1977 Beechcraft King Air C90
Location: Knoxville, TN
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Download | Browse | Engine Logbook LH PC-E24364 |
Download | Browse | Engine Logbook RH PC-E24410 |
Download | Browse | Propeller Logbook LH FY3324 |
Download | Browse | Propeller Logbook RH FY3326 |
Download | Browse | Salvage Bid Request N25DL |
- Item # 363483
DESCRIPTION OF ACCIDENT: "The cause of the loss was the collapse of the aircraft’s main landing gear roughly 800’ after the aircraft touched down at the McGee Tyson Airport in Knoxville, TN." "The nose gear stayed down and locked, so the failure was within the main landing gear down lock system."
AIRCRAFT: 1977 Beechcraft King Air C90 N25DL S/N: LJ-716 TT: ~9587.4
ENGINE: Pratt & Whitney Model: PT6A-21 S/N: PC-E 24364 TT: -9528 TSMOH: ~2574.7
ENGINE: Pratt & Whitney Model: PT6A-21 S/N: PC-E 24410 TT: -9528 TSMOH: ~2574.7
PROPELLER: Hartzell Model: HC-D4N-3C/D9290K S/N: FY3324 TT: ~218.4
PROPELLER: Hartzell Model: HC-D4N-3C/D9290K S/N: FY3326 TT: ~218.4
Date of Accident: April 9, 2019
Date of Last Annual Inspection: ; April 8, 2019, Complied with phase 1-4 inspection
EQUIPMENT:
Garmin GMA 340
Garmin GMS 530
Garmin GNS 430
Garmin GTX 330
Garmin GTX 327
Avidyne FlightMax Ex500
DESCRIPTION OF DAMAGES:
Damage to belly skin, inboard and outboard flaps, one propeller, gear doors, landing gear
The damage noted during our survey lists as follows:
The ventral fin sustained damage
The left and right tail strakes are damaged
The tail stinger/cone with nav lamp assembly is damaged
There is an indentation in the aft fuselage belly within the pressure bulkhead
There are several belly skins near the cabin entrance door on the aircraft’s belly that were abraded from sliding on the runway
The left and right inboard and outboard flaps are damaged
The left propeller has dirt on its blades but does not appear to have hit the ground. The propeller may require inspection to verify that it was not damaged
There is minor damage to two blades of the right propeller
Due to the right propeller strike, the power section from the right-side Pratt and Whitney PT6A-21 series engine will require a tear down inspection
The nose and main gear doors may require replacement or repair pending further inspection
The nose wheel and tire assembly appear damaged
The trailing edge of the left and right inboard wings are damaged from the recovery lifting straps
The inboard leading edge of the horizontal stabilator’s left and right side is damaged
The main landing gear and nose landing gear components are damaged
There is possible spar damage to the wing’s center section
LOCATION OF AIRCRAFT: Tac Air, Knoxville TN
SALVAGE MAY BE INSPECTED BY CONTACTING: Jim Cohrs (770) 570-7473
REMARKS: Aircraft logbook entry 11/21/20019: Installed Raisebeck Quiet Turbo Fan Propeller System per STC SA3593NM issued Sept 12, 1986 and NTO letter dated Sept 28, 2009 for majicam installation without Autofeather system.
NOTE: A backhoe was used to lift straps that were placed around the wing roots from front to aft. The straps cut into the left and right wing roots and the left and right side of the horizontal was pushed in due to strap pressure. They also pulled the aircraft by its nose gear by placing the nose wheel into the bucket of the backhoe and pulling it.