- Registered owner
- Highlands Group LLC
- Location
- Lahaina, HI
- Owner type
- LLC
- Serial number
- 465-34
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- November 20, 2019
- Expires
- November 30, 2029
- Mode S code
- A5C056
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1970 | 1 |
| 1975 | 1 |
| 1980 | 1 |
| 1982 | 1 |
| 1983 | 2 |
| 1993 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1999 | 1 |
| 2001 | 1 |
| 2006 | 1 |
Airframe · Rockwell International NA-265-65
AD 2005-25-18Wing center sectionAD 2001-22-14Fire Extinguishing System Bottle CartridgesAD 97-05-03 R1Global Positioning SystemsAD 97-04-15Fire Extinguisher Bottle CartridgesAD 96-25-12Auxiliary Power UnitsAD 95-26-15 R1Traffic Alert and Collision Avoidance SystemsAD 94-01-05Traffic Alert and Collision Avoidance System II ProcessorsAD 92-27-16Hydraulic PumpAD 82-26-02Vertical Floor Panel InspectionAD 82-27-10Horizontal Stabilizer Trim ActuatorAD 82-10-02 R1Flap Screwjack InspectionAD 80-05-02Safety Belt AssembliesAD 75-04-05Engine Fuel Pressure SwitchesAD 70-24-03Engine Fire Control HandleAD 69-10-01Main Landing Gear PistonsInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N47SEMatched 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 Rockwell International NA-265-65 aircraft
FAA incident reports
No FAA accident or incident reports matched to N47SEMatched 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 Rockwell International NA-265-65 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 UVVR2010022600006Floorbeam · corrodedANGLE CORRODED (EXFOLIATED) ON LOWER FS 166.3 FUSELAGE FLOOR SUPPORT WEB RT BP 8-10, ATTACHED TO LOWER FUSELAGE SKIN AND WEB.SDR UVVR2010021500005Skin · crackedFUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF LEFT OVERWING ESCAPE HATCH OPENING.SDR UVVR2010021500004Skin · crackedFUSELAGE SKIN CRACKED AT LOWER FWD CORNER OF RT OVERWING ESCAPE HATCH OPENING.SDR UVVR2010021100001Frame · cracked3 INCH CRACK IN LEFT FUSELAGE SIDE FRAME AT FUSELAGE STATION 257.65 APPROXIMATELY 2 INCHES ABOVE CABIN FLOOR.SDR JV2R20040001Tire · separatedTIRE TREAD SEPARATION FROM TIRE CASING. EACH TIRE REPORTED HAS LESS THAN TWENTY LANDINGS ON IT. THIS PROBLEM REPORTED TO TIRE MFG. SAMPLES OF DISCREPANT UNITS FORWARDED TO MFG FOR EVALUATION. THIS IS THE FIRST OF NINE KNOWN FAILURES OF THESE TIRES. ONE OT
STCs that may be installed · 105
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Rockwell International NA-265-65
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC ST11216DSInstallation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft