20130816016519I

Incident · No damage

FAA incident report · Pacific Aerospace 750XL · Tecumseh, MI · August 16, 2013

Date
August 16, 2013 · 17:00 local
Place
Tecumseh, MI
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N750UP
Reported as
Pacific Aerospace 750XL
Reported engine
Pratt & Whitney Canada PT6A-34
People aboard
0
Fatal injuries
0
Other injuries
1

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.

Aircraft departed 3TE, Tecumseh, MI approx. 1700 local. With a load of 14 skydivers, approximately 400 lbs. Of fuel. This was the 10th flight of the day. At approximately 1900 ft. AGL, the engine made a couple of ?surges? Then the power rolled back to idle. The pilot ordered the able jumpers to exit. He cycled the power lever with no results, and then feathered the propeller.

5 Single jumpers were able to exit. The remaining were tandem jumpers, and the altitude was too low for them to exit. The jump instructors told them exiting jumpers to ?exit on reserve?. One jump instructor stated that one of the single jumpers deployed his main chute, had sniveling line twists?, then his aad fired and the reserve chute deployed. He descended under two canopies, in a downplane, into the trees. He sustained back injuries and was medevac?d from the scene. This was his 3rd jump of the day. He is a student jumper with only 12 total jumps.

After the jumpers exited, it was determined that the engine was at 50% ng. He executed precautionary engine restart procedures (igniters, fuel pump, and fuel valve on), unfeathered the prop, and unsecured the emergency power lever and looked for a suitable landing field. The emergency power was able to maintain approximately 500 ft. AGL. He flew approx. 1 mile to a private strip, paved strip and made an uneventful landing.

After landing engine runs confirmed the faults. Fuel quantity and visually verified by the pilot and airfield owner. Iic confirmed a fuel load of approximately 328 lbs. On 8/20/2013

The fuel control unit and fuel pump intermediate drive shaft were replaced on aug. 22 2013. Repair facility was contacted for a copy the fcu tear down report.

The injured jumper?s main chute was a solo 230; reserve chute was a smart 220.

As the FAA filed it

AIRCRAFT DEPARTED 3TE, TECUMSEH, MI APPROX. 1700 LOCAL. WITH A LOAD OF 14 SKYDIVERS, APPROXIMATELY 400 LBS. OF FUEL. THIS WAS THE 10TH FLIGHT OF THE DAY. AT APPROXIMATELY 1900 FT. AGL, THE ENGINE MADE A COUPLE OF ?SURGES? THEN THE POWER ROLLED BACK TO IDLE. THE PILOT ORDERED THE ABLE JUMPERS TO EXIT. HE CYCLED THE POWER LEVER WITH NO RESULTS, AND THEN FEATHERED THE PROPELLER.

5 SINGLE JUMPERS WERE ABLE TO EXIT. THE REMAINING WERE TANDEM JUMPERS, AND THE ALTITUDE WAS TOO LOW FOR THEM TO EXIT. THE JUMP INSTRUCTORS TOLD THEM EXITING JUMPERS TO ?EXIT ON RESERVE?. ONE JUMP INSTRUCTOR STATED THAT ONE OF THE SINGLE JUMPERS DEPLOYED HIS MAIN CHUTE, HAD SNIVELING LINE TWISTS?, THEN HIS AAD FIRED AND THE RESERVE CHUTE DEPLOYED. HE DESCENDED UNDER TWO CANOPIES, IN A DOWNPLANE, INTO THE TREES. HE SUSTAINED BACK INJURIES AND WAS MEDEVAC?D FROM THE SCENE. THIS WAS HIS 3RD JUMP OF THE DAY. HE IS A STUDENT JUMPER WITH ONLY 12 TOTAL JUMPS.

AFTER THE JUMPERS EXITED, IT WAS DETERMINED THAT THE ENGINE WAS AT 50% NG. HE EXECUTED PRECAUTIONARY ENGINE RESTART PROCEDURES (IGNITERS, FUEL PUMP, AND FUEL VALVE ON), UNFEATHERED THE PROP, AND UNSECURED THE EMERGENCY POWER LEVER AND LOOKED FOR A SUITABLE LANDING FIELD. THE EMERGENCY POWER WAS ABLE TO MAINTAIN APPROXIMATELY 500 FT. AGL. HE FLEW APPROX. 1 MILE TO A PRIVATE STRIP, PAVED STRIP AND MADE AN UNEVENTFUL LANDING.

AFTER LANDING ENGINE RUNS CONFIRMED THE FAULTS. FUEL QUANTITY AND VISUALLY VERIFIED BY THE PILOT AND AIRFIELD OWNER. IIC CONFIRMED A FUEL LOAD OF APPROXIMATELY 328 LBS. ON 8/20/2013

THE FUEL CONTROL UNIT AND FUEL PUMP INTERMEDIATE DRIVE SHAFT WERE REPLACED ON AUG. 22 2013. REPAIR FACILITY WAS CONTACTED FOR A COPY THE FCU TEAR DOWN REPORT.

THE INJURED JUMPER?S MAIN CHUTE WAS A SOLO 230; RESERVE CHUTE WAS A SMART 220.

Other reports on N750UP · 1

Matched to the same aircraft by N-number and date.