N785JP

RAYTHEON AIRCRAFT COMPANY C90A · 2004 · Fixed-wing multi-engine · 2 engines · 9 seats · Valid Registration

Registered owner: GUARDIAN FLIGHT LLC, TX (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Guardian Flight, LLC. (G1IA)Certificate holder—Matched by certificate designator

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.

2 reports on file, 2021-05-07 – 2024-09-15.

OTHER · 2024-09-15 Matched by certificate designator
ATA 2150

Part: MOTOR — DEFECTIVE (AIR CON CMPRESSR) · airframe 7,946 hrs · 10,922 cycles

AIR CONDITIONER MOTOR FAILED.

Source: SDR G1IA2024092000015
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2021-05-07 Matched by certificate designator
ATA 7200

Part: ENGINE — SURGES (LEFT) · airframe 5,608 hrs · 7,816 cycles

7-10 MILES FROM KFLG THE LEFT ENGINE BEGAN TO SURGE 50-100 FT/LBS ON THE TORQUE. NO OTHER FLUCTUATIONS ON THE LEFT ENGINE GAUGES WERE OBSERVED. THIS FLUCTUATION WAS FIRST NOTICES AUDIBLY. THIS OCCURRED UPON REDUCING THE THROTTLES TO 400 FT/LBS. AT APPROXIMATELY 4-5 MILES FROM KFLG THE LEFT ENGINE BEGAN TO SURGE 300-400 FT/LBS. NO OTHER FLUCTUATIONS CAN BE RECALLED FROM MEMORY ON THE OTHER GAUGES DUE TO SUN GLARE AND PROXIMITY TO LANDING. THE THROTTLE SETTINGS WERE BROUGHT BACK TO 200 FT/LBS PRIOR TO THESE SURGES. BRINGING THE THROTTLES TO FULL IDLE MADE THE SURGE SPREAD HIGHER ON THE LEFT ENGINE. PERFORMED A GROUND OPERATIONAL CHECK. ADJUSTED BOTH L/H AND R/H PROPELLER RPM ADJUSTMENT SCREWS 2 TURNS CLOCKWISE TO REDUCE MAX RPM. GROUND FUNCTIONAL CHECKS PERFORMED WITH SATISFACTORY RESULTS IAW BLACKHAWK DOCUMENT NO. 200710-30 REV 1R ENGINE RIGGING FOR CONTROL PROCEDURES. OPERATIONAL CHECK FLIGHT PERFORMED FOR L/H AND R/H PROP RPM ADJUSTMENTS AND L/H ENGINE SURGING AND WAS FOUND TO BE SATISFACTORY

Source: SDR G1IA20210507006