N437AW

Service difficulty reports · 234

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 = 'N437AW' 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 A6WA202406038759Ecu · unknownRECEIVED FLAP FAIL CAUTION MSG FLAPS WERE AT 0, AIRCRAFT REMOVED FROM SERVICE. R&R FECU IAW AMM 27-51 OPS CHECK GOODJun 3, 2024 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202406028757Control Unit · faultedFLAP FAIL AT FL190. RAN QRH PROCEDURE. AND MSG REMAINED. PREFOREMD FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE REF LP 353462-1, R&R OF FECU. OPS CHECK GOOD. REMOVED PLACARD AND FROM MJun 2, 2024 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202311138670Unknown · unknownAFTER T/O OUT OF ORD, HEARD LOUD NOISE FROM NOSE OF AIRCRAFT. RH SIDE. ******AIRCRAFT REMOVED FROM SERVICE********* FOUND CREW O2 SERVICING DOOR OPEN ON ARRIVAL. VISUALLY INSPECTED DOOR AND LATCHES, NO DEFECTS AT THIS TIME. DOOR SECURES CLOSED.Nov 13, 2023 · N437AW · Cndair CL6002B19 · Accessory Compartment DoorsSDR A6WA202308208648Unknown · unknownON CLIMBOUT, RECEIVED FUEL IMBALANCED CAUTION MSG WITH LH QTY EXCEEDING RH QTY BY 800+LBS AUTO CROSSFLOW WOULD NOT COMMENCE INITIALLY, BUT LATER WORKED NORMAL RETURNED AC TO A BALANCED CONDITION. SINGLE ENGINE TAXI PRIOR TO TAKEOFF ON RH ENGINE WITH LH BOOST PAug 20, 2023 · N437AW · Cndair CL6002B19 · Aircraft Fuel SystemSDR A6WA202307158641Unknown · unknownON DEPARTURE UPON SELECTING GEAR UP RECIEVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MSGS C/W QRH EXTENDED GEAR GEAR MSGS WENT AWAY AIRCRAFT REMOVED FROM SERVICE. INSTALLED NOSE AND MAIN GEAR LOCK PINS PER AMM SUP. 11-054A FOR M ACTION OF MEL 32-30-01. SEE Jul 15, 2023 · N437AW · Cndair CL6002B19 · Landing Gear SystemSDR A6WA202204068165Bulkhead · noneREAR PRESSURE BULKHEAD WEB REQUIRES MODIFICATION PER E17/003/453 ****AIRCRAFT REMOVED FROM SERVICE**** MODIFIED THE REAR PRESSURE BULKHEAD WEB FS 621.00 IAW GREO 601-53-61-1240 REV DApr 6, 2022 · N437AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA202204068166Bulkhead · gougedBULKHEAD Z-MEMBER AT FS 621.00, CENTER, SHOWS DEEP GAUGE LOCATED AT THE TOP END. ****AIRCRAFT REMOVED FROM SERVICE**** REPAIRED BULKHEAD AFT VERTICAL STIFFENER AT FS 621.00 IAW EA# AWAC-CRJ253-01806Apr 6, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202204058162Stiffener · crackedANGLE STIFFENER AT FS 516, ON RH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON RH BL 45.00 IAW ED# AWAC-CRJ 253-01816Apr 5, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202204058163Stiffener · crackedANGLE STIFFENER AT FS 516, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817Apr 5, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202105127774Bpsu · warning messageFLAPS FAIL CAUTION ON TAKEOFF, PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I BOX 12 FLAP RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FOUND RT WING BRAKE AND POSITION SENSOR OUT OF RIG, AND RT WING POSITION 10 FLEX DRIVE WORN, May 10, 2021 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202101287570Clamp · looseJUST AFTER VR RECEIVED WING OVERHEAT WARNING MESSAGE, FOLLOWED BY ANTI-ICE DUCT WARNING MESSAGE. CW QRH MESSAGES CLEARED. RETURNED TO MKE. 14TH STAGE SOVS AND WING AND COWL AI VALVES WERE ALL SELECED ON. THE 10TH STAGE SOVS WERE CLOSED AT THE TIME. QRH ACJan 27, 2021 · N437AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA202101227561Skin · corrodedUPPER FUSELAGE TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DAMAGE ON TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L, P(1) 1.0L X 0.70W, P(2) 1.2L X 0.60W, P(3) 0.8L X 0.95W, P(4) 1.Jan 20, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202101257564Flange · gougedFUEL PRESSURE BOX AFT UPPER FLANGE, INBOARD AND OUTBOARD CORNERS GOUGED BLEND OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER RT FLANGE, 0.390 L X 0.120 W X 0.045 D, REF REO 601R-28-20-044, REV A DATE: 2021-01-21. BLENDED OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER LJan 16, 2021 · N437AW · Cndair CL6002B19 · Aircraft Fuel SystemSDR A6WA202101217559Skin · dentedUPPER SURFACE OF FUSELAGE HAS DENT AT FS 596.00, STGR 3R AND STGR 4R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 596.00, STGR 3R AND STGR 4R, 1.7 L X 1.6 W X 0.057 D, FOUND TO BE OUT OF LIMITS FOR SHARP CREASES. IAW CRJ200 SRM 53-00-31, (REV 38). AJan 16, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202101257565Access Panel · crackedVERTICAL STABILIZER PANEL 326AL AFT END BENT AND 1 EA DENT. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND MEASURED 1 (EA) DENT ON VERTICAL STABILIZER PANEL 326AL, 0.700 L X 0.500 W X 0.007 D, DENT FOUND TO BE WITHIN LIMITS, REF CRJ200 SRM 55-00-31 AND A.W. SUJan 15, 2021 · N437AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR A6WA202101217558Channel · corrodedLEFT HAND WING AFT CHANNEL AT WS 53.60 HAS POSSIBLE CORROSION AROUND UPPER LIGHTNING HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT LT WS.53.60, REF CRJ200 SRM 51-21-06, (REV 38). REWORKED AREA MEASURES 1.7L X 1.0W, REF CRJ200 SRM 51-21-06, (REV Jan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA202101217557Channel · corrodedRIGHT HAND WING AFT CHANNEL AT WS 53.60 HAS POSSIBLE CORROSION ON INBOARD SURFACE. AIRCRAFT REMOVED FROM SERVICE. REMOVED ANGLE SUPPORT AND NUTPLATE AT RT WS 53.60, REF CRJ200 SRM 51-42-21 AND CRJ 200 SRM 51-45-00, (REV.38). REMOVED CORROSION AT (2 EA) LOCAJan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA202101217556Channel · corrodedRIGHT HAND WING AFT CHANNEL AT WS 48.30 HAS POSSIBLE CORROSION ON INBOARD SURFACE. AIRCRAFT REMOVED FROM SERVICE. REMOVED NUTPLATE AT WS 48.30, REF CRJ200 SRM 51-45-00, (REV 38). REMOVED CORROSION AT (2 EA) LOCATIONS ON CHANNEL AT WS 48.30, REF CRJ200 SRM 5Jan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA202101087520Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 103.43 TO WL 114.93 LENGTH 11.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM. L=12.0'' W=1.8'', REF BOMBARDIER REO 601R-53-61-1285 REV E DATED 2016-10-31. PERFORMED HFEC INSPECTIJan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202101087516Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 126.88 TO WL 136.18 LENGTH 9.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=10.0'' W=1.85''. CUT OUT ON STRAP FOR REPAIR DIM L=7.0'' W=2.50'', REF BOMBARDIER REO 601R-53-61-128Jan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202101087519Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 131.98 TO WL 135.93 LENGTH 5.0'' RBL 18.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=4.9'' W=1.7''. CUT OUT ON STRAP FOR REPAIR DIM L=8.2'' W=2.5'', REF BOMBARDIER REO 601R-53-61-1285Jan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202101157546Floorbeam · corrodedFLOOR SUPPORT STRUCTURES AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42 HAND AND RT HAND BLENDED OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED RT HAND AND LT HAND FLOOR SUPPORT AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42, IAW CRJ 200 SRM 51 Jan 7, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101257566Angle · crackedFLOOR CROSS MEMBER GAPPED DUE TO FASTENER SWOLLEN BETWEEN STRUCTURES AT FUSELAGE STATION 559.00, LBL 8. AIRCRAFT REMOVED FROM SERVICE. UPON EVALUATION OF DAMAGE OF CROSS MEMBER AT FUSELAGE STATION 559.00, LBL 8. DAMAGE FOUND TO MEASURE 1.78 L X 0.620 W X 0.0Jan 2, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101157543Pressure Deck · corrodedPRESSURE FLOOR PANEL AT FS 484.00 +9, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 484.00 +9, LBL 429, LBL 42. REWORKED DIMENSIONS P(1) 0.5 L X 0.34 W, P(2) 1.0 L X 1.0 W, P(3) 0.59 L X 0.45 W, REF Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202012297521Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137530Floorbeam · 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. REWORKED DIMENSIONS 0.6 L X 0.3 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC INDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137526Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42. REWORKED DIMENSIONS 0.720 L X 0.420 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137535Floorbeam · 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. REWORKED DIMENSIONS 1.1 L X 0.7 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC PRDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137536Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 + 5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.070'' L X Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137537Floorbeam · 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. REWORKED DIMENSIONS P(1) 1.260 L X 0.640 W, P(2) 1.220 L X 0.710 W, REF REO 601R-53-41-666 REV (C) DADec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137533Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. BY BLENDING. BLENDED AREA MEASURED (P1) 2.330''L X 0.950''W (P2) 1.160''L X 0Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137523Floor Support · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 499.00 TO FS 513 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 499.00 TO FS 513 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 2.64''L X 1.11''W (P2) 1.Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202101137529Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 2.780''L X 1.530''W (P2) 0.920''L X 0.340''W TOOL USED DIGITAL CDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137534Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS. 513.00 TO FS. 513.00 + 5, RBL 36 TO RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00 +5, RBL 36 TO RBL 42. REWORKED DIMENSIONS P(1) 3.0 L X 1.0 W, P(2) 1.Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137540Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 439.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 439.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.00'' L X 0.720'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137539Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 484.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 484.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.250'' L X 0.800'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137525Floor Support · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 544.00 +11 TO FS 559 +2 AND LBL 41 TO LBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 544.00 +11 TO FS 559 + 2 AND LBL 41 TO LBL 43. BY BLENDING. BLENDED AREA MEASURED 2.480'' L X 0.Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202101137527Pressure Deck · corrodedCORROSION ON PRESSURE FLOOR PANEL AT NUT-PLATE FS 529.00 +10 AND LBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT NUT-PLATE FS 529.00 +10 AND LBL 43 BY BLENDING. BLENDED AREA MEASURED (P1) 1.530'' L X 0.630'' W (P2) 1.17Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202001137538Floor Support · corrodedPRESSURE FLOOR ANGLE AT FS 544 +11 TO FS 599, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544 +11 TO FS 599, LBL 42. REWORKED DIMENSIONS 2.7 L X 1.5 W, REF REO 601R-53-41-666. REV (C) DATED 2012-1Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202101137531Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.180'' L X 0Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137532Floor Support · corrodedPRESSURE FLOOR ANGLE AT FS 499.00 TO FS 513.00, RBL 36 TO RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 499.00 TO FS 513.00, RBL 36 TO RBL 42. REWORKED DIMENSIONS P(1) 1.7 L X 1.0 W, P(2) 2.0 L X 0.6Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202101137542Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 RBL 42.BY BLENDING. BLENDED AREA MEASURED (P1) 1.00''L X 1.700''W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/20Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101137541Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 +9 RBL 36 TO RBL 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 RBL 36 TO RBL 38 BY BLENDING. BLENDED AREA MEASURED (P1) 1.20''L X 0.796''W TOOL USED DIGITAL CALIPER SDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137524Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42. REWORKED DIMENSIONS P (1) 0.4 L X 2.7 W, P(2) 0.76 L X 0.5, W P(3) 0.4 L X 0.3Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137528Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38. REWORKED DIMENSIONS 1.45 L X 0.55 W, REF REO 601R-53-41-666 REV (C) DATED 20Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202001137521Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMDec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202101257563Pressure Blkhd · crackedAFT PRESSURE BULKHEAD FWD SURFACE FS 621.00, WL 130.93 TO WL 133.93 CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED SPRING BRACKET AND CARGO DOOR TRACK AT REPAIR AREA, REF CRJ200 SRM 51-40-11, (REV 38) AND BOMBARDIER REO 601R-53-61-1541 DATED: 2020-12-06, (RDec 1, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2019121847064Display · failedBOTH MFD FAILED AT 1000 FT AGL AIRCRAFT REMOVED FROM SERVICE REPLACED L MFD IAW AMM 31-61-01. OPS CK GOODDec 16, 2019 · N437AW · Cndair CL6002B19 · Central DisplaySDR A6WA2019082846809Warning Message · false activationTHE CREW RECEIVED AN OUTBOARD ANTI SKID MESSAGE UPON LOWERING LANDING GEAR. THE CREW OPTED TO DIVERT TO MKE FOR A LONGER RUNWAY. FLIGHT LANDED NORMALLY, NO EMERGENCY DECLARED AND NO ADVERSE REACTION FROM PASSENGERS. SYSTEM WAS SUCCESSFULLY RESET ONCE THE AIRCRAug 27, 2019 · N437AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA201904126552Warning Message · illuminatedINFLIGHT WITH WING ANTIICE ON IN NORMAL MODE, RECEIVED WING OVERHEAT WARNING. SUSPECT LEFT WING. C/W'D QRH & SELECTED WING ANTI-ICE OFF. MESSAGE CLEARED IMMEDIATELY. PER QRH, SELECTED WING ANTI-ICE TO STBY, THEN RECEIVED LEFT WING ANTI-ICE CAUTION & SYNOPTIC SApr 10, 2019 · N437AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
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