Registered owner
Cff Air Inc
Owner type
Corporation
Serial number
205
Year built
1978
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Special flight permit
Airworthiness date
July 7, 2008
Certificate issued
December 5, 2022
Expires
December 31, 2029
Mode S code
A745E8

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 41

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1975In forceSuperseded2026
ADs by the year they took effect: 44 ADs
19751
19781
19804
19811
19821
19831
19841
19852
19862
19872
19881
19891
19911
19921
19953
19964
19982
19993
20002
20013
20041
20052
20072
20181
20221
See all 44 ADs

Information bulletins that may apply · 4

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N568PAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Gates Learjet 35A aircraft

FAA incident reports

No FAA accident or incident reports matched to N568PAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Gates Learjet 35A aircraft

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR ESPA2023072400308Unknown · unknownDURING CRUISE, RH ENGINE EXPERIENCED A FLAMEOUT. THE FLIGHT CREW SECURED THE MOTOR AND RETURNED TO BASE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RH FUEL CONTROL AND FUEL FILTER, PERFORMED FUEL PUMP FUNCTIONAL TESTS, AND PERFORMED FIVE POINT RUNS WITH ACJul 17, 2023 · N568PA · Lear 35A · Fuel Control/Turbine EnginesSDR 2013F00018Swivel Fitting · blew outAFTER TAKEOFF PILOT REPORTED NO HYD PRESSURE. UPON LANDING SAFELY AND TROUBLESHOOTING THE ISSUE , FOUND THE MLG ACTUATOR RETRACT SWIVEL FITTING HAD FAILED. R & R THE SWIVEL FITTING WITH A NEW PART (PN 142870). PERFORMED ALL GEAR SWINGS AND ASSOCIATED HYDJan 15, 2013 · N568PA · Lear 35A · Hydraulic System, MainSDR ESPADJ2008-2Wire · brokenON LIFT OFF, CREW NOTED FUMES AND SMOKE IN ACFT, AND THE ACFT PRESSURIZATION SYS WAS IN EMERGENCY. POWER WAS REDUCED AND ENGINE BLEED AIR SWITCHES WERE CYCLED, BUT LT ENGINE REMAINED IN EMERGENCY. CAPTAIN DECLARED AN EMERGENCY TO GET PRIORITY LANDING AND RETURNov 17, 2008 · N568PA · Lear 35A · Engine Bleed Air System WiringSDR ESP2008F00000Circuit Breaker · loose(30) MINUTES AFTER THE ACTIVATION OF WINDSHIELD HEAT, THE RT ESSENTIAL BUS CIRCUIT BREAKER POPPED. CREW COMPLETED EMERGENCY CHECKLIST FOR AN ELECTRICAL FAILURE. THE CIRCUIT BREAKER WOULD NOT RESET. ATC GAVE VECTORS AND DESCENT. CREW DID A VISUAL APPROACH. Jul 5, 2008 · N568PA · Lear 35A · Electrical Power System WiringSDR ESPAOdor · detectedSMOKE WAS SUSPECTED IN CABIN. ENTIRE AREA IN SUSPECTED AREA WAS INSPECTED. NO DEFECTS WERE FOUND. PILOT REPORTED LEADING EDGE ANTI-ICE WAS INADVERTENTLY LEFT ON POSSIBLE CAUSING THE SMELL OF SMOKE. AIRCRAFT WAS RUN, SYSTEMS WERE OPERATIONALLY CHECKED AND FFeb 25, 2004 · N568PA · Lear 35A · Air Distribution System

STCs that may be installed · 228

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 228 STCs