# Textron 750

- Type: Aircraft model (FAA registry)
- Registry code: 2076820
- Manufacturer (registry): TEXTRON AVIATION INC
- Model: 750
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 12
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS T00007WI](https://openairdocs.org/tcds/T00007WI) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 15
- Page: https://openairdocs.org/model/textron-750

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2013-04-03](https://openairdocs.org/ad/2013-04-03): Pitot/Static Anti-Ice System · Cessna 750. Effective Apr 11, 2013
- [AD 2012-18-16](https://openairdocs.org/ad/2012-18-16): Electrical power · Cessna 750. Effective Oct 24, 2012
- [AD 2011-03-16](https://openairdocs.org/ad/2011-03-16): Electrical power · Cessna 750. Effective Mar 22, 2011
- [AD 2010-20-10](https://openairdocs.org/ad/2010-20-10): Flight Controls · Cessna 750. Effective Nov 1, 2010
- [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007
- [AD 2006-24-01](https://openairdocs.org/ad/2006-24-01): Auxiliary power unit (APU) fuel tube assembly · Cessna 750. Effective Dec 6, 2006
- [AD 98-16-17 R1](https://openairdocs.org/ad/98-16-17-R1): Secondary horizontal stabilizer · Textron 750. Effective Oct 23, 2003
- [AD 2002-23-05](https://openairdocs.org/ad/2002-23-05): Circuit Breakers for the Auxiliary Hydraulic Pump System and the King KHF 950 High Frequency Communication System(s) · Cessna 750. Effective Dec 26, 2002
- [AD 2001-07-04](https://openairdocs.org/ad/2001-07-04): Roll Control System · Cessna 750. Effective May 15, 2001
- [AD 98-05-02](https://openairdocs.org/ad/98-05-02): Aileron Feel Cartridge Assembly Shaft · Cessna 750. Effective Mar 16, 1998

Historical (superseded or no longer in force):

- [AD 2006-23-05](https://openairdocs.org/ad/2006-23-05) (historical): Inboard- hinge brackets · Cessna 750. Effective Nov 22, 2006
- [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006
- [AD 2005-09-01](https://openairdocs.org/ad/2005-09-01) (historical): Auxiliary power unit (APU) fuel tube assembly · Cessna Aircraft Company, The 750. Effective May 10, 2005
- [AD 98-16-17](https://openairdocs.org/ad/98-16-17) (historical): Secondary Horizontal Stabilizer Trim Actuator · Cessna Aircraft Company, The 750. Effective Aug 24, 1998

## Information bulletins (advisory) (8)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010
- [SAIB NM-10-45](https://openairdocs.org/saib/NM-10-45): Landing Gear: Nose/Tail Landing Gear Attach Section. Issued Aug 11, 2010
- [SAIB CE-10-29R1](https://openairdocs.org/saib/CE-10-29R1): Lights  Aft Side Ledger Divider Light. Issued May 21, 2010
- [SAIB CE-10-29](https://openairdocs.org/saib/CE-10-29) (historical): Lights  Aft Side Ledger Divider Light. Issued Apr 28, 2010
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010

## Registered aircraft (15)

- [N10HH](https://openairdocs.org/aircraft/N10HH): [Transwestern Transports LLC](https://openairdocs.org/faa-owner/TRANSWESTERN%20TRANSPORTS%20LLC), [Baker, MT](https://openairdocs.org/faa-place/MT/Baker), built 2018, S/N 750-0530
- [N255FP](https://openairdocs.org/aircraft/N255FP): [Ufp Industries Inc](https://openairdocs.org/faa-owner/UFP%20INDUSTRIES%20INC), [Grand Rapids, MI](https://openairdocs.org/faa-place/MI/Grand%20Rapids), built 2017, S/N 750-0527
- [N387SL](https://openairdocs.org/aircraft/N387SL): [Indigo Rio Management LLC](https://openairdocs.org/faa-owner/INDIGO%20RIO%20MANAGEMENT%20LLC), [Corona, CA](https://openairdocs.org/faa-place/CA/Corona), built 2017, S/N 750-0524
- [N3B](https://openairdocs.org/aircraft/N3B): [Going Up LLC](https://openairdocs.org/faa-owner/GOING%20UP%20LLC), [Stockton, CA](https://openairdocs.org/faa-place/CA/Stockton), built 2015, S/N 750-0521
- [N427TF](https://openairdocs.org/aircraft/N427TF): [G3 Aviation LLC](https://openairdocs.org/faa-owner/G3%20AVIATION%20LLC), [Cranston, RI](https://openairdocs.org/faa-place/RI/Cranston), built 2018, S/N 750-0528
- [N478PM](https://openairdocs.org/aircraft/N478PM): [Air Reese LLC](https://openairdocs.org/faa-owner/AIR%20REESE%20LLC), [Cypress Mill, TX](https://openairdocs.org/faa-place/TX/Cypress%20Mill), S/N 750-0518
- [N520CX](https://openairdocs.org/aircraft/N520CX): [N520cx Aviation LLC](https://openairdocs.org/faa-owner/N520CX%20AVIATION%20LLC), [Taylor, LA](https://openairdocs.org/faa-place/LA/Taylor), built 2015, S/N 750-0520
- [N587SL](https://openairdocs.org/aircraft/N587SL): [Nutramax Laboratories Consumer Care Inc](https://openairdocs.org/faa-owner/NUTRAMAX%20LABORATORIES%20CONSUMER%20CARE%20INC), [Lancaster, SC](https://openairdocs.org/faa-place/SC/Lancaster), built 2017, S/N 750-0526
- [N61FN](https://openairdocs.org/aircraft/N61FN): [Aluma-Form Inc](https://openairdocs.org/faa-owner/ALUMA-FORM%20INC), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2016, S/N 750-0503
- [N628RP](https://openairdocs.org/aircraft/N628RP): [Global Services Detroit LLC](https://openairdocs.org/faa-owner/GLOBAL%20SERVICES%20DETROIT%20LLC), [Detroit, MI](https://openairdocs.org/faa-place/MI/Detroit), built 2018, S/N 750-0532
- [N743DB](https://openairdocs.org/aircraft/N743DB): [Dhb Leasing Co](https://openairdocs.org/faa-owner/DHB%20LEASING%20CO), [Waukesha, WI](https://openairdocs.org/faa-place/WI/Waukesha), built 2016, S/N 750-0525
- [N751EA](https://openairdocs.org/aircraft/N751EA): [Santa Fe Aviation LLC](https://openairdocs.org/faa-owner/SANTA%20FE%20AVIATION%20LLC), [Rancho Santa Fe, CA](https://openairdocs.org/faa-place/CA/Rancho%20Santa%20Fe), built 2017, S/N 750-0529
- [N75EG](https://openairdocs.org/aircraft/N75EG): [Kirby-Smith Machinery Inc](https://openairdocs.org/faa-owner/KIRBY-SMITH%20MACHINERY%20INC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 2016, S/N 750-0523
- [N8168](https://openairdocs.org/aircraft/N8168): [Wings Jet Flight Training LLC](https://openairdocs.org/faa-owner/WINGS%20JET%20FLIGHT%20TRAINING%20LLC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita), built 2018, S/N 750-0531
- [N98EF](https://openairdocs.org/aircraft/N98EF): [Ellman Aviation LLC](https://openairdocs.org/faa-owner/ELLMAN%20AVIATION%20LLC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 2016, S/N 750-0522

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (2,733, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR WNDA202610120827](https://openairdocs.org/sdr/WNDA202610120827), Oct 10, 2026: HYDRAULIC LINE. LEAKING. FIRST OFFICER AND SIC WERE CONDUCTING A REPOSITION FLIGHT FROM KGKY TO KADS. ON APPROACH AND CONFIGURED AIRCRAFT FOR LANDING, AN EICAS MESSAGE INDICATED HYD QTY
- [SDR AJXA2026100600049](https://openairdocs.org/sdr/AJXA2026100600049), Oct 5, 2026: YAW DAMPER. FAILED. CASS MESSAGE "YD FAIL UPPER A" AFTER TAKOFF. AFTER TAKING OFF FROM KMDW WITH THE CASS MESSAGE THE PILOTS RETURNED TO KMDW. ONCE THE PILOTS WERE ON THE GROUND TH
- [SDR AJXA2026092500048](https://openairdocs.org/sdr/AJXA2026092500048), Sep 21, 2026: FLAP SYSTEM. WARNING MESSAGE. PILOT REPORTED AMBER CAS MESSAGE FLAP FAIL AND DIVERTED TO KIAH
- [SDR AJXA2026091700047](https://openairdocs.org/sdr/AJXA2026091700047), Sep 13, 2026: TIRE. WORN. PILOT ABORTED TAKEOFF DUE TO SEVERE VIBRATION ON NLG.
- [SDR AJXA2026090300046](https://openairdocs.org/sdr/AJXA2026090300046), Sep 1, 2026: YAW DAMPER. FAULTED. YAW DAMPER OFF, MACH TRIM OFF AT 50 KNOTS / FGC ADC MIS-COMPARE AUTOPILOT DISENGAGED
- [SDR 19MA20260707001](https://openairdocs.org/sdr/19MA20260707001), Jul 6, 2026: A/C PACK. OVERHEATED. CABIN PACK OVERHEAT CAS MESSAGE ACCOMPANIED WITH AN ASSOCIATED SLOW DEPRESSURIZATION OF THE CABIN; EMERGENCY DECENT PROCEDURE WAS PERFORMED WITH CABIN ALTITUDE 
- [SDR AJXA2026051100044](https://openairdocs.org/sdr/AJXA2026051100044), May 11, 2026: BUSHING. WORN. DURING TAKEOFF ROLL AIRCRAFT EXPERIENCED VIBRATION IN THE NOSE LANDING GEAR / YAW DAMPER LOWER OFF AMBER MESSAGE
- [SDR AJXA2026051500045](https://openairdocs.org/sdr/AJXA2026051500045), May 5, 2026: HINGE. BROKEN. DURING FLIGHT PILOTS REPORTED AN AMBER CASS MESSAGE FUEL DOOR OPEN AND THEY ALSO EXPERIENCED VIBRATION DURING THE FLIGHT. SINGLE POINT DOOR HINGE FOUND BROKEN. 
- [SDR 2026FA0000276](https://openairdocs.org/sdr/2026FA0000276), Apr 17, 2026: HYDRAULIC LINE. RUPTURED. JUST AFTER TAKE OFF OUT OF KTLI, AT POSITIVE RATE AND SELECTED GEAR UP, AT THE MOMENT THE CREW GOT INDICATION OF HYDRAULIC A QUANTITY DROPPING, THEY IMMEDIATELY
- [SDR 2026FA0000247](https://openairdocs.org/sdr/2026FA0000247), Apr 1, 2026: PUMP. FAULTED. DURING FLIGHT IAD TO SDL WITH OWNER ON-BOARD AND THEY LOST HYD A FLUID IN FLIGHT. THE INDICATOR WENT DOWN TO %9 FAST. THE PILOT PULLED THE PTU CB. DECLARED AN E
- [SDR R3WA20260429001](https://openairdocs.org/sdr/R3WA20260429001), Mar 19, 2026: PULLEY BRACKET. CHAFED. DURING SCHEDULED MAINTENANCE, A DETAILED VISUAL INSPECTION OF THE RUDDER CONTROL SYSTEM DISCOVERED A RUDDER CONTROL CABLE RUBBING AGAINST A PULLEY BRACKET WHICH
- [SDR AJXA2026030900043](https://openairdocs.org/sdr/AJXA2026030900043), Mar 8, 2026: ACTUATOR. LEAKING. PILOT REPORTS HYDRAULIC SYSTEM A LOW
- [SDR CVGA20260207001](https://openairdocs.org/sdr/CVGA20260207001), Feb 6, 2026: COUPLING. LEAKING. ABORTED TAKE OFF DUE TO A LEFT ENGINE PYLON BLEED LEAK CAS MESSAGE AND SMOKE IN THE COCKPIT/ CABIN. UPON INVESTIGATION THE LT ENGINE OTBD PRECOOLER V-BAND COUPL
- [SDR AJXA2026020500042](https://openairdocs.org/sdr/AJXA2026020500042), Jan 31, 2026: RVDT. PILOT ERROR. PILOT REPORTED YAW DAMPER UPPER A FAIL CYAN EICAS MESSAGE IMMEDIATELY AFTER TAKEOFF. THE PILOT ALSO REPORTED AN OVERSPEED MESSAGE WHICH WAS DETERMINED TO BE CAU
- [SDR AJXA2026013000041](https://openairdocs.org/sdr/AJXA2026013000041), Jan 30, 2026: STRUT. DISCHARGED. AFTER TAKEOFF, THE PILOT ATTEMPTED TO RETRACT THE LANDING GEAR AND THE LAND GEAR DID NOT RETRACT. THE NOSE LANDING GEAR WAS SERVICED. GEAR AND GEAR RETRACTION O
- [SDR 4USA2026F00000](https://openairdocs.org/sdr/4USA2026F00000), Dec 27, 2025: FLAP SYSTEM. FAULT MESSAGE. DURING APPROACH INTO KBZN WHILE ATTEMPTING TO LOWER THE FLAPS TO 5 DEGREES, GOT THE "FLAP FAIL" MESSAGE. FLAP SYSTEM INSPECTED AND FOUND BIT CODES 2, 5 & 8 ON F
- [SDR AJXA2025122300040](https://openairdocs.org/sdr/AJXA2025122300040), Dec 20, 2025: WHEEL. VIBRATION. THERE WAS VIBRATION ON THE NOSE GEAR APPROACHING 80 KNOTS
- [SDR 1JAA2025121800016](https://openairdocs.org/sdr/1JAA2025121800016), Dec 16, 2025: FLEX HOSE. BLEW OUT. LOSS OF SYSTEM A HYDRAULICS RESULTING IN AN EMERGENCY LANDING. UPON LANDING INSPECTION REVEALED A 3000PSI HYDRAULIC LINE JUST AFT OF GEAR HAD BLOWN OUT AND DUMP
- [SDR 4USA2025121100820](https://openairdocs.org/sdr/4USA2025121100820), Dec 8, 2025: STRUT. LOW PRESSURE. AIRCRAFT TOOK OFF, GEAR RETRACTED, ALL NORMAL. AT ABOUT 40K FT, CAPTAIN HEARD A LOUD THUD & THE NOSE GEAR UNLOCK INDICATION CAME ON. CREW REPORTED RESISTANCE FR
- [SDR AJXA2025112100039](https://openairdocs.org/sdr/AJXA2025112100039), Nov 21, 2025: RUDDER. MALFUNCTIONED. THE CREW REPORTED THAT AFTER 50 MINUTES THE RUDDER TRIM BEGAN TO TURN TO THE LEFT & THEN TO THE RIGHT
- [SDR AJXA2025111800038](https://openairdocs.org/sdr/AJXA2025111800038), Nov 14, 2025: ACTUATOR. MALFUNCTIONED. THE PILOT REPORTED UPON DEPARTURE WHETHER TURNING RIGHT OR LEFT, THE UPPER RUDDER / AIRCRAFT SWAYED LEFT AND RIGHT BEFORE CORRECTING
- [SDR 4USA2025111800762](https://openairdocs.org/sdr/4USA2025111800762), Nov 14, 2025: PROXIMITY SWITCH. DEFECTIVE. AFTER TAKEOFF, CABIN NOT PRESSURIZING. CABIN DOOR OPEN AND CABIN DOOR VENT OPEN MESSAGE APPEARED ON EICAS. CORRECTIVE ACTION: TROUBLESHOT SYSTEM. FOUND DEFECTIV
- [SDR 2025F00269](https://openairdocs.org/sdr/2025F00269), Nov 10, 2025: ISOLATION VALVE. FAULTED. DURING CRUISE CREW HEARD A SMALL MUFFLED POP. IN A FEW SECONDS, GOT A BAGGAGE ALTITUDE CAS MESSAGE. CREW STARTED TO DISCUSS CAS MESSAGE WHILE NOTICING CABIN ALT
- [SDR CVGA20251103001](https://openairdocs.org/sdr/CVGA20251103001), Oct 31, 2025: FLAP SYSTEM. FAILED. FLAPS FAILED AT 5° ON APPROACH INTO KLAS. DECLARED EMERGENCY. REMOVED FAILED FLAP CONTROLLER AND INSTALLED A TESTED FLAP CONTROLLER IAW CE-750 AMM 27-51-00. OPS
- [SDR 3EJA979JS102625](https://openairdocs.org/sdr/3EJA979JS102625), Oct 26, 2025: ROLLER. WORN. CLIMBING THROUGH ABOUT FL340 WE EXPERIENCED A LOUD BANGING NOISE WITH VIOLENT SHAKING. THE BANGING AND NOISE CONTINUED IN RHYTHM AND IN UNISON WITH THE GEAR RED
- [SDR 3EJA202601092125](https://openairdocs.org/sdr/3EJA202601092125), Oct 21, 2025: ELEC CONNECTOR. DIRTY. AFTER TAKEOFF GEAR WAS SELECTED UP. THE RIGHT GEAR INDICATION REMAINED GREEN DURING THE INITIAL CLIMB. CLEANED ELECRICAL CONNECTOR FOR DOWN LOCK SWITCH, OPS CHE
- [SDR AJXA202510200038](https://openairdocs.org/sdr/AJXA202510200038), Oct 20, 2025: ELECTRICAL SYS. FAULTED. PILOT REPORTED A PARTIAL ELECTRICAL FAILURE IN COCKPIT. POWER WAS LOST ON THE COPILOTS MFD AND PFD.
- [SDR AJXA2025101500037](https://openairdocs.org/sdr/AJXA2025101500037), Oct 12, 2025: AOA. FAILED. PILOTS ANGLE OF ATTACK FAILED. MAINTENANCE PERFORMED BIT TEST OF AOA COMPUTER AND COULD NOT DUPLICATE THE FAULT.AIRCRAFT WAS RETURNED TO SERVICE AND HASS COMPLE
- [SDR 2025FA0000686](https://openairdocs.org/sdr/2025FA0000686), Oct 6, 2025: LANDING GEAR. FAULTED. LANDING GEAR WOULD NOT COME DOWN OR GIVE INDICATION IT WAS . I OPTED FOR THE LONGER RUNWAY AT PBI , WE USED THE EMERGENCY GEAR EXTENSIONS AND LANDED NORMAL.
- [SDR 3EJA2025102400006](https://openairdocs.org/sdr/3EJA2025102400006), Sep 29, 2025: SENSOR. FAILED. AMBER "STAB A/I HOT R" CAS MSG AFTER T/O. WITH A/I ALL OFF. MSG REMAINED UNTIL ENGINE SHUT DOWN. REMOVED FAILED RH STAB ANTI ICE SENSOR TH006 AND REPLACED WITH 
- [SDR 2025FA0000655](https://openairdocs.org/sdr/2025FA0000655), Sep 17, 2025: WHEEL. ABNORMAL. NOSE WHEEL SHIMMY, GEAR COLAPS UPON STOPING
- [SDR 2025FA0000656](https://openairdocs.org/sdr/2025FA0000656), Sep 14, 2025: HYDRAULIC LINE. LEAKING. PILOT REPORTED: ON TAKEOFF AT KPHL, WE LOST A SYSTEM HYDRAULICS WHEN RAISING THE GEAR. LOST VOLUME ON THE A SIDE. WE LANDED AT KPNE AFTER RUNNING APPROPRIATE EM
- [SDR 2025FA0000654](https://openairdocs.org/sdr/2025FA0000654), Sep 7, 2025: HYDRAULIC LINE. RUPTURED. A SIDE HYDRAULIC BLOW OUT IN FLIGHT
- [SDR AJXA2025090800037](https://openairdocs.org/sdr/AJXA2025090800037), Sep 5, 2025: TUBE. RUPTURED. DURING CLIMB PILOT RECEIVED EICAS MESSAGE "PAC HP VLV OPN L-R"
- [SDR AJXA2025090200036](https://openairdocs.org/sdr/AJXA2025090200036), Aug 29, 2025: DAU. MALFUNCTIONED. FLAP FAILED DURING TAKE OFF, UNABLE TO RETRACT / DAU 2A FAIL
- [SDR CVGA20250902001](https://openairdocs.org/sdr/CVGA20250902001), Aug 27, 2025: RELAY. FAILED. FLAPS FAIL CAS MESSAGE ON DEPARTURE. EMERGENCY DECLARED. REMOVED AND REPLACED FLAP RELAY BOX ASSEMBLY IAW CESSNA 750 MM 27-51-00. OPERATIONAL CHECK PASSED, REMO
- [SDR 4USA2025081800547](https://openairdocs.org/sdr/4USA2025081800547), Aug 16, 2025: HYDRAULIC LINE. CHAFED. CREW REPORTED HYDRAULIC SYSTEM A LOW QUANTITY DURING FLIGHT FROM TEB TO PBI. CREW FOLLOWED CHECKLIST AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND 2 HYDRA
- [SDR 2025FA0000653](https://openairdocs.org/sdr/2025FA0000653), Aug 13, 2025: GENERATOR. BOWED. LOST EVERYTHING ON THE RIGHT SIDE. INCLUDING MACH TRIM FEDEC FAULTS FIVE INDICATIONS. DAU FAILS, TRIM FAIL.
- [SDR AJXA2025090200035](https://openairdocs.org/sdr/AJXA2025090200035), Aug 9, 2025: ANTI-ICE VALVE. UNSERVICEABLE. DURING TAKEOFF ROLL STAB ANTI ICE AMBER CAS MESSAGE ILLUMINATED.
- [SDR AJXA2025090200034](https://openairdocs.org/sdr/AJXA2025090200034), Aug 9, 2025: OVERHEAT SENSOR. FAULTY. DURING TAKEOFF ROLL THE STAB ANIT ICE HOT LEFT AMBER CAS MESSAGE ILLUMINATED.
- [SDR 3EJA20250825001](https://openairdocs.org/sdr/3EJA20250825001), Aug 8, 2025: CONTROLLER. FAULTED. CLIMBING THROUGH 4000 FT. OUT OF MYNN AMBER CABIN ALTITUDE MESSAGE ILLUMINATED. AT 10,000 FEET RED CABIN ALTITUDE ILLUMINATED. LITTLE NEEDLE ON PRESSURIZATION N
- [SDR CVGA20250801001](https://openairdocs.org/sdr/CVGA20250801001), Jul 29, 2025: SEAL. FAULTED. AIRCRAFT FAILED TO PRESSURIZE DURNING CLIMB - THE PRESSURIZATION ISSUE WAS CAUSED BY THE DOOR HANDLE NOT BEING PROPERLY CLOSED AND THE DOOR SEAL NOT INFLATING. 
- [SDR 4USA2025072100510](https://openairdocs.org/sdr/4USA2025072100510), Jul 19, 2025: GENERATOR. FAILED. DURING CRUISE, CREW REPORTED “GEN FAIL R”. APPROXIMATELY 5-10 MINUTES LATER, IT WAS FOLLOWED BY “OIL LEVEL LOW R”. ABOUT 5 MINUTES LATER, THE CAPTAIN NOTICED TH
- [SDR AJXA2025071600032](https://openairdocs.org/sdr/AJXA2025071600032), Jul 12, 2025: GCU. UNSERVICEABLE. DURING FLIGHT AT FL450 AIRCRAFT LOST POWER ON EICAS DISPLAY UNITS, 1 ,2, AND 3 CAUSED DUE TO A POWER LOSS ON THE NR 1 POWER BUSS. THE LOSS OF ONE THE NR 1 BUSS 
- [SDR AJXA2025072100033](https://openairdocs.org/sdr/AJXA2025072100033), Jul 7, 2025: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB EICAS AMBER CAS MESSAGE "CABIN ALTITUDE" ILLUMINATED. THE PRESSURIZATION SYSTEM WAS PLACED ON MEL AND FLOWN TO MAINTENANCE IN KOAK. ONCE IN MAINTEN
- [SDR 3EJA928JS070425](https://openairdocs.org/sdr/3EJA928JS070425), Jul 4, 2025: CABIN PRESSURE. LOST. LOST PRESSURIZATION AT FL240. NOTIFIED ATC AND REQUESTED A DECENT.
- [SDR CVGA20250519002](https://openairdocs.org/sdr/CVGA20250519002), May 14, 2025: CONTROL HANDLE. DIRTY. AMBER FLAP FAIL CAS DURING CLIMB THROUGH FL390 WOULD NOT RESET. SLATS WERE AVAILABLE - REMOVED FLAP HANDLE CLEANED DUST OUT OF INSIDE WITH A SMALL AMOUNT OF AIR
- [SDR LDIA2025051400001](https://openairdocs.org/sdr/LDIA2025051400001), May 12, 2025: GENERATOR. DESTROYED. DC GENERATOR BEARING FAILED CAUSING GENERATOR TO PARTIALLY DISINTEGRATE AND BECOME DETACHED FROM ITS DRIVE PAD. DURING THE FAILURE THE FIRE LOOP WAS STRUCK CAUS
- [SDR AJXA2025050100031](https://openairdocs.org/sdr/AJXA2025050100031), Apr 27, 2025: SEAL. WORN. DURING FLIGHT THE AMBER CABIN DOOR SEAL CAME ON CAUSING A WHISTLING SOUND AND ULTIMATELY CREATED DIFFICULTY IN MAINTAINING PROPER CABIN PRESSURIZATION.
- [SDR AJXA2025033000029](https://openairdocs.org/sdr/AJXA2025033000029), Mar 30, 2025: GPWS. WARNING MESSAGE. PILOT REPORTED A EGPWS AND WIND SHEAR FAIL EICAS MESSAGE

All 2,733: https://openairdocs.org/model/textron-750/reports.md

## STCs that may be installed (OpenAirDocs) (73, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification 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. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04578CH](https://openairdocs.org/stc/ST04578CH): Installation of SmartSky system. Apcela ATG
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST04269AT](https://openairdocs.org/stc/ST04269AT): Installation of Send Solutions, LLC Airtext Messaging System which connects the passengers phones and portable electronic devices via Bluetooth to provide the passengers with in-flight messaging service via the Iridium Satellite Communication Network. Send Solutions LLC
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST11873SE](https://openairdocs.org/stc/ST11873SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST12016IB](https://openairdocs.org/stc/ST12016IB): Installation of Gogo AVANCE L5/LX5. Sky Service F.B.O Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC
- [STC ST04519CH](https://openairdocs.org/stc/ST04519CH): Installation of a Honeywell FANS-1/A+ Datalink Communications System in accordance with West Star Aviation Master Data List, Doc. No. A21311L-658, Revision A, dated November 3, 2021, or later FAA-approved revision. West Star Aviation
- [STC SA04518CH](https://openairdocs.org/stc/SA04518CH): Installation of a Honeywell Flight Management System Software Update to version NZ 6.2.1 in accordance with West Star Aviation Master Data List, Doc. No. A21312L-652, Revision I/R, dated October 4, 2021, or later FAA-approved revision. West Star Aviation
- [STC ST02715SE](https://openairdocs.org/stc/ST02715SE): Installation of the Honeywell RDR-7000 Volumetric Buffer Weather Radar System. Honeywell International Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST01950WI](https://openairdocs.org/stc/ST01950WI): Installation of Gogo Business Aviation AVANCE L5 Broadband. Duncan Aviation Inc
- [STC ST01942WI](https://openairdocs.org/stc/ST01942WI): Installation of Garmin G5000 System Release v4.5. Wichita Citation Center
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST00954DE](https://openairdocs.org/stc/ST00954DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST01859WI](https://openairdocs.org/stc/ST01859WI): Installation of Gogo Business Aviation's Gogo Biz 4G Air-to-Ground System. Textron Aviation Inc Wichita Citation Service Center
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST02119LA](https://openairdocs.org/stc/ST02119LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST00135BO](https://openairdocs.org/stc/ST00135BO): Modification of Honeywell TCAS II system installation with R/T 910 and software Version 6.4a to R/T 910 with Change 7.0 software; or TCAS 2000 system with R/T 950, 951 and software Version 6.4a to R/T 950, 951 with Change 7.0 software. Pro Star Aviation, LLC
- [STC ST04146NY](https://openairdocs.org/stc/ST04146NY): Upgrade for ADS-B Out capability on aircraft equipped with Primus II Radio Suites. 328 Support Services GmbH
- [STC ST01720WI](https://openairdocs.org/stc/ST01720WI): Installation of a Safe Flight Instrument Corporation Auto Throttle System. Textron Aviation Inc
- [STC ST03271CH](https://openairdocs.org/stc/ST03271CH): Upgrade existing Honeywell Mark V Enhanced Ground Proximity Warning System software level and activate the Runway Awareness Advisory System (including enhanced features known as SmartRunway SmartLanding). Textron Aviation Inc
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST04194CH](https://openairdocs.org/stc/ST04194CH): Install Honeywell Liquid Crystal Display (LCD) Flight Displays. Pentastar Aviation LLC
- [STC ST03957AT](https://openairdocs.org/stc/ST03957AT): Activation of Aircell Axxess Cabin Telecommunications Router (CTR) Wireless Local Area Network (WLAN) in accordance with Constant Aviation LLC, Master Drawing List DB1107001, Revision IR, dated December 9, 2011, or later FAA approved revision. Nextant Aerospace
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01545WI](https://openairdocs.org/stc/ST01545WI): Installation of winglets, wing structural reinforcement, and related system changes. Winglet Technology LLC
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST00796DE](https://openairdocs.org/stc/ST00796DE): Installation of Teledyne Battery Products P/N 7638-44T Lead-Acid Battery. Teledyne Battery Products
- [STC ST01399WI](https://openairdocs.org/stc/ST01399WI): Installation of Honeywell DL-950 Data Loader. Textron Aviation Inc
- [STC SA04006CH](https://openairdocs.org/stc/SA04006CH): Installation of Fuel Vent Scoop. Textron Aviation Inc
- [STC ST02127LA](https://openairdocs.org/stc/ST02127LA): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc

All 73: https://openairdocs.org/model/textron-750/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Cessna 750](https://openairdocs.org/model/cessna-750): 271 registered aircraft, registry code 2076810
- [Charles A Miranda 750](https://openairdocs.org/model/charles-a-miranda-750): 1 registered aircraft, registry code 0563889
- [Cessna 750](https://openairdocs.org/model/cessna-750): 1 registered aircraft, registry code 2076809

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