20160519024479I

Incident · Minor damage

FAA incident report · Beech E-90 · May 19, 2016

Date: May 19, 2016 · 14:35 local
Airport: Phoenix Deer Valley
Phase of flight: Landing: Touchdown
Operating rules: Pilot school (Part 141)
Damage: Minor damage
Aircraft: N26E
Reported as: Beech E-90
Reported engine: Pratt & Whitney PT6A series
People aboard: 3
Fatal injuries: 0
Other injuries: 0
Pilot’s certificates: Airline transport, flight instructor
Pilot’s flight hours: 3,400 total

N26ERegistered now · Beech E-90S/N LW-62 Airframe modelBeech E-90 Engine modelPratt & Whitney PT6A seriesTurbo-prop

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 was landing with student pilot at controls. The CFI aboard stated that after touchdown on rwy 25R he noted the student was using excessive braking and instructed him to ?engage reverse? And ?reduce braking pressure?. At that time the aircraft the left side of the aircraft dropped several inches and the aircraft veered to the left approximately 20 degrees. The CFI issued the command ?my controls? And applied right rudder input. As full right rudder input was applied the aircraft left the paved runway area and entered midfield. As the CFI continued to manipulate the controls the aircraft straightened out and came to a complete stop.

Aircraft had no visible damage other than a blown left tire. No one on board received injuries during the landing.

As the FAA filed it

AIRCRAFT WAS LANDING WITH STUDENT PILOT AT CONTROLS. THE CFI ABOARD STATED THAT AFTER TOUCHDOWN ON RWY 25R HE NOTED THE STUDENT WAS USING EXCESSIVE BRAKING AND INSTRUCTED HIM TO ?ENGAGE REVERSE? AND ?REDUCE BRAKING PRESSURE?. AT THAT TIME THE AIRCRAFT THE LEFT SIDE OF THE AIRCRAFT DROPPED SEVERAL INCHES AND THE AIRCRAFT VEERED TO THE LEFT APPROXIMATELY 20 DEGREES. THE CFI ISSUED THE COMMAND ?MY CONTROLS? AND APPLIED RIGHT RUDDER INPUT. AS FULL RIGHT RUDDER INPUT WAS APPLIED THE AIRCRAFT LEFT THE PAVED RUNWAY AREA AND ENTERED MIDFIELD. AS THE CFI CONTINUED TO MANIPULATE THE CONTROLS THE AIRCRAFT STRAIGHTENED OUT AND CAME TO A COMPLETE STOP.

AIRCRAFT HAD NO VISIBLE DAMAGE OTHER THAN A BLOWN LEFT TIRE. NO ONE ON BOARD RECEIVED INJURIES DURING THE LANDING.