N879AS

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 = 'N879AS' 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 ASOA200901454Access Panel · crackedFOUND RT WING LOWER PLANK FUEL ACCESS HOLE 650CB HAS MULTIPLE INDICATIONS NOTED APPROX 5.0: AREA INBD SIDE NON-CRITICAL 70 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED FORMS TODec 21, 2009 · N879AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA200901453Access Panel · crackedFOUND LT WING LWR PLANK FUEL ACCESS HOLE 540DB HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERENCE OF LANDING 70 PERCENT FSH FAILED NDT INSP, NON-CRITICAL & CRITICAL AREAS. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL RDec 21, 2009 · N879AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA200901452Access Panel · crackedFOUND LT WING LWR PLANK FUEL ACCESS HOLE 540CB HAS 2 INDICATIONS NOTED, INBD SIDE NON-CRITICAL AREA OF LANDING 50 PERCENT FSH APPROX 2.0" IN LENGTH, FAILED NDT INSP. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FORWARDED ALL REQUIRED Dec 21, 2009 · N879AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA200901426Floorbeam · corrodedFLOORBEAM AT FS 349, RBL 43 HAS CORROSION .040 DEEP.Dec 16, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA200901425Web · crackedPAX DOOR FWD WEB IS CRACKED IN RADIUS BETWEEN FIXED STEP AND STEP 832CT. APPROX .200" LONG.Dec 16, 2009 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901424Bracket · corrodedFS 349.0 FLOORBEAM JOINT BRACKET HAS CORROSION RT SIDE.Dec 16, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901408Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. LOCATED AND DRILLED NEW POST IAW SRM 51-40-11. ATTACHED POST TOGETDec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901407Structure · corrodedCORROSION FOUND ON FLOOR SUPPORT STRUCTURE JUST FWD AND AFT OF FS 349.0 WL 73.5, RBL 45.0.Dec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA200901406Frame · corrodedFS 349.0 FRAME CORRODED STR 26L TO STR 27 FWD SIDE OF FRAME.Dec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200901405Frame · corrodedFS 333.0 FRAME CORRODED STR 26R TO STR 27 FWD AND AFT SIDES.Dec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200901404Frame · corrodedFS 319.70 FRAME CORRODED STR 26R AFT SIDE.Dec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200901403Frame · corrodedFS 310.0 FRAME CORRODED STR 26R TO STR 27 AFT SIDE.Dec 13, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200901389Skin · corrodedJOB 2760011, OPERATION 339/ EXTERIOR SKIN SURFACE FS 559 TO FS 559+32 STRINGER 24L TO 24R HAS CORROSION AROUND FASTENER HOLES AND DRAIN HOLE.Dec 11, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA200901388Skin · corrodedJOB 2760011, OPERATION 338/ EXTERIOR SKIN SURFACE FS 559+32 TO 574.00 HAS SURFACE CORROSION STRINGER 25L TO 25R.Dec 11, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA200901387Skin · corrodedJOB 2760011, OPERATION 337/ EXTERIOR SKIN AND SURFACE IS CORRODED FS 559+80 TO FS 559+96 STRINGER 22R TO 23R AROUND FASTENER HOLES.Dec 11, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA200901384Angle · crackedFOUND FS559 HAS 2 INDICATIONS NOTED RT FS559 WEB WL 59.10 APPROX .3" IN LENGTH 70 PERCENT FSH AND LT FS559 LAP ANGLE L8L18 APPROX .2" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. REPAIRED FS 559 FROM LBL 27 TO RBL 27 WEB AND CAP ANGLES IAW REO 601R-53-41-2Dec 10, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901451Floorbeam · corrodedCARGO BAY FLOORBEAM CAP AT LBL27 BETWEEN FS 574.00 AND FS 621.00 HAS MINOR CORROSION AROUND OTBD NUTPLATES.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA200901401Web · crackedPASSENGER DOOR FWD WEB IS CRACKED BETWEEN STEPS 832AT AND 832BT APPROX .250" LONG.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901399Web · crackedPASSENGER DOOR WEB UNDER TOP FOLDING STEP IS CRACKED AT FWD SIDE APPROX 1.250".Dec 10, 2009 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901396Placard · missingALL EXTERIOR PLACARDS ON CREW ESCAPE HATCH MISSING OR UNREADABLE.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA200901386Support Beam · crackedJOB 2760015, OPERATION 92/ CARGO DOOR SUPPORT BEAM LWR AFT ANGLE IS CRACKED APPROX 1" IN LENGTH.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA200901385Bulkhead · damagedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDING THE LINTEL FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 90 PERCENT FSH FAILED NDT INSP. REPAIRED IAW EC/TC REO 601R-53-61-1230.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200901383Web · crackedJOB 2760011, OPERATION 306/ PASSENGER DOOR AFT WEB IS CRACKED BETWEEN FIXED STEP AND 832CT APPROX .200".Dec 10, 2009 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901382Intercostal · crackedJOB 2760011, OPERATION 303/ FS 484 RBL 36.0 INTERCOSTAL ANGLE CRACKED IN RADIUS.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901381Intercostal · crackedJOB 2760011 OPERATION 302/FS 484.0 LBL 36.0 INTERCOSTAL ANGLE CRACKED IN RADIUS.Dec 10, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901398Glowstrip · crackedPHOTOLUMINESCENT TRACK LIGHTING, AFT OF OVER WING INDICATORS, REQUIRES REPLACEMENT DUE TO CRACKED BASES, CRACKED COVERS, AND DETERIORATED CHEVRON MARKINGS. PHOTO STRIPS ARE STILL SERVICEABLE.Dec 7, 2009 · N879AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA200901362Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED AT RADIUS APPROX 1.0" LONG. REMOVED AND REPLACED INTERCOSTAL AT FS 621 TO FS 625.30, STR 14L WITH A NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-21 11.A AND B(1), AND 9C(1-2).Dec 6, 2009 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901286Light · inoperativeRT FWD MOST EXTERNAL FUSELAGE EMERGENCY LIGHT INOP.Nov 11, 2009 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200801617Light · inoperativeAFT SECTION OF OVERHEAD EMERGENCY LIGHT, BOTH CENTER OVERWING EMERGENCY LIGHTS, AND NR 3 EMERGENCY FLOOD LIGHT INOP.Dec 3, 2008 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200800685Line · leakingHYD 1 MSG PSI FLUXED AND QTY WENT FROM 70 TO 5%. ENG OPERATED 32 MIN WITH 0 PSI ON HYD SYS 1 (EN ROUTE TO ATL ACFT DIVERTED TO BNA DUE TO MTC, EMERGENCY DECLARED). FLT 4740 DEL 79 MINS. REMOVED AND REPLACED HYD LINE P/N 601R752501 PER CRJ AMM 29-00, NO HELPMay 24, 2008 · N879AS · Cndair CL6002B19 · Hydraulic System, MainSDR TRAX200800660Step · crackedASD BOTTOM STEP CRACKED. REMOVED AND REPLACED ASD BOTTOM STEP IAW AMM 52-11-04. OPS CK GOOD. (B)May 18, 2008 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200800329Light · inoperativeCEILING AFT MOST EMERGENCY LIGHT INOP.Feb 26, 2008 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200800326Light · inoperativeLT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP.Feb 26, 2008 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200800325Light · inoperativeCEILING EMERGENCY LIGHT 2ND FROM FRONT INOP.Feb 26, 2008 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200701981Light · inoperativeRT AFT OVERWING EMERGENCY LIGHT IS INOP.Dec 25, 2007 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200701876Light · inoperativeCENTER EMERGENCY EXIT LIGHT HAS 4 BULBS INOP.Dec 6, 2007 · N879AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200701845Bulkhead · crackedAAR - PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED. Dec 1, 2007 · N879AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200701821Angle · corrodedFS 280 FWD ANGLE CORRODED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00399. REMOVED AND LOCATED NEW ANGLE P/N 600-34017-351 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED ANGLE IAW CRJ 200 SRM 51-42-06. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS AND Nov 28, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701780Angle · crackedAAR-1049, FS 280 LBL 27 O/B ANGLE CRACKED. RESOLVED ON W/O: 75509 TASKCARD: N/R-00333, REMOVED DAMAGED ANGLE FROM FS 280 LBL 27. FS 280 LBL 27 O/B CLIP ANGLE WAS REPLACED ON W/C 1000/0050 PER REO 601R-53-11-1290.Nov 26, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701781Floor Support · corrodedFLOOR SUPPORT AFT OF CARGO DOOR HAS CORROSION. Nov 26, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701779Floorbeam · crackedFS 280 RBL 36 I/B ANGLE IS CRACKED. Nov 26, 2007 · N879AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200701772Structure · corrodedPAX DOOR CUTOUT FRAME FS 349.00 HAS CORROSION. REMOVED MINOR SURFACE CORROSION FROM FWD BRACKET. IAW CRJ SRM 51-21-06. ASSEMBLED BRACKETS TO ANGLES REPLACING CORRODED PART. Nov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200701767Angle · crackedFS 280 LBL 27 ANGLE CRACKED OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00249. REMOVED AND FABRICATED ANGLE CLIP FOR FS 280LBL 20 OB SIDE IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. INSTALLED PANENov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701766Angle · crackedFS 280 RBL 9 ANGLES CRACKED IB AND OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00248). REMOVED 280 RBL 9 CRACKED ANGLE CLIPS I/B AND O/B. FABRICATED SERVICEABLE CLIP ANGLES. REFER TO FORM 412 IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOPCOAT FASTENERS APPLINov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701768Angle · crackedLT OBLIQUE ANGLE ON FS 625 CRACKED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00281. REMOVED CRACKED ANGLE, LOCATED IAW CRJ SRM.Nov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701769Attach Bracket · crackedLEFT WING CENTER L/E INBOARD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED ATTACH BRACKET WITH SERVICEABLE BRACKET PN 600-12045-11 IAW CRJ MM 20-21-00. Nov 21, 2007 · N879AS · Cndair CL6002B19 · Wing, Attach FittingsSDR TRAX200701765Angle · crackedFS 280 LBL 9 ANGLES CRACKED I/B AND O/B. FS 280LBL 9 O/B CLIP ANGLE WAS REPLACED PER REO 601R-53-21-787. Nov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701764Floorbeam · crackedFS 280 AFT ANGLE CRACKED O/B OF LBL 9 AND RBL 9. CUT AWAY DAMAGED SECTION OF FS280 AFT ANGLE IAW REO 601R-53-11-136. PERFORMED LPI PER NDTM 51-20-08 ON LT & RT CUT LINES TO ENSURE DAMAGE REMOVAL IAW REO 601R-53-11-136 (NO DEFECTS NOTED AT THIS TIME). FABRICANov 21, 2007 · N879AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200701771Placard · wornAAR - ALL PLACARDS ON CREW ESCAPE HATCH EXTERIOR ARE WORN. Nov 19, 2007 · N879AS · Cndair CL6002B19 · Placards and MarkingsSDR TRAX200701755Fitting · crackedAAR - O/B 280 CLIP AT LBL 9 ON FLOORBEAM HAS A SUSPECTED CRACK. DUPLICATE, REFER TO W/O: 50229 W/C 1000-0041 FOR CORRECTIVE ACTION. SUPPLEMENTAL - SDR CLOSED 11/27/07. Nov 19, 2007 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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