# Canadair CL-44J - Type: Aircraft model (FAA registry) - Registry code: 1900104 - Manufacturer (registry): CANADAIR LTD - Model: CL-44J - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-prop - Seats: 181 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS 1A20](https://openairdocs.org/tcds/1A20) (OpenAirDocs) - Holder: Bombardier Inc. - Registered aircraft: 0 - Page: https://openairdocs.org/model/canadair-cl-44j Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [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 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 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011 - [AD 97-25-12](https://openairdocs.org/ad/97-25-12): AFM - Limitations Section - Power Levers · Bombardier CL-44D4 and CL-44J. Effective Jan 13, 1998 - [AD 91-06-05](https://openairdocs.org/ad/91-06-05): Supplemental Inspection Program · Bombardier CL-44D4 and CL-44J. Effective Apr 8, 1991 - [AD 89-04-07](https://openairdocs.org/ad/89-04-07): Upper Wing Skin · Bombardier CL-44D4 and CL-44J. Effective Mar 7, 1989 - [AD 86-16-10](https://openairdocs.org/ad/86-16-10): Lugs - Main Landing Gear · Bombardier CL-44D4 and CL-44J. Effective Sep 8, 1986 - [AD 83-24-06](https://openairdocs.org/ad/83-24-06): L&R Upper MLG Eye Attachment Pins · Bombardier CL-44D4 and CL-44J. Effective Dec 20, 1983 - [AD 83-10-05](https://openairdocs.org/ad/83-10-05): Horizontal Stabilizer Rear Attachment Fittings · Bombardier CL-44D4 and CL-44J. Effective Jun 6, 1983 - [AD 81-07-05](https://openairdocs.org/ad/81-07-05): Nose Landing Gear Crossbeam · Bombardier CL-44D4 and CL-44J. Effective Mar 31, 1981 - [AD 71-20-06](https://openairdocs.org/ad/71-20-06): Horizontal Stabilizer · Bombardier CL-44D4 and CL-44J. Effective Feb 21, 1980 - [AD 79-10-12](https://openairdocs.org/ad/79-10-12): Main Landing Gear Actuating System · Bombardier CL-44D4 and CL-44J. Effective May 18, 1979 - [AD 79-10-04](https://openairdocs.org/ad/79-10-04): Fireproofing · Bombardier CL-44D4 and CL-44J. Effective May 9, 1979 - [AD 78-23-05](https://openairdocs.org/ad/78-23-05): Spline Wear On Elevator Travel · Bombardier CL-44D4 and CL-44J. Effective Nov 10, 1978 - [AD 76-15-05](https://openairdocs.org/ad/76-15-05): Nose Landing Gear Bolts · Bombardier CL-44D4 and CL-44J. Effective Apr 17, 1978 - [AD 77-17-01](https://openairdocs.org/ad/77-17-01): Structural Integrity · Bombardier CL-44D4 and CL-44J. Effective Aug 18, 1977 - [AD 77-02-10](https://openairdocs.org/ad/77-02-10): Fuselage Bonding Strips · Bombardier CL-44D4 and CL-44J. Effective Feb 4, 1977 - [AD 75-24-08](https://openairdocs.org/ad/75-24-08): Landing Gear Attach Bolts · Bombardier CL-44D4 and CL-44J. Effective Nov 25, 1975 - [AD 75-08-01](https://openairdocs.org/ad/75-08-01): Nose Landing Gear · Bombardier CL-44D4 and CL-44J. Effective Apr 7, 1975 - [AD 74-05-02](https://openairdocs.org/ad/74-05-02): Main Landing Gear Uplock Cylinder · Bombardier CL-44D4 and CL-44J. Effective Feb 26, 1974 - [AD 74-04-05](https://openairdocs.org/ad/74-04-05): Main Landing Gear Uplock Fitting · Bombardier CL-44D4 and CL-44J. Effective Feb 20, 1974 - [AD 74-04-04](https://openairdocs.org/ad/74-04-04): Main Landing Gear Attach Fitting · Bombardier CL-44D4 and CL-44J. Effective Feb 18, 1974 - [AD 72-21-05](https://openairdocs.org/ad/72-21-05): Horizontal Stabilizer · Bombardier CL-44D4 and CL-44J. Effective Oct 17, 1972 - [AD 69-12-05](https://openairdocs.org/ad/69-12-05): Cracks In Access Cutouts · Bombardier CL-44D4 and CL-44J. Effective Jun 27, 1969 - [AD 68-10-08](https://openairdocs.org/ad/68-10-08): Main Landing Gear Actuator Attach · Bombardier CL-44D4 and CL-44J. Effective May 21, 1968 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19800603053799I](https://openairdocs.org/incident/19800603053799I), Jun 3, 1980: Cndair CL44D4 (N4998S), Miami, FL, Minor damage. During ground taxi aircraft struck barricade damaging propeller. ## STCs that may be installed (OpenAirDocs) (5) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA5656NM](https://openairdocs.org/stc/SA5656NM): Installation of burglar alarm system. Thompson Harold S --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.