20000924030809I

Incident

FAA incident report · Cessna 560CESSNA · Jacksonville, FL · September 24, 2000

Date
September 24, 2000 · 21:40 local
Place
Jacksonville, FL
Airport
Jacksonville International
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N309QS
Reported as
Cessna 560CESSNA
Reported engine
Pratt & Whitney JT15D5
People aboard
2
Fatal injuries
0
Pilot’s flight hours
5,829 total499 in this make and model85 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)Stuck elevator. Diverted to jax. Landed safely. At flight level 250 auto pilot trim comparator illuminated. Crew attempted to trim aircraft using trim wheel. Trim wheel was stuck. Auto-pilot was disconnected and crew completed checklist and declared an emergency an uneventful no flaps was accomplished aircraft landed safely. Corrective action: found faulty printed circuit board trim unit that had a stuck relay. Replaced new p.c. board & ops checked ok in accordance with CE-560 maintenance manual chapter 27-30-00.

As the FAA filed it

(-23)STUCK ELEVATOR. DIVERTED TO JAX. LANDED SAFELY. AT FLIGHT LEVEL 250 AUTO PILOT TRIM COMPARATOR ILLUMINATED. CREW ATTEMPTED TO TRIM AIRCRAFT USING TRIM WHEEL. TRIM WHEEL WAS STUCK. AUTO-PILOT WAS DISCONNECTED AND CREW COMPLETED CHECKLIST AND DECLARED AN EMERGENCY AN UNEVENTFUL NO FLAPS WAS ACCOMPLISHED AIRCRAFT LANDED SAFELY. CORRECTIVE ACTION: FOUND FAULTY PRINTED CIRCUIT BOARD TRIM UNIT THAT HAD A STUCK RELAY. REPLACED NEW P.C. BOARD & OPS CHECKED OK IN ACCORDANCE WITH CE-560 MAINTENANCE MANUAL CHAPTER 27-30-00.