20090713011989I

Incident · Minor damage

FAA incident report · Cessna 525A · July 13, 2009

Date: July 13, 2009 · 14:00 local
Phase of flight: Other, Specify
Operating rules: General operating rules (Part 91)
Damage: Minor damage
Aircraft: N140DA
Reported as: Cessna 525A
Reported engine: WILINT FJ442C
People aboard: 4
Fatal injuries: 0
Other injuries: 0
Pilot’s flight hours: 2,500 total1,800 in this make and model10 in the last 90 days

N140DARegistered now · Cessna 525AS/N 525A0140 · Built 2003 Airframe modelCessna 525A Engine modelWilliams FJ-44 seriesTurbo-fan

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 July 10, 2009, at 1400 hours this aircraft departed philadelphia for jenks,ok (rvs). The aircraft made stops at louisville (sdf) and tulsa (tul), completeing the flight at 1630 local time, landing at rvs. The pilot indicated the flight was conducted under FAR 91, visual flight rules. There was a post flight completed at sdf and no faults were noted. The pilot stated there was never an indication of a problem throughout the flight. There was no walk around conducted at tul, the number two was not shut down at tul. After arrival at rvs a post flight inspection revealed the number 2 attenuator was missing. The part number for the number 2 (r/h) thrust attenuator part is 6354152-6.

As the FAA filed it

(-23) ON JULY 10, 2009, AT 1400 HOURS THIS AIRCRAFT DEPARTED PHILADELPHIA FOR JENKS,OK (RVS). THE AIRCRAFT MADE STOPS AT LOUISVILLE (SDF) AND TULSA (TUL), COMPLETEING THE FLIGHT AT 1630 LOCAL TIME, LANDING AT RVS. THE PILOT INDICATED THE FLIGHT WAS CONDUCTED UNDER FAR 91, VISUAL FLIGHT RULES. THERE WAS A POST FLIGHT COMPLETED AT SDF AND NO FAULTS WERE NOTED. THE PILOT STATED THERE WAS NEVER AN INDICATION OF A PROBLEM THROUGHOUT THE FLIGHT. THERE WAS NO WALK AROUND CONDUCTED AT TUL, THE NUMBER TWO WAS NOT SHUT DOWN AT TUL. AFTER ARRIVAL AT RVS A POST FLIGHT INSPECTION REVEALED THE NUMBER 2 ATTENUATOR WAS MISSING. THE PART NUMBER FOR THE NUMBER 2 (R/H) THRUST ATTENUATOR PART IS 6354152-6.