20010809035899I

Incident

FAA incident report · Gulstm GV · Cleveland, OH · August 9, 2001

Date
August 9, 2001 · 17:12 local
Place
Cleveland, OH
Airport
Cleveland-Hopkins International
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N15UC
Reported as
Gulstm GV

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 August 9, 2001 at approximately 1700 local time, N15UC, gulfstream-v, enroute from lexington KY, (lex) to tetrboro, NJ (teb) the crew experienced a fire/overheat warning light for left aft duct. They requested and received priority handling and diverted to Cleveland Hopkins airport (cle) and landed without incident at 1712 local. Upon investigation it was found that the thermal switch part number 512T130B150-001 was defective and the manufacturer had installed the wrong part. Replaced thermal switch with part number GAS850DF512-250 as per the illustrated parts catalog 26-10-00 figure 1 item 5. The previous installed switch was 150 degree setting, the required switch settings should be 250 degree setting. Performed operational check. System operational check good. No defects noted. Aircraft returned to service.

As the FAA filed it

(-23) ON AUGUST 9, 2001 AT APPROXIMATELY 1700 LOCAL TIME, N15UC, GULFSTREAM-V, ENROUTE FROM LEXINGTON KY, (LEX) TO TETRBORO, NJ (TEB) THE CREW EXPERIENCED A FIRE/OVERHEAT WARNING LIGHT FOR LEFT AFT DUCT. THEY REQUESTED AND RECEIVED PRIORITY HANDLING AND DIVERTED TO CLEVELAND HOPKINS AIRPORT (CLE) AND LANDED WITHOUT INCIDENT AT 1712 LOCAL. UPON INVESTIGATION IT WAS FOUND THAT THE THERMAL SWITCH PART NUMBER 512T130B150-001 WAS DEFECTIVE AND THE MANUFACTURER HAD INSTALLED THE WRONG PART. REPLACED THERMAL SWITCH WITH PART NUMBER GAS850DF512-250 AS PER THE ILLUSTRATED PARTS CATALOG 26-10-00 FIGURE 1 ITEM 5. THE PREVIOUS INSTALLED SWITCH WAS 150 DEGREE SETTING, THE REQUIRED SWITCH SETTINGS SHOULD BE 250 DEGREE SETTING. PERFORMED OPERATIONAL CHECK. SYSTEM OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.