# Service difficulty reports: N434AW

A list on [N434AW](https://openairdocs.org/aircraft/N434AW.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 6 · 281 reports

- [SDR A6WA202408158792](https://openairdocs.org/sdr/A6WA202408158792.md): Outflow Valve · failed · Aug 15, 2024 · N434AW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > DURING CLIMB NOTICED CABIN ALTITUDE CLIMBING ABNORMALLY HIGH. RECEIVED CABIN ALT CAUTION MSG. FOLLOWED BY CABIN ALT WARNING. CW IAC AND QRH CMSGS CLEARED IN DECENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND OVB EXHAUST SOV NOT FULLY CLOSED. SET TO
- [SDR A6WA202407278782](https://openairdocs.org/sdr/A6WA202407278782.md): Panel · open · Jul 27, 2024 · N434AW · Cndair CL6002B19 · Accessory Compartment Doors
  > AFTER TAKEOFF FROM KCMH & GEAR WERE RETRACTED, CREW HEARD AN UNUSUAL NOISE. NO CAUTION OR WARNING MESSAGE NOTED BY CREW. VOLUME OF NOISE INCREASED ABOVE 250 KNOTS. CREW CONTACTED ATC TO MAKE AWARE OF SITUATION & DECLARED AN EMERGENCY. FLIGHT ATTENDANT & PAX BR
- [SDR A6WA202402068716](https://openairdocs.org/sdr/A6WA202402068716.md): Skin · dented · Feb 6, 2024 · N434AW · Cndair CL6002B19 · Wing, Plate/Skin
  > CREW REPORTED DENT LOCATED ON UPPER LH WINGSKIN DURING WALKAROUND. WORKING WITH MHI, DENT WAS FOUND TO BE A PREVIOUS BLEND REPAIR WITH UNDERLYING FREEZE PLUG IN THE FWD AND MID WING PLANKS. MHI OR AWA COULD NOT FIND ANY DOCUMENTATION FOR THIS REPAIR. MHI IS
- [SDR A6WA202303288640](https://openairdocs.org/sdr/A6WA202303288640.md): Spar · damaged · Mar 28, 2023 · N434AW · Cndair CL6002B19 · Wing Spar
  > FOUND DRILL START DAMAGE ON RH WINGLET REAR SPAR P/N: 600-15104-6 ON THE IB SIDE OF THE REAR SPAR CHANNEL BETWEEN WGLT STA 6.36 - 12.50 MEASURING 0.180"L X 0.180"W X 0.026"D. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DRILL START DAMAGE TO A SMOOTH CONTOUR
- [SDR A6WA202303288639](https://openairdocs.org/sdr/A6WA202303288639.md): Skin · dented · Mar 28, 2023 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND 3 DENTS ON FUSELAGE SKIN AROUND PASSENGER DOOR CUTOUT, FS 310, STR 14L - 15L = 1.2"L X.400"W X.315"D; FS 349 AT STR 14L = 2.8"L X.350"W X.162"D; AND FS 349, STR 15L - 16L = 0.9"L X 0.320"W X 0.145"D. AIRCRAFT REMOVED FROM SERVICE. PERFORMED TRIM O
- [SDR A6WA202205208501](https://openairdocs.org/sdr/A6WA202205208501.md): Skin · none · May 20, 2022 · N434AW · Cndair CL6002B19 · Wing Structure
  > LEFT-WING LEADING-EDGE SKIN P/N 601R12074-3 SHOWS EROSION/ROUGHNESS OF 0.005" MULTIPLE SPOTS. ******AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED LEADING EDGE SKIN P/N 601R12074-3.
- [SDR A6WA202205108510](https://openairdocs.org/sdr/A6WA202205108510.md): Unknown · unknown · May 10, 2022 · N434AW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > RIGHT-WING LEADING-EDGE SHOWS SIGNS OF ROUGHNESS ********AIRCRAFT REMOVED FROM SERVICE********* RE-SKIN OTB SECTION OF RH WING OUTB LEADING EDGE AND INSTALLED 1 EA RIB AND 1 EA STRAP
- [SDR A6WA202205098502](https://openairdocs.org/sdr/A6WA202205098502.md): Skin · none · May 9, 2022 · N434AW · Cndair CL6002B19 · Wing Structure
  > LH OUTBOARD LEADING EDGE SKIN P/N 601R12074-3 FOUND ERODED BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** REMOVED AND REPLACED SKIN P/N 601R12074-3.
- [SDR A6WA202204118483](https://openairdocs.org/sdr/A6WA202204118483.md): Angle · cracked · Apr 11, 2022 · N434AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FLOOR SUPPORT ANGLE ALONG FS621 BULKHEAD OUTBOARD OF FLOOR BEAM LBL27 IS CRACKED (MARKED) *****AIRCRAFT REMOVED FROM SERVICE***** R&R -1 ANGLE, (EXISTING REPAIR), REF BOMBARDIER REO 601R-53-61-117 REV-D DATED 2017-02-26 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51
- [SDR A6WA202204088484](https://openairdocs.org/sdr/A6WA202204088484.md): None · none · Apr 8, 2022 · N434AW · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT RH OTBD FLAP UPPER SKIN *****AIRCRAFT REMOVED FROM SERVICE**** REPAIRED
- [SDR A6WA202202218117](https://openairdocs.org/sdr/A6WA202202218117.md): None · none · Feb 19, 2022 · N434AW · Cndair CL6002B19 · Engine Exhaust System
  > UPON FIRST WALK AROUND FO FOUND LH STANG FAIRING MISSING. R&R LH ENG STANG FAIRING IAW AMM 78-34
- [SDR A6WA202106157803](https://openairdocs.org/sdr/A6WA202106157803.md): Transceiver · faulted · Jun 11, 2021 · N434AW · Cndair CL6002B19 · Weather Radar System
  > WEATHER RDR TURNED ITSELF OFF AND WOULD NOT TURN BACK ON. AIRCRAFT REMOVED FROM SERVICE. R&R WEATHER RADAR RECIEVER/TRANSMITTER ASSY IAW AMM 34-41-01. OPS TEST GOOD. SN REMOVED: 1C6WV SN INSTALLED: 58VU
- [SDR A6WA202104127737](https://openairdocs.org/sdr/A6WA202104127737.md): Pseu · fault message · Apr 10, 2021 · N434AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > PROX SYS CHAN CAUTION MSG IN FLIGHT. QRH C/W. MANUALLY EXTENDED LANDING GEAR. INSTALLED GEAR PINS. ***AIRCRAFT REMOVED FROM SERVICE*** INTERROGATED PSEU, FOUND CODES A01-A06 AND RED FAIL LIGHT ILLUMINATED. R&R PSEU IAW AMM 32-61-01. OPS CHECK GOOD. GE
- [SDR A6WA202104067735](https://openairdocs.org/sdr/A6WA202104067735.md): Floorbeam · damaged · Mar 13, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > TOOL MARK COMMON TO FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED TOOL MARK ON FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 WITH BLEND DIMENSIONS OF 0.600Ï¿½L X 0.500Ï¿½W X 0.027Ï¿½D WITH A REMAINING THICKNESS OR 0.0
- [SDR A6WA202103247726](https://openairdocs.org/sdr/A6WA202103247726.md): Seat Track · corroded · Mar 13, 2021 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AND GOUGES WITH CORROSION COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL 9. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SEAT TRACK COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL
- [SDR A6WA202103227720](https://openairdocs.org/sdr/A6WA202103227720.md): Beam · damaged · Mar 13, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LIGHTNING HOLE HAS TORN AREAS X2 AT TOP OF HOLE FS 409.00+69+11.5" TO FS409.00+96+13 RBL 8 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 DAMAGED AREAS ON LIGHTNING HOLES AT FS 409.00+69+11.5 TO 409.00+69+13 RBL 8 FOUND WITHIN LIMITS REF ASAP EA# AWAC-CRJ25
- [SDR A6WA202103267730](https://openairdocs.org/sdr/A6WA202103267730.md): Skin · damaged · Mar 12, 2021 · N434AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650BB HAS CRACK INDICATION AT AFT INBOARD ARC APPROX. WS180.00, INDICATION MEASURES APPROX. 0.10. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WING LOWER PLANK ACCESS PAN
- [SDR A6WA202103267731](https://openairdocs.org/sdr/A6WA202103267731.md): Skin · damaged · Mar 12, 2021 · N434AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650AB HAS CRACK INDICATION AT OUTBOARD ARC APPROX. WS173.00, INDICATION MEASURES APPROX. 0.10. (INITIATES AWAC EO6/021/457) ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WI
- [SDR A6WA202103247725](https://openairdocs.org/sdr/A6WA202103247725.md): Door Frame · cracked · Mar 11, 2021 · N434AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AFT ***AIRCRAFT REMOVED FROM SERVICE*** PAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AF
- [SDR A6WA202103227721](https://openairdocs.org/sdr/A6WA202103227721.md): Fairing · gouged · Mar 11, 2021 · N434AW · Cndair CL6002B19 · Vertical Stabilizer
  > STAB FAIRING 326CR GOUGED FROM STAB MOVEMENT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON VERTICAL STABILIZER FAIRING PANEL 326CR. FOUND WITHIN LIMITS REF EA# AWAC-CRJ255-01588 REV A DATED 3/19/2021
- [SDR A6WA202103197719](https://openairdocs.org/sdr/A6WA202103197719.md): Bulkhead Web · damaged · Mar 11, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE HAS SCRATCHES COMMON TO FORWARD SIDE OF 621.00 BULKHEAD LBL 18 AT TOP OF BULKHEAD AROUND CANNON PLUGS. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED THREE BLENDED AREAS ON REAR PRESSURE BULKHEAD DOUBLER FORWARD FACE OF UPP
- [SDR A6WA202103197718](https://openairdocs.org/sdr/A6WA202103197718.md): Skin · dented · Mar 10, 2021 · N434AW · Cndair CL6002B19 · Trailing Edge Flaps
  > INWARD DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROXIMATELY WING STATION 106.40. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROX. WING STATION 106.40
- [SDR A6WA202103157713](https://openairdocs.org/sdr/A6WA202103157713.md): Skin · dented · Mar 10, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3.75, STR 23L+4.25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 265.00+3.75, SR 23L+4.25 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED, REF ASAP EA# AWAC-CRJ-253-0158
- [SDR A6WA202103157714](https://openairdocs.org/sdr/A6WA202103157714.md): Skin · dented · Mar 10, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INWARD DENT COMMON TO EXTERIOR SKIN AT FS 235.00-13, STRINGER 24L+4 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 235.00+13, STR 24L+4 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# CRJ253-01586 REV IR DT
- [SDR A6WA202103157716](https://openairdocs.org/sdr/A6WA202103157716.md): Skin · dented · Mar 10, 2021 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3, STR 23L+1 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED INWARD DENT AT FS 265.00+3 STR 23L+1 TO ORIGINAL CONTOUR. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# AWAC - CRJ253-01585 REV
- [SDR A6WA202010257348](https://openairdocs.org/sdr/A6WA202010257348.md): Bpsu · failed · Oct 25, 2020 · N434AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > WHILE AT CRUISE FL300, FLAP FAIL CAUTION MESSAGE APPEARED WITH NO INPUT ON FLAP HANDLE. RAN QRH. TOUCHDOWN BELOW MAX LANDING WEIGHT. BRAKE TEMP MAX WERE 5 RT OUTBOARD BRAKE. FLAP FAIL REMAINED DISPLAYED ON TAXI TO GATE. PERFORMED FLAP RESET PROCEDURE, IA
- [SDR A6WA2020041347257](https://openairdocs.org/sdr/A6WA2020041347257.md): Circuit Breaker · shorted · Apr 10, 2020 · N434AW · Cndair CL6002B19 · Electrical Power System
  > ON TAKE-OFF ROLL, PRIOR TO ROTATION, WE SAW AND HEARD ELECTRICAL FLASHES BEHIND CAPTAIN AND SCREENS FLICKERED, ALSO SMELLED ELECTRICAL SMOKE BRIEFLY. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND RAZOR BLADE MAKING CONTACT WITH CBP1-A2 AND A5 (FOR
- [SDR A6WA202002147182](https://openairdocs.org/sdr/A6WA202002147182.md): Floor Support · corroded · Feb 14, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IN AFT CARGO HAS SPOTS OF CORROSION, FS559.00+80 TO FS559.00+112. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL -.063 MATERIAL LOSS -.063 REMAINING THICKNESS -.000 ALLOWABLE LIMITS -.015 REMOVED AND REPLACED F
- [SDR A6WA2020021347174](https://openairdocs.org/sdr/A6WA2020021347174.md): Floor Support · corroded · Feb 13, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM FS409.00+128 TO FS559.00, RBL 9 AIRCRAFT REMOVED FROM SERVICE ORIGINAL MATERIAL.063 MATERIAL REMOVED.026 REMAINING MATERIAL.037 ALLOWABLE LOSS.005 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-01439
- [SDR A6WA2020021347170](https://openairdocs.org/sdr/A6WA2020021347170.md): Bulkhead Web · cracked · Feb 12, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0, WL 111.00. AIRCRAFT REMOVED FROM SERVICE WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING BOMBAR
- [SDR A6WA2020021347172](https://openairdocs.org/sdr/A6WA2020021347172.md): Frame · corroded · Feb 12, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGERS 25R AND 26L. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS.050 MATERIAL LOSS.012 REMAINING MATERIAL.038 ALLOWABLE LOSS.005 REMOVED AND REPLACED FRAME
- [SDR A6WA2020021247167](https://openairdocs.org/sdr/A6WA2020021247167.md): Floor Support · corroded · Feb 12, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM 409+128-559.00, INBD SIDE OF BEAM. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS.063 MATERIAL LOSS.026 REMAINING MATERIAL.037 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-0
- [SDR A6WA2020021247168](https://openairdocs.org/sdr/A6WA2020021247168.md): Strap · corroded · Feb 12, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT STRAP IS CORRODED AT FS559.00+112, RBL27-RBL45. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL.100 MATERIAL LOSS.013 REMAINING MATERIAL.087 ALLOWABLE LOSS.010 REMOVED AND REPLACED STRAP IAW CRJ200 SRM 51-42-06
- [SDR A6WA2020021247162](https://openairdocs.org/sdr/A6WA2020021247162.md): Floor Support · corroded · Feb 11, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED FROM FS574.00 TO FS621.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION IAW CRJ200 SRM 53-61-43 & 51-31-59. ORIGINAL THICKNESS.050 ALLOWABLE LOSS.020 ACTUAL MATERIAL LOSS.050 REMAINING THICKNESS.000 REMOVED
- [SDR A6WA2020021147161](https://openairdocs.org/sdr/A6WA2020021147161.md): Floor Support · corroded · Feb 11, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED AT FS584.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE REMOVED CORROSION IAW AWAC SUPPLEMENT 19-206. ORIGINAL THICKNESS.050 MATERIAL LOST.029 ALLOWABLE LOSS LIMITS.013 REMAINING THICKNESS.021 REMOVED AND REPLACED FLOOR BEAM IAW BOMB
- [SDR A6WA2020021147159](https://openairdocs.org/sdr/A6WA2020021147159.md): Spar · damaged · Feb 9, 2020 · N434AW · Cndair CL6002B19 · Wing Spar
  > L/H WING FRONT SPAR HAS DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H WING FRONT SPAR DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE IAW BOMB. REO 601R57-00-116.
- [SDR A6WA2020021147158](https://openairdocs.org/sdr/A6WA2020021147158.md): Floor Support · corroded · Feb 8, 2020 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CORRODED AT FS621.00 TO FS574, LBL 9. AIRCRAFT REMOVED FROM SERVICE REPAIRED FLOOR SUPPORT IAW AWAC SUPPLEMENT 20-024.
- [SDR A6WA2020021147157](https://openairdocs.org/sdr/A6WA2020021147157.md): Angle · cracked · Feb 8, 2020 · N434AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RIB ON LH PYLON LOWER FLANGE CRACKED FS605. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED IAW AWAC SUPPLEMENT 14-252A.
- [SDR A6WA20200207156](https://openairdocs.org/sdr/A6WA20200207156.md): Strap · corroded · Feb 7, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR STRAP AT FS559.00, RBL 45 TO RBL 27, IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLOOR STRAP IAW CRJ200 SRM 51-42-06 AND TR 51-42.
- [SDR A6WA20200207155](https://openairdocs.org/sdr/A6WA20200207155.md): Access Panel · cracked · Feb 6, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PANEL 630BL HAS CHAFFING ON INNER SURFACE. CRACK INDICATIONS NOTED DURING HFEC INSPECTION OF REPAIRED SURFACE. AIRCRAFT REMOVED FROM SERVICE REPAIRED PANEL 630BL IAW AWAC SUPPLEMENT 19-218A.
- [SDR A6WA2020020547152](https://openairdocs.org/sdr/A6WA2020020547152.md): Bracket · corroded · Feb 4, 2020 · N434AW · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING TRANSITION PICOLLO TUBE BRACKET BETWEEN INBOARD AND CENTER LEADING EDGES IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED PICOLLO TUBE TRANSITION TUBE BRACKET IAW CRJ200 SRM 51-42-06 % 51-41-06.
- [SDR A6WA202002057151](https://openairdocs.org/sdr/A6WA202002057151.md): Seat Track · corroded · Feb 4, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK BETWEEN FS449.85 & FS499.00 HAS CORROSION AND GOUGED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.
- [SDR A6WA202020347146](https://openairdocs.org/sdr/A6WA202020347146.md): Frame · corroded · Feb 1, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 310 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGER 24L AND 24R, IN THE FWD E&E BAY. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FRAME SEGMENT IAW CRJ200 SRM 51-42-06 AND 51-42-21.
- [SDR A6WA202020347145](https://openairdocs.org/sdr/A6WA202020347145.md): Floorbeam · corroded · Feb 1, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT IS CORRODED AT FS589.00, LBL 9 TO LBL 27. AIRCRAFT REMOVED FROM SERVICE INSTALLED NEW FABRICATED CAP STRIP AT FLOOR SUPPORT AT FS589.00, LBL 9 TO LBL 27 IAW CRJ200 SRM 51-42-06, 51-24-36 AND TR 51-42.
- [SDR A6WA2020020347147](https://openairdocs.org/sdr/A6WA2020020347147.md): Frame Angle · corroded · Feb 1, 2020 · N434AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 409 AFT ANGLE SPLICE HAS CORROSION SPOTS BETWEEN STRINGER 26L THRU 26R IN THE FWD E&E BAY AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE AT FRAME 409 AFT ANGLE SPLICE BETWEEN STINGER 26L AND 26R AND INSTALLED NEW ANLGE SPLICE IAW CRJ 200 SRM 51-42-06 AN
- [SDR A6WA2020020347143](https://openairdocs.org/sdr/A6WA2020020347143.md): Seat Track · corroded · Jan 31, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT FS559+112 TO FS574, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-00-49.
- [SDR A6WA202020347144](https://openairdocs.org/sdr/A6WA202020347144.md): Seat Track · corroded · Jan 31, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT FS559+86 TO FS559+96, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.
- [SDR A6WA202020347140](https://openairdocs.org/sdr/A6WA202020347140.md): Seat Track · corroded · Jan 31, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO TRACK IAW CRJ200 AMM 53-00-49.
- [SDR A6WA202020347141](https://openairdocs.org/sdr/A6WA202020347141.md): Seat Track · corroded · Jan 31, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.
- [SDR A6WA202020347142](https://openairdocs.org/sdr/A6WA202020347142.md): Seat Track · corroded · Jan 31, 2020 · N434AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT FS559+86 TO FS559+96, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.

Next page: https://openairdocs.org/aircraft/N434AW/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 = 'N434AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N434AW/reports

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