N444ZW

Service difficulty reports · 193

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR A6WA202608198908Antenna · faultedON 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 AIRCRAFTAug 19, 2026 · N444ZW · Cndair CL6002B19 · Ground Proximity SystemSDR A6WA202501228854Stiffener · meltedREQUEST 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 1Jan 22, 2025 · N444ZW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202501018849Strut · dischargedAFTER 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. AIRCRAJan 1, 2025 · N444ZW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA202406148766Warning Message · false activation6171 - 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 TIMEJun 14, 2024 · N444ZW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA202405238752Bracket · corrodedCORROSION 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 May 23, 2024 · N444ZW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA202405158749Bracket · corrodedPOSSIBLE 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.May 15, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202405068741Floor Support · corrodedCABIN 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 PLAMay 6, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202404258736Brace · crackedANGLE 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 39Apr 25, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202404308736Bracket · crackedANGLE 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 39Apr 25, 2024 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202401288707Unknown · smokeON 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.Jan 28, 2024 · N444ZW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA202312088680Unknown · unknownRECEIVED 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 24-11Dec 8, 2023 · N444ZW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA202311038667Unknown · unknownRECEIVED 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 MAINTENANCENov 3, 2023 · N444ZW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA202206088189Oil System · warning messageAT 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 DJun 8, 2022 · N444ZW · Cndair CL6002B19 · Engine Oil CoolerSDR A6WA202205268221Skin · dentedR/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 07-1May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202205268214Bracket · crackedL/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 BETWMay 26, 2022 · N444ZW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA202205268213Seat Track · corrodedL/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. *********AIRCRAFTMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202205268217Seat Track · corrodedR/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. *********AIRMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202205268212Seat Track · corrodedR/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 REMOVMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202205268218Seat Track · corrodedL/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. *********AIRMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202205268211Seal · crackedR/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 EACMay 26, 2022 · N444ZW · Cndair CL6002B19 · SpoilersSDR A6WA202205268215Seat Track · corrodedL/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. *********AIRCRMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202205268220Strap · corrodedCORROSION 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"May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA202205268216Seat Track · corrodedR/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. *********AIRCRMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202205268219Seat Track · corrodedR/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 May 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202205268204Seat Track · corrodedL/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 REMOVMay 26, 2022 · N444ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202109177880None · noneL 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 RECESep 16, 2021 · N444ZW · Cndair CL6002B19 · Pneumatic SystemSDR A6WA202109167880Warning Message · illuminatedL 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 RECESep 16, 2021 · N444ZW · Cndair CL6002B19 · Engine Bleed Air SystemSDR A6WA202011167424Engine · overheatedCLIMBING 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 87230Nov 15, 2020 · N444ZW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA202010267360Skin · dented3 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 AOct 25, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202010267353Floorbeam · corrodedCORROSION 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 0.08Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202010277366Floor Support · corrodedCORROSION 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 0.080Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010277368Floor Support · corrodedCORROSION 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 TOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010277367Floor Support · corrodedCORROSION 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 .0Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267350Floor Support · corrodedCORROSION 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 MAOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010277370Floor Support · corrodedFLOOR 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 Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010277365Floor Support · corrodedCORROSION 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" REMAININGOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010277369Floor Support · corrodedCORROSION 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 THICKNEOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267358Floor Support · corrodedCORROSION 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 THICKNESOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267355Floor Support · corrodedCORROSION 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", REMAOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267361Floor Support · corrodedCORROSION 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", ROct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267354Floor Support · corrodedCORROSION 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 THICKNOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267362Floor Support · corrodedCORROSION 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"Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267359Floor Support · corrodedFS 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 INDICOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267349Floor Support · corrodedCORROSION 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 THICKOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267351Floor Support · corrodedCORROSION 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 Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267356Floor Support · corrodedFS 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 INDICOct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267352Floor Support · corrodedCORROSION 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 .08Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202010267357Floorbeam · corrodedCORROSION 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 Oct 21, 2020 · N444ZW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201846018Bulkhead · puncturedAPB 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 --Aug 29, 2018 · N444ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018082946013Bulkhead · crackedAFT 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.Aug 28, 2018 · N444ZW · Cndair CL6002B19 · Fuselage Main, Bulkhead
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