20070320007779I

Incident · Minor damage

FAA incident report · Piper PA-44-180 · Stockton, CA · March 20, 2007

Date
March 20, 2007 · 10:00 local
Place
Stockton, CA
Airport
Stockton Metropolitan
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N98749
Reported as
Piper PA44180
People aboard
2
Fatal injuries
0
Pilot’s flight hours
3,700 total300 in this make and model200 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 a training flight, while on an ATC vector for a practice ILS approach, the instructor reduced power to simulate single engine operation. With the landing gear up, the warning horn activated and continued to beep. Since it was still too early in the approach to lower the landing gear, the instructor elected to disable the horn by pulling the circuit breaker. Disabling the circuit breaker also disables the green panel gear lights and the hydraulic pump. When on final approach and intercepting the glideslope, the pilot selected the landing gear to the down position. The pilot did not see that the lights were not illuminated nor did he notice that there was no change in the noise around the aircraft. The aircraft continued the approach and landed with the gear still retracted.

As the FAA filed it

(-23) ON A TRAINING FLIGHT, WHILE ON AN ATC VECTOR FOR A PRACTICE ILS APPROACH, THE INSTRUCTOR REDUCED POWER TO SIMULATE SINGLE ENGINE OPERATION. WITH THE LANDING GEAR UP, THE WARNING HORN ACTIVATED AND CONTINUED TO BEEP. SINCE IT WAS STILL TOO EARLY IN THE APPROACH TO LOWER THE LANDING GEAR, THE INSTRUCTOR ELECTED TO DISABLE THE HORN BY PULLING THE CIRCUIT BREAKER. DISABLING THE CIRCUIT BREAKER ALSO DISABLES THE GREEN PANEL GEAR LIGHTS AND THE HYDRAULIC PUMP. WHEN ON FINAL APPROACH AND INTERCEPTING THE GLIDESLOPE, THE PILOT SELECTED THE LANDING GEAR TO THE DOWN POSITION. THE PILOT DID NOT SEE THAT THE LIGHTS WERE NOT ILLUMINATED NOR DID HE NOTICE THAT THERE WAS NO CHANGE IN THE NOISE AROUND THE AIRCRAFT. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITH THE GEAR STILL RETRACTED.

Other reports on N98749 · 1

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