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 ASOA2013111909423Skin · crackedFOUND RT LOWER WING FUEL ACCESS HOLE 650BB INBD LANDING HAS MULTIPLE INDICATIONS NOTED 5.0" IN L X .250" W 50 PERCENT FSH FAILED NDT INSPECTION. C/W ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV K.Oct 31, 2013 · N879AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013111909422Skin · crackedLOWER WING PLANK RT BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES 60 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-57-21-2022, REV.Oct 29, 2013 · N879AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013111909421Floor Support · corrodedLEFT FLOOR SUPPORT HAS CORROSION AT FS 473.15 & 461. REMOVED CORROSION IAW SRM 51-21-06 & REO 601R-53-41-666. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.Oct 27, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111909420Support Beam · crackedFOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .5 IN LENGTH. REMOVED SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21. LOCATED FASTENER HOLES IN NEW SERVICEABLE SUPPORT BEAM AFT LOWER ANGLE AND INSTALLED IAW SRM 51-40-11 & 51-42-21.Oct 26, 2013 · N879AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013111909419Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION LBL 27.50, WL 130 APPROX .4 INCHES IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION, COMPLIED WITH REO 601R-53-61-1541 AND ECTC REO 601R-53-61-1541.Oct 26, 2013 · N879AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013111909418Floor Panel · corrodedRT PRESSURE FLOOR PANEL JUST FORWARD OF BS 559 HAS CORROSION AROUND NUTPLATE HOLE. REMOVED CORROSION IAW REO 601R-53-41-666 & SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666 REV C.Oct 26, 2013 · N879AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2013111509410Floor Support · corrodedRIGHT PRESSURE FLOOR SUPPORT HAS AREA OF CORROSION AT FS 513. REMOVED CORROSION IAW SRM 51-21-06 & REO 601R-53-41-666. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.Oct 26, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509409Floor Support · corrodedLEFT PRESSURE FLOOR ANGLE HAS AREA OF CORROSION AT BS 513. REPAIRED IAW ECTC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.Oct 26, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509408Post · crackedFOUND FS 409+128 VERTICAL POST LBL 18, HAS A CRACK INDICATION AT AFT FLANGE RADIUS APPROX .2 INCHES IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED VERT POST ASSY IAW SRM 51-42-06. INSTALLED SERVICEABLE POST ASSY IAW SRM 51-42-06, REO 601R-53-41-88Oct 23, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509407Post · crackedFOUND FS 409+128, VERTICAL POST BL 0, RT SIDE HAS A CRACK INDICATION AT AFT FLANGE RADIUS APPROX .4 INCHES IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06 AND 51-42-21. DRILL & LOCATED NEW SERVICEABLE POST ASSY. IOct 23, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509406Attach Fitting · crackedLEFT ENGINE FRONT FRAME AFT HUB ATTACH FLANGE CRACKED AT BOLT HOLE ABOVE AGB MOUNT AT 9 O'CLOCK POSITION OF ENGINE. C/W ECTC CF34-3 ENG CHANGE. RECEIVED ALL APPLICABLE PARTS CERTIFICATION PAPERWORK PERTAINING TO LT ENG REPLACEMENT FROM STORES DEPT.Oct 23, 2013 · N879AS · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR ASOA2013111509405Isolator · crackedAFT PRESSURE BULKHEAD HAS ISOLATOR CRACKED. REMOVED ISOLATOR IAW SRM 51-42-06. INSTALLED NEW ISOLATOR IAW SRM 51-42-06.Oct 23, 2013 · N879AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013111509404Angle · crackedRT FS 484 FLOOR SUPPORT REPAIR ANGLE CRACKED AT RBL 36.0. COMPLIED WITH EO CL600-2B19-53-I00449.Oct 21, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509403Angle · crackedLEFT FS 484 FLOORBEAM REPAIR ANGLE CRACKED AT LBL 36.0. REMOVED CRACKED ANGLE IAW SRM 51-42-06. REPLACED ANGLE IAW REO 601R-53-41-059 AND W/O 312243.Oct 21, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509402Vertical Beam · crackedLEFT FS 409+128 VERTICAL BEAM AT LBL 27 SHOWS VISUAL SIGNS OF A CRACK ON INBD SIDE AT BOTTOM RIVET. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056 REV F. REPAIRED VERTICAL BEAM IAW REO 601R-53-41-056, REV F, DATED 9-2-11.Oct 20, 2013 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013111509401Light · brokenEXIT FLOORLIGHT ON BOTTOM OF THE ENTRY WARDROBE IS BROKEN. R & R FLOODLIGHT IAW MM 33-51-19-000-801/400-801. PERFORMED SUCCESSFUL OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801.Oct 18, 2013 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013031903238Lamp · burned outINTERIOR CEILING EMERGENCY LIGHT OUT AT ROW 10. R & R LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.Mar 15, 2013 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012081702077Pump · malfunctionedHYD SYS 3 INDICATED 20 PERCENT, SELECTED HANDLE DOWN, RECEIVED NOSE GEAR GROUND INDICATION, THEN RECEIVED MAIN DISAGREE MSG. PERFORMED LANDING GEAR MANUAL EXT EMERGENCY DECLARED AS A PRECAUTION. R & R 3A HYD PUMP IAW AMM 29-12-03. R & R NLG SELECTOR VALVE IAug 13, 2012 · N879AS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR ASOA201200913Bulb · burned outEMERGENCY LIGHT AT SERVICE DOOR IS INOPERATIVE. R & R BULBS. OP'S CHECKED GOOD.Mar 16, 2012 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201200560Light · inoperativeTHE MIDDLE LEFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW THE AMM 33-51-21. OPS CHECKED GOOD.Feb 22, 2012 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201200242Lamp · inoperativeAFT WING EMERGRNCY LIGHT INOPERATIVE. RELAMPED AFT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jan 21, 2012 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102311Anchor Fitting · crackedPAX DOOR FWD ANCHOR FITTING CRACKED. R & R PAX DOOR FWD ANCHOR FITTING IAW AMM TASK 52-11-17-000-804 & 52-11-17-400-804.Dec 2, 2011 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102252Seat Track · corrodedRT SIDE SEAT TRACK CORRODED AT FS 349.00 TO 409.00. CORROSION OUT OF LIMITS. R & R SEAT TRACK SECTION IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Nov 23, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102230Seat Track · corrodedLT SIDE SEAT TRACK CORRODED FROM FS 349 TO 409. REMOVED MINOR CORROSION FROM SEAT TRACK, REMOVAL FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-21-49-FIG 1.Nov 23, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102343Sill · corrodedCABIN AREA SERVICE DOOR SILL CORRODED BY AFT THRESHOLD ATTACHMENT BRACKET. REMOVED CORRODED ANGLE AT SERVICE DOOR SILL IAW SRM 51-42-21, CORROSION EXCEEDS ALLOWABLE DAMAGES IAW SRM 53-21-23. LOCATED AND DRILLED NEW SILL SURROUND IAW SRM 51-40-11, INSTALLED Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201102342Floor Support · corrodedPAX DOOR SILL, AFT HAND RAIL STOWAGE CUP FLOOR SUPPORT CLIP CORRODED. R & R CLIP AT PAX DOOR SILL, AFT SIDE IAW SRM 51-42-06. THIS IS A MINOR REPAIR.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2011111802292Anchor Fitting · crackedPAX DOOR AFT ANCHOR FITTING CRACKED. R & R PAX DOOR AFT ANCHOR FITTING IAW AMM TASK 52-11-17-000-804 & 52-11-17-400-804.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2011111802291Anchor Fitting · crackedPAX DOOR FWD ANCHOR FITTING CRACKED. R & R WITH NEW ANCHOR FITTING IAW SRM 51-42-21.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102251Attach Fitting · crackedCABIN AREA, AFT BS 280 HAS CRACKED ATTACH FITTING AT STR 3L. REMOVED CRACKED ATTACH FITTING IAW SRM 51-42-21 AND 51-42-06. DRILLED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21, 51-42-06 AND 51-23-00.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201102215Sill · corrodedCARGO COMPARTMENT LT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 559.00 AND FS 559.00+112 AROUND FASTENER HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06. PEFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERINov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201102214Sill · corrodedCARGO COMPARTMENT RT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 574.00+86 AND 559.00+112 AROUND FASTENER HOLES CORRODED. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL RENov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201102213Sill · corrodedCARGO COMPARTMENT RT FLOOR SILL UPPER SURFACE BEWTEEN SURFACE BETWEEN FS 574.00 AND FS 589.00 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3. MIN MATERIAL REMAINING IS .048". BLENDNov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201102212Tie Down · corrodedCARGO COMPARTMENT RBL 27.00 BETWEEN FS 559.00+80 AND FS 559.00+96 HAS 1EA TIE DOWN TRACK SEGMENT CORRODED. R & R TIE DOWN TRACK SEGMENT IAW SRM 51-41-04, 53-61-49.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102211Tie Down · corrodedCARGO BAY RBL 9.00 BETWEEN FS 559.00+85 AND FS 574.00 HAS 2EA TIE DOWN TRACK SEGMENT CORRODED. R & R TIE DOWN TRACKS IAW SRM 51-41-02 AND SRM 53-61-49-00, FIG 2. MINOR REPAIR.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102210Tie Down · corrodedCARGO BAY LBL 9.00 BETWEEN FS 559.00+85 AND FS 621.00 HAS 3EA TIE DOWN TRACK SEGMENT AND 2EA TIE DOWN PUCKS CORRODED. R & R CORRODED TIE DOWN TRACKS IAW SRM 51-41-02.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102209Tie Down · corrodedCARGO BAY LBL 27.00 BETWEEN FS 559.00+80 AND FS 574.00 HAS 1EA TIE DOWN TRACK SEGMENT AND 3 EA TIE DOWN PUCKS CORRODED. REMOVED TIE DOWN IAW AMM 53-01-11-000-802. INSTALLED TIE DOWN IAW AMM 53-01-11-400-802.Nov 18, 2011 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102250Attach Fitting · corrodedWHILE REMOVING FOAM FROM UPPER PART OF AIRSTAIR DOOR, FOUND 3 EA ATTACH FITTINGS CORRODED. R & R 3 EA CORRODED FITTINGS IAW 51-40-11, 51-42-06, & 51-23-00.Nov 17, 2011 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102249Attach Fitting · crackedCABIN AREA BS 280 CLIP CRACKED AT RBL 9 OTBD SIDES. REMOVED IAW SRM 51-42-20. FABRICATED IAW REO 601R-53-11-171. INSTALLED IAW SRM 51-42-21 AND REO 601R-53-11-171.Nov 17, 2011 · N879AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201102204Drag Angle · crackedPAX DOOR DRAG ANGLE CRACKED AT RADIUS JUST ABOVE DOOR ASSIT MOTOR PULLEY BRACKET. . R & R DRAG ANGLE IAW REO 601R-52-11-513.Nov 16, 2011 · N879AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102195Skin · corrodedSERVICE DOOR LOWER SKIN CORRODED UNDER SCUFF PLATE AFT SECTION. REMOVED CORROSION IAW SRM 51-21-06, STEP 3B, RESTORED FINISH IAW SRM 51-25-01. MINOR REPAIR.Nov 15, 2011 · N879AS · Cndair CL6002B19 · Service DoorsSDR ASOA201101988Flt Controls · erraticACFT AGGRESSIVELY ROLLED RT WHEN FLAPS SELECTED FROM 30 TO 45. REQUIRED MORE THAN HALF SCALE LWD AILERON TRIM, AT WHICH TIME AILERON CONTROL BECAME ERRATIC DURING NORMAL CORRECTIONS. THERE WAS 'NULL' ZONE AT CENTER OF AILERON TRAVEL AND 'JERKS' WITH SMALL LT Oct 17, 2011 · N879AS · Cndair CL6002B19 · Flight Control SystemSDR ASOA201101681Line · leakingSTRONG SMELL OF EXHAUST AND OR OIL FUMES IN COCKPIT AND CABIN. R & R APU FUEL SECONDARY MANIFOLD LINES IAW CMM 49-26-39. LEAK AND OPS CHECKED GOOD.Sep 8, 2011 · N879AS · Cndair CL6002B19 · APU Engine Fuel and ControlSDR ASOA201101308Bulb · burned outLT MIDDLE EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R LT MIDDLE EXTERNAL EMERGENCY LIGHT BULB. IAW AMM 33-51-21. OP'S CHECKED GOOD.Jul 9, 2011 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100543Terminal · arcedF/O WINDSHEILD ARCHING IN FLIGHT COMPLIED WITH QRH PROCEDURES. R & R F/O'S WINDSHEILD IAW AMM 56-11-01. OPS TEST GOOD LEAK CHECK REQUIRED. (CLOSED)Mar 21, 2011 · N879AS · Cndair CL6002B19 · Ice/Rain Protection System WiringSDR ASOA201100007Bulb · burned outRT AFT FUSELAGE EMERGENCY LIGHT INOP. REMOVED THE INOP BULB AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECK GOOD.Jan 1, 2011 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001993Lamp · inoperativeAFT MOST LT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED AFT MOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED AFT MOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.Dec 19, 2010 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001533Placard · missingEXIT PLACARD ON ASD MISSING. INSTALLED EXIT PLACARD ON AIR STAIR DOOR IAW AMM 11-30-00. CLEARED PLACARD REMOVED.Oct 10, 2010 · N879AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000291Light · brokenFLOOR EMERGENCY STRIP BROKEN NEAR LAV ON LT. SECURED EMER FLOOR STRIP IAW AMM 25-60-00. (CLOSED)Feb 21, 2010 · N879AS · Cndair CL6002B19 · Emergency LightingSDR ASOA20100012Sill · corrodedREPAIRED SILL IAW EC/TC REO 601R-53-21-326 IAW REO 601R-53-21-326 AND COMPLIED WITH EC/TC REO 601R-53-21-1084 IAW REO 601R-53-21-1084. LIGHTNING PORTECTIVE PANEL REQUIRES INSTALL. OK TO INSTALL LIGHTNING STRIKE PANELS. INSTALLED (3) LIGHTNING STRIKE PANELS Jan 5, 2010 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000012Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT STRUCTURE JUST FWD AND AFT OF FS 349.00 WL 72.5, RBL 45.0.Jan 5, 2010 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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