# Service difficulty reports: N459AW

A list on [N459AW](https://openairdocs.org/aircraft/N459AW.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 A6WA202608098906](https://openairdocs.org/sdr/A6WA202608098906.md): Engine · faulted · Aug 9, 2026 · N459AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ABORTED T/OFF AT 110 KTS, FLAPS 20, DUE TO A POPPING SOUND AND A/C PULLED TO THE RIGHT, DURING ROLL OUT WITH T/R'S DEPLOYED, NOTICED ITT ON RT ENGINE WAS RED. RETURNED TO NORMAL WHEN RESTOWING T/R'S. (BRAKE TEMP'S 8'S ACROSS THE BRD) AIRCRAFT REMOVED FROM SER
- [SDR A6WA202607128900](https://openairdocs.org/sdr/A6WA202607128900.md): Heat Exchanger · faulted · Jul 11, 2026 · N459AW · Cndair CL6002B19 · Engine Oil Indicating System
  > DURING CLIMB-OUT AT CLIMB POWER NR 2 ENGINE OIL TEMP WAS 150 DEG AND SLOWLY CLIMBING. IT RETURNED TO THE GREEN WHEN POWER WAS RETARDED. RTN TO AZA. AIRCRAFT REMOVED FROM SERVICE. R & R RT ENGINE HEAT EXCHANGER IAW AMM 79-21-07 OPS CHECK GOOD LEAK CHECK GOOD
- [SDR A6WA202407168779](https://openairdocs.org/sdr/A6WA202407168779.md): Frame · damaged · Jul 16, 2024 · N459AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION DAMAGED FRAME AT FS 605.00 BETWEEN STR 24L AND 20R. AIRCRAFT REMOVED FROM SERVICE. DAMAGED FRAME WAS REPAIRED BY CREATING A DOUBLER PER REO 601R-53-61-8207 REV --.
- [SDR A6WA202309288656](https://openairdocs.org/sdr/A6WA202309288656.md): Shutoff Valve · failed · Sep 28, 2023 · N459AW · Cndair CL6002B19 · Pneumatic System
  > LEFT 10TH STAGE FAILED CLOSED IN FLIGHT, UNABLE TO PROVIDE PRESSURE TO SINGLE PACK. (MOC NOTE RH PACK ON MEL) C/W IAC AND QRH FOR EMER DECENT. PASSENGER OXYGEN MASKS DEPLOYED, ON COMMAND. ISO VALVE FAILED TO OPEN WHEN COMMANDED. EMERGENCY DECLAIRED. AIRCRAFT
- [SDR A6WA202210258419](https://openairdocs.org/sdr/A6WA202210258419.md): Drag Angle · cracked · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE P/N: 601R-31907-301 AT FS 349 HAS A CRACK APPROX. 3.0" LENGTH******AIRCRAFT REMOVED FROM SERVICE********* PERFORMED CUTOUT ON PASSENGER DOOR AFT DRAG ANGLE WITH DIMENSIONS OF 21.0"L X 1.8"W IAW MHIRJ REO 601R-52-11-513 REV C DATE
- [SDR A6WA202210258420](https://openairdocs.org/sdr/A6WA202210258420.md): Bracket · corroded · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PASSENGER DOOR LOWER SURROUND STRUCTURE HAS CORROSION ON ANGLE P/N:601R31527-221 AND BRACKET CONNECTOR P/N: 601R31771-1 LOCATED BETWEEN FS 333 - FS 349 AND LBL 42 - LBL 44. *****************AIRCRAFT REMOVED FROM SERVICE********************** BLENDED 1 EA AREA
- [SDR A6WA202210258417](https://openairdocs.org/sdr/A6WA202210258417.md): Skin · dented · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Engine Air Intake System
  > RIGHT ENGINE LOWER TRANSLATING COWL HAD A DENT ON THE OUTER SKIN. AIRCRAFT REMOVED FROM SERVICE. FOUND OUT OF LIMITS IAW CMM 78-30-00, REV 24. CLEANED AND DRIED REPAIR AREA COMMON TO DENT IAW EA AWAC-CRJ254-01933, REV IR. INJECTED STRUCTURAL ADHESIVE INTO OP
- [SDR A6WA202210258416](https://openairdocs.org/sdr/A6WA202210258416.md): Anchor Fitting · corroded · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PASSENGER DOOR COUNTERBALANCE TWO ANCHOR FITTINGS, BS 310 - 349, LBL 44 HAVE SEVERE CORROSION OVER ENTIRE SURFACE OF FITTINGS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ANCHOR FITTINGS, IAW SRM 51-40-11 REV 39 AND AMM 52-11-17 REV 66.
- [SDR A6WA202210258413](https://openairdocs.org/sdr/A6WA202210258413.md): Fitting · chafed · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage, Wing Attach Fittings
  > LEFT WING TO FUSELAGE FITTING HAD WEAR. AIRCRAFT REMOVED FROM SERVICE. BLENDED THE TWO AREAS OF DAMAGE TO A SMOOTH CONTOUR 1.0"L X 0.300"W X 0.002"D AND 1.200"L X 0.090"W X 0.007"D IAW EA AWAC-CRJ252-01927 REV A. ACCOMPLISHED HFEC INSPECTION AT BLEND AREAS
- [SDR A6WA202210258412](https://openairdocs.org/sdr/A6WA202210258412.md): Arm · chafed · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD UPPER ROLLER ARM P/N: 601R318968-4 HAS WEAR MARKS. AIRCRAFT REMOVED FROM SERVICE. BLENDED DAMAGE TO A SMOOTH CONTOUR 0.4"L X 0.110"W X 0.090"D IAW EA CRJ252-01930, REV IR. ACCOMPLISHED HFEC INSPECTION AT BLEND AREA IAW NDT PART 1, 51-2
- [SDR A6WA202210258400](https://openairdocs.org/sdr/A6WA202210258400.md): Cover Plate · corroded · Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL COVER PLATE HAD SEVERAL AREAS OF SEVERE CORROSION ALONG ENTIRE LENGTH OF PLATE FROM BS 319 - 349, RBL 42 - 46. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR LOWER SILL COVER PLATE IAW 51-41-02, REV 39.
- [SDR A6WA202112108021](https://openairdocs.org/sdr/A6WA202112108021.md): Control Panel · false activation · Dec 9, 2021 · N459AW · Cndair CL6002B19 · Smoke Detection
  > RECIEVED CARGO SMOKE IN FLIGHT C/W QRH CARGO FIRE BOTTLE DISCHARGED. AIRCRAFT DECLARED AND EMERGENCY AND DIVERTED TO MEM. ONCE ON GROUND INSPECTED CARGO BIN, NO EVIDENCE OF SMOKE OR FIRE ***AIRCRAFT REMOVED FROM SERVICE*** R+R CARGO FIREX CONTROL PANEL
- [SDR A6WA202104027734](https://openairdocs.org/sdr/A6WA202104027734.md): Servo · malfunctioned · Apr 2, 2021 · N459AW · Cndair CL6002B19 · Autopilot System
  > ON 2 MILE FINAL, DISCONNECTED THE A/P AND IT DISENGAGED. HAD ROLL CONTROL, BUT PITCH CONTROL WAS STUCK. PRESSED AP DISCONNECT AGAIN, PITCH CONTROL REMAINED STUCK. PUSHED/PULLED ON CONTROL YOKE AND PITCH CONTROL POPPED FREE. STAB CHANNEL 1 INOP MESSAGE APPE
- [SDR A6WA202102087619](https://openairdocs.org/sdr/A6WA202102087619.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, BLENDED AREA MEASURES 1.460Ï¿½ L X 0.740Ï¿½ W, REF BOMBARDIER REO: 60
- [SDR A6WA202102087618](https://openairdocs.org/sdr/A6WA202102087618.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AR FS542.00 RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR PANEL AT FS542.00 RBL 42. EVALUATED BLEND AREA AND FOUND TO BE WITHIN ALOWABLE LIMITS. HFCC INSPECTION PERFORMED WITH NO INDICATIONS NOT
- [SDR A6WA202102087617](https://openairdocs.org/sdr/A6WA202102087617.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AR FS 536.00 RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR PANEL AT FS536.00 RBL 42. EVALUATED BLEND AREA AND FOUND TO BE WITHIN ALOWABLE LIMITS. HFCC INSPECTION PERFORMED WITH NO INDICATIONS N
- [SDR A6WA202102087625](https://openairdocs.org/sdr/A6WA202102087625.md): Bulkhead Web · cracked · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THERE WERE 13 CRACK INDICATIONS DURING THE TIME OF THIS INSPECTION ROW CRS 4AER685B W/O 003154 CARD NO. 453-280-607. THE CRACK LOCATIONS ARE LISTED BELOW: FS 621 WL 110-111.5, RBL 27.5+.375 CRACK LENGTH 1.5" FS 621 WL 108.5-109.5, RBL 27.50+.375 CRACK LENG
- [SDR A6WA202102087616](https://openairdocs.org/sdr/A6WA202102087616.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS 531.00 RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 531.00 RBL 42. EVALUATED BLEND AREA AND FOUND TO BE WITHIN ALLOWABLE LIMITS. HFCC INSPECTION PERFORMED WITH NO INDICAI
- [SDR A6WA202102057606](https://openairdocs.org/sdr/A6WA202102057606.md): Pressure Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 459.00, RBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 459.00, RBL 42, BLENDED AREA MEASURES 1.380 L X 0.750 W, REF BOMBARDIER REO: 601R-53-41-666, REV
- [SDR A6WA202102057602](https://openairdocs.org/sdr/A6WA202102057602.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 461.00 + 7, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 461.00 + 7, LBL 42, BLENDED AREA MEASURES 1.210 L X 0.650 W, REF BOMBARDIER REO: 601R-53-41-6
- [SDR A6WA202102057600](https://openairdocs.org/sdr/A6WA202102057600.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 499.00 + 9, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 499.00 + 9, LBL 42, BLENDED AREA MEASURES 1.99 L X 1.31 W, REF BOMBARDIER REO: 601R-53-41-666
- [SDR A6WA202102057608](https://openairdocs.org/sdr/A6WA202102057608.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 555.00, RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 555.00, RBL 42, BLENDED AREA MEASURES 1.510 L X 1.160 W, REF BOMBARDIER REO: 601R-53-41-666, REV C, ISSUE DATE: 11-06-
- [SDR A6WA202102057607](https://openairdocs.org/sdr/A6WA202102057607.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS. 524.00, RBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 524.00, RBL 42, BLENDED AREA MEASURES 1.800Ï¿½ L X 1.100Ï¿½ W, REF BOMBARDIER REO: 601R-53-41-666, REV (C), IS
- [SDR A6WA202102057604](https://openairdocs.org/sdr/A6WA202102057604.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 484.00, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT MOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 484.00, LBL 42, BLENDED AREA MEASURES 1.550 L X 0.901 W, REF BOMBARDIER REO: 601R-53-41-666, REV C,
- [SDR A6WA202102057603](https://openairdocs.org/sdr/A6WA202102057603.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 473.15 + 5, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 473.15 + 5, LBL 42, BLENDED AREA MEASURES 1.510 L X 0.840 W, REF BOMBARDIER REO: 601R-53-41-6
- [SDR A6WA202102057605](https://openairdocs.org/sdr/A6WA202102057605.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 484.00 + 2, RBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 484.00 + 2, RBL 42, BLENDED AREA MEASURES 1.610 L X 0.950 W, REF BOMBARDIER REO: 601R-53-41-6
- [SDR A6WA202102057601](https://openairdocs.org/sdr/A6WA202102057601.md): Floor Panel · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL AT FS 461.00, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 461.00, LBL 42, BLENDED AREA MEASURES 0.460L X 0.330 W, REF BOMBARDIER REO: 601R-53-41-666, REV
- [SDR A6WA202102047585](https://openairdocs.org/sdr/A6WA202102047585.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 542.00, RBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 542.00, RBL 42, BLENDED AREA MEASURES 1.54Ï¿½ L X 1.26Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DA
- [SDR A6WA202102047580](https://openairdocs.org/sdr/A6WA202102047580.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, HAS CORROSION AROUND NUT-PLATE ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 7, LBL 42, AT NUT-PLATE HOLE, BLENDED AREA MEASURES 1.46Ï¿½ L X 0.740Ï¿½ W REF BOMB
- [SDR A6WA202102047584](https://openairdocs.org/sdr/A6WA202102047584.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 536.00, RBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 536.00, RBL 42, BLENDED AREA MEASURES 1.53Ï¿½ L X 0.96Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DA
- [SDR A6WA202102047581](https://openairdocs.org/sdr/A6WA202102047581.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 529.00 + 2, LBL 42, HAS CORROSION AROUND NUT-PLATE ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 2, LBL 42, AT NUT-PLATE HOLE, BLENDED AREA MEASURES 0.88Ï¿½ L X 0.81Ï¿½ W REF BOMBA
- [SDR A6WA202102047582](https://openairdocs.org/sdr/A6WA202102047582.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR PANEL AT FS. 529.00 + 13, LBL 42, HAS CORROSION AROUND NUT-PLATE ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 529.00 + 13, LBL 42, AT NUT-PLATE HOLE, BLENDED AREA MEASURES 1.00Ï¿½ L X 0.070Ï¿½ W REF BO
- [SDR A6WA202102047598](https://openairdocs.org/sdr/A6WA202102047598.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 513.00 + 6, LBL 42, HAS CORROSION AROUND NUT PLATE HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 513.00 + 6, LBL 42, BLENDED AREA MEASURES 0.88Ï¿½ L X 0.34Ï¿½ W, REF BOMBARDIER REO:
- [SDR A6WA202102047583](https://openairdocs.org/sdr/A6WA202102047583.md): Pressure Deck · corroded · Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 531.00, RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 531.00, RBL 42, BLENDED AREA MEASURES 1.540Ï¿½ L X 1.00Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DATE: 1
- [SDR A6WA202102087620](https://openairdocs.org/sdr/A6WA202102087620.md): Skin · dented · Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OUTWARD DENT C/T EXTERIOR SKIN AT FS682.00 +8 STRINGER 23R+3 ***AIRCRAFT REMOVED FROM SERVICE*** REPAIR PERFORMED I.A.W. ASAP EA#AWAC - CRJ253-01558 REV IR DATED 01/29/2021. REPAIR PERFORMED ON AERSALE W/O 003154 CARD NO 20128.CID 533818
- [SDR A6WA202102087623](https://openairdocs.org/sdr/A6WA202102087623.md): Skin · dented · Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OUTWARD DENT C/T EXTERIOR SKIN AT FS682.00 +21 STR 23R+4. AIRCRAFT REMOVED FROM SERVICE. REPAIR PERFORMED IAW ASAP EA #AWAC - CRJ253 - 01558 REV IR DATED 01/29/2021. REPAIR PERFORMED IAW W/O 003154 CARD NO 20128.CID 533818.
- [SDR A6WA202102087622](https://openairdocs.org/sdr/A6WA202102087622.md): Skin · dented · Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTS WITH CREASES FOUND BETWEEN FS682.00 AND FS700.00 STR 23R-24R AIRCRAFT REMOVED FROM SERVICE. REPAIR PERFORMED IAW ASAP EA# AWAC CRJ253-01558 REV IR DATED 01/29/2021. REPAIR PERFORMED ON AERSALE W/O 003154 CARD NO 20128.CID 533818.
- [SDR A6WA202102087624](https://openairdocs.org/sdr/A6WA202102087624.md): Skin · dented · Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OUTWARD DENT C/T EXTERIOR SKIN AT FS 682.00+16 & S23R+3" ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR ON SKIN AT FS 682 TO FS 700 AND S23R TO S24R. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF. ASAP EA# AWAC-CRJ253-01558. REV IR
- [SDR A6WA202102057609](https://openairdocs.org/sdr/A6WA202102057609.md): Skin Panel · dented · Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > OUTWARD DENT AT FUSELAGE EXTERIOR SKIN AT FS. 654.50 + 22, STGR 23R + 3. AIRCRAFT REMOVED FROM SERVICE. MEASURED DENT AT FS. 654.50 + 22, STGR 23R + 3, DENT MEASURES 0.750” L X 0.600” W X 0.010” D REF AIR WISCONSIN SUPPLEMENT NO. 14-239. CALIPER SN: 0036003
- [SDR A6WA202102087612](https://openairdocs.org/sdr/A6WA202102087612.md): Bulkhead Web · cracked · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT FS. 621.00, WL 100.5 TO WL 102.5, RBL 27.50 +.375, CRACK 2.50Ï¿½L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUT-OUT ON DAMAGED AREA OF AFT PRESSURE BULKHEAD AT FS. 621.00, RBL 27.50, CUT-OUT DIMENSIONS: 14.00Ï¿½ L X 1.7
- [SDR A6WA202102047596](https://openairdocs.org/sdr/A6WA202102047596.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 499.00, LBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 499.00, LBL 42, BLENDED AREA MEASURES P(1) 0.950Ï¿½ L X 0.452Ï¿½ W, REF REO: 601R-53-41-666, REV (C), ISSUE DATE
- [SDR A6WA202102047597](https://openairdocs.org/sdr/A6WA202102047597.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 499.00 + 5 TO FS. 499.00 + 9, LBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 499.00 + 5 TO FS. 499.00 + 9, LBL 42, BLENDED AREA MEASURES P(1) 7.50Ï¿½ L X 1.0Ï¿½ W, REF
- [SDR A6WA202102047595](https://openairdocs.org/sdr/A6WA202102047595.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 484.00, LBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 484.00, LBL 42, BLENDED AREA MEASURES P(1) 2.821Ï¿½ L X 0.943Ï¿½ W, REF REO: 601R-53-41-666, REV (C), ISSUE DATE
- [SDR A6WA202102047586](https://openairdocs.org/sdr/A6WA202102047586.md): Pressure Deck · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS. 559.00, LBL 42, HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS. 559.00, LBL 42, BLENDED AREA MEASURES 2.17Ï¿½ L X.73Ï¿½ W REF BOMBARDIER REO 601R-53-41-666, REV (C), ISSUE DAT
- [SDR A6WA202102047593](https://openairdocs.org/sdr/A6WA202102047593.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 544.00, RBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 544.00, RBL 42, BLENDED AREA MEASURES P(1) 1.00Ï¿½ L X 0.56Ï¿½ W, REF REO: 601R-53-41-666, REV (C), ISSUE DATE:
- [SDR A6WA202102047587](https://openairdocs.org/sdr/A6WA202102047587.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 461.00, LBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 461.00, LBL 42, BLENDED AREA MEASURES P(1) 1.95Ï¿½ L X 0.900Ï¿½ W, P(2) 0.500Ï¿½ L X 0.180Ï¿½ W, REF REO: 601R-
- [SDR A6WA202102047589](https://openairdocs.org/sdr/A6WA202102047589.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 461.00 + 7, LBL 36 TO LBL 40, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 461.00 + 7, LBL 36 TO LBL 40, BLENDED AREA MEASURES P(1) 1.66Ï¿½ L X 0.680Ï¿½ W, P(2) 0.95Ï¿½ L X
- [SDR A6WA202102047588](https://openairdocs.org/sdr/A6WA202102047588.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 513.00 + 3, LBL 36 TO 40, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 513.00 + 3, LBL 36 TO 40, BLENDED AREA MEASURES P(1) 1.16Ï¿½ L X 0.710Ï¿½ W, P(2) 1.98Ï¿½ L X 0.55Ï¿½
- [SDR A6WA202102047594](https://openairdocs.org/sdr/A6WA202102047594.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 473.15 + 4, LBL 36 TO LBL 40, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 473.15 + 4, LBL 36 TO LBL 40, BLENDED AREA MEASURES P(1) 6.5Ï¿½ L X 0.514Ï¿½ W, REF REO: 601R-53-4
- [SDR A6WA202102047591](https://openairdocs.org/sdr/A6WA202102047591.md): Floor Support · corroded · Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS. 461.00, RBL 42, HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS. 461.00, RBL 42, BLENDED AREA MEASURES P(1) 2.149Ï¿½ L X.780Ï¿½ W, REF REO: 601R-53-41-666, REV (C), ISSUE DATE:

Next page: https://openairdocs.org/aircraft/N459AW/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 = 'N459AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N459AW/reports

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