N510UP

CESSNA 560XL · 2005 · Fixed-wing multi-engine · 2 engines · 13 seats · Valid Registration

Registered owner: CORPORATE FLIGHT MANAGEMENT INC, TN (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Gama Aviation LLC (O2GA)Certificate holderMatched 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.

3 reports on file, 2015-04-02 – 2020-02-11.

WARNING INDICATION · 2020-02-11 Matched by certificate designator
ATA 3234

Part: CONTROL HANDLE — INTERMITTENT (MLG) · airframe 11,904 hrs · 8,575 cycles

AFTER LANDING AND CLEARING THE RUNWAY EXPERIENCED A PRIMARY BRAKE SYSTEM FAILURE FOLLOWED BY LOSS OF BRAKE PRESSURE/ANTI-SKID MASTER WARNING. APPLIED EMERGENCY BRAKES TO STOP AIRCRAFT WHERE IT WAS THEN TOWED TO FBO. MAINTENANCE REPLACED THE RELAY, DIODE AND LANDING GEAR CONTROL HANDLE. SYSTEM OPERATIONAL/TAXI CHECK WAS ACCOMPLISHED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR O2GA2020021815101
AFFECT SYSTEMS · 2018-11-27 Matched by certificate designator
ATA 2910

Part: VALVE — INTERMITTENT (HYD SYSTEM) · airframe 11,050 hrs · 7,942 cycles

DURING APPROACH SPEDD BRAKES WOULD NOT DEPLOY, FLAPS WOULD NOT MOVE AND LANDING GEAR WOULD NOT DEPLOY. NO WARNING ANNUNCIATORS ILLUMINATED AND CIRCUIT BREAKERS WERE NOT TRIPPED. CREW FOLLOWED THE NO FLAPS AND LANDING GEAR EXTENSION PROCEDURE PER CHECKLIST. EMERGENCY WAS DECLARED. LANDING WAS UNEVENTFUL. MAINTENANCE ISOLATED THE DISCREPANCY TO FAULTY HYDRAULIC LOADING VALVE. VALVE REPLACED AND A OPERATION CHECKS PERFORMED WITH NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR O2GA201812035101
OTHER · 2015-04-02 Matched by certificate designator
ATA 2510

Part: COVER — CRACKED (COCKPIT) · airframe 8,055 hrs · 5,718 cycles

DURING UNSCHEDULED ELEVATOR COUNTERWEIGHT MAINTENANCE, PLASTIC TRIM COVER WAS FOUND CRACKED INSIDE PEDESTAL COMPARTMENT. IAW ENGINEERING LETTER M150404DK DATED 04 02 2015 PANEL WAS DEFERRED & PLACED ON 04 19 2015. ACFT WAS RETURNED TO SERVICE.

Source: SDR O2GA2015042851001