20010321003909I

Incident · Minor damage

FAA incident report · Cessna 210B · Phoenix, AZ · March 21, 2001

Date
March 21, 2001 · 12:38 local
Place
Phoenix, AZ
Airport
Phoenix-Deer Valley Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9565X
Reported as
Cessna 210B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
647 total433 in this make and model32 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 return flight from cez to dvt the pilot was unable to lower the landing gear prior to landing at dvt. After recycling the landing gear all three wheels remained up and locked. After performing the emergency gear extension procedure all three landing gear remained in the up and locked position. Pilot performed gear up landing resulting in damage to the propeller and minor skin damage to the aircraft belly. Post landing inspection indicated possible failure of hydraulic system relief valve resulting in insufficient hydraulic pressure to open the up locks.

As the FAA filed it

(-23) ON RETURN FLIGHT FROM CEZ TO DVT THE PILOT WAS UNABLE TO LOWER THE LANDING GEAR PRIOR TO LANDING AT DVT. AFTER RECYCLING THE LANDING GEAR ALL THREE WHEELS REMAINED UP AND LOCKED. AFTER PERFORMING THE EMERGENCY GEAR EXTENSION PROCEDURE ALL THREE LANDING GEAR REMAINED IN THE UP AND LOCKED POSITION. PILOT PERFORMED GEAR UP LANDING RESULTING IN DAMAGE TO THE PROPELLER AND MINOR SKIN DAMAGE TO THE AIRCRAFT BELLY. POST LANDING INSPECTION INDICATED POSSIBLE FAILURE OF HYDRAULIC SYSTEM RELIEF VALVE RESULTING IN INSUFFICIENT HYDRAULIC PRESSURE TO OPEN THE UP LOCKS.

Other reports on N9565X · 1

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