# N730AS: 2023 Bombardier BD-100-1A10

- Status: Valid registration
- Airframe: [Bombardier BD-100-1A10](https://openairdocs.org/model/bombardier-bd-100-1a10) (registry code 1390044, 8 seats)
- Engine: [Honeywell AS907-2-1A](https://openairdocs.org/engine/honeywell-as907-2-1a) (registry code 33401)
- Data sheets: [TCDS T00005NY](https://openairdocs.org/tcds/T00005NY) (Bombardier Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 20948
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 28, 2023
- Certificate issued: September 5, 2025
- Expires: September 30, 2032
- Mode S code: A9CB1C
- Registered owners: [Bjaup LLC](https://openairdocs.org/faa-owner/BJAUP%20LLC), [Fowler Aviation LLC](https://openairdocs.org/faa-owner/FOWLER%20AVIATION%20LLC), [Hw Transit LLC](https://openairdocs.org/faa-owner/HW%20TRANSIT%20LLC), [Ima Financial Group Inc](https://openairdocs.org/faa-owner/IMA%20FINANCIAL%20GROUP%20INC), [Mac Benefit Advisor Co](https://openairdocs.org/faa-owner/MAC%20BENEFIT%20ADVISOR%20CO), [Pioneer Nutrition LLC](https://openairdocs.org/faa-owner/PIONEER%20NUTRITION%20LLC)
- Location: [Overland Park, KS](https://openairdocs.org/faa-place/KS/Overland%20Park)
- Owner type: Co-owned, fractional ownership
- Owner's area on the map: 38.9251° N, 94.6356° W: Placed by OpenAirDocs at the center of ZIP code 66211, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=730AS
- Page: https://openairdocs.org/aircraft/N730AS

From the FAA registry file of October 22, 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): 55 in force

### Matched by airframe (Bombardier BD-100-1A10)

- [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 2026-02-06](https://openairdocs.org/ad/2026-02-06): Flight controls · Bombardier BD-100-1A10. Effective Feb 25, 2026
- [AD 2026-01-07](https://openairdocs.org/ad/2026-01-07): Time Limits/Maintenance Checks · Bombardier BD-100-1A10. Effective Feb 20, 2026
- [AD 2025-02-01](https://openairdocs.org/ad/2025-02-01): Flight controls · Bombardier BD-100-1A10. Effective Mar 17, 2025
- [AD 2024-21-04](https://openairdocs.org/ad/2024-21-04): Electrical Power · Bombardier BD-100-1A10. Effective Dec 17, 2024
- [AD 2024-18-03](https://openairdocs.org/ad/2024-18-03): Electrical Power · Bombardier BD-100-1A10. Effective Nov 12, 2024
- [AD 2024-16-18](https://openairdocs.org/ad/2024-16-18): Nacelles/Pylons · Bombardier BD-100-1A10. Effective Oct 30, 2024
- [AD 2024-16-13](https://openairdocs.org/ad/2024-16-13): Ice and Rain Protection · Bombardier BD-100-1A10. Effective Oct 29, 2024
- [AD 2024-16-04](https://openairdocs.org/ad/2024-16-04): Equipment/Furnishings · Bombardier BD-100-1A10. Effective Oct 23, 2024
- [AD 2024-11-02](https://openairdocs.org/ad/2024-11-02): Stabilizer · Bombardier BD-100-1A10. Effective Aug 26, 2024
- [AD 2024-01-09](https://openairdocs.org/ad/2024-01-09): Landing gear · Bombardier BD-100-1A10. Effective Mar 21, 2024
- [AD 2023-26-02](https://openairdocs.org/ad/2023-26-02): Pneumatic · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 27, 2024
- [AD 2023-23-05](https://openairdocs.org/ad/2023-23-05): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 14, 2023
- [AD 2023-13-06](https://openairdocs.org/ad/2023-13-06): Time limits/maintenance checks, Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Sep 1, 2023
- [AD 2023-14-11](https://openairdocs.org/ad/2023-14-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 10, 2023
- [AD 2023-12-06](https://openairdocs.org/ad/2023-12-06): Auto flight · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 7, 2023
- [AD 2023-11-04](https://openairdocs.org/ad/2023-11-04): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 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 2023-03-18](https://openairdocs.org/ad/2023-03-18): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 4, 2023
- [AD 2023-02-01](https://openairdocs.org/ad/2023-02-01): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 14, 2023
- [AD 2022-12-02](https://openairdocs.org/ad/2022-12-02): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 21, 2022
- [AD 2022-09-02](https://openairdocs.org/ad/2022-09-02): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 16, 2022
- [AD 2022-03-11](https://openairdocs.org/ad/2022-03-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 17, 2022
- [AD 2021-25-07](https://openairdocs.org/ad/2021-25-07): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 15, 2022
- [AD 2021-23-14](https://openairdocs.org/ad/2021-23-14): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 10, 2022
- [AD 2021-14-01](https://openairdocs.org/ad/2021-14-01): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 24, 2021
- [AD 2021-10-26](https://openairdocs.org/ad/2021-10-26): Hydraulic power · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 6, 2021
- [AD 2021-09-17](https://openairdocs.org/ad/2021-09-17): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 23, 2021
- [AD 2021-09-16](https://openairdocs.org/ad/2021-09-16): Pneumatic; Engine Fuel and Control · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 1, 2021
- [AD 2021-03-10](https://openairdocs.org/ad/2021-03-10): Fire protection · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 31, 2021
- [AD 2020-25-06](https://openairdocs.org/ad/2020-25-06): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 27, 2021
- [AD 2020-11-14](https://openairdocs.org/ad/2020-11-14): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 2020
- [AD 2020-11-10](https://openairdocs.org/ad/2020-11-10): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 14, 2020
- [AD 2019-15-04](https://openairdocs.org/ad/2019-15-04): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 23, 2019
- [AD 2019-03-29](https://openairdocs.org/ad/2019-03-29): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 6, 2019
- [AD 2019-07-06](https://openairdocs.org/ad/2019-07-06): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective May 28, 2019
- [AD 2018-20-16](https://openairdocs.org/ad/2018-20-16): Hydraulic Power · Bombardier BD-100-1A10 (Challenger 300). Effective Nov 23, 2018
- [AD 2018-14-05](https://openairdocs.org/ad/2018-14-05): SUMMARY: We are adopting a new airworthiness directive (AD) for certain  
 Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by reports  
 of fire incidents of the auxiliary power unit (APU) inlet, which caused tail  
 cone damage after an initial failed APU start followed by two or more in-flight  
 APU start attempts. This AD requires modification of the APU electronic control  
 unit (ECU) wiring harness. We are issuing this AD to address the unsafe · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 13, 2018
- [AD 2018-13-04](https://openairdocs.org/ad/2018-13-04): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 25, 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 2017-17-13](https://openairdocs.org/ad/2017-17-13): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Oct 2, 2017
- [AD 2017-14-16](https://openairdocs.org/ad/2017-14-16): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 1, 2017
- [AD 2017-12-11](https://openairdocs.org/ad/2017-12-11): Equipment/ Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 20, 2017
- [AD 2017-11-12](https://openairdocs.org/ad/2017-11-12): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 11, 2017
- [AD 2016-02-05](https://openairdocs.org/ad/2016-02-05): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 8, 2016
- [AD 2015-26-03](https://openairdocs.org/ad/2015-26-03): Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 2, 2016
- [AD 2015-23-07](https://openairdocs.org/ad/2015-23-07): Electrical Power · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 22, 2015
- [AD 2015-15-08](https://openairdocs.org/ad/2015-15-08): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 28, 2015
- [AD 2014-05-23](https://openairdocs.org/ad/2014-05-23): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 15, 2014
- [AD 2012-12-17](https://openairdocs.org/ad/2012-12-17): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 30, 2012

### Matched by engine (Honeywell AS907-2-1A)

- [AD 2018-04-13](https://openairdocs.org/ad/2018-04-13): Engine Controls Section · Honeywell International AS907-1-1A, AS907-2-1A, AS907-2-1G and 1 more. Effective Apr 12, 2018

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

- [AD 2023-11-01](https://openairdocs.org/ad/2023-11-01) (historical): Electrical Power · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 15, 2023
- [AD 2020-07-13](https://openairdocs.org/ad/2020-07-13) (historical): Auto flight · Bombardier BD-100-1A10 (Challenger 300). Effective May 18, 2020
- [AD 2013-11-12](https://openairdocs.org/ad/2013-11-12) (historical): Hydraulic Power · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 9, 2013
- [AD 2011-07-10](https://openairdocs.org/ad/2011-07-10) (historical): Air conditioning · Bombardier BD-100-1A10 (Challenger 300). Effective May 5, 2011
- [AD 2010-10-18](https://openairdocs.org/ad/2010-10-18) (historical): Air conditioning and Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 1, 2010
- [AD 2009-25-13](https://openairdocs.org/ad/2009-25-13) (historical): Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 28, 2009

All 61: https://openairdocs.org/aircraft/N730AS/ads.md

## Information bulletins (advisory) (2 in force)

- [SAIB AIR-22-02R1](https://openairdocs.org/saib/AIR-22-02R1): PITOT/STATIC ANTI-ICE SYSTEM. Issued May 17, 2022
- [SAIB NM-18-32R1](https://openairdocs.org/saib/NM-18-32R1): Electrical Power - Direct Current Power Center. Issued Mar 22, 2021
- [SAIB AIR-22-02](https://openairdocs.org/saib/AIR-22-02) (historical): PITOT/STATIC ANTI-ICE SYSTEM. Issued Feb 25, 2022
- [SAIB NM-18-32](https://openairdocs.org/saib/NM-18-32) (historical): Electrical Power - Direct Current Power Center. Issued Dec 3, 2018

## NTSB investigations

None matched to N730AS.

## FAA accident and incident reports

None matched to N730AS.

## Reports on N730AS not matched to an aircraft (6)

They name N730AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20040509007719I](https://openairdocs.org/incident/20040509007719I), May 9, 2004: Boeing 737290C (N730AS), Juneau, AK. (-23) Asa flight 64 on takeoff/climbout, crew had unsafe door indication (L2 door) returned to Juneau without further incident. Alaska airlines maintenance…
- [Accident 19940719018879A](https://openairdocs.org/incident/19940719018879A), Jul 19, 1994: Boeing 737290C (N730AS), Nome, AK, Substantial damage. During takeoff roll, hit a seagull and aborted takeoff.
- [Incident 19891204059729I](https://openairdocs.org/incident/19891204059729I), Dec 4, 1989: Boeing 737290C (N730AS), Juneau, AK. Flaps malfunctioned hydraulically. Reset electrically and landed safely.
- [Incident 19890215009559I](https://openairdocs.org/incident/19890215009559I), Feb 15, 1989: Boeing 737290C (N730AS), Nome, AK. Found left inboard wheel assembly missing after landing. Later found at departure site. No cause stated.
- [Incident 19860921051319I](https://openairdocs.org/incident/19860921051319I), Sep 21, 1986: Boeing 737290C (N730AS), Fairbanks, AK. Unscheduled landing after epr gauge malfunctioned.
- [Incident 19860702044019I](https://openairdocs.org/incident/19860702044019I), Jul 2, 1986: Boeing 737290C (N730AS), Kotzebue, AK. Returned after bird was ingested in NR1 engine during takeoff.

## 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 N730AS not matched to an aircraft (393, newest 50)

They name N730AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASAA0510041](https://openairdocs.org/sdr/ASAA0510041), Apr 11, 2006: SEAT TRACK. CORRODED. YXX-RT OB SEAT TRACK CORRODED AT BSTA 520-540. INSTALLED NEW SEAT TRACK. (K)
- [SDR ASAA0610132](https://openairdocs.org/sdr/ASAA0610132), Feb 5, 2006: SKIN. DENTED. FOUND EXTERNAL DENT BETWEEN STR 27R 27L AT BSTA 960. CUTOUT DAMAGED SKIN FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53 30 3 FIG 48.
- [SDR ASAA0610131](https://openairdocs.org/sdr/ASAA0610131), Feb 5, 2006: REPAIR. DAMAGED. AFT ACCY BAY FRAME REPAIR AT BS 967 BL 0 DOUBLER IS GAPPED AT BOTH ENDS OF UPPER FRAME. REPAIRED FRAME DOUBLER PER EA 5310 02566.
- [SDR ASAA0610130](https://openairdocs.org/sdr/ASAA0610130), Feb 5, 2006: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AND BENT AT LWR CENTER LINE OF ACFT AT BSTA 947.5. FABRICATED NEW INTERCOSTAL AND INSTALLED PER SRM 51-20-1.
- [SDR ASAA0510089](https://openairdocs.org/sdr/ASAA0510089), Apr 20, 2005: STRINGER. CRACKED. YXX - FOUND STRINGER 13R AT BS 500A PLUS 15 INCHES CRACKED. CRACK REMOVED AT STRINGER 13R BS 500A PLUS 15 INCHES PER EA 5330-01918. (M)
- [SDR ASAA0510088](https://openairdocs.org/sdr/ASAA0510088), Apr 20, 2005: FUEL TANK. CORRODED. YXX - FOUND FUEL CENTER TANK CORRODED AT UPPER STRUCTURE AT BS 578 LBL 67. CORROSION REMOVED IAW EA 5710-01119. (M)
- [SDR ASAA0510087](https://openairdocs.org/sdr/ASAA0510087), Apr 20, 2005: SKIN. CORRODED. YXX - AROUND CARGO SKIN AT STRINGER 27L BS 817-837 CORROSION FOUND UPON REMOVAL OF STRINGER. CORROSION REMOVED IAW B737-200 SRM 53-30-3 FIG 48. (M)
- [SDR ASAA0510086](https://openairdocs.org/sdr/ASAA0510086), Apr 20, 2005: CHANNEL. CORRODED. YXX - AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES HAVE CORROSION AT BS 847 PLUS 15 INCHES RBL 8. AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES C
- [SDR ASAA0510084](https://openairdocs.org/sdr/ASAA0510084), Apr 20, 2005: STRINGER. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE BS 470, STRINGER 22L. REPAIRED AND REMOVED CRACK IAW B737-200 SRM 53-10-3 FIG 1. (M)
- [SDR ASAA0510083](https://openairdocs.org/sdr/ASAA0510083), Apr 20, 2005: SHEAR TIE. CRACKED. YXX - FOUND NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BS 480, BETWEEN STRINGER 18L AND 19L. REPLACED SHEAR TIE AND CRACK REMOVED IAW B737-200 
- [SDR ASAA0510082](https://openairdocs.org/sdr/ASAA0510082), Apr 20, 2005: STRINGER. CRACKED. YXX - NDT CRACK INDICATIONS AT FASTENERS HOLES ON STRINGER 19 LEFT, BS 460-480. CRACK REMOVED IAW B737-200 SRM 53-10-3 FIGURE 1. (M)
- [SDR ASAA0510080](https://openairdocs.org/sdr/ASAA0510080), Apr 19, 2005: WINDOW FRAME. CRACKED. YXX - FOUND LOWER AFT CORNER OF WINDOW FRAME CRACKED IN FASTENER HOLE AT BS 500A PLUS 15 INCHES RT. REPAIRED IAW ERO 3774 CRACK REMOVED ERO 3774 STEP 1.1. (M)
- [SDR ASAA0510079](https://openairdocs.org/sdr/ASAA0510079), Apr 19, 2005: DOUBLER. CORRODED. YXX - UPON REMOVAL OF PREVIOUS REPAIR AT BS 500B PLUS 17 INCHES CORROSION ON RT KEEL BEAM AT BS 535. REPAIRED IAW ERO 3838 AND 3846 AND EA 5310-02458. CORROSION
- [SDR ASAA0510076](https://openairdocs.org/sdr/ASAA0510076), Apr 17, 2005: KEELBEAM. CORRODED. YXX - FOUND LEFT KEEL BEAM CORROSION AT BS 535 ON LOWER FLANGE. REPAIRED IAW RO 3838 AND EA 5310-02458. (M)
- [SDR ASAA0510075](https://openairdocs.org/sdr/ASAA0510075), Apr 16, 2005: SKIN. CORRODED. FOUND CORROSION ON FUSELAGE SKIN IN FORWARD BILGE AT BS 500B PLUS 17 INCHES OUTBOARD OF STRINGER 28 RT. REPAIRED IAW EA 5330-01925. (M)
- [SDR ASAA0510073](https://openairdocs.org/sdr/ASAA0510073), Apr 16, 2005: FRAME. GOUGED. YXX - FORWARD CARGO FRAME ANGLE AT BS 4600, 3 INCHES BELOW STRINGER 20L HAS GOUGE. REPAIRED IAW B737-200 SRM 53-10-04 FIG 10 AND EA 5330-01923. (M)
- [SDR ASAA0510072](https://openairdocs.org/sdr/ASAA0510072), Apr 16, 2005: FUEL TANK. CORRODED. YXX - FUEL CENTER TANK CORRODED AT UPPER SURFACE BS 578 RBL 67. REPAIRED IAW EA 5710-01118. (M)
- [SDR ASAA0510078](https://openairdocs.org/sdr/ASAA0510078), Apr 15, 2005: KEELBEAM. DAMAGED. YXX - RIGHT KEEL BEAM SUPPORT ANGLE AT BS 520 TO 535 HAS PREVIOUS DAMAGE. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-10-1 PARAGRAPH 5A
- [SDR ASAA0510077](https://openairdocs.org/sdr/ASAA0510077), Apr 15, 2005: SHEAR TIE. DAMAGED. YXX - FOUND BS 520 SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 27R AND 28R DISPLACED FROM PREVIOUS REPAIRS. REPLACED ATTACH ANGLES IAW B737-200 SRM 53-10-4 FIGU
- [SDR ASAA0510069](https://openairdocs.org/sdr/ASAA0510069), Apr 15, 2005: WEB. CORRODED. YXX - FOUND FLOOR WEB AT RT BS 578-597 CORRODED. REPLACED FLOOR WEB RT BS 578-597 WITH MADE REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-30-2 FIGURE 3. (M)
- [SDR ASAA0510068](https://openairdocs.org/sdr/ASAA0510068), Apr 15, 2005: SHEAR TIE. DAMAGED. YXX - BS 520 FRAME TO SKIN ATTACHMENT AT STRINGER 28L TO STRINGER 27 HAS LOW EDGE MARGIN. REPLACED ATTACHMENT PER B737-200 SRM 53-10-4 FIGURE 6. (M)
- [SDR ASAA0510067](https://openairdocs.org/sdr/ASAA0510067), Apr 15, 2005: SHEAR TIE. DAMAGED. YXX - FOUND SHEAR TIE AT BS 480 BETWEEN STRINGER 20L AND 21L HAS LOW EDGE MARGIN. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-30-2 PARA 4.
- [SDR ASAA0510062](https://openairdocs.org/sdr/ASAA0510062), Apr 14, 2005: SKIN. CRACKED. YXX- CRACK AT FASTENER, WINDOW 6R BSTA 455R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 6R BSTA 455 LOWER AT CORNER REPAIRED IAW EA. (K)
- [SDR ASAA0510061](https://openairdocs.org/sdr/ASAA0510061), Apr 14, 2005: ATTACH ANGLE. CORRODED. YXX- FWD CARGO SKIN-TO-FRAME ATTACH ANGLE AT BSTA 500 AND STR 28 LT CORRODED. REPAIRED WITH MADE REPAIR PART. (K)
- [SDR ASAA0510065](https://openairdocs.org/sdr/ASAA0510065), Apr 14, 2005: FRAME. CRACKED. FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED. FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED FRAME REPAIRED IAW SRM. (K)
- [SDR ASAA0510064](https://openairdocs.org/sdr/ASAA0510064), Apr 14, 2005: SKIN. CRACKED. CRACK AT FASTENER, WINDOW 10R BSTA 500A=15R-LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 10R BSTA 500A=15R LOWER AFT CORNER REPAIRED IAW EA. (K)
- [SDR ASAA0510063](https://openairdocs.org/sdr/ASAA0510063), Apr 14, 2005: SKIN. CRACKED. CRACK AT FASTENER, WINDOW 8R BSA 495R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 8R BSTA 495 LOWER AFT CORNER REPAIRED IAW EA. (K)
- [SDR ASAA0510071](https://openairdocs.org/sdr/ASAA0510071), Apr 14, 2005: STRINGER. CORRODED. YXX - FOUND CORROSION IN AFT CARGO PIT ON STRINGER 21L AT BS 940. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)
- [SDR ASAA0510053](https://openairdocs.org/sdr/ASAA0510053), Apr 11, 2005: STRINGER. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLES ON STR 20L, BSTA 460-481. REPAIRED IAW SRM. (K)
- [SDR ASAA0510052](https://openairdocs.org/sdr/ASAA0510052), Apr 11, 2005: STRINGER. CRACKED. YXX- NDT CRACK INDICATION AT FASTENER HOLES ON STR 19L, BSTA 460-480. REPAIRED IAW SRM. (K)
- [SDR ASAA0510051](https://openairdocs.org/sdr/ASAA0510051), Apr 11, 2005: SHEAR TIE. CRACKED. YXX- NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 18L AND STR 19L. REPLACED SHEAR TIE ANGLE IAW SRM. (K)
- [SDR ASAA0510050](https://openairdocs.org/sdr/ASAA0510050), Apr 11, 2005: SHEAR TIE. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 19L AND STR 20L. REPLACED SHEAR TIE ANGLE IAW SRM. (K)
- [SDR ASAA0510049](https://openairdocs.org/sdr/ASAA0510049), Apr 11, 2005: FRAME. CRACKED. YXX- NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 19L AND STRINGER 20L. REPAIRED FRAME IAW SRM. (K)
- [SDR ASAA0510048](https://openairdocs.org/sdr/ASAA0510048), Apr 11, 2005: FRAME. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 20L AND STRINGER 21L. REPAIRED FRAME IAW SRM. (K)
- [SDR ASAA0510047](https://openairdocs.org/sdr/ASAA0510047), Apr 11, 2005: FRAME. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 21L AND STRINGER 22L. REPAIRED FRAME IAW SRM. (K)
- [SDR ASAA0510046](https://openairdocs.org/sdr/ASAA0510046), Apr 11, 2005: FRAME. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 20L AND STRINGER 22L. REPAIRE FRAME IAW SRM. (K)
- [SDR ASAA0510045](https://openairdocs.org/sdr/ASAA0510045), Apr 11, 2005: FRAME. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 19L STRINGER 20L. REPAIRED FRAME IAW SRM. (K)
- [SDR ASAA0510044](https://openairdocs.org/sdr/ASAA0510044), Apr 11, 2005: STRINGER. CRACKED. YXX - STRINGER 20L AT BSTA 390 CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM. (K)
- [SDR ASAA0510043](https://openairdocs.org/sdr/ASAA0510043), Apr 11, 2005: STRINGER. CRACKED. YXX - NDT CRACK INDICATION AT FASTENER HOLE BSTA 470, STR 22L. REPAIRED IAW SRM. (K)
- [SDR ASAA0510042](https://openairdocs.org/sdr/ASAA0510042), Apr 11, 2005: SKIN. TOOL DAMAGE. YXX - BONDED DOUBLER AND AIRCRAFT SKIN DAMAGED AT BSTA 827 AT STR 21L BY TOOL. BONDED DOUBLER AND AIRCRAFT SKIN AT BSTA 827 AT STR 21L REPAIRED IAW SRM. (K)
- [SDR ASAA0510058](https://openairdocs.org/sdr/ASAA0510058), Apr 11, 2005: SHEAR TIE. CORRODED. SHEAR TIE AT BSTA 967 BETWEEN STRINGER 27L THRU 27R HAS CORROSION. SHEAR TIE BETWEEN STRINGER 27L AND 22R REPAIRED IAW SRM. (K)
- [SDR ASAA0510057](https://openairdocs.org/sdr/ASAA0510057), Apr 11, 2005: ATTACH FITTING. OUT OF TOLERANCE. BSTA 460 BETWEEN STRINGER 20L AND 21L SKIN TO FRAME ATTACHMENT HAS LOW EDGE MARGIN. REPAIRED IAW SRM. (K)
- [SDR ASAA0510056](https://openairdocs.org/sdr/ASAA0510056), Apr 11, 2005: SHEAR TIE. OUT OF TOLERANCE. SHEAR TIE ANGLE BSTA 460 BETWEEN STR 19 AND 20 HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K)
- [SDR ASAA0510055](https://openairdocs.org/sdr/ASAA0510055), Apr 11, 2005: SHEAR TIE. DAMAGED. SHEAR TIE ANGLE BS 460 BETWEEN STR 20L AND 21L HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K)
- [SDR ASAA0510054](https://openairdocs.org/sdr/ASAA0510054), Apr 11, 2005: SHEAR TIE. DAMAGED. BSTA 480 BETWEEN STR 20L AND 21L SHEAR TIE ANGLE HAS LOW EDGE MARGIN. REPLACED ANGLE IAW SRM. (K)
- [SDR ASAA0510040](https://openairdocs.org/sdr/ASAA0510040), Apr 4, 2005: FRAME. CRACKED. YXX - FWD CARGO BSTA 480 FRAME CRACKED NEAR STR 22L. FRAME REPAIRED IAW SRM. (K)
- [SDR ASAA0510039](https://openairdocs.org/sdr/ASAA0510039), Apr 4, 2005: STRINGER. CORRODED. YXX- AFT CARGO PIT BSTA 827, STR 23L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 23L REPAIRED IAW SRM. (K)
- [SDR ASAA0510038](https://openairdocs.org/sdr/ASAA0510038), Apr 4, 2005: STRINGER. CORRODED. YXX - AFT CARGO PIT BSTA 827, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 21L REPAIRED IAW SRM. (K)
- [SDR ASAA0510037](https://openairdocs.org/sdr/ASAA0510037), Apr 4, 2005: STRINGER. CORRODED. YXX- AFT CARGO PIT BSTA 907, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907, STR 21L REAPIRED IAW SRM. (K)
- [SDR ASAA0510034](https://openairdocs.org/sdr/ASAA0510034), Apr 4, 2005: SPLICE. CORRODED. AFT CARGO PIT BSTA 907, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907 STR 26L SPLICE REPALCED WITH MADE PART IAW SRM. (K)

All 393: https://openairdocs.org/aircraft/N730AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (141, 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-100-1A10)

- [STC ST11935CH](https://openairdocs.org/stc/ST11935CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC 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 ST12288IB](https://openairdocs.org/stc/ST12288IB): Demonstration of TPED Tolerance. Bombardier Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12036WI](https://openairdocs.org/stc/ST12036WI): Installation of Gogo Business Aviation Galileo Half-Duplex (HDX). Gogo Business Aviation LLC
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST04560AT](https://openairdocs.org/stc/ST04560AT): Replacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assemblies. Quiet Technology Aerospace
- [STC ST01569LA](https://openairdocs.org/stc/ST01569LA): 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 ST02691SE](https://openairdocs.org/stc/ST02691SE): Installation of Head-up Display System (HUD) Model 6650 and Enhance Vision System (EVS) Model 3600. Rockwell Collins Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST00200IB](https://openairdocs.org/stc/ST00200IB): Installation of Gogo AVANCE L5 System. Sky Service F.B.O. Inc
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01970WI](https://openairdocs.org/stc/ST01970WI): Installation of an Aircraft Health Management System (AHMS). Learjet Inc
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02765LA](https://openairdocs.org/stc/ST02765LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc
- [STC ST04544CH](https://openairdocs.org/stc/ST04544CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388. StandardAero Business Aviation Services LLC
- [STC ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace LLC
- [STC ST01991WI](https://openairdocs.org/stc/ST01991WI): Installation of Switch Bezels. Duncan Aviation Inc
- [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd
- [STC ST04490CH](https://openairdocs.org/stc/ST04490CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388 in accordance with StandardAero Master Data List 1039044, Revision (B), dated November 13, 2020 or later FAA approved revision. Learjet Inc
- [STC ST02293SE](https://openairdocs.org/stc/ST02293SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Aerospace Corp
- [STC ST04508CH](https://openairdocs.org/stc/ST04508CH): Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome in accordance with Master Data List (MDL), 1039410, Revision (F), dated November 05, 2021, or later FAA Approved Revision. StandardAero Business Aviation Services LLC
- [STC ST02047NY](https://openairdocs.org/stc/ST02047NY): Modification of Complete Custom Aircraft Interior to be completed. Bombardier Aerospace
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04455CH](https://openairdocs.org/stc/ST04455CH): Installation of a Viasat Ka Radome in accordance with StandardAero Master Data List 1038145, Revision (E), dated November 13, 2020 or later FAA approved revision. Learjet Inc
- [STC ST04457CH](https://openairdocs.org/stc/ST04457CH): Installation of a Viasat Ka Terminal in accordance with StandardAero Master Data List 1038079, Revision (B), dated November 14, 2020 or later FAA approved revision. Learjet Inc
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST04352NY](https://openairdocs.org/stc/ST04352NY): Installation of Fire Extinguishers with Halocarbon Clean Extinguishing Agents. Bombardier Inc
- [STC ST04391NY](https://openairdocs.org/stc/ST04391NY): Installation of Galley with Compartment for Commercial-off-the-shelf (COTS) Appliances or Equipment. Bombardier Inc
- [STC ST00923DE](https://openairdocs.org/stc/ST00923DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00395BO](https://openairdocs.org/stc/ST00395BO): Installation of a Honeywell GoDirect Router. Pro Star Aviation, LLC
- [STC ST04236NY](https://openairdocs.org/stc/ST04236NY): Installation of Lavatory Glass Mirror. Bombardier Inc
- [STC ST00267BO](https://openairdocs.org/stc/ST00267BO): Installation of a Honeywell HD-710 High Speed Data Receiver, EMS AMT-50 High Gain Antenna System, and EMS CNX-200 Cabin Network Router in accordance with Pro Star Aviation Master Document List 20674-MDL-02, Revision D, dated March 17, 2008, or later FAA-approved revision. Pro Star Aviation, LLC
- [STC ST00268BO](https://openairdocs.org/stc/ST00268BO): Installation of an EMS Satcom AMT-50 High Gain Antenna System. Pro Star Aviation, LLC
- [STC ST02130LA](https://openairdocs.org/stc/ST02130LA): Installation of Honeywell MKV Enhanced Ground Proximity Warning System (EGPWS) with Runway Awareness and Advisory System (RAAS). Pro Star Aviation, LLC
- [STC ST04148NY](https://openairdocs.org/stc/ST04148NY): Installation of the Rockwell Collins TDR-94D ADS-B Out Upgrade. Mid Canada Mod Center
- [STC ST02976NY](https://openairdocs.org/stc/ST02976NY): Installation of ADS-B Out System in the Bombardier BD-100-1A10 (CH 300) aircraft with Rockwell Collins Pro Line 21 Series Avionics System. Flying Colours Corp
- [STC ST04123NY](https://openairdocs.org/stc/ST04123NY): Installation of Bleed Air Leak Detection System Loop Element Shell and Insert Assembly Replacement. Bombardier Inc
- [STC ST04290CH](https://openairdocs.org/stc/ST04290CH): Wireless Local Area Network (WLAN) Cabin Router and Aircraft Transmitting Portable Electronic Device (TPED) Compatibility. Comlux America LLC
- [STC ST00896DE](https://openairdocs.org/stc/ST00896DE): Installation of a 3-Place Side-Facing Divan. Lee Products Engineering Services, Inc

All 141: https://openairdocs.org/aircraft/N730AS/stcs.md

## Related

- Other Bombardier BD-100-1A10 aircraft: https://openairdocs.org/model/bombardier-bd-100-1a10/aircraft.md
- The Honeywell AS907-2-1A engine: https://openairdocs.org/engine/honeywell-as907-2-1a.md

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