# Canadair CL215 1A10

- Type: Aircraft model (FAA registry)
- Registry codes: 1900111, 1900320
- Manufacturer (registry): CANADAIR LTD · CANADAIR
- Model: CL215 1A10
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 10
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A14EA](https://openairdocs.org/tcds/A14EA) (OpenAirDocs)
- Holder: De Havilland Aircraft of Canada Limited
- Registered aircraft: 2
- Page: https://openairdocs.org/model/canadair-cl215-1a10

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. The FAA lists this model under more than one registry code, usually for different spellings of the maker. This page covers them all.

## 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 2023-07-10](https://openairdocs.org/ad/2023-07-10): Equipment/furnishings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). 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 2019-25-11](https://openairdocs.org/ad/2019-25-11): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Feb 10, 2020
- [AD 2019-02-05](https://openairdocs.org/ad/2019-02-05): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Mar 22, 2019
- [AD 2017-17-17](https://openairdocs.org/ad/2017-17-17): Hydraulic power · Viking Air CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 11, 2017
- [AD 2012-11-04](https://openairdocs.org/ad/2012-11-04): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jul 9, 2012
- [AD 2012-05-05](https://openairdocs.org/ad/2012-05-05): Equipment/Furnishings · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Apr 24, 2012
- [AD 2011-22-06](https://openairdocs.org/ad/2011-22-06): Landing Gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 14, 2011
- [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 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2004-03-13](https://openairdocs.org/ad/2004-03-13): Main landing gear (MLG) axles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 17, 2004
- [AD 2002-12-12](https://openairdocs.org/ad/2002-12-12): Wing-to-Fuselage Frame Angles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jul 25, 2002
- [AD 96-23-13](https://openairdocs.org/ad/96-23-13): DC Generators · Bombardier CL-215-1A10. Effective Dec 5, 1996
- [AD 96-05-06](https://openairdocs.org/ad/96-05-06): Inspect Main Distribution Center and Electrical Components · Bombardier CL-215-1A10. Effective Mar 22, 1996
- [AD 93-16-06 R2](https://openairdocs.org/ad/93-16-06-R2): Rudder-Aileron Interconnect Tab · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 25, 1995
- [AD 78-08-02](https://openairdocs.org/ad/78-08-02): Water Door Hinge Plates · Bombardier CL-215-1A10. Effective Apr 14, 1978
- [AD 77-17-13](https://openairdocs.org/ad/77-17-13): Nose Landing Gear Doors · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Aug 30, 1977
- [AD 77-15-03](https://openairdocs.org/ad/77-15-03): Elevator Torque Tube Quadrant · Bombardier CL-215-1A10. Effective Jul 27, 1977
- [AD 77-13-05](https://openairdocs.org/ad/77-13-05): Missing Rivets In Bulkhead · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 29, 1977
- [AD 77-10-14](https://openairdocs.org/ad/77-10-14): Main Landing Gear Actuator · Bombardier CL-215-1A10. Effective May 26, 1977
- [AD 77-09-06](https://openairdocs.org/ad/77-09-06): Lower Rudder Bearing · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-05](https://openairdocs.org/ad/77-09-05): Nose Landing Gear · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-04](https://openairdocs.org/ad/77-09-04): Main Landing Gear Wheel Well · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 75-12-02](https://openairdocs.org/ad/75-12-02): Engine Fire Bottles · Bombardier CL-215-1A10. Effective May 30, 1975
- [AD 72-15-04](https://openairdocs.org/ad/72-15-04): Flame Propagation In Engine Fire Zone · Bombardier CL-215-1A10. Effective Jul 25, 1972
- [AD 71-04-04](https://openairdocs.org/ad/71-04-04): Failure Water Door Tension Rod · Bombardier CL-215-1A10. Effective Feb 25, 1971
- [AD 70-01-05](https://openairdocs.org/ad/70-01-05): Chine Spray Strips · Bombardier CL-215-1A10. Effective Dec 8, 1970

Historical (superseded or no longer in force):

- [AD 2013-11-03](https://openairdocs.org/ad/2013-11-03) (historical): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 14, 2013
- [AD 2011-03-08](https://openairdocs.org/ad/2011-03-08) (historical): Landing gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 14, 2011
- [AD 2005-18-05](https://openairdocs.org/ad/2005-18-05) (historical): Lower caps of the wing front spar and rear spar · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 6, 2005
- [AD 99-16-04](https://openairdocs.org/ad/99-16-04) (historical): Inspect Fuselage Frame-Angles · Bombardier CL-215-1A10. Effective Sep 7, 1999
- [AD 98-04-08](https://openairdocs.org/ad/98-04-08) (historical): Inspect Lower Cap of Wing Front & Rear Spars · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 4, 1998
- [AD 96-12-11](https://openairdocs.org/ad/96-12-11) (historical): Water Door Actuator Microswitches · Bombardier CL-215-1A10. Effective Jun 21, 1996
- [AD 95-22-04](https://openairdocs.org/ad/95-22-04) (historical): Main Landing Gear Axle · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 8, 1995

## Registered aircraft (2)

- [N36CL](https://openairdocs.org/aircraft/N36CL): [Cl415 Aviation Salvage LLC](https://openairdocs.org/faa-owner/CL415%20AVIATION%20SALVAGE%20LLC), [Belgrade, MT](https://openairdocs.org/faa-place/MT/Belgrade), S/N 1068
- [N65CL](https://openairdocs.org/aircraft/N65CL): [Cl415 Aviation Salvage LLC](https://openairdocs.org/faa-owner/CL415%20AVIATION%20SALVAGE%20LLC), [Belgrade, MT](https://openairdocs.org/faa-place/MT/Belgrade), S/N 1065

## 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 20080328831549I](https://openairdocs.org/incident/20080328831549I), Mar 28, 2008: Cndair CL2151A10 (N215NC), Belews Lake, NC, Minor damage. (-23) During firefighting operations, aircraft was picking up water from Belews Lake as an in-flight operation. On 13th water pickup, wind shifted to crosswind…

## Service difficulty reports (333, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR N6WA2023031401](https://openairdocs.org/sdr/N6WA2023031401), Mar 10, 2023: ELT. INOPERATIVE. PORTABLE ELT INOP. R/R PORTABLE ELT BATTERY IEW ARTEX CMM 25-62-30 OPS CHECKS GOOD. BATTERY EXPIRES MAY/2029
- [SDR VNAA202302100004](https://openairdocs.org/sdr/VNAA202302100004), Feb 10, 2023: DOUBLER. CORRODED. ANTENNA DOUBLER IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND AT STGR 27 CORRECTIVE ACTION REMOVED ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-
- [SDR VNAA202302100003](https://openairdocs.org/sdr/VNAA202302100003), Feb 10, 2023: NONE. CRACKED. PAX DOOR AT ZONE 3 - AFT SIDE OF PAX DOOR PULLY STFFENER LOWER SECTION HAS CRACK AND REQUIRES REPAIR. CORRECTIVE ACTION: COMPLIED WITH CRJ700 SRM 52-11-04-201-0
- [SDR VNAA202302100002](https://openairdocs.org/sdr/VNAA202302100002), Feb 10, 2023: NONE. NONE. SB_670BA-53-040-REQ (FUSELAGE CENTER FUSELAGE, PRIMARYSTRUCTURE FS280.00 TO FS295.00 INSPECTION AND REINFORCEMENT OFLINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR
- [SDR VNAA202302100001](https://openairdocs.org/sdr/VNAA202302100001), Feb 10, 2023: NONE. CRACKED. SRM-52-11-04 AFT (ZONE 3) (PERM REPAIR - PAX DOOR CRACKS ZONE 3 -AFT SIDE OF PAX DOOR) PERM REPAIR NEEDS PERFORMED FOR CRACKSIN ZONE 3 ON AFT SIDE OF PAX DOOR. 
- [SDR A6WA202210158343](https://openairdocs.org/sdr/A6WA202210158343), Oct 15, 2022: SHEAR PLATE. CORRODED. INBOARD OF RBL9 AT FS310 AND FS330.0 SHEAR PLATE AND MOUNT CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED INBOARD OF RBL9 AT FS310 AND FS3
- [SDR A6WA202210158344](https://openairdocs.org/sdr/A6WA202210158344), Oct 15, 2022: NONE. CORRODED. FLOOR BEAM CAP RBL 9 FROM FS559+96 TO FS 559+16 HAS AREA OF CORROSION ****AIRCRAFT REMOVED FROM SERVICE **** FLOOR BEAM REPLACED
- [SDR A6WA202210148340](https://openairdocs.org/sdr/A6WA202210148340), Oct 14, 2022: NONE. CORRODED. LH SIDE SEAT RAIL, APPROX. FS364.00 THRU FS409+16 HAS MULTIPLE AREA'S OF CORROSION. FLAGGED ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW LH S
- [SDR A6WA202210148342](https://openairdocs.org/sdr/A6WA202210148342), Oct 14, 2022: NONE. NONE. A-SKID INOP CAUTION MSG OBSERVED AT 120KIAS, T/O ABORTED, BTMS 5,5,7,3 MAX ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED A-SKID CONTROL UNIT IAW A
- [SDR A6WA202210148341](https://openairdocs.org/sdr/A6WA202210148341), Oct 14, 2022: NONE. CORRODED. FLOOR BEAM CAP LBL27 NEAR FS559+112 HAS AREA OF CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** REPAIRED FLOOR BEAM CAP LBL 27 NEAR FS 559+112 REF CRJ 200 SRM 5
- [SDR A6WA202210138339](https://openairdocs.org/sdr/A6WA202210138339), Oct 13, 2022: NONE. NONE. RECEIVED GEAR DISAGREE WARNING AFTER DEPARTURE, C/W QRH, MESSAGE REMAINED. TIME OF MESSAGE WAS APPROX 15-20 SECONDS AFTER GEAR SELECTED UP. RECEIVED NOSE DOOR O
- [SDR A6WA202209088338](https://openairdocs.org/sdr/A6WA202209088338), Oct 12, 2022: NONE. NONE. GEAR DISAGREE ON TAKEOFF. LDG SELECTED UP. MSG RCVD AFTER 6 SEC. STEERING INOP AND NLG DOOR CAU MSG. NO HYD MSG. MANAUL RELESES SYS OPERATED. HYDS PUMP ON. EMER
- [SDR SWIA202266599](https://openairdocs.org/sdr/SWIA202266599), Oct 9, 2022: NONE. FAILED. GEAR DISAGREE AFTER SELECTING GEAR UP. NOSE WHEEL NOT LOCKED. (FLIGHT 4923 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25627409 WITH THE FOLLO
- [SDR A6WA202210098320](https://openairdocs.org/sdr/A6WA202210098320), Oct 9, 2022: NONE. CHAFED. LH MLG DOOR HAS CHAFING ON THE FWD EDGE IN SEVERAL AREAS. ***AIRCRAFT REMOVED FROM SERVICE *** REMOVED AND REPLACED REPAIR FILLER IAW CRJ200 SRM 52-82-00-02 SUP
- [SDR A6WA202210098321](https://openairdocs.org/sdr/A6WA202210098321), Oct 9, 2022: VANE CAP. CHAFED. *RH INBOARD FLAP VANE SKIN HAS 3 AREAS WITH CHAFING (MARKED) ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND WET INSTALLED OUTBD EDGE NEW VANE CAP SKIN ON RH 
- [SDR A6WA202210088319](https://openairdocs.org/sdr/A6WA202210088319), Oct 8, 2022: NONE. CORRODED. SERVICE DOOR SILL HAS AREAS OF CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND INSTALL NEW SERVICE DOOR SILL
- [SDR A6WA202210088318](https://openairdocs.org/sdr/A6WA202210088318), Oct 8, 2022: SEAT TRACK. CHAFED. CO-PILOT FLOOR SEAT RAIL L/H INBOARD HAS CHAFING AND INDENTS ON FORWARD PART ****AIRCRAFT REMOVED FROM SERVICE **** REMOVE AND INSTALLED NEW CO-PILOT INBOARD SE
- [SDR A6WA202210068314](https://openairdocs.org/sdr/A6WA202210068314), Oct 6, 2022: SEAT TRACK. NONE. THE TEMPORARY REPAIR TO THE LH & RH SEAT RAIL TRACK - MISSING 2 RIVETS ON THE LH SIDE AND MISSING 3 RIVETS ON THE RH SIDE - HAS BEEN COMPLIED WITH IAW GREO 601R
- [SDR A6WA202210058313](https://openairdocs.org/sdr/A6WA202210058313), Oct 5, 2022: NONE. NONE. ON LADING ROLL OUT ON RNW 24 LEFT IN DAY I VEER IN TO THE RIGHT IN THE GRASS AND HIT SOMETHING THAT CAUSED DAMAGE TO THE LEFT WING. WITH REVERSER OUT, IT STARTE
- [SDR A6WA202210028311](https://openairdocs.org/sdr/A6WA202210028311), Oct 2, 2022: ANGLE. CORRODED. PAX DOOR FWD HANDLE CUP IS CORRODED. MARKED ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW PAX DOOR FWD HANDLE CUP REF CRJ-200-SRM 51-42-06 AN
- [SDR A6WA202210028312](https://openairdocs.org/sdr/A6WA202210028312), Oct 2, 2022: ANGLE. CORRODED. PAX DOOR AFT HANDLE CUP IS CORRODED. MARKED ***AIRCRAFT REMOVED FROM SERVICE*** REMPVED AND INSTALLED NEW PAX DOOR AFT HANDLE CUP REF CRJ-200-SRM 51-42-06 AND B
- [SDR A6WA202209088334](https://openairdocs.org/sdr/A6WA202209088334), Sep 8, 2022: FLOOR SUPPORT. DAMAGED. FLOOR SUPPORT STRUCTURE BETWEEN FS 409+128 - FS 424 & LBL 9 - RBL 27 HAVE ELONGATED HOLES. ***************REMOVED AIRCRAFT FROM SERVICE********************* OPE
- [SDR A6WA202209088335](https://openairdocs.org/sdr/A6WA202209088335), Sep 8, 2022: NONE. CHAFED. R/H I/B FLAP VANE L/E HAS WEAR DAMAGE AT WS 50.498+6. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGE TO A SMOOTH CONTOUR WIT
- [SDR A6WA202209088336](https://openairdocs.org/sdr/A6WA202209088336), Sep 8, 2022: NONE. CHAFED. R/H I/B FLAP VANE L/E HAS WEAR DAMAGE AT WS 98.50+7. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGE TO A SMOOTH CONTOUR WITH
- [SDR A6WA202209088337](https://openairdocs.org/sdr/A6WA202209088337), Sep 8, 2022: NONE. NONE. R/H TRU ACCESS DOOR ASSEMBLY AT FS 173 TO FS 193 HAS DAMAGE/DELAMINATION ON OUTER PLIES INTO THE HONEYCOMB MEASURING 1"L X 1"W X .063"D. *************AIRCRAFT R
- [SDR A6WA202209088324](https://openairdocs.org/sdr/A6WA202209088324), Sep 8, 2022: HINGE FITTING. GOUGED. R/H ELEVATOR HINGE #2 I/B FITTING GOUGED .8"L X .159"W X .010"D & O/B FITTING GOUGED .8"L X .159"W X .010"D AT RBL 55.89. EVALUATED DAMAGED AREAS AND FOUND NOT 
- [SDR A6WA202209088323](https://openairdocs.org/sdr/A6WA202209088323), Sep 8, 2022: HINGE FITTING. GOUGED. L/H ELEVATOR HINGE #2 FITTING GOUGED .550"L X .500"W X .010"D BETWEEN FS 59.02 AND FS 62.02. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 S
- [SDR A6WA202209088327](https://openairdocs.org/sdr/A6WA202209088327), Sep 8, 2022: NONE. CHAFED. PASSENGER DOOR HINGE LUG #1, #7, AND #9 ON DOOR SIDE OF HINGE HAVE WEAR AREAS ON OUTSIDE OF LUG. *************REMOVED AIRCRAFT FROM SERVICE*********************
- [SDR A6WA202209088333](https://openairdocs.org/sdr/A6WA202209088333), Sep 8, 2022: NONE. CHAFED. R/H AILERON LOWER SHROUD L/E HAS WEAR DAMAGE AT WS 360. **************REMOVED AIRCRAFT FROM SERVICE************************* BLENDED DAMAGE AREA TO A SMOOTH CON
- [SDR A6WA202209088325](https://openairdocs.org/sdr/A6WA202209088325), Sep 8, 2022: HINGE FITTING. GOUGED. R/H HSTAB HINGE #2 I/B FITTING GOUGED .7"L X .1"W X .020"D & O/B FITTING GOUGED .6"L X .1"W X .011"D AT RBL 55.89 AND I/B PLATE .6"L X .1"W X .010"D & O/B PLATE
- [SDR A6WA202209088326](https://openairdocs.org/sdr/A6WA202209088326), Sep 8, 2022: FLOOR PANEL. DAMAGED. MIS-LOCATED HOLE ON FLOOR PANEL #231ALF FOR FORWARD GALLEY ATTACH THROUGH POINT. *****************AIRCRAFT REMOVED FROM SERVICE******************** REMOVED DAMA
- [SDR A6WA202209088332](https://openairdocs.org/sdr/A6WA202209088332), Sep 8, 2022: NONE. GOUGED. AFT FACE OF AFT PRESSURE BULKHEAD "Z" STIFFENER AT FS 621 BL 0 AND WL 135.12 HAS A GOUGE .800"L X .500"W X .060"D. **************AIRCRAFT REMOVED FROM SERVICE**
- [SDR A6WA202209088316](https://openairdocs.org/sdr/A6WA202209088316), Sep 8, 2022: NONE. CORRODED. R/H FLOOR SEAT TRACK FROM FS 394 TO FS 409+128 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 394 TO FS 409+128
- [SDR A6WA202209088315](https://openairdocs.org/sdr/A6WA202209088315), Sep 8, 2022: PLATE. CORRODED. CORROSION ON FWD GALLEY SUPPORT PLATE AT FS 321 TO FS 327 AND RBL 4 TO RBL 8 AT WL 73.5. *******************AIRCRAFT REMOVED FROM SERVICE********************* U
- [SDR A6WA202209088317](https://openairdocs.org/sdr/A6WA202209088317), Sep 8, 2022: NONE. CORRODED. R/H FLOOR SEAT TRACK FROM FS 559 TO FS 559+112 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559 TO FS 559+112
- [SDR REXA2022091602101](https://openairdocs.org/sdr/REXA2022091602101), Sep 7, 2022: PANEL. CHAFED. TRANSCOWL PANEL 443BT IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-12-00-001-001-A01
- [SDR VNAA202209081111](https://openairdocs.org/sdr/VNAA202209081111), Sep 5, 2022: FADEC. UNSERVICEABLE. DUAL R ENG FADEC FAULT RESULTING IN R ENG FLAMEOUT DURING CLIMB. HAD SUCCESSFUL AUTO RE-LIGHT. PREFORMED A VISUALLY CHECK OF RH FADEC AND MADE SURE ALL CONNECTO
- [SDR 2022F00352](https://openairdocs.org/sdr/2022F00352), Sep 5, 2022: PITOT LINE. CONTAMINATED. NO AIRSPEED ON ISI, ABORTED TAKEOFF. REMOVED CONTAMINATION ON STANDBY PITOT LINE P3 IAW CRJ AMM 34-11-00. ALSO REMOVED AND REINSTALLED STANDBY PITOT HEAD AFTER 
- [SDR N6WA2022090801](https://openairdocs.org/sdr/N6WA2022090801), Sep 3, 2022: LIGHT. INOPERATIVE. EMERGENCY EXIT SIGNS ON FWD AND AFT R/H SIDE MID MONUMENTS ARE INOP.
- [SDR N6WA2022082901](https://openairdocs.org/sdr/N6WA2022082901), Aug 29, 2022: NONE. NONE. OVERHEAD EMERGENCY LIGHTS NOT WORKING AT ROWS 1, 3, 7, 17.REMOVED AND REPLACED EMERGENCY BATTERY PACKS 1,2,3,4 IAW CRJ AMM 33-51-17. SYSTEM OPS CHECKS GOOD.
- [SDR REXA2022083001985](https://openairdocs.org/sdr/REXA2022083001985), Aug 27, 2022: FRAME. CORRODED. FRAME AT F.S.319.00 IS CORRODED BETWEEN STRINGER 21L TO STRINGER 18L REMOVED AND REPLACED FRAME SECTOR AT F.S.319
- [SDR REXA2022083001983](https://openairdocs.org/sdr/REXA2022083001983), Aug 27, 2022: NONE. CRACKED. "FOUND CRACK AT EXISTING COCKPIT FLOOR BEAM REPAIR AT LBL 12 AND F.S280 " REPAIRED IAW CRJ-900 SRM 51-40-11-001-001-A01
- [SDR A6WA202207308300](https://openairdocs.org/sdr/A6WA202207308300), Aug 25, 2022: NONE. NONE. NOSE GEAR DISAGREE MESSAGE APPEARED AFTER LANDING GEAR WAS MOVED TO UP POSITION. RAN QRH, MESSAGE PERSIST. MANUALLY DEPLOY GEAR AND MESSAGE CLEARED. NOSE DOOR O
- [SDR A6WA202208238294](https://openairdocs.org/sdr/A6WA202208238294), Aug 23, 2022: CLEAT. CORRODED. CLEAT ATTACHED TO FS313.56 FRAME 601R318086-1 IS CORRODED ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW CLEAT IAW CRJ200 SRM 51-42-06
- [SDR A6WA202208208292](https://openairdocs.org/sdr/A6WA202208208292), Aug 20, 2022: NONE. NONE. ***SUPPLEMENTAL INFORMATION *****L REV UNLOCKED CAUTION MESSAGE ON DEPARTURE. IACS AND QRH C/W. YELLOW REV ICON. L REVRESER APPEARS PHYSICALLY STOWED. ***AIRCRA
- [SDR A6WA202208208293](https://openairdocs.org/sdr/A6WA202208208293), Aug 20, 2022: WEB. CORRODED. ****SUPPLEMENTAL INFORMATION *****MULTIPLE SPOTS OF CORROSION NOTED ON AFT PAX DOOR WEB (MARKED) ***AIRCRAFT REMOVED FROM SERVICE **** REPLACED PAX DOOR STAIRS 
- [SDR A6WA202208208291](https://openairdocs.org/sdr/A6WA202208208291), Aug 20, 2022: INTERCOSTAL. CORRODED. INTERCOSTAL BETWEEN FS333- FS349 STGR21L HAS CORROSION ****AIRCRAFT REMOVED FROM SERVICE **** REPLACED INTERCOSTAL BETWEEN FS333- FS349 STGR21L
- [SDR A6WA202208198290](https://openairdocs.org/sdr/A6WA202208198290), Aug 19, 2022: SEAT TRACK. CORRODED. CORROSION NOTED ON R/H FLOOR SEAT TRACK AT RBL9 BETWEEN FS409.00-409.00+120 ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW SEAT TRACK AT RBL9 BETWEEN FS409
- [SDR A6WA202208198289](https://openairdocs.org/sdr/A6WA202208198289), Aug 19, 2022: SEAT TRACK. CORRODED. RH SIDE SEAT RAIL FS409+16 TO FS409+112 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED A NEW RH SIDE SEAT RAIL FROM FS409.00+
- [SDR A6WA202208188286](https://openairdocs.org/sdr/A6WA202208188286), Aug 18, 2022: SEAT TRACK. CORRODED. CORROSION NOTED ON R/H FLOOR SEAT RAIL AT RBL9 AND APPROX. BETWEEN FS364.00-FS398] ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED SEAT RAIL ON RBL 9 FLOOR BEA

All 333: https://openairdocs.org/model/canadair-cl215-1a10/reports.md

## STCs that may be installed (OpenAirDocs) (15)

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 ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC ST04689NY](https://openairdocs.org/stc/ST04689NY): Installation of the Artex Emergency Locator Transmitter (ELT). Genesys Certification Services Inc
- [STC ST04653NY](https://openairdocs.org/stc/ST04653NY): Installation of the Collins Aerospace Angle of Attack Indicating System. B/E Aerospace Limited
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC
- [STC SA571NE](https://openairdocs.org/stc/SA571NE): Installation of cockpit vapor cycle air conditioning system kit No. 215-CCA-001. Rilpa Enterprises, Ltd
- [STC ST01425NY](https://openairdocs.org/stc/ST01425NY): Installation of a Flight Deck Cooling System. ACS-NAI Limited
- [STC ST01824NY](https://openairdocs.org/stc/ST01824NY): Installation of Northern Airborne Technology Satphone. Northern Airborne Technology Ltd
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies
- [STC SQ00643NY](https://openairdocs.org/stc/SQ00643NY): Installation of spinners and balancing weights for dynamic propeller balancing. Airworthiness Resources Corporation
- [STC SA2178WE](https://openairdocs.org/stc/SA2178WE): Installation of liquid spray system. Aviation Specialties Inc

## PMA parts (OpenAirDocs) (302, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122857459820241107175402.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [LA555153](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187300776320240904014314.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555153 · Aug 28, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173336744520241016174856.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA3460X240A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172487862520240904014158.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R03460X240A20B6 · Aug 28, 2024
- [LA559018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170560101920240904014321.0001): Dilution Screen. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 559018 · Aug 28, 2024
- [LA555015](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169167416420240904014246.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555015 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166541228120241016174949.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [LA555033](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160010110220240904014259.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555033 · Aug 28, 2024
- [LA495357](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158121345820240904014218.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 495357 · Aug 28, 2024
- [LA490X190A5005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138749531720240904014211.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00490X190A50D5 · Aug 28, 2024
- [LA220X160A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130516305920240904014152.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00220X160A20B6 · Aug 28, 2024
- [LA553008](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130343847220240904014226.0001): Gasket. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553008 · Aug 28, 2024
- [LA412505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127651422320240904014205.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 412505 · Aug 28, 2024
- [LA555012](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122337498620240904014239.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555012 · Aug 28, 2024
- [LA555070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114325356220240904014307.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555070 · Aug 28, 2024
- [LA553044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112890959020240904014232.0001): Valve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553044 · Aug 28, 2024
- [LA555016](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111529370720240904014252.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555016 · Aug 28, 2024
- [422B340LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198888423020240724143348.0001): Overhaul Kit. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 422B340 · Jul 3, 2024
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193765214920260304184319.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191913431920260304184316.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189695445320260311205448.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175347865120260304184322.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [PTA12-300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159155630820260304184318.0001): POTS Telephone Adapter with NVIS B Display. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Replaces PTA12-300 · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143473343220260311205444.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [PTA12-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142392616220260304184316.0001): POTS Telephone Adapter with Display. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Replaces PTA12-100 · Nov 1, 2021
- [PTA12-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137382967220260311205444.0001): POTSTelephone Adapter with Display. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Replaces PTA12-100 · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137200348620260311205447.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124920604120260311205445.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122341736820260304184320.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114403996720260311205446.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [PTA12-300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108124104220260311205445.0001): POTSTelephone Adapter with NVIS B Display. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Replaces PTA12-300 · Nov 1, 2021
- [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105325781520260304184318.0001): “. Chelton Avionics Inc. dba Canyon Aeroconnect · PMA PQ2204NM · Nov 1, 2021
- [SP3558-50-1020B](https://drs.faa.gov/browse/excelExternalWindow/9D6A8DE9179A14F08625862B00460568.0001): Sleeve. Soundair Aviation Services · PMA PQ2540NM · Replaces 495357 · Oct 21, 2020
- [SP3558-51-1450](https://drs.faa.gov/browse/excelExternalWindow/2303B92B6268F03A86258570004EAB4A.0001): Gasket, Dilution. Soundair Aviation Services · PMA PQ2540NM · Replaces 553008 · Oct 16, 2019
- [449189LA](https://drs.faa.gov/browse/excelExternalWindow/4C2A2307ABFB46A88625834B005E392E.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449189 · Sep 23, 2018
- [422B340LA](https://drs.faa.gov/browse/excelExternalWindow/8C45C6BF9F6BB6DA86258344006D7F2C.0001): Overhaul Kit. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 422B340 · Sep 6, 2018
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/E23CF976882B9D34862583370055CCC2.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Jul 24, 2018
- [TAE0528-1X](https://drs.faa.gov/browse/excelExternalWindow/F588B8F46C785161862582A60062074D.0001): Par 36 Lamp Cool Spot Hi Intensity. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0528-1W](https://drs.faa.gov/browse/excelExternalWindow/E8E9E4B13657A183862582A60062074C.0001): Par 36 Lamp Warm Spot. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0528-2](https://drs.faa.gov/browse/excelExternalWindow/C4958AB365AFD03E862582A60062074F.0001): Par 36 Lamp Cool Wide. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0528-2W](https://drs.faa.gov/browse/excelExternalWindow/9A52E69503003D74862582A600620750.0001): Par 36 Lamp Warm Wide. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0628-1](https://drs.faa.gov/browse/excelExternalWindow/7BBB8098D24505E6862582A60062075D.0001): Par 46 Lamp Cool Spot. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0528-1](https://drs.faa.gov/browse/excelExternalWindow/4D0CCF177D7F40A8862582A600620749.0001): Par 36 Lamp Cool Spot. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [TAE0628-2](https://drs.faa.gov/browse/excelExternalWindow/02F9E37823E68557862582A600620770.0001): Par 46 Lamp Cool Wide. Talon Aerospace · PMA PQ4013CE · Modification part · Apr 15, 2018
- [87-05208-001](https://drs.faa.gov/browse/excelExternalWindow/E637622B78D6C2AB8625822E007853C7.0001): Assembly, Light, PAR 46 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces TAE0628-1 · Jan 23, 2018
- [87-05208-002](https://drs.faa.gov/browse/excelExternalWindow/3CD0B411F422074A8625822E007853C9.0001): Assembly, Light, PAR 46 Taxi. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces TAE0628-2 · Jan 23, 2018
- [LA419628](https://drs.faa.gov/browse/excelExternalWindow/6CA7F032229EE5338625818D0059B92E.0001): Block, Locking. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 419628 · May 25, 2017
- [LA553044](https://drs.faa.gov/browse/excelExternalWindow/FDE8730A8189275E8625807B006FD294.0001): Valve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553044 · Nov 22, 2016
- [LA555012](https://drs.faa.gov/browse/excelExternalWindow/D36AE95795CCEB148625807B006FD307.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555012 · Nov 22, 2016
- [LA555015](https://drs.faa.gov/browse/excelExternalWindow/D1C492114DB82CEE8625807B006FD37B.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555015 · Nov 22, 2016

All of them: https://openairdocs.org/model/canadair-cl215-1a10/pma.md

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