# N624BR: 2007 Bombardier BD-700-1A10

- Status: Valid registration
- Airframe: [Bombardier BD-700-1A10](https://openairdocs.org/model/bombardier-bd-700-1a10) (registry code 1390006, 23 seats)
- Engine: [Rolls-Royce Deutschland BR700-710A220](https://openairdocs.org/engine/rolls-royce-deutschland-br700-710a220) (registry code 54004)
- Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY) (Bombardier Inc.), [TCDS E00057EN](https://openairdocs.org/tcds/E00057EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 9236
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 23, 2008
- Certificate issued: June 1, 2018
- Expires: June 30, 2028
- Mode S code: A82542
- Registered owner: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=624BR
- Page: https://openairdocs.org/aircraft/N624BR

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): 75 in force

### Matched by airframe (Bombardier BD-700-1A10)

- [AD 2026-15-09](https://openairdocs.org/ad/2026-15-09): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 3, 2026
- [AD 2026-11-07](https://openairdocs.org/ad/2026-11-07): Equipment/furnishings · Bombardier BD-700-1A10, BD-700-1A11 and BD-700-2A12. Effective Jul 20, 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 2026-09-18](https://openairdocs.org/ad/2026-09-18): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 26, 2026
- [AD 2026-08-04](https://openairdocs.org/ad/2026-08-04): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 29, 2026
- [AD 2025-14-51](https://openairdocs.org/ad/2025-14-51): Indicating/Recording System · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 4, 2026
- [AD 2025-16-07](https://openairdocs.org/ad/2025-16-07): Oxygen · Bombardier BD-700-1A10. Effective Sep 18, 2025
- [AD 2025-12-01](https://openairdocs.org/ad/2025-12-01): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 17, 2025
- [AD 2025-07-11](https://openairdocs.org/ad/2025-07-11): Hydraulic Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 2, 2025
- [AD 2025-09-04](https://openairdocs.org/ad/2025-09-04): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 6, 2025
- [AD 2024-26-09](https://openairdocs.org/ad/2024-26-09): Time Limits/Maintenance Checks; Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 11, 2025
- [AD 2024-23-02](https://openairdocs.org/ad/2024-23-02): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2025
- [AD 2024-23-08](https://openairdocs.org/ad/2024-23-08): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 6, 2025
- [AD 2024-07-09](https://openairdocs.org/ad/2024-07-09): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 17, 2024
- [AD 2024-03-08](https://openairdocs.org/ad/2024-03-08): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 3, 2024
- [AD 2024-02-05](https://openairdocs.org/ad/2024-02-05): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 9, 2024
- [AD 2023-24-08](https://openairdocs.org/ad/2023-24-08): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 6, 2024
- [AD 2023-12-02](https://openairdocs.org/ad/2023-12-02): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 7, 2023
- [AD 2023-13-15](https://openairdocs.org/ad/2023-13-15): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 27, 2023
- [AD 2023-08-01](https://openairdocs.org/ad/2023-08-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 20, 2023
- [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 2023-05-11](https://openairdocs.org/ad/2023-05-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 12, 2023
- [AD 2022-24-01](https://openairdocs.org/ad/2022-24-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 9, 2023
- [AD 2022-25-13](https://openairdocs.org/ad/2022-25-13): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 13, 2023
- [AD 2022-14-07](https://openairdocs.org/ad/2022-14-07): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 19, 2022
- [AD 2022-13-05](https://openairdocs.org/ad/2022-13-05): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 11, 2022
- [AD 2022-11-17](https://openairdocs.org/ad/2022-11-17): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 22, 2022
- [AD 2022-12-01](https://openairdocs.org/ad/2022-12-01): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 19, 2022
- [AD 2021-21-04](https://openairdocs.org/ad/2021-21-04): Powerplant · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 8, 2021
- [AD 2021-10-22](https://openairdocs.org/ad/2021-10-22): Fuel · Bombardier BD-700-1A10. Effective Jul 6, 2021
- [AD 2021-08-11](https://openairdocs.org/ad/2021-08-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 27, 2021
- [AD 2021-03-17](https://openairdocs.org/ad/2021-03-17): Lights · Bombardier BD-700-1A10. Effective Mar 30, 2021
- [AD 2020-12-14](https://openairdocs.org/ad/2020-12-14): Electrical power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2020
- [AD 2020-12-15](https://openairdocs.org/ad/2020-12-15): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 24, 2020
- [AD 2020-05-27](https://openairdocs.org/ad/2020-05-27): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 7, 2020
- [AD 2020-03-21](https://openairdocs.org/ad/2020-03-21): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2020-02-15](https://openairdocs.org/ad/2020-02-15): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2019-12-02](https://openairdocs.org/ad/2019-12-02): Electrical Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 12, 2019
- [AD 2019-03-22](https://openairdocs.org/ad/2019-03-22): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 15, 2019
- [AD 2018-25-07](https://openairdocs.org/ad/2018-25-07): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2019
- [AD 2018-22-08](https://openairdocs.org/ad/2018-22-08): Fire protection · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 10, 2018
- [AD 2018-20-20](https://openairdocs.org/ad/2018-20-20): Flilght Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 20, 2018
- [AD 2018-21-03](https://openairdocs.org/ad/2018-21-03): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 19, 2018
- [AD 2018-09-15](https://openairdocs.org/ad/2018-09-15): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 15, 2018
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2017-19-11](https://openairdocs.org/ad/2017-19-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 23, 2017
- [AD 2017-14-15](https://openairdocs.org/ad/2017-14-15): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2017
- [AD 2016-17-16](https://openairdocs.org/ad/2016-17-16): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 5, 2016
- [AD 2016-15-06](https://openairdocs.org/ad/2016-15-06): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2016
- [AD 2016-15-03](https://openairdocs.org/ad/2016-15-03): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2016

### Matched by engine (Rolls-Royce Deutschland BR700-710A220)

- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

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

- [AD 2023-03-06](https://openairdocs.org/ad/2023-03-06) (historical): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 13, 2023
- [AD 2021-10-02](https://openairdocs.org/ad/2021-10-02) (historical): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 29, 2021
- [AD 2016-25-18](https://openairdocs.org/ad/2016-25-18) (historical): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 3, 2017
- [AD 2014-03-05](https://openairdocs.org/ad/2014-03-05) (historical): Ice and Rain Protection · Bombardier BD-700-1A10. Effective Apr 1, 2014
- [AD 2008-24-12](https://openairdocs.org/ad/2008-24-12) (historical): Bolt which connects the PCU (power control unit) to the elevator surface · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 15, 2008
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 85: https://openairdocs.org/aircraft/N624BR/ads.md

## Information bulletins (advisory) (3 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-11-34](https://openairdocs.org/saib/NM-11-34): Doors: Passenger/Crew Doors, Tensator Springs of the Door Actuator. Issued May 17, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N624BR.

## FAA accident and incident reports

None matched to N624BR.

## Reports on N624BR not matched to an aircraft (1)

They name N624BR, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19980123004759I](https://openairdocs.org/incident/19980123004759I), Jan 23, 1998: Cndair CL6002B19 (N624BR), Nashville, TN, Minor damage. Narrative: acft was at 10,000' MSL & 290 KIAS, beginning approach vectors to rwy 02L ILS at bna in VMC conditions. Capt.'s fwd windscreen shattered without…

## 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 N624BR not matched to an aircraft (26)

They name N624BR, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR VTZA200500176](https://openairdocs.org/sdr/VTZA200500176), Sep 8, 2005: FLOORBEAM. CORRODED. RBL 27 FLOORBEAM HAS CORROSION AT FS 337.
- [SDR VTZA200500175](https://openairdocs.org/sdr/VTZA200500175), Sep 8, 2005: FLOOR SUPPORT. CORRODED. RBL 9 FLOORBEAM HAS CORROSION AT FS 325 TO 392.
- [SDR VTZA200500174](https://openairdocs.org/sdr/VTZA200500174), Sep 8, 2005: FLOORBEAM. CRACKED. LT FS 621 FLOOR SUPPORT IS CRACKED AT 1" IN ANGLE.
- [SDR VTZA200500173](https://openairdocs.org/sdr/VTZA200500173), Sep 8, 2005: FLOOR SUPPORT. CORRODED. LBL 27 FLOOR SUPPORT HAS CORROSION AT FS 325.5 AND 333.5.
- [SDR VTZA200500177](https://openairdocs.org/sdr/VTZA200500177), Sep 8, 2005: ANGLE. CORRODED. FS 280 BETWEEN LBL 19.0 AND RBL 12.0 HAS LEVEL 2 CORROSION.
- [SDR VTZA200500169](https://openairdocs.org/sdr/VTZA200500169), Sep 8, 2005: DOOR FRAME. CRACKED. PAX DOOR FRAME TOP RADIUS CRACKED AT 1" IN LENGTH FORWARD OF DATUM 1 AT FS 338.90.
- [SDR VTZA200500172](https://openairdocs.org/sdr/VTZA200500172), Sep 8, 2005: FLOOR SUPPORT. CORRODED. LBL 9 FLOOR SUPPORT HAS CORROSION AT FS 325 TO 379.
- [SDR VTZA200500171](https://openairdocs.org/sdr/VTZA200500171), Sep 8, 2005: ANGLE. CRACKED. RT FS 621 FLOOR SUPPORT IS CRACKED AT 1" IN ANGLE.
- [SDR VTZA200500168](https://openairdocs.org/sdr/VTZA200500168), Sep 8, 2005: INTERCOSTAL. CRACKED. PAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1" IN LENGTH AT DATUM FS 338.
- [SDR VTZA200500170](https://openairdocs.org/sdr/VTZA200500170), Sep 8, 2005: SUPPORT BEAM. CRACKED. RT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75".
- [SDR 05020624](https://openairdocs.org/sdr/05020624), Jan 20, 2005: A/C PACK. OVERHEATED. EVENT SUMMARY STATED LT PACK OVERHEAT IN AUTO, ADG AUTO DEPLOY. REMOVED AND REPLACED DEPLOYMENT SQUIB. RETRACTED ADG. SYSTEM OPS CHECK GOOD.
- [SDR 04361624](https://openairdocs.org/sdr/04361624), Dec 26, 2004: WINDSHIELD. CRACKED. CA'S WINDOW CRACKED. RTF. MX REMOVED AND REPLACED LT FRONT WINDSHIELD. DID PRESSURIZATION CHECK.
- [SDR 04257624](https://openairdocs.org/sdr/04257624), Sep 13, 2004: A/C PACK. INOPERATIVE. CREW REPORT STATED THAT WITH ONE PACK DEFERRED, RECEIVED PACK OVER PRESSURE WARNING ON T/O ROLL. ABORTED T/O. RESET AND SUCCESSFULLY TOOK OFF. NO RETURN TO GATE
- [SDR 04227624](https://openairdocs.org/sdr/04227624), Aug 14, 2004: SQUAT SWITCH. DEFECTIVE. AFTER TAKEOFF CREW RECEIVED GEAR DISAGREE WITH GEAR UP. WOW INPUT FAIL AND NOSE STEERING MESSAGE. CREW DECLARED AN EMERGENCY. ADJUSTED NLG WOW SENSORS AND PERFO
- [SDR 04121624](https://openairdocs.org/sdr/04121624), Apr 30, 2004: BULB. BURNED OUT. DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND IOPERATIVE AND REPLACED. A SATISFACTRY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS 
- [SDR 04096624](https://openairdocs.org/sdr/04096624), Apr 5, 2004: BULB. BURNED OUT. DURING INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED.
- [SDR 03238624](https://openairdocs.org/sdr/03238624), Aug 26, 2003: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION THE 3RD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY EXIT SIGN BULB. A SATI
- [SDR 03113624](https://openairdocs.org/sdr/03113624), Apr 23, 2003: LAMP. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGEN
- [SDR 03042624](https://openairdocs.org/sdr/03042624), Feb 11, 2003: LAMP. During preflight inspection, the crew reported that the forward emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the
- [SDR VTZA98233](https://openairdocs.org/sdr/VTZA98233), Jun 30, 1998: DOOR. OPEN. FLT 6771 - IAD-GSP - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOUD NOISE COMING FROM COCKPIT RIGHT SIDE. AIRCRAFT RETURNED TO GATE WITH NO FURT
- [SDR VTZA98163](https://openairdocs.org/sdr/VTZA98163), Apr 15, 1998: ADS CONTROLLER. FAILED. IAD/BNA - FLT 6700 - DURING CRUISE AT 0745 HOURS ON 4-15-98, AIRCRAFT MADE UNSCHEDULED LANDING DUE TO TAT AND RT PITOT HEAT FAILURE. AIRCRAFT LANDED AT IND AND 
- [SDR VTZA98151](https://openairdocs.org/sdr/VTZA98151), Apr 3, 1998: RETRACT MECH. MALFUNCTIONED. IAD/IND - FLT 6724 - DURING APPROACH AT 1415 HRS ON 4-3-98, AIRCRAFT MADE ABORTED APPROACH INTO IND DUE TO LANDING GEAR FAILED TO EXTEND NORMALLY AND CREW USED 
- [SDR VTZA98140](https://openairdocs.org/sdr/VTZA98140), Mar 20, 1998: RADOME. DAMAGED. FLT 6718 - ATL-IAD - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH AIRCRAFT WAS DAMAGED BY HAIL AND A/C HAD A ENGINE SHUTDOWN DUE
- [SDR VTZA98052](https://openairdocs.org/sdr/VTZA98052), Feb 8, 1998: CIRCUIT BREAKER. TRIPPED. IAD/TPA - FLT 6681 - DURING CRUISE AT 0720 HOURS ON 2-8-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT AOA STALL VANE HEAT FAILED. AIRCRAFT RETURNED TO GATE
- [SDR VTZA98029](https://openairdocs.org/sdr/VTZA98029), Jan 27, 1998: WINDSCREEN. SHATTERED. IAD/RSW - FLT 6677 - DURING CRUISE ON 1-27-98 AT 1310 HOURS, EXPERIENCED A SHATTERING OF THE CAPTAIN'S WINDSCREEN. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT 
- [SDR VTZA98027](https://openairdocs.org/sdr/VTZA98027), Jan 23, 1998: WINDSHIELD. SHATTERED. IAD/BNA - FLT 6702 - DURING CRUISE ON 1-23-98 AT 1402 HOURS, EXPERIENCED A SHATTERING OF THE CAPTAIN'S WINDSCREEN. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT 

## STCs that may be installed (OpenAirDocs) (432, 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 (Bombardier BD-700-1A10)

- [STC ST12509WI](https://openairdocs.org/stc/ST12509WI): Change to Layout of Passenger Accommodations. Duncan Aviation, Inc
- [STC ST04612CH](https://openairdocs.org/stc/ST04612CH): Installation of a SpaceX Starlink Aviation System. Nextant Aerospace
- [STC ST12507IB](https://openairdocs.org/stc/ST12507IB): Iridium Antenna relocation. Q.C.M. DESIGN GmbH
- [STC ST01418NY](https://openairdocs.org/stc/ST01418NY): Interior Completion Modification IAW Aero Consulting Services Modification Data Summary C88100, Rev B dated 11/30/01. Approved for serial number 9068 ONLY. Bombardier Inc
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST12362IB](https://openairdocs.org/stc/ST12362IB): Ferry Kit Lift Raft installation equipment must be installed in accordance with Transport Canada Civil Aviation (TCCA) approved Bombardier Inc. Modification Data Summary RAZ-BM700-323 Rev--, dated July 16, 2024, or later TCCA approved revision. Bombardier Inc
- [STC ST12269WI](https://openairdocs.org/stc/ST12269WI): Installation of a supplemental cooling system. Learjet Inc
- [STC ST12183WI](https://openairdocs.org/stc/ST12183WI): Installation of Outer Mold Line modifications, MZFW increase and related avionics updates. Learjet Inc
- [STC ST12188WI](https://openairdocs.org/stc/ST12188WI): Relocation of the DME 1, DME 2 (and transceiver), ATC 2, and lower directional TCAS antennas. Learjet Inc
- [STC ST12189WI](https://openairdocs.org/stc/ST12189WI): Relocation of the lower anti-collision light and installation of an additional beacon light. Learjet Inc
- [STC ST03199NY](https://openairdocs.org/stc/ST03199NY): Installation of ABC Completions Electronic Flight Bag Display Mounts and DAC International GDC-64. Delta Engineering Corporation
- [STC ST12270IB](https://openairdocs.org/stc/ST12270IB): Installation of Gogo Galileo Satcom System. Q.C.M. DESIGN GmbH
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST04754NY](https://openairdocs.org/stc/ST04754NY): Installation of LAI Windshields. Lee Aerospace Inc
- [STC ST12078IB](https://openairdocs.org/stc/ST12078IB): Installation of wiring provisions for a subsequent interior completion. Bombardier Inc
- [STC ST12029CH](https://openairdocs.org/stc/ST12029CH): Installation of Gogo MB13 antennas. Premier Air Center, LLC d/b/a West Star Aviation
- [STC ST00240MC](https://openairdocs.org/stc/ST00240MC): The installation of wing internal hardpoints on the Bombardier BD-700-1A10. Learjet Inc
- [STC ST12022IB](https://openairdocs.org/stc/ST12022IB): Installation of Interior Completion, Cabin Reconfiguration. Bombardier Inc
- [STC ST00941LA](https://openairdocs.org/stc/ST00941LA): Installation of floor proximity emergency escape path marking system. Bruce Aerospace 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 ST04677NY](https://openairdocs.org/stc/ST04677NY): Installation of Demonstration of Transmitting Personal Electronic Device (TPED) Tolerance. Bombardier Inc
- [STC ST09931AC](https://openairdocs.org/stc/ST09931AC): Installation of an Aspire 400 Satcom System. L2 Aviation
- [STC ST03759NY](https://openairdocs.org/stc/ST03759NY): Installation of INGENIO Cockpit Tripod Electronic Flight Bag (EFB) Mount. INGENIO Aerospace Inc
- [STC ST02032WI](https://openairdocs.org/stc/ST02032WI): Installation of Gogo Business Aviation AVANCE L5/X3 System or Optional AVANCE L5 System with MB13 antennas. Duncan Aviation Inc
- [STC ST04591NY](https://openairdocs.org/stc/ST04591NY): Structural integration and installation of Iridium Satcom Antenna. ALAMO Engineering GmbH
- [STC ST11840WI](https://openairdocs.org/stc/ST11840WI): Change to Layout of Passenger Accommodations (LOPA). Duncan Aviation Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST04561CH](https://openairdocs.org/stc/ST04561CH): Installation of a Latitude Technologies Corporation DL-150 Satellite Data Unit (SDU) and Iridium Antenna. West Star Aviation
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02022WI](https://openairdocs.org/stc/ST02022WI): Installation of a Bombardier Smart Router. Learjet Inc
- [STC ST00046MC-D](https://openairdocs.org/stc/ST00046MC-D): Installation of structural and electrical provisions for communications equipment. Learjet Inc
- [STC ST00187MC](https://openairdocs.org/stc/ST00187MC): Installation of a Raytheon APX-119 Transponder System with/without a Honeywell H-764 EGI. Learjet Inc
- [STC ST00208IB](https://openairdocs.org/stc/ST00208IB): Installation of Fuel Recirculation System Modification. Bombardier Aerospace
- [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 ST01057WI](https://openairdocs.org/stc/ST01057WI): Installation of a Vision Safe Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST00190IB](https://openairdocs.org/stc/ST00190IB): Installation of a Satcom Iridium Datalink Unit with FANS 1/A+ capability and removal of the installed Inmarsat Swift 64 satcom system. ALAMO ENGINEERING GmbH
- [STC ST04268NY](https://openairdocs.org/stc/ST04268NY): Replacement of Honeywell DU-870 display units with DU-875 Elite display units with basic functions. ALAMO ENGINEERING GmbH
- [STC ST00175IB](https://openairdocs.org/stc/ST00175IB): Installation of Interior Modifications. Innotech Aviation a Division of IMP Group Limited
- [STC ST00167IB](https://openairdocs.org/stc/ST00167IB): Installation of Ku-Band Satcom with TMA. ALAMO ENGINEERING GmbH
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST00126IB](https://openairdocs.org/stc/ST00126IB): Replacement of Halon agent with alternate Halon-free Portable Fire Extinguisher agent. AMAC Aerospace Switzerland AG
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [STC ST01970WI](https://openairdocs.org/stc/ST01970WI): Installation of an Aircraft Health Management System (AHMS). Learjet Inc
- [STC ST00122IB](https://openairdocs.org/stc/ST00122IB): Installation of Satellite Communications (SATCOM). Bombardier Inc
- [STC ST02012WI](https://openairdocs.org/stc/ST02012WI): Upgrade of Gogo Business Aviation AVANCE L5 to AVANCE L5/X3 System with MB13 Antennas. Duncan Aviation Inc
- [STC ST04396CH](https://openairdocs.org/stc/ST04396CH): Installation of SATCOM system and associated KuKa Radome. Envoy Aerospace LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01134WI](https://openairdocs.org/stc/ST01134WI): Installation of metallic window blanks for direct replacement of factory installed windowpane assemblies. Learjet Inc

All 432: https://openairdocs.org/aircraft/N624BR/stcs.md

## Related

- Other Bombardier BD-700-1A10 aircraft: https://openairdocs.org/model/bombardier-bd-700-1a10/aircraft.md
- The Rolls-Royce Deutschland BR700-710A220 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-710a220.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.