# Service difficulty reports: Canadair CL215 1A10

A list on [Canadair CL215 1A10](https://openairdocs.org/model/canadair-cl215-1a10.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 333 reports

- [SDR N6WA2023031401](https://openairdocs.org/sdr/N6WA2023031401.md): Elt · inoperative · Mar 10, 2023 · N547GJ · Cndair CL2151A10 · Emergency Locator Beacon
  > 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.md): Doubler · corroded · Feb 10, 2023 · N544EA · Cndair CL2151A10 · Fuselage Main, Structure
  > 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 51-42-06-001-001-A01. INSTALLED NEW ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-06-
- [SDR VNAA202302100003](https://openairdocs.org/sdr/VNAA202302100003.md): None · cracked · Feb 10, 2023 · N537EA · Cndair CL2151A10 · Doors
  > 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 52-11-04-201-009-A01
- [SDR VNAA202302100002](https://openairdocs.org/sdr/VNAA202302100002.md): None · none · Feb 10, 2023 · N537EA · Cndair CL2151A10 · Fuselage Main, Structure
  > 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) CORRECTIVE ACTION: C/W SB_670BA-53-040-REQ (FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.
- [SDR VNAA202302100001](https://openairdocs.org/sdr/VNAA202302100001.md): None · cracked · Feb 10, 2023 · N537EA · Cndair CL2151A10 · Doors
  > 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. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-52-11-1314 REV IR
- [SDR A6WA202210158343](https://openairdocs.org/sdr/A6WA202210158343.md): Shear Plate · corroded · Oct 15, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Internal Stairs
  > 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 FS330.0 SHEAR PLATE AND MOUNT
- [SDR A6WA202210158344](https://openairdocs.org/sdr/A6WA202210158344.md): None · corroded · Oct 15, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Structure (General)
  > 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.md): None · corroded · Oct 14, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > 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 SIDE SEAT RAIL, APPROX. FS364.00 THRU FS409+16
- [SDR A6WA202210148342](https://openairdocs.org/sdr/A6WA202210148342.md): None · none · Oct 14, 2022 · N466AW · Cndair CL2151A10 · Tire
  > 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 AMM 32-42-06 PERFORMED A-SKID ADJUSTMENT TEST. OPS CHECK GOOD P
- [SDR A6WA202210148341](https://openairdocs.org/sdr/A6WA202210148341.md): None · corroded · Oct 14, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Structure (General)
  > 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 53-00-43
- [SDR A6WA202210138339](https://openairdocs.org/sdr/A6WA202210138339.md): None · none · Oct 13, 2022 · N448AW · Cndair CL2151A10 · Landing Gear Actuator
  > 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 OPEN WARNING MESSAGE WHILE C/W QRH. NOSE GEAR BOX TURNED RED ON EICAS, MANUAL DEPLOYMENT WAS REQUI
- [SDR A6WA202209088338](https://openairdocs.org/sdr/A6WA202209088338.md): None · none · Oct 12, 2022 · N464AW · Cndair CL2151A10 · Nose/Tail Landing Gear Attach Section
  > 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 DECLARED. NLG REMAINED DOWN WHEN SELECTING GEAR UP. ****AIRCRAFT REMOVED FROM SERVICE**** SERVICE
- [SDR SWIA202266599](https://openairdocs.org/sdr/SWIA202266599.md): None · failed · Oct 9, 2022 · N709SK · Cndair CL2151A10 · Landing Gear Door Actuator
  > GEAR DISAGREE AFTER SELECTING GEAR UP. NOSE WHEEL NOT LOCKED. (FLIGHT 4923 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25627409 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC FOUND GEAR DISAGREE B1- 007437. TROUBLESHOT IN REF T
- [SDR A6WA202210098320](https://openairdocs.org/sdr/A6WA202210098320.md): None · chafed · Oct 9, 2022 · N456ZW · Cndair CL2151A10 · Doors
  > 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 SUPPLEMENT #13-117 AND REO 601R-52-82-366 DATED 22MAR2013 APPENDIX-A
- [SDR A6WA202210098321](https://openairdocs.org/sdr/A6WA202210098321.md): Vane Cap · chafed · Oct 9, 2022 · N456ZW · Cndair CL2151A10 · Aileron Tabs
  > *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 I/B FLAP. REF CRJ-200 SRM 51-42-13.
- [SDR A6WA202210088319](https://openairdocs.org/sdr/A6WA202210088319.md): None · corroded · Oct 8, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Internal Mounting Structure
  > 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.md): Seat Track · chafed · Oct 8, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Main, Keel
  > 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 SEAT RAIL
- [SDR A6WA202210068314](https://openairdocs.org/sdr/A6WA202210068314.md): Seat Track · none · Oct 6, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Main, Keel
  > 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-53-11-1093 REV C. (LP 342242/1 & 2). PERFORM PERMANENT REPAIR AS REQUIRED. ****AIRCRAFT REMOVED FRO
- [SDR A6WA202210058313](https://openairdocs.org/sdr/A6WA202210058313.md): None · none · Oct 5, 2022 · N447AW · Cndair CL2151A10 · Landing Gear System
  > 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 STARTED TO SLOWLY VEER TO THE RIGHT, I TOOK THE REVERS OUT THINKING THIS WILL HELP THE SITUATION AND THEN
- [SDR A6WA202210028311](https://openairdocs.org/sdr/A6WA202210028311.md): Angle · corroded · Oct 2, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Main, Frame
  > 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 AND BOMBARDIER DRAWING 601R31527 REV AM
- [SDR A6WA202210028312](https://openairdocs.org/sdr/A6WA202210028312.md): Angle · corroded · Oct 2, 2022 · N456ZW · Cndair CL2151A10 · Fuselage Main, Frame
  > 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 BOMBARDIER DRAWING 601R31527 REV AM
- [SDR A6WA202209088334](https://openairdocs.org/sdr/A6WA202209088334.md): Floor Support · damaged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage, Door Hinge
  > FLOOR SUPPORT STRUCTURE BETWEEN FS 409+128 - FS 424 & LBL 9 - RBL 27 HAVE ELONGATED HOLES. ***************REMOVED AIRCRAFT FROM SERVICE********************* OPENED DAMAGED HOLES TO MINIMUM DIAMETER COMPLETELY REMOVING DAMAGE WITHOUT EXCEEDING.350" IAW MHIRJ
- [SDR A6WA202209088335](https://openairdocs.org/sdr/A6WA202209088335.md): None · chafed · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Aileron Tabs
  > 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 WITH DIMENSIONS OF 1.2"L X.500"W X.025"D IAW ASAP EA #AWAC-CRJ257-01891 REV B DATED 10/08/2022. VERIF
- [SDR A6WA202209088336](https://openairdocs.org/sdr/A6WA202209088336.md): None · chafed · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Aileron Tabs
  > 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 DIMENSIONS OF 1.2"L X.500"W X.014"D IAW ASAP EA #AWAC-CRJ257-01890 REV B DATED 10/12/2022. VERIFI
- [SDR A6WA202209088337](https://openairdocs.org/sdr/A6WA202209088337.md): None · none · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Accessory Compartment Doors
  > 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 REMOVED FROM SERVICE************************* REPAIRED DAMAGE ON R/H TRU ACCESS DOOR IAW ASAP EA #AWA
- [SDR A6WA202209088324](https://openairdocs.org/sdr/A6WA202209088324.md): Hinge Fitting · gouged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Elevator, Plate/Skin
  > 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 WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-20-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE******
- [SDR A6WA202209088323](https://openairdocs.org/sdr/A6WA202209088323.md): Hinge Fitting · gouged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Empennage Structure
  > 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 SRM 55-20-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** PERFORMED BLE
- [SDR A6WA202209088327](https://openairdocs.org/sdr/A6WA202209088327.md): None · chafed · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Doors
  > PASSENGER DOOR HINGE LUG #1, #7, AND #9 ON DOOR SIDE OF HINGE HAVE WEAR AREAS ON OUTSIDE OF LUG. *************REMOVED AIRCRAFT FROM SERVICE************************ BLENDED PASSENGER DOOR HINGE LUGS TO MINIMUM REMAINING WALL THICKNESS OF #1 (.084), #7 (.082),
- [SDR A6WA202209088333](https://openairdocs.org/sdr/A6WA202209088333.md): None · chafed · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Wing Structure
  > R/H AILERON LOWER SHROUD L/E HAS WEAR DAMAGE AT WS 360. **************REMOVED AIRCRAFT FROM SERVICE************************* BLENDED DAMAGE AREA TO A SMOOTH CONTOUR WITH DIMENSIONS OF 2.0"L X 1.0"W X.037"D IAW ASAP EA #AWAC-CRJ257-01895 REV A DATED 09/30/2022
- [SDR A6WA202209088325](https://openairdocs.org/sdr/A6WA202209088325.md): Hinge Fitting · gouged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Horizontal Stabilizer, Plate/Skin
  > 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.6"L X.1"W X.017"D. DAMAGE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-20-00 REV 39. *********A
- [SDR A6WA202209088326](https://openairdocs.org/sdr/A6WA202209088326.md): Floor Panel · damaged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage Structure (General)
  > MIS-LOCATED HOLE ON FLOOR PANEL #231ALF FOR FORWARD GALLEY ATTACH THROUGH POINT. *****************AIRCRAFT REMOVED FROM SERVICE******************** REMOVED DAMAGED OUTER PLIES IN AREAS OF MIS-LOCATED HOLE. POTTED HOLE USING MAGNABOND 92-1 AND APPLIED REPAIR P
- [SDR A6WA202209088332](https://openairdocs.org/sdr/A6WA202209088332.md): None · gouged · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage Structure (General)
  > 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*********************** BLENDED GOUGE ON "Z" STIFFENER TO A SMOOTH CONTOUR ENSURING REPORTED DEPTH OF
- [SDR A6WA202209088316](https://openairdocs.org/sdr/A6WA202209088316.md): None · corroded · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage Structure (General)
  > 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 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT RE
- [SDR A6WA202209088315](https://openairdocs.org/sdr/A6WA202209088315.md): Plate · corroded · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > 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********************* UPON FURTHER INSPECTION OF SUPPORT PLATE FOUND INTERGRANULAR CORROSION NOT WITHIN ALLOWABLE LIMITS I
- [SDR A6WA202209088317](https://openairdocs.org/sdr/A6WA202209088317.md): None · corroded · Sep 8, 2022 · N460AW · Cndair CL2151A10 · Fuselage Structure (General)
  > 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 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT RE
- [SDR REXA2022091602101](https://openairdocs.org/sdr/REXA2022091602101.md): Panel · chafed · Sep 7, 2022 · N919XJ · Cndair CL2151A10 · Engine Thrust Reverser
  > TRANSCOWL PANEL 443BT IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-12-00-001-001-A01
- [SDR VNAA202209081111](https://openairdocs.org/sdr/VNAA202209081111.md): Fadec · unserviceable · Sep 5, 2022 · N565NN · Cndair CL2151A10 · Engine (Turbine/Turboprop)
  > 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 CONNECTORS ARE SECURED, NO DEFECTS NOTED. PERFORMED A POWER ON BUILT IN TEST IAW CRJ900 AMM 71-00-00-710-801
- [SDR 2022F00352](https://openairdocs.org/sdr/2022F00352.md): Pitot Line · contaminated · Sep 5, 2022 · N524GJ · Cndair CL2151A10 · Altimeter, Barometric/Encoder
  > 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 CONTAMINATION REMOVAL IAW CRJ AMM 34-11-02.
- [SDR N6WA2022090801](https://openairdocs.org/sdr/N6WA2022090801.md): Light · inoperative · Sep 3, 2022 · N548GJ · Cndair CL2151A10 · Emergency Lighting
  > EMERGENCY EXIT SIGNS ON FWD AND AFT R/H SIDE MID MONUMENTS ARE INOP.
- [SDR N6WA2022082901](https://openairdocs.org/sdr/N6WA2022082901.md): None · none · Aug 29, 2022 · N578GJ · Cndair CL2151A10 · Emergency Lighting
  > 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.md): Frame · corroded · Aug 27, 2022 · N8918B · Cndair CL2151A10 · Fuselage Miscellaneous Structure
  > 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.md): None · cracked · Aug 27, 2022 · N8918B · Cndair CL2151A10 · Fuselage Main, Structure
  > "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.md): None · none · Aug 25, 2022 · N463AW · Cndair CL2151A10 · Landing Gear System
  > 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 OPEN WARNING MESSAGE APPEARED AFTER GEAR DISAGREE MESSAGE WAS DISPLAYED. NO GEAR BOXES WERE RED, ONL
- [SDR A6WA202208238294](https://openairdocs.org/sdr/A6WA202208238294.md): Cleat · corroded · Aug 23, 2022 · N452AW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > 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.md): None · none · Aug 20, 2022 · N425AW · Cndair CL2151A10 · Engine Exhaust System
  > ***SUPPLEMENTAL INFORMATION *****L REV UNLOCKED CAUTION MESSAGE ON DEPARTURE. IACS AND QRH C/W. YELLOW REV ICON. L REVRESER APPEARS PHYSICALLY STOWED. ***AIRCRAFT REMOVED FROM SERVICE ***** LFT TR DEACTIVATED PER AWAC SUP 15-046D. THE TR WAS FOUND TO BE IN
- [SDR A6WA202208208293](https://openairdocs.org/sdr/A6WA202208208293.md): Web · corroded · Aug 20, 2022 · N452AW · Cndair CL2151A10 · Doors
  > ****SUPPLEMENTAL INFORMATION *****MULTIPLE SPOTS OF CORROSION NOTED ON AFT PAX DOOR WEB (MARKED) ***AIRCRAFT REMOVED FROM SERVICE **** REPLACED PAX DOOR STAIRS AFT WEB
- [SDR A6WA202208208291](https://openairdocs.org/sdr/A6WA202208208291.md): Intercostal · corroded · Aug 20, 2022 · N452AW · Cndair CL2151A10 · Fuselage Floor Panel
  > INTERCOSTAL BETWEEN FS333- FS349 STGR21L HAS CORROSION ****AIRCRAFT REMOVED FROM SERVICE **** REPLACED INTERCOSTAL BETWEEN FS333- FS349 STGR21L
- [SDR A6WA202208198290](https://openairdocs.org/sdr/A6WA202208198290.md): Seat Track · corroded · Aug 19, 2022 · N452AW · Cndair CL2151A10 · Fuselage, Door Hinge
  > 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 FS409.00 TO FS409.00+120 REF CRJ200 AMM 53-01-11-400-802. TOOL# TUC8612 CAL DUE DATED 31-OCT-22.
- [SDR A6WA202208198289](https://openairdocs.org/sdr/A6WA202208198289.md): Seat Track · corroded · Aug 19, 2022 · N452AW · Cndair CL2151A10 · Fuselage, Door Hinge
  > 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+16-FS409.00+112 WITH NEW HARDWARE. REF CRJ 200 AMM 53-01-11-400-802 AND REO 601R-53-00-055 REV-C DAT
- [SDR A6WA202208188286](https://openairdocs.org/sdr/A6WA202208188286.md): Seat Track · corroded · Aug 18, 2022 · N452AW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > 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 BEAM BETWEEN FS 364 AND FS 398 REF CRJ200 AMM 53-01-11-400-802

Next page: https://openairdocs.org/model/canadair-cl215-1a10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'CL2151A10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/canadair-cl215-1a10/reports

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