20130508006669I

Incident · Substantial damage

FAA incident report · David C Morris RV-8 · Chandler, AZ · May 8, 2013

Date
May 8, 2013 · 13:55 local
Place
Chandler, AZ
Airport
Chandler Municipal
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N96DM
Reported as
David C Morris RV-8
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
24,687 total12 in this make and model12 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.

Following takeoff, pilot proceeded on runway heading until approximately 1 mile south of the runway when the tower cleared the pilot to turn left. As the pilot turned left, he increased his climb speed to approximately 150 mph. During the climb at approximately 2800 MSL, the pilot noted both dynon D100 and D180 screens illuminate with a ?caution canopy unlocked? Warning. Pilot then reached for the canopy lever but failed to reach it before the canopy tore off the aircraft.

Pilot lost his headset and eyeglasses due to the wind. Pilot also experienced a cut on his ear, a knot on the side of his head and felt ?dazed?. Pilot proceeded to verify the aircraft flight controls were ok but noted he had no communications due to the loss of his headset. In addition, the pilot could not see the instruments and was having vision problems due to his glasses being blown off.

Pilot then proceeded to land back at chd with no further events taking place.

Inspectors from the scottsdale FSDO reviewed the aircraft records, pilots written statement, inspected the aircraft and the detached canopy. The inspection included operationally checking the canopy locked/unlocked indicating system which appeared to functioning correctly. It was noted that several of the jam nuts on the canopy lock pins were loose. Pilot stated that these were tight before the flight. No damage on the airframe side of the canopy locking systems was noted (signs of lock pins tearing through or gouging, etc). No further discrepancies were noted with the canopy locking system.

As the FAA filed it

FOLLOWING TAKEOFF, PILOT PROCEEDED ON RUNWAY HEADING UNTIL APPROXIMATELY 1 MILE SOUTH OF THE RUNWAY WHEN THE TOWER CLEARED THE PILOT TO TURN LEFT. AS THE PILOT TURNED LEFT, HE INCREASED HIS CLIMB SPEED TO APPROXIMATELY 150 MPH. DURING THE CLIMB AT APPROXIMATELY 2800 MSL, THE PILOT NOTED BOTH DYNON D100 AND D180 SCREENS ILLUMINATE WITH A ?CAUTION CANOPY UNLOCKED? WARNING. PILOT THEN REACHED FOR THE CANOPY LEVER BUT FAILED TO REACH IT BEFORE THE CANOPY TORE OFF THE AIRCRAFT.

PILOT LOST HIS HEADSET AND EYEGLASSES DUE TO THE WIND. PILOT ALSO EXPERIENCED A CUT ON HIS EAR, A KNOT ON THE SIDE OF HIS HEAD AND FELT ?DAZED?. PILOT PROCEEDED TO VERIFY THE AIRCRAFT FLIGHT CONTROLS WERE OK BUT NOTED HE HAD NO COMMUNICATIONS DUE TO THE LOSS OF HIS HEADSET. IN ADDITION, THE PILOT COULD NOT SEE THE INSTRUMENTS AND WAS HAVING VISION PROBLEMS DUE TO HIS GLASSES BEING BLOWN OFF.

PILOT THEN PROCEEDED TO LAND BACK AT CHD WITH NO FURTHER EVENTS TAKING PLACE.

INSPECTORS FROM THE SCOTTSDALE FSDO REVIEWED THE AIRCRAFT RECORDS, PILOTS WRITTEN STATEMENT, INSPECTED THE AIRCRAFT AND THE DETACHED CANOPY. THE INSPECTION INCLUDED OPERATIONALLY CHECKING THE CANOPY LOCKED/UNLOCKED INDICATING SYSTEM WHICH APPEARED TO FUNCTIONING CORRECTLY. IT WAS NOTED THAT SEVERAL OF THE JAM NUTS ON THE CANOPY LOCK PINS WERE LOOSE. PILOT STATED THAT THESE WERE TIGHT BEFORE THE FLIGHT. NO DAMAGE ON THE AIRFRAME SIDE OF THE CANOPY LOCKING SYSTEMS WAS NOTED (SIGNS OF LOCK PINS TEARING THROUGH OR GOUGING, ETC). NO FURTHER DISCREPANCIES WERE NOTED WITH THE CANOPY LOCKING SYSTEM.