N871AS

Service difficulty reports · 156

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 = 'N871AS' 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 ASOA2015072513534Stringer · crackedSTR 3L IS CRACKED AT FWD SIDE OF FS 379 APPROXIMATELY .5" LONG. REMOVED FASTENERS FROM STR 3L, FS 379 IAW SRM 51-42-06. COMPLIED WITH SRM 53-00-03, REV 53-51, STR SPLICE REPAIR. INSTALLED STRINGER SPLICE REPAIR AT 3L FWD SIDE OF FS 379 IAW SRM, REV 53-51, SJul 25, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2015072413568Shroud · chafedRT AILERON UPPER OTBD L/E SHROUD IS CHAFED FROM 4" INBD OF OTBD HINGE TO OTBD END. BLENDED RT AILERON L/E DAMAGE IAW REO 601R-57-60-013, REV A DATED 08/05/2013. COMPLIED WITH EC/TC REO 601R-57-60-013 IAW REO 601R-57-60-013, REV A.Jul 24, 2015 · N871AS · Cndair CL6002B19 · AileronsSDR ASOA2015072413567Shroud · chafedLEFT AILERON UPPER L/E SHROUD IS CHAFED FROM ABOUT 6" INBD OF OTBD HINGE TO THE OTBD END. COMPLIED WITH REO 601R-57-60-013, REV A DATE 2013/08/05.Jul 24, 2015 · N871AS · Cndair CL6002B19 · AileronsSDR ASOA2015072413533Isolator · crackedFS 621 BULKHEAD FWD FACE ABOVE FLOOR HAS 8 CRACKED SCREW MOUNT ISOLATORS: 4 AT RBL 45, 1 RBL 36, 1 LBL 9, 1 LBL 18 AND 1 LBL 27. REMOVED UNSERVICEABLE ISOLATORS 8 EA IAW SRM 51-42-06. INSTALLED SERVICEABLE ISOLATORS 8 EA IAW SRM 51-42-10.Jul 24, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015052212887Skin · dentedRIGHT WING FIXED L/E PANEL DENT DAMAGED BY FUEL TRUCK. REMOVED RT WING FIXED L/E PANEL TO SUBMIT DENT DAMAGE. SUBMITTED DENT TO STS ENGINEERING IAW SRM 51-13-01, DENT MEASURES 3.9"L X 3.6"W X .200" DEEP. RECEIVED EA 20-2015-119, 05/18/2015, COLD WORKED DAMAMay 18, 2015 · N871AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015031612411Wire · disconnectedFOUND 4 WIRES GOING TO 2 EMERGENCY LIGHTS ON WARDROBE DAMAGED. REQUIRES NEW PINS/QUICK DISCONNECTS. INSTALLED CONNECTORS FOR EMERGENCY LIGHT AT WAREDROBE IAW ESPM 20-17-00 AND WM 33-51-60. OPS CHECK GOOD IAW AMM 33-51-00.Mar 12, 2015 · N871AS · Cndair CL6002B19 · Light System WiringSDR ASOA2014081511070Battery · dischargedFWD EMERGENCY FLOOD LIGHT INOPERATIVE. ALLOWED EMENGENCY BATTERY PACK TO CHARGE, COMPLIED WITH OPS TEST OF EMERGENCY LIGHTS IAW 33-51-04 AMM OPS TEST CHECK GOOD.Aug 14, 2014 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014030410056Lamp · burned outRIGHT NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Feb 28, 2014 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013072608791Isolator · brokenBROKEN ISOLATORS ON FWD SIDE OF FS 621 BULKHEAD. R & R FOUR ISOLATORS IAW SRM 51-42-13-00.Jul 22, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013080508830Trunnion · crackedRT MLG TRUNNION HAS ONE FASTENER HOLES WITH CRACK INDICATION. REPAIRED IAW REO 601R-57-21-1973. MAJOR REPAIRJul 16, 2013 · N871AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2013080508829Trunnion · crackedLT MLG TRUNNION HAS 3EA HI-LIGHT HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-5721-1973. MAJOR REPAIR.Jul 16, 2013 · N871AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2013071908743Seat Track · corrodedSEAT TRACK RBL 9 CORRODED BEYOND SRM LIMITS. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Jul 16, 2013 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013071908742Seat Track · corrodedSEAT TRACK LBL 9 CORRODED BEYOND LIMITS. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.Jul 16, 2013 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013071908741Floor Support · crackedFOUND SUPPORT CRACKED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED IAW SRM 51-40-06 AND SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT PER REO 601R-53-61-1230. REPAIR CLASSIFIED AS MAJOR.Jul 12, 2013 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013071808730Isolator · brokenISOLATOR BROKEN ON REAR PRESSURE BULKHEAD FWD FACE AT LBL 9.5. R & R ISOLATOR ON REAR PRESSURE BULKHEAD IAW SRM 51-42-13.Jul 11, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013071908740Floorbeam · crackedPRESSURE FLOORBEAM INBD FLANGE IS CRACKED AT FS 484 AT RBL 36. REPAIRED IAW SRM 51-42-21 AND 51-42-06.Jul 7, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2013071808729Floor Support · corrodedCORROSION DAMAGE ON LT SIDE PRESSURE FLOOR SUPPORT ANGLE FS 499 - 513, LBL 43. REPAIRED IAW REO 601R-53-41-666 REV C. CLASSIFIED A MAJOR REPAIR .Jul 7, 2013 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013071808728Floor Support · corrodedCORROSION DAMAGE ON LT SIDE PRESSURE FLOOR SUPPORT FS 507, LBL 42. REPAIRED IAW REO 601R-53-41-666, REV C. CLASSIFIED A MAJOR REPAIR.Jul 7, 2013 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013080508828Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN CRACKED ABOVE CARGO DOOR AFT TRACK APPROX 1" LONG. REPAIRED IAW REO 601R-53-61-1541, REV D, DATED 10/31/2011. REPAIR CLASSIFIED AS MAJOR.Jul 5, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013071908739Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED IN TWO PLACES AROUND CARGO DOOR CUTOUT AFT LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230. REPAIR CLASSIFIED AS A MAJOR.Jul 5, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013071808727Angle · crackedCARGO DOOR TRACK CROSS MEMBER AFT LOWER ATTACH ANGLE CRACKED. REMOVED ANGLE IAW SRM 51-40-11. LOCATED AND DRILLED BRACKET. INSTALLED ANGLE IAW SRM 51-40-11 AND DWG 601R35050.Jul 5, 2013 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072308753Drag Angle · crackedASD AFT DRAG ANGLE CRACKED. REPAIRED IAW REO 601R-52-11-513. REPAIR CLASSIFIED AS MAJOR.Jul 3, 2013 · N871AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013072308752Frame · crackedFRAME BS 333 AT 12 O`CLOCK POSITION IS CRACKED IN HALF. REMOVED DAMAGED FRAME SECTION IAW SRM 51-42-06 AND 51-42-20. LOCATED AND DRILLED REPLACEMENT FRAME IAW SRM 51-42-06. REPAIR CLASSIFIED AS MAJOR.Jul 3, 2013 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013071808726Flap · gougedASD VENT-FLAP GOUGED & DENTED. REPAIRED IAW REO 601R-52-11-1040. CLASSIFIED A MAJOR REPAIR.Jul 3, 2013 · N871AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013021403010Glowstrip · missingEMERGENCY EXIT ROW 8AB FWD PHOTOLUMINESCENT PATH CHEVRON MARKER MISSING. INSTALLED NEW CHEVRON MARKER AND COVER IAW EO 600-33-0015.Feb 11, 2013 · N871AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2012071301900Unknown · odorON DESCENT F/A SMELLED AN ELECTRICAL ODOR IN GALLEY AREA, NO VISABLE SMOKE, ODOR WENT AWAY ONCE THE ACFT IS ON THE GROUND. PERFORMED OP'S CK OF LT AND RT PACK IAW AMM 21-51-00. OP'S CK GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.Jul 9, 2012 · N871AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201102439Light · inoperativeRIGHT EXTERIOR OVERWING EMERGENCY LIGHT IS INOP. R & R LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Dec 27, 2011 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101202Floor Support · corrodedFLOORBOARD SUPPORT IN AVIONICS BAY AT FS349.00 CORRODED ON FWD SIDE. REPAIRED IAW REO 601R-53-21-1299, REV.Jun 21, 2011 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101191Beam · corrodedOP 115 AVIONICS BAY BEAM AT FS 349 BTWN STG 26L AND 26R IS CORRODED ON THE FWD SIDE. COMPLIED WITH EC/TC REO 601R-53-21-1299.Jun 15, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101185Beam · corrodedAVIONICS BAY FUSELAGE BEAM AT FS 333.00 BETWEEN STR 26L- STR 26R IS CORRODED ON FWD AND AFT SIDE. COMPLIED WITH REO 601R-53-21-1299.Jun 14, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101163Floor Support · corrodedCARGO BAY FLOOR SUPPORT AT LBL27 HAS CORRODED NUT PLATES. PERFORMED LPI, TYPE 1, METHOD C ON FABRICATED REPAIR ANGLE IAW SRM 53-00-43 IAW NDT INSP PROCEDURE PT-1 NO INDICATIONS NOTED AT THIS TIME. FABRICATED PARTS IAW SRM 53-00-43, INSTALLED FABRICATED PARJun 8, 2011 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101131Floorbeam · corrodedFLOORBEAM CORRODED AT APPROX 559+96 ON RBL 9. REMOVED CORROSION IAW SRM 51-21-06. FOUND BLEND AREAS WERE WITHIN LIMITS IAW REO 601R-53-00-0005, FIG 1.Jun 6, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101161Floor Support · corrodedCARGO BAY FLOORBEAM AT LBL 27 HAS CORRODED NUT PLATES. REMOVED CORROSION IAW SRM 51-21-06. MECHANICAL MEASURED BLEND AREAS ON LBL 27 BETWEEN FS 621-559+112. ALL BLENDS WITH IN ALLANCE LIMITS IAW SRM 53-61-43 AND 53-00-00. NOMINAL THICKNESS IS .063. REMAIJun 3, 2011 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101101Seat Track · corrodedSEAT TRACK AT APROX FS 559. + 96 AT RBL CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT TRACK IAW SRM 51-40-06, 51-40-02. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Jun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101100Floor Support · corrodedFLOORBAORD SUPPORT IN AVIONICS BAY AT FS 349.00 CORRODED ON FWD SIDE. REMOVED CORROSION IAW SRM 51-21-06.Jun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101099Attach Fitting · crackedTWO CLIPS CRACKED AT FS 280.00, RBL 9.0. REMOVED CRACKED CLIPS IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW CLIPS IAW SRM 51-42-06 AND SRM 51-42-21. THIS IS A MINOR REPAIR.Jun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201101098Beam · corrodedAVIONICS BAY FUSELAGE BEAM AT FS 310.00 IS CORRODED BETWEEN S26L-S26R ON AFT SIDE AND SMALL AREA ON FRONT SIDE AT S27. REMOVED CORROSION DAMAGE IAW SRM 51-42-06 AND SRM 51-21-06.Jun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101097Beam · corrodedAVIONICS BAY FUSELAGE BEAM AT FS 333.00 BETWEEN STR26L-STR26R IS CORRODED ON FWD AND AFT SIDE. REMOVED CORROSION IAW SRM 51-42-06 AND SRM 51-21-06.Jun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101096Beam · corrodedAVIONICS BAY FUSELAGE BEAM AT FS 349.00 BETWEEN S26L-R IS CORRODED ON THE FWD SIDE. REMOVE CORROSION & FASTENERS AS REQUIRED. EVALUATE 349 FRAME. REMOVED CORROSION IAW SRM 51-42-06 AND 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREA OF FRAME SECTOR IAJun 1, 2011 · N871AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101092Charger · inoperativeSEVERAL EMERGENCY LIGHTS INOPERATIVE. R & R NR 3 BATTERY PACK CHARGER ASSY IAW AMM 33-51-05-000-801 AND 33-51-05-400-801.May 31, 2011 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100038Flashlight · inoperativeF/O'S FLASHLIGHT DOES NOT WORK. REPLACED F/O FLASHLIGHT IAW AMM 25-61-00.Jan 5, 2011 · N871AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001794Door · jammedFLT 5570 - FLIGHT ATTENDANTS REPORTS MAIN PAX DOOR DIFFICULT TO OPEN. COMPLIED WITH PAX DOOR OPS CHECK POSITION CABLE ON DOOR GROUND STAND SUPPORT WHEEL, OK PER CRJ200 AMM 52-11-00.Nov 16, 2010 · N871AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000208Unknown · odorBURNING ODOR COMING FROM BEHIND CAPT'S SEAT, LIKE RUBBER. POWERED UP ALL SYS. OPENED PILOT SIDE C/B PANELS. INSPECTED, NO DEFECTS FOUND. UNABLE TO DUPLICATE ODOR.Feb 11, 2010 · N871AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA200900709Post · damagedFS 409.0+128 VERTICAL POST LBL 18.0 HAS INDICATION NOTED AT O/B SIDE WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST LBL 18 FS 409 + 128 IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST AT LBL 18.0 FS 409.0 + Jun 24, 2009 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900708Post · damagedFS 409+128 VERTICAL POST RBL 18.0 HAS INDICATION NOTED AT I/B SIDE WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED POST FS 409 + 128 RBL 18 IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST AT RBL 18.0 FS 409.0 + 128 USING 70Jun 24, 2009 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900707Anchor Fitting · crackedPAX DOOR FWD/AFT ANCHOR FITTINGS ARE CRACKED. REMOVED PAX DOOR FWD AND AFT ANCHOR FITTINGS AND INSTALLED NEW SERVICEABLE ONES IAW AMM 52-11-17-400-804 STEPS 1-2. WHILE PERFORMING ADJUSTMENT OF PAX DOOR COUNTER BALANCE SYSTEM, FOUND AFT ANCHOR FITTING TO HAVJun 24, 2009 · N871AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900706Angle · corrodedPAX DOOR LOWER SILL ANGLE SEVERELY CORRODED P/N 601R31527-221 LOCATED DIRECTLY BELOW ATTACH NUT PLATES FOR TOP STEP, MARKED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06 AND SRM 51-42-10. ANGLE IS OUT OF LIMITS. ANGLE REQUIRES REPLACEMENT. LOCATED SEJun 24, 2009 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900705Angle · damagedFOUND FS 559 CAP ANGLE HAS A INDICATION NOTED AT LBL 18.0 APPROX .3 INCH LENGTH 80 PERCENT FSH AND RT FS 559 BULKHEAD WEB HAS A INDICATION NOTED AT WL 58.70 TO O/B OF RBL 9. APPROX .2 INCH IN LENGTH 50 PERCENT FSH BOTH FAILED NDT INSP. COMPLIED WITH EC/TC REOJun 24, 2009 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900701Angle · crackedCARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .2 INCH IN LENGTH. REMOVED AND REPLACED AFT LOWER ANGLE FOR CARGO DOOR SUPPORT BEAM. INSTALLED WITH LOCK FASTENERS IAW SRM 51-42-21.Jun 24, 2009 · N871AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA200900741Sill · corrodedLT PRESSURE FLOOR SILL ASSY CORRODED ON SILL PNL AND ON FLOOR ANGLE APPROX .002 INCH DEEP FROM FS 513 TO FS 559 UNDER CABIN FLOOR PNL 261DLF. C/W REO 601R-53-41-666 REV O.Jun 23, 2009 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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