- Registered owner
- Kap Air LLC
- Location
- Canton, OH
- Owner type
- LLC
- Serial number
- E-3772
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- April 13, 2007
- Certificate issued
- October 8, 2022
- Expires
- October 31, 2029
- Mode S code
- A762F0
Hawker Beechcraft G36TCDS 3A15Airframe · Hawker Beechcraft G36TCDS E3SOEngine · Continental IO-550-B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 28
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 1 |
|---|---|
| 1988 | 3 |
| 1991 | 1 |
| 1993 | 3 |
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2004 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2022 | 3 |
| 2023 | 6 |
Airframe · Hawker Beechcraft G36
AD 2023-10-02Indicating/Recording System, NavigationAD 2022-03-15Fuel Quantity IndicatorAD 2009-15-01Wire harness/connector(s)Information bulletins that may apply · 15
Advisory, not mandatory.
Airframe · Hawker Beechcraft G36
SAIB CE-15-22Wing Leading Edge Hinge-Pin CorrosionSAIB CE-12-36Flight Controls: AileronSAIB CE-12-18Flight Controls: Elevator Control Cable ConditionSAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsEngine · Continental IO-550-B
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB NE-17-11POWERPLANT Engine damage as a result of kickbackSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-10-07Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.SAIB NE-09-08Reciprocating Engine Cylinder SectionSAIB NE-07-09R1Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum HeadNTSB investigations
No NTSB investigations matched to N575WMatched 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 Hawker Beechcraft G36 aircraft
FAA incident reports
No FAA accident or incident reports matched to N575WMatched 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 Hawker Beechcraft G36 aircraft
Reports on N575W not matched to an aircraft · 2
They name N575W, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19971209042239IBeech B99 · Koyuk, AKNarrative: enroute from fairbanks, Alaska to nome, Alaska flight crew heard engine surging and noticed flames emitting from the #1 engine area. Being unable to determine source of flames, crew elected to secure engine and made an emergency landing at Koyuk,…Incident 19841127069819ICessna 550 · Hartford, CTWhile taxiing to ramp struck parked N54857. Minor damage to parked aircraft.
Service difficulty reports
No reports matched to N575WGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Hawker Beechcraft G36 aircraft
Reports on N575W not matched to an aircraft · 3
They name N575W, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX1587Filler Cap · looseOIL PRESSURE ON RIGHT ENGINE STARTED DROPPING SHORTLY AFTER TAKEOFF. FINDINGS: OIL LOSS DUE TO UNSECURED OIL CAP.SDR 99ZZZX434Bearing · stiffJUST AFTER LEVEL-OFF, THE RIGHT ENGINE WOULD NOT RESPOND TO POWER REDUCTIONS. IN ORDER TO NOT OVER-TORQUE THE ENGINE ON DESCENT, THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED.SDR 97ZZZX830Power Pack · malfunctionNITROGEN PRE-CHARGE LEAKED PAST ACCUMULATOR PISTON CAUSING PRESSURE BUILD-UP IN RETRACT SIDE OF LANDING GEAR SYSTEM AND COLLAPSE OF LEFT MAIN GEAR WHILE AIRCRAFT WAS BEING TOWED. SUBMITTER STATED LATER DASH NUMBER HYDRAULIC POWER PACK INCORPORATES A VENT VALV
STCs that may be installed · 176
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.