- Registered owner
- Wheels Up Partners LLC
- Location
- New York, NY
- Owner type
- LLC
- Serial number
- FL-905
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, commuter
- Airworthiness date
- January 27, 2014
- Certificate issued
- February 4, 2014
- Expires
- February 28, 2030
- Mode S code
- AB32AB
Beechcraft B300TCDS A24CEAirframe · Beechcraft B300TCDS E4EAEngine · Pratt & Whitney Canada PT6A-60A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1992 | 2 |
|---|---|
| 1994 | 3 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 6 |
| 1999 | 4 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 4 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2019 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 40 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Beechcraft B300
SAIB CE-15-15Empennage Horizontal & Vertical Stabilizer StructureSAIB CE-12-36Flight Controls: AileronNTSB investigations
No NTSB investigations matched to N820UPMatched 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 Beechcraft B300 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVGA20260402001Switch · faultyFLAPS FAILED ON APPROACH. SUSPECTED RIGHT HAND SAFETY SWITCH AT FAULT. REMOVED AND REPLACED SAFETY SWITCH. SWITCH CONDITION NEW, P/N ON101-521054-2 S/N ON 13292340C. P/N OFF101-52-1054-2 S/N UNK IAWB300AMM27-50-11. SAFETY SWITCH LINK ARM WORN. REMOVED AND REPSDR O2GA2023032782001Valve · intermittentAT FL310 RIGHT ENGINE OIL TEMPERATURE EXCEEDED 99* CELSIUS FOR MORE THAN 10 MINUTES. PEAKED AT 102* CELSIUS AND WAS STABLE AT 101* CELSIUS WHEN THE RIGHT THROTTLE WAS REDUCED TO IDLE. AT BELOW FL180 THE ENGINE OIL TEMPERATURE RETURNED TO NORMAL RANGE. ENGINE OSDR O2GA2015062482001Fuel Cell · leakingUPON SHUTDOWN POST FLIGHT FUEL LEAK DISCOVERED FROM RT ENG NACELLE. REPLACED THE RT FUEL CELL. LEAK CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.SDR O2GA2015030282001Accumulator · defectiveDEPARTED, SHORTLY AFTER LEVELING OFF AT FL 250, HYD FLUID LOW, CAUTION ANNUNCIATOR ILLUMINATED. FOLLOWED CHECKLIST & CONTINUED TO DESTINATION. DURING NEXT SEVERAL MINUTES CREW HEARD GEAR PUMP MOTOR CYCLING FOLLOWED BY LG RELAY CB EXTENDED. DURING APPROACH LSDR O2GA2014112482001Unknown · smokeBEFORE TAXIING CREW EXPERIENCED SMOKE ENTERING THE CABIN AFTER ENG START. SMOKE WENT AWAY WHEN RT ENG BLEED AIR WAS TURNED OFF. CREW IMMEDIATELY SHUTDOWN THE ENG. PERFORMED ENG RUNS WITH CREW. ENG BLEED & ENVIRONMENTAL SYS WAS OPERATED & NO DEFECTS WERE NOSDR O2GA2014090282001Sense Line · faultyDURING CLIMB THE RT ENG BLEED FAIL ANNUNCIATOR LIGHT CAME ON. ACCOMPLISHED THE BLEED AIR FAILURE CHECKLIST THEN REQUESTED CLEARANCE TO LAND. LANDING WAS UNEVENTFUL. TROUBLE SHOT THE DISCREPANCY & FOUND A FAULTY RT BLEED AIR SENSE LINE. SENSE LINE WAS REPLA
STCs that may be installed · 428
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beechcraft B300
STC SA03025CHInstallation of weather research equipment and weather modification equipment for the purpose of modifying weather conditionsSTC SA04617NYInstallation of the Medivac Audio SystemSTC SA04218NYInstallation of Wing Tip Low Profile Pylons with Pods, Underwing Wiring Tunnel and Optional Underwing Antenna Provisions and Antennas