# N369CA: 2009 Dassault FALCON 7X

- Status: Valid registration
- Airframe: [Dassault FALCON 7X](https://openairdocs.org/model/dassault-falcon-7x) (registry code 2730176, 11 seats)
- Engine: [Pratt & Whitney Canada PW307A](https://openairdocs.org/engine/pratt-whitney-canada-pw307a) (registry code 52157)
- Data sheets: [TCDS A59NM](https://openairdocs.org/tcds/A59NM) (Dassault Aviation), [TCDS E00071EN](https://openairdocs.org/tcds/E00071EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 087
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 18, 2018
- Certificate issued: August 19, 2024
- Expires: August 31, 2031
- Mode S code: A42DEE
- Registered owner: [Jmsj Texas LLC](https://openairdocs.org/faa-owner/JMSJ%20TEXAS%20LLC)
- Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)
- Owner type: LLC
- Owner's area on the map: 29.7393° N, 95.4464° W: Placed by OpenAirDocs at the center of ZIP code 77027, 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=369CA
- Page: https://openairdocs.org/aircraft/N369CA

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.

## ADs that may apply (OpenAirDocs): 44 in force

### Matched by airframe (Dassault FALCON 7X)

- [AD 2026-11-03](https://openairdocs.org/ad/2026-11-03): Flight Controls · Dassault Falcon 7X. Effective Jul 9, 2026
- [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 2025-22-05](https://openairdocs.org/ad/2025-22-05): Navigation · Dassault Falcon 7X. Effective Jan 2, 2026
- [AD 2025-13-11](https://openairdocs.org/ad/2025-13-11): Flight Controls · Dassault Falcon 7X. Effective Aug 14, 2025
- [AD 2025-06-05](https://openairdocs.org/ad/2025-06-05): Information systems · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective May 2, 2025
- [AD 2024-16-11](https://openairdocs.org/ad/2024-16-11): Wings · Dassault Falcon 7X. Effective Oct 23, 2024
- [AD 2024-15-04](https://openairdocs.org/ad/2024-15-04): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Oct 15, 2024
- [AD 2024-14-09](https://openairdocs.org/ad/2024-14-09): Standard Practices/Structures · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Oct 15, 2024
- [AD 2024-13-06](https://openairdocs.org/ad/2024-13-06): Pneumatic · Dassault Falcon 7X. Effective Sep 24, 2024
- [AD 2024-13-04](https://openairdocs.org/ad/2024-13-04): Powerplant · Dassault Falcon 7X. Effective Aug 16, 2024
- [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 2023-03-11](https://openairdocs.org/ad/2023-03-11): Electrical power · Dassault Falcon 7X. Effective Apr 4, 2023
- [AD 2022-17-10](https://openairdocs.org/ad/2022-17-10): Oxygen · Dassault Falcon 7X. Effective Oct 27, 2022
- [AD 2022-18-18](https://openairdocs.org/ad/2022-18-18): Flight controls · Dassault Falcon 7X. Effective Sep 19, 2022
- [AD 2021-20-14](https://openairdocs.org/ad/2021-20-14): Equipment/Furnishings · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Nov 18, 2021
- [AD 2021-14-04](https://openairdocs.org/ad/2021-14-04): Equipment/Furnishings · Dassault Falcon 7X and FALCON 2000EX. Effective Aug 26, 2021
- [AD 2021-03-18](https://openairdocs.org/ad/2021-03-18): Oxygen · Dassault Falcon 7X. Effective Feb 22, 2021
- [AD 2020-20-01](https://openairdocs.org/ad/2020-20-01): Instruments · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Oct 21, 2020
- [AD 2020-05-10](https://openairdocs.org/ad/2020-05-10): Navigation · Dassault Falcon 7X. Effective Mar 26, 2020
- [AD 2018-03-19](https://openairdocs.org/ad/2018-03-19): Structure · Dassault Falcon 7X. Effective Mar 20, 2018
- [AD 2018-02-06](https://openairdocs.org/ad/2018-02-06): Navigation · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Feb 5, 2018
- [AD 2017-20-03](https://openairdocs.org/ad/2017-20-03): Standard Practices Airframe--Electrical Wiring · Dassault Falcon 7X. Effective Nov 6, 2017
- [AD 2017-18-07](https://openairdocs.org/ad/2017-18-07): Standard practices/structures · Dassault Falcon 7X. Effective Oct 5, 2017
- [AD 2017-17-11](https://openairdocs.org/ad/2017-17-11): Engine Controls · Dassault Falcon 7X. Effective Sep 29, 2017
- [AD 2017-13-02](https://openairdocs.org/ad/2017-13-02): Fuselage · Dassault Falcon 7X. Effective Jul 27, 2017
- [AD 2016-24-07](https://openairdocs.org/ad/2016-24-07): Fuel · Dassault Falcon 7X. Effective Jan 9, 2017
- [AD 2016-13-15](https://openairdocs.org/ad/2016-13-15): Fuselage · Dassault Falcon 7X. Effective Aug 16, 2016
- [AD 2016-08-01](https://openairdocs.org/ad/2016-08-01): Electrical power · Dassault Falcon 7X. Effective May 31, 2016
- [AD 2016-07-15](https://openairdocs.org/ad/2016-07-15): Fuel · Dassault Falcon 7X. Effective May 16, 2016
- [AD 2015-06-04](https://openairdocs.org/ad/2015-06-04): Navigation · Dassault Falcon 7X. Effective May 1, 2015
- [AD 2014-16-23](https://openairdocs.org/ad/2014-16-23): Flight Controls · Dassault Falcon 7X. Effective Oct 9, 2014
- [AD 2014-16-21](https://openairdocs.org/ad/2014-16-21): Main Landing Gear · Dassault Falcon 7X. Effective Oct 2, 2014
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-15-10](https://openairdocs.org/ad/2014-15-10): Flight Controls · Dassault Falcon 7X. Effective Sep 2, 2014
- [AD 2013-16-02](https://openairdocs.org/ad/2013-16-02): Landing gear · Dassault Falcon 7X. Effective Aug 21, 2013
- [AD 2013-07-13](https://openairdocs.org/ad/2013-07-13): Oxygen · Dassault Falcon 7X. Effective May 6, 2013
- [AD 2012-15-11](https://openairdocs.org/ad/2012-15-11): Oxygen · Dassault Falcon 7X. Effective Sep 11, 2012
- [AD 2012-12-18](https://openairdocs.org/ad/2012-12-18): Electrical Power · Dassault Falcon 7X. Effective Jul 30, 2012
- [AD 2011-27-06](https://openairdocs.org/ad/2011-27-06): Electrical Power · Dassault Falcon 7X. Effective Feb 7, 2012
- [AD 2011-14-04](https://openairdocs.org/ad/2011-14-04): Hydraulic Power · Dassault Falcon 7X. Effective Aug 10, 2011
- [AD 2011-09-18](https://openairdocs.org/ad/2011-09-18): Landing Gear · Dassault Falcon 7X. Effective Jun 6, 2011
- [AD 2010-24-02](https://openairdocs.org/ad/2010-24-02): Fuselage · Dassault Falcon 7X. Effective Dec 29, 2010
- [AD 2008-13-10](https://openairdocs.org/ad/2008-13-10): Secondary Power Distribution Boxes (SPDB) · Dassault Falcon 7X. Effective Jul 7, 2008

### Matched by engine (Pratt & Whitney Canada PW307A)

- [AD 2024-03-01](https://openairdocs.org/ad/2024-03-01): Turbine Section · Pratt & Whitney Canada PW307A and PW307D. Effective Mar 27, 2024

### Historical (superseded or no longer in force)

- [AD 2023-22-13](https://openairdocs.org/ad/2023-22-13) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Dec 29, 2023
- [AD 2023-04-15](https://openairdocs.org/ad/2023-04-15) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective May 10, 2023
- [AD 2022-12-10](https://openairdocs.org/ad/2022-12-10) (historical): Navigation · Dassault Falcon 7X. Effective Sep 1, 2022
- [AD 2022-02-10](https://openairdocs.org/ad/2022-02-10) (historical): Standard Practices/Structures · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Mar 15, 2022
- [AD 2021-19-20](https://openairdocs.org/ad/2021-19-20) (historical): Oxygen · Dassault Falcon 7X. Effective Sep 16, 2021
- [AD 2021-09-12](https://openairdocs.org/ad/2021-09-12) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Jun 8, 2021
- [AD 2020-07-16](https://openairdocs.org/ad/2020-07-16) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective May 18, 2020
- [AD 2019-03-20](https://openairdocs.org/ad/2019-03-20) (historical): Time limits/maintenance checks. · Dassault Falcon 7X. Effective Apr 2, 2019
- [AD 2016-16-09](https://openairdocs.org/ad/2016-16-09) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Sep 14, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2011-16-01](https://openairdocs.org/ad/2011-16-01) (historical): Flight controls · Dassault Falcon 7X. Effective Aug 22, 2011
- [AD 2011-13-07](https://openairdocs.org/ad/2011-13-07) (historical): Navigation · Dassault Falcon 7X. Effective Jul 27, 2011
- [AD 2011-12-51](https://openairdocs.org/ad/2011-12-51) (historical): Flight controls · Dassault Falcon 7X. Effective Jul 12, 2011
- [AD 2011-10-01](https://openairdocs.org/ad/2011-10-01) (historical): Electrical power · Dassault Falcon 7X. Effective Jun 9, 2011
- [AD 2010-18-03](https://openairdocs.org/ad/2010-18-03) (historical): Electrical Power · Dassault Falcon 7X. Effective Sep 8, 2010
- [AD 2010-02-02](https://openairdocs.org/ad/2010-02-02) (historical): Navigation · Dassault Falcon 7X. Effective Jan 28, 2010

## Information bulletins (advisory) (1 in force)

- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014

## NTSB investigations

None matched to N369CA.

## FAA accident and incident reports

None matched to N369CA.

## Service difficulty reports (2)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 2026FA0000148](https://openairdocs.org/sdr/2026FA0000148), Feb 27, 2026: GENERATOR. FAILED. PIREP: N369CA SN 087 DEPARTED KHOU TO KIAD. DURING AIRCRAFT CLIMB THE PILOT IDENTIFIED AN AMBER CAS MESSAGE. "ELEC: GEN 2 FAULT". THE CREW ACCOMPLISHED THE ASSO
- [SDR 2023FA0000407](https://openairdocs.org/sdr/2023FA0000407), Aug 10, 2023: ENGINE. STALLED. IN CRUISE THE # 1 ENGINE DID AN UNCOMMANDED SHUTDOWN. THE CREW RESTARTED THE ENGINE BUT OBSERVED THAT THE ITT WAS HIGHER THAN THE OTHER ENGINES. THE POWER LEVER

## Service difficulty reports on N369CA not matched to an aircraft (134, newest 50)

They name N369CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR V0XD20180810003](https://openairdocs.org/sdr/V0XD20180810003), Aug 10, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL BS 319.7 - 349 AT STRINGER 20R HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 53-21-23, 51-42-21, 51-40-11, 51-25-16
- [SDR V0XD20180810002](https://openairdocs.org/sdr/V0XD20180810002), Aug 9, 2018: DRAG ANGLE. CRACKED. VERTICAL STABILIZER FWD DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV A, AND 670-55-31-1
- [SDR V0XD2018081001](https://openairdocs.org/sdr/V0XD2018081001), Aug 9, 2018: DRAG ANGLE. CRACKED. LEFT VERTICAL STABILIZER AFT DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV.
- [SDR V0XD2018080900006](https://openairdocs.org/sdr/V0XD2018080900006), Aug 9, 2018: STRIKER. CORRODED. GALLEY SERVICE DOOR LOWER SEAL STRIKER HAD SIGNS OF CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-
- [SDR V0XD20180809006](https://openairdocs.org/sdr/V0XD20180809006), Aug 9, 2018: BRACKET. CRACKED. PAX DOOR OTBD CLOSE ASSIST BRACKET WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06, AND 51-42-10.
- [SDR V0XD2018080900005](https://openairdocs.org/sdr/V0XD2018080900005), Aug 9, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL AT BS 310 TO 333, STINGER 21L HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 53-21-23, 51-42-06, 51-40-11, 51-42-21, 51-42-13,
- [SDR V0XD20180809MD4](https://openairdocs.org/sdr/V0XD20180809MD4), Aug 9, 2018: FRAME. CORRODED. THE FRAME AT BS 319.70, BETWEEN STRINGERS 18L - 21L HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FRAME SECTION BETWEEN STRINGERS 18L - 21L IAW SRM 51-42-06,
- [SDR V0XD2018080900001](https://openairdocs.org/sdr/V0XD2018080900001), Aug 9, 2018: ANGLE. CORRODED. PASSENGER DOOR MID-CAP ANGLE HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE PASSENGER DOOR MID-CAP ANGLE IAW SRM 51-41-02.
- [SDR V0XD20180809MD3](https://openairdocs.org/sdr/V0XD20180809MD3), Aug 8, 2018: FIRE SEAL. TORN. LEFT LOWER ENGINE COWLING DRAIN PAN FIRE SEAL WAS TORN. REPAIRED THE FIRE SEAL IAW REO 670-54-23-959, REV E, AND REO 670-54-23-1166.
- [SDR V0XD2018080900002](https://openairdocs.org/sdr/V0XD2018080900002), Aug 6, 2018: SKIN. GOUGED. FUSELAGE SKIN GOUGED AT BS 977, STRINGER 27. REPAIRED THE SKIN IAW REO 670-53-135, AND REO 670-53-00-290, REV D.
- [SDR V0XD2018080800002](https://openairdocs.org/sdr/V0XD2018080800002), Aug 3, 2018: PLATE. CORRODED. OVERWING EMERGENCY EXIT RT AND LT STEP PLATES HAD SIGNS OF CORROSION AROUND FASTENER HOLES. EVALUATED THE LT AND RT OVERWING EXIT STEP PLATES, RT STEP PLATE HAD
- [SDR V0XD2018080200001](https://openairdocs.org/sdr/V0XD2018080200001), Aug 2, 2018: WEB. CRACKED. RT FLOOR WEB IN FORWARD EQUIPMENT COMPARTMENT IS CRACKED. REPAIRED RT FLOOR WEB IN FORWARD EQUIPMENT COMPARTMENT IAW REO 670-53-11-509 REV D DATED 2016-06-29 AN
- [SDR V0XD20180808DP1](https://openairdocs.org/sdr/V0XD20180808DP1), Aug 1, 2018: BRACKET. CRACKED. RIGHT WING SLAT TRACK 1 - 3 HOUSING BRACKET WAS CRACKED. REPAIRED THE BRACKET IAW REO 670-57-42-577, REV--.
- [SDR V0XD2018080400004](https://openairdocs.org/sdr/V0XD2018080400004), Aug 1, 2018: SEAT TRACK. CORRODED. RIGHT SEAT TRACK, BS 581 - 691 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
- [SDR V0XD201808040003](https://openairdocs.org/sdr/V0XD201808040003), Aug 1, 2018: SEAT TRACK. CORRODED. LEFT SEAT TRACK, BS 581 - 691 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
- [SDR V0XD201808040002](https://openairdocs.org/sdr/V0XD201808040002), Aug 1, 2018: SEAT TRACK. CORRODED. LEFT SEAT TRACK FROM BS 485 - 581 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
- [SDR V0XD201808040001](https://openairdocs.org/sdr/V0XD201808040001), Aug 1, 2018: SEAT TRACK. CORRODED. RIGHT SEAT TRACK, BS 485 - 581 WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
- [SDR V0XD2018080800004](https://openairdocs.org/sdr/V0XD2018080800004), Jul 28, 2018: RETAINER. DAMAGED. FWD CARGO DOOR AFT, LOWER INBD AND OTBD SEAL RETAINERS WERE BENT AND GOUGED. REPAIRED IAW REO 670-42-35-127, AND SRM 51-21-16.
- [SDR V0XD2018080800003](https://openairdocs.org/sdr/V0XD2018080800003), Jul 28, 2018: WEB. CRACKED. LEFT FLOOR WEB IN THE FWD EQUIPMENT BAY WAS CRACKED. REPAIRED THE WEB AT BS 193 IAW REO 670-53-11-509, REV D.
- [SDR V0XD201808040006](https://openairdocs.org/sdr/V0XD201808040006), Jul 28, 2018: ANGLE. CRACKED. PAX DOOR INNER ANGLE FOR DOOR LATCH MECHANISM CRACKED. REPLACED THE ANGLE IAW SRM 51-25-21, 51-21-11, AND 51-42-06.
- [SDR V0XD201808040005](https://openairdocs.org/sdr/V0XD201808040005), Jul 28, 2018: BRACKET. BENT. PAX DOOR SUPPORT WHEEL CABLE, LOWER PULLEY BRACKET WAS BENT. REMOVED AND REPLACED THE LOWER PULLEY BRACKET IAW SRM 51-40-11, 51-42-06, 51-25-21.
- [SDR N6WA2018010201](https://openairdocs.org/sdr/N6WA2018010201), Jan 2, 2018: COVER. BROKEN. RIGHT EMERGENCY EXIT HANDLE COVER BROKEN OFF. REPLACED THE HANDLE COVER IAW NEF 25-100-6.
- [SDR N6WA2017112301](https://openairdocs.org/sdr/N6WA2017112301), Nov 23, 2017: WARNING MESSAGE. ILLUMINATED. SERVICE DOOR OUTER HANDLE CAUTION MESSAGE.
- [SDR N6WA2017082801](https://openairdocs.org/sdr/N6WA2017082801), Aug 27, 2017: WARNING MESSAGE. ILLUMINATED. PAX DOOR OUTER HANDLE CAUTION.
- [SDR V0XD20170309017](https://openairdocs.org/sdr/V0XD20170309017), Mar 14, 2017: STRINGER. CORRODED. STRINGER 24L BETWEEN BS 517-533 CORRODED. REPAIRED IAW SRM 53-00-03, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16, 51-25-06, AND AMM 51-21-01.
- [SDR V0XD20170309016](https://openairdocs.org/sdr/V0XD20170309016), Mar 7, 2017: INTERCOSTAL. CORRODED. SKIN SIDE FOOT OF INTERCOSTAL ANGLE LBL24 HAS SIGNS OF CORROSION. REPAIRED BY BLENDING IAW REO 670-53-32-030 REV_ 2017-3-08. NDT PERFORMED. NO CRACK INDICATIONS
- [SDR V0XD20170308014](https://openairdocs.org/sdr/V0XD20170308014), Mar 7, 2017: SKIN. DAMAGED. DAMAGE TO FUSELAGE SKIN INTERIOR SURFACE BETWEEN FS517-FS533 AND STR 20-21L. BLENDED DAMAGE AND RESTORED FINISH IAW REO 670-53-31-407, DATED 2017-03-07, SRM 51-
- [SDR V0XD20170309015](https://openairdocs.org/sdr/V0XD20170309015), Mar 4, 2017: STRINGER. CORRODED. SIGNS OF CORROSION ON STRINGER 21L BETWEEN BS 517 AND 533. BLENDED AND RESTORED FINISH IAW SRM 53-31-03, 51-42-06, 51-21-11, 51-25-06, AND 51-25-16. FOUND TO BE
- [SDR V0XD20170308013](https://openairdocs.org/sdr/V0XD20170308013), Mar 3, 2017: AILERON. GOUGED. LT AILERON IB TRAILING EDGE GOUGED. REPAIRED LT AILERON IB TRAILING EDGE IAW REO 670-57--61-001 REV C, DATED 2012-01-16. NDT PERFORMED.
- [SDR WVER2016052700003](https://openairdocs.org/sdr/WVER2016052700003), May 27, 2016: SKIN. DAMAGED. WHILE PERFORMING SB 670BA-57-020, REV C, FOUND 2 EA FASTENERS IN THE RT WING PLANK TO BE OVERSIZE.
- [SDR WVER2016052700002](https://openairdocs.org/sdr/WVER2016052700002), May 27, 2016: BULKHEAD. DAMAGED. FS 202.75 FWD SIDE OF BULKHEAD, LBL30 STIFFENER HAS AN INDICATION .25" LONG IN THE UPPER EDGE OF FLANGE. FAILED NDT INSPECTION.
- [SDR WVER2016052700001](https://openairdocs.org/sdr/WVER2016052700001), May 27, 2016: FRAME. CRACKED. RT FS 235 HAS AN INDICATION .200" LONG PROPAGATING FROM THE RADIUS AT STR 13A.
- [SDR N6WA2016030703](https://openairdocs.org/sdr/N6WA2016030703), Mar 7, 2016: MOUNT. DISCONNECTED. MAIN CABIN LT HANDLE MOUNT DISCONNECTED. POSITIONED MAIN CABIN LT HANDLE MOUNT IAW AMM 52-11-05. OPERATIONS CHECKED GOOD.
- [SDR V0XD20160215035](https://openairdocs.org/sdr/V0XD20160215035), Feb 16, 2016: STRUCTURE. SCRATCHED. RIGHT HORIZONTAL STABILIZER IS SCRATCHED. CUT OUT, OUT OF LIMITS DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-55-11-314 DATED 15 FEB 2016. BLENDED & 
- [SDR V0XD20160212028](https://openairdocs.org/sdr/V0XD20160212028), Feb 11, 2016: DRAG ANGLE. CRACKED. PASSENGER DOOR AFT DRAG ANGLE 1/2 WAY UP IS CRACKED. R & R DAMAGED DRAG ANGLE SECTION PN 601R31772-5 IAW SRM 51-42-13, 51-42-06, 51-40-11, 51-25-06 & 51-25-16.
- [SDR V0XD20160208017](https://openairdocs.org/sdr/V0XD20160208017), Feb 8, 2016: SUPPORT BRACKET. CRACKED. PASSENGER DOOR, AFT LOWER PULLEY SUPPORT BRACKET IS CRACKED. R & R PAX DOOR AFT LOWER PULLEY SUPPORT BRACKET, PN 601R317186-1, IAW SRM 51-42-06, AMM 52-11-13, 5
- [SDR V0XD20160208018](https://openairdocs.org/sdr/V0XD20160208018), Feb 7, 2016: CABLE. FRAYED. PASSENGER DOOR, ASSIST CABLE IS FRAYED. R & R PAX DOOR ASSIST CABLE, PN 2R59573001-1SD, IAW AMM 52-11-08.
- [SDR V0XD20160208019](https://openairdocs.org/sdr/V0XD20160208019), Feb 5, 2016: BRACKET. CORRODED. AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE LT BRACKET AT FS 939.00 IS CORRODED. R & R LT BRACKET, PN:SH670-39189-1 IAW SRM 51-42-06, 51-45-00, 51-25-16.
- [SDR V0XD20160207015](https://openairdocs.org/sdr/V0XD20160207015), Feb 5, 2016: BRACKET. CRACKED. AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE, LT BRACKET CRACKED FS 939.00. R & R LT ANGLE, PN SH670-39189-1, IAW SRM 51-42-06, 51-45-00 & 51-25-16.
- [SDR V0XD20160207016](https://openairdocs.org/sdr/V0XD20160207016), Feb 4, 2016: INTERCOSTAL. CORRODED. AVIONICS BAY AT FS 364.00 2 INTERCOSTAL LT INBD & RT INBD, SHOWING SIGNS OF CORROSION. R & R 2 INTERCOSTAL, LT & RT INBD INTERCOSTALS, PN SH670-32075-3 & -4, IA
- [SDR N6WA2015122801](https://openairdocs.org/sdr/N6WA2015122801), Dec 28, 2015: OIL SYSTEM. LOW. APU OVERTEMP MASTER WARNING IN FLIGHT, NR 2 IDG ALREADY DEFERRED. INSPECTED APU IAW AMM 49-10-00, SERVICED APU OIL IAW AMM 12-13-49 & INSPECTED APU THERMOCOUPLE
- [SDR N6WA2015122201](https://openairdocs.org/sdr/N6WA2015122201), Dec 22, 2015: COVER. LOOSE. RIGHT SIDE EMER EXIT ROW HANDLE COVER LOOSE. SECURED RT SIDE EMER DOOR EXIT HANDLE COVER IAW ALL 25-26-09.
- [SDR N6WA2015120502](https://openairdocs.org/sdr/N6WA2015120502), Dec 5, 2015: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT AT ROW 9 INOPERATIVE. DEFERRED EMER CEILING LIGHT AT ROW 9 IAW MEL 33-51-01 CAT C.
- [SDR N6WA2015102405](https://openairdocs.org/sdr/N6WA2015102405), Oct 24, 2015: LIGHT. INOPERATIVE. CEILING EMER LIGHT AT 9 INOPERATIVE. DEFERRED IAW MEL 33-51-01B CAT C.
- [SDR N6WA2015102404](https://openairdocs.org/sdr/N6WA2015102404), Oct 24, 2015: LIGHT. INOPERATIVE. CROSS AISLE EMER LIGHT OUT. RELAMPED AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.
- [SDR N6WA2015102402001](https://openairdocs.org/sdr/N6WA2015102402001), Oct 24, 2015: LIGHT. INOPERATIVE. CEILING EMER LIGHT INOPERATIVE AT ROW 9. DEFERRED EMER LIGHT IAW MEL 33-51-01B.
- [SDR N6WA2015102401](https://openairdocs.org/sdr/N6WA2015102401), Oct 24, 2015: LIGHT. INOPERATIVE. CROSS AISLE EMER LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-00.
- [SDR N6WA2015100401](https://openairdocs.org/sdr/N6WA2015100401), Oct 4, 2015: DOOR SEAL. DIRTY. LOUD WHISTLING NOISE COMING FROM RT OVERWING EMER EXIT DOOR INFLIGHT. PRESSURIZATION OK & DOOR SHOWS CLOSED. PERFORMED INSPECTION OF RT EMER EXIT DOOR. FOUND DE
- [SDR N6WA2015042501](https://openairdocs.org/sdr/N6WA2015042501), Apr 25, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT UNDER FWD FLASHLIGHT IS INOPERATIVE. R & R FLOOR LEVEL EMER LIGHT BULBS IAW AMM 33-51-11. OPERATIONS CHECKED GOOD.
- [SDR N6WA2015041302](https://openairdocs.org/sdr/N6WA2015041302), Apr 13, 2015: WARNING MESSAGE. ACTIVATED. PASSENGER DOOR LATCH CAUTION MSG. DEFERRED PAX DOOR LATCH MSG IAW MEL 52-70-01 CAT C.

All 134: https://openairdocs.org/aircraft/N369CA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (40)

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 (Dassault FALCON 7X)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST12403IB](https://openairdocs.org/stc/ST12403IB): Installation and maintenance of HAFEX (P/N P3APP003010D, Umlaut GmbH) and HBPE (P/N 351, Amerex) Halon-free handheld fire extinguishers. Q.C.M. DESIGN GmbH
- [STC ST03620NY](https://openairdocs.org/stc/ST03620NY): Installation of Gogo Galileo HDX System. Dassault Falcon Jet Corp
- [STC ST03600NY](https://openairdocs.org/stc/ST03600NY): Installation of a GoGo AVANCE L5 system in Dassault Aviation Falcon 7X aircraft. Dassault Falcon Jet Corp
- [STC ST11282DS](https://openairdocs.org/stc/ST11282DS): Installation of a wireless cabin management system. Cabin Management Solutions
- [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 ST03616NY](https://openairdocs.org/stc/ST03616NY): Installation of SpaceX Starlink Aviation System i. Dassault Falcon Jet Corp
- [STC ST03611NY](https://openairdocs.org/stc/ST03611NY): Installation of Garmin GI 275 Standby Flight Display System (SFDS). Dassault Falcon Jet Corp
- [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 ST01973WI](https://openairdocs.org/stc/ST01973WI): Installation of Aviation Clean Air Ionization System. Dassault Falcon Jet Corp
- [STC ST00136IB](https://openairdocs.org/stc/ST00136IB): Installation of Entryway & Aft Lavatory Vinyl Flooring, SATCOM ON/OFF Switch, & Galley Equipment. The Bank of Nova Scotia
- [STC ST00133IB](https://openairdocs.org/stc/ST00133IB): Installation of 4G LRU and ACM, Below Floor between FR 13-15, Structural Provision Only. The Bank of Nova Scotia
- [STC ST00101IB](https://openairdocs.org/stc/ST00101IB): Activation of WIFI Network. Dassault Falcon Service
- [STC ST03609NY](https://openairdocs.org/stc/ST03609NY): Installation of the Viassat Global Aero Terminal GAT-5510 Ka-Band Satelite Communication System. Dassault Aircraft Services (DAS)
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04594NY](https://openairdocs.org/stc/ST04594NY): Installation of cabin 14 pax configuration. Dassault Falcon Service
- [STC ST04574NY](https://openairdocs.org/stc/ST04574NY): Installation of Interior Reconfiguration. Elisen & Associes Inc
- [STC ST04469NY](https://openairdocs.org/stc/ST04469NY): Activation of DLU TrueNorth Satcom. Dassault Falcon Service
- [STC ST04509NY](https://openairdocs.org/stc/ST04509NY): Installation of Interior Refurbishment. Elisen & Associes Inc
- [STC ST02672LA](https://openairdocs.org/stc/ST02672LA): Installation of Honeywell DU-1310-2 Display Unit in accordance. Honeywell International Inc
- [STC ST01921WI](https://openairdocs.org/stc/ST01921WI): Interior reconfiguration. Duncan Aviation Inc
- [STC ST04379NY](https://openairdocs.org/stc/ST04379NY): Installation of LH Galley Bulkhead and aircraft curtains modification. Dassault Falcon Service
- [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 ST04384CH](https://openairdocs.org/stc/ST04384CH): Reconfiguration of the Cabin Interior in accordance with StandardAero Master Data List 1035953, Revision (A), dated April 5, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST00391BO](https://openairdocs.org/stc/ST00391BO): Installation of a Honeywell CNX-900 Cabin Network Accelerator and PED tolerance certification. Pro Star Aviation LLC
- [STC ST00383BO](https://openairdocs.org/stc/ST00383BO): Installation of a Honeywell DLMU-W. Pro Star Aviation, LLC
- [STC ST01886WI](https://openairdocs.org/stc/ST01886WI): 3-Place 16G Divan Installation. Duncan Aviation Inc
- [STC ST00833DE](https://openairdocs.org/stc/ST00833DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation LLC
- [STC ST04296CH](https://openairdocs.org/stc/ST04296CH): Reconfiguration of the cabin floor plan arrangement. StandardAero Business Aviation Services, LLC
- [STC ST04278CH](https://openairdocs.org/stc/ST04278CH): Reconfiguration of the cabin floor plan arrangement. StandardAero Business Aviation Services, LLC
- [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 ST04170CH](https://openairdocs.org/stc/ST04170CH): Activation of an 802.11 b/g/n/ac WiFi System. StandardAero Business Aviation Services, LLC
- [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 ST04273AT](https://openairdocs.org/stc/ST04273AT): Replace Original Main Battery Connector with Concorde Connector, Part Number 4000. Concorde Battery Corporation
- [STC ST04185AT](https://openairdocs.org/stc/ST04185AT): Replacement of the original equipment valve regulated sealed Lead-acid batteries with Concorde valve regulated sealed Lead-acid batteries with associated hardware. Concorde Battery Corporation
- [STC ST03384CH](https://openairdocs.org/stc/ST03384CH): Reconfiguration of cabin floor Plan Arrangement in accordance with Standard Aero Master Data List 1026983, Revision (F), dated October 02, 2014 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST11036SC](https://openairdocs.org/stc/ST11036SC): Installation of a window shade assembly. A & C Products
- [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX). EMS Technologies Canada Ltd
- [STC ST02893AT](https://openairdocs.org/stc/ST02893AT): Installation of a Boom Beam Taxi/Landing Light System. Whelen Aerospace Technologies

## Related

- Other Dassault FALCON 7X aircraft: https://openairdocs.org/model/dassault-falcon-7x/aircraft.md
- The Pratt & Whitney Canada PW307A engine: https://openairdocs.org/engine/pratt-whitney-canada-pw307a.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.