20040430006529I

Incident · Minor damage

FAA incident report · Piper PA-24-250 · Columbia, SC · April 30, 2004

Date
April 30, 2004 · 20:40 local
Place
Columbia, SC
Airport
Owens Downtown Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6799P
Reported as
Piper PA24250
People aboard
3
Fatal injuries
0
Pilot’s flight hours
7,015 total161 in this make and model72 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 following factors contributed to the gear up landing of N6799P, on may 1, 2004: 1. Mr. Lintner has approximately 3 hours in a Piper PA-24, in the last ninety days, including the flight down to hilton head. 2. The landing gear switch has a neutral position that could be confused with the down position. 3. Mr. Lintner's power setting was probably above 12 inches of mercury on final so the landing gear warning horn would not have sounded. The landing gear system performed correctly on three separate cycles. Even if the circuit breaker was popped, and Mr. Lintner had selected the down position on the landing gear switch, the landing gear indicating light (green) would not have illuminated indicated the gear was down and locked.

As the FAA filed it

(-23) THE FOLLOWING FACTORS CONTRIBUTED TO THE GEAR UP LANDING OF N6799P, ON MAY 1, 2004: 1. MR. LINTNER HAS APPROXIMATELY 3 HOURS IN A PIPER PA-24, IN THE LAST NINETY DAYS, INCLUDING THE FLIGHT DOWN TO HILTON HEAD. 2. THE LANDING GEAR SWITCH HAS A NEUTRAL POSITION THAT COULD BE CONFUSED WITH THE DOWN POSITION. 3. MR. LINTNER'S POWER SETTING WAS PROBABLY ABOVE 12 INCHES OF MERCURY ON FINAL SO THE LANDING GEAR WARNING HORN WOULD NOT HAVE SOUNDED. THE LANDING GEAR SYSTEM PERFORMED CORRECTLY ON THREE SEPARATE CYCLES. EVEN IF THE CIRCUIT BREAKER WAS POPPED, AND MR. LINTNER HAD SELECTED THE DOWN POSITION ON THE LANDING GEAR SWITCH, THE LANDING GEAR INDICATING LIGHT (GREEN) WOULD NOT HAVE ILLUMINATED INDICATED THE GEAR WAS DOWN AND LOCKED.

Other reports on N6799P · 2

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