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|
Attributes | |
ACN | 796751 |
Time | |
Date | 200807 |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | msl single value : 585 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : zzz.tracon |
Operator | general aviation : personal |
Make Model Name | Other |
Operating Under FAR Part | Part 91 |
Flight Phase | climbout : initial ground : takeoff roll landing : roll |
Person 1 | |
Affiliation | other |
Function | flight crew : single pilot |
Qualification | pilot : private pilot : instrument |
Experience | flight time last 90 days : 3 flight time total : 4952 flight time type : 10 |
ASRS Report | 796751 |
Events | |
Anomaly | aircraft equipment problem : critical excursion : runway other anomaly |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : landed in emergency condition flight crew : regained aircraft control |
Consequence | other |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
After maintenance work on the propeller; I proceeded to test fly the sport cruiser to make sure the setting of full power on takeoff climb out would not exceed 6000 RPM redline. Using the sport cruiser flight checklist for the flight; I started the engine and completed the checklist in front of the hangar. I closed the canopy and locked the canopy with the tee-hand lock on the panel between seat backs. I called ZZZ ground control on 121.15 MHZ and requested to taxi to the active runway. ZZZ controller responded aircraft number to taxi on runway 17. I taxied to runway 17 hold line and changed to gpm tower frequency 128.55 MHZ. I called the tower and said I was ready for departure for a maintenance flight and would remain in the pattern. The tower controller responded for me to hold; as a helicopter was departing the area. I responded that I was holding for runway 17. After the helicopter cleared the area the tower controller announced I was 'cleared for departure; announce base leg.' as I accelerated to takeoff speed; I was monitoring the instruments and runway. I lifted off about 1200 ft down the runway and began a climb out about 80 KTS when the canopy started to open. I pulled the canopy down by the gas lift strut attachment and reduced power to attempt to land. I decided I would not be able to land with the altitude and remaining usable runway. I added some power and was in some difficulty trying to fly the aircraft and keep the canopy from going completely up with the gas lift struts pushing it up as well as the turbulence in the cockpit. I attempted to keep my speed to 80 KTS and control the airplane while holding down the canopy. I flew a close pattern and turned base holding about 80 KTS and reduced the power. On final; I touched down in the grass left of the runway centerline as a result of the control problems experienced while attempting to maintain control of the aircraft by holding the canopy down with the gas lift strut. The left main gear struck the runway identify sign as I returned to the runway. I continued on the runway to the east midfield taxiway and exited the runway. I then taxied to the maintenance hangar and shut down the engine. I checked the aircraft for damage. The left main wheel pant had some minor damage from the sign. The left flap had some small dents and scrapes on the underside. We are examining the canopy lock to determine why it failed. I inspected the aircraft for damage and determined as a certified mechanic that there was no structural damage or primary control damage to this aircraft. The problem was the canopy latch mechanism. Recommendation: a better canopy latch control mechanism.
Original NASA ASRS Text
Title: MAINT TEST FLT OF SPORT CRUISER LSA ENDS WITH LANDING OFF PAVED SURFACE WHEN CANOPY LOCKING MECHANISM FAILS WHICH COMPLICATES THE PLT'S TASK.
Narrative: AFTER MAINT WORK ON THE PROP; I PROCEEDED TO TEST FLY THE SPORT CRUISER TO MAKE SURE THE SETTING OF FULL PWR ON TKOF CLBOUT WOULD NOT EXCEED 6000 RPM REDLINE. USING THE SPORT CRUISER FLT CHKLIST FOR THE FLT; I STARTED THE ENG AND COMPLETED THE CHKLIST IN FRONT OF THE HANGAR. I CLOSED THE CANOPY AND LOCKED THE CANOPY WITH THE TEE-HAND LOCK ON THE PANEL BTWN SEAT BACKS. I CALLED ZZZ GND CTL ON 121.15 MHZ AND REQUESTED TO TAXI TO THE ACTIVE RWY. ZZZ CTLR RESPONDED ACFT NUMBER TO TAXI ON RWY 17. I TAXIED TO RWY 17 HOLD LINE AND CHANGED TO GPM TWR FREQ 128.55 MHZ. I CALLED THE TWR AND SAID I WAS READY FOR DEP FOR A MAINT FLT AND WOULD REMAIN IN THE PATTERN. THE TWR CTLR RESPONDED FOR ME TO HOLD; AS A HELI WAS DEPARTING THE AREA. I RESPONDED THAT I WAS HOLDING FOR RWY 17. AFTER THE HELI CLRED THE AREA THE TWR CTLR ANNOUNCED I WAS 'CLRED FOR DEP; ANNOUNCE BASE LEG.' AS I ACCELERATED TO TKOF SPD; I WAS MONITORING THE INSTS AND RWY. I LIFTED OFF ABOUT 1200 FT DOWN THE RWY AND BEGAN A CLBOUT ABOUT 80 KTS WHEN THE CANOPY STARTED TO OPEN. I PULLED THE CANOPY DOWN BY THE GAS LIFT STRUT ATTACHMENT AND REDUCED PWR TO ATTEMPT TO LAND. I DECIDED I WOULD NOT BE ABLE TO LAND WITH THE ALT AND REMAINING USABLE RWY. I ADDED SOME PWR AND WAS IN SOME DIFFICULTY TRYING TO FLY THE ACFT AND KEEP THE CANOPY FROM GOING COMPLETELY UP WITH THE GAS LIFT STRUTS PUSHING IT UP AS WELL AS THE TURB IN THE COCKPIT. I ATTEMPTED TO KEEP MY SPD TO 80 KTS AND CTL THE AIRPLANE WHILE HOLDING DOWN THE CANOPY. I FLEW A CLOSE PATTERN AND TURNED BASE HOLDING ABOUT 80 KTS AND REDUCED THE PWR. ON FINAL; I TOUCHED DOWN IN THE GRASS L OF THE RWY CTRLINE AS A RESULT OF THE CTL PROBS EXPERIENCED WHILE ATTEMPTING TO MAINTAIN CTL OF THE ACFT BY HOLDING THE CANOPY DOWN WITH THE GAS LIFT STRUT. THE L MAIN GEAR STRUCK THE RWY IDENT SIGN AS I RETURNED TO THE RWY. I CONTINUED ON THE RWY TO THE E MIDFIELD TXWY AND EXITED THE RWY. I THEN TAXIED TO THE MAINT HANGAR AND SHUT DOWN THE ENG. I CHKED THE ACFT FOR DAMAGE. THE L MAIN WHEEL PANT HAD SOME MINOR DAMAGE FROM THE SIGN. THE L FLAP HAD SOME SMALL DENTS AND SCRAPES ON THE UNDERSIDE. WE ARE EXAMINING THE CANOPY LOCK TO DETERMINE WHY IT FAILED. I INSPECTED THE ACFT FOR DAMAGE AND DETERMINED AS A CERTIFIED MECH THAT THERE WAS NO STRUCTURAL DAMAGE OR PRIMARY CTL DAMAGE TO THIS ACFT. THE PROB WAS THE CANOPY LATCH MECHANISM. RECOMMENDATION: A BETTER CANOPY LATCH CTL MECHANISM.
Data retrieved from NASA's ASRS site as of May 2009 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.