19960504021949I

Incident · Minor damage

FAA incident report · Cessna 210 · Tacoma, WA · May 4, 1996

Date
May 4, 1996 · 17:07 local
Place
Tacoma, WA
Airport
Mcchord Afb
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9668T
Reported as
Cessna 210
Reported engine
Continental IO470E
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,200 total250 in this make and model30 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: pilot said he had trouble retracting landing gear on takeoff, so he returned to airport. Pilot was unable to fully extend right main gear. A partial gear-up landing was made. Aircraft sustained minor damage to the right wing tip and right horizontal stabilizer. Investigation revealed that the hydraulic reservoir was depleted. A leak was discovered originating from a 1/4 inch aluminum hydraulic line connected to the lock cylinder in the nose wheel well. The line was cracked at the flare that attaches to the lock cylinder. The weather information at the time of the incident was: tiw sa 2345 15 sct 50 sct 40 58/32/2609/025.

As the FAA filed it

NARRATIVE: PILOT SAID HE HAD TROUBLE RETRACTING LANDING GEAR ON TAKEOFF, SO HE RETURNED TO AIRPORT. PILOT WAS UNABLE TO FULLY EXTEND RIGHT MAIN GEAR. A PARTIAL GEAR-UP LANDING WAS MADE. AIRCRAFT SUSTAINED MINOR DAMAGE TO THE RIGHT WING TIP AND RIGHT HORIZONTAL STABILIZER. INVESTIGATION REVEALED THAT THE HYDRAULIC RESERVOIR WAS DEPLETED. A LEAK WAS DISCOVERED ORIGINATING FROM A 1/4 INCH ALUMINUM HYDRAULIC LINE CONNECTED TO THE LOCK CYLINDER IN THE NOSE WHEEL WELL. THE LINE WAS CRACKED AT THE FLARE THAT ATTACHES TO THE LOCK CYLINDER. THE WEATHER INFORMATION AT THE TIME OF THE INCIDENT WAS: TIW SA 2345 15 SCT 50 SCT 40 58/32/2609/025.

Other reports on N9668T · 1

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