NTSB Identification: FTW81FPA12
14 CFR Part 91 General Aviation
Aircraft: CESSNA A188B, registration: N9295R----------------------------------------------------------------------------------------------------------------------------
FILE DATE LOCATION AIRCRAFT DATA INJURIES FLIGHT PILOT DATA
F S M/N PURPOSE
----------------------------------------------------------------------------------------------------------------------------
3-1028 81/5/7 CELINA,TX CESSNA A188B CR- 0 1 0 COMMERCIAL COMMERCIAL, AGE 41, 17000
TIME - 0700 N9295R PX- 0 0 0 AERIAL APPLICATION TOTAL HOURS, 700 IN TYPE,
DAMAGE-SUBSTANTIAL OT- 0 0 0 NOT INSTRUMENT RATED.
DEPARTURE POINT INTENDED DESTINATION
DENTON,TX LOCAL
TYPE OF ACCIDENT PHASE OF OPERATION
ENGINE FAILURE OR MALFUNCTION IN FLIGHT: PROCEDURE TURNAROUND
COLLISION WITH GROUND/WATER: CONTROLLED LANDING: LEVEL OFF/TOUCHDOWN
PROBABLE CAUSE(S)
POWERPLANT - ENGINE STRUCTURE: MASTER AND CONNECTING RODS
MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON LAND
SPECIAL DATA
TOTAL HOURS IN CROP CONTROL - UNKNOWN/NOT REPORTED KIND OF OPERATION - SPRAYING CROPS
KIND OF CROP - UNKNOWN/NOT REPORTED TYPE OF CHEMICAL USED - LIQUID CHEMICAL-TOXIC
PILOT' S SEAT BELT -FASTENED-PROPERLY CRASH HELMET - AVAILABLE USED
COCKPIT CRASHPAD - INSTALLED TANK/HOPPER-LOCATION - FORWARD OF PILOT
TERRAIN-TYPE -LEVEL,FLAT ELEVATION-AREA BEING TREATED-FEET - 650
SWATH RUN-HOW FLOWN - CROSSWIND PROCEDURE TURNAROUND - FIRST 1/3 TURN
REMARKS- #5 CON ROD DRIVEN THROUGH CRANKCASE.
Index for May1981 | Index of months