N426AW

Service difficulty reports · 233

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 = 'N426AW' 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 A6WA201312054440Skin · corrodedLEFT WING UPPER ACCESS PANEL 540CT LANDING HAS FRETTING CORROSION. BLEND TO ALLOWABLE LIMITS IAW REO 601R-57-21-2053.Dec 5, 2013 · N426AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201312054439Skin · corrodedLEFT WING UPPER ACCESS PANEL 540BT LANDING HAS FRETTING CORROSION. BLENDED TO ALLOWABLE LIMITS IAW REO 601R-57-21-2053.Dec 5, 2013 · N426AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201312054424Stop Fitting · chafedSERVICE DOOR STOPS AT FS 349, STRINGER 11R & 12R ARE CHAFED. BLENDED CHAFES TO ALLOWABLE DAMAGES IAW REO 601R-53-21-2484.Dec 5, 2013 · N426AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201312044445Spoiler · gougedLEFT WING FWD EDGE OF FLIGHT SPOILER INBD MOST END HAS GOUGE LOWER SIDE. BLENDED OUT GOUGES & FOUND TO BE WITHIN LIMITS IAW REO 601R-57-73-226.Dec 4, 2013 · N426AW · Cndair CL6002B19 · SpoilersSDR A6WA201312044444Spoiler · gougedLEFT WING OTBD MOST FWD EDGE OF FLIGHT SPOILER GOUGED FROM BENT UP SPRING SEAL. BLENDED OUT GOUGE & FOUND TO BE WITHIN LIMITS IAW REO 601R-57-73-226.Dec 4, 2013 · N426AW · Cndair CL6002B19 · SpoilersSDR A6WA201312044433Striker · gougedSERVICE DOOR CUT OUT LOWER STRIKER GOUGED ON TWO LOCATIONS. BLENDED GOUGES TWO LOCATIONS, OUT OF LIMITS IAW CRJ 200 SRM 52-00-00 & 51-12-00 REV D. NEW DEPRESSOR INSTALLED ONE EACH IAW CRJ 200 SRM 51-41-00.Dec 4, 2013 · N426AW · Cndair CL6002B19 · Service DoorsSDR A6WA201312044432Sill · corrodedSERVICE DOOR LOWER SILL CORRODED AROUND SPRICOT FITTING. R & R ANGLE IAW CRJ 200 SRM 51-42-01.Dec 4, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201312034437Skin · crackedRIGHT UPPER LE RUDDER SKIN CRACKED. R & R RUDDER SKIN.Dec 3, 2013 · N426AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA201312034436Hinge · damagedRUDDER CTR UPPER & LOWER HINGE BORE DIMENSIONS ARE OUT OF TOLERANCES. R & R HINGES.Dec 3, 2013 · N426AW · Cndair CL6002B19 · Rudder StructureSDR A6WA201312034434Floorbeam · corrodedSPAN WISE FLOOR SUPPORT BEAM AT FS 349 CORRODED AT RBL 27 TO 32 & BEAM HAS ONE DISCREPANT HOLE AT RBL 36. REMOVED CORROSION FOUND TO BE WITHIN SERVICEABLE LIMITS IAW CRJ 200 SRMS 51-21-06 & 53-21-15. REPAIRED DISCREPANT HOLE AT RBL 36 IAW STS EA 12-2013-567.Dec 3, 2013 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201312024449Bracket · crackedPASSENGER DOOR LOWER STEP SUPPORT SKIN FWD & AFT BRACKETS ARE CRACKED. REPAIRED IAW STS EA 15-2013-509, 11-27-2013.Dec 2, 2013 · N426AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201312024423Plate · dentedPASSENGER DOOR SEAL STRIKER PLATE HAS A DENT FS 349 LT STRINGER 6. REPAIR IAW REO 601R-53-22-033 REV C.Dec 2, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311294428Seat Track · corrodedFLOOR SEAT TRACK ON RBL 9 & LBL 9 CORRODED AT FS 379.00. BOTH FLOOR SEAT TRACKS RBL 9 & LBL 9 WERE 80% OUT OF LIMITS IAW CRJ 1200 SRM 53-21-49 FIG 10. RECEIVED & INSTALLED NEW SEAT TRACKS AT LBL 9 & RBL 9 IAW CRJ 200 AMM 53-01-11 & SRM 51-41-02.Nov 29, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311294418Sill · corrodedCARGO DOOR FLOOR SILL CORRODED AROUND NUTPLATES ON UPPER & LOWER SURFACE. REMOVED UNSERVICEABLE SECTION OF CARGO DOOR FLOOR SILL BETWEEN FS 580 & 621. FABRICATED & INSTALLED NEW SERVICEABLE SECTION OF CARGO DOOR FLOOR SILL IAW CRJ 200 SRM 51-24-21, 51-40-11, Nov 29, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311274448Retainer · corrodedAVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. R & R AVIONICS BAY DOOR SEAL RETAINER IAW CRJ 200 SRM 51-42-06.Nov 27, 2013 · N426AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA201311274447Mount Bracket · crackedRIGHT BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED & BROKEN. R & R BRACKET IAW CRJ 200 SRM 51-42-06.Nov 27, 2013 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201311274425Seat Track · corrodedCORROSION ON RT WALL SEAT TRACK AT FS 559+116 - 559+32. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-01-11.Nov 27, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311274417Plate · damagedFUEL PRESS BOX AFT PROTECTOR PLATE NUT HOLES DO NOT ALIGN. R & R IAW SRM.Nov 27, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311264442Bracket · crackedLEFT WING LE EDGE BRACKET CRACKED OTBD END AT WS 150. R & R DUPLICATED BRACKET.Nov 26, 2013 · N426AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201311264421Seat Track · corrodedCORROSION ON LT WALL SEAT TRACK AT FS 424. BLENDED CORROSION FOUND TO BE WITHIN LIMITS WITH MATERIAL LOSS OF .014 MAX ALLOWED IS .020 IAW CRJ 200 SRM 53-21-49.Nov 26, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311254435Fitting · crackedCARGO DOOR FWD STOP MOUNT LOWER CLIP IS CRACKED UNDER SILL. REMOVED UNSERVICEABLE CLIP, FABRICATED & INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 53-61-23,51-24-21, 51-40-11, 51-42-21.Nov 25, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311244438Mount Bracket · crackedLEFT ENG JET PIPE INBD & OTBD MOUNT NUTPLATE BRACKETS ARE CRACKED. R & R CRACKED NUTPLATE BRACKETS IAW CRJ 200 SRM 51-42-06.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201311244431Tie Down · corrodedEXFOLIATED CARGO TIE DOWN, REMOVED & REPLACED.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Cargo CompartmentsSDR A6WA201311244429Seat Track · corrodedCARGO FLOOR TRACK CORRODED ON RBL 9 AT FS 559+112 & FS 559+98. R & R FLOOR TRACK.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311244427Seat Track · corrodedCARGO FLOOR TRACKS CORRODED ON LBL 9 AT FS 559+112 & 559+98. R & R FLOOR TRACK.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311244426Seat Track · corrodedCORROSION ON SEAT TRACK RBL 9 AT MULTIPLE AREAS FS 449.85, FS 494, FS 513, FS 529, FS 544, FS 559 & FS 461.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201311244419Fitting · crackedFUSELAGE STATION 280 CLIP CRACKED AT LT STRINGER 3L. R & R IAW SRM.Nov 24, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311234430Fitting · crackedFUSELAGE STATION 280 AT RBL 9 CLIP CRACKED. REMOVED, FABRICATED & INSTALLED NEW CLIP.Nov 23, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311234416Fitting · crackedFUSELAGE STATION 280 LBL 9 CLIP CRACKED. REMOVED, FABRICATED & INSTALLED NEW CLIP.Nov 23, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201311224422Fitting · crackedCLIP AT FS 484 & RBL 27 IS CRACKED. R & R CLIP.Nov 22, 2013 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA20130418004Spring · failedDURING GEAR SWINGS FOR MLG CHANGES GEAR DISAGREE (NLG). REPLACED SPRING UNIT ASSY ON NLG MANUAL RELEASE MECHANISM REF AMM 32-34-15 OPS CHECKED OKJun 30, 2013 · N426AW · Bombdr CL6002D15 · Landing Gear Retraction/Extension SystemSDR A6WA201141152Control Unit · malfunctionedANTI-ICE DUCT WARNING MESSAGE IN FLT SELECTED WING ANTI-ICE OFF. RT WING ANTI-ICE OFF. RT WING DUCT IND RED IN CRUSE. TROUBLESHOT IAW FIM 36-20-00. VERIFIED NO LEAKS FROM RT PICCALO TUBE COUPLINGS. R & R RT BLEED LEAK CONTROL UNIT IAW AMM 36-21-10. OPS CDec 29, 2011 · N426AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA201240028Oxygen Mask · no testO2 MASKS INCLUDING LAV, DID NOT DEPLOY DURING AUTO OR MANUAL DEPLOYMENT TEST. FOUND FIG 3636 AT FS 409, WL 128.05, RBL 40.95 VERY LOOSE, CAUSING INTERMITTENT O2 MASK DEPLOY RETURN. TIGHTENED GS IAW ESPM 20-20-00.Dec 15, 2011 · N426AW · Cndair CL6002B19 · Passenger Oxygen SystemSDR A6WA201240029Rib · crackedRT BATT RIB CRACKED. COMPLIED WITH REO 601R-57-51-5663 ON RT CRACKED BATT RIB.Dec 3, 2011 · N426AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201240039Skin · chafedRT UPPER NOSE COWL T/E STRIP CHAFED. REPAIRED RT UPPER NOSE COWL T/E STRIP IAW CMM 71-14-01.Nov 30, 2011 · N426AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240053Handle · gougedSERVICE DOOR INNER HANDLE GOUGED. REPAIRED GOUGE IAW REO 601R-52-41-199.Nov 30, 2011 · N426AW · Cndair CL6002B19 · Service DoorsSDR A6WA201240033Floorbeam · corrodedFLOORBEAM CAP UNDER FLOORBOARD 281LLF IS CORRODED. REPAIRED FLOORBEAM CAP AT FS 615 & LBL 27.00 IAW REO 601R-53-61-4289.Nov 29, 2011 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201240035Angle · crackedRT PYLON PANEL 422BT AFT ANGLE CRACKED. REMOVED UNSERVICEABLE RT PYLON PANEL: 422BT AFT ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06.Nov 29, 2011 · N426AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201240048Attach Fitting · chafedRT MLG, GEAR DOOR ATTACH LUG CHAFED. BLENDED DAMAGED AREA ON RT MLG DOOR IAW REO 601R-52-92-43.Nov 29, 2011 · N426AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240045Hinge Fitting · chafedRT INBD FLAP INBD HINGE BOX TOP INBD LUG CHAFED. REPAIRED RT INBD FLAP INBD HINGE BOX LUG IAW REO 601R-57-21-1554.Nov 29, 2011 · N426AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240030Fairing · chafedLOWER FUSELAGE UNDER EACH OTBD ENDS OF MLG FWD FAIRING HAVE CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-880.Nov 28, 2011 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201240036Skin · gougedRT LOWER CORE COWL FWD INNER SKIN GOUGED 6 SPOTS. REPAIRED RT LOWER CORE COWL FWD INNER SKIN IAW REO 601R-71-12-4086.Nov 28, 2011 · N426AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240052Handle · crackedPAX DOOR OUTER HANDLE CRACKED. R & R WITH NEW HANDLE.Nov 28, 2011 · N426AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240049Bulkhead · damagedRT SIDE OF 280 BULKHEAD DAMAGED FROM GALLEY DOOR COMPLIED WITH REO 601R-53-11-1727 & 601R-53-11-2237.Nov 27, 2011 · N426AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240046Access Panel · corrodedINDICATION OF CORROSION INBD END OF C/O 650AB. REPAIRED IAW REO 601R-57-21-030.Nov 26, 2011 · N426AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201240034Angle · crackedRT & LT FS 625.00 OBLIQUE ANGLES CRACKED. REPAIRED L/R 625.00 OBLIQUE ANGLES BY INCORPORATING REO 601R-53-61-100 & 601R-53-61-422.Nov 23, 2011 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240051Handle · chafedPAX DOOR FWD PULL IN LEVER CHAFED, BLENDED IAW SRM 51-12-00 (TOOL 1671 CAL DUE4/12/12). REMOVED .030, WITHIN LIMITS IAW REO 601R-52-11-524, FIG 1. NDT INSPECTED, ALODINED, PRIMED, TOP COATED.Nov 22, 2011 · N426AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240050Striker · chafedPAX DOOR FWD & AFT STRIKER PLATES CHAFED. BLENDED FWD & AFT STRIKER PLATES IAW SRM 51-12-00. ORG THICKNESS .187 AFTER BLENDING FWD .155, AFT .163 WITHIN LIMITS IAW REO 601R-52-11-296. ALODINED, PRIMED, TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16.Nov 22, 2011 · N426AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240043Rib · crackedFOUND LT BATT RIB CRACKED. REPAIRED LT BATT RIB IAW REO601R-57-51-046.Nov 21, 2011 · N426AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240044Panel · chafedLT WING AILERON PANEL 559AB HAS AREAS OF CHAFING. BLENDED DAMAGED AREA IAW SRM 51-12-00. ORG THICKNESS .055 AFTER BLENDING MIN THICKNESS .048 TOOL REF 326 (CAL DUE 6/14/12. WITHIN LIMITS IAW REO 601R-57-60-020. NDT INSPECTION ALODINED, PRIMED, TOP COATED INov 21, 2011 · N426AW · Cndair CL6002B19 · Ailerons
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