20200907016649A

Accident · Substantial damage

FAA accident report · Piper PA-32R-301T · Bonham, TX · September 7, 2020

Date
September 7, 2020 · 08:00 local
Place
Bonham, TX
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3576X
NTSB investigation
NTSBCEN20LA384
Reported as
Piper PA-32R-301T
Reported engine
Lycoming TI0-540
People aboard
2
Fatal injuries
0
Other injuries
0

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.

On September 7, 2020, at approximately 0800, N3576X departed jones field airport (foo- Bonham, Texas) in route to commerce municipal airport (2F7- commerce, Texas). During the climb out the pilot in command noticed a high turbine inlet temperature which was followed by high cylinder head temperature indication. Upon leveling off, all indications returned to normal but the pilot decided to return to jones field (F00) based on the high temperature indications (he was approximately 3 miles from jones field at this point). At approximately 1.5 to 2 miles from the field, the engine lost power and a field was chosen for an emergency landing. During the landing, the right hand main landing gear collapsed causing the nose, propeller, and right hand wing to contact the ground, causing the aircraft to skid to a stop.

The right hand wing tip lens was broken and there was a slight twist on the right wing leading edge just forward of the spar and out board of the over wing fuel filler port. The nose landing gear doors and the lower engine cowl were also damaged. All three propeller blades were ben backwards from the root.

Examination of the aircraft confirmed continuity of all flight and engine controls. During the engine examination, it was noted that the fuel injector line going to the number 6 cylinder had come undone. No damage was noted either on the line nor the fitting. The engine fuel supply was checked and upon running the boost pump with throttle and mixture control input, it was confirmed that fuel was available to the engine and that fuel was squirting out of the loose line.

Records review indicated that the last engine work performed was during the last 100 hour inspection which was performed on October 15, 2019 (tach: 425.6).

Last annual was performed October 15, 2019.

As the FAA filed it

ON SEPTEMBER 7, 2020, AT APPROXIMATELY 0800, N3576X DEPARTED JONES FIELD AIRPORT (FOO- BONHAM, TEXAS) IN ROUTE TO COMMERCE MUNICIPAL AIRPORT (2F7- COMMERCE, TEXAS). DURING THE CLIMB OUT THE PILOT IN COMMAND NOTICED A HIGH TURBINE INLET TEMPERATURE WHICH WAS FOLLOWED BY HIGH CYLINDER HEAD TEMPERATURE INDICATION. UPON LEVELING OFF, ALL INDICATIONS RETURNED TO NORMAL BUT THE PILOT DECIDED TO RETURN TO JONES FIELD (F00) BASED ON THE HIGH TEMPERATURE INDICATIONS (HE WAS APPROXIMATELY 3 MILES FROM JONES FIELD AT THIS POINT). AT APPROXIMATELY 1.5 TO 2 MILES FROM THE FIELD, THE ENGINE LOST POWER AND A FIELD WAS CHOSEN FOR AN EMERGENCY LANDING. DURING THE LANDING, THE RIGHT HAND MAIN LANDING GEAR COLLAPSED CAUSING THE NOSE, PROPELLER, AND RIGHT HAND WING TO CONTACT THE GROUND, CAUSING THE AIRCRAFT TO SKID TO A STOP.

THE RIGHT HAND WING TIP LENS WAS BROKEN AND THERE WAS A SLIGHT TWIST ON THE RIGHT WING LEADING EDGE JUST FORWARD OF THE SPAR AND OUT BOARD OF THE OVER WING FUEL FILLER PORT. THE NOSE LANDING GEAR DOORS AND THE LOWER ENGINE COWL WERE ALSO DAMAGED. ALL THREE PROPELLER BLADES WERE BEN BACKWARDS FROM THE ROOT.

EXAMINATION OF THE AIRCRAFT CONFIRMED CONTINUITY OF ALL FLIGHT AND ENGINE CONTROLS. DURING THE ENGINE EXAMINATION, IT WAS NOTED THAT THE FUEL INJECTOR LINE GOING TO THE NUMBER 6 CYLINDER HAD COME UNDONE. NO DAMAGE WAS NOTED EITHER ON THE LINE NOR THE FITTING. THE ENGINE FUEL SUPPLY WAS CHECKED AND UPON RUNNING THE BOOST PUMP WITH THROTTLE AND MIXTURE CONTROL INPUT, IT WAS CONFIRMED THAT FUEL WAS AVAILABLE TO THE ENGINE AND THAT FUEL WAS SQUIRTING OUT OF THE LOOSE LINE.

RECORDS REVIEW INDICATED THAT THE LAST ENGINE WORK PERFORMED WAS DURING THE LAST 100 HOUR INSPECTION WHICH WAS PERFORMED ON OCTOBER 15, 2019 (TACH: 425.6).

LAST ANNUAL WAS PERFORMED OCTOBER 15, 2019.

NTSB investigation

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