# N610AW: 2004 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: 9143
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 6, 2018
- Certificate issued: April 7, 2025
- Expires: April 30, 2032
- Mode S code: A7EED3
- Registered owner: [Ms Hawker LLC](https://openairdocs.org/faa-owner/MS%20HAWKER%20LLC)
- Location: [Farmington Hills, MI](https://openairdocs.org/faa-place/MI/Farmington%20Hills)
- Owner type: LLC
- Owner's area on the map: 42.5043° N, 83.3492° W: Placed by OpenAirDocs at the center of ZIP code 48334, 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=610AW
- Page: https://openairdocs.org/aircraft/N610AW

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/N610AW/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 N610AW.

## FAA accident and incident reports

None matched to N610AW.

## Reports on N610AW not matched to an aircraft (1)

They name N610AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19971122042499I](https://openairdocs.org/incident/19971122042499I), Nov 22, 1997: Bac 146200A (N610AW), Milwaukee, WI. Narrative: according to the cabin crew, all carry-bags were properly stowed prior to departure from the denver airport. It could not be determined if the carry…

## 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 N610AW not matched to an aircraft (118, newest 50)

They name N610AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR A6WA200560017](https://openairdocs.org/sdr/A6WA200560017), Jul 30, 2005: APU. BIRD INGESTION. SMOKE IN CABIN WHEN TURNING ON PACKS. MAINTNANCE C/W EO, BOTH AC PACKS. FOUND BIRD AND OIL IN APU INTAKE. REMOVED AND REPLACED APU, BOTH AC PACKS, JET PUMPS AND
- [SDR A6WA20046002](https://openairdocs.org/sdr/A6WA20046002), Jun 13, 2004: ECU. MALFUNCTIONED. WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE 
- [SDR A6WA200360058](https://openairdocs.org/sdr/A6WA200360058), Oct 18, 2003: WIRE. LOOSE. DURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANC
- [SDR A6WA200360016](https://openairdocs.org/sdr/A6WA200360016), Apr 24, 2003: PANEL. CHAFED. NR 4 PYLON PANEL 481 AT LOWER FORWARD RIGHT ATTACH HOLE CHAFED BADLY FROM LOOSE AND VIBRATING SCREW. HOLE WORN EXCESSIVELY. REPAIRED PANEL IAW BARA/AVR/6361/03-
- [SDR A6WA200360015](https://openairdocs.org/sdr/A6WA200360015), Apr 23, 2003: SKIN. CRACKED. CRACKED IN HALF ABOVE PYLON NR 2 LEADING EDGE FIXED STRUCTURE. REMOVED AND REPLACED DOUBLER, P/N HC572H1080-001. 2 INCH CRACK TO NUTPLATE. PIECE INTACT, BUT CRA
- [SDR A6WA200360018](https://openairdocs.org/sdr/A6WA200360018), Apr 23, 2003: SKIN. DAMAGED. LEFT WING INBOARD LEADING EDGE HAS 1 HOLE ENLARGED IN TOP SKIN ABOVE NR 2 PYLON. REPAIRED IAW RIL HC572H9066 AND FAX BARA/AVR/6362/03-DC. (M)
- [SDR A6WA200360017](https://openairdocs.org/sdr/A6WA200360017), Apr 23, 2003: PANEL. DAMAGED. LT WING LEADING EDGE PANEL 464AT HAS SEVERAL ELONGATED HOLES. REPAIRED IAW RIL HC5459009 AND FAX BARA/AVR/6365/03-DC.
- [SDR 99ZZZX2702](https://openairdocs.org/sdr/99ZZZX2702), Aug 21, 1998: BRACKET. CRACKED. LEFT WING TE HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET.
- [SDR 99ZZZX2688](https://openairdocs.org/sdr/99ZZZX2688), Aug 21, 1998: STIFFENER. CRACKED. LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 5 AND 6 IS CRACKED AT FORWARD END. REPAIRED IAW BAE RDO DJR/RJ0630-98. REF: W/C 5035 FOR ALODINE PRIM
- [SDR 99ZZZM560](https://openairdocs.org/sdr/99ZZZM560), Aug 21, 1998: BRACKET. CRACKED. LEFT WING TE HYD LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. (M)
- [SDR 99ZZZM480](https://openairdocs.org/sdr/99ZZZM480), Aug 21, 1998: SCREW. DAMAGED. RIGHT WING SHORT STALL BAR PULLING OVER CORNER MOUNT SCREWS. REPAIRED SCREWS AS REQ'D IAW AVRO FAX DJR/RJO638-98, GCB/RJ1344-94, JEN/RJ1331-94. OK FOR SERVICE I
- [SDR 99ZZZX2689](https://openairdocs.org/sdr/99ZZZX2689), Aug 20, 1998: STIFFENER. CRACKED. LEFT WING TOP WING STIFFENER AFT OF REAR SPAR BETWEEN RIBS 8 AND 9 IS CRACKED AT FORWARD ENG. REPAIRED IAW BAE RDO EJR/RJ0630-98. REF: W/C 5035 FOR ALODINE, PRI
- [SDR 99ZZZX2685](https://openairdocs.org/sdr/99ZZZX2685), Aug 20, 1998: BEARING. WORN. RIGHT WING INNER FLAP TAB NR 1 HINGE BEARING IS WORN. REMOVED AND REPLACED RIGHT NR 1 FLAP TAB HINGE BEARING.
- [SDR 99ZZZX2675](https://openairdocs.org/sdr/99ZZZX2675), Aug 20, 1998: ANGLE. CRACKED. LEFT WING T/E, LOWER SHROUD STIFFENER, AND AFT TAG ANGLE CRACKED BETWEEN RIBS 7 AND 8. REPLACED LEFT WING T/R LOWER SHROUD STIFFENER AND AFT TAG ANGLE BETWEEN R
- [SDR 99ZZZX2674](https://openairdocs.org/sdr/99ZZZX2674), Aug 20, 1998: SKIN. DENTED. DENT LEFT FUSELAGE AT FRAME 47 BETWEEN STRINGERS 14 AND 16. REPAIRED DENT IAW BAE FAX REF DJR/RJ0620-98.
- [SDR 99ZZZX2696](https://openairdocs.org/sdr/99ZZZX2696), Aug 19, 1998: FLOOR. BROKEN. NR 9 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. ACFT TT: 19,327 HOURS. ACFT TC: 22,789.
- [SDR 99ZZZX2695](https://openairdocs.org/sdr/99ZZZX2695), Aug 19, 1998: FLOOR. BROKEN. NR 8 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-30-9804-06 OF PS-1.
- [SDR 99ZZZX2693](https://openairdocs.org/sdr/99ZZZX2693), Aug 19, 1998: FLOOR. BROKEN. NR 9 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2692](https://openairdocs.org/sdr/99ZZZX2692), Aug 19, 1998: FLOOR. BROKEN. NR 7 RT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW 25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2691](https://openairdocs.org/sdr/99ZZZX2691), Aug 19, 1998: FLOOR. BROKEN. NR 6 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9084-06 OF PS-I.
- [SDR 99ZZZX2690](https://openairdocs.org/sdr/99ZZZX2690), Aug 19, 1998: FLOOR. BROKEN. NR 8 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-96 (PART OF PS-1).
- [SDR 99ZZZX2687](https://openairdocs.org/sdr/99ZZZX2687), Aug 19, 1998: SKIN. DENTED. DENT AT BOXING JT RT FUSELAGE FORWARD OF REAR CARGO DOOR DUE REPAIR IN 3,000 CYCLES. CURRENT CYCLES: 29,794. REPAIR DUE BY 32,794 CYCLES. REPAIRED DENT IAW BAE 
- [SDR 99ZZZX2684](https://openairdocs.org/sdr/99ZZZX2684), Aug 19, 1998: FLOOR. BROKEN. NR 5 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2673](https://openairdocs.org/sdr/99ZZZX2673), Aug 19, 1998: FLOOR. BROKEN. NR 1 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.
- [SDR 99ZZZX2672](https://openairdocs.org/sdr/99ZZZX2672), Aug 19, 1998: FLOOR. BROKEN. NR 5 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.
- [SDR 99ZZZX2671](https://openairdocs.org/sdr/99ZZZX2671), Aug 19, 1998: FLOOR. BROKEN. NR 1 RT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2670](https://openairdocs.org/sdr/99ZZZX2670), Aug 19, 1998: FLOOR. BROKEN. NR 3 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2669](https://openairdocs.org/sdr/99ZZZX2669), Aug 19, 1998: FLOOR. BROKEN. NR 7 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2668](https://openairdocs.org/sdr/99ZZZX2668), Aug 19, 1998: FLOOR. BROKEN. NR 6 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE IAW DRAWING AW-25-20-9084-06 OF PSI-1.
- [SDR 99ZZZX2667](https://openairdocs.org/sdr/99ZZZX2667), Aug 19, 1998: FLOOR. BROKEN. NR 2 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2666](https://openairdocs.org/sdr/99ZZZX2666), Aug 19, 1998: FLOOR. BROKEN. NR 3 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2665](https://openairdocs.org/sdr/99ZZZX2665), Aug 19, 1998: FLOOR. BROKEN. NR 2 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.
- [SDR 99ZZZX2664](https://openairdocs.org/sdr/99ZZZX2664), Aug 19, 1998: FLOOR. BROKEN. NR 4 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804.
- [SDR 99ZZZM486](https://openairdocs.org/sdr/99ZZZM486), Aug 19, 1998: FLOOR. BROKEN. NR 4 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1, COMPLETED WEIGHT CHANGE NOTIFICATION FORM (ATTACHED) AND T
- [SDR 99ZZZX2686](https://openairdocs.org/sdr/99ZZZX2686), Aug 18, 1998: STIFFENER. CRACKED. RT WING T/E SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 9 AND 10. REPAIRED PER BAE FAX JM/RJ0317/97 USING 2024T3 .040 INCH AND AW FAX HC/142-97 AND
- [SDR 99ZZZM484](https://openairdocs.org/sdr/99ZZZM484), Aug 18, 1998: BRACKET. CRACKED. RIGHT WING TE TOP HYDRAULIC LINE CLAMP BRACKET CRACKED RIB NR 6. REMOVED AND REPLACED BRACKET. (M)
- [SDR 99ZZZM478](https://openairdocs.org/sdr/99ZZZM478), Aug 18, 1998: STIFFENER. CRACKED. RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 5/6. REMOVED AND REPLACED RIGHT WING TE SHROUD TOP STIFFENER. (M)
- [SDR 99ZZZM477](https://openairdocs.org/sdr/99ZZZM477), Aug 18, 1998: MOUNT. CRACKED. RIGHT LIFT SPOILER VALVE MOUNT PLATE CRACKED. REPLACED MOUNT PLATE. (M)
- [SDR 99ZZZM476](https://openairdocs.org/sdr/99ZZZM476), Aug 18, 1998: RIVET. LOOSE. RIGHT WING TE SHROUD TOP STIFFENER BETWEEN RIB 4/5 HAS LOOSE RIVET, AFT END. REMOVED AND REPLACED LOOSE RIVET. (M)
- [SDR 99ZZZM475](https://openairdocs.org/sdr/99ZZZM475), Aug 18, 1998: BRACKET. CRACKED. RIGHT WING TE LOWER HYDRAULIC LINE BRACKET CRACKED AT RIB NR 5. REMOVED BRACKET AND FABRICATED NEW BRACKET PER DRAWING HC9 32H0211. INSTALLED BRACKET AND ATTACH
- [SDR 99ZZZM481](https://openairdocs.org/sdr/99ZZZM481), Aug 17, 1998: BEARING. WORN. RIGHT AILERON OUTBOARD HINGE 'A' FRAME BEARINGS WORN. REMOVED AND REPLACED RIGHT AILERON OUTBOARD 'A' FRAME. W/C GEN FOR FUNCTIONAL CHECK. (M)
- [SDR 99ZZZM482](https://openairdocs.org/sdr/99ZZZM482), Aug 14, 1998: STIFFENER. CRACKED. RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END AND RIVET POPPED (AFT END) BETWEEN RIBS 3/4. REPLACED RIGHT WING TRAILING EDGE SHROUD TOP STIFFENER BE
- [SDR 99ZZZM479](https://openairdocs.org/sdr/99ZZZM479), Aug 14, 1998: STIFFENER. CRACKED. TE RIGHT WING TOP SHROUD STIFFENER OUTBOARD CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED RIGHT WING TRAILING EDGE SHROUD TO STIFFENER BETWEEN RIBS 8/9. (M)
- [SDR 99ZZZX2694](https://openairdocs.org/sdr/99ZZZX2694), Aug 13, 1998: SKIN. DENTED. REPAIR DENT ON LEFT SIDE OF FUSELAGE AT FRAME 9, 3.25 INCHES BELOW SKIN LAP B AND 4.00 INCHES FORWARD OF FRAME 9 IN 3,000 CYCLES. CURRENT TCA 29,540 DUE AT 32,5
- [SDR 99ZZZX2683](https://openairdocs.org/sdr/99ZZZX2683), Aug 13, 1998: SUB FRAME. CRACKED. SUB-FRAME AFT OF FRAME 50 CRACKED AT LOWER LT CORNER. REPAIRED SUB-FRAME AFT OF FRAME 50 AT LOWER LT CORNER IAW BAE FAX DJR/RJ0602-98.
- [SDR 99ZZZX2676](https://openairdocs.org/sdr/99ZZZX2676), Aug 13, 1998: RIVET. LOOSE. NUMEROUS LOOSE RIVETS AT LT WING T/E LOWER SKIN, AFT OF REAR SPAR. REMOVED AND REPLACED NUMEROUS LOOSE RIVETS ON LT WING T/E LOWER SKIN AFT OF REAR SPAR.
- [SDR 99ZZZM485](https://openairdocs.org/sdr/99ZZZM485), Aug 13, 1998: SKIN. DENTED. COMPLIED WITH REPAIR OF 2 DENTS AT FRAME 20, STRINGER 20, PORT SIDE IAW SRM 53-00-12 FIG 202 WITHIN 3000 CYCLES, CURRENT CYCLES 29320, DUE BY 32320 CYCLES. REPA
- [SDR 99ZZZX2682](https://openairdocs.org/sdr/99ZZZX2682), Aug 12, 1998: LONGERON. CRACKED. ATTACHMENT ANGLE/GUSSET AT THE AFT END OF THE UPPER MOST LEFT AIRBRAKE HINGE LONGERON IS CRACKED. FABRICATED LEFT GUSSET PLATE PER BAE DRAWING HC539H0229. REPLA
- [SDR 99ZZZM483](https://openairdocs.org/sdr/99ZZZM483), Aug 12, 1998: STIFFENER. CRACKED. LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8 IS CRACKED AT FORWARD END. REMOVED AND REPLACED TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 
- [SDR 99ZZZX2679](https://openairdocs.org/sdr/99ZZZX2679), Aug 11, 1998: FRAME. CHAFED. NR 1 ENGINE FORWARD LEFT COWL DOOR LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE LEFT FORWARD COWL DOOR LOWER AFT FRAME IAW SRM 54-10-11.

All 118: https://openairdocs.org/aircraft/N610AW/unmatched-reports.md

## 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/N610AW/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

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