20001101031989I

Incident · Minor damage

FAA incident report · Cessna 172RG · Oakland, CA · November 1, 2000

Date
November 1, 2000 · 20:30 local
Place
Oakland, CA
Airport
Metropolitan Oakland International
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9639B
Reported as
Cessna 172RG
People aboard
2
Fatal injuries
0
Pilot’s flight hours
374 total300 in this make and model

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)At about 2030 hrs on approach to iak instructor pilot selected "landing gear down". Down & locked light did not illuminate. Nose & r/h main verified down & locked. L/h MLG would not fully extend. Attempts to lock gear using emergency extension mechanism was not successful. I/p landed the aircraft with minimum skin damage to underside. Propeller struck ground, sudden engine stoppage procedures to follow. Unpon jacking acft. It was noted the l/h MLG swung freely & would not retract or respond to hydraulic actuation. Removal of actuating cylinder revealed a fractured pivot shaft-actuating cyliner side. Detailed inspection of landing gear components of follow. Malfunction or defect report completed by operator. Investigation closed.

As the FAA filed it

(-23)AT ABOUT 2030 HRS ON APPROACH TO IAK INSTRUCTOR PILOT SELECTED "LANDING GEAR DOWN". DOWN & LOCKED LIGHT DID NOT ILLUMINATE. NOSE & R/H MAIN VERIFIED DOWN & LOCKED. L/H MLG WOULD NOT FULLY EXTEND. ATTEMPTS TO LOCK GEAR USING EMERGENCY EXTENSION MECHANISM WAS NOT SUCCESSFUL. I/P LANDED THE AIRCRAFT WITH MINIMUM SKIN DAMAGE TO UNDERSIDE. PROPELLER STRUCK GROUND, SUDDEN ENGINE STOPPAGE PROCEDURES TO FOLLOW. UNPON JACKING ACFT. IT WAS NOTED THE L/H MLG SWUNG FREELY & WOULD NOT RETRACT OR RESPOND TO HYDRAULIC ACTUATION. REMOVAL OF ACTUATING CYLINDER REVEALED A FRACTURED PIVOT SHAFT-ACTUATING CYLINER SIDE. DETAILED INSPECTION OF LANDING GEAR COMPONENTS OF FOLLOW. MALFUNCTION OR DEFECT REPORT COMPLETED BY OPERATOR. INVESTIGATION CLOSED.

Other reports on N9639B · 1

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