# N750NA: 2000 Cessna 750 - Status: Valid registration - Airframe: [Cessna 750](https://openairdocs.org/model/cessna-750) (registry code 2076810, 12 seats) - Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028) - Data sheets: [TCDS T00007WI](https://openairdocs.org/tcds/T00007WI) (Textron Aviation Inc.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs) - Serial number: 750-0104 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 31, 2000 - Certificate issued: February 14, 2013 - Expires: February 28, 2029 - Mode S code: AA1B36 - Registered owner: [N A Citation (2012) LLC](https://openairdocs.org/faa-owner/N%20A%20CITATION%20(2012)%20LLC) - Location: [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach) - Owner type: LLC - Owner's area on the map: 26.7158° N, 80.0668° W: Placed by OpenAirDocs at the center of ZIP code 33401, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=750NA - Page: https://openairdocs.org/aircraft/N750NA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Allison AE3007C model are included. ## ADs that may apply (OpenAirDocs): 24 in force ### Matched by airframe (Cessna 750) - [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 ### Matched by engine (Allison AE3007C series) - [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018 - [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017 - [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015 - [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009 - [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008 - [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002 - [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001 - [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001 - [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000 - [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000 - [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000 - [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 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 - [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000 - [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999 ## Information bulletins (advisory) (6 in force) - [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021 - [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011 - [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 NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010 - [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011 - [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021 - [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010 - [SAIB CE-10-29](https://openairdocs.org/saib/CE-10-29) (historical): Lights Aft Side Ledger Divider Light. Issued Apr 28, 2010 ## NTSB investigations None matched to N750NA. ## FAA accident and incident reports None matched to N750NA. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N750NA not matched to an aircraft (104, newest 50) They name N750NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR NOCA201110210611](https://openairdocs.org/sdr/NOCA201110210611), Oct 21, 2011: WIRE. LOOSE. ACFT ABORTED TAKEOFF DUE TO LEFT ENGINE BLEED FAULT LIGHT AND EICAS MESSAGE DISPLAYED MOMENTARILY . ACCOMPLISHED VISUAL INSPECTION ON BLEED LINES. FOUND GROUND - [SDR NOCA08511](https://openairdocs.org/sdr/NOCA08511), Sep 11, 2011: TRANSCEIVER. INOPERATIVE. AIRCRAFT HAD AN AIR TURNBACK INTO LEJ DUE TO RIGHT WX RADAR FAILED AND LEFT SYSTEM ALREADY PLACARD. REMOVED AND CHECKED BOTH WX TRANSCEIVERS AND CHECKED FOR BEN - [SDR NOCA08411](https://openairdocs.org/sdr/NOCA08411), Sep 8, 2011: LINK ASSY. DEFECTIVE. AIRCRAFT FAILED RUDDER FREEPLAY CHECK AS PER EO 757-27-027 AD 2006-07-23. FOUND LOWER PCA ACTATOR LINK. REMOVED AND REPLACED LINK ASSY AND BUSHING AS PER MM 27- - [SDR NOCA06911](https://openairdocs.org/sdr/NOCA06911), Jul 24, 2011: MODULE. INOPERATIVE. EMERGENCY DECLARED FOR LEFT LANDING GEAR LIGHT FAILED TO ILLUMINATE UPON GEAR HANDLE MOVEMENT TO EXTEND/DOWN POSITION. REPLACED LIGHT MODULE, OPS CHECK NORMAL P - [SDR NOCA06311](https://openairdocs.org/sdr/NOCA06311), Jun 18, 2011: SLIDE. UNWANTED DEPLOY. L4 DOOR EMERGENCY SLIDE DEPLOYED DURING CATERING. REMOVED AND REPLACED L4 DOOR EMERGENCY SLIDE PER NAA TASK CARD 25-66-01-4A, OPS CHECKS NORMAL. - [SDR NOCA02511](https://openairdocs.org/sdr/NOCA02511), Mar 17, 2011: GIRT BAR. LACK OF LUBE. L1 DOOR SLIDE ARM LIGHT STAYS ON WITH DOOR DISARMED. CLEANED AND LUBED GIRT BAR AND OPERATIONAL CHECKED AS PER MM 52-11-25 OPS CHECK GOOD. - [SDR NOCA02011](https://openairdocs.org/sdr/NOCA02011), Mar 15, 2011: LIGHT. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTING IS INOP AT ROW 12-17. RELAMPED FLOOR TRACK LIGHT AT ROW 12-17 PER MM 33-51-11, OPS CHECK GOOD. - [SDR NOCA01911](https://openairdocs.org/sdr/NOCA01911), Mar 15, 2011: WIRE. LOOSE. L4 DOOR EXTERIOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. T/S DOOR EXTERIOR LIGHT AND FOUND CENTER CONDUCTOR WIRE LOOSE AT L56 SOCKET SECURED PER SWPM 20-00-00 - [SDR NOCA01811](https://openairdocs.org/sdr/NOCA01811), Mar 15, 2011: SWITCH. OBSTRUCTED. L1 DOOR SLIDE ARM LIGHT STAYS ON WITH DOOR DISARMED. REMOVED DEBRIS FROM L1 DOOR SLIDE ARM SWITCHES, OPS CHECK GOOD PER MM 25-66-00. - [SDR NOCA01711](https://openairdocs.org/sdr/NOCA01711), Mar 12, 2011: GIRT BAR. OBSTRUCTED. R1 DOOR SLIDE WILL NOT ARM. REMOVED DEBRIS FROM SLIDE GIRT BAR AREA, OPS CHECK NORMAL PER MM 25-66-11. - [SDR NOCA00711](https://openairdocs.org/sdr/NOCA00711), Jan 24, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHTS AREA LIGHT SEAT ROW 14D INOP. RELAMPED EMERGENCY LIGHT ROW 14D AS PER MM 33-51-05, OPS CHECK OK. - [SDR NOCA00611](https://openairdocs.org/sdr/NOCA00611), Jan 24, 2011: BULB. BURNED OUT. EMERGENCY EXIT LIGHT AT L2 DOOR INOP. REPLACED LIGHT AS PER MM 33-51-06, OPS CHECK OK. - [SDR NOCA07110](https://openairdocs.org/sdr/NOCA07110), Jan 2, 2011: LAMP. INOPERATIVE. L1 EMERGENCY LIGHT EXTERIOR INOP. RE-LAMPED EMERGENCY LIGHT, OPS CHECK OK PER AMM 33-51-00. - [SDR NOCA02510](https://openairdocs.org/sdr/NOCA02510), Mar 12, 2010: SUPPORT FITTING. CORRODED. AFT MID LAV, AFT IND LOWER CORNER HAS EVIDENCE OF CORROSION. CLEANED LOWER AFT I/B CORNER OF MID LAV FOUND OUT OF LIMITS IAW B757 AMM 51-00-53. REMOVED LOWER SU - [SDR NOCA02210](https://openairdocs.org/sdr/NOCA02210), Feb 28, 2010: UNKNOWN. MALFUNCTIONED. ON INITIAL TAKEOFF ROLL AT ABOUT 40 KNOTS RT RECIRC FAN ANNUNCIATED FOLLOWED BY RIGHT AND LEFT UTILITY BUSES OFF ON EICAS ABORTED TAKEOFF. ACCOMPLISHED FIM 24-5 - [SDR NOCA01310](https://openairdocs.org/sdr/NOCA01310), Jan 31, 2010: LIGHT. INOPERATIVE. LEFT AFT LAV FLOOR EMERGENCY LIGHT OUT. DEFERRED PER MEL 33-51-3. REPLACED EMERGENCY FLOOR LIGHT ASSY, AS PER MM 33-51-11, OPS CHECK GOOD ITEM CLOSED. - [SDR NOCA06909](https://openairdocs.org/sdr/NOCA06909), Nov 25, 2009: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AT OVERHEAD BIN 1 ABC. REPLACED LIGHT AS PER MM 33-51-05. - [SDR NOCA06709](https://openairdocs.org/sdr/NOCA06709), Nov 25, 2009: LIGHT. BROKEN. EMERGENCY FLOOR PATH LIGHT ASSY LOCK BROKEN AT 26C. REPLACED EMERGENCY FLOOR PATH LIGHT ASSY AS PER MM 33-51-11. - [SDR NOCA06609](https://openairdocs.org/sdr/NOCA06609), Nov 25, 2009: CONNECTOR. LOOSE. EMERGENCY LIGHT INOP L1 DOOR. RESECURED LOOSE CONNECTOR OPS CHECK OK AS PER MM 33-51-05 - [SDR NOCA06509AA](https://openairdocs.org/sdr/NOCA06509AA), Nov 25, 2009: LAMP. BURNED OUT. EMERGENCY LIGHT INOP AT OVERHEAD BIN 1 ABC. REPLACED LIGHT AS PER MM 33-51-05. - [SDR NOCA04709](https://openairdocs.org/sdr/NOCA04709), Jul 31, 2009: AUTOTHROTTLE SYS. MALFUNCTIONED. REJECTED TAKEOFF DUE TO A/T DISCONNECT AND AUTOTHROT DISC EICAS LIGHTS ILLUM WITH A/T ENGAGED IN EPR MODE. THRUST REF MODE DISP ON EICAS AND F/S POINTER DISPLAY - [SDR NOCA04609BB](https://openairdocs.org/sdr/NOCA04609BB), Jul 31, 2009: AUTOTHROTTLE SYS. DISCONNECTED. REJECTED TAKEOFF DUE TO A/T DISCONNECT RTO 90 KNOTS. HIGH ENERGY STOP INSPECTION ACCOMPLISHED/ PLACARD A/T INOP PER MEL 22-30-1, ITEM REMAINS OPEN. - [SDR NOCA03809](https://openairdocs.org/sdr/NOCA03809), Jun 17, 2009: APU. INOPERATIVE. APU INFLT START UNSUCCESSFUL, OK ON GROUND. - [SDR NOCA03609](https://openairdocs.org/sdr/NOCA03609), Jun 9, 2009: APU. MALFUNCTIONED. FLIGHT CREW REPORTED DURING SCHEDULED APU INFLT START APU DID NOT START INFLIGHT. FLIGHT WAS NOT AN ETOPS FLIGHT. OAT (-58 C), ALT FL 390, PEAK EGT 20, 3 ATTEMP - [SDR NOCA03209](https://openairdocs.org/sdr/NOCA03209), May 25, 2009: CHARGER. INOPERATIVE. EMERGENCY LIGHTS INOP ROW 12 ABC- 20 ABC. REPLACED BATTERY CHARGER ASSEMBLY AS PER MM 33-51-07. - [SDR NOCA01409](https://openairdocs.org/sdr/NOCA01409), Mar 23, 2009: FUSE. BLOWN. EXTERIOR EMERGENCY EXIT LIGHT AT DOOR 2R LIGHT IS INOP. REPLACED LIGHT ASSY FUSE AND CLEANED TERMINALS, OPS CHECK GOOD AS PER MM 33-51-00. - [SDR NOCA01109](https://openairdocs.org/sdr/NOCA01109), Mar 8, 2009: EEC. FAULTY. N1/EPR FAILED TO ENGAGE TO THRUST WHEN SELECTED ON TAKEOFF ROLL. RT ENGINE LIMITER MESSAGE ILLUMINATED ON EICAS FOR APPROXIMATELY 3 SECONDS THEN EXTINGUISHED. R - [SDR NOCA00309](https://openairdocs.org/sdr/NOCA00309), Jan 6, 2009: SLIDE. INOPERATIVE. AFTER ENG SHUTDOWN R4 DOOR WAS SLIGHTLY OPENED BY F/A WHILE STILL ARMED. SLIDE DID NOT DEPLOY. ACFT MX FERRY FOR SLIDE REPLACEMENT. REMOVED AND REPLACED DOOR R4 - [SDR NOCA08808](https://openairdocs.org/sdr/NOCA08808), Dec 15, 2008: CHARGER. INOPERATIVE. FLOOR EMERGENCY LIGHTS AT SEATS 7 AND 8 ABC ARE INOP. REPLACED BATTERY AND CHARGER AS PER MM 33-51-07, OPS CHECK OK. - [SDR NOCA09008](https://openairdocs.org/sdr/NOCA09008), Dec 10, 2008: LIGHT. INOPERATIVE. R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT AS PER MM 33-51-07. - [SDR NOCA08908](https://openairdocs.org/sdr/NOCA08908), Dec 10, 2008: BATTERY. DISCHARGED. EMERGENCY OVERHEAD BIN LIGHT INOP AT SEAT 11 DEF. REPLACED THE R2 BATTERY ASSY AS PER MM 33-51-07. - [SDR NOCA08508](https://openairdocs.org/sdr/NOCA08508), Nov 30, 2008: TRANSMITTER. DEFECTIVE. ABNORMAL ENGINE PARAMETERS DURING CRUISE. REMOVED AND REPLACED LEFT ENG EPR TRANSMITTER PER MM 77-11-01 PERFORMED TEST 13 FOUND OK AS PER MM 71-00-00. FOUND LEF - [SDR NOC2008F00005](https://openairdocs.org/sdr/NOC2008F00005), Sep 21, 2008: BUSS. OVERHEATED. ACFT DIVERTED TO STL, SMOKE IN COCKPIT EMERGENCY DECLARED CAPT REPORTS THE RT ACFT BUSS OVERHEATED ITEM REMAINS OPEN. (K) - [SDR NOCA04108](https://openairdocs.org/sdr/NOCA04108), May 18, 2008: WIRE HARNESS. OUT OF POSITION. RIGHT ENGINE O/H LP 1 STATUS MSG DISPLAYED. CHECKED OVERHEAT SENSORS RESISTANCE AND CHECKED OK. REPOSITIONED HARNESS AND CLEARED CONNECTOR PER MM 26-11-00 AND O - [SDR NOCA03108](https://openairdocs.org/sdr/NOCA03108), Apr 30, 2008: PRESSURE SWITCH. MALFUNCTIONED. CENTER HYD SYSTEM PRESS EICAS & OVERHEAD PANEL LIGHT ILLUMINATED ON TAKEOFF ROLL, 60 KTS. T/S PER SSM 29-00-04 FOUND C HYD PRESS SWITCH AT FAULT S10002. REMOVED - [SDR NOCA02708](https://openairdocs.org/sdr/NOCA02708), Apr 29, 2008: LIGHT. INOPERATIVE. TOP POSITION LAMP INOP IN EXIT LOCATOR SIGN AT 3R DOOR SIDEWALL. REPLACED LAMP AT 3R EXIT SIGN AS PER MM 33-51-10. - [SDR NOCA02908](https://openairdocs.org/sdr/NOCA02908), Apr 29, 2008: LIGHT. INOPERATIVE. THE 2R EMERGENCY LIGHT INOP. RELAMPED 2R EMERGENCY PER MM 33-51-01. - [SDR NOCA02808](https://openairdocs.org/sdr/NOCA02808), Apr 29, 2008: LIGHT. INOPERATIVE. TOP POSITION LAMP INOP AT 3L DOOR EXIT LOCATOR SIGN AT SIDEWALL. REPLACED LAMP AS PER MM 33-51-10. - [SDR NOCA03008](https://openairdocs.org/sdr/NOCA03008), Apr 29, 2008: LIGHT. INOPERATIVE. THE 3L EMERGENCY LIGHT INOP. RELAMPED 3L EMERGENCY LIGHT AS PER MM 33-51-10. - [SDR NOCA00908](https://openairdocs.org/sdr/NOCA00908), Jan 18, 2008: LIGHT. INOPERATIVE. EMERGENCY STRIP LIGHT OUT ROW 36L. RELAMPED LIGHT, OPS CHECK GOOD PER MM 33-51-05. - [SDR NOCA17107](https://openairdocs.org/sdr/NOCA17107), Dec 14, 2007: ACTUATOR. MALFUNCTIONED. ON TAKEOFF OUT OF YQX HAD `L/E SLAT DISAGREE` EICAS CAUTION MESSAGE. AIR TURNBACK TO YQX. ITEM REMAINS OPEN, MX FERRY BACK TO JFK. REPLACED NR 10 L/E ROTARY ACT - [SDR NOCA17007](https://openairdocs.org/sdr/NOCA17007), Dec 12, 2007: ELECTRONIC UNIT. MALFUNCTIONED. LEADING EDGE SLAT DISAGREE MESSAGE AIR TURNBACK INTO KWI. FLAP/SLAT ELECTRONIC UNIT BITE (FSEU) PER FIM 27-51-00 FIG 104B UNABLE TO DUPLEATE SWAPPED FSEU NR 1 B - [SDR NOCA16907](https://openairdocs.org/sdr/NOCA16907), Dec 9, 2007: SWITCH. FAULTY. LEADING EDGE SLAT DISAGREE EICAS MSG WHILE RETRACTING FLAPS 1 TO 0 AIR TURNBACK TO JFK. T/S PER FIM TASK 27-51-00 FIG 104B AND 115 FOUND SWITCH S1 CONNECTOR AT - [SDR NOCA14807](https://openairdocs.org/sdr/NOCA14807), Aug 4, 2007: PUMP. FAILED. ON TAXI IN GEO RAMP LEFT ENG SHUT DOWN (UNCOMMANDED) PERFORMED FIM 73-11-00. REMOVED AND REPLACED HP AND LP FUEL PUMP AS PER MM 73-11-01 & 73-11-03 RAN ENG AND - [SDR NOCA14507](https://openairdocs.org/sdr/NOCA14507), Jul 30, 2007: ADC. MALFUNCTIONED. REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT AIRSPEED INDICATOR. REPLACED AIRSPEED INDICATOR AND LEFT AIR DATA COMPUTER ITEM REMAINS OPEN, SECOND TIME - [SDR NOCA14207](https://openairdocs.org/sdr/NOCA14207), Jul 18, 2007: SLIDE. UNWANTED DEPLOY. L1 SLIDE DEPLOYED ON GROUND. REMOVED AND REPLACED L1 SLIDE AS PER MM 52-11-33 SYSTEM CHECK OK ACCOMPLISHED EO 757-25-199. - [SDR NOCA13607](https://openairdocs.org/sdr/NOCA13607), Jul 9, 2007: WIRE. BROKEN. SECTION OF E-PATH LIGHTING INOP AT L3 DOOR. FOUND BROKEN WIRE IN A FEW SPOTS AND RE-SPLICED WIRE, OPS CHECK GOOD. - [SDR NOCA10207](https://openairdocs.org/sdr/NOCA10207), May 18, 2007: BLOWER. MALFUNCTIONED. THE -AFT DET FAN- STATUS MESSAGE ON EICAS. REMOVED AND REPLACED NR 3 AFT BLOWER IAW AMM 26-16-02 AND REMOVED AND REPLACED BLOWER NR 3 RELAY K10379 BLOWER RELAY - [SDR NOCA10107](https://openairdocs.org/sdr/NOCA10107), May 14, 2007: CONTROL UNIT. MALFUNCTIONED. LEFT ENG EXCEEDANCE EGT AND N2 ON TAKEOFF ROLL FOR LESS THAN ONE SECOND. REMOVED AND REPLACED NR 1 ENG BVCU IAW MM 75-32-01. IDLE RUN DONE. BVCU BITE CKS OK IAW - [SDR NOCA09707](https://openairdocs.org/sdr/NOCA09707), Apr 30, 2007: TRANS PANEL. CORRODED. LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1530-1640 LEFT SIDE. REMOVED CORROSION, TREATED, PRIMED AND PAINTED AS PER SRM 51-10-01 AND 51-20-01. All 104: https://openairdocs.org/aircraft/N750NA/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (73, first 50) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Cessna 750) - [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/aircraft/N750NA/stcs.md ## Related - Other Cessna 750 aircraft: https://openairdocs.org/model/cessna-750/aircraft.md - The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.