19960124000889A

Accident · Substantial damage

FAA accident report · AMD FALCON10 · Detroit, MI · January 24, 1996

Date
January 24, 1996 · 10:18 local
Place
Detroit, MI
Airport
Detroit Metro Wayne County
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N191MC
NTSB investigation
NTSBCHI96LA082
Reported as
AMD FALCON10
Reported engine
Garrett TFE73121C
People aboard
8
Fatal injuries
0
Pilot’s flight hours
11,163 total1,330 in this make and model78 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.

Aircraft came in with possible landing gear problems, aircraft did a fly by then landed runway, gear collapsed. (.4)the pilot reported getting an unsafe indication on the right main landing gear when the landing gear was lowered. The crew recycled the landing gear and got the same unsafe indication. The crew retracted the gear and diverted to Detroit. On arrival, the crew performed the 'landing gear abnormal extension checklist,' but the unsafe indication remained. The air traffic control tower reported that the gear appeared normal. During the landing, the right main landing gear retracted. The airplane slid sideways, striking a runway marker as it departed the runway, and came to rest in a field. Examination revealed that the right landing gear downlock mechanism could be overcome with physical force. Examination of the right landing gear actuator revealed that one of the six shims which separate the spacers and help guide the safety lock switch was out of position and lying on top of the lock assembly. (-23) the aircraft was diverted to Detroit metro airport (dtw) due to an un safe right landing gear (red) light. The aircraft touched down on runway 3R and the right landing gear collapsed at about 4800 feet from runway threshold. The aircraft skidded right and departed off the runway and struck the 5000 feet runway length marker with the left wing inboard slat. The aircraft continued to skid for about 700 feet and struck the runway visual range (RVR) equipment with the lower forward fuselage section and the cabin entry door. The aircraft came to rest on top of the RVR equipment.

As the FAA filed it

AIRCRAFT CAME IN WITH POSSIBLE LANDING GEAR PROBLEMS, AIRCRAFT DID A FLY BY THEN LANDED RUNWAY, GEAR COLLAPSED. (.4)THE PILOT REPORTED GETTING AN UNSAFE INDICATION ON THE RIGHT MAIN LANDING GEAR WHEN THE LANDING GEAR WAS LOWERED. THE CREW RECYCLED THE LANDING GEAR AND GOT THE SAME UNSAFE INDICATION. THE CREW RETRACTED THE GEAR AND DIVERTED TO DETROIT. ON ARRIVAL, THE CREW PERFORMED THE 'LANDING GEAR ABNORMAL EXTENSION CHECKLIST,' BUT THE UNSAFE INDICATION REMAINED. THE AIR TRAFFIC CONTROL TOWER REPORTED THAT THE GEAR APPEARED NORMAL. DURING THE LANDING, THE RIGHT MAIN LANDING GEAR RETRACTED. THE AIRPLANE SLID SIDEWAYS, STRIKING A RUNWAY MARKER AS IT DEPARTED THE RUNWAY, AND CAME TO REST IN A FIELD. EXAMINATION REVEALED THAT THE RIGHT LANDING GEAR DOWNLOCK MECHANISM COULD BE OVERCOME WITH PHYSICAL FORCE. EXAMINATION OF THE RIGHT LANDING GEAR ACTUATOR REVEALED THAT ONE OF THE SIX SHIMS WHICH SEPARATE THE SPACERS AND HELP GUIDE THE SAFETY LOCK SWITCH WAS OUT OF POSITION AND LYING ON TOP OF THE LOCK ASSEMBLY. (-23) THE AIRCRAFT WAS DIVERTED TO DETROIT METRO AIRPORT (DTW) DUE TO AN UN SAFE RIGHT LANDING GEAR (RED) LIGHT. THE AIRCRAFT TOUCHED DOWN ON RUNWAY 3R AND THE RIGHT LANDING GEAR COLLAPSED AT ABOUT 4800 FEET FROM RUNWAY THRESHOLD. THE AIRCRAFT SKIDDED RIGHT AND DEPARTED OFF THE RUNWAY AND STRUCK THE 5000 FEET RUNWAY LENGTH MARKER WITH THE LEFT WING INBOARD SLAT. THE AIRCRAFT CONTINUED TO SKID FOR ABOUT 700 FEET AND STRUCK THE RUNWAY VISUAL RANGE (RVR) EQUIPMENT WITH THE LOWER FORWARD FUSELAGE SECTION AND THE CABIN ENTRY DOOR. THE AIRCRAFT CAME TO REST ON TOP OF THE RVR EQUIPMENT.

NTSB investigation

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