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 A6WA201240599Door · chafedAFT GALLEY CLOSET DOOR CHAFED. REPAIRED IAW REO 601R-53-11-1727, REV E, DATE 01/14/2011.May 17, 2012 · N437AW · Cndair CL6002B19 · Fixed Inner DoorsSDR A6WA201240615Hinge · corrodedLAVATORY SERVICE DOOR LOWER HINGE AND HARDWARE CORRODED. REMOVED UNSERVICEABLE LAVATORY SERVICE DOOR LOWER HINGE AND HARDWARE AND REPLACED WITH SERVICEABLE HINGE IAW SRM 51-41-00.May 16, 2012 · N437AW · Cndair CL6002B19 · Accessory Compartment DoorsSDR A6WA201240609Structure · damagedCORE COWLING 435AT INBD L/E CORNER DAMAGED CUTOUT DAMAGED AREA OF 435AT CORE COWLING INBD L/E CORNER IAW CMM 71-12-01. SRS18 SEE FORM 412 FOR INSTALL, FAB OF DOUBLER AND FILLER.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240610Structure · gougedCORE COWL 435AB DAMAGE ON INNER CENTER STIFFENER. BLENDED GOUGE ON INNER CENTER HOT CHANNEL .050. REMOVED .008 REMAINING, .042 WITHIN LIMITS USING AMM 51-21-400 IAW CMM 71-12-01, SRM 51-21-11, 57-25-06, 51-25-26.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240608Structure · damagedCORE COWLING 435AB INBD L/E CORNER DAMAGED. CUTOUT DAMAGED CORNER OF 435AB CORE COWL INBD L/E IAW CMM 71-12-01. SEE FORM 412 FOR FAB AND INSTALL OF FILLER AND DOUBLER.May 15, 2012 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240607Angle · crackedLEFT LOWER OBLIBUE ANGLE ON 621 BULKHEAD AFT SIDE CRACKED. REMOVED UNSERVICEABLE LT LOWER OBLIQUE ANGLE ON 621 BULKHEAD AFT SIDE. INSTALLED SERVICEABLE LT LOWER OBLIQUE ANGLE.May 14, 2012 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240476Warning Message · false activationRECEIVED CAUTION MESSAGE ON TAKE-OFF, ANTI-SKID OTBD MESSAGE DID NOT REAPPEAR WITH LANDING GEAR DOWN SELECTED DOWN. PERFORMED ASCU BITE TEST. OPS CHECKED GOOD IAW AMM 32-44-06.Apr 22, 2012 · N437AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA201240409Pcu · malfunctionedAFTER TAKE OFF, RECEIVED WHITE SPOILERON FAULT "ON FLIGHT CONTROL, PAGE RT SPOILERON WAS WHITE" ON FINAL, RECEIVED RT SPOILERON CAUTION MESSAGE WITH WHITE T/B GROUND SPOILER FAULT AND OTBD SPOILERON FAULTS. REMOVED RT SPOILERON OTBD PCU IAW AMM 27-62-01. OPApr 7, 2012 · N437AW · Cndair CL6002B19 · Drag Control ActuatorSDR A6WA201040524Step · crackedPAX DOOR HAS CRACK IN RADIUS OF 3RD STEP FROM TOP AFT REPAIRED TOP AFT RADIUS CRACK ON 3RD STEP IAW REO 601R-52-11-702 ZONE REPAIR 4,2, AND 3.Jun 22, 2010 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040404Attach Angle · crackedFLOOR ATTACH ANGLE TO THE 280.0 BULKHEAD IS CRACKED JUST OTBD OF THE LBL 9. REPAIR FLOOR ATTACH ANGLE IAW REO 601R-53-11-136 REV A CUT OUT DAMAGE AND INSTALL SECTION OF FLOOR ANGLE.Jun 1, 2010 · N437AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040390Fairing · chafedHAS CHAFING DAMAGE AT AFT WING TO FUSELAGE PART UNDER AND FWD OF FLAP STUB FAIRING BLENDED OUT DAMAGE AREA AS REQUIRED IAW REO 601R-53-41-1219 REV N/C DAMAGE DID NOT EXCEED EXISTING DEPTH.May 25, 2010 · N437AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201040393Hinge · chafedPAX DOOR HINGE (PIANO) HAS CHAFING DAMAGE ON LUG PAX DOOR HINGE. REPAIRED IAW REO 601R-52-11-1347.May 25, 2010 · N437AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201040392Lever · chafedPAX DOOR FWD PULL IN LEVER CHAFED REPAIRED IAW REO 601R-52-11-524, REV A.May 25, 2010 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040391Fairing · chafedRT FUSELAGE HAS CHAFING DAMAGE AT AFT WING TO FUSELAGE POINT UNDER FLAP STUB FAIRING. BLENDED RT FUSELAGE AFT WING TO FUSELAGE DOES NOT EXCEED ALLOWABLE LIMITS IAW 601R-53-45-1215.May 25, 2010 · N437AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201040369Fitting · crackedBATHTUB FITTING AT FS 484, RBL 9 CRACKED. FLAGGED R & R WITH SERVICEABLE BATHTUB FITTING PN 600-31068-19 AT FS 484, RBL9 ALL WORK DONE IAW SRM 51-42-06, 51-42-21, 51-21-11.May 23, 2010 · N437AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040368Bulkhead · crackedFS 559, WEB HAS INDICATED CRACK BETWEEN RBL9 AND RBL18. REPAIRED FS 559 CRACK BETWEEN RBL9 AND RBL18 BY INCORPORATION OR REO 601R-53-41-260, REV D AND 601R-53-41-609, REV B. DEVIATION E ON LT AND RT SIDES BETWEEN RBL 27 AND LBL 27.May 23, 2010 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040374Drag Angle · crackedPAX DOOR FWD DRAG ANGLE CRACKED UNDER ASSIST CABLE PULLEY BRACKET SPLICED IN NEW DRAG ANGLE.May 22, 2010 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040373Angle · crackedCRACK ON ANGLE ON PANEL 422AT, BLENDED OUT CRACK ON PANEL 422AT IAW SRM 51-12-00.May 21, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040370Angle · crackedFLOOR ATTACH ANGLE ON THE 280.0 BULKHEAD IS CRACKED, 3RD RIVET OTBD OF RBL 9. REPAIRED FLOOR ATTACH ANGLE AT FS 280.0 BULKHEAD IAW REO 601R-53-11-136 REV A AND SRM 51-40-11, 51-24-36, 51-21-11, 51-25-06 AND 51-25-16, RBL 9.0.May 21, 2010 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040525Hinge · chafedPAX DOOR HINGE CHAFED.May 20, 2010 · N437AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201040371Sill · corrodedRT CARGO BAY FLOOR SILL CORRODED AROUND ANCHOR NUTS (NUT PLATES). CORROSION REMOVED IAW SRM 51-21-06.May 19, 2010 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040372Stiffener · chafedVERTICAL STIFFENER FOUND CHAFED AFT PRESSURE BULKHEAD BL 0. BLENDED CHAFED AREA IAW REO 601R-53-61-1523, REV: N/C AND 601R-53-61-3674, REV N/C FOUND WITHIN LIMITS FOR REO`S. APPLIED ALODINE, PRIMED, AND TOP COATED IAW SRM 51-21-11, 51-21-16, AND 51-25-06.May 17, 2010 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040362Bracket · chafedCHAFING FOUND ON BRACKET PN 601R10371-2, RT WING ROOT. R & R BRACKET.May 15, 2010 · N437AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201040361Strip · chafedRT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED, SHORTS IPS 71-14-01, FIG 1, ITEM 45. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-108 AT RT ENGINE UPPER NOSE COWL ALL WORK DONE IAW CMM 71-14-01, SRM 51-21-11, 51-25-06, 51-25-16.May 14, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040359Strip · chafedRT ENGINE LOWER NOSE COWL AFT EDGE STRAP IS CHAFED, SHORTS IPC 71-14-01, FIG 2, ITEM 105. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50081-108 AT RT ENGINE LOWER NOSE COWL WORN DOWN IAW SRM 51-21-11, 51-25-06, 57-25-18.May 14, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040356Separator · chafedDIVIDERS ON PANEL 422DB HAS CHAFING CONDITION. R & R 2 EA DIVIDER PANELS IAW SRM.May 13, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040358Separator · chafedDIVIDER PLATES ARE KNIFE EDGED AND CHAFED, R & R DIVIDER PLATES PN 601R37138-27 AND 601R37138-25 IAW SRM 51-42-06, 51-42-13 AND 51-40-11.May 13, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040363Skin · chafedLOWER L/E HAS EVIDENCE OF CHAFING REWORK CHAFING AREAS AS REQUIRE IAW REO 601R-57-60-020, REV N/C AND SRM 51-21-11, 51-25-06, 51-25-16.May 13, 2010 · N437AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040360Splice · chafedUPPER NOSE COWL AFT EDGE STRIP IS CHAFED, SHORTS IPC 71-14-01, FIG 1, ITEM 40. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-107 ALL WORN DOWN IAW CMM 71-14-01 AND SRM 51-21-11, 51-25-06, 51-25-16.May 13, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040364Rib · crackedBATT RIB CRACKED PN LT WW REPAIRED BATT RIB AT LT WW IAW REO 601R-57-51-046, REV B AND SRM 51-21-11, 51-25-06, 51-41-02 AND AMM 20-10-00.May 12, 2010 · N437AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040526Skin · debondedLT WING OTBD L/E OTBD INNER SKIN DISBONDED AND 2 SHEARED RIVET. BONDED INNER SKIN ON LT WING OTBD L/E TO L/E SKIN AND REMOVED 2 SHEARED RIVETS, INSTALLED 2 NEW RIVETS PRIMED ALL AREAS INVOLVED IN WORK.May 10, 2010 · N437AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940810Unknown · vibrationAFTER GEAR RETRACTION ON T/O, HEARD LOUD BANGING NOISE COMING FROM NOSE WHEEL AREA. SOUND LASTED 3 TO 5 MIN THEN EXTINGUISHED. DURING WHICH NOSE DOOR OPEN WARNING MSG WAS ON. INSP NOSE GEAR AREA, DOORS, NOSE GEAR, NO DAMAGE NOTED. INSP FUSELAGE, ENGS AND EDec 15, 2009 · N437AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA200940809Controller · malfunctionedAFTER TAKEOFF RECEIVED RT STATIC HEAT, RT PITOT HEAT, RT AOA HEAT, TAT HEAT. C/W`D QRH MSG`S PERSIST. C/W`D OPS TEST OF AIR DATA HEAT CONTROLLERS IAW AMM 30-31-15-710-801, ALL PROBES HEAT & NO CAS MSG`S. (K)Dec 11, 2009 · N437AW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA200840480Sensor · malfunctionedFLAP FAIL MESSAGE WHEN FLAPS SET TO 8 DEGREES ON APPROACH TO LGA. DIVERTED TO PHL, ZERO FLAP LANDING. REMOVED AND REPLACED RT BPSU LAW AMM 27-51-10. OPS CHECK AND RIG CHECK OF BPSU AND FLAPS ARE GOOD AT THIS TIME. (A)Jun 4, 2008 · N437AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200840423Flap · failedFLAPS FAILED AFTER TAKEOFF AT 12 DEGREES, PERFORMED QRH, RETURNED TO CMH. OPEN (A)May 15, 2008 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840422Flap · malfunctionedFLAP FAILURE AFTER TAKEOFF DURING RETRACTION FROM 20 DEGREES. FAILED AT 16 DEGREES. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. (S)May 14, 2008 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840396Ring · wornCORE COWL 445 CLOSURE RING WORN BEYOND LIMITS. CORE COWL 445AB CLOSURE RING REPLACES IAW 71-12-01-300-820-A01 REPAIR. (A)May 7, 2008 · N437AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA200840384Piccolo Tube · dentedRT WING INTERNAL OUTBOARD LEADING EDGE AT W/S 252, PICCOLLO TUBE DENTED (.300 X .200 X .040 DEEP). PICCOLLO TUBE REPLACED IAW AMM TASK 30-11-41-400-801. (A)May 6, 2008 · N437AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA200840383Strip · gougedLT ENGINE UPPER NOSE ACCESS COWL AFT EDGE STRIP GOUGE. LT UPPER ENGINE COWL, AFT EDGE STRIP REPLACED IAW CMM 71-14-01-300-814-A01.May 6, 2008 · N437AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA200840382Strip · chafedRT ENGINE NOSE ACCESS COWL (LOWER) TRAILING EDGE STRIP CHAFED BEYOND LIMIT. RT ENGINE NOSE ACCESS COWL (LOWER), NEW TRAILING EDGE STRIP INSTALLED IAW CMM 71-14-01-300-815-A01.May 6, 2008 · N437AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA200840381Angle · crackedANGLE CRACK ON ACCESS PANEL 422 BT. CRACKED ANGLE REPLACED ON ACCESS PANEL 422BT IAW SRM 51-42-06.May 5, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840397Sill · corrodedSERVICE DOOR LOWER SILL PLATE CORRODED OVER LIMITS. SERVICE DOOR LOWER SILL PLATE REPLACED IAW SRM 51-41-02. (A)May 4, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840392Intercostal · crackedCRACK EXISTS ON INTERCOSTAL FS 621 TO 625 STR R14. REPLACED IAW SRM 51-42-06. (A)May 2, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840391Intercostal · crackedCRACK EXISTS ON INTERCOSTAL FS 621 TO 625 LT. REPLACED IAW SRM 51-42-06. (A)May 2, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840387Structure · crackedREPAIR CRACK ON AFT OF PAX DOOR. REPAIR ON AFT SIDE OF PAX DOOR IAW REO 601R-52-11-279. (A)May 1, 2008 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840386Separator · crackedSEPARATOR CRACK ON ACCESS PANEL 422DB. NEW SEPARATOR INSTALL ON ACCESS PANEL 422DB IAW CRJ200 SRM 51-42-06. (A)May 1, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840378Drag Angle · crackedPAX DOOR AFT DRAG ANGLE FOUND CRACKED. PAX DOOR DRAG ANGLE REPAIRED IAW REO 601R-52-11-513.May 1, 2008 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840429Handle · corrodedCREW ESCAPE HATCH OUTSIDE HANDLE IS SEIZED AND CORRODED. CREW ESCAPE HATCH HANDLE REPLACED IAW CRJ 200 AMM 52-22-03-400-801 AND HARTWELL CMM 52-22-03. (A)Apr 30, 2008 · N437AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200840377Lens · erodedERROSION OF THE LT WING TIP POSITION LIGHT LENS. REPLACED LT WINGTIP POSITION LIGHT LENS IAW AMM 57-30-39-400-801 SUPP NR 07-009.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Exterior LightingSDR A6WA200840376Sill · corrodedCORROSION EXISTS ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45. CORROSION REMOVED ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45 IAW SRM 51-21-06.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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