N824AS, cancelled Nov 13, 2017

Service difficulty reports · 226

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 = 'N824AS' AND deregistration_id = 'N824AS-2017-11-13'
  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 SWIA201540909Skin · dentedLEFT INBD FLAP LOWER SKIN IS DENTED AT 2 LOCATIONS, APPROXIMATELY WS 56.30. AND WS64.30. REQUIRING SKIN REPLACEMENT. C-CHECK, RO 3/23/15, REPAIRED LT INBD FLAP LOWER INBD SKIN HALF FOR STS EA,ALL STEPS 1 THRU 7 COMPLIED WITH.THIS IS A PERMANENT REPAIR.Mar 11, 2015 · N824AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540913Floor Panel · corrodedRIGHT OTBD PRESSURE FLOOR PANEL FS 473.15 TO 559 RBL 43 HAS CORROSION AROUND FASTENER HOLES. C-CHECK RO 3/23/15, REPAIRED CORROSION DAMAGE ON RT OTBD PRESSURE FLOOR PANEL FS 473.15 TO FS 559.0 RBL 43. ORIGINAL THICKNESS .055", IN CHEM-MILL POSKET, REMAININMar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201540910Floor Panel · corrodedLEFT OTBD PESSURE FLOOR PANEL FS 484 TO 559 LBL43 HAS CORROSION AROUND FASTENER HOLES. C-CHECK RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT OTBD PRESSURE FLOOR PANEL FS 484.0 TO FS 559.0 LBL 43. ORIGINAL THICKNESS .055", IN CHEM-MILL POCKET, REMAINING THICKNMar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201540903Skin · crackedSUSPECTED CRACK IN LOWER FUSELAGE SKIN AT AFT LT CORNER OF NLG AFT DOOR CUT-OUT. C-CHECK, RO 3/23/15, REPAIRED CRACK IN LOWER FUSELAGE AT AFT LT CORNER OF NLG DOOR CUTOUT REF PRESSURE CHECK GOOD. COMPLIED WITH ST 51-900-1003.Mar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201540912Floor Support · corrodedLT SILL STRUCTURE FLOOR ANGLE FS 473.15 TO 513 HAS CORROSION. C-CHECK, RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT SILL STRUCTURE FLOOR ANGLE FS 473.15 TO FS 513.0 . ORIGINAL THICKNESS .080", REMAINING THICKNESS .074", MATERIAL LOSS .006", WITHIN LIMIT REF RMar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201540911Floor Support · corrodedLEFT SILL STRUCTURE FLOOR ANGLE FS 409+128 TO 473.15 HAS CORROSION. C-CHECK, RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT SILL STRUCTURE FLOOR ANGLE FS 409+128 TO FS 473.15. ORIGINAL THICKNESS .080", REMAINING THICKNESS .069", MATERIAL LOSS .011", WITHIN LIMIMar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201540902Seat Track · corrodedRT SEAT RAIL FS 349 TO 409+128, RBL 9 HAS CORROSION AND GOUGE DAMAGE. C-CHECK, RO 3/23, BLENDED GOUGE DAMAGE AT RBL 9, FS409+42 , IAW SRM, LOCATION, ORIGINAL WIDTH IS .420?, REMOVED MATERIAL IS .080"?, REMAINING WIDTH IS .500"?, SEAT TRACK RAIL IS OUT OF Mar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201540918Skin · corrodedCORROSION AROUND FASTENER ON FUSELAGE BELLY SKIN FS 559+16, STR 26R APPROXIMATELY AS MARKED, C-CHECK, RO 3/23/15. REMOVED CORROSION FROM EXTERIOR FUSLEAGE BELLY SKIN FS 559+16, STR 26R, AND BLENDED SMOOTH IAW STS EA. BEGINNING MATERIAL THICKNESS IN DAMAGE ARMar 2, 2015 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201540914Hinge · gougedRT OTBD FLAP AFT HINGE BOX-ATTACH FITTING AT WS 264.00 HAS 2 EA, GOUGES. C-CHECK, RO 3/23/15, BLENDED OUT GOUGES AND FOUND WITHIN LIMITS OF STS EA.Mar 1, 2015 · N824AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540908Skin · chafedLT AILERON LOWER L/E SKIN CHAFED INBD OF CENTER HINGES, C-CHECK, RO 3/23/15. COMPLIED WITH REPAIR OF THE LT AILERON LOWER L/E INBD OF THE CENTER HINGES REF REO.Mar 1, 2015 · N824AS · Cndair CL6002B19 · AileronsSDR SWIA201439264Charger · failedEMERGENCY LIGHTS STAY ILLUMINATED AT OVERWING EXITS. R & R THE AFT BATTERY CHARGER IN THE CABIN.Sep 10, 2014 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014051510493Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AFTER CHARGING, OPS CHECKED GOOD IAW AMM 33-51-00, ACFT OK FOR SERVICE.May 11, 2014 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014050910482Frame · crackedPAX DOOR FRAME CRACKED AT BS 338 TOP OF DOOR. REPAIRED IAW REO 601R-52-11-402 .May 2, 2014 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014050910481Door Frame · crackedPAX DOOR FRAME CRACKED AT BS 320.1, TOP OF DOOR. REPAIRED IAW 52-11-04-000-808 AND 52-11-04-000-810 AND SRM 51-42-13-00. COMPLIED WITH OPS TEST F/O ASD IAW AMM 52-11-00-710-801, OPS TESTED GOOD. MAJOR REPAIR.May 2, 2014 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014050910480Floor Support · crackedFLOOR SUPPORT CRACKED & CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21 AND REO: 601R-53-61-593.Apr 26, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014050910479Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN BS 559+112 TO 521 LT SIDE. FLOOR SUPPORT REPLACED IAW REO 601R-53-61-593.Apr 23, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014050910478Floor Support · corrodedLEFT CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 574 - 621, LBL 27 OTBD SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-21 AND 51-42-22.Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014050910477Floor Support · corrodedCARGO LT FLOOR SUPPORT HAS CORROSION BETWEEN BS 559+80-FS 559+96, LBL 47. REPAIRED IAW EC/TC REO 601R-53-00-526 AND REO 601R-53-00-526.Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014050910476Isolator · brokenFOUR ISOLATORS BROKEN ON FWD FACE OF FS 621 BULKHEAD IN CARGO BAY. REMOVED BROKEN ISOLATORS FROM MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA). INSTALLED NEW SERVICEABLE ISOLATORS ON MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA).Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014050910475Floor Support · crackedFS 484, FLOOR SUPPORT CRACKED AT RBL 27.0. REMOVED D & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-21.Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014050910474Floor Skin · crackedPRESSURE FLOOR SKIN CRACKED APPROX 3 INCH AT FS 460 BETWEEN BL 0 AND RBL 9. COMPLIED WITH REO:601R-53-41-1808.Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014050910473Rub Strip · wornVERTICAL STABILIZER LT UPPER VISOR ASSY FWD RUB STRIP IS WORN AND DETACHED. RECEIVED AND COMPLIED WITH ECTC OF REO 601R-52-11-2219 FOR DEVIATION OF GENERIC REO 601R-52-11-402. EC/TC REO 601R-52-11-2216 HAS BEEN COMPLETED AND ALL STEPS HAVE BEEN DOCUMENTED AApr 21, 2014 · N824AS · Cndair CL6002B19 · Vertical StabilizerSDR ASOA2013082308902Lamp · burned outLEFT NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Aug 19, 2013 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013062103862Fuse · blownNR 2 AND 4 CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE ON NR 4 BATTERY POWER SUPPLY IAW CMM 33-21-70. OPS CHECKED GOOD IAW AMM 33-51-00.Jun 17, 2013 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013062103861Lamp · burned outRIGHT REAR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.Jun 17, 2013 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013051703598Structure · crackedPAX DOOR HAS A CRACK. REPAIRED IAW REO 601R-52-11-1359-01.May 14, 2013 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013041203368Door · bindingPAX DOOR IS HARD TO OPEN , F/A CANNOT GET THE HANDLE TO STOW , .2500" GAP AT THE TOP OF THE DOOR. PREFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00, PRESSURIZED ACFT , OPS CHECKED GOOD.Apr 9, 2013 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013032503251Rib · crackedRT HORIZONTAL STAB RIB 9 IS CRACKED. REMOVED THE RT HORIZONTAL STAB RIB AND DRILLED NEW RIB AND TRANSFERED ALL ANGLES AND BRACKETS IAW SRM 51-42-13 AND IAW SRM 51-42-06. INSTALLED NEW RIB 9 IAW SRM 51-42-13 , 51-45-00.Mar 21, 2013 · N824AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR ASOA2013021203004Unknown · odorSTRONG BURNING ODOR THROUGH COCKPIT GASPERS. F/A CALLED AND REPORTED THE SAME. ELECTRICAL COMPONENT BURNING ODOR. F/A REPORTED NO SMOKE BUT ODOR WAS STRONG. HAD F/A PULL GALLEY C/B'S AND ODOR WENT AWAY AFTER 1-2 MINUTES. ( GALLEY HEATING SYSTEM: FAN ) EMEFeb 8, 2013 · N824AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA2012102902402Latch · jammedPASSENGER DOOR LATCH HARD TO CLOSE AND OPEN. LOWER LATCH ESPCIALLY. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-03. OPS CHECKED GOOD. SDR CLOSED.Oct 24, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012101202349Handle · inoperativePASSENGER DOOR WILL NOT OPEN FROM THE INSIDE OR OUTSIDE. R & R HANDLE. OPS CHECKED GOOD. ACFT OK FOR FURTHER SERVICE.Oct 10, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012091402217Door · lack of lubeMAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED PAX DOOR , OPS CHECKED GOOD IAW AMM 52-11-00.Sep 11, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081002054Counterbalance · out of adjustF/O UNABLE TO OPEN PAX DOOR ( DOORS AND OVERWING EMERGENCY EXITS ) ADJUSTED PAX DOOR COUNTERBALANCE IAW AMM 52-11-17, OPS CK GOOD DEFER CLEARED PLACARD REMOVED.Aug 7, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081002053Latch · contaminatedF/A UNABLE TO OPEN MAIN PAX DOOR. FOUND DEBRIS IN LATCH ON MECHANISM CLEANED OUT AND LUBRICATED IAW AMM 52-11-03. ALL ROLL FITTINGS ACFT OK FOR SERVICE.Aug 7, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012080302035Handle · lack of lubePAX OUTER HANDLE HARD TO PUSH OPEN. PAX OUTER HANDLE LUBRICATED IAW AMM 52-11-03. OPS CHECKED GOOD.Aug 1, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012072701996Handle · obstructedMAIN PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FOUND EXCESSIVE DEBRIS AND GREASE ON DOOR LOCKING HANDLE MECHANISM, CLEANED AND PERFORMED OPS TEST IAW AMM 52-11-00. OPS TESTED GOOD ACFT OK FOR SERVICE.Jul 24, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012070301854Floor Support · corrodedRT FLOOR SUPPORT BEHIND FS 349 IS CORRODED. INSTALLED NEW FLOOR SUPPORT SECTION IAW REO 601R-53-21-425.Jun 11, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012062001813Strap · corrodedSTRAP AT FS 559 AT RBL 36-45 CORRODED. APPLIED FINISH TO REWORKED AREA IAW SRM 51-21-11.Jun 11, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070301853Floorbeam · corrodedAFTER REMOVAL OF SERVICE DOOR SILL, FOUND CORROSION ON FS 349 FLOORBEAM LATERAL FRAME AT RBL 42. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06. CUT AWAY DAMAGE ON FLOORBEAM IAW REO 601R-53-21-2320, STEP 1 & 3. COMPLIED WITH STEP 2 OF REO 601R-53-21-2320 IAW NJun 7, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201778Seat Track · corrodedSEAT TRACK AT RBL 9.0 BETWEEN FS 559+4 - 559+86 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Jun 7, 2012 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201766Support Bracket · corrodedCORROSION ON UPPER AND LOWER SURFACE OF TOP FLANGE ON WINDSCREEN SUPPORT BRACKET. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06-00 & 51-42-21-00.Jun 4, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201765Light · brokenEMERGENCY EXIT LIGHT ASSY AT GALLEY/SERVICE DOOR BROKE. REMOVED UNSERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM TASK 25-31-01-000-802 SUBTASK 25-31-01-000-011. INSTALLED SERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM 25-31-01-400-802.Jun 4, 2012 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012071701910Sill · corrodedSERVICE DOOR SILL IS CORRODED BETWEEN FS 319-349. R & R SERVICE DOOR SILL IAW EO 600-53-0724.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201759Strap · corrodedSTRAP AT FS 559 RBL 36-45 CORRODED. BLEND CORROSION ON STRAP AT FS559.0 AT RBL 36-45 AND EVALUATE. BLENDED CORROSION IAW SRM 53-00-00, FIG 101. PERFORMED UT THICKNESS INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-41-1584.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201758Floorbeam · corrodedCARGO FLOORBEAM AT FS 349 BETWEEN LBL 27 - LBL 42 IS CORRODED ON UNDERSIDE. REPAIRED IAW SRM 51-42-06, 51-42-21.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201757Floorbeam · corrodedCARGO FLOORBEAM AT FS 589 BETWEEN RBL 27 - RBL 41 IS CORRODED. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-321-06 & SRM 53-00-00. PERFORMED UT INSPECTION OF BLEND AREA IAW MWC NDT INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-61-4557.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201756Floorbeam · corrodedCARGO FLOORBEAM AT FS 574 BETWEEN LBL 9.0 - RBL 9.0 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED CAP STRIP IAW SRM 51-42-06 AND 51-45-00, 51-42-15 AND DWG NR 601R35031.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201755Floor Support · corrodedCARGO RT FLOOR SILL IS CORRODED BETWEEN FS 559+80 - 621. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. WITHIN LIMITS OF SRM 53-00-00.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201754Floorbeam · corrodedCARGO FLOORBEAM AT FS 621 BETWEEN LBL 9 - 27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. BEYOND LIMITS IAW SRM 53-61-49.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201753Cargo Track · corrodedCARGO TRACK AT LBL 9 BETWEEN FS 612 - 616 IS CORRODED. CARGO TRACK FOUND TO BE UNSERVICEABLE IAW SRM 53-61-49. R & R CARGO TRACK IAW AMM 53-01-11-000-802.Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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