# N604AL: 1997 Canadair CL-600-2B16

- Status: Valid registration
- Airframe: [Canadair CL-600-2B16](https://openairdocs.org/model/canadair-cl-600-2b16) (registry code 1900305, 22 seats)
- Engine: [GE CF34-3B](https://openairdocs.org/engine/ge-cf34-3b) (registry code 30069)
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA) (Bombardier Inc.), [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 5360
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 3, 2016
- Certificate issued: February 5, 2026
- Expires: February 28, 2033
- Mode S code: A7D626
- Registered owner: [Sabby Aviation LLC](https://openairdocs.org/faa-owner/SABBY%20AVIATION%20LLC)
- Location: [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach)
- Owner type: LLC
- Owner's area on the map: 25.7612° N, 80.1308° W: Placed by OpenAirDocs at the center of ZIP code 33109, 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=604AL
- Page: https://openairdocs.org/aircraft/N604AL

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): 129 in force

### Matched by airframe (Canadair CL-600-2B16)

- [AD 2026-14-09](https://openairdocs.org/ad/2026-14-09): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (600), CL-600-2B16 (601-3A Variant), CL-600-2B16 (601-3R Variant) and 2 more. Effective Aug 18, 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 2026-07-01](https://openairdocs.org/ad/2026-07-01): Landing gear · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective May 8, 2026
- [AD 2025-24-11](https://openairdocs.org/ad/2025-24-11): Auxiliary Power · Bombardier CL-600-2A12 (601), CL-600-2B16 (601-3A Variant), CL-600-2B16 (601-3R Variant) and 1 more. Effective Jan 16, 2026
- [AD 2025-22-04](https://openairdocs.org/ad/2025-22-04): Flight Controls · Bombardier CL-600-2B16 (604 Variant). Effective Dec 23, 2025
- [AD 2025-07-09](https://openairdocs.org/ad/2025-07-09): Oxygen · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective Jul 2, 2025
- [AD 2024-13-01](https://openairdocs.org/ad/2024-13-01): Fuel · Bombardier CL-600-2B16 (604 Variant). Effective Aug 16, 2024
- [AD 2024-07-10](https://openairdocs.org/ad/2024-07-10): Landing gear · Bombardier CL-600-2B16 (604 Variant). Effective Jun 6, 2024
- [AD 2024-03-06](https://openairdocs.org/ad/2024-03-06): Landing gear · Bombardier CL-600-2B16 (CL-604). Effective Apr 16, 2024
- [AD 2023-26-08](https://openairdocs.org/ad/2023-26-08): Flight Controls · Bombardier CL-600-2B16 (CL-604). Effective Mar 20, 2024
- [AD 2023-24-05](https://openairdocs.org/ad/2023-24-05): Oxygen System · Bombardier CL-600-2B16 (CL-604). Effective Jan 22, 2024
- [AD 2023-22-16](https://openairdocs.org/ad/2023-22-16): Pneumatic · Bombardier Aerospace CL-600-2B16 (CL-604). Effective Jan 5, 2024
- [AD 2023-17-06](https://openairdocs.org/ad/2023-17-06): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Oct 19, 2023
- [AD 2023-16-01](https://openairdocs.org/ad/2023-16-01): Oxygen · Bombardier CL-600-2B16 (CL-604) with STC ST02355NY. Effective Aug 23, 2023
- [AD 2023-07-04](https://openairdocs.org/ad/2023-07-04): Auto flight · Bombardier CL-600-2B16 (CL-604). Effective May 30, 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 2023-06-04](https://openairdocs.org/ad/2023-06-04): Oxygen System · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 18, 2023
- [AD 2023-06-02](https://openairdocs.org/ad/2023-06-02): Equipment/furnishings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 18, 2023
- [AD 2023-25-13](https://openairdocs.org/ad/2023-25-13): Oxygen · Bombardier CL-600-2B16 (CL-604). Effective Feb 7, 2023
- [AD 2022-20-05](https://openairdocs.org/ad/2022-20-05): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Nov 25, 2022
- [AD 2022-12-13](https://openairdocs.org/ad/2022-12-13): Auto flight · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Oct 19, 2022
- [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022
- [AD 2022-10-10](https://openairdocs.org/ad/2022-10-10): Ice and Rain Protection · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jul 5, 2022
- [AD 2022-09-01](https://openairdocs.org/ad/2022-09-01): Ice and Rain Protection, Potable Water System · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 31, 2022
- [AD 2021-26-23](https://openairdocs.org/ad/2021-26-23): Fuel · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Feb 25, 2022
- [AD 2021-25-13](https://openairdocs.org/ad/2021-25-13): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Feb 15, 2022
- [AD 2021-13-12](https://openairdocs.org/ad/2021-13-12): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Sep 9, 2021
- [AD 2021-07-06](https://openairdocs.org/ad/2021-07-06): Navigation · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective May 11, 2021
- [AD 2021-05-17](https://openairdocs.org/ad/2021-05-17): NAVIGATION SYSTEM · Rockwell Collins FDSA-6500, CL-600-2B16 (CL-604), 525B and 7 more. Effective Apr 29, 2021
- [AD 2019-21-03](https://openairdocs.org/ad/2019-21-03): Navigation · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Dec 18, 2019
- [AD 2019-15-01](https://openairdocs.org/ad/2019-15-01): Main landing gear · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Sep 19, 2019
- [AD 2019-08-08](https://openairdocs.org/ad/2019-08-08): Hydraulic power · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 27, 2019
- [AD 2018-20-21](https://openairdocs.org/ad/2018-20-21): Lights · Bombardier CL-600-2B16 (CL-604). Effective Nov 20, 2018
- [AD 2018-17-02](https://openairdocs.org/ad/2018-17-02): Flight controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Sep 19, 2018
- [AD 2018-09-17](https://openairdocs.org/ad/2018-09-17): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 25, 2018
- [AD 2018-06-06](https://openairdocs.org/ad/2018-06-06): Autopilot System · Bombardier CL-600-2B16 (CL-604). Effective Apr 19, 2018
- [AD 2017-23-09](https://openairdocs.org/ad/2017-23-09): Periodic inspections · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Dec 26, 2017
- [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 2017-22-11](https://openairdocs.org/ad/2017-22-11): Navigation · Bombardier CL-600-2B16 (CL-604). Effective Dec 20, 2017
- [AD 2017-20-11](https://openairdocs.org/ad/2017-20-11): Fuselage · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Nov 15, 2017
- [AD 2017-19-06](https://openairdocs.org/ad/2017-19-06): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Oct 27, 2017
- [AD 2017-16-13](https://openairdocs.org/ad/2017-16-13): Oxygen · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Sep 25, 2017
- [AD 2016-20-09](https://openairdocs.org/ad/2016-20-09): Fuel · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Jan 9, 2017
- [AD 2016-21-06](https://openairdocs.org/ad/2016-21-06): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Dec 19, 2016
- [AD 2016-13-09](https://openairdocs.org/ad/2016-13-09): Flight Controls · Bombardier CL-600-2B16 (CL-604). Effective Aug 16, 2016
- [AD 2016-10-10](https://openairdocs.org/ad/2016-10-10): Fuel · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Jun 23, 2016
- [AD 2016-08-15](https://openairdocs.org/ad/2016-08-15): Wings · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Jun 6, 2016
- [AD 2015-25-05](https://openairdocs.org/ad/2015-25-05): Electrical Power · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Jan 28, 2016
- [AD 2015-07-02](https://openairdocs.org/ad/2015-07-02): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 4, 2015
- [AD 2015-05-07](https://openairdocs.org/ad/2015-05-07): Flight Controls · Bombardier CL-600-2B16 (CL-604). Effective Mar 16, 2015

### Matched by engine (GE CF34-3B)

- [AD 2020-08-01](https://openairdocs.org/ad/2020-08-01): Turbine Engine Inlet Section · General Electric CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 15, 2020
- [AD 2009-26-09](https://openairdocs.org/ad/2009-26-09): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 11, 2010
- [AD 2010-01-04](https://openairdocs.org/ad/2010-01-04): Fan blade · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 25, 2010
- [AD 2009-07-12](https://openairdocs.org/ad/2009-07-12): High-pressure (HP) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 7, 2009
- [AD 2006-04-12](https://openairdocs.org/ad/2006-04-12): Stage 5 low pressure turbine (LPT) disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Mar 30, 2006
- [AD 2004-26-02](https://openairdocs.org/ad/2004-26-02): Certain high pressure compressor (HPC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 26, 2005
- [AD 2003-05-10 R1](https://openairdocs.org/ad/2003-05-10-R1): B-Sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Nov 18, 2003
- [AD 2001-12-06](https://openairdocs.org/ad/2001-12-06): Lubrication System for the Engine Bearings · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 20, 2001
- [AD 99-23-26 R1](https://openairdocs.org/ad/99-23-26-R1): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 17, 2000

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

- [AD 2025-17-12](https://openairdocs.org/ad/2025-17-12) (historical): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective Oct 31, 2025
- [AD 2023-12-20](https://openairdocs.org/ad/2023-12-20) (historical): Oxygen · Bombardier CL-600-2B16 (CL-604) with STC ST02355NY. Effective Aug 23, 2023
- [AD 2021-20-13](https://openairdocs.org/ad/2021-20-13) (historical): Landing gear · Bombardier CL-600-2B16 (CL-604). Effective Nov 18, 2021
- [AD 2020-19-13](https://openairdocs.org/ad/2020-19-13) (historical): Oxygen · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Nov 3, 2020
- [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019
- [AD 2019-12-09](https://openairdocs.org/ad/2019-12-09) (historical): Navigation · Bombardier CL-600-2B16 (CL-604), Flight Display System Application FDSA-6500, 525B and 13 more. Effective Jul 23, 2019
- [AD 2017-22-06](https://openairdocs.org/ad/2017-22-06) (historical): Fuel · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Nov 30, 2017
- [AD 2015-02-06](https://openairdocs.org/ad/2015-02-06) (historical): Flight Controls · Bombardier CL-600-2B16 (CL-604). Effective Mar 6, 2015
- [AD 2015-02-23](https://openairdocs.org/ad/2015-02-23) (historical): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Feb 18, 2015
- [AD 2014-17-51](https://openairdocs.org/ad/2014-17-51) (historical): Wings · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Nov 12, 2014
- [AD 2014-20-01](https://openairdocs.org/ad/2014-20-01) (historical): Fuel · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and CL-600-2B16 (CL-604). Effective Oct 20, 2014
- [AD 2010-14-05](https://openairdocs.org/ad/2010-14-05) (historical): Hydraulic power · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 5, 2010
- [AD 2009-06-05](https://openairdocs.org/ad/2009-06-05) (historical): Wing anti-ice piccolo · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Apr 28, 2009
- [AD 2008-08-06](https://openairdocs.org/ad/2008-08-06) (historical): Airplane flight manuals (AFMs) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 4 more. Effective Apr 21, 2008
- [AD 2007-14-02](https://openairdocs.org/ad/2007-14-02) (historical): Nose landing gear (NLG) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 16, 2007
- [AD 2006-22-06](https://openairdocs.org/ad/2006-22-06) (historical): Emergency and Abnormal Procedures section of the AFM · Bombardier CL-600-2B16 (CL-604), CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Nov 14, 2006
- [AD 2006-18-04](https://openairdocs.org/ad/2006-18-04) (historical): Stabilizer trim runaway · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 2 more. Effective Sep 1, 2006
- [AD 2005-15-04](https://openairdocs.org/ad/2005-15-04) (historical): Landing gear parts · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 30, 2005
- [AD 2005-04-07](https://openairdocs.org/ad/2005-04-07) (historical): Airplane Flight Manuals (AFM) - Cold Weather Operations · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 4 more. Effective Feb 22, 2005
- [AD 2003-08-12](https://openairdocs.org/ad/2003-08-12) (historical): Flap Vane Bracket and Vane Actuator Beam of Wing Flap Systems · Bombardier Aerospace CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 8, 2003
- [AD 2000-01-51](https://openairdocs.org/ad/2000-01-51) (historical): Fuel Service Panel Maintenance Light · Bombardier CL-600-2B16 (CL-604) with STC SA8060NM-D or 2 others. Effective Jan 7, 2000
- [AD 97-24-02](https://openairdocs.org/ad/97-24-02) (historical): Underfloor Pressure Bulkhead of Fuselage · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Dec 3, 1997
- [AD 2009-24-11](https://openairdocs.org/ad/2009-24-11) (historical): Fan blades · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 4, 2010
- [AD 2007-07-07 R1](https://openairdocs.org/ad/2007-07-07-R1) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Sep 12, 2007
- [AD 2007-07-07](https://openairdocs.org/ad/2007-07-07) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 23, 2007
- [AD 2007-05-16](https://openairdocs.org/ad/2007-05-16) (historical): Fan disks for an arc-out defect · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Mar 12, 2007
- [AD 2007-04-51](https://openairdocs.org/ad/2007-04-51) (historical): Uncontained fan disk failure during flight operation · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1
- [AD 2006-05-04](https://openairdocs.org/ad/2006-05-04) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 7, 2006
- [AD 2003-05-10](https://openairdocs.org/ad/2003-05-10) (historical): B-sump Oil Scavenge System · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Apr 2, 2003
- [AD 2001-19-02](https://openairdocs.org/ad/2001-19-02) (historical): B-sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Oct 9, 2001
- [AD 2001-10-03](https://openairdocs.org/ad/2001-10-03) (historical): Fan Disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 31, 2001
- [AD 99-23-26](https://openairdocs.org/ad/99-23-26) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Dec 6, 1999
- [AD 99-11-08](https://openairdocs.org/ad/99-11-08) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 27, 1999

All 162: https://openairdocs.org/aircraft/N604AL/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-11-51](https://openairdocs.org/saib/NM-11-51): Ice and Rain Protection: Wing Anti-Ice System. Issued Aug 30, 2011
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NE-03-28](https://openairdocs.org/saib/NE-03-28): . Issued Mar 10, 2003
- [SAIB NE-04-77](https://openairdocs.org/saib/NE-04-77): . Issued Aug 12, 2004
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N604AL.

## FAA accident and incident reports

None matched to N604AL.

## 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 N604AL not matched to an aircraft (332, newest 50)

They name N604AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR IXXA110045O](https://openairdocs.org/sdr/IXXA110045O), Jun 5, 2011: LATCH. FAILED. AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NOSE GEAR AND FOUND RT NOSE GE
- [SDR DHL2004809005](https://openairdocs.org/sdr/DHL2004809005), Mar 15, 2004: RIB. CRACKED. LEFT-HAND INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 INCH CRACK OUTBOARD RIB LOWER CORD 40 INCHES FROM TRAILING EDGE. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING 
- [SDR DHL2004809004](https://openairdocs.org/sdr/DHL2004809004), Mar 15, 2004: SPAR. CRACKED. LT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BO
- [SDR DHL2004809003](https://openairdocs.org/sdr/DHL2004809003), Mar 15, 2004: FITTING. CRACKED. RIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING T
- [SDR DHL2004809002](https://openairdocs.org/sdr/DHL2004809002), Feb 27, 2004: WINDSHIELD. CRACKED. F/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S FORWARD SIDE WINDOW IAW DC8 M/M 56-10-2, NO LEAKS NOTED.
- [SDR DHL2004809001](https://openairdocs.org/sdr/DHL2004809001), Feb 17, 2004: FAN. NOISY. ON TAKEOFF AND AT CRUISE ALTITUDE, RECIRCULATION FAN IS LOUD & VIBRATION IS FELT UNDERFLOOR NEAR LAV NOISE DECREASES WITH FAN OFF. DEFERRED RECIRCULATION FAN, P
- [SDR DHL2003809011](https://openairdocs.org/sdr/DHL2003809011), Dec 31, 2003: BATTERY. INOPERATIVE. DURING BISE CHECK - EMERGENCY LIGHT SWITCH MUST BE RECYCLED ONCE BEFORE EMERGENCY LIGHTS FUNCTION NORMALLY. REMOVED AND REPLACED AIRCRAFT BATTERY, OPS CHECKED G
- [SDR DHL2003809010](https://openairdocs.org/sdr/DHL2003809010), Dec 28, 2003: BELLCRANK. CRACKED. MAIN ENTRY DOOR IS DIFFICULT TO OPEN AND CLOSE. FOUND BAYONET BELLCRANK CRACKED, ALSO FOUND DAMAGED ROLLER ASSEMBLY ON DOOR SEAL ACTUATING CRANK. REMOVED BAD PA
- [SDR DHL2003809009](https://openairdocs.org/sdr/DHL2003809009), Dec 27, 2003: DOOR. LACK OF LUBE. MAIN CABIN DOOR HARD TO CLOSE. LUBED MAIN CABIN DOOR MECHANISM. OPS CHECKED GOOD PER 52-11-1.
- [SDR DHL2003809008](https://openairdocs.org/sdr/DHL2003809008), Dec 2, 2003: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOPERATIVE. RECHARGED BATTERY AND OPS CHECKED GOOD PER M/M 33-50-0.
- [SDR DHL2003809007](https://openairdocs.org/sdr/DHL2003809007), Nov 29, 2003: DOOR. OUT OF ADJUST. COCKPIT DOOR BINDING OUTSIDE KNOB SO SMOOTH YOU CAN NOT PULL DOOR OPEN WHEN UNLOCKED. ADJUSTED DOOR IAW SMM 52-51-01 OPS CHECKED OK.
- [SDR DHL2003809006](https://openairdocs.org/sdr/DHL2003809006), Nov 22, 2003: LATCH. OUT OF ADJUST. FLIGHT DECK DOOR WILL NOT LATCH CLOSED PROPERLY AND JAMS IN CLOSED POSITION. ADJUSTED UPPER LATCH AND OPS CHECKED PER MSI M/M 52-10-0. ALL CHECKS GOOD.
- [SDR DHL2003809005](https://openairdocs.org/sdr/DHL2003809005), Nov 12, 2003: HANDLE. UNSECURE. AT BEGINNING OF TAKEOFF ROLL BELLY DOOR LIGHT ILLUMINATED. DURING TAXI DOOR LIGHT ILLUMINATED INTERMITTENTLY. FOUND B PIT DOOR HANDLE NOT SECURED. RE-SECURED HA
- [SDR DHL2003809004](https://openairdocs.org/sdr/DHL2003809004), Nov 8, 2003: DOOR. OUT OF ADJUST. COCKPIT ENTRY DOOR JAMS AND IS VERY HARD TO OPEN FROM THE GALLEY SIDE. ADJUSTED DOOR PER SMM AND M/M 51-10-0.
- [SDR DHL2003809003](https://openairdocs.org/sdr/DHL2003809003), Oct 31, 2003: DOOR. OUT OF ADJUST. COCKPIT DOOR IS HARD TO OPEN FROM THE OUTSIDE. DOOR JAMMED CLOSED. ADJUSTED COCKPIT DOOR PER M/M 52-10-0. OPS CHECKED GOOD.
- [SDR DHL2003809002](https://openairdocs.org/sdr/DHL2003809002), Oct 8, 2003: MEC. MALFUNCTIONED. NR 3 ENG FAILED 3-5 MIN AFT SETTING CRUISE THRUST (0938Z) ENG LOST POWER SLOWLY. PERFORMED ENG FAILURE CHECKLIST ATTEMP RESTART, NO FUEL FLOW, OR EGT INDICATION
- [SDR DHL2003809001](https://openairdocs.org/sdr/DHL2003809001), Sep 12, 2003: BATTERY. DISCHARGED. DURING PREFLIGHT EMERGENCY EXIT LIGHTS AND STANDBY ATTITUDE INDICATOR WERE FOUND INOPERATIVE. TROUBLESHOT SYSTEM, FOUND EMERGENCY LIGHTS NOT GETTING ENOUGH POWE
- [SDR DHL2003604790](https://openairdocs.org/sdr/DHL2003604790), Aug 18, 2003: WARNING SYSTEM. FAULTY. GPWS FAIL LIGHT ILLUMINATED. REPLACED GPWS MK II WITH GPWS/WS MKVII AND OPS CHECKED GOOD IAW J/C EA34450002-001-D.
- [SDR DHL2003604756](https://openairdocs.org/sdr/DHL2003604756), Jul 24, 2003: DOOR FRAME. DAMAGED. TWO INTERIM REPAIRS ON LT AFT LWR CORNER OF MAIN CARGO DOOR STA 270.000 BETWEEN L-20L AND L-22L. REMOVED FASTENERS AND INTERIM REPAIR. TRIMMED OUT DAMAGED AREA 
- [SDR DHL2003604696](https://openairdocs.org/sdr/DHL2003604696), Jul 14, 2003: SPLICE. CRACKED. FWD CARGO COMPT SPLICE FITTING CRACKED 2.000 STA 440.000 - 460.000, L-31L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED SPLICE FIT
- [SDR DHL2003604747](https://openairdocs.org/sdr/DHL2003604747), Jul 14, 2003: SKIN. CORRODED. FUSELAGE NOSE SECTION EXTERNAL SKIN CORRODED & DENTED BETWEEN STA 35.000 AND STA 70.000, L-31L TO L-31R. REMOVED FASTENERS & EXISTING EXTERNAL DOUBLER. REMOVED 
- [SDR DHL2003604757](https://openairdocs.org/sdr/DHL2003604757), Jul 9, 2003: STRINGER. CRACKED. LT WING NR 1 ALT TANK, S-59 CRACKED 1.500 (LOWER), NEAR XRS 463.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG 3D, 3E, 3F. REMOVED FASTENERS IAW 
- [SDR DHL2003604675](https://openairdocs.org/sdr/DHL2003604675), Jul 8, 2003: FRAME. BROKEN. AFT CARGO COMPT. DOOR NR 4 FRAME ANGLE BROKEN, STA.1440.000. REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG.1. FABRICATED NEW ANGLE (2024-T3 AL0.040) IAW SRM 53-2-0 PG.
- [SDR DHL2003604676](https://openairdocs.org/sdr/DHL2003604676), Jul 7, 2003: ANGLE. BROKEN. AFT CARGO COMPT DOOR NR 4 FRAME ANGLE BROKEN, STA 1440.000 CORR REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG 1. FABRICATED NEW ANGLE IAW SRM 53-2-0 PG 1-2. CLEANED, T
- [SDR DHL2003604670](https://openairdocs.org/sdr/DHL2003604670), Jul 4, 2003: ATTACH FITTING. CRACKED. LT WING T/E INNER UPPER FITTING CRACKED 1.000 AT XRS.434.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. 
- [SDR DHL2003604758](https://openairdocs.org/sdr/DHL2003604758), Jun 28, 2003: SKIN. DENTED. RT ELEVATOR UPPER PLATING CTR. SECTION HAS DENTS FROM XE. 132.000 TO XE. 246.000 PERFORMED MAJOR REPAIR IAW EODHL-030525, ED-3276. REMOVED FASTENERS IAW SRM 51-
- [SDR DHL2003604787](https://openairdocs.org/sdr/DHL2003604787), Jun 25, 2003: SKIN. DENTED. FUSELAGE EXTERIOR SKIN SHOWS DENTS (03 EA), FS 255.000, L-24L TO L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030516, ED-3357. REMOVED FASTENERS IAW S
- [SDR DHL2003604672](https://openairdocs.org/sdr/DHL2003604672), Jun 25, 2003: SKIN. DAMAGED. LT IB AILERON LWR SURFACE WITH INTERIM REPAIR BETWEEN STA.XA441.000 AND XA.502.000. PERFORMED MAJOR REPAIR IAW EODHL-030569, ED-3399. REMOVED FASTENERS AND DAMA
- [SDR DHL2003604591](https://openairdocs.org/sdr/DHL2003604591), Jun 25, 2003: PANEL. CRACKED. RT OUTBOARD SLOT UPPER CENTER DOOR WITH 0.500 CRACK IN IT. REMOVED AND REPLACED RT OUTBOARD SLOT UPPER CENTER DOOR IAW MM 27-80-2 PG 201-204. REFER TO NR 0531 F
- [SDR DHL2003604793](https://openairdocs.org/sdr/DHL2003604793), Jun 24, 2003: CARGO TRACK. WORN. MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA -55.000 - STA 310.000. REMOVED NR 2 TRACK WITH WORN LUGS IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SR
- [SDR DHL2003604667](https://openairdocs.org/sdr/DHL2003604667), Jun 24, 2003: SKIN. CORRODED. RT ELEVATOR UPPER SKIN INBD SECTION SHOW CORROSION, SEVERAL DENTS AND INTERIM REPAIR FROM STA XAR 0.000 TO XE 132.000. REMOVED FASTENERS AND THE DAMAGED SKIN PA
- [SDR DHL2003604666](https://openairdocs.org/sdr/DHL2003604666), Jun 24, 2003: SKIN. CORRODED. RT ELEVATOR LOWER OUTER SKIN CORRODED ON SEVERAL SPOTS FROM STA XE 246.000 TO STA XH 285.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030574, ED 3411. 
- [SDR DHL2003604674](https://openairdocs.org/sdr/DHL2003604674), Jun 24, 2003: SKIN. CORRODED. RT ELEVATOR LOWER PART EXTERNAL SKIN SHOWS DEFLECTION AND CORROSION FROM STA. XAR.0.000 TO XE.132.000. PERFORMED MAJOR REPAIR IAW EODHL-030521, ED-3405. REMOVED
- [SDR DHL2003604768](https://openairdocs.org/sdr/DHL2003604768), Jun 24, 2003: SKIN. CORRODED. RT ELEVATOR UPPER PLATING OTBD SECTION SHOWS INTERIM REPAIR AND CORROSION FROM STA XE 246.000 TO XH 285.000. REMOVED FASTENERS, REMOVED CORROSION AND FOUND OUT 
- [SDR DHL2003604777](https://openairdocs.org/sdr/DHL2003604777), Jun 24, 2003: FITTING. CRACKED. MAIN CARGO COMPT DOOR FRAME LOWER INTERNAL SKIN FITTING 2.00 CRACKED AT STA 255.000, L-21L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. REMOVED
- [SDR DHL2003604748](https://openairdocs.org/sdr/DHL2003604748), Jun 24, 2003: SKIN. DENTED. RT ELEVATOR OUTER LOWER SKIN HAS DENTS ON SEVERAL SPOTS FROM STA. XE.132.000 TO XE.246.000. PERFORMED MAJOR REPAIR IAW EODHL-030522, ED-3406. REMOVED FASTENERS 
- [SDR DHL2003604762](https://openairdocs.org/sdr/DHL2003604762), Jun 22, 2003: SKIN. CORRODED. FWD CTR SECTION SHOWS SEVERAL SPOTS OF CORROSION AND DOUBLER REPAIR (03 EA.) BETWEEN STA.660.000 AND STA.725.000, L-34L TO L-34R. PERFORMED MAJOR REPAIR IAW EOD
- [SDR DHL2003604738](https://openairdocs.org/sdr/DHL2003604738), Jun 22, 2003: SKIN. CORRODED. LOWER FUSELAGE PLATING SHOWS 04 SPOTS OF CORROSION BETWEEN STA 743.000 AND STA 767.000, L-35L TO L-35R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. R
- [SDR DHL2003604603](https://openairdocs.org/sdr/DHL2003604603), Jun 22, 2003: FAIRING. DELAMINATED. LT OTBD FAIRING ASSY WITH EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED OB FAIRING ASSY ON LT WING IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR
- [SDR DHL2003604664](https://openairdocs.org/sdr/DHL2003604664), Jun 21, 2003: PLATE. DENTED. RT WING INBD FLAP UPPER PLATING SHOWS DENTS AND WEAR OUT OR LIMITS BETWEEN STA XW 104.000 TO XW 115.000. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-2
- [SDR DHL2003604701](https://openairdocs.org/sdr/DHL2003604701), Jun 21, 2003: FRAME. CRACKED. FWD ACCY COMPT FRAME CRACKED 2.000, STA 55.000, L-24L. TRIMMED OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. CLEANED, TREATED AND PRIMED
- [SDR DHL2003604741](https://openairdocs.org/sdr/DHL2003604741), Jun 20, 2003: SKIN. CORRODED. LT WING INBD. L/E SLANT PANEL UPPER CAP SHOWS CORROSION FROM XFS.63.750 TO XFS.82.500 AND REPAIR DOUBLER FROM XFS.201.000 TO XFS.207.000. PERFORMED MAJOR REPAIR
- [SDR DHL2003604724](https://openairdocs.org/sdr/DHL2003604724), Jun 20, 2003: SKIN. CORRODED. RT INNER WING LE SLANT PANEL UPPER CAP SHOWS CORROSION BETWEEN XFS.93.000 AND XFS.107.500, REPAIR DOUBLERS. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2
- [SDR DHL2003604725](https://openairdocs.org/sdr/DHL2003604725), Jun 19, 2003: DOOR FRAME. CRACKED. SECTION AROUND EMERGENCY EXIT DOOR AFT LOWER JAMB HAS TWO CRACKS OF 0.750 AND 0.500 AT STA. 415.250 BETWEEN L-19L AND L-22L PERFORMED MAJOR REPAIR. REMOVED FAST
- [SDR DHL2003604582](https://openairdocs.org/sdr/DHL2003604582), Jun 19, 2003: SKIN. DELAMINATED. RT NR 2 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER ON RT WING IAW 27-81-1 PG 201-206. FOR OPS CHECK SEE N/R 0531.
- [SDR DHL2003604729](https://openairdocs.org/sdr/DHL2003604729), Jun 17, 2003: SPLICE. CRACKED. FWD CARGO COMPT. SPLICE FITTING CRACKED 1.000, STA.200.000 - 220.000, L-27R. (MAJOR REPAIR) CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM NR P0201388, 
- [SDR DHL2003604709](https://openairdocs.org/sdr/DHL2003604709), Jun 17, 2003: SKIN. DENTED. "A" CARGO DOOR EXTERNAL SKIN HAS (2) INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG.1, SRM 52-4-1 FIG.2 BOEING MESSAGE DHL-
- [SDR DHL2003604785](https://openairdocs.org/sdr/DHL2003604785), Jun 17, 2003: FRAME. CORRODED. FWD CARGO COMPT PRESSURE BULKHEAD FRAME CORRODED STA 70.000, L-28L - L-32L. REMOVED FASTENERS AND ATTACH FITTING (04 EA). REMOVED CORROSION ON FRAME STA.70.000,
- [SDR DHL2003604774](https://openairdocs.org/sdr/DHL2003604774), Jun 17, 2003: SPLICE. CRACKED. AFT ACCESSORY COMPT FRAME SPLICE FITTING HAS A 2.000 CRACK, STA 660.000 L-35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201385, DWG 3750498. REMOVED CR
- [SDR DHL2003604681](https://openairdocs.org/sdr/DHL2003604681), Jun 16, 2003: FRAME. CORRODED. LT MLG W/W SPOILER AND AILERON ACTUATING MECH SUPPORT Z-FORMER CORRODED AT STA 857.000, LBL-54. REMOVED CORROSION ON FORMER IAW SRM 51-1-8 PG 17, 18. FOUND OUT 

All 332: https://openairdocs.org/aircraft/N604AL/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (857, 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 (Canadair CL-600-2B16)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12422IB](https://openairdocs.org/stc/ST12422IB): Water System Modifications. Bombardier Inc
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04735NY](https://openairdocs.org/stc/ST04735NY): Installation of LAI Windshields. Lee Aerospace Inc
- [STC ST12339IB](https://openairdocs.org/stc/ST12339IB): Installation of Cabin CMS Upgrade, Seat Replacement, and Miscellaneous Interior Modifications. Flying Colours Corp
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST12328IB](https://openairdocs.org/stc/ST12328IB): Demonstration of TPED Tolerance. Bombardier Inc
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST11291DS](https://openairdocs.org/stc/ST11291DS): Installation of new Bulkhead Display Units (BDUX) monitors. BHE & Associates
- [STC ST11292DS](https://openairdocs.org/stc/ST11292DS): Installation of a new wireless access point (WAP-6000) and local antenna unit (ANT-200). BHE & Associates Ltd
- [STC ST12196IB](https://openairdocs.org/stc/ST12196IB): Installation of the Gogo Galileo HDX High-Speed Internet System. Sky Service F.B.O. Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST04115NY](https://openairdocs.org/stc/ST04115NY): Installation of Mission Equipment. Delta Engineering Corporation
- [STC ST01642NY](https://openairdocs.org/stc/ST01642NY): Installation of Safe Flight P/N C88627-1 throttle quadrant in place of P/N FE341000000 Throttle Quadrant. Safe Flight Instrument 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 ST10973SC](https://openairdocs.org/stc/ST10973SC): Activation of a high power cabin telecommunication router. BHE & Associates LTD
- [STC ST01930WI](https://openairdocs.org/stc/ST01930WI): Installation of SmartSky Networks 4G System. L2 Aviation
- [STC ST00431WI-D](https://openairdocs.org/stc/ST00431WI-D): Installation of a Fairchild F-1000 Data Flight Data Recorder System. KGB Aviation Solutions LLC
- [STC SA6011NM](https://openairdocs.org/stc/SA6011NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST11293DS](https://openairdocs.org/stc/ST11293DS): The installation of an AirSync flight data monitoring system. BHE & Associates Ltd
- [STC ST209CH](https://openairdocs.org/stc/ST209CH): Installation of a model TCAS 791 TCAS I. Acron Aviation 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 ST09940AC](https://openairdocs.org/stc/ST09940AC): Installation of an Aspire 400 Satcom System. L2 Aviation
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST11850CH](https://openairdocs.org/stc/ST11850CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [STC ST03810NY](https://openairdocs.org/stc/ST03810NY): Installation of the INGENIO Cockpit Tripod Electronic Flight Bag (EFB) Mount. Ingenio Aerospace Inc
- [STC ST00690DE](https://openairdocs.org/stc/ST00690DE): Installation of Electronic Cable Specialists, ECS EZMount Arm of Bombardier CL-600 Series Aircraft. Amphenol Cable and Interconnect Technologies Inc
- [STC ST04745NY](https://openairdocs.org/stc/ST04745NY): Installation of LAI Cockpit Side Windows. Lee Aerospace Inc
- [STC ST02586AK](https://openairdocs.org/stc/ST02586AK): Approval of the Thomas Global Systems TFD-4000/4100 Active Matrix Liquid Crystal Display. ADS-B Technologies
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST02021WI](https://openairdocs.org/stc/ST02021WI): Installation of Gogo Business Aviation AVANCE L5/X3 System. Duncan Aviation, Inc
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST02035WI](https://openairdocs.org/stc/ST02035WI): Installation of a Collins IRT-4400 Iridium Certus Cabin SATCOM system. Learjet Inc
- [STC ST04653CH](https://openairdocs.org/stc/ST04653CH): Installation of Gogo L5 System with MB13 Antennas. STANDARDAERO BUSINESS AVIATION SERVICES LLC,
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02781SE](https://openairdocs.org/stc/ST02781SE): Non-Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval. AeroMech Incorporated
- [STC ST02022WI](https://openairdocs.org/stc/ST02022WI): Installation of a Bombardier Smart Router. Learjet Inc
- [STC ST02782SE](https://openairdocs.org/stc/ST02782SE): Non-Group Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC ST09374SC](https://openairdocs.org/stc/ST09374SC): Installation of a passenger oxygen distribution system. Gulfstream Aerospace Corporation
- [STC ST00206IB](https://openairdocs.org/stc/ST00206IB): Installation of the Gogo AVANCE L5 Upgrade. Sky Service F.B.O. Inc
- [STC ST04631CH](https://openairdocs.org/stc/ST04631CH): Installation of a Latitude Technologies Corporation DL-150 Satellite Data Unit (SDU) and Iridium Antenna. WEST STAR AVIATION
- [STC ST01066DE](https://openairdocs.org/stc/ST01066DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, Inc 
- [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 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 ST01012WI](https://openairdocs.org/stc/ST01012WI): Installation of an Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST01556WI](https://openairdocs.org/stc/ST01556WI): Installation of the Universal Avionics Dual 1Lw Flight Management System (FMS). Global Aviation Tech LLC
- [STC ST01778WI](https://openairdocs.org/stc/ST01778WI): Installation of a Universal Avionics Dual UNS-1Fw Flight Management System (FMS). Global Aviation Tech LLC
- [STC ST04839NY](https://openairdocs.org/stc/ST04839NY): Installation of LED Position/Anti-Collision Lights. Sterling Helicopter

All 857: https://openairdocs.org/aircraft/N604AL/stcs.md

## Related

- Other Canadair CL-600-2B16 aircraft: https://openairdocs.org/model/canadair-cl-600-2b16/aircraft.md
- The GE CF34-3B engine: https://openairdocs.org/engine/ge-cf34-3b.md

---
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