19980702039009A

Accident · Substantial damage

FAA accident report · Cessna A150M · Langley, WA · July 2, 1998

Date
July 2, 1998 · 16:00 local
Place
Langley, WA
Airport
Whidbey Air Park Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8153V
NTSB investigation
NTSBSEA98LA116
Reported as
Cessna A150M
Reported engine
Continental O200A
Fatal injuries
0
Pilot’s flight hours
305 total19 in this make and model10 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.

(.4) The pilot reported that he had departed with full fuel tanks. The pilot stated that during the takeoff he noted a 'perceived lack of power.' The pilot reported two reasons for this, (1) he had been flying a larger aircraft with more power, and (2) he and his passenger were fairly heavy. The pilot flew to another airstrip and set up for a touch-and-go landing. The pilot stated that the approach was a little high and the landing was a little long. The pilot remembers adding power and retracting the flaps for the takeoff, but does not recall any events after this point. A witness reported that the aircraft was taking off when the nose of the airplane dropped and descended into the trees. Post-crash inspection of the airplane did not reveal evidence of a mechanical failure or malfunction. The weight and balance was calculated for the initial take off and for the take off from the second location. In both cases, the gross weight of the airplane was exceeded by approximately 55 pounds and 19 pounds respectively. During the on-site documentation, the carburetor hear was found partially on. (-23)pilot lost contorl after touch and go landing. Aircraft may have been at max gross weight. Carburetor heat may have been on.

As the FAA filed it

(.4) THE PILOT REPORTED THAT HE HAD DEPARTED WITH FULL FUEL TANKS. THE PILOT STATED THAT DURING THE TAKEOFF HE NOTED A 'PERCEIVED LACK OF POWER.' THE PILOT REPORTED TWO REASONS FOR THIS, (1) HE HAD BEEN FLYING A LARGER AIRCRAFT WITH MORE POWER, AND (2) HE AND HIS PASSENGER WERE FAIRLY HEAVY. THE PILOT FLEW TO ANOTHER AIRSTRIP AND SET UP FOR A TOUCH-AND-GO LANDING. THE PILOT STATED THAT THE APPROACH WAS A LITTLE HIGH AND THE LANDING WAS A LITTLE LONG. THE PILOT REMEMBERS ADDING POWER AND RETRACTING THE FLAPS FOR THE TAKEOFF, BUT DOES NOT RECALL ANY EVENTS AFTER THIS POINT. A WITNESS REPORTED THAT THE AIRCRAFT WAS TAKING OFF WHEN THE NOSE OF THE AIRPLANE DROPPED AND DESCENDED INTO THE TREES. POST-CRASH INSPECTION OF THE AIRPLANE DID NOT REVEAL EVIDENCE OF A MECHANICAL FAILURE OR MALFUNCTION. THE WEIGHT AND BALANCE WAS CALCULATED FOR THE INITIAL TAKE OFF AND FOR THE TAKE OFF FROM THE SECOND LOCATION. IN BOTH CASES, THE GROSS WEIGHT OF THE AIRPLANE WAS EXCEEDED BY APPROXIMATELY 55 POUNDS AND 19 POUNDS RESPECTIVELY. DURING THE ON-SITE DOCUMENTATION, THE CARBURETOR HEAR WAS FOUND PARTIALLY ON. (-23)PILOT LOST CONTORL AFTER TOUCH AND GO LANDING. AIRCRAFT MAY HAVE BEEN AT MAX GROSS WEIGHT. CARBURETOR HEAT MAY HAVE BEEN ON.

NTSB investigation

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