N459AW

Service difficulty reports · 216

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 = 'N459AW' 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 A6WA202608098906Engine · faultedABORTED 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 SERAug 9, 2026 · N459AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA202607128900Heat Exchanger · faultedDURING 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 Jul 11, 2026 · N459AW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR A6WA202407168779Frame · damagedCORROSION 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 --.Jul 16, 2024 · N459AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA202309288656Shutoff Valve · failedLEFT 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. AIRCRAFTSep 28, 2023 · N459AW · Cndair CL6002B19 · Pneumatic SystemSDR A6WA202210258419Drag Angle · crackedPASSENGER 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 DATEOct 25, 2022 · N459AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202210258420Bracket · corrodedPASSENGER 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 AREAOct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR A6WA202210258417Skin · dentedRIGHT 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 OPOct 25, 2022 · N459AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA202210258416Anchor Fitting · corrodedPASSENGER 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.Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA202210258413Fitting · chafedLEFT 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 AREASOct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage, Wing Attach FittingsSDR A6WA202210258412Arm · chafedPASSENGER 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, 51-2Oct 25, 2022 · N459AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202210258400Cover Plate · corrodedSERVICE 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.Oct 25, 2022 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202112108021Control Panel · false activationRECIEVED 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 Dec 9, 2021 · N459AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA202104027734Servo · malfunctionedON 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 APPEApr 2, 2021 · N459AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA202102087619Pressure Deck · corrodedPRESSURE 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: 60Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102087618Pressure Deck · corrodedPRESSURE 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 NOTJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102087617Pressure Deck · corrodedPRESSURE 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 NJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102087625Bulkhead Web · crackedTHERE 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 LENGJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202102087616Pressure Deck · corrodedPRESSURE 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 INDICAIJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102057606Pressure Panel · corrodedPRESSURE 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 Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057602Floor Panel · corrodedPRESSURE 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-53-41-6Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057600Floor Panel · corrodedPRESSURE 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-53-41-666Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057608Floor Panel · corrodedPRESSURE 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-Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057607Floor Panel · corrodedPRESSURE 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), ISJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057604Floor Panel · corrodedPRESSURE 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,Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057603Floor Panel · corrodedPRESSURE 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-53-41-6Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057605Floor Panel · corrodedPRESSURE 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-53-41-6Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102057601Floor Panel · corrodedPRESSURE 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 Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202102047585Pressure Deck · corrodedPRESSURE 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 DAJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047580Pressure Deck · corrodedPRESSURE 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 BOMBJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047584Pressure Deck · corrodedPRESSURE 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 DAJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047581Pressure Deck · corrodedPRESSURE 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 BOMBAJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047582Pressure Deck · corrodedPRESSURE 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 BOJan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047598Pressure Deck · corrodedPRESSURE 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: Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047583Pressure Deck · corrodedPRESSURE 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: 1Jan 31, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102087620Skin · dentedOUTWARD 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 533818Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202102087623Skin · dentedOUTWARD 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.Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202102087622Skin · dentedDENTS 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.Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202102087624Skin · dentedOUTWARD 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 Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202102057609Skin Panel · dentedOUTWARD 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: 0036003Jan 29, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102087612Bulkhead Web · crackedAFT 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 1.7Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202102047596Floor Support · corrodedPRESSURE 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 DATEJan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047597Floor Support · corrodedPRESSURE 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, REFJan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047595Floor Support · corrodedPRESSURE 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 DATEJan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047586Pressure Deck · corrodedPRESSURE 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 DATJan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202102047593Floor Support · corrodedPRESSURE 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: Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047587Floor Support · corrodedPRESSURE 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-Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047589Floor Support · corrodedPRESSURE 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 XJan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047588Floor Support · corrodedPRESSURE 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¿½Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047594Floor Support · corrodedPRESSURE 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-53-4Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202102047591Floor Support · corrodedPRESSURE 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:Jan 28, 2021 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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