20151109020859A

Accident · Destroyed

FAA accident report · Cirrus Design SR22 · Colorado Spring, CO · November 9, 2015

Date
November 9, 2015 · 10:51 local
Place
Colorado Spring, CO
Airport
City Of Colorado Springs Municipal
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N752C
NTSB investigation
NTSBCEN16FA034
Reported as
Cirrus Design SR22
Reported engine
Continental IO-550 series
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
2,900 total

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.

After declaring engine problems and twice communicating a desire to turn around on tower frequency, a 2002 Cirrus SR22 single-engine, constant-speed-propeller aircraft crashed approximately one minute after being cleared for takeoff from approximately the midpoint of Colorado Springs, CO. Airport runway 35L (taxiway A36,400 from the runway end). After climbing to approximately 200 to 300 feet above the ground, the aircraft pitched nose-down to the left, entered a one-turn spin, crashed in a relatively-flat field in a nose and wings-level attitude, and burned almost completely approximately 2500 north of the takeoff- runway end and 700' west of the extended centerline of runway 35L. There were two fatalities: the pilot and one passenger. The destination (not-filed) was "southeast," probably roanoke, TX, the home base of the aircraft. The last normal tower control clearance was "turn right heading 060." An eyewitness indicated that the engine revved and backed off for 5 to 6 cycles between liftoff and pitch-up, and that he did not remember any engine sound after observing the aircraft break off to the left. Another witness indicated the aircraft consumed more runway during takeoff than usual and that flaps were deployed (investigation of the crash produced evidence that the flaps were at 50%, which can be considered normal for this aircraft, but which would have made recovery from an uncommanded, low-level power loss more difficult). A surface tailwind of 5KTS existed at the time. A short connector taxiway was used from the parking ramp which offered little room for an engine runup. Approximately 2.5 minutes elapsed between acknowledgement of the taxi clearance on the ramp and clearance for takeoff. Witnesses testified that the aircraft had been topped-off with an appropriate grade of aviation gasoline upon its arrival two days prior, and offered the observation that the pilot did not seem agitated or in a particular hurry to depart. The airman and aircraft logs burned in the aircraft, but enough pages survived to disclose that the pilot had approximately 2,900 total hours.

As the FAA filed it

AFTER DECLARING ENGINE PROBLEMS AND TWICE COMMUNICATING A DESIRE TO TURN AROUND ON TOWER FREQUENCY, A 2002 CIRRUS SR22 SINGLE-ENGINE, CONSTANT-SPEED-PROPELLER AIRCRAFT CRASHED APPROXIMATELY ONE MINUTE AFTER BEING CLEARED FOR TAKEOFF FROM APPROXIMATELY THE MIDPOINT OF COLORADO SPRINGS, CO. AIRPORT RUNWAY 35L (TAXIWAY A36,400 FROM THE RUNWAY END). AFTER CLIMBING TO APPROXIMATELY 200 TO 300 FEET ABOVE THE GROUND, THE AIRCRAFT PITCHED NOSE-DOWN TO THE LEFT, ENTERED A ONE-TURN SPIN, CRASHED IN A RELATIVELY-FLAT FIELD IN A NOSE AND WINGS-LEVEL ATTITUDE, AND BURNED ALMOST COMPLETELY APPROXIMATELY 2500 NORTH OF THE TAKEOFF- RUNWAY END AND 700' WEST OF THE EXTENDED CENTERLINE OF RUNWAY 35L. THERE WERE TWO FATALITIES: THE PILOT AND ONE PASSENGER. THE DESTINATION (NOT-FILED) WAS "SOUTHEAST," PROBABLY ROANOKE, TX, THE HOME BASE OF THE AIRCRAFT. THE LAST NORMAL TOWER CONTROL CLEARANCE WAS "TURN RIGHT HEADING 060." AN EYEWITNESS INDICATED THAT THE ENGINE REVVED AND BACKED OFF FOR 5 TO 6 CYCLES BETWEEN LIFTOFF AND PITCH-UP, AND THAT HE DID NOT REMEMBER ANY ENGINE SOUND AFTER OBSERVING THE AIRCRAFT BREAK OFF TO THE LEFT. ANOTHER WITNESS INDICATED THE AIRCRAFT CONSUMED MORE RUNWAY DURING TAKEOFF THAN USUAL AND THAT FLAPS WERE DEPLOYED (INVESTIGATION OF THE CRASH PRODUCED EVIDENCE THAT THE FLAPS WERE AT 50%, WHICH CAN BE CONSIDERED NORMAL FOR THIS AIRCRAFT, BUT WHICH WOULD HAVE MADE RECOVERY FROM AN UNCOMMANDED, LOW-LEVEL POWER LOSS MORE DIFFICULT). A SURFACE TAILWIND OF 5KTS EXISTED AT THE TIME. A SHORT CONNECTOR TAXIWAY WAS USED FROM THE PARKING RAMP WHICH OFFERED LITTLE ROOM FOR AN ENGINE RUNUP. APPROXIMATELY 2.5 MINUTES ELAPSED BETWEEN ACKNOWLEDGEMENT OF THE TAXI CLEARANCE ON THE RAMP AND CLEARANCE FOR TAKEOFF. WITNESSES TESTIFIED THAT THE AIRCRAFT HAD BEEN TOPPED-OFF WITH AN APPROPRIATE GRADE OF AVIATION GASOLINE UPON ITS ARRIVAL TWO DAYS PRIOR, AND OFFERED THE OBSERVATION THAT THE PILOT DID NOT SEEM AGITATED OR IN A PARTICULAR HURRY TO DEPART. THE AIRMAN AND AIRCRAFT LOGS BURNED IN THE AIRCRAFT, BUT ENOUGH PAGES SURVIVED TO DISCLOSE THAT THE PILOT HAD APPROXIMATELY 2,900 TOTAL HOURS.

NTSB investigation

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