19951118037799I

Incident · Minor damage

FAA incident report · Cessna 337C · West Palm Beach, FL · November 18, 1995

Date
November 18, 1995 · 16:20 local
Place
West Palm Beach, FL
Airport
Palm Beach International
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2503S
Reported as
Cessna 337C
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,500 total800 in this make and model5 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.

Narrative: immediately after takeoff the pilot smelled the odor of hydraulic fluid and observed the gear had not fully retracted. He notified the control tower and did two fly-by's. ground personnel confirmed the gear was in the intermediate position. He was unable to extend it with the emergency hand pump and elected to fly around for two hours to burn fuel. About 10 mi. From the airport he feathered the rear engine and positioned the prop in the horizontal position. The nose gear was down and locked and the aircraft settled on the rear of the fuselage and the left lower vertical stabilizer causing minor damage. Loss of hydraulic fluid/pressure caused by flexible hyd. Brake hose which chaffed hole in aluminum hyd. Line allowing fluid to escape.

As the FAA filed it

NARRATIVE: IMMEDIATELY AFTER TAKEOFF THE PILOT SMELLED THE ODOR OF HYDRAULIC FLUID AND OBSERVED THE GEAR HAD NOT FULLY RETRACTED. HE NOTIFIED THE CONTROL TOWER AND DID TWO FLY-BY'S. GROUND PERSONNEL CONFIRMED THE GEAR WAS IN THE INTERMEDIATE POSITION. HE WAS UNABLE TO EXTEND IT WITH THE EMERGENCY HAND PUMP AND ELECTED TO FLY AROUND FOR TWO HOURS TO BURN FUEL. ABOUT 10 MI. FROM THE AIRPORT HE FEATHERED THE REAR ENGINE AND POSITIONED THE PROP IN THE HORIZONTAL POSITION. THE NOSE GEAR WAS DOWN AND LOCKED AND THE AIRCRAFT SETTLED ON THE REAR OF THE FUSELAGE AND THE LEFT LOWER VERTICAL STABILIZER CAUSING MINOR DAMAGE. LOSS OF HYDRAULIC FLUID/PRESSURE CAUSED BY FLEXIBLE HYD. BRAKE HOSE WHICH CHAFFED HOLE IN ALUMINUM HYD. LINE ALLOWING FLUID TO ESCAPE.