# Service difficulty reports: N426AW

A list on [N426AW](https://openairdocs.org/aircraft/N426AW.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 · 233 reports

- [SDR A6WA202412138845](https://openairdocs.org/sdr/A6WA202412138845.md): Control Handle · malfunctioned · Dec 13, 2024 · N426AW · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF RECEIVED ANTISKID IB AND PAKING BRAKE SOV CAUTION MESSAGES AFTER GEAR SELECTED TO UP POSITION. GEAR INDICATED DOWN 3 GREEN WITH GEAR LEVER IN UP POSITION DID NOT RECEIVE GEAR DISAGREE WARNING. DID NOT EXCEED SPEED LIMITATIONS REMAINED UNDER 250 K
- [SDR A6WA202403048720](https://openairdocs.org/sdr/A6WA202403048720.md): Landing · cracked · Mar 4, 2024 · N426AW · Cndair CL6002B19 · Wing Main, Frame Structure
  > 50057 334424 601R-57-21-3821 HRS 24.45 CRACK FOUND ON LOWER WING SKIN LANDING UNDER ACCESS PANEL 601R10213-4. AIRCRAFT REMOVED FROM SERVICE. (RH MLG) REPAIR WAS PERFORMED TO THE RH WING LOWER AFT PLANK BY MHI MRT. REF. MHI RJ REO 601R-57-21-3821 REV. A DA
- [SDR A6WA202402218717](https://openairdocs.org/sdr/A6WA202402218717.md): Doubler · corroded · Feb 21, 2024 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE AT FS605 BETWEEN STR 25R AND 26R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND REMOVED CORROSION FROM FUSELAGE SKIN AT FS605 TO 621 STR 25R AND 26R REF CRJ200 SRM 53-00-00, AND 53-00-31 REV39, AND REMOVED AND REPLACED INTERNAL DOUBLE
- [SDR A6WA202401248711](https://openairdocs.org/sdr/A6WA202401248711.md): Bracket · cracked · Jan 24, 2024 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED BRACKET ON PREVIOUS REPAIR ON AFT PRESSURE BULKHEAD NEAR LINTEL AT FS 629.00 AND LBL36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CHANNEL AT FS 629.00 AND LBL36 WITH FABRICATED NEW CHANNEL. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMIT
- [SDR A6WA202303148500](https://openairdocs.org/sdr/A6WA202303148500.md): Unknown · unknown · Mar 13, 2023 · N426AW · Cndair CL6002B19 · Landing Gear Door Actuator
  > RECEIVED GEAR DISAGREE AND NOSE DOOR WARNING MSGS ON TAKEOFF CW QRH MSGS CLEARED. MSGS POSTED ABOUT 6 SECONDS AFTER RETRACTION WAS SELECTED. NO HYD SYSTEM ABNORMALITIES WERE NOTED LANDING WEIGHT WAS 46800 AND LANDING WAS SMOOTH. NO GEAR LIT UP RED ON EICAS.
- [SDR A6WA2023012768447](https://openairdocs.org/sdr/A6WA2023012768447.md): Ecu · faulted · Jan 26, 2023 · N426AW · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION CLIMBING THROUGH FL140. C/W QRH MESSAGE PERSISTS. AFTER LANDING WITH NWS ARMED, MESSAGE RETURNED. *****AIRCRAFT REMOVED FROM SERVICE****** R&R NWS ECU IAW AMM 32-51-10. PERFORMED OPS CHECK, OPS CHECK GOOD.PN: 16900-107 S/N OFF: 02-744
- [SDR A6WA202301208433](https://openairdocs.org/sdr/A6WA202301208433.md): Rib · damaged · Jan 20, 2023 · N426AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > TEMPORARY REPAIR TO THE R/H HORIZONTAL STABILIZER CLOSING RIB ******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED CLOSING RIB REF REO 601R-55-11-739 REV A DATED 2023-01-19
- [SDR A6WA202112318175](https://openairdocs.org/sdr/A6WA202112318175.md): None · corroded · Dec 31, 2021 · N426AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > R/H SIDEWALL SEAT TRACKS (3 EA) FROM FS 409+111.98 TO FS 549.06 HAVE SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 409+111.98 TO FS 549.06 FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AI
- [SDR A6WA202112288174](https://openairdocs.org/sdr/A6WA202112288174.md): Skin · dented · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > DENT ON FORWARD FUSELAGE LOWER SKIN AT FS283 AND STR23R - STR24R. ****AIRCRAFT REMOVED FROM SERVICE **** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS283 AND STR23R - STR24R. PN 601R31022-3. DENT DIMENSIONS P1- L = 1.20Ï¿½ X W = 1.00Ï¿½ X D = 0.023Ï¿½. ORIGINAL
- [SDR A6WA202112288172](https://openairdocs.org/sdr/A6WA202112288172.md): Skin · dented · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S25L - S26L. ***AIRCRAFT REMOVED FROM SERVICE **** VERIFIED NO LOOSE OR PULLED FASTENERS AROUND DENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S25L - S26L. PN 601R35005-143. DENT DIMENSIONS P1- L
- [SDR A6WA202112288170](https://openairdocs.org/sdr/A6WA202112288170.md): Seat Track · corroded · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > RH SIDEWALL SEAT TRACK FROM FS364 TO FS409.00 + 16 HAS SURFACE CORROSION. ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS364 TO FS409.00 + 16. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS
- [SDR A6WA202112288171](https://openairdocs.org/sdr/A6WA202112288171.md): Skin · dented · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS654.50 Ï¿½ FS672.20 AND S25L - S26L. ****AIRCRAFT REMOVED FROM SERVICE ***** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS654.50 Ï¿½ FS672.20 AND S25L - S26L. PN 601R35005. DENT DIMENSIONS P1- L = 0.500Ï¿½ X W = 0.500Ï¿½ X D = 0.
- [SDR A6WA202112288169](https://openairdocs.org/sdr/A6WA202112288169.md): Seat Track · corroded · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)
  > RH SIDEWALL SEAT TRACK FROM FS409.00 + 16 TO FS409.00 + 112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 + 16 TO FS409.00 + 112. RESTORED PROTECTIVE FINISH. ALL WORK W
- [SDR A6WA202112288173](https://openairdocs.org/sdr/A6WA202112288173.md): Fitting · gouged · Dec 28, 2021 · N426AW · Cndair CL6002B19 · Leading Edge Devices
  > CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING. ****AIRCRAFT REMOVED FROM SERVICE ****** BLENDED CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING PN601R10315. CHAFE DIMENSIONS L = 0.500Ï¿½ X W = 1.750Ï¿½ X D = 0.020Ï¿½. PERFORMED HFEC
- [SDR A6WA202111187973](https://openairdocs.org/sdr/A6WA202111187973.md): None · corroded · Nov 13, 2021 · N426AW · Cndair CL6002B19 · Horizontal Stabilizer, Tab Structure
  > PAX DOOR FWD ANCHO FITTING PLATE P/N600-38061-11 WAS FOUND CORRODED. THE EXPANSION CAUSED THE PAX DOOR FWD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR FWD ANCHOR PLATE AND ALL ATTACHING HARDWARE, FWD PAX DOOR SWIVEL CABLE END,
- [SDR A6WA2020031047220](https://openairdocs.org/sdr/A6WA2020031047220.md): Wire Harness · defective · Mar 8, 2020 · N426AW · Cndair CL6002B19 · Landing Gear System Wiring
  > ON FINAL NLG DID NOT SHOW DOWN & GREEN. DID NOT RECEIVE GEAR DISAGREE MESSAGE. NLG INDICATED RED. RAN GEAR DISAGREE QRH. NLG BOX TURNED GREEN AND MESSAGE CLEARED. NO ABNORMAL HYD INDICATIONS. NO OTHER EICAS MESSAGES NOTED. AIRCRAFT REMOVED FROM
- [SDR A6WA2020010647091](https://openairdocs.org/sdr/A6WA2020010647091.md): Skin · damaged · Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PER CUSTOMER REQUEST, APPLY GENERIC REO 601R-53-11-0048 ON LEFT SIDE SKIN RADIUS AT FS 235. AIRCRAFT REMOVED FROM SERVICE REPAIRED NLG CUTOUT, LH SIDE, AT FS235 I/A/W BOMBARDIER REO 601R-53-11-0048 REV. D.
- [SDR A6WA2020010647094](https://openairdocs.org/sdr/A6WA2020010647094.md): Skin · cracked · Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT AFT RIGHT CORNER NEXT TO SPADE DOOR IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPAIRED FUSELAGE SKIN IAW REO 601R-53-11-3525 REV-- DATED 01-02-2020.
- [SDR A6WA2020010647092](https://openairdocs.org/sdr/A6WA2020010647092.md): Stiffener · cracked · Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HAND VERTICAL STIFFENER ON OUTBOARD SIDE OF NOSE LANDING GEAR WHEEL WELL STRUCTURE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH SIDE VERTICAL STIFFENER ON OUTBOARD SIDE OF NLG WHEEL WELL IAW CRJ200 SRM 51-42-06 AND 51-42-21.
- [SDR A6WA2020010647090](https://openairdocs.org/sdr/A6WA2020010647090.md): Retainer · chafed · Jan 4, 2020 · N426AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SEAL RETAINER CHAFFED IN MULTIPLE SPOTS. AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR SEAL RETAINER I/A/W CRJ200 SRM 51-42-06 & 51-42-21. CARGO DOOR LEAK CHECK GOOD I/A/W CRJ200 AMM 52-31-07-710-801
- [SDR A6WA2020010647088](https://openairdocs.org/sdr/A6WA2020010647088.md): Strut · cracked · Jan 2, 2020 · N426AW · Cndair CL6002B19 · APU Cowling/Containment
  > BOTTOM SIDE OF APU ENCLOSURE WELD REPAIR IS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED APU ENCLOSURE IAW AWAC SUP 19-341C
- [SDR A6WA2019123047081](https://openairdocs.org/sdr/A6WA2019123047081.md): Rib · cracked · Dec 22, 2019 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 446AL HAS PREVIOUS REPAIR DOUBLER CRACKED ON 2ND RIB AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED 2ND RIB ON PANEL 446AL IAW BOMB. CMM 20-42-06
- [SDR A6WA2019122347078](https://openairdocs.org/sdr/A6WA2019122347078.md): Floor Support · corroded · Dec 20, 2019 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL CORRODED AT NUT PLATE, FS 295.00-319.70, STR17R. AIRCRAFT REMOVED FROM SERVICE REPLACED SILL IAW CRJ200 SRM 51-42-13.
- [SDR A6WA2019122047070](https://openairdocs.org/sdr/A6WA2019122047070.md): Fitting · cracked · Dec 18, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > RIGHT LOWER WING TO FUSELAGE FAIRING FITTING CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED FITTING IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA20192047072](https://openairdocs.org/sdr/A6WA20192047072.md): Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > LEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA20195047074](https://openairdocs.org/sdr/A6WA20195047074.md): Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > LEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AT FS461.00,LBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
- [SDR A6WA20192047076](https://openairdocs.org/sdr/A6WA20192047076.md): Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > RIGHT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED AT FS 449.85, RBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
- [SDR A6WA20192047075](https://openairdocs.org/sdr/A6WA20192047075.md): Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > LEFT WING TO BODY FAIRING ATTACH BRACKET CRACKED AT FS 449.85, LBL 45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA20192047071](https://openairdocs.org/sdr/A6WA20192047071.md): Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic Fairings
  > LEFT FUSELAGE TO WING FAIRING BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA2019121947068](https://openairdocs.org/sdr/A6WA2019121947068.md): Attach Bracket · cracked · Dec 17, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FAIRING ATTACH BRACKET ON FUSELAGE LONGERON AT RBL 45 AND FS 469.63 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM 51-42-06
- [SDR A6WA2019121847066](https://openairdocs.org/sdr/A6WA2019121847066.md): Fitting · cracked · Dec 16, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT LOWER SIDE WINDOW JOINT TO FUSELAGE ATTACH FITTING IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ATTACH FITTING IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2019123047082](https://openairdocs.org/sdr/A6WA2019123047082.md): Support · cracked · Dec 15, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS621 APB SUPPORT CRACKED AT LBL45 WL80 AN AFT SIDE OF BULKHEAD AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED STIFFNER IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019121847063](https://openairdocs.org/sdr/A6WA2019121847063.md): Floorbeam · cracked · Dec 14, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > L/H FLOOR SUPPORT SILL PLATE CRACKED AT FS 605.0 ADJACENT TO FASTENER COMMON TO SILL AND FLOOR SUPPORT BEAM AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H FLOOR SILL PLATE AT FS 605.0 IAW REO 601R-53-61-433
- [SDR A6WA2019121847060](https://openairdocs.org/sdr/A6WA2019121847060.md): Skin · cracked · Dec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT HAND DOOR 211AL AFT LATCH CUT-OUT IS CRACKED REPAIRED SKIN IAW AWAC SUP. 19-016B
- [SDR A6WA2019121847058](https://openairdocs.org/sdr/A6WA2019121847058.md): Bulkhead Web · cracked · Dec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PERFORM MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS 621.0 AIRCRAFT REMOVED FROM SERVICE COMPLETED MODIFICATION OF THE REAR PRESSURE BULKHEAD AT FS 621.0 IAW REO 601R-53-61-1240 REV D
- [SDR A6WA2019121847062](https://openairdocs.org/sdr/A6WA2019121847062.md): Attach Angle · cracked · Dec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE COMMON TO FS621.0 RPB AND CARGO NET AFT TIE DOWN FITTING SUPPORT STRUCTURE IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ANGLE IAW CRJ -200 SRM 51-42-21
- [SDR A6WA2019121847059](https://openairdocs.org/sdr/A6WA2019121847059.md): Skin · chafed · Dec 13, 2019 · N426AW · Cndair CL6002B19 · Ailerons
  > R/H AILERON OUTBOARD LOWER SKIN LEADING EDG IS CHAFFED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEADING EDGE IAW CRJ-200 SRM 51-42-21 AND 51-42-06
- [SDR A6WA2019111847014](https://openairdocs.org/sdr/A6WA2019111847014.md): Connector · loose · Nov 15, 2019 · N426AW · Cndair CL6002B19 · Electrical Power System Wiring
  > GEN #1 CAUTION MESSAGE IN CRUISE C/W QRH DID NOT RESET. AIRCRAFT REMOVED FROM SERVICE. #1 IDG TEMP BULB CANNON PLUG FOUND LOOSE RE-SECURED CANNON PLUG REF AMM 24-12 OPS CHECK GOOD.
- [SDR A6WA2018111246144](https://openairdocs.org/sdr/A6WA2018111246144.md): Unknown · malfunctioned · Nov 9, 2018 · N426AW · Cndair CL6002B19 · Pneumatic Distribution System
  > AT CRUISE FL250 NOTICED RT PACK OFF STATUS MESSAGE AND RT PACK OFF SWITCH LIGHT ILLUMINATED. CYCLED RT PACK SWITCH TWICE. PACK REMAINED OFF. SELECTED ECS PAGE ON EICAS. RT 10TH STAGE BLEED CLOSED. CYCLED R 10TH SWITCH CLOSED THEN OPEN. PRESSURIZATION RESUMED.
- [SDR A6WA2018100846101](https://openairdocs.org/sdr/A6WA2018100846101.md): Acm · malfunctioned · Oct 5, 2018 · N426AW · Cndair CL6002B19 · Cabin Cooling System
  > DURING SINGLE PACK OPERATION ON ENGINE BLEED AIR IN CLIMB AT APPROX 92% N1 RECEIVED RIGHT PACK OFF LIGHT AND RIGHT PACK OVERPRESS MESSAGE C/W QRH AND IAC RIGHT PACK OPERATION NORMAL ON APU BLEED R/R ACM IAW 21-51-10. OPS CK GOOD.
- [SDR A6WA2017122145495](https://openairdocs.org/sdr/A6WA2017122145495.md): Skin · dented · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER SKIN IS DENTED 22 INCHES FROM INBD EDGE AND 16 INCHES FROM T/E.
- [SDR A6WA2017122145491](https://openairdocs.org/sdr/A6WA2017122145491.md): Frame · cracked · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 BETWEEN STRINGER 2 AND 3 LEFT IS CRACKED.
- [SDR A6WA2017122145496](https://openairdocs.org/sdr/A6WA2017122145496.md): Bulkhead Web · damaged · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD ABOVE FLOOR HAS SCRATCHES AND BARE METAL. REPAIRED THE BULKHEAD.
- [SDR A6WA2017122145492](https://openairdocs.org/sdr/A6WA2017122145492.md): Skin · corroded · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN PANEL PITTED WITH BARE METAL AT WS 56.30 TO WS 75.27.
- [SDR A6WA2017122145493](https://openairdocs.org/sdr/A6WA2017122145493.md): Frame · cracked · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 605 ATTACHMENT FLANGES CRACKED ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME
- [SDR A6WA2017122145494](https://openairdocs.org/sdr/A6WA2017122145494.md): Vane · chafed · Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANE.
- [SDR A6WA2017121945486](https://openairdocs.org/sdr/A6WA2017121945486.md): Floorbeam · cracked · Dec 15, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 280 IS CRACKED AT THE LOWER ANGLE JUST OB OF THE MLG ALT CABLE PULLEY BRACKET. REPAIRED THE ANGLE.
- [SDR A6WA2017121945485](https://openairdocs.org/sdr/A6WA2017121945485.md): Floorbeam · cracked · Dec 14, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280, LBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE
- [SDR A6WA2017121945484](https://openairdocs.org/sdr/A6WA2017121945484.md): Floorbeam · cracked · Dec 14, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 RBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE
- [SDR A6WA201745480](https://openairdocs.org/sdr/A6WA201745480.md): Angle · cracked · Dec 13, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > 1015090-3000-0014 - L/H UPPER OBLIQUE ANGLE CRACKED AFT PRESSURE BULKHEAD

Next page: https://openairdocs.org/aircraft/N426AW/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 = 'N426AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N426AW/reports

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