# Service difficulty reports: N464AW

A list on [N464AW](https://openairdocs.org/aircraft/N464AW.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 · 216 reports

- [SDR A6WA202609018913](https://openairdocs.org/sdr/A6WA202609018913.md): Fire Warning · activated · Sep 6, 2026 · N464AW · Cndair CL6002B19 · Detection System
  > LEFT FIRE WARNING AND THEN AFTER LANDING C/W IAC FOR LT ENGINE FIRE INDICATION DID NOT GO OUT AFTER 10 SECONDS PER IAC BOTH LT ENGINE BOTTLES DEPLOYED NO VISIBLE FIRE NOTED EMERGENCY WAS DECLARED. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202603208880](https://openairdocs.org/sdr/A6WA202603208880.md): Window · faulted · Mar 18, 2026 · N464AW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > LEFT WINDOW HEAT CAUTION MSG RAN QRH MSG CLEARED. AIRCRAFT REMOVED FROM SERVICE. ON LEFT WINDOW SWAPPED WIRES FROM S5 AND S6 BACK TO S1 AND S2. THIS CLEARS DIL REF 371644-2 IAW 30-41-06. REF 371644-2 SWAPPED S3, S4 TO S5, S6 ON LEFT HAND WINDOW REF AMM 30-
- [SDR A6WA202408278794](https://openairdocs.org/sdr/A6WA202408278794.md): Control Lever · faulted · Aug 23, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT 30 DEG WHEN SELECTING FLAPS DOWN. Ï¿½PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED FLAP CONTROL LEVER IAW AMM SUPPLEMENT
- [SDR A6WA202408018786](https://openairdocs.org/sdr/A6WA202408018786.md): Shutoff Valve · faulted · Aug 1, 2024 · N464AW · Cndair CL6002B19 · Cabin Cooling System
  > CLIMBING THROUGH 20000 FEET REV'D RT PACK OFF STATUS MESSAGE. LH PACK ON MEL. RT 10TH STAGE BLEED AIR VALVE INDICATE CLOSED IN COMMANDED OPEN POSITION. C/W QRH FOR UNPRESSURIZED FLIGHT. MESSAGE DID NOT CLEAR. DIVERTED TO MCI. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202407288783](https://openairdocs.org/sdr/A6WA202407288783.md): Warning Message · false activation · Jul 28, 2024 · N464AW · Cndair CL6002B19 · Cabin Cooling System
  > 6170 - LEAVING TVC ON CLIMB OUT RH PACK HI PRESS CAUTION CAME ON REMAINED 2 SECONDS CREW DESCENDED 10K FT CW QRH RH PACK OPERATES NORMALLY. AIRCRAFT REMOVED FROM SERVICE. C/W INSPECTION OF RH PACK. FOUND TEMP HI PRESS CHECK IAW AMM 21-50-00. OPS CHECK GOOD AT
- [SDR A6WA202407148778](https://openairdocs.org/sdr/A6WA202407148778.md): Proximity Sensor · false indication · Jul 14, 2024 · N464AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MSG IN FLIGHT WITH LDG LEVER IN UP POS. MSG INTERMITTENT. GEAR INDICATION ON ED1 WAS LH, RH MAIN GEAR UP AND NOSE GEAR DOWN. C/W QRH MSG REMAINED CLEAR. AIRSPEED WAS 250 KTS WHILE ON APPROACH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED
- [SDR A6WA202407098775](https://openairdocs.org/sdr/A6WA202407098775.md): Sensor · faulted · Jul 9, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > 6172 - DESCENT IN CRUISE LEAVING FL260 FOR FL 240 RCVD FLAP FAIL CAUTION. FLAP LEVER NEVER TOUCHED. BTMS 6,7,7,6. DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. R&R RT BPSU IAM AMM 27-51-10-000-801 OPS CK GOOD
- [SDR A6WA202406288770](https://openairdocs.org/sdr/A6WA202406288770.md): Panel · cracked · Jun 28, 2024 · N464AW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING TE PANEL AT WS 137.60 $ WS148.019 A SMALL CRACK WAS NOTED EMINATING FROM RIVET HOLE FROM A RIVET HOLE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW MHI REO 601R-57-21-3847 REV (--)
- [SDR A6WA202406038760](https://openairdocs.org/sdr/A6WA202406038760.md): Flap System · faulted · Jun 3, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION IN CRUISE FAIL. FLAPS FAILED AT ZERO. RAN QRH PROCEDURE FOR FLAPS ZERO LANDING. NORMAL LANDING. AIRCRAFT REMOVED FROM SERVICE. IN WORK. PERFORMED RIGGING OF BPSU'S IAW AMM 27-51-10. FLAPS OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND
- [SDR A6WA202406018756](https://openairdocs.org/sdr/A6WA202406018756.md): Sensor · faulted · Jun 1, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL 6 DEG ON APPROACH ***** AIRCRAFT REMOVED FROM SERVICE ***** C/W FIM RESET PLACED ON MEL. R&R RH BPSU IAW AMM 27-51-10 AND SUPP 04-048B. OPS TEST GOOD. REMOVED PLACARD AND REMOVED FROM MEL.
- [SDR A6WA202403158725](https://openairdocs.org/sdr/A6WA202403158725.md): Unknown · odor · Mar 15, 2024 · N464AW · Cndair CL6002B19 · Air Distribution System
  > SMELL SIMILAR TO HOT METAL DETECTED IN FLIGHT DECK FOR ABOUT 10 SECS ROUGHLY 15 MIN APPLYING AC ELECTRICAL PWR TO AC REQ INSP. NO BREAKERS FOUND OPEN. APU WAS NOT OPERATING. NO SMOKE OR HAZE NOTED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED COCKPIT AND AVI
- [SDR A6WA202401148696](https://openairdocs.org/sdr/A6WA202401148696.md): Unknown · unknown · Jan 14, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILED WHEN FLAPS SELECTED TO 20 DEGREE ON APPROACH. AIRCRAFT REMOVED FROM SERVICE REF 364863/1 FOR CORRECTIVE ACTION OPS CK GOOD IAW AMM 27-54-00 TROUBLESHOT FLAP FAIL PER FIM 27-50-00. REFERENCE FIM 27-50-00 FIG 103 BLK 21. OPS CK GOOD. REMOVED PL
- [SDR A6WA202401138695](https://openairdocs.org/sdr/A6WA202401138695.md): Unknown · unknown · Jan 13, 2024 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > 364863-1 FLAPS FAILED AT 0 DEGREES ON APPROACH WHEN SELECTING FLAPS 8. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT FLAP FAIL PER FIM 27-50-00. REFERENCE FIM 27-50-00 FIG 103 BLK 21. OPS CK GOOD. REMOVED PLACARD AND REMOVED FROM MEL
- [SDR A6WA202307028635](https://openairdocs.org/sdr/A6WA202307028635.md): Position Sensor · unknown · Jul 2, 2023 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER TAKEOFF FLAPS SELECTED ZERO AND SHORTLY THERAFTER RCVD FLAP FAIL CAU MSG. AIRCRAFT REMOVED FROM SERVICE. R&R OF BPSU ON RIGHT WING. OPS CHECK GOOD.
- [SDR A6WA202306308633](https://openairdocs.org/sdr/A6WA202306308633.md): Control Unit · unknown · Jun 30, 2023 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION CLIMBING THROUGH 20,000FT. FLAPS INDICATE 0 DEGREES. AIRCRAFT REMOVED FROM SERVICE. R & R FECU IAW AMM 27-51-05 OPS CHECK GOOD AT THIS TIME.
- [SDR A6WA202304088543](https://openairdocs.org/sdr/A6WA202304088543.md): Bulkhead Web · damaged · Apr 8, 2023 · N464AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > "Ï¿½REAR PRESSURE BULKHEAD FRAME STATION 621 DRILL START REVEALED AFTER REMOVAL OF FIRE BARRIER TOP FASTENER OTBD SIDE, FLAGGED. ***** AC REMOVED FROM SERVICE ***** REAR PRESSURE BULKHEAD STA. 621 REPAIRED IAW CRJ 200 REO 601R-61-7982 REV.-- DATED ON 31/ MAR/
- [SDR A6WA202304048532](https://openairdocs.org/sdr/A6WA202304048532.md): Beam · cracked · Apr 4, 2023 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > BEAM 601R31119-60 CRACKED AT TOP AFT OUTBOARD CORNER LOCATED AT LBL9.00 BETWEEN FS559.00+16 AND FS559.00+32 *******AIRCRAFT REMOVED FROM SERVICE******* FABRICATED NEW BEAM AT LBL9.00 FS559.00+16 TO FS559.00+32 IAW DRAWING 601R31119 REV H. REMOVED AND REPLACED
- [SDR A6WA202303228523](https://openairdocs.org/sdr/A6WA202303228523.md): Floor Support · corroded · Mar 22, 2023 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT FUSELAGE INTERIOR, FLOORBOARD SUPPORT STRUCTURE CORRODED, 8" LEFT OF CTR LINE, 3" FWD OF FS 559+16 *********AIRCRAFT REMOVED FROM SERVICE************** REMOVED AND INSTALLED NEW FLOOR SUPPORT T. CAP FROM FS 559 TO 559+112 LBL 9.00 IAW CRJ 200 SRSM 51-40-1
- [SDR A6WA202303178520](https://openairdocs.org/sdr/A6WA202303178520.md): Seat Track · corroded · Mar 17, 2023 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT FUSELAGE INTERIOR, FLOORBOARD SUPPORT STRUCTURE CORRODED FROM FS574 TO FS609 @ LBL27. REMOVED AND REPLACED FLOARBOARD SUPPORT STRUCTURE IAW EA# 105-2023-024 *******AIRCRAFT REMOVED FROM SERVICE*********** REMOVED AND REPLACED FLOARBOARD SUPPORT STRUCTURE I
- [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 A6WA202101118066](https://openairdocs.org/sdr/A6WA202101118066.md): Computer · faulted · Jan 10, 2022 · N464AW · Cndair CL6002B19 · Central Warning
  > RECEIVED STALL CAUTION MESSAGE AFTER TAKEOFF CW QRH MESSAGE REMAINED, NO OTHER ASSOCIATED MESSAGES. FLAPS AND EICAS MATCHES FLAP POSITION COMMANDED AND GEARS COMMANDED UP IN TRANSITION. AIRCRAFT REMOVED FROM SERVICE. R & R STALL WARING COMPUTER IAW AMM 27
- [SDR A6WA202109277888](https://openairdocs.org/sdr/A6WA202109277888.md): Floorbeam · corroded · Sep 14, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION DAMAGE AT AFT CABIN FLOOR SUPPORT AT FS559+59.5 AND RBL 9. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED FLOOR BEAM FLANGE REPAIR NO. 1 PER SRM 53-00-43 REV 38. P1 DAMAGE DIMENSION L= 1.900Ï¿½ X W= 0.700Ï¿½. CUT OUT DIMENSION L= 1.70Ï¿½ X W= 0.900Ï
- [SDR A6WA202109177882](https://openairdocs.org/sdr/A6WA202109177882.md): Skin · dented · Sep 11, 2021 · N464AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON AFT FUSELAGE SKIN FS640.00 TO FS644.5 AND S21R TO S22R. ***AIRCRAFT REMOVED FROM SERVICE*** DENT EVALUATED AND FOUND TO BE STRUCTURALLY ACCEPTABLE PER EA. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS P
- [SDR A6WA202110157900](https://openairdocs.org/sdr/A6WA202110157900.md): None · cracked · Sep 10, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD FS621 HAS INDICATION OF A CRACK AT BL 0.0 AND WL 125. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED INTERIM REPAIR TO AFT PRESSURE BULKHEAD FS621 AT BL 0.0 AND WL 125 TO WL134. PERFORMED DOUBLER REPAIR TO THE AFT PRESSURE BULKHEAD FS621.
- [SDR A6WA202109277889](https://openairdocs.org/sdr/A6WA202109277889.md): Doubler · dented · Sep 10, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS682.00 TO FS700.00 AND S22R TO S23R FOUND NEXT TO AN AN EXISTING DOUBLER REPAIR WITH A DISTANCE OF 1.70Ï¿½ AWAY. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN BY REMOVING EXISTING DOUB
- [SDR A6WA202109277887](https://openairdocs.org/sdr/A6WA202109277887.md): Skin · dented · Sep 10, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT WITH CREASE ON AFT FUSELAGE SKIN AT FS625.00-FS640.0 AND S25R TO S26R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN AT FS625.00-FS640.0 AND S25R TO S26R. DENT DIMENSION L = 1.100Ï¿½ X W = 0.600Ï¿½ X D = 0.013Ï¿½
- [SDR A6WA202109227885](https://openairdocs.org/sdr/A6WA202109227885.md): Skin · dented · Sep 10, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT FUSELAGE SKIN HAS TWO DENTS AT FS625.30 TO FS640.0 AND S20L TO S21L, DENTS ARE APPROXIMATELY 1 INCH APART. ***AIRCRAFT REMOVED FROM SERVICE*** THE TWO DENTS EVALUATED AND FOUND TO BE STRUCTURALLY ACCEPTABLE PER EA. P/N 601R35005. PERFORMED HFEC WITH NO I
- [SDR A6WA202109277890](https://openairdocs.org/sdr/A6WA202109277890.md): Skin · dented · Sep 7, 2021 · N464AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT LOWER FUSELAGE SKIN DENT BELOW CARGO DOOR LOWER AFT CORNER FS621.00 AND S19L. ***AIRCRAFT REMOVED SERVICE*** PERFORMED A HAND DRESS TO FUSELAGE SKIN DENT BELOW CARGO DOOR LOWER AFT CORNER FS621.00 AND S19L. DENT DIMENSIONS PRIOR TO REWORK L=
- [SDR A6WA202103197717](https://openairdocs.org/sdr/A6WA202103197717.md): Anti-Ice Valve · failed · Mar 17, 2021 · N464AW · Cndair CL6002B19 · Engine Anti-Icing System
  > RECEIVED LH ENG COWL A-ICE CAUTION MESSAGE IN FLIGHT WITH SYSTEM OFF. RAN QRH, MESSAGE CLEARED AFTER CLOSING LH 14TH STAGE SOV. LH PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN ON THE GROUND. ***AIRCRAFT REMOVED FROM SERVICE*** R&R LH ENG COWL ANTI-ICE VALVE IA
- [SDR A6WA202010127319](https://openairdocs.org/sdr/A6WA202010127319.md): Controller · malfunctioned · Oct 9, 2020 · N464AW · Cndair CL6002B19 · Cabin Pressure Controller
  > DURING CLIMB FROM FL 280 WE HEARD A SOUND, SO WE CHECKED CABIN ALT, THAT WAS NORMAL. THE NOISE WAS GETTING LOUDER AND CABIN ALT SLOWLY INCREASED. AFTER DESCENDING THROUGH FL 250 RECEIVED CABIN ALT CAUTION FOLLOWED BY WARNING MESSAGE. CABIN O2 MASKS AUTO DEP
- [SDR A6WA202009187288](https://openairdocs.org/sdr/A6WA202009187288.md): Antenna · failed · Sep 17, 2020 · N464AW · Cndair CL6002B19 · Weather Radar System
  > "RADAR FAULT" MESSAGE ON MFD, RADAR MOSTLY INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED WEATHER RADAR ANTENNA, PER AMM 34-41-01. OPS CHECK GOOD, PN 622-9302-003 S/N OFF 1WWH, S/N ON 3893 - LN.
- [SDR A6WA2020070867264](https://openairdocs.org/sdr/A6WA2020070867264.md): Actuator · malfunctioned · Jul 6, 2020 · N464AW · Cndair CL6002B19 · Landing Gear Actuator
  > UPON LDG EXTENSION, RECEIVED RT MLG INDICATION NOT DOWN WITH A GEAR DISAGREE AURAL WARNING. FOLLOWED QRH PROCEDURE, GEAR SHOWED DOWN AND LOCK AFTER 1 CYCLE OF THE GEAR LEVER. NO OTHER EICAS MESSAGES PRESENT, NO ABNORMAL HYD INDICATIONS NOTED. MANUAL RELEASE
- [SDR A6WA2020020547150](https://openairdocs.org/sdr/A6WA2020020547150.md): Transmitter · malfunctioned · Feb 3, 2020 · N464AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON APPROACH WHEN SELECTING FLAPS TO LANDING CONFIGURATION (45 DEGREES) THE INDICATION STOPPED AT 42 DEGREES. THE CAPTAIN EXECUTED A GO A ROUND DUE TO THIS. AIRCRAFT REMOVED FROM SERVICE. C/W "M" ACTION TO DEACTIVATE LH FPTU IAW AMM 27-54-00-040-801.
- [SDR A6WA2020013147139](https://openairdocs.org/sdr/A6WA2020013147139.md): Flap System · malfunctioned · Jan 30, 2020 · N464AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > INFLIGHT WHEN FLAPS WERE SELECTED TO 45 DEGREES, EICAS PAGE SHOWS FLAPS AT 42 DEGREES ON BOTH WINGS. NO CAUTION MESSGES. EXECUTED GO-AROUND, FLAPS RETRACTED NORMALLY, UPON EXTENSION BOTH FLAPS SHOW 42 DEGREES. AIRCRAFT REMOVED FROM SERVICE COMPLIED WITH FEC
- [SDR A6WA2019100846909](https://openairdocs.org/sdr/A6WA2019100846909.md): Frame · corroded · Oct 8, 2019 · N464AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605 FRAME BETWEEN STR 25R AND STR 25L HAS HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFOREMENT ANGLE IAW SRM 51-42-06 AND 51-42-21
- [SDR A6WA2019100846908](https://openairdocs.org/sdr/A6WA2019100846908.md): Frame · corroded · Oct 8, 2019 · N464AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605 FRAME BETWEEN STR 25R AND STR 25L HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFORCEMENT ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21
- [SDR A6WA2019100846910](https://openairdocs.org/sdr/A6WA2019100846910.md): Frame · corroded · Oct 8, 2019 · N464AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605 FRAME BETWEEN STR 17R AND STR 18R HAS CORROSION REPAIR FRAME SECTION IAW REO 601R-53-61-7149
- [SDR A6WA2019100246899](https://openairdocs.org/sdr/A6WA2019100246899.md): Frame · corroded · Oct 1, 2019 · N464AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 589 FRAME BETWEEN STR 25R AND 25L AND BETWEEN STR 22R AND 21R HAS CORROSION. REPLACED
- [SDR A6WA2019100246900](https://openairdocs.org/sdr/A6WA2019100246900.md): Angle · corroded · Oct 1, 2019 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE LOCATED AT FS 589 BETWEEN STRINGERS 22R AND 24R CORRODED. REPLACED
- [SDR A6WA2019100146898](https://openairdocs.org/sdr/A6WA2019100146898.md): Vane · chafed · Sep 30, 2019 · N464AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH WING I/B FLAP VANE LEADING EDGE IS CHAFED AT I/B SECTION REMOVED AND REPLACED RH WING IB FLAP VANE LEADING EDGE SKIN IB SECTION IAW CRJ 200 SRM 51-42-13
- [SDR A6WA2019100246901](https://openairdocs.org/sdr/A6WA2019100246901.md): Skin · chafed · Sep 29, 2019 · N464AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH WING INBD FLAP VANE LEADING EDGE IS CHAFFED AT CENTER SECTION. REPLACED
- [SDR A6WA2019100146896](https://openairdocs.org/sdr/A6WA2019100146896.md): Beam · gouged · Sep 29, 2019 · N464AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM MEMBER HAS DEEP CUTS FWD AND AFT FROM THE CARGO DOOR PULLEYS REMOVED AND REPLACED CARGO DOOR BEAM MEMBER IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019100146897](https://openairdocs.org/sdr/A6WA2019100146897.md): Bracket · cracked · Sep 29, 2019 · N464AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKED LOWER ANGLE BRACKET ON 621 BULKHEAD REMOVED AND REPLACED LOWER ANGLE BRACKET IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2019100146892](https://openairdocs.org/sdr/A6WA2019100146892.md): Floor Support · corroded · Sep 28, 2019 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM CAP CORRODED IN AFT CARGO AREA, LBL 27 FS 559+80TI FS621.00. REPLACED BEAM CAP IAW REO 601R-53-00-027 REV-D.
- [SDR A6WA2019100146894](https://openairdocs.org/sdr/A6WA2019100146894.md): Stiffener · cracked · Sep 28, 2019 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 BULKHEAD RBL 18 O/B POST IS CRACKED AT THE BOTTOM GOING APPROXIMATELY.200" PASSED THE BOTTOM RIVET REPAIR FS 409+128 BULKHEAD RBL 18 O/B POST IAW BOMBARDIER REO 601R-53-41-889 REV D.
- [SDR A6WA2019100146893](https://openairdocs.org/sdr/A6WA2019100146893.md): Floor Support · corroded · Sep 28, 2019 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM CAP CORRODED AT RBL27, FS 559+80 TO 559+100. REPLACED BEAM CAP IAW REO 601R-53-00-027 REV-D,
- [SDR A6WA2019100146895](https://openairdocs.org/sdr/A6WA2019100146895.md): Cargo Track · corroded · Sep 28, 2019 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT FS 559+78 TO FS 559+95 ON RBL 27 HAS CORROSION REMOVED AND REPLACED CARGO TRACK AT FS 559+78 TO FS 559+95 ON RBL27 IAW CRJ 200 AMM 53-00-49
- [SDR A6WA2019100146891](https://openairdocs.org/sdr/A6WA2019100146891.md): Seat Track · corroded · Sep 27, 2019 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK NR 3 CORRODED. REPLACED SEAT TRACK IAW 19-254A.
- [SDR A6WA2019100146889](https://openairdocs.org/sdr/A6WA2019100146889.md): Seat Track · corroded · Sep 26, 2019 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK NR 2 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2019100146888](https://openairdocs.org/sdr/A6WA2019100146888.md): Seat Track · corroded · Sep 26, 2019 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK NR 4 CORRODED. REPLACED RIGHT FLOOR SEAT TRACK NR 4 IAW AMM 53-01-11.

Next page: https://openairdocs.org/aircraft/N464AW/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 = 'N464AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N464AW/reports

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