- Registered owner
- Textron Aviation Inc
- Location
- Wichita, KS
- Owner type
- Corporation
- Serial number
- 680-0004
- Year built
- 2004
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 30, 2016
- Certificate issued
- September 30, 2024
- Expires
- September 30, 2031
- Mode S code
- A00F7D
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1998 | 1 |
| 2005 | 3 |
| 2008 | 1 |
| 2012 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2023 | 1 |
| 2026 | 1 |
Airframe · Cessna 680
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2018-07-13Landing GearAD 2017-06-13FuselageAD 2012-07-04Electrical PowerAD 2007-26-16Aft fairing wire bundle assemblyAD 2005-18-20"FASTprop" propeller de-icersAD 2005-08-03Cockpit display unitsAD 2005-01-19Mode S transpondersAD 98-14-03TranspondersAD 78-05-06Flexible Fuel CellsInformation bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N1027PMatched 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 Cessna 680 aircraft
FAA incident reports
No FAA accident or incident reports matched to N1027PMatched 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 Cessna 680 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2022101212895Pressure Switch · failedTHE FLIGHT CREW REPORTED AN AMBER CAS MESSAGE "HP VALVE FAIL R" ILLUMINATED ON EICAS AFTER LANDING AND REMAINED ILLUMINATED UNTIL SHUTDOWN. THE MAINTENANCE PROVIDER TROUBLESHOT AND DETERMINED THE RIGHT ENGINE HP BLEED DIFFERENTIAL PRESSURE SWITCH HAD FAILED. TSDR 9JLA2022100712894Actuator · faultedTHE FLIGHT CREW REPORTED THAT THE RUDDER TRIM INDICATOR WAS NOT INDICATING FULL TRAVEL. THE MAINTENANCE PROVIDER FOUND THE TRIM INDICATOR WAS STOPPING OUTSIDE THE GREEN ARE WHEN MOVED TO THE RIGHT. THEY THEN CONFIRMED THAT THE TRIM ACTUATOR WAS NOT MOVING FULLSDR 9JLA2022091212890Carbon Seal · faultedFLIGHT CREW REPORTED THAT DURING FLIGHT OF OBSERVING SMOKE IN THE CABIN, THE CREW RAN THE CHECKLIST, DONNED OXYGEN MASKS AND ISOLATED THE BLEAD AIR SOURCE TO THE NO1 ENGINE. SMOKE DIMINISHED. APPROACH AND LANDING WAS UNEVENTFUL. THE MAINTENANCE PROVIDER TROUBLSDR 9JLA2022031412867Actuator · defectiveCREW REPORTED RUDDER BIAS CHECK - UNSATISFACTORY, NO CHANGE IN RUDDER PEDAL WITH ENGINE POWER UP LEFT OR RIGHT. THE MAINTENANCE VENDOR DETERMINED THE RUDDER BIAS ACTUATOR WAS DEFECTIVE AND REQUIRED TO BE REPLACED WITH AN OVERHAULED UNIT. OPS CHECKS SATISFACTORSDR 9JLA2021113017650Drive Unit · faultedTHE FLIGHT CREW REPORTED THAT DURING DESCENT FOR LANDING THE FLAP SYSTEM STOPPED EXTENSION BETWEEN THE 15 AND 35 POSITION. THE APPROACH AND LANDING WAS UNEVENTFUL. THE MAINTENANCE TEAM DETERMINED THE FLAP DRIVE WAS AT FAULT. THE FLAP DRIVE UNIT WAS REMOVED ANDSDR 9JLA2021093017627Valve · faultedTHE FLIGHT CREW REPORTED THE LOSS OF ENGINE OIL PRESSURE ON THE NO2 ENGINE DURING THE DOWNWIND LEG OF THE APPROACH FOR LANDING. THE FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY SHUTDOWN OF THE NO2 ENGINE. THE APPROACH AND LANDING WAS UNEVENTFUL. NO PASSENGERS WERESDR 9JLA2021080317622Sensor · faultedFLIGHT CREW A "PITOT/STATIC COLD - R" MESSAGE DISPLAYED. THE MAINTENANCE VENDOR TROUBLESHOT AND FOUND THE RIGHT PITOT HEAT CURRENT SENSOR FAULTY. THE SENSOR WAS REMOVED AND A NEW SENSOR INSTALLED. ALL WORK AND GROUND FUNCTIONAL CHECKS WERE SATISFACTORY. THE AISDR 9JLA2021020417606Detector · failedTHE FLIGHT CREW REPORTED THAT DURING PREFLIGHT CHECKS THE RIGHT WING BLEED CHECK FAILED DURING THE ROTARY TEST. THE MAINTENANCE VENDOR DETERMINED THAT THE RIGHT WING BLEED LEAK DETECTOR UNIT FAILED. THE DETECTOR UNIT WAS REMOVED AND REPLACED WITH NEW. OPS CHECSDR 9JLA2018071300001Frame · crackedDURING A ROUTINE DOCUMENT INSPECTION THE MAINTENANCE VENDOR DISCOVERED A CRACKED FRAME AT FS 72 IN THE NOSE LANDING GEAR WHEEL WELL TUNNEL. DURING THE REMOVAL OF THE CRACKED FRAME SECTION, THEY IDENTIFIED OTHER CRACKS IN A DOUBLER ASSOCIATED WITH THE FS 72 SEC
STCs that may be installed · 50
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 680
STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher
Earlier aircraft with this N-number · 1
This aircraft carried N1027P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.