20031019026959I

Incident · Minor damage

FAA incident report · Piper PA-28R-200 · Wendover, UT · October 19, 2003

Date
October 19, 2003 · 19:15 local
Place
Wendover, UT
Airport
Wendover Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N15546
Reported as
Piper PA28R200
People aboard
4
Fatal injuries
0
Pilot’s flight hours
530 total145 in this make and model27 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) The pilot lined up with the runway on final approach. He was landing into the late afternoon sun. He put the landing gear handle in the gear down position, but did not get a gear down and locked light. The pilot thought that the landing gear had failed to extend. Three attempts were made to extend the gear with the gear down handle. All attempts failed to get a gear down and locked light. The pilot tried to extend the gear with the emergency gear down system. These attempts failed to get a gear down and locked light. The pilot may have failed to use the correct emergency gear extension procedures, to extend the gear. The aircraft landing gear was tested, and found to work normally. The gear was cycled 10 times and worked each time. The emergency gear extension system was tested and found to work properly. The landing gear down and locked light intensity was in the dime position. The light was tied into the cockpit lighting system, and that system was at max dim. Landing into the late evening sun would make it extremely difficult, to determine the gear position with the light fully dimmed.

As the FAA filed it

(-23) THE PILOT LINED UP WITH THE RUNWAY ON FINAL APPROACH. HE WAS LANDING INTO THE LATE AFTERNOON SUN. HE PUT THE LANDING GEAR HANDLE IN THE GEAR DOWN POSITION, BUT DID NOT GET A GEAR DOWN AND LOCKED LIGHT. THE PILOT THOUGHT THAT THE LANDING GEAR HAD FAILED TO EXTEND. THREE ATTEMPTS WERE MADE TO EXTEND THE GEAR WITH THE GEAR DOWN HANDLE. ALL ATTEMPTS FAILED TO GET A GEAR DOWN AND LOCKED LIGHT. THE PILOT TRIED TO EXTEND THE GEAR WITH THE EMERGENCY GEAR DOWN SYSTEM. THESE ATTEMPTS FAILED TO GET A GEAR DOWN AND LOCKED LIGHT. THE PILOT MAY HAVE FAILED TO USE THE CORRECT EMERGENCY GEAR EXTENSION PROCEDURES, TO EXTEND THE GEAR. THE AIRCRAFT LANDING GEAR WAS TESTED, AND FOUND TO WORK NORMALLY. THE GEAR WAS CYCLED 10 TIMES AND WORKED EACH TIME. THE EMERGENCY GEAR EXTENSION SYSTEM WAS TESTED AND FOUND TO WORK PROPERLY. THE LANDING GEAR DOWN AND LOCKED LIGHT INTENSITY WAS IN THE DIME POSITION. THE LIGHT WAS TIED INTO THE COCKPIT LIGHTING SYSTEM, AND THAT SYSTEM WAS AT MAX DIM. LANDING INTO THE LATE EVENING SUN WOULD MAKE IT EXTREMELY DIFFICULT, TO DETERMINE THE GEAR POSITION WITH THE LIGHT FULLY DIMMED.

Other reports on N15546 · 1

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