19980806028699A

Accident · Substantial damage

FAA accident report · Beech D95A · Albuquerque, NM · August 6, 1998

Date
August 6, 1998 · 18:30 local
Place
Albuquerque, NM
Airport
Double Eagle II Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N924JL
NTSB investigation
NTSBFTW98LA375
Reported as
Beech D95A
Reported engine
Lycoming IO360B1B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
19,000 total15 in this make and model15 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.

(There were no remarks indicated prior to .4 entry) (from .4) the pilot reported that he was landing on runway 22, and during landing roll, the airplane pitched forward and to the right. He said that the airplane exited the runway to the right and came to rest facing the opposite direction. Postaccident examination of the landing gear system revealed no mechanical anomalies which would have precluded normal operation. The right main inner gear door exhibited crushing and inward deformation. A representative from Beechcraft stated that when the landing gear is down and locked, the inner gear doors are up and locked (flush with the bottom of the airplane). He further stated that the landing gear handle and the flap handle in this airplane are reverse from the majority of general aviation aircraft. The pilot reported that he purchased the airplane on July 30, 1998, 7 days before the accident. He further indicated on his ntsb's pilot/operator aircraft accident report that he had a total of 15 hours of flight experience in N924JL. (-23) on 08/06/98, at approximately 2000 MDT, N924JL, a Beechcraft traveler, upon rollout on runway 22 at aeg experienced nose gear failure. The airc raft exited the runway and came to rest 180 degrees in the opposite direction on the grasss parallel to the runway. No injuries.

As the FAA filed it

(THERE WERE NO REMARKS INDICATED PRIOR TO .4 ENTRY) (FROM .4) THE PILOT REPORTED THAT HE WAS LANDING ON RUNWAY 22, AND DURING LANDING ROLL, THE AIRPLANE PITCHED FORWARD AND TO THE RIGHT. HE SAID THAT THE AIRPLANE EXITED THE RUNWAY TO THE RIGHT AND CAME TO REST FACING THE OPPOSITE DIRECTION. POSTACCIDENT EXAMINATION OF THE LANDING GEAR SYSTEM REVEALED NO MECHANICAL ANOMALIES WHICH WOULD HAVE PRECLUDED NORMAL OPERATION. THE RIGHT MAIN INNER GEAR DOOR EXHIBITED CRUSHING AND INWARD DEFORMATION. A REPRESENTATIVE FROM BEECHCRAFT STATED THAT WHEN THE LANDING GEAR IS DOWN AND LOCKED, THE INNER GEAR DOORS ARE UP AND LOCKED (FLUSH WITH THE BOTTOM OF THE AIRPLANE). HE FURTHER STATED THAT THE LANDING GEAR HANDLE AND THE FLAP HANDLE IN THIS AIRPLANE ARE REVERSE FROM THE MAJORITY OF GENERAL AVIATION AIRCRAFT. THE PILOT REPORTED THAT HE PURCHASED THE AIRPLANE ON JULY 30, 1998, 7 DAYS BEFORE THE ACCIDENT. HE FURTHER INDICATED ON HIS NTSB'S PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT THAT HE HAD A TOTAL OF 15 HOURS OF FLIGHT EXPERIENCE IN N924JL. (-23) ON 08/06/98, AT APPROXIMATELY 2000 MDT, N924JL, A BEECHCRAFT TRAVELER, UPON ROLLOUT ON RUNWAY 22 AT AEG EXPERIENCED NOSE GEAR FAILURE. THE AIRC RAFT EXITED THE RUNWAY AND CAME TO REST 180 DEGREES IN THE OPPOSITE DIRECTION ON THE GRASSS PARALLEL TO THE RUNWAY. NO INJURIES.

NTSB investigation

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