N877AS

Service difficulty reports · 292

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 = 'N877AS' 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 ASOA2015082413726Seat Track · corrodedSEAT TRACK LBL 9, BS 364-394 FOUND CORRODED . OUT LIMITS IAW SRM 53-21-49-01. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413725Seat Track · corrodedSEAT TRACK RBL 27, BETWEEN BS 559 + 80 AND 559+112 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49, AND 53-51-49, 53-21-49. REMOVED AND REPLACED IAW AMM 53-00-49-000-801, REO 601R-53-00-485, AND AMM 53-00-49-400-801.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413724Seat Track · corrodedSEAT TRACK RBL 9 BETWEEN BS 559+80 AND 559+112 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AMM 53-00-49-000-801, REO 601 R -53-00-485, AMM 53-00-49-400-801, AND GREO 53-00-485, REV A.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413723Seat Track · corrodedSEAT TRACK LBL 9 BETWEEN BS 559 + 80 AND 559 +112 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-111-400-802, AND GREO 601R-53-00-485, REV A.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413722Seat Track · corrodedSEAT TRACK LBL 27 BETWEEN BS -559 + 80 - 559+112 IS CORRODED. OUT OF LIMITS IAW AMM 53-00-49-000-801. REMOVED AND REPLACED IAW REO 601R-53-00-485, AND AMM TASK 53-00-49-400-801.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413721Seat Track · corrodedSEAT TRACK RBL 9 BETWEEN BS 559 +112 - 574 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49, 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, AND REO 601R-53-00-485.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413720Cargo Track · corrodedCARGO TRACK LBL 9 BETWEEN BS 605 - 621.00 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE CARGO TRACK IAW AMM TASK 53-00-49-000-801 AND REO 601R 53-00-485. IAug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413719Seat Track · corrodedSEAT TRACK LBL 9 BETWEEN FS 559 + 80 - 567 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49 53-61-49. REMOVED AND REPLACED THE SEAT TRACK, IAW AMM 53-00-49-000-801, AND REO 601R-53-00-485.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015082413718Anchor · corrodedANCHOR PLATE AT LBL 27, AT FS 559 + 96 IS CORRODED. R & R ANCHOR PLATE IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015082413717Anchor · corrodedANCHOR PLATE AT LBL 27 BETWEEN BS 559 + 96 IS CORRODED. R & R THE ANCHOR IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015082413716Door Sill · corrodedSERVICE DOOR LOWER SILL CORRODED FWD CORNER. REPLACEED IAW SRM 53-21-23. REMOVED SERVICE DOOR LWR SILL FWD CLEAT. DRILLED NEW CLEAT IAW SRM 51-40-11-00. COMPLETED INSTALLATION OF NEW SERVICE CLEAT AT LOWER SILL FWD CORNER OF SERVICE DOOR IAW SRM 51-42-21-00.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015082413715Door Sill · corrodedSERVICE DOOR LOWER SILL CORRODED AFT CORNER. FOUND CORROSION DAMAGE AFT CLEAT AND REQUIRE REPLACEMENT OF PART IAW SRM 53-21-23. REMOVED SERVICE DOOR LWR SILL AFT CLEAT. INSTALLED NEW CLEAT AT SERVICE DOOR LWR SILL AFT IAW SRM 51-42-21-00.Aug 24, 2015 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015082013714Skin · crackedLEFT WING PLANK CRACKED AT WS 148.019 AT AFT SPAR. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GREO 601R-57-21-130, REV K DATED 11/27/2013. COMPLIED WITH EC/TC REO 601R-57-21-131, REV B DATED 11-28-2013 AS WRITTEN.Aug 20, 2015 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015040712543Lamp · burned outWARDROBE LWR EMERGENCY LIGHT HAS SEVERAL INOPERATIVE BULBS. RELAMPED WARDROBE LWR EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECK GOOD.Apr 3, 2015 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015030912342Lens · missingLENS MISSING ON EXIT SIGNAL LIGHT, INTERIOR LIGHT LENS, COVERS, EXCLUDING EMERGENCY LIGHTS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-50-00. NO DEFECTS NOTED AT THIS TIME, DEFECT CLEARED.Mar 7, 2015 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013110809387Trunnion · crackedRT MLG TRUNNION FITTING AFT HOLE ON STEEL STRAP HAS AN INDICATION 100 PERCENT FSH AT THE 1 O'CLOCK POSITION, 12 O'CLOCK POSITION IS FWD AND 6 O'CLOCK IS AFT LOOKING UP. REAMED THE HOLE IN QUESTION ON THE RT MLG TRUNNION FITTING TO A .297" TO CLEAN UP DAMAGE IOct 21, 2013 · N877AS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR ASOA2013110809386Trunnion · damagedWHILE PERFORMING SB 601R-57-048 DAMAGED OCCURED TO MLG TRUNNION AT THE RT MLG FWD DOOR HINGE FWD FASTENER HOLE. HOLE DIAMETER IS CURRENTLY AT 0.2684" WITH APPROX 0.010" D, DAMAGE INSIDE HOLE. REAMED FASTENER HOLES AND ENSURED COMPLETE DAMAGE REMOVAL IAW REO Oct 20, 2013 · N877AS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR ASOA2013110809385Skin · chafedLOWER WING PLANK IS CHAFED AT LT AND RT WS 46 AND T/E LT APPROX 1.300" X .600" X .030" DEEP. RT APPROX 1.000" X .600" X .020" DEEP. PERFORMED REPAIR TO LOWER WING PLANK AT LT/RT WS 46 AT T/E IAW REO 601R-57-21-880, REV C AND COMPLIED WITH EC/TC REO 601R-57-21Oct 19, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809384Skin · crackedLOWER WING PLANK RT BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. BLENDED PANEL LANDING AT 610CB. .003 MATERIAL REMOct 19, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809383Skin · crackedLOWER WING PLANK LANDING FOR ACCESS PANEL 550FB HAS MULTIPLE INDICATIONS NOTED ON TEH OTBD SIDE APPROX .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR ACCESS PANEL 550FB IAW REO 601R-57-21-030, REV K, STEPS 1 THOct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809382Skin · crackedLOWER WING PLANK LANDING FOR PANEL 610AB, HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERENCE APPROX .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 610AB IAW REO 601R-57-21-030 REV K, STEPS 1 THROUGH 12 Oct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809381Skin · crackedLOWER WING PLANK LANDING FOR ACCESS PANEL 550GB HAS MULTIPLE INDICATONS AROUND ENTIRE CIRCUMFERENCE APPROX .250" X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIRS TO LOWER WING PLANK LANDING FOR PNL 550GB IAW REO 601R-57-21-030, REV K AND COMPLIED WIOct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809380Skin · crackedLOWER WING PLANK LANDING FOR PANEL 650GB HAS AN INDICATION NOTED ON THE INBD AFT SIDE APPROX .250" X .5 X 50 PERCENT. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PNL 650GB IAW REO 601R-57-21-030, REV K AND COMPLIED WITH EC/TC EO 60Oct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110809379Skin · crackedLOWER WING PLANK LANDING FOR PANEL 550BB HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERANCE APPROX .250" X 70 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 550BB IAW REO 601R-57-21-030, REV K, STEPS 1 THROUGH 12Oct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110709370Skin · crackedLOWER WING PLANK LANDING FOR PANEL 640AB HAS AN INDICATION NOTED ON THE INBD SIDE APPROX 2" X .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 640AB IAW REO 601R-57-21-030, REV K. AND COMPLIED WITH EC/TC EOOct 18, 2013 · N877AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013110709369Post · crackedFOUND FS 409+128 VERTICAL POST RBL 18 HAS A CRACK INDICATION NOTED AT AFT FLANGE RADIUS APPROX .3 INCHES IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. DRILL, LOCATED AND INSTALLED SERVICABLE POST ASSY IAW SRM 51-42-06,Oct 16, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709368Post · crackedFOUND FS 409+128 VERTICAL POST LBL 18, HAS A CRACK INDICATION NOTED AT AFT FLANGE RADIUS APPROX .2 INCHES IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. DRILL, LOCATED AND INSTALLED SERVICABLE POST ASSY IAW SRM 51-42-06Oct 16, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709367Attach Angle · crackedONE ATTACHMENT ANGLE THAT ATTACHES TO ACFT SKIN LOCATED BETWEEN FS 621-625 AT STR 14R CRACKED. R & R WITH NEW IAW SRM 51-42-21, SRM 51-42-06.Oct 16, 2013 · N877AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2013110709366Channel · crackedTWO U-CHANNELS THAT ATTACH TO ACFT SKIN LOCATED BETWEEN FS 621-625 STR 13-14L ARE CRACKED. REMOVED CHANNELS IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW CHANNEL AND INSTALLED IAW SRM 51-40-06, SRM 51-40-11, SRM 51-42-06 AND SRM 51-42-21.Oct 16, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709365Floor Support · corrodedCARGO BAY BETWEEN BS 589 - 617, RBL 27, FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21, 51-42-22.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709364Floor Support · corrodedCARGO BAY BETWEEN BS 589 - 610 LBL 9, OTBD SIDE, FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3780 AND IAW SRM 51-40-11.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709363Floor Support · corrodedCARGO BAY BETWEEN BS 574 - 584 LBL 36.00 FLOOR SUPPORT CORRODED. REMOVED IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW IAW REO 601R-53-61-1574.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709362Angle · crackedLT OBLIQUE ANGLE LOCATED BETWEEN FS 621-625, LBL 45, STR 14L AND WL 97.5 IS CRACKED AT AFT END. R & R OBLIQUE ANGLE IAW SRM 51-42-21.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013110709361Wire · brokenCONNECTION SPLICE FOR THE EMERGENCY EXIT SIGN ON THE WARDROBE IS BROKEN. INSTALLED QUICK DISC SPLICE IAW ESPM 20-16-00. OPS CHECK OF WARDROBE EMERGENCY EXIT SIGN IS GOOD IAW AMM 33-51-00-710-801.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Light System WiringSDR ASOA2013110709360Glowstrip · missingPHOTOLUMINESCENT AISLE PATH MARKERS MISSING (4) END INDICATORS AND RT EMERGENCY EXIT CHEVRONS OTBD SHOULD BE INBD. ADJUSTED RT EMERGENCY EXIT CHEVRONS TO INBD SIDE AND INSTALLED END INDICATORS 4 EA AT EMERGENCY EXITS IAW SAFTGLO DWG SG-CRJ, REV B PN'S SG9952Oct 15, 2013 · N877AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2013110709359Bulkhead · chafedBS 621 BULKHEAD IS CHAFED RBL 18, RBL 27, RBL 36, LBL 18 AND LBL 27, 30 INCHES ABOVE FLOOR. COMPLIED WITH EC/TC REO 601R-53-61-2155, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013110709358Bulkhead · scratchedBULKHEAD HAS A SCRATCH APPROXIMATELY 2 INCHES LONG X .002 DEEP AT LBL 27, 16 INCHES ABOVE FLOOR. COMPLIED WITH EC/TC REO 601R-53-61-2155, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.Oct 15, 2013 · N877AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013010202729Light · inoperativeLEFT EXTERIOR MIDDLE EMERGENCY LIGHT INOPERATIVE. R & R THE LT EXTERIOR MIDDLE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Dec 30, 2012 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012082202088Bulb · burned outRT AFT EXTERNAL EMERGENCY LIGHT IS INOP. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. OP'S CHECKED GOOD. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. AMM 33-51-21. OP'S CHECKED GOOD.Aug 18, 2012 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102083Holder · damagedRT FWD EXTERNAL EMERGENCY LIGHT INOP. TROUBLESHOOTING REVEALED DEFECTIVE LAMP HOLDER. ALSO, FOUND NO POWER ATB LIGHT LEADS. FURTHER TROUBLESHOOTING REQUIRED. REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21-000-801 AND 33-51-21-400-801. OP TEST GOOD.Oct 31, 2011 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102082Connector · brokenEMERGENCY LIGHT ON AFT ON AFT SIDE OF F/A STATION WARDROBE UNIT HAS BROKEN CONNECTOR. REPLACED BROKEN CONNECTOR IAW ESPM 20-17-10, WITH NEW SERVICEABLE CONNECTOR.Oct 31, 2011 · N877AS · Cndair CL6002B19 · Light System WiringSDR ASOA201102048Floorbeam · crackedFLOORBEAM FS 280, LBL9 AND RBL9 CRACKED. REPAIRED IAW REO 601R-53-11-926.Oct 24, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201102025Floor Support · corrodedFLOOR SUPPORT CORRODED AROUND NUT PLATE HOLES FROM FS 621 TO FS 559+112. LBL 27. REPAIRED IAW REO 601R-53-43-778 AND GREO 601R-53-61-3778, REV "A".Oct 21, 2011 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101987Frame · corrodedBS 310 FRAME CORRODED S26L TO 26R.Oct 17, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201101986Frame · corrodedFS 310 FRAME CORRODED, S26L TO 26R. REMOVED FRAME IAW SRM 51-42-06. DRILLED FRAME IAW SRM 51-40-11 & ALODINE IAW SRM 51-21-11. INSTALLED FRAME IAW SRM 51-42-06.Oct 17, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201101985Frame · corrodedFS 349 FRAME CORRODED, S25-26R. DRILLED NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SRM 51-42-06.Oct 17, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201102047Sill · crackedPASSENGER DOOR UPPER SILL CRACKED AT FS280 AND STR 3L. REMOVED 3 CRACKED CLIPS & INSTALLED 3 NEW CLIPS IAW SRM 51-25-16, 51-40-11, 51-42-06 & 51-14-06.Oct 11, 2011 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101953Attach Angle · crackedATTACH ANGLE CRACKED AT FS 409.00+128, BL 0.00. REMOVED ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 & SRM 51-25-16.Oct 11, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201101952Floorbeam · corrodedFS 349 FLOORBEAM CORRODED AT APPROX RBL 41. REPAIRED IAW REO 601R-53-21-2204.Oct 11, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101951Floorbeam · corrodedFS 280 RBL & LBL 9 FOUND FWD FLOORBEAM CORRODED. REMOVED CORROSION IAW SRM 51-21-06. CORROSION OUT OF LIMITS IAW SRM 53-00-00. REPAIRED IAW REO 601R-53-11-926.Oct 11, 2011 · N877AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
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