19991216037679A

Accident · Substantial damage

FAA accident report · Piper PA-31T1 · Santa Fe, NM · December 16, 1999

Date
December 16, 1999 · 15:15 local
Place
Santa Fe, NM
Airport
Santa Fe County Municipal Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N919RD
NTSB investigation
NTSBDEN00LA030
Reported as
Piper PA31T1
Reported engine
Pratt & Whitney PT6A11
Fatal injuries
0
Pilot’s flight hours
1,098 total401 in this make and model24 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.

(.19) On December 16, 1999, at 1515 mountain standard time, a Piper PA-31T1, N919RD, impacted terrain during initial climb following takeoff from Santa Fe, new Mexico, after a partial power loss. The private pilot and his two passengers received minor injuries and the aircraft sustained substantial damage. Visual meteorological conditions prevailed and no flight plan was filed for this local area flight operating under title 14 CFR part 91. (.4)on takeoff during the initiation of a cross-country flight, the pilot raised the landing gear following liftoff and the aircraft settled back onto the ground off the end of the runway. According to the pilot and the FAA inspector who examined the aircraft, both engines were producing normal power. The elevator trim was set at 12 degrees nose up vice 3-6 degrees required, and the aircraft was within weight and balance limits. The pilot lowered the landing gear prior to impact. According to information provided by the aircraft manufacturer, induced drag increases during landing gear retraction and extension due to the landing gear doors being extended into the air stream as the landing gear cycles. (-23)on December 16, 1999, at 1513 MST, a Piper PA-31T, N919RD, impacted terrain during initial climb following departure from runway 33 at Santa Fe municipal airport, Santa Fe, folllowing a reported power loss. The private pilot and sole occupant, received serious injuries and the aircraft incurred substantial damage. Visual meteorological conditions prevailed, an IFR lflight plan was filed for the proposed flight to johnson city, KS. The flight was being operated under title 14 CFR part 91.

As the FAA filed it

(.19) ON DECEMBER 16, 1999, AT 1515 MOUNTAIN STANDARD TIME, A PIPER PA-31T1, N919RD, IMPACTED TERRAIN DURING INITIAL CLIMB FOLLOWING TAKEOFF FROM SANTA FE, NEW MEXICO, AFTER A PARTIAL POWER LOSS. THE PRIVATE PILOT AND HIS TWO PASSENGERS RECEIVED MINOR INJURIES AND THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED FOR THIS LOCAL AREA FLIGHT OPERATING UNDER TITLE 14 CFR PART 91. (.4)ON TAKEOFF DURING THE INITIATION OF A CROSS-COUNTRY FLIGHT, THE PILOT RAISED THE LANDING GEAR FOLLOWING LIFTOFF AND THE AIRCRAFT SETTLED BACK ONTO THE GROUND OFF THE END OF THE RUNWAY. ACCORDING TO THE PILOT AND THE FAA INSPECTOR WHO EXAMINED THE AIRCRAFT, BOTH ENGINES WERE PRODUCING NORMAL POWER. THE ELEVATOR TRIM WAS SET AT 12 DEGREES NOSE UP VICE 3-6 DEGREES REQUIRED, AND THE AIRCRAFT WAS WITHIN WEIGHT AND BALANCE LIMITS. THE PILOT LOWERED THE LANDING GEAR PRIOR TO IMPACT. ACCORDING TO INFORMATION PROVIDED BY THE AIRCRAFT MANUFACTURER, INDUCED DRAG INCREASES DURING LANDING GEAR RETRACTION AND EXTENSION DUE TO THE LANDING GEAR DOORS BEING EXTENDED INTO THE AIR STREAM AS THE LANDING GEAR CYCLES. (-23)ON DECEMBER 16, 1999, AT 1513 MST, A PIPER PA-31T, N919RD, IMPACTED TERRAIN DURING INITIAL CLIMB FOLLOWING DEPARTURE FROM RUNWAY 33 AT SANTA FE MUNICIPAL AIRPORT, SANTA FE, FOLLLOWING A REPORTED POWER LOSS. THE PRIVATE PILOT AND SOLE OCCUPANT, RECEIVED SERIOUS INJURIES AND THE AIRCRAFT INCURRED SUBSTANTIAL DAMAGE. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AN IFR LFLIGHT PLAN WAS FILED FOR THE PROPOSED FLIGHT TO JOHNSON CITY, KS. THE FLIGHT WAS BEING OPERATED UNDER TITLE 14 CFR PART 91.

NTSB investigation

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