# Service difficulty reports: N444ZW

A list on [N444ZW](https://openairdocs.org/aircraft/N444ZW.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 4 · 193 reports

- [SDR A6WA202608198908](https://openairdocs.org/sdr/A6WA202608198908.md): Antenna · faulted · Aug 19, 2026 · N444ZW · Cndair CL6002B19 · Ground Proximity System
  > ON T/O, RADAR ALTIMETER MALFUNCTIONED READING 1000FT WHILE A/C WAS CLIMBING 2200 AGL RECEIVED TERRAIN GPWS AURAL ON APPROACH TO AEX RAD ALT ( CONT BLOCK 3) WAS INTERMITTENTLY BOUNCING FROM TRUE ALT TO ERRONEOUS READINGS ABOUT 800 AGL NO GPWS AURAL'S AIRCRAFT
- [SDR A6WA202501228854](https://openairdocs.org/sdr/A6WA202501228854.md): Stiffener · melted · Jan 22, 2025 · N444ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > REQUEST INSPECTION FOR SHORTED GROUND POWER RECEPTACLE. AC GROUND POWER AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FND A/C RECEPT AND SHIELD MELTED, RECEPT SUPPORT MEMBER & INTERCOSTAL HAS HEAT DAMAGE AND MELTED AREAS. FWD PRESS BULHEAD HAS APPROX 2"X 1
- [SDR A6WA202501018849](https://openairdocs.org/sdr/A6WA202501018849.md): Strut · discharged · Jan 1, 2025 · N444ZW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AFTER DEPARTURE AND SELECTING LANDING GEAR LEVER TO UP POSITION, RECEIVED NOSE DOOR OPEN WARNING AND NOSE STEERING INOP CAUTION, WOW INPUT CAUTION AND WOW OUTPUT STATUS. C/W QRH. NLG INDICATING DOWN AND LOCK AND LT AND RT MLG INDICATED UP AND LOCKED. AIRCRA
- [SDR A6WA202406148766](https://openairdocs.org/sdr/A6WA202406148766.md): Warning Message · false activation · Jun 14, 2024 · N444ZW · Cndair CL6002B19 · Hydraulic System, Main
  > 6171 - SHORTLY AFTER TAKEOFF HYD 3 LOW PRESSURE CAUTION MESSAGE. C/W QRH MESSAGE CLEARED. AIRCRAFT REMOVED FROM SERVICE. PER OPS CK SYS 3A AND 3B PER AMM 29-12-03 OPS CK GOOD AT THIS TIME
- [SDR A6WA202405238752](https://openairdocs.org/sdr/A6WA202405238752.md): Bracket · corroded · May 23, 2024 · N444ZW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > CORROSION ON BRACKET AT WS 48.30 AT LH TE WING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET AT WS 48.30 AT LH TE WING REF. CRJ-200 SRM 51-42-06 AND 51-42-20 REV. 39. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED UNDER AERSALE WORK ORDER
- [SDR A6WA202405158749](https://openairdocs.org/sdr/A6WA202405158749.md): Bracket · corroded · May 15, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > POSSIBLE CORROSION ON ENTRY DOOR SILL AT FS310.00 TO FS349.00 LBL 40 TO 44. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FWD & AFT BRACKETS WITH P/N 601R31527-217 & FABRICATED NEW CLEAT WITH P/N 601R31527-176, ON SURROUND STRUCTURE AT PAX DOOR I.A.W.
- [SDR A6WA202405068741](https://openairdocs.org/sdr/A6WA202405068741.md): Floor Support · corroded · May 6, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLA
- [SDR A6WA202404258736](https://openairdocs.org/sdr/A6WA202404258736.md): Brace · cracked · Apr 25, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39
- [SDR A6WA202404308736](https://openairdocs.org/sdr/A6WA202404308736.md): Bracket · cracked · Apr 25, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39
- [SDR A6WA202401288707](https://openairdocs.org/sdr/A6WA202401288707.md): Unknown · smoke · Jan 28, 2024 · N444ZW · Cndair CL6002B19 · Air Distribution System
  > ON ARRIVAL AT GATE, NOTICED SMOKE IN CABIN, SMELLS ELECTRICAL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PACK BURN OUT FOR CLEARING UNUSUAL ORDERS IAW AWA SUP 09-037E. NO DISCREPANCIES NOTED.
- [SDR A6WA202312088680](https://openairdocs.org/sdr/A6WA202312088680.md): Unknown · unknown · Dec 8, 2023 · N444ZW · Cndair CL6002B19 · AC Generator-Alternator
  > RECEIVED IDG 2 CAUTION MULTIPLE TIMES IN FLIGHT. DID NOT RUN QRH MESSAGE CLEARED BELOW 15KFT. R/R BROKEN PIN ON P22EZ IAW ESPM 20-16 OPS CHECK GOOD IAW AMM 24-11
- [SDR A6WA202311038667](https://openairdocs.org/sdr/A6WA202311038667.md): Unknown · unknown · Nov 3, 2023 · N444ZW · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > RECEIVED LT AOA HEAT AFTER TAKE-OFF THEN RECEIVED LT PITOT HEAT, LT STATIC HEAT AND PITOT BASE HEAT. PERFORMED QRH AND MESSAGE REMAINED. C/W FIM RESET. SYSTEM OPERATES NORMAL. *******AIRCRAFT REMOVED FROM SERVICE****** NOTED BY MAINTENANCE
- [SDR A6WA202206088189](https://openairdocs.org/sdr/A6WA202206088189.md): Oil System · warning message · Jun 8, 2022 · N444ZW · Cndair CL6002B19 · Engine Oil Cooler
  > AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE D
- [SDR A6WA202205268221](https://openairdocs.org/sdr/A6WA202205268221.md): Skin · dented · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > R/H AFT LOWER SKIN IS DENTED AND HAS SCRATCHED ON FS 589 - FS 605 AT S-24R TO S-25R. ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER TO REPAIR AREA ON AIRCRAFT SKIN EXTERIOR IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-1
- [SDR A6WA202205268214](https://openairdocs.org/sdr/A6WA202205268214.md): Bracket · cracked · May 26, 2022 · N444ZW · Cndair CL6002B19 · Engine Air Intake System
  > L/H #1 ENGINE BRACKET P/N:228-50020-805 CRACKED AT 7 O'CLOCK POSITION AND BRACKET P/N: 228-50020-161 CRACKED AT 11-12 O'CLOCK POSITON ON NOSE INLET ATTACH RING. L/H #1 ENGINE NOSE COWL ATTACH RING FLANGE HAS 2 EA ELONGATED HOLES AT 7 O'CLOCK POSITION AND BETW
- [SDR A6WA202205268213](https://openairdocs.org/sdr/A6WA202205268213.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Floor Panel
  > L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+128 LBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 364 TO FS409+128 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT
- [SDR A6WA202205268217](https://openairdocs.org/sdr/A6WA202205268217.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 RBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND RBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIR
- [SDR A6WA202205268212](https://openairdocs.org/sdr/A6WA202205268212.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Floor Panel
  > R/H SIDEWALL SEAT TRACK FROM FS 349 TO FS 409 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACK AT FS 349 TO FS 409 AND RBL 46 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOV
- [SDR A6WA202205268218](https://openairdocs.org/sdr/A6WA202205268218.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 LBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND LBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIR
- [SDR A6WA202205268211](https://openairdocs.org/sdr/A6WA202205268211.md): Seal · cracked · May 26, 2022 · N444ZW · Cndair CL6002B19 · Spoilers
  > R/H WING FLIGHT SPOILER AT WS 264 HAS A CRACKED SEAL P/N: 601R10226-130 JUST BENEATH FWD EDGE OF SPOILER ON WING. CRACK DIMENSIONS ARE 6.5"L X.050"W. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EAC
- [SDR A6WA202205268215](https://openairdocs.org/sdr/A6WA202205268215.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 LBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCR
- [SDR A6WA202205268220](https://openairdocs.org/sdr/A6WA202205268220.md): Strap · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32 AND RBL 27 TO RBL 36. ******************AIRCRAFT REMOVED FROM SERVICE********************** BLENDED 2 EACH AREAS ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32: (P1) = 4.5"L X 2.0"W X.019"
- [SDR A6WA202205268216](https://openairdocs.org/sdr/A6WA202205268216.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCR
- [SDR A6WA202205268219](https://openairdocs.org/sdr/A6WA202205268219.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK FROM FS 364 TO FS 409 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 364 TO FS 409 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED
- [SDR A6WA202205268204](https://openairdocs.org/sdr/A6WA202205268204.md): Seat Track · corroded · May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDEWALL SEAT TRACK FROM FS 409+16 TO FS 409+112 HAS SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACK AT FS 409+16 TO FS 409+112 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOV
- [SDR A6WA202109177880](https://openairdocs.org/sdr/A6WA202109177880.md): None · none · Sep 16, 2021 · N444ZW · Cndair CL6002B19 · Pneumatic System
  > L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECE
- [SDR A6WA202109167880](https://openairdocs.org/sdr/A6WA202109167880.md): Warning Message · illuminated · Sep 16, 2021 · N444ZW · Cndair CL6002B19 · Engine Bleed Air System
  > L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECE
- [SDR A6WA202011167424](https://openairdocs.org/sdr/A6WA202011167424.md): Engine · overheated · Nov 15, 2020 · N444ZW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH 7000 RH ENG ITT 888 FLASH RED AT N1 87% AFTER APPROXIMATELY 10 SEC HEARD BANG AND SHUTTER. A/C YAWED AS RH, ENG POWER REDUCED. ACCOMPLISHED ENG SHUTDOWN. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H ENGINE S/N 872452 OFF WITH S/N 87230
- [SDR A6WA202010267360](https://openairdocs.org/sdr/A6WA202010267360.md): Skin · dented · Oct 25, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 3 EA PROTRUDING DENTS IN AFT FUSELAGE SKIN AT FS 682.00 BETWEEN STR 23R AND STR 24R. AIRCRAFT REMOVED FROM SERVICE. CUTOUT DAMAGE AREA AT FS 672 TO FS 682 BETWEEN STR 23R AND STR 24R, REF CRJ200 SRM 53-00-31 REV 38. PERFORMED HFEC INSPECTION AROUND CUTOUT A
- [SDR A6WA202010267353](https://openairdocs.org/sdr/A6WA202010267353.md): Floorbeam · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, TO LBL 37. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, LBL 37, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.851" W=0.080" D=0.005", ORIGINAL THICKNESS 0.08
- [SDR A6WA202010277366](https://openairdocs.org/sdr/A6WA202010277366.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 517, RBL 39, TO RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 517 RBL 39 TO RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=2.000" W=1.800" D=0.007" ORIGINAL THICKNESS 0.080
- [SDR A6WA202010277368](https://openairdocs.org/sdr/A6WA202010277368.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 447,AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 447 AND RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.920" W=1.400" D=0.007" ORIGINAL THICKNESS 0.080" REMAINING T
- [SDR A6WA202010277367](https://openairdocs.org/sdr/A6WA202010277367.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT FS 500 TO FS 513 RBL 47. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 500 TO FS 503 AND BL 47, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.6" L X 0.9" W X.006 D. ORIGINAL MATERIAL THICKNESS.0
- [SDR A6WA202010267350](https://openairdocs.org/sdr/A6WA202010267350.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT FS 484 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 484 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.96" L X 1.44" W X.005" D, ORIGINAL MATERIAL THICKNESS.080", REMAINING MA
- [SDR A6WA202010277370](https://openairdocs.org/sdr/A6WA202010277370.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL PANEL AT FS 441 & RBL 42 AROUND NUTPLATE HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X.003" D. PERFORMED HFEC, NO
- [SDR A6WA202010277365](https://openairdocs.org/sdr/A6WA202010277365.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 468, TO STATION 470, LBL 40. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 468 TO STATION 470, REF CRJ 200 SRM 53-41-06. MEASURE OF REWORK AREA L=3.500" W=I.400" D=0.006" ORIGINAL THICKNESS 0.080" REMAINING
- [SDR A6WA202010277369](https://openairdocs.org/sdr/A6WA202010277369.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT FS 448 TO FS 451 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 448 TO FS 451 RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.80" L X 0.95" W X.003" D. ORIGINAL MATERIAL THICKNE
- [SDR A6WA202010267358](https://openairdocs.org/sdr/A6WA202010267358.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.141" W=0.883" D=0.006", ORIGINAL THICKNES
- [SDR A6WA202010267355](https://openairdocs.org/sdr/A6WA202010267355.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 461.50 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.003", ORIGINAL THICKNESS 0.080", REMA
- [SDR A6WA202010267361](https://openairdocs.org/sdr/A6WA202010267361.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL PANEL STATION 467, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR SILL PANEL AT STATION 467, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.950" W=0.780" D=0.006", ORIGINAL THICKNESS 0.055", R
- [SDR A6WA202010267354](https://openairdocs.org/sdr/A6WA202010267354.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AT NUT PLATE ON FLOOR SILL PANEL FS 522 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FS 522 & RBL 42 AT NUT PLATE ON FLOOR SILL, REF CRJ 200 SRM 51-21-06. REWORKED ARE MEASURES.925" L X.912" W X.005" D. ORIGINAL MATERIAL THICKN
- [SDR A6WA202010267362](https://openairdocs.org/sdr/A6WA202010267362.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 508, LBL 36 TO 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 508, TO STATION 510, LBL 36, TO LBL 38, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.702" W=1.643" D=0.006", ORIGINAL THICKNESS 0.080"
- [SDR A6WA202010267359](https://openairdocs.org/sdr/A6WA202010267359.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 441 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X.003" D. PERFORMED HFEC NO INDIC
- [SDR A6WA202010267349](https://openairdocs.org/sdr/A6WA202010267349.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGEL AT STATION 438 TO STATION 439 RBL 40C. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT STATION 439, TO 439 & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.377" W=0.390" D=0.003", ORIGINAL THICK
- [SDR A6WA202010267351](https://openairdocs.org/sdr/A6WA202010267351.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.373" W=0.961" D=0.011", ORIGINAL THICKNESS IS 0.080". REMAINING
- [SDR A6WA202010267356](https://openairdocs.org/sdr/A6WA202010267356.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 541 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 541 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.267" L X 1.006" W X.004" D. PERFORMED HFEC NO INDIC
- [SDR A6WA202010267352](https://openairdocs.org/sdr/A6WA202010267352.md): Floor Support · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE FS 523 TO FS 530, RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 523 TO FS 530 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 2.5" L X 1.40" W X.006" D. ORIGINAL MATERIAL THICKNESS.08
- [SDR A6WA202010267357](https://openairdocs.org/sdr/A6WA202010267357.md): Floorbeam · corroded · Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR ANGLE AT STATION 468 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.013" ORIGINAL THICKNESS 0.080" REMAINING
- [SDR A6WA201846018](https://openairdocs.org/sdr/A6WA201846018.md): Bulkhead · punctured · Aug 29, 2018 · N444ZW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > APB FS 621 IS PUNCTURED JUST ABOVE FLOOR AT LBL 24.0 REPAIRED APB FS 621 JUST ABOVE FLOOR LBL 24 IAW BOMBARIDER REO# 601R-53-61-6673 REV --
- [SDR A6WA2018082946013](https://openairdocs.org/sdr/A6WA2018082946013.md): Bulkhead · cracked · Aug 28, 2018 · N444ZW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WAS CRACKED AT THE AFT CARGO DOOR TRACK, LBL 27.5, WL 125. REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541 REV-F.

Next page: https://openairdocs.org/aircraft/N444ZW/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 = 'N444ZW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N444ZW/reports

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