20060430009519A

Accident · Substantial damage

FAA accident report · Piper PA-44-180 · Phoenix, AZ · April 30, 2006

Date
April 30, 2006 · 08:50 local
Place
Phoenix, AZ
Airport
Phoenix-Deer Valley Municipal Airport
Phase of flight
Sfl Final Approach
Operating rules
General operating rules (Part 91)
Operator
FQAS
Damage
Substantial damage
Aircraft
N449PA
NTSB investigation
NTSBLAX06CA152
Reported as
Piper PA44180
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,091 total191 in this make and model177 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.

(-23) Instructor simulated right engine failure inside final approach fix. Instructor believes he simulated engine failure via retarding throttle on right engine. During simulated single engine landing the student bounced the aircraft. Following bounce the instructor instructed the student to go around. When throttles were advanced for both engines the right engine failed as climb was established resulting in the aircraft rolling and turning to the right. As directional control was being lost the instructor took over controls, reduced power, and righted the aircraft prior to impact. Aircraft crossed the infield and taxiway then came to rest on parking ramp. When aircraft recovery was initiated by mechanic he noted that the left fuel selector was on and the right fuel selector was off. Neither the instructor nor student remembers turning fuel selector off until after the aircraft had crashed. Aircraft received substantial damage consisting of bent right wing, collapsed nose gear, blown left main tire, right prop strike and wrinkling of both sides of the fuselage from the nose to just aft of the pilot seats. During subsequent inspection of the fuel system it was noted that there was no fuel in the right carburetor float bowl nor anywhere else in the fuel system outboard of the fuel selector valve for the right engine. When the fuel system was reconnected and the right fuel selector turned on, the right engine started and idled normally.

As the FAA filed it

(-23) INSTRUCTOR SIMULATED RIGHT ENGINE FAILURE INSIDE FINAL APPROACH FIX. INSTRUCTOR BELIEVES HE SIMULATED ENGINE FAILURE VIA RETARDING THROTTLE ON RIGHT ENGINE. DURING SIMULATED SINGLE ENGINE LANDING THE STUDENT BOUNCED THE AIRCRAFT. FOLLOWING BOUNCE THE INSTRUCTOR INSTRUCTED THE STUDENT TO GO AROUND. WHEN THROTTLES WERE ADVANCED FOR BOTH ENGINES THE RIGHT ENGINE FAILED AS CLIMB WAS ESTABLISHED RESULTING IN THE AIRCRAFT ROLLING AND TURNING TO THE RIGHT. AS DIRECTIONAL CONTROL WAS BEING LOST THE INSTRUCTOR TOOK OVER CONTROLS, REDUCED POWER, AND RIGHTED THE AIRCRAFT PRIOR TO IMPACT. AIRCRAFT CROSSED THE INFIELD AND TAXIWAY THEN CAME TO REST ON PARKING RAMP. WHEN AIRCRAFT RECOVERY WAS INITIATED BY MECHANIC HE NOTED THAT THE LEFT FUEL SELECTOR WAS ON AND THE RIGHT FUEL SELECTOR WAS OFF. NEITHER THE INSTRUCTOR NOR STUDENT REMEMBERS TURNING FUEL SELECTOR OFF UNTIL AFTER THE AIRCRAFT HAD CRASHED. AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE CONSISTING OF BENT RIGHT WING, COLLAPSED NOSE GEAR, BLOWN LEFT MAIN TIRE, RIGHT PROP STRIKE AND WRINKLING OF BOTH SIDES OF THE FUSELAGE FROM THE NOSE TO JUST AFT OF THE PILOT SEATS. DURING SUBSEQUENT INSPECTION OF THE FUEL SYSTEM IT WAS NOTED THAT THERE WAS NO FUEL IN THE RIGHT CARBURETOR FLOAT BOWL NOR ANYWHERE ELSE IN THE FUEL SYSTEM OUTBOARD OF THE FUEL SELECTOR VALVE FOR THE RIGHT ENGINE. WHEN THE FUEL SYSTEM WAS RECONNECTED AND THE RIGHT FUEL SELECTOR TURNED ON, THE RIGHT ENGINE STARTED AND IDLED NORMALLY.

NTSB investigation

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

Other reports on N449PA · 2

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