N660CC

RAYTHEON AIRCRAFT COMPANY 400A · 2001 · Fixed-wing multi-engine · 2 engines · 10 seats · Valid Registration

Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2009-06-18 – 2012-06-10.

SMOKE/FUMES/ODORS/SPARKS · 2012-06-10 Matched by certificate designator
ATA 2150

Part: A/C PACK — FAILED (ZONE 100) · airframe 3,330 hrs · 3,262 cycles

SMOKE AND UNCOMMANDED HEAT IN COCKPIT SHORTLY AFTER TAKEOFF. THE FREON AIR CONDITIONING SYS HAD BEEN DEFERRED DUE TO A DAMAGED DRIVE BELT REQUIRING REPLACEMENT. THE (M) PROCEDURE 21-50.1 CALLED FOR THE "AIR COND" CIRCUIT BREAKER TO BE PULLED/COLLARED. WITH THIS CIRCUIT BREAKER PULLED AIR CONDITIONING SYS GOES TO MANUAL MODE, NOT AUTOMATIC MODE THEREFORE THE CABIN VALVE GOES FULL HOT RESULTING IN EXTREME HEAT IN DUCTING WHICH ALSO CAUSED LIGHT SMOKE (PROBABLY FROM DEBRIS). RESET AIR/COND CIRCUIT BREAKER, SYS OPS CHECKED GOOD. PULLED CIRCUIT BREAKER 410 FOR FREON AIR SYS VERIFIED FREON AIR SYS INOP. FOUND (M) PROCEDURE FOR DMI 21-50. 1 IDENTIFIES THE WRONG C/B FOR DEACTIVATION. THE FREON AIR CONDITIONING SYS WAS REPAIRED, THE DEFERRAL CLEARED. THE AIR CONDITIONING SYS WAS VERIFIED TO BE OPS. MEL PROCEDURE 21-50-1 IS TO BE REWRITTEN.

Source: SDR UG8A20120610660
SMOKE/FUMES/ODORS/SPARKS · 2012-06-10 Matched by certificate designator
ATA 3510

Part: OXYGEN MASK — SEPARATED · airframe 3,330 hrs · 3,262 cycles

DURING A DECLARED EMERGENCY FOR SMOKE AND HEAT IN COCKPIT, THE PILOT OXYGEN MASK BROKE UPON DEPLOYMENT. IT APPEARS THE MASK WAS DEFECTIVE. IT WAS IN DUE O/H BY THE END OF JUNE 2012. THE MASK WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.

Source: SDR UG8A201206190001
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2009-06-18 Unresolved
ATA 7320

Part: FUEL CONTROL — POWER LOSS (ZONE 400) · airframe 2,573 hrs · 2,483 cycles

"RT ENG EFC OFF" ANNUNCIATOR ILLUMINATED DURING FLIGHT. RT ENGINE ROLLED BACK 35-40 PERCENT N1.

Source: SDR BUEA634C61809