20040728021369I

Incident · Minor damage

FAA incident report · Blanca 17-30A · Sylacauga, AL · July 28, 2004

Date
July 28, 2004 · 17:30 local
Place
Sylacauga, AL
Airport
Merkel Field Sylacauga Municipal
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7373V
Reported as
Blanca 1730A
Reported engine
Continental IO520K
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,300 total900 in this make and model12 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 July 28, 2004, about 1230 CST, a Bellanca 17-30A, N7373V, landed with the gear up. Investigation of the incident revealed that the hydraulic system malfunctioned which caused the gear not to extend. The private-rated pilot received no injury and the airplane incurred minor belly damage. The pilot stated that while performing slow flight maneuvers he disabled the auto-axion (automatic landing gear control) and forgot to enable the auto-axion after the manuevers. The above action may have contributed to the landing gear not extending when the aircraft speed dropped below 100 knots. The on site investigation of the incident revealed that the landing gear motor worked intermediately. The emergency landing gear lever was activated and the landing gear extended properly and locked. The aircraft's wings, the main landing gears' clam shell doors and the propeller blades were damaged.

As the FAA filed it

(-23) ON JULY 28, 2004, ABOUT 1230 CST, A BELLANCA 17-30A, N7373V, LANDED WITH THE GEAR UP. INVESTIGATION OF THE INCIDENT REVEALED THAT THE HYDRAULIC SYSTEM MALFUNCTIONED WHICH CAUSED THE GEAR NOT TO EXTEND. THE PRIVATE-RATED PILOT RECEIVED NO INJURY AND THE AIRPLANE INCURRED MINOR BELLY DAMAGE. THE PILOT STATED THAT WHILE PERFORMING SLOW FLIGHT MANEUVERS HE DISABLED THE AUTO-AXION (AUTOMATIC LANDING GEAR CONTROL) AND FORGOT TO ENABLE THE AUTO-AXION AFTER THE MANUEVERS. THE ABOVE ACTION MAY HAVE CONTRIBUTED TO THE LANDING GEAR NOT EXTENDING WHEN THE AIRCRAFT SPEED DROPPED BELOW 100 KNOTS. THE ON SITE INVESTIGATION OF THE INCIDENT REVEALED THAT THE LANDING GEAR MOTOR WORKED INTERMEDIATELY. THE EMERGENCY LANDING GEAR LEVER WAS ACTIVATED AND THE LANDING GEAR EXTENDED PROPERLY AND LOCKED. THE AIRCRAFT'S WINGS, THE MAIN LANDING GEARS' CLAM SHELL DOORS AND THE PROPELLER BLADES WERE DAMAGED.

Other reports on N7373V · 1

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