# N104DA: 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: 9266
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 31, 2007
- Certificate issued: October 2, 2024
- Expires: October 31, 2031
- Mode S code: A013DC
- 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=104DA
- Page: https://openairdocs.org/aircraft/N104DA

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/N104DA/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 N104DA.

## FAA accident and incident reports

None matched to N104DA.

## Reports on N104DA not matched to an aircraft (3)

They name N104DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20010110001049I](https://openairdocs.org/incident/20010110001049I), Jan 10, 2001: Boeing 767232 (N104DA), Salt Lake City, UT, Minor damage. (-23)During a cat ii approach, upon touchdown, the crew noticed several eicas warning messages horn, heard several circuit breakers popping, and smelled…
- [Incident 20000123000319I](https://openairdocs.org/incident/20000123000319I), Jan 23, 2000: Boeing 757232 (N104DA), Covington/Cinci, KY, Minor damage. (-23) During deicing, aircraft moved forward and struck spray truck boom causing damage to right wing tip and position lights. No other damage was noted.
- [Incident 19860728051079I](https://openairdocs.org/incident/19860728051079I), Jul 28, 1986: Boeing 767232 (N104DA), Dallas Fort Wor, TX. Diverted with engine shutdown due to high oil temperature. Replaced oil temperature bulb, oil heat exchanger.

## 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 N104DA not matched to an aircraft (32)

They name N104DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DL767040957](https://openairdocs.org/sdr/DL767040957), Oct 10, 2004: ODOR. DETECTED. RAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE.
- [SDR DL767040009](https://openairdocs.org/sdr/DL767040009), Jan 5, 2004: BEAM. CORRODED. CORROSION WAS FOUND IN THE HOLE BORES OF THE '9-10' BEAM WHICH PROVIDES THE OUTBOARD SUPPORT FOR THE INBOARD FLAP ON THE LT WING. THE CORRODED HOLES WERE OVERSI
- [SDR DL767030284](https://openairdocs.org/sdr/DL767030284), Mar 27, 2003: WEDGE. DEBONDED. LEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.
- [SDR DL767030130](https://openairdocs.org/sdr/DL767030130), Feb 6, 2003: DUCT. RUPTURED. LEFT AND RIGHT DUCT LEAK INDICATION IN COCKPIT FOUND FWD CARGO HEAT DUCT AND CROSSOVER MANIFOLD RUPTURED PER IPC 36-11-01-10
- [SDR DL767030092](https://openairdocs.org/sdr/DL767030092), Jan 26, 2002: LINE. CHAFED. PILOT REPORT--AT 2500 AFTER T/O RT RSVR AND RT ENG PRESS LIGHT ILLUMINATED TOWER REPORTED SMOKE FROM RT ENGINE. RETURNED TO LAS NORMAL LANDING. RT HYD QTY ON EI
- [SDR DL767011077](https://openairdocs.org/sdr/DL767011077), Jun 26, 2001: BULKHEAD. CRACKED. DURING ACCOMPLISHMENT INSPECTIONS PER BAC S/B 767-53-0078, CRACKS WERE FOUND IN THE TENSION FITTING, FWD OUTER CHORD, AND SKIN. THE S/B ONLY COVERS CRACKS IN TH
- [SDR DL767011056](https://openairdocs.org/sdr/DL767011056), Jun 19, 2001: FITTING. CRACKED. WHILE ACCOMPLISHING THE STRUT IMPROVEMENT PROGRAM MODIFICATION ON THE LT WING SUPPORT STRUCTURE, A CRACK INDICATION WAS FOUND IN THE O/B ROW 2ND HOLE FROM BOTTO
- [SDR DL767010205](https://openairdocs.org/sdr/DL767010205), Feb 5, 2001: FLOORBEAM. DAMAGED. THE LOWER CHORD AREA OF THE FS 266.5 FLOORBEAM SUFFERED HEAT DAMAGE FROM AN ELECTRICAL WIRE ARCING BETWEEN RBL 23 & 30. THE LOWER CHORD AND LOWER PORTION OF THE
- [SDR DL767010161](https://openairdocs.org/sdr/DL767010161), Jan 10, 2001: HARNESS. OVERHEATED. MULTIPLE EICAS WARNINGS AND AN ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND WIRE BUNDLE BURNED ABOVE P50 PANEL DUE TO CHAFING ON STRUCTURE. REPAIRED W
- [SDR DL767010052](https://openairdocs.org/sdr/DL767010052), Jan 10, 2001: HARNESS. BURNED. MULTIPLE EICAS WARNINGS AND ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND INBOARD MOST WIRE BUNDLE IN RIGHT HAND TUNNEL AREA OF MAIN E AND E AT STATION
- [SDR DL767010034](https://openairdocs.org/sdr/DL767010034), Jan 6, 2001: SKIN. DAMAGED. THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR WHICH WAS INSTALLED BETWEEN FS 500 & 521 AND BETWEEN STRINGERS 33L & 39L. THE UPPER PORTION OF
- [SDR DL767010023](https://openairdocs.org/sdr/DL767010023), Jan 4, 2001: SKIN. DAMAGED. THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR LOCATION AT FS 456 AND STRINGERS 33L-34L. THE REPAIR WAS REMOVED AND ALL UNDERLYING DAMAG
- [SDR DL767010022](https://openairdocs.org/sdr/DL767010022), Jan 4, 2001: FITTING. DAMAGED. THE CORNER SPLICE FITTING OF THE FS 500 FRAME AT STRINGER 33L WAS DAMAGED BY GROUND EQUIPMENT STRIKING THE AIRCRAFT. THE DAMAGED FITTING WAS REMOVED AND A NEW F
- [SDR DL767001599](https://openairdocs.org/sdr/DL767001599), Aug 19, 2000: FLASHLIGHT. INOPERATIVE. FLASHLIGHT AT 2R DOES NOT INDICATE CHARGE. FOUND LED INDICATOR INOP. REMOVED AND REPLACED FLASHLIGHT.
- [SDR DL767991853](https://openairdocs.org/sdr/DL767991853), Aug 18, 1999: OVERHEAT LOOP. FAILED. AFTER T/O ENG EICAS MSG LT ENG OVHT LP1/LP2 FIRE OVHT SYS FAIL LIGHT ON. REPLACED M687 AND M688 LEFT OVHT LOOP 1 AND 2 CARDS, INSPECTED LEFT ENG PNEU DUCTS AND 
- [SDR DL767991612](https://openairdocs.org/sdr/DL767991612), Jul 18, 1999: LATCH. WORN. THE RT OVERWING SLIDE DOOR WOULD NOT OPEN MANUALLY DUE TO WORN SPOTS IN THE LATCH CAM PLATE. THE DOOR OPERATED NORMALLY AFTER REPLACING THE WORN LATCHES.
- [SDR DL767991227](https://openairdocs.org/sdr/DL767991227), Jun 1, 1999: COFFEEMAKER. DIRTY. ELECTRICAL SMELL IN FWD GALLEY AFTER LANDING, STRONG ODOR UTILITY BUSSES TURNED OFF. NO ELECTRICAL ODOR NOTED ON ENTRY. CKD ALL COMPONENTS IN GALLEY, ALL CK NOR
- [SDR DL767981281](https://openairdocs.org/sdr/DL767981281), Jun 9, 1998: SKIN. DELAMINATED. DELAMINATION WAS FOUND ON SEVERAL T/E WEDGES OF THE L/E SLATS (NR 1, 2, 4 AND 5). REPAIRED PER ERA 365004-14AD.
- [SDR DL767971849](https://openairdocs.org/sdr/DL767971849), Sep 20, 1997: HYD LINE. LEAKING. LT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AN APPROVED INTERIM LINE HAD BEEN INSTALLED AT MIA BECAUSE OF A HYDRAULIC LEAK. REPLACED LINE WITH PERMANE
- [SDR DL767971118](https://openairdocs.org/sdr/DL767971118), May 26, 1997: SKIN. DENTED. THE RT SIDE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BELOW THE C3 CARGO DOOR, RESULTING IN A DEEP DENT AT FS 1435 ABOVE STRINGER 35L. THE DAMAGE REQUIRES R
- [SDR DL767971010](https://openairdocs.org/sdr/DL767971010), May 25, 1997: POWER SUPPLY. INOPERATIVE. RT CEILING EMERGENCY LIGHTS OUT. REPLACED POWER SUPPLY M730.
- [SDR DL767970728](https://openairdocs.org/sdr/DL767970728), Apr 11, 1997: SKIN. CORRODED. DURING HMV, EXTENSIVE CORROSION WAS FOUND IN THE BELLY SKIN AND STRINGERS BETWEEN STA 1220 TO 1362 AND BETWEEN STRINGERS S-36L AND S-36R. THE FWD SKIN WAS TRIMM
- [SDR DL767970727](https://openairdocs.org/sdr/DL767970727), Apr 11, 1997: STRINGER. CORRODED. MTC DETERMINED THAT ALL STRINGERS FROM 34L TO 32R, EXCEPT 35R, ARE CORRODED BEYOND ALLOWABLE LIMITS. INSTRUCTIONS GIVEN TO SPLICE IN NEW STRINGER SECTIONS.
- [SDR DL767970729](https://openairdocs.org/sdr/DL767970729), Apr 7, 1997: SKIN. GOUGED. THE FUSELAGE SKIN WAS FOUND TO BE DAMAGED IN SEVERAL LOCATIONS AFT OF THE LOWER PORTION OF THE L2 DOOR CUTOUT. THE DAMAGE CONSISTED OF SEVERAL GOUGES, A DENT AN
- [SDR DL767970710](https://openairdocs.org/sdr/DL767970710), Apr 7, 1997: SKIN. DENTED. A FUSELAGE DENT RUNNING FROM S-39L TO S-34L AND BETWEEN FS 500 AND FS 552 WAS FOUND TO BE OUTSIDE OF ALLOWABLE DAMAGE LIMITS. THE DAMAGE REQUIRES A CUTOUT OF TH
- [SDR DL767970373](https://openairdocs.org/sdr/DL767970373), Feb 26, 1997: SKIN. CORROSION. DURING HMV, BULGING WAS DISCOVERED ON THE UPPER SURFACE OF THE CENTER WING, UPPER SKIN PANEL AT THE BUTT-SPLICE, BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRI
- [SDR DL767970305](https://openairdocs.org/sdr/DL767970305), Feb 13, 1997: SKIN. CORROSION. DURING AN INSPECTION OF THE FAR AFT BELLY SKIN, FURTHER CORROSION WAS FOUND AROUND A CUTOUT REPAIRED PREVIOUSLY BY DAL MTC PER SRM GUIDELINES. THE CUTOUT, APPRO
- [SDR DL767961183](https://openairdocs.org/sdr/DL767961183), May 16, 1996: WIRE. CUT. SECTION OF FLOOR TRACK LIGHTS INOP IN MID GALLEY. REPAIRED WIRING.
- [SDR DL767960487](https://openairdocs.org/sdr/DL767960487), Mar 4, 1996: PRESS LINE. LEAKING. LEFT HYDRAULIC SYSTEM FAILURE IN-FLIGHT. RETURNED DFW. FOUND ENGINE PRESSURE LINE WITH HOLE IN IT. REPLACED LINE.
- [SDR DL767954722](https://openairdocs.org/sdr/DL767954722), Dec 8, 1995: FAN. FAILED. IR - GASPER FAN OFF LIGHT ILLUMINATED WITH SWITCH ON AND ACCOMPANIED BY ELECTRICAL SMELL REPORTED IN CABIN. FORWARD TO MCO AND PLACKARD PER MEL. REPLACED GASPER
- [SDR DL767954656](https://openairdocs.org/sdr/DL767954656), Dec 7, 1995: EXTINGUISHER. LEAKING. VERBAL FROM CREW ON ARRIVAL, AFT CABIN WATER FIRE EXTINGUISHER LEAKING. REPLACED EXTINGUISHER.
- [SDR DL767953734](https://openairdocs.org/sdr/DL767953734), Sep 18, 1995: EEL. INOPERATIVE. AFT LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED AFT LEFT OVERWING EMERGENCY LIGHT. LIGHT OPS CHECK NORMAL.

## 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/N104DA/stcs.md

## Earlier aircraft with N104DA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N104DA before.

- [Cancelled 2007-06-06](https://openairdocs.org/deregistered/N104DA-2007-06-06): Mitsubishi MU-2B-36A, S/N 727SA. Exported to Brazil. Owner: [Woolie Enterprises Inc](https://openairdocs.org/faa-owner/WOOLIE%20ENTERPRISES%20INC), [Oldsmar, FL](https://openairdocs.org/faa-place/FL/Oldsmar)

## 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

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