N841AS, cancelled Aug 11, 2021

Service difficulty reports · 133

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 = 'N841AS' AND deregistration_id = 'N841AS-2021-08-11'
  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 ASOA2015111714089Smoke Detector · false indication"SMOKE TOILET" CAUTION ON TAKEOFF, MESSAGE WENT AWAY ON FINAL APPROCH. R & R LAV SMOKE DETECTOR REF AMM 26-16-01. OPS CHECK GOOD, NO OTHER DEFECTS NOTED.Nov 17, 2015 · N841AS · Cndair CL6002B19 · Smoke DetectionSDR ASOA2015012812105Isolator · brokenBROKEN ISOLATOR ON FS 621 BULKHEAD. R & R ISOLATOR IAW SRM 51-42-13.Jan 20, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015012612092Angle · crackedBS 621 ANGLE CRACKED. R & R THE ANGLE IAW SRM 51-42-21 & TR 51-32.Jan 20, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012812104Floor Support · corrodedLT CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS OF REO 601R-53-41-666 BS 426 - 519. CUT OUT DAMAGE IAW REO 601R-53-41-1871, REV P1. FABRICATED REPAIR IAW REO 601R-53-41-1871, REV P1. INSTALLED THE REPAIR IAW REO 601R-53-41-1871, REV P1Jan 13, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012812103Skin · crackedRT LOWER WING PLANK/TRUNNION HAS AN INDICATION NOTED IN BORE OF THE 4TH FASTENER GOING AFT FROM FWD END NOTED IN SB 601R-57-046, REV C. INDICATION IS ON INBD SIDE .450" FROM LOWER SURFACE, .150" LONG AND 60 PERCENT FSH. FAILED NDT. COMPLIED WITH STEP 13 OF RJan 13, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012812102Skin · corrodedCORROSION FOUND ON LOWER WING PLANK LANDING AFT/INBD EDGE UNDER PANEL 650BB. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Jan 12, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012612091Angle · crackedBS 621, UPPER LT AND RT OBLIQUE ANGLES ARE CRACKED. R & R THE ANGLES IAW SRM 51-42-21.Jan 12, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612090Stringer · crackedSTRINGER 3L AT BS 280 BULKHEAD CRACKED. REPAIRED IAW SRM 51-42-06 AND SRM 51-40-11-00.Jan 9, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2015012812101Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION. LBL 18.00, WL 140 REMOVED FS 621.00 BULKHEAD STIFFENING ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE FS 621, BULKHEAD STIFFENING ANGLE IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-5420, REV. COJan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015012812100Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT BL 0.0, WL 102 . REPAIRED IAW EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015012812099Floor Support · corrodedPRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. FOUND TO BE WITHIN LIMITS OF REO 601R-53-41-666.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012812098Skin · crackedLOWER WING PLANK ACCESS HOLE HAS AN INDICATION NOTED ON LANDING, FOR PANEL 650DB AT AFT INBD EDGE APPROXIMATELY .250" X .250" X 50 PERCENT FSH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012812097Skin · crackedLOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED, ON LANDING FOR PANEL 610AB AT FWD OUTBD EDGE, APPROXIMATELY 1.0" X .250" X 50 PERCENT FSH, FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012812096Skin · crackedLOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED ON LANDING FOR PANEL 650FB AT FWD AND OTBD EDGE, APPROXIMATELY .250" X .250" X 50 PERCENT FSH. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012612089Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76.0. REPAIRED IAW REO 601R-53-61-5417, REV.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015012612088Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18.00, WL 108. REPAIRED IAW EC/TC REO 601R-53-61-1285 & GREO 601R-53-61-1285.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015012612087Floor Support · corrodedPRESSURE FLOOR SUPPORT HAS MINOR CORROSION BETWEEN BS 409+128 - 559. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612086Intercostal · crackedINTERCOSTAL AT STRINGER 13L BS 621 IS CRACKED. REMOVED AND REPLACED TEH INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612085Angle · crackedINTERCOSTAL AT BS 484, LBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.Jan 8, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612084Angle · crackedINTERCOSTAL AT FS 484, LBL 36 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612083Angle · crackedINTERCOSTAL AT BS 484, RBL 27 HAS A CRACKED ANGLE. R & R THE ANGLE IAW SRM 51-40-11 AND 51-42-21.Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612082Angle · crackedINTERCOSTAL AT FS 484, RBL 36.00 HAS A CRACKED ANGLE. REPAIRED IAW REO 601R-53-41-1870 AND REO 601R-53-41-059.Jan 7, 2015 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015012612081Skin · crackedRT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL AND HORIZONTAL LANDING 60 PERCENT FSH FAIL NDT. COMPLIED WITH EA 32-2015-004.Jan 6, 2015 · N841AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015012812095Door · delaminatedLEFT NLG DOOR L/E DELAMINATED. REPAIRED LT NLG DOOR IAW REO 601R-52-81-020, REV NC DATED 99-09-17. PAINTED REPAIRED AREA ON LT NLG DOOR L/E IAW SRM 51-25-01. APPLIED ABRASION RESISTANT FILM ON LT NLG DOOR L/E IAW SRM 51-27-19. COMPLIED WITH EC/TC REO 601R-Jan 3, 2015 · N841AS · Cndair CL6002B19 · Landing Gear DoorsSDR ASOA2015010512002Landing Gear · malfunctionedNOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO DEPARTURE. GEAR EXTENDED MANUALLY.Dec 28, 2014 · N841AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2014122211893Rod · brokenPAX DOOR WILL NOT OPEN. FOUND PRESSURE RELIEF VENT FLAP ROD BROKEN. REPLACED PAX DOOR VENT FLAP ROD IAW AMM 52-11-15. OPS CHECK GOOD. ACFT OK FOR SERVICE.Dec 18, 2014 · N841AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014013109816Support Bracket · crackedFWD SUPPORT BRACKET IN AFT CARGO DOOR IS CRACKED. R & R FWD SUPPORT BRACKET IAW SRM 51-42-06.Jan 26, 2014 · N841AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA2013062708511Skin · damagedFUSELAGE SKIN DAMAGED AT FS 310 NEAR STR 16L AT SKIN EDGE. REPAIRED IAW GREO 601R-53-21-160, REO 601R-53-21-2447.Jun 23, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2013020702969Floor Support · corrodedRT FLOOR SUPPORT FWD OF SERVICE DOOR CUTOUT IS CORRODED FROM FS 310 TO FS 319. R & R FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11.Jan 23, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020502958Rib · crackedRT WING L/E RIB AT WS 167.46 IS CRACKED AT EDGE OF PICCOLO TUBE CUTOUT. REMOVED CRACKED RIB AT WS 167.46 IAW SRM 51-42-06. INSTALLED NEW RIB, PN 601R12047-4 IAW SRM 51-42-06.Jan 21, 2013 · N841AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA2013020502957Angle · crackedWHILE REPLACING FWD J ANGLE ON FS 280, FOUND INBD CLIPS AT LBL 9 & RBL 9 TO BE CRACKED. REMOVED CLIPS IAW SRM 51-42-21. FABRICATED & INSTALLED INBD CLIPS AT LBL 9 & RBL 9 IAW REO 601R-53-11-926.Jan 21, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020702968Post · crackedFOUND FS 409.00+128 VERTICAL POST BL 0.0 LT & RT SIDE HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION. REMOVED FS 409+128 BL 0 VERT POST ASSY IAW SRM 51-42-06 & 51-42-21. DRILL/LOCATED NEW SERVICEABLE FS Jan 17, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020702967Angle · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-13 & 51-42-06. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-2Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020602964Beam · corrodedCORROSION FOUND ON END OF TRANSVERSE BEAM AT FS 349 RT SIDE. REPAIRED IAW REO 601R-53-21-2401.Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013020602963Sill · corrodedCORROSION FOUND ON LOWER SERVICE DOOR SILL ANGLE BETWEEN FS 319 AND FS 349. REMOVED CORRODED SILL FOR REPLACEMENT IAW SRM 51-42-06, 51-42-13 AND 51-42-21. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06, SRM 51-42-13 & SRM 51-42-21. LOCATED AND DRILLED NEW SERVICJan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020602962Fitting · crackedCO-PILOT SIDE POST LOWER AFT FITTING IS CRACKED (FITTING IS FOR WINDOWS). R & R LOWER AFT FITTING ON THE CO-PILOT'S SIDE POST WITH A NEW SERVICEABLE FITTING IAW SRM 51-42-21.Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2013020502956Frame · corrodedFRAME 605 IS CORRODED AT STRINGER 27. PERFORMED FRAME REPAIR NR 2 FRAME OUTER FLANGE REPAIR TO FS 605 BETWEEN STR 26-27 IAW SRM 53-00-15, REPAIR NR 2. COMPLIED WITH SRM 53-00-15.Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013020502955Angle · corrodedCORROSION ON FS 280.00 J-ANGLE. R & R WITH NEW SERVICEABLE J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.Jan 16, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020602961Seat Track · corrodedCORROSION ON LT AND RT AISLE SEAT TRACKS FROM FS 364.00 TO FS 559.00+32. REMOVED LT NR 1 SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED & DRILLED NR 1 LT SEAT TRACK FABBED FROM N126-2075 EXTRUSION IAW REO 601R-53-00-485. INSTALLED LT NR 1 FABBED SEAT TRACK PNJan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013020602960Skin · corrodedEXTERIOR SKIN PANELS BETWEEN FS 559.00+96 AND 559.00+112 CENTERLINE OF BELLY HAS CORROSION AROUND BUTTON HEAD RIVETS. BETWEEN FS 559+96 AND FS 559+112 BETWEEN STR 26L & STR 26R BLENDED AREAS TO SMOOTH CONTOUR. REPAIRED IAW REO 601R-53-51-215 AND SRM 51-42-06Jan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2013020502954Rib · crackedRT BATT RIB ASSY CRACKED AT WS 53.60 APPROX 1" LONG. REPAIRED IAW REO 601R-57-51-046.Jan 15, 2013 · N841AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA2013020102951Bracket · crackedREAR PRESSURE BULKHEAD AT FS 621.00 HAS 4 ISOLATOR BRACKET ASSY CRACKED AT RBL 45, 1 BRACKET AT RBL 9, 1 BRACKET AT LBL 9, 1 BRACKET AT LBL 27 AND 1 BRACKET AT LBL 36. REMOVED 8 EA DAMAGED ISOLATORS FROM FS 621 PRESSURE BULKHEAD AND INSTALLED NEW ISOLATORS, Jan 15, 2013 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013020102950Angle · crackedRT FS 621-625 INTERCOSTAL ANGLE CRACKED AT S14R. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11 AND INSTALLED NEW ANGLE IAW SRM 51-42-21.Jan 14, 2013 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012071301899Lamp · burned outFWD WARDROBE FLOOR FLOOD EMERGENCY LIGHT HAS SEVERAL BULBS INOPERATIVE. RELAMPED FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE. OPS CHECKED GOOD.Jul 9, 2012 · N841AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100845Latch · bindingUNABLE TO UNLATCH PAX DOOR FROM OUTSIDE. PERFORMED OPS CHECK OF PAX DOOR HANDLE IAW AMM 52-11-02.Apr 25, 2011 · N841AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100218Light · brokenEMERGENCY LIGHT FLOOR LEVEL FLOODLIGHT AT PASSENGER DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW CRJ 200 33-51-19-000-801 & -400-801. EMERGENCY LIGHTS OPS CHECKED OK IAW MM 33-51-00-710-801.Feb 4, 2011 · N841AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100208Wire · brokenPANEL 232BZ HAS A BROKEN WIRE ON THE EXIT LIGHT PANEL. R & R EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. OPS CHECK DUE. PERFORMED OPS CHECK FOR EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-00-710-805. OPS CHECK GOOD. (CLOSED)Jan 25, 2011 · N841AS · Cndair CL6002B19 · Light System WiringSDR ASOA201100184Isolator · brokenAFT BULKHEAD 621 ISOLATOR IS BROKEN. INSTALLED A NEW SERVICEABLE ISOLATOR ON THE 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Jan 24, 2011 · N841AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201100161Web · crackedPAX DOOR AFT WEB IS CRACKED AT FWD EDGE OF STEP 832AT. REPAIRED DAMAGE IAW REO NR: 601R-52-11-1901.Jan 24, 2011 · N841AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100160Floor Support · corrodedCORROSION ON NUTPLATES OF FLOOR SUPPORT FS 585 - 600 LBL 27.Jan 24, 2011 · N841AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N841AS, cancelled Aug 11, 2021