20010517008249I

Incident

FAA incident report · Saab 340B · Albany, NY · May 17, 2001

Date
May 17, 2001 · 16:00 local
Place
Albany, NY
Airport
Albany County
Phase of flight
Descent
Operating rules
Air carrier (Part 121)
Operator
SIMA
Aircraft
N297AE
Reported as
Saab 340B
Reported engine
GE CT79B

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 05/17/2001, aircraft departed buf enroute to jfk, during climb aircraft developed a strong vibration above 1270 prpm. As per aom vol 1 powerplant page 12, crew located the vibration as coming from the #1 engine. At 1230 prpm the engine ran normal with no other indications. Crew decided to shut down the #1 engine and divert the aircraft to alb. Aircraft landed on rwy 19 without further incident. Maintenance reported the #1 propeller was out of balance. Mechanics re-balanced the #1 engine propeller i/a/w Saab 340 maintenance manual 61-10-00, and found the propeller to be within normal operation limits. Maintenence requested a functional check flight (fcf) to verify reprair of #1 engine vibration in flight. Fcf proved to be satisfactory.

As the FAA filed it

(-23)ON 05/17/2001, AIRCRAFT DEPARTED BUF ENROUTE TO JFK, DURING CLIMB AIRCRAFT DEVELOPED A STRONG VIBRATION ABOVE 1270 PRPM. AS PER AOM VOL 1 POWERPLANT PAGE 12, CREW LOCATED THE VIBRATION AS COMING FROM THE #1 ENGINE. AT 1230 PRPM THE ENGINE RAN NORMAL WITH NO OTHER INDICATIONS. CREW DECIDED TO SHUT DOWN THE #1 ENGINE AND DIVERT THE AIRCRAFT TO ALB. AIRCRAFT LANDED ON RWY 19 WITHOUT FURTHER INCIDENT. MAINTENANCE REPORTED THE #1 PROPELLER WAS OUT OF BALANCE. MECHANICS RE-BALANCED THE #1 ENGINE PROPELLER I/A/W SAAB 340 MAINTENANCE MANUAL 61-10-00, AND FOUND THE PROPELLER TO BE WITHIN NORMAL OPERATION LIMITS. MAINTENENCE REQUESTED A FUNCTIONAL CHECK FLIGHT (FCF) TO VERIFY REPRAIR OF #1 ENGINE VIBRATION IN FLIGHT. FCF PROVED TO BE SATISFACTORY.