# Service difficulty reports: N425AW

A list on [N425AW](https://openairdocs.org/aircraft/N425AW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 210 reports

- [SDR A6WA202410058833](https://openairdocs.org/sdr/A6WA202410058833.md): Pressure Blkhd · damaged · Oct 5, 2024 · N425AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING REPLACEMENT OF THE AFT CARGO DOOR BALANCE SPRING MOUNTING BRACKET, MAINTENANCE FOUND THREE ELONGATED RIVET HOLES. ***** AIRCRAFT REMOVED FROM SERVICE ***** MHI WAS CONTACTED AND REO 601R-53-61-8234 WAS ISSUED. THREE FASTENER LOCATIONS WERE OVERSIZED AN
- [SDR A6WA202404048729](https://openairdocs.org/sdr/A6WA202404048729.md): Tube · clogged · Apr 4, 2024 · N425AW · Cndair CL6002B19 · Airspeed/Mach Indicator
  > DURING 80 KNOT CROSS CHECK DURING TAKE-OFF ROLL, PM NOTED STANDBY AIRSPEED INDICATOR FLUCTUATE AND DROP TO 0 IAS. PM CALLED ABORTED TAKE-OFF. BRAKE TEMPS REMAINED NORMAL. AIRCRAFT REMOVED FROM SERVICE. C/W INSPECTION OF STANDBY PITOT P3 DRAIN COLLECTOR TUBE I
- [SDR A6WA202304218576](https://openairdocs.org/sdr/A6WA202304218576.md): Hinge Fitting · unknown · Apr 21, 2023 · N425AW · Cndair CL6002B19 · Wing Structure
  > FOUND I/B BUSHING LUG BORE OF O/B FITTING FOR RH WING SIDE AILERON ATTACH POINT TO BE PREVIOUSLY OVERSIZED. ***** AC REMOVED FROM SERVICE ***** REPAIRED IAW BOMBARDIER REO 601R-57-51-05 REV NC DATED AUG 09, 1995, AND MHIRJ REO 601R-57-51-1011 REV-- DATED 2023-
- [SDR A6WA202304198568](https://openairdocs.org/sdr/A6WA202304198568.md): Drag Angle · cracked · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE DRAG ANGLE PN 601R31772-5S ONTO AFT WEB IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR A6WA202304198574](https://openairdocs.org/sdr/A6WA202304198574.md): Former · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FWD FORMER F.S.311.75 BETWEEN DD5 AND DD4 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED, AND INSTALLED SERVICEABLE PAX DOOR FWD FORMER P/N 601R318031-5 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21.
- [SDR A6WA202304198569](https://openairdocs.org/sdr/A6WA202304198569.md): Seat Track · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > Ï¿½LBL9 SEAT TRACK FS559+4 - FS559+86 SEGMENT IS CORRODED. ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW SEAT TRACK P/N 601R31032-9S LOCATED, DRILLED, AND INSTALLED AT LBL9 BETWEEN FS559+4 AND FS559+86 IAW CRJ-200 SRM 51-40-11 AND AMM 53-00-49-400-801
- [SDR A6WA202304198567](https://openairdocs.org/sdr/A6WA202304198567.md): Hinge · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > Ï¿½PAX DOOR LOWER FOLDING STEP HINGE THAT ATTACHES TO THE PAX DOOR SILL HAS EXFOLIATION IN 2 PLACES. ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW HINGE ON TOP STEP P/N (601R31980-41) IAW CRJ200 51-41-02
- [SDR A6WA202304198571](https://openairdocs.org/sdr/A6WA202304198571.md): Cleat · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED, AND INSTALLED SERVICEABLE DD4 FWD CLEAT P/N 600-31902-269 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR A6WA202304198573](https://openairdocs.org/sdr/A6WA202304198573.md): Frame · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Main, Frame
  > PAX DOOR FRAME 313.56 BETWEEN DD4 AND DD5 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED AND DRILLED NEW PAX DOOR FRAME AT F/S 313.56 IAW CRJ 200 SRM 51-40-11, INSTALLED NEW FRAME P/N 601R318086-1 IAW CRJ 200 SRM 51-42-06
- [SDR A6WA202304198572](https://openairdocs.org/sdr/A6WA202304198572.md): Intercostal · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR MID INTERCOSTAL DD6 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATE, DRILLED AND INSTALLED SERVICEABLE INTERCOSTAL DD6 MID P/N 601R318057-1 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21.
- [SDR A6WA202304198570](https://openairdocs.org/sdr/A6WA202304198570.md): Intercostal · corroded · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR INTERCOSTAL DD7 FWD IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED AND INSTALLED SERVICEABLE DD7A FWD INTERCOSTAL IAW CRJ 200 SRM 51-40-11 AND 51-46-06.
- [SDR A6WA202304198566](https://openairdocs.org/sdr/A6WA202304198566.md): Angle · cracked · Apr 19, 2023 · N425AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR INNER ANGLE AT PRESSURE RELEASE DOOR IS CRACKED. *********AIRCRAFT REMOVED FROM SERVICE************ REMOVED CRACKED ANGLE, LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE PN 601R318072-1 IAW CRJ 200 SRM 51-40-11 AND 51-42-06
- [SDR A6WA202304188564](https://openairdocs.org/sdr/A6WA202304188564.md): Cap · corroded · Apr 18, 2023 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > 3 EA. TOP PLATES CORRODED ON FLOOR BEAM AT FS589 BETWEEN LBL9 AND RBL9 *********AIRCRAFT REMOVED FROM SERVICE********* UPON INVESTIGATION FOUND DAMAGE TO BOTH LBL9 AND RBL 9 TO BE WITHIN LIMITS. LBL9 CAP SPLICE: LOWEST REMAINING 0.076". ORIGINAL THICKNESS WAS
- [SDR A6WA202304188565](https://openairdocs.org/sdr/A6WA202304188565.md): Diaphragm · corroded · Apr 18, 2023 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > JUST FWD. OF F.S.621 @ FWD. FLOOR BEAM (PRESSURE DIAPRAM AREA) TOP BEAM CAP IS CORRODED (AS MARKED) UNDER 281CLF ********AIRCRAFT REMOVED FROM SERVICE*********** DIAPHRAGM ASSEMBLY REQUIRES REPLACEMENT RECEIVED LOCATED AND DRILLED NEW SERVICEABLE DIAPHRAGM A
- [SDR A6WA202304188563](https://openairdocs.org/sdr/A6WA202304188563.md): Floorbeam · corroded · Apr 18, 2023 · N425AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL27 FLOOR BEAM IS CORRODED BETWEEN FS569 AND FS621. ******AIRCRAFT REMOVED FROM SERVICE******** INSTALLED LBL27 FLOOR BEAM BETWEEN FS569 AND FS621 IAW CRJ-200 SRM 51-42-21, 51-42-34, AND REO 601R-53-61-3778 REV -B DATED: 2016-1
- [SDR A6WA202304138584](https://openairdocs.org/sdr/A6WA202304138584.md): Bushing · unknown · Apr 13, 2023 · N425AW · Cndair CL6002B19 · Wing Structure
  > FOUND I/B BUSHING LUG BORE OF O/B FITTING FOR RH WINGSIDE AILERON ATTACH POINT TO BE PREVIOUSLY OVERSIZED. ***** AC REMOVED FROM SERVICE ***** COMPLIED WITH MHIRJ REO 601R-57-51-1011 REV -- DATED 2023-04-18.
- [SDR A6WA202304078549](https://openairdocs.org/sdr/A6WA202304078549.md): Track · corroded · Apr 7, 2023 · N425AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. ******AIRCRAFT REMOVED FROM SERVICE******** INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL9 FS 559+86 TO 559+96 IAW CRJ200 AMM 53-01-11-400-802.
- [SDR A6WA202304078548](https://openairdocs.org/sdr/A6WA202304078548.md): Seat Track · corroded · Apr 7, 2023 · N425AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK FS559+4 - FS559+86 SEGMENT IS CORRODED. ******AIRCRAFT REMOVED FROM SERVICE******* EVALUATED CORROSION AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS, IAW CRJ200 SRM 53-21-49. RBL 9 FS 559+4 TO 559+86 SEAT TRACK REQUIRE REPLACEMEN
- [SDR A6WA202304078550](https://openairdocs.org/sdr/A6WA202304078550.md): Track · corroded · Apr 7, 2023 · N425AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL27 SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. ********AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL27, FS559+78 TO FS 559+96 IAW CRJ200 AMM 53-01-11-400-802.
- [SDR A6WA202304078551](https://openairdocs.org/sdr/A6WA202304078551.md): Seat Track · corroded · Apr 7, 2023 · N425AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. *******AIRCRAFT REMOVED FROM SERVICE******** REMOVED UNSERVICEABLE CARGO TIE DOWN TRACK, FIT, & DRILLED FROM P/N 20276-288-0-0A, PAINTED AND INSTALLED NEW SECTION IAW BOMBARDIER REO# 601R-53-00-485, REV-
- [SDR A6WA202302188466](https://openairdocs.org/sdr/A6WA202302188466.md): Unknown · unknown · Feb 18, 2023 · N425AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER CLEARING RUNWAY FOR ABORTED TAKE-OFF, TOWER INFORMED US THE LH ENGINE WAS SMOKING. ALL LH ENG INDICATIONS WERE "0". PERFORMED ENG SHUT DOWN. NO LH ENGINE FIRE INDICATION IN THE COCKPIT. FIRE BOTTLES DISCHARGED. PAX EVACUATED THROUGH MAIN CABIN DOOR.
- [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 A6WA202202048095](https://openairdocs.org/sdr/A6WA202202048095.md): None · none · Feb 2, 2022 · N425AW · Cndair CL6002B19 · Rate of Climb Indicator
  > IN CRUISE RECEIVED IAS COMP ON FLAG ON CAPT PFD. CW QRH MESSAGE CLEARED AFTER SELECTING AIR DATA COMPUTER TO #2 PER QRH. ***AIRCRAFT REMOVED FROM SERVICE*** R&R #1 ADC IAW AMM 34-13-01 AND SUP 17-010A. ALL OPS AND FUNC TEST GOOD
- [SDR A6WA202109227886](https://openairdocs.org/sdr/A6WA202109227886.md): Frame · corroded · Sep 22, 2021 · N425AW · Cndair CL6002B19 · Fuselage Floor Panel
  > FWD FACE OF FRAME AT FS 333.0 CORRODED BETWEEN STR 21R TO 24R. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FRAME AT FS 333.0 BETWEEN STR 17R TO 22R IAW CRJ-200 SRM 51-42-06 AND 51-42-21
- [SDR A6WA202109217884](https://openairdocs.org/sdr/A6WA202109217884.md): Frame · corroded · Sep 21, 2021 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FWD AND AFT FACE, AND LWR LEG OF FRAME AT FS 605.00 CORROSION BETWEEN STR 26R AND 23R ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM FWD AND AFT FACE OF FRAME AT FS 605.00 BETWEEN STR 26R AND 23R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS.050,
- [SDR A6WA202109217883](https://openairdocs.org/sdr/A6WA202109217883.md): Frame · corroded · Sep 21, 2021 · N425AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT FACE OF FRAME AT FS 589.0 SEVERAL SPOTS OF CORROSION BETWEEN STR 25R AND 27. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM AFT FACE AT FS 589.0 BETWEEN STR 25R AND 27R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS.050, THICKNESS REMAINING.
- [SDR A6WA202109157878](https://openairdocs.org/sdr/A6WA202109157878.md): Washer · corroded · Sep 15, 2021 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH AND RH GEAR WELLS PASS THROUGH AT FS 544-549 HAS CORROSION REQUIRES FURTHER EVAL UPON FURTHER INVESTIGATION FOUND WASHERS TO BE CORRODED, REMOVED AND REPLACED WASHERSIAW CRJ-200 SRM 51-41-02 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED WASHERS
- [SDR A6WA202103097710](https://openairdocs.org/sdr/A6WA202103097710.md): Control Unit · malfunctioned · Mar 8, 2021 · N425AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > DURING APPROACH SELECTED FLAPS 8 THEN RECEIVED FLAPS FAIL CAUTION MSG FLIGHT CONTROL SYSNOPTIC PAGE SHOWED FLAPS AT 0 DEGREES,COMPLIED WITH QRD CK LIST. NORAML LANDING,SMOTH TOUCHDOWN, BPMS READING SHOWED 5-5-4-4. PERFORMED FLAP RESET PROCEDURE IAW AWAC SOP 98
- [SDR A6WA2020080657281](https://openairdocs.org/sdr/A6WA2020080657281.md): Bpsu · malfunctioned · Aug 5, 2020 · N425AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECIEVED FLAPS FAIL CAUTION MESSAGE DURING THE APPROACH. FLAPS FAILED AT ZERO DEGREES. COMPLIED WITH QRH. LANDED AT FLAPS ZERO. PERFORMED FLAP RESET PROCEDURE IAW 98-18I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. RIGGED THE LT AND RT FLAP
- [SDR A6WA2019112047020](https://openairdocs.org/sdr/A6WA2019112047020.md): Strut · malfunctioned · Nov 16, 2019 · N425AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > SUPPLIMENTAL INFORMATION, AFTER T/O, ON LANDING GEAR UP, WE RECIEVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES WITH WOW INPUT CAUTION MESSAGE. AIRCRAFT REMOVED FROM SERVICE. SERVICED NLG SHOCK STUT IAW AMM 12-12-32-610-803.
- [SDR A6WA2019110546976](https://openairdocs.org/sdr/A6WA2019110546976.md): Door Sill · corroded · Nov 5, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL HAS CORROSION ON THE UPPER AND LOWER SURFACES AT NUT PLATE LOCATIONS BETWEEN FS559+80 AND 621 AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H FLOOR SILL @ FS559+80 IAW CRJ-206 00 SRM 51-42-AND 51-22-21
- [SDR A6WA2019110546975](https://openairdocs.org/sdr/A6WA2019110546975.md): Door Sill · corroded · Nov 5, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL HAS CORROSION ON THE UPPER AND LOWER SURFACES AT NUT PLATE LOCATIONS BETWEEN FS559+80 AND 621 REMOVED AND REPLACED R/H FLOOR SILL @ FS559+80 IAW CRJ-200 SRM 51-42-06 AND 51-22-21
- [SDR A6WA2019110546973](https://openairdocs.org/sdr/A6WA2019110546973.md): Post · cracked · Nov 4, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 POST AT LEFT BL18 IS CRACKED IN THE O/B RADIUS. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FS409+128 POST IAW REO 601R-53-41-889 REV-D.
- [SDR A6WA2019110546974](https://openairdocs.org/sdr/A6WA2019110546974.md): Angle · corroded · Nov 4, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE CORRODED AIRCRAFT REMOVED FROM SERVICE REPLACED LOWER SILL ANGLE IAW CRJ200 SRM 51-42-06, 53-00-00.
- [SDR A6WA2019110146967](https://openairdocs.org/sdr/A6WA2019110146967.md): Bracket · cracked · Oct 30, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 449 RBL 47 FAIRING BRACKET IS CRACKED. AIRCRAFT GROUNDED REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM 51-42-06.
- [SDR A6WA2019102946966](https://openairdocs.org/sdr/A6WA2019102946966.md): Frame · corroded · Oct 29, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 513 MACHINED FRAME HAS CORROSION AT STR 5R. REPAIRED FRAME SECTOR AT FS 513.0 STR 5R IAW EA AWAC-CRJ253-01360
- [SDR A6WA2019102946965](https://openairdocs.org/sdr/A6WA2019102946965.md): Skin · dented · Oct 28, 2019 · N425AW · Cndair CL6002B19 · Spoilers
  > RT WING I/B GRND SPOILER HAS DENT ON BOTTOM SURFACE. REPAIRED RT WING I/B GRND SPOILER BOTTOM SURFACE IAW AWAC-CRJ257-01361 REV IR DATE 10/26/2019
- [SDR A6WA2019102946964](https://openairdocs.org/sdr/A6WA2019102946964.md): Skin · damaged · Oct 28, 2019 · N425AW · Cndair CL6002B19 · Spoilers
  > RT WING I/B GRND SPOILER HAS ROCK CHIP DAMAGE ON BOTTOM SURFACE. REPAIRED RT WING I/B GRND SPOILER BOTTOM SURFACE IAW AWAC-CRJ257-01361 REV IR DATE 10/26/2019
- [SDR A6WA2019102846961](https://openairdocs.org/sdr/A6WA2019102846961.md): Vane · chafed · Oct 26, 2019 · N425AW · Cndair CL6002B19 · Leading Edge Devices
  > LEFT I/B VANE L/E CHAFFED IN 3 PLACES. REMOVED AND REPLACED LEFT MIDDLE FLAP VANE L/E IAW CRJ-200 SRM 51-42-10. BLENDED LEFT I/B AND O/B TO SMOOTH CONTOUR. FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.
- [SDR A6WA2019102846956](https://openairdocs.org/sdr/A6WA2019102846956.md): Post · corroded · Oct 24, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBOARD POST AT FS 409+128 LBL 18 HAS CORROSION. REPLACED
- [SDR A6WA2019102846957](https://openairdocs.org/sdr/A6WA2019102846957.md): Stiffener · cracked · Oct 24, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LOWER 621 BULKHEAD STIFFENER AT LBL 36 CRACKED. REPLACED
- [SDR A6WA201910246941](https://openairdocs.org/sdr/A6WA201910246941.md): Angle · cracked · Oct 23, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 605 CLIP UNDERNEATH THE CARGO DOOR SILL AT STR 17L IS CRACKED. REMOVED AND INSTALLED NEW CLIP UNDER CARGO DOOR SILL AT STR 17L FS 605 IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2019102446951](https://openairdocs.org/sdr/A6WA2019102446951.md): Angle · cracked · Oct 23, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER AFT ANGLE 601R35050-109 FOR CARGO DOOR BEAM CRACKED. REMOVED AND REPLACED LOWER AFT ANGLE P/N 601R35050-109 IAW CRJ 200 SRM 53-61-23
- [SDR A6WA2019102346938](https://openairdocs.org/sdr/A6WA2019102346938.md): Bracket · cracked · Oct 22, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > F.S. 461 RBL 47 FAIRING BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06
- [SDR A6WA2019102346939](https://openairdocs.org/sdr/A6WA2019102346939.md): Bracket · cracked · Oct 20, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 469 RBL 47 FAIRING BRACKET IS CRACKED. REPLACED
- [SDR A6WA2019102346940](https://openairdocs.org/sdr/A6WA2019102346940.md): Bracket · cracked · Oct 20, 2019 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 449 LBL FAIRING BRACKET CRACKED. REPLACED
- [SDR A6WA2019102146933](https://openairdocs.org/sdr/A6WA2019102146933.md): Door Sill · cracked · Oct 20, 2019 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL AT FS 589 AT INBOARD RIVET IS CRACKED. REMOVED DAMAGED AREA IAW BOMB. REO 601R-53-61-433 REV C
- [SDR A6WA2019102146932](https://openairdocs.org/sdr/A6WA2019102146932.md): Retainer · cracked · Oct 20, 2019 · N425AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > PANEL 422DB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019041506557](https://openairdocs.org/sdr/A6WA2019041506557.md): Controller · malfunctioned · Apr 14, 2019 · N425AW · Cndair CL6002B19 · Cabin Pressure Controller
  > THE CREW ADVISED DISPATCH THAT THE AIRCRAFT WAS UNABLE TO PRESSURIZE AND WAS LEVELING OFF AT 10,000. CREW COMPLIED WITH QRH AND SWITCHED TO CONTROLLER 2 AND MANUAL MODE; NEITHER CORRECTED THE ISSUE. THE FLIGHT BURNED OFF FUEL AND RETURNED TO CAE. RTN-CABIN W/
- [SDR A6WA2019031846484](https://openairdocs.org/sdr/A6WA2019031846484.md): Warning System · activated · Mar 15, 2019 · N425AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > LT AND RT WING A-ICE CAUTION ON CLIMB OUT POWER AT T/O THRUST. C/W QRH MSG'S LEARED. WITH A-ICE IN STANDBY MODE. ON APROACH RECEIVED LT AND RT WING A-ICE CAUTION IN STANDBY MODE. WITH POWER GREATER THAN 85 PERCENT N2 UNABLE TO CLEAR MESSAGE BY INCREASING POWER

Next page: https://openairdocs.org/aircraft/N425AW/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 n_number = 'N425AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N425AW/reports

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