# Service difficulty reports: N433AW

A list on [N433AW](https://openairdocs.org/aircraft/N433AW.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 · 259 reports

- [SDR A6WA202607028897](https://openairdocs.org/sdr/A6WA202607028897.md): Acm · faulted · Jul 2, 2026 · N433AW · Cndair CL6002B19 · Cabin Cooling System
  > RT PACK TRIPPED OFF LINE 2 TIMES AT 80 PSI, PACK RESET EACH TIME, PACK HI TEMP CAUTION AT 30 DEG C PACK RESET PER QRH. NO PRESSURIZATION ISSUES. AIRCRAFT REMOVED FROM SERVICE, EMER DEPRESS SWITCH/ LIGHT PUSHED IN. DEACTIVATED BOTH A/C PACKS. DEACTIVATED
- [SDR A6WA202604068882](https://openairdocs.org/sdr/A6WA202604068882.md): Control Lever · faulted · Mar 28, 2026 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20* ON APPROACH C/W QRH AND LANDED NORMALLY. MAX BRAKE TEMP 04 ALL WHEELS. PREFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 11. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE IAW W/O 347359. FLAP FAIL INTEROGATION
- [SDR A6WA202602228879](https://openairdocs.org/sdr/A6WA202602228879.md): Priority Valve · faulted · Feb 22, 2026 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MSG AFTER T/O. NOSE GEAR INDICATED UNSAFE AND NOT UP AND LOCKED. C/W QRH. GEAR INDICATED DOWN AND LOCKED AFTER USING EMERGENCY EXTENSION HANDLE. ALL MSG'S EXTINGUISHED AFTER QRH. GEAR DISAGREE MESSAGE ORIGINALLY APPEARED 6-10 SECONDS AFTE
- [SDR A6WA202601318875](https://openairdocs.org/sdr/A6WA202601318875.md): Selector Valve · faulted · Jan 31, 2026 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING WITH TRIPLE CHIME AFTER TAKE OFF. C/W QRH, DECLARED EMERGENCY, AND RETURNED TO MSP. WARNING OCCURRED 28 SECONDS AFTER TAKE OFF, NO OTHER MSGS, NOSE GEAR RED, MANUAL RELEASE USED, HYD PUMPS AUTO, 160KTS, SMOOTH LANDING. REMOVED FLAGS FROM
- [SDR A6WA202211228386](https://openairdocs.org/sdr/A6WA202211228386.md): Ballast · smoke · Nov 22, 2022 · N433AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > DISCREPANCY: CREW WITNESSED SMOKE COMING FROM ABOVE BIN OVER ROW 10AB AS WELL AS BURN MARKS ON THE CEILING. ****AIRCRAFT REMOVED FROM SERVICE***** REMOVED AND REPLACED SIDEWALL BALLAST LOCATED AT 10AB. OPS CHECK GOOD. IAW AMM 33-21-10. REF 339930-2 FOR
- [SDR A6WA202201318148](https://openairdocs.org/sdr/A6WA202201318148.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H CABIN FLOOR SUPPORT BEAM P/N: 601R35031-3 HAS CORROSION AT FS 589 TO FS 621 AND LBL 27. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA OF CORROSION ON FLOOR SUPPORT BEAM P/N: 601R35031-3 AT FS 589-621 WITH ORIGINAL MATE
- [SDR A6WA202201318147](https://openairdocs.org/sdr/A6WA202201318147.md): None · cracked · Jan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H CABIN FLOOR SUPPORT ANGLE P/N: 601R 53-61-004-1 HAS A CRACK.900"L ON FORWARD INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED PREVIOUS REPAIR SPLICE ON L/H CABIN FLOOR SUPPORT ANGLE P/N: 601R-53-61-004-
- [SDR A6WA202201318142](https://openairdocs.org/sdr/A6WA202201318142.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > R/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRC
- [SDR A6WA202201318145](https://openairdocs.org/sdr/A6WA202201318145.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Floor Panel
  > R/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRC
- [SDR A6WA202201318146](https://openairdocs.org/sdr/A6WA202201318146.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 HAS AREA OF SURFACE CORROSION AT FS 574 TO FS 621 AT LBL 42 TO LBL 46. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA ON L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 AT
- [SDR A6WA202201318136](https://openairdocs.org/sdr/A6WA202201318136.md): Fitting · corroded · Jan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION ON PASSENGER DOOR FITTING P/N: 601R31527-217 AT FS 341 TO FS 345 AND LBL 42 TO LBL 44 AND WL 73.50. ************AIRCRAFT REMOVED FROM SERVICE**************************** UPON FURTHER INSPECTION, FOUND SEVERE CORROSION ON PASSENGER DOOR BRACKET P/N
- [SDR A6WA202201318135](https://openairdocs.org/sdr/A6WA202201318135.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > R/H O/B FLOOR SILL AT FS 559+80 TO FS 559+115 AND LATERAL FLOOR BEAM AT 559+80 I/B AFT CORNER ARE CORRODED. CLEANED I/B LATERAL FLOOR BEAM AT FS 559+80 IAW CRJ200 51-26-00 REV 38. UPON FURTHER INVESTIGATION OF I/B LATERAL FLOOR BEAM AT FS 559+80 FOUND NO COR
- [SDR A6WA202201318132](https://openairdocs.org/sdr/A6WA202201318132.md): None · dented · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > AIRCRAFT L/H SKIN EXTERIOR HAS 2 EACH DENTS AT FS 625 TO FS 640 AND S19L TO S20L. DENT DIMENSIONS ARE: (P1) 1.0"L X.900"W X.015"D; (P2).800"L X.800"W X.012"D. EVALUATED BOTH DENTS AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. *
- [SDR A6WA202201318131](https://openairdocs.org/sdr/A6WA202201318131.md): None · gouged · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > CARGO DOOR FWD ROLLER TRACK AT FS 574.00 AND STR 12L TO STR 13L HAS WEAR DAMAGE MEASURING.200"L X.200"W X.020"D (P1) ON UPPER SIDE AND.300"L X.200"W X.040"D (P2) ON LOWER SIDE. THE TRACK IS MACHINED FROM 7075-T7451 PLATE WITH A LOCAL FLANGE THICKNESS OF
- [SDR A6WA202201318122](https://openairdocs.org/sdr/A6WA202201318122.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage, Door Hinge
  > R/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38.
- [SDR A6WA202201318123](https://openairdocs.org/sdr/A6WA202201318123.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage, Door Hinge
  > R/H SIDEWALL SEAT TRACKS FROM FS 349.00 TO FS 409+128 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS349 TO FS 409+16 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. R/H SEAT TR
- [SDR A6WA202201318121](https://openairdocs.org/sdr/A6WA202201318121.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > L/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38.
- [SDR A6WA202201318124](https://openairdocs.org/sdr/A6WA202201318124.md): None · corroded · Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)
  > AFT LAVATORY SERVICE DOOR LOWER HINGE HAS CORROSION. REMOVED CORROSION AT AFT LAVATORY SERVICE DOOR LOWER HINGE BRACKET IAW CRJ200 SRM 51-12-00 REV 38. EVALUATED CORROSION REMOVAL ON AFT LAVATORY SERVICE DOOR HINGE BRACKET AND FOUND NOT WITHIN ALLOWABLE LIM
- [SDR A6WA202111107957](https://openairdocs.org/sdr/A6WA202111107957.md): Control Unit · failed · Nov 10, 2021 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CLIMBING THRU FLIGHT LEVEL 180 RECEIVED FLAP FAIL MSG CW QRH LANDED AT FLAP ZERO DEG. SMOOTH LANDING MAX BTMS 4. PERFORMED FLAP RESET PROCEEDURE IAW AWAC SUP 98-018I BOX 12 FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CON
- [SDR A6WA202109107875](https://openairdocs.org/sdr/A6WA202109107875.md): Water Separator · odor · Sep 9, 2021 · N433AW · Cndair CL6002B19 · Humidity Control System
  > HAZE/SMOKE IN CABIN ON INSPECTION RT PACK 120C. UNABLE TO COOL IN MANUAL OR AUTO MODE. LT PACK IS OPERATING NORMALLY. BOTH PACKS WERE RUNNING OFF OF APU AIR. ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 310433 WC 3,4,5 FOR R&R OF LH ACM IN COMPLIANCE OF AW
- [SDR A6WA202011307429](https://openairdocs.org/sdr/A6WA202011307429.md): Bpsu · malfunctioned · Nov 24, 2020 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO IN CRUISE. ALT 14K FT PERFORMED QRH UNEVENTFUL LANDING. PERFORMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12 FLAPS RESET. PLACRDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FLAP BPSU, PER AMM 2
- [SDR A6WA2020021347173](https://openairdocs.org/sdr/A6WA2020021347173.md): Control Cable · damaged · Jan 30, 2020 · N433AW · Cndair CL6002B19 · Aileron Control System
  > OUTBOARD FUSELAGE AILERON CIRCUIT CABLE FOUND DAMAGED AT QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEFT HAND OUTBOARD FUSELAGE CABLE REF. CRJ-200 AMM 27-00-00 AND 27-11-00 REV. 60
- [SDR A6WA2020021247163](https://openairdocs.org/sdr/A6WA2020021247163.md): Skin · damaged · Jan 28, 2020 · N433AW · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 HAS A SCRATCH INTO METAL. AIRCRAFT REMOVED FROM SERVICE BLENDED SCRATCH ON L/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 BLEND MEASUREMENTS ARE 1.0"L X.040"W X.006"D, NO CRACKS NOTED AT THIS TIM
- [SDR A6WA202047171](https://openairdocs.org/sdr/A6WA202047171.md): Control Cable · damaged · Jan 27, 2020 · N433AW · Cndair CL6002B19 · Aileron Control System
  > RIGHT HAND OUTBOARD AILERON FUSELAGE CABLE FRAYED AT RIGHT HAND QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RIGHT HAND OUTBOARD AILERON FUSELAGE CABLE REF. CRJ-200 AMM 27-11-00 REV. 60
- [SDR A6WA2020021247165](https://openairdocs.org/sdr/A6WA2020021247165.md): Fitting · gouged · Jan 26, 2020 · N433AW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > L/H WING AFT WING TO FUSELAGE FITTINGS (UPPER & LOWER) HAVE TOOLING MARKS. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGE TO SMOOTH CONTOUR ON THE L/H WINGBOX TO FUSELAGE MACHINED FRAME AT FS 473.15 BLEND DIMENSIONS FOUND TO BE.500"L X.200"W X.043"D, NDT
- [SDR A6WA202021247164](https://openairdocs.org/sdr/A6WA202021247164.md): Hinge · gouged · Jan 25, 2020 · N433AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > ENTRY DOOR HINGE ON DOOR SIDE HAS MULTIPLE LUGS WITH WEAR. AIRCRAFT REMOVED FROM SERVICE LUG #26 BLENDED BELOW.100" LIMIT REFERENCE REO REF REO 601R-52-11-1347 REV C DTD 2017-08-02. DOOR HINGE LUG BLENDED TO.094" PERFORMED A SMOOTH CONTOUR OF 5:1 PERFORME
- [SDR A6WA2019112147026](https://openairdocs.org/sdr/A6WA2019112147026.md): Pressure Switch · malfunctioned · Nov 19, 2019 · N433AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > 3158 - L WING ANTI ICE CAUTION MESSAGE IN FLIGHT. C/W QRH MESSAGE CLEARED AND LEFT ICING CONDITIONS MESSAGE OCCURED BETWEEN CLIMBOUT AND CRUISE WITH WING ANTI ICE SELECTED ON. L WING SHOWED YELLOW ON SYNOPTIC MESSAGE CLEARED WHEN 14TH STAGE ISOL VALVE OPENED
- [SDR A6WA2019083046822](https://openairdocs.org/sdr/A6WA2019083046822.md): Landing Gear · malfunctioned · Aug 28, 2019 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKE-OFF, RECEIVED WARNING FOR GEAR DISAGREE. NOSE WHEEL WAS SHOWING YELLOW BOX, THEN UP 2 TIMES. ON EXTENSION, NOSE GEAR TOOK LONGER TO EXTEND WITH EXTRA NOISES FROM GEAR DURING EXTENSION. HYDRAULIC SYSTEMS SHOW NORMAL. CREW REPORTED VIA ACARS THA
- [SDR A6WA201908146792](https://openairdocs.org/sdr/A6WA201908146792.md): Warning Message · illuminated · Aug 12, 2019 · N433AW · Cndair CL6002B19 · Engine Thrust Reverser
  > R TR UNLOCK (C) IN FLIGHT AT 29,000FT 290 KT AMBER REV ICON. T/R APPEARS PHYSICALLY STOWED. EMER STOW PRESSED MSG REMAINED. DURING THE CRUISE, THE FLIGHT CREW RECEIVED A THRUST REVERSER UNLOCKED CAUTION MESSAGE. AFTER COORDINATING WITH DISPATCH AND WORKING TH
- [SDR A6WA2019053046640](https://openairdocs.org/sdr/A6WA2019053046640.md): Warning System · false activation · May 30, 2019 · N433AW · Cndair CL6002B19 · Engine Thrust Reverser
  > 4804 RT REV UNLCKEDE CAUTION MSG ILLUMINATED IN FLT. CW QRH MSG DID NOT CLEAR. DIVERTED TO DAY. REV ICON IN RT N1 IND. MSGS CLEARED ON ENGINE SHUTDOWN. RT TR APPEARS TO BE STOWED.
- [SDR A6WA2018032645731](https://openairdocs.org/sdr/A6WA2018032645731.md): Pseu · faulted · Mar 25, 2018 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > DURING CRUISE, RECEIVED A PROXIMITY SYS CHANNEL CAUTION MESSAGE. COMPLIED WITH QRH. MANUAL GEAR EXTENSION, NWS SELECTED OFF, LANDED WITHOUT ISSUE, TOWED OFF RUNWAY TO THE GATE. PSEU FAULTED, REPLACE PSEU
- [SDR A6WA201845544](https://openairdocs.org/sdr/A6WA201845544.md): Frame · corroded · Jan 5, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAMES 333 BETWEEN STR'S 25R AND 25L CORRODED. REPLACED
- [SDR A6WA2018010445536](https://openairdocs.org/sdr/A6WA2018010445536.md): Structure · dented · Jan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, Structure
  > STRUCTURE DENTED BETWEEN BS 589 AND 604. REPAIRED THE STRUCTURE.
- [SDR A6WA2018010445538](https://openairdocs.org/sdr/A6WA2018010445538.md): Floor Support · corroded · Jan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN CABIN LEFT FLOOR SUPPORT IN PAX DOOR CORRODED. REPLACED THE FLOOR SUPPORT
- [SDR A6WA2018010445537](https://openairdocs.org/sdr/A6WA2018010445537.md): Frame · corroded · Jan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, Frame
  > E&E BAY FRAME BS 349, STRINER 25L TO 25R CORRODED. REPLACED THE FRAME.
- [SDR A6WA2017010245531](https://openairdocs.org/sdr/A6WA2017010245531.md): Vane · chafed · Dec 30, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE IS CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANE
- [SDR A6WA2017010245530](https://openairdocs.org/sdr/A6WA2017010245530.md): Rib · damaged · Dec 30, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge Flaps
  > ON REMOVAL OF THE LT WING FLAP VANE INBD LE, FOUND DAMAGED FASTENER HOLES IN THE INBD RIB. REPLACED THE RIB.
- [SDR A6WA2017010245532](https://openairdocs.org/sdr/A6WA2017010245532.md): Attach Fitting · cracked · Dec 30, 2017 · N433AW · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > NR 1 PYLON LE ACCESS ATTACH FLANGE IS CRACKED ON THE LOWER PYLON.
- [SDR A6WA2017010245525](https://openairdocs.org/sdr/A6WA2017010245525.md): Frame · cracked · Dec 29, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 605 ATTACH FLANGES CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.
- [SDR A6WA2017010245527](https://openairdocs.org/sdr/A6WA2017010245527.md): Floor Support · corroded · Dec 29, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CABIN FLOOR SUPPORT BS 349 - 409, LBL 42-46 CORRODED. REPAIRED THE FLOOR SUPPORT
- [SDR A6WA2017010245526](https://openairdocs.org/sdr/A6WA2017010245526.md): Intercostal · corroded · Dec 28, 2017 · N433AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD 7 CORRODED. REPLACED THE INTERCOSTAL.
- [SDR A6WA201745514](https://openairdocs.org/sdr/A6WA201745514.md): Skin · cracked · Dec 28, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CRACKED SKIN ON THE LT LOWER NOSE HYD COMPARTMENT AFT UPPER LATCH CUT OUT.
- [SDR A6WA201745512](https://openairdocs.org/sdr/A6WA201745512.md): Skin · damaged · Dec 27, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER SURFACE SKIN NICKED.
- [SDR A6WA201745506](https://openairdocs.org/sdr/A6WA201745506.md): Skin · corroded · Dec 26, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP INBD LOWER SKIN PANEL PITTED.
- [SDR A6WA2017010245509](https://openairdocs.org/sdr/A6WA2017010245509.md): Frame · cracked · Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 718 FRAME FLANGE CRACKED. REPAIRED THE FRAME.
- [SDR A6WA2017010245507](https://openairdocs.org/sdr/A6WA2017010245507.md): Structure · corroded · Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN CABIN, BS 343, LBL 39 HINGE CUTOUR IS CORRODED. REPLACED THE STRUCTURE.
- [SDR A6WA2017010245508](https://openairdocs.org/sdr/A6WA2017010245508.md): Structure · corroded · Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Structure
  > MAIN CABIN, BS 316, LBL 39 HINGE CUTOUT IS CORRODED. REPLACED THE STRUCTURE.
- [SDR A6WA2017010245502](https://openairdocs.org/sdr/A6WA2017010245502.md): Fastener · missing · Dec 23, 2017 · N433AW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT UPPER PRESSURE FLOOR SKIN IS MISSING 7 RIVETS FROM BS 513 - 559 ON TOP OF RBL 36, IN THE CABIN.
- [SDR A6WA2017010245511](https://openairdocs.org/sdr/A6WA2017010245511.md): Stringer Clip · cracked · Dec 22, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 280 STRINGER 3L CRACKED. REPLACED THE STRINGER CLIP.
- [SDR A6WA201745499](https://openairdocs.org/sdr/A6WA201745499.md): Angle · corroded · Dec 21, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR STRUCTURE ANGLE AT LBL43 IS CORRODED FROM FS409+128 TO FS559.

Next page: https://openairdocs.org/aircraft/N433AW/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 = 'N433AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N433AW/reports

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