAY 27 (4,400 FEET BY 44 FEET, DRY ASPHALT), AT THE EAST KANSAS CITY AIRPORT, GRAIN VALLEY, MISSOURI. THE PERSONAL FLIGHT WAS BEING CONDUCTED UNDER THE PROVISIONS OF 14 CFR PART 91 AND WAS NOT ON A FLIGHT PLAN. THE PILOT, WHO WAS THE SOLE OCCUPANT, REPORTED NO INJURIES. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT AND WAS EN ROUTE TO THE KANSAS CITY INTERNATIONAL AIRPORT, KANSAS CITY, MISSOURI. (-23)THE PIC STATED HE LOST DIRECTIONAL CONTROL DURING TAKEOFF. AT A POINT APPROXIMATELY 500' INTO THE TAKEOFF ROLL THE AIRCRAFT DEPARTED FROM CENTERLINE AND EXITED THE RUNWAY ON THE LEFT SIDE AND THEN CROSSED THE RUNWAY AND EXITED ON THE RIGHT SIDE OF THE RUNWAY AND APPROXIMATELY 1500' WEST OF THE DEPARTURE END OF RUNWAY 27. THIS OPERATION RESULTED IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT. ALL THREE LANDING GEAR HAD SEPARATED FROM THE AIRCRAFT, BOTH PROPELLERS WERE DAMAGED, RIGHT ENGINE HAD BROKEN LOOSE FROM THE MOUNTS AND DAMAGE TO THE WING SPAR, AND STABILIZER AS WELL AS OTHER AIRFRAME DAMAGE. (.4) DURING TAKEOFF, THE AIRCRAFT DEPARTED THE PREPARED RUNWAY SURFACE AND IMPACTED A DITCH ADJACENT TO THE RUNWAY. DURING A POST ACCIDENT EXAMINATION, A FEDERAL AVIATION ADMINISTRATION INSPECTOR NOTED THAT THE TAILWHEEL WAS NOT IN THE LOCKED POSITION. NO ANOMALIES WERE FOUND THAT COULD BE ASSOCIATED WITH A PREEXISTING CONDITION.

NTSB investigation

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