20060322011999A

Accident · Substantial damage

FAA accident report · Lear 35LEAR · Philadelphia, PA · March 22, 2006

Date
March 22, 2006 · 01:55 local
Place
Philadelphia, PA
Airport
Philadelphia International
Phase of flight
To Aborted (Fixed Wing)
Operating rules
Air taxi and commuter (Part 135)
Operator
BKAA
Damage
Substantial damage
Aircraft
N58EM
NTSB investigation
NTSBNYC06LA081
Reported as
Lear 35LEAR
Reported engine
Garrett TFE73122B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
2,893 total1,267 in this make and model235 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) On March 22, 2006 a bankair, inc (bkaa), Learjet LR-35, N58EM, was cleared to depart runway 27L at Philadelphia International Airport (phl) to charolette (clt). The normal, before taxi, runup and inline checks were completed. According to crew statements and interviews, the aircraft was rolling down the runway, the pnf (SIC) called out a "fluctuation in N1." At this time the aircraft started to "yaw" to the left, the pnf confirmed that they were below V1 and called for an abort (SIC stated that the a/c was under 100 knts). During this time the pf (PIC) was trying to maintain directional control. As the call for abort was made, the pf, retarded the throttles to flight idle and deployed the spoilers. The aircraft was realigned on the runway centerline, but then again yawed to the left, at this time directional control was completely lost and the aircraft began to skid and rotate 180 degrees opposite of the runway heading. The aircraft stopped off the south side of runway 27L approximately 180 degrees in the opposite direction of the departure runway. Engines, anti-skid, nosewheel steering, gear and brake systems removed for testing (honeywell/bombardier). Drag chute was never deployed. (-23 amendment) this is part of the preflight and oral (before take off) briefing. The drag chute handle is large and located on the left side of the power quadrant, but this was also missed. Retraining has been conducted for both pilots. Counseling has been requested. The counseling was conducted by the poi. This company has also incorporated printed advisories, on each of the five aircraft that are equipped with drag chutes, advising the crew that the aircraft they are flying does in fact have an operational drag chute. This advisory is located on the dispatch "can" for each aircraft. This matter is closed.

As the FAA filed it

(-23) ON MARCH 22, 2006 A BANKAIR, INC (BKAA), LEARJET LR-35, N58EM, WAS CLEARED TO DEPART RUNWAY 27L AT PHILADELPHIA INTERNATIONAL AIRPORT (PHL) TO CHAROLETTE (CLT). THE NORMAL, BEFORE TAXI, RUNUP AND INLINE CHECKS WERE COMPLETED. ACCORDING TO CREW STATEMENTS AND INTERVIEWS, THE AIRCRAFT WAS ROLLING DOWN THE RUNWAY, THE PNF (SIC) CALLED OUT A "FLUCTUATION IN N1." AT THIS TIME THE AIRCRAFT STARTED TO "YAW" TO THE LEFT, THE PNF CONFIRMED THAT THEY WERE BELOW V1 AND CALLED FOR AN ABORT (SIC STATED THAT THE A/C WAS UNDER 100 KNTS). DURING THIS TIME THE PF (PIC) WAS TRYING TO MAINTAIN DIRECTIONAL CONTROL. AS THE CALL FOR ABORT WAS MADE, THE PF, RETARDED THE THROTTLES TO FLIGHT IDLE AND DEPLOYED THE SPOILERS. THE AIRCRAFT WAS REALIGNED ON THE RUNWAY CENTERLINE, BUT THEN AGAIN YAWED TO THE LEFT, AT THIS TIME DIRECTIONAL CONTROL WAS COMPLETELY LOST AND THE AIRCRAFT BEGAN TO SKID AND ROTATE 180 DEGREES OPPOSITE OF THE RUNWAY HEADING. THE AIRCRAFT STOPPED OFF THE SOUTH SIDE OF RUNWAY 27L APPROXIMATELY 180 DEGREES IN THE OPPOSITE DIRECTION OF THE DEPARTURE RUNWAY. ENGINES, ANTI-SKID, NOSEWHEEL STEERING, GEAR AND BRAKE SYSTEMS REMOVED FOR TESTING (HONEYWELL/BOMBARDIER). DRAG CHUTE WAS NEVER DEPLOYED. (-23 AMENDMENT) THIS IS PART OF THE PREFLIGHT AND ORAL (BEFORE TAKE OFF) BRIEFING. THE DRAG CHUTE HANDLE IS LARGE AND LOCATED ON THE LEFT SIDE OF THE POWER QUADRANT, BUT THIS WAS ALSO MISSED. RETRAINING HAS BEEN CONDUCTED FOR BOTH PILOTS. COUNSELING HAS BEEN REQUESTED. THE COUNSELING WAS CONDUCTED BY THE POI. THIS COMPANY HAS ALSO INCORPORATED PRINTED ADVISORIES, ON EACH OF THE FIVE AIRCRAFT THAT ARE EQUIPPED WITH DRAG CHUTES, ADVISING THE CREW THAT THE AIRCRAFT THEY ARE FLYING DOES IN FACT HAVE AN OPERATIONAL DRAG CHUTE. THIS ADVISORY IS LOCATED ON THE DISPATCH "CAN" FOR EACH AIRCRAFT. THIS MATTER IS CLOSED.

NTSB investigation

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