N856AS

Service difficulty reports · 339

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 = 'N856AS' 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 ASOA201101993Cargo Track · corrodedCARGO TRACK LBL 9 IS CORRODED. (OPEN)Oct 18, 2011 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101992Floorbeam · corrodedFLOORBEAM BETWEEN LBL 9 & 18 AT FS 589 CORRODED. BLENDED CORROSION, MAX REMOVED MATERIAL .006 IAW SRM 51-21-06. REPAIR CLASSIFIED AS MINOR.Oct 18, 2011 · N856AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101991Floorbeam · corrodedFLOORBEAM CAP AT LBL 27 FROM FS 559+112 TO FS 621 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND OUT OF LIMITS, REPAIRED IAW REO 601R-53-51-174.Oct 18, 2011 · N856AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101990Isolator · crackedFS 621 PRESSURE BULKHEAD HAS ONE CRACKED ISOLATOR AT RBL 27. REPLACED FOUR RIVETS. REPLACED ISOLATOR IAW SRM 51-42-06. REPAIR IS CLASSIFIED AS MINOR.Oct 18, 2011 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201101984Angle · crackedLEFT UPPER OBLIQUE ANGLE CRACKED FS 625. R & R OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21. MINOR REPAIR.Oct 17, 2011 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900874Angle · crackedFS 621 TO FS 625 RT UPPER OBLIQUE ANGLE RBL 45.0 STR 14R CRACKED IN RADIUS 1.25 INCH.Aug 11, 2009 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900861Bracket · crackedFS 621 FWD PRESSURE BULKHEAD HAS A CRACKED ISOLATOR BRACKET JUST ABOVE WL 106 AT LBL 18.Aug 7, 2009 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900916Sign · brokenSERVICE DOOR UPPER SURROUND EXIT SIGN IS BROKE.Aug 5, 2009 · N856AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA200900866Pressure Panel · damagedWHILE PERFORMING HFEC INSPECTION OF FS 460.00 PRESSURE FLOOR MULTIPLE INDICATIONS OF VARYING LENGTHS WERE NOTED APPROX 1.25 INCH FWD OF INTERCOSTALS IN THE THREE BAYS BETWEEN LBL 18.00 AND RBL 9.00. INDICATIONS RANGE FROM 30 - 60 PERCENT FSH. FAILS NDT INSPECAug 5, 2009 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900852Frame · crackedFRAME 718.0 HAS A .025 INCH LONG CRACK FROM TOP RIVET TO EDGE OF ATTACHING POINT JUST BELOW STR 11R ON FWD SIDE OF FRAME MEMBER. TRIMMED CRACKED FLANGE PER REO 601R-53-61-193 REV A, VIEW C. C/W LPI OF THE RT FRAME 718.0 REPAIR CUT LINE PER REO 601R-53-61-193Aug 5, 2009 · N856AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200900851Bulkhead · damagedRIGHT FS 559 BULKHEAD WEB HAS 2 INDICATIONS NOTED: 1) O/B OF RBL 9.0 WL 58.70 APPROX .2 INCH IN LENGTH 80 PERCENT FSH, 2) I/B OF RBL 18.0 WL 59.10 APPROX .3 INCH IN LENGTH 80 PERCENT FSH. BOTH AREAS FAILED NDT INSPECTION.Aug 5, 2009 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900846Bulkhead · damagedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .1 INCH IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. C/W REO 601R-53-61-1230 STEPS 1-24 REPAIR TO PRESSURE BULKHEAD WEB FS 621 LINTEL REV D.Aug 4, 2009 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900724Light · inoperativeCABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP INOP.Jun 26, 2009 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900723Light · brokenFLIGHT ATTENDANT WARDROBE OUTBOARD EMERGENCY LIGHT BASE BROKEN.Jun 26, 2009 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900514Windshield · crackedF/O'S WINDSHIELD CRACKED ON DESCENT BELOW 12000 FEET. EMERGENCY DECLARED.May 3, 2009 · N856AS · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA200900462Anchor Fitting · crackedASD AFT ANCHOR FITTING CRACKED.Apr 18, 2009 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900035Flap · failedFLAP FAIL AT 45 DEGREES. EMERGENCY DECLARED.Jan 2, 2009 · N856AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA200801726Sign · missingEXIT SIGN MISSING BY MAIN CABIN DOOR.Dec 26, 2008 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200801075Handle · brokenPAX DR OUTER HANDLE BROKENAug 31, 2008 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200800905Shear Pin · inoperativeSERVICE DOOR SHEAR PIN RELEASE HANDLE INOPERATIVE. FLT 4497. REMOVED AND REPLACED SERVICE DOOR SHEAR PIN OPS CHECKED GOOD. IN ACCORDANCE WITH AMM 42-41-00. OK FOR SERVICE. (B)Jul 12, 2008 · N856AS · Cndair CL6002B19 · Service DoorsSDR TRAX200800860Handle · lack of lubeMAIN CABIN DOOR COULD NOT BE OPENED FROM OUTSIDE. COMPLIED WITH INSP OF PAX DOOR HANDLE CLEARED AND LUBE HANDLE OPS CHECK GOOD OK FOR SERVICE PER CRJ200AMM52-10.--[SDR CLOSED](B)Jul 1, 2008 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200800388Light · inoperativeFWD FACING OVERWING EMERGENCY EXIT LIGHTS IN CEILING INOP. RESET SYS C/B.Mar 7, 2008 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200800308Flap · failedWHEN SELECTING FLAPS FROM 0 DEG TO 8 DEG ON APPROACH, FLAPS FAILED AT 2 DEG. FLAPS FAIL MESSAGE. EMERGENCY DECLARED.Feb 22, 2008 · N856AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701938Light · inoperativeEMERGENCY EXIT CEILING LIGHT INOP.Dec 15, 2007 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200701347Battery · dischargedCAPTAIN`S FLASHLIGHT INOP. WILL NOT TURN OFF. BATTERY DEAD.Sep 14, 2007 · N856AS · Cndair CL6002B19 · Emergency EquipmentSDR TRAX200700597Light · detachedEMERGENCY LIGHT AT TOP OF ENTRY DOOR NEED TO BE REATTACHED. FLT 4568 DEL 69 MINS.May 1, 2007 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200700581Charger · defectiveTROUBLESHOT EMERGENCY LIGHTS FOUND NR 1 BATTERY MOUNT CHARGER UNIT DEFECTIVE.Apr 27, 2007 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200700570Light · inoperativeASD FLOOD LIGHT AND BOTH FWD EXTERIOR EMERGENCY LIGHTS INOP.Apr 25, 2007 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200700514Frame · corrodedFS 333 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY REMOVED FASTNERS ,BLENDED FS 333 FRAME IAW CRJ 200 SRM 51-21-06.Apr 11, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200700513Frame · corrodedFS 349 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY CORROSION WAS REMOVED UNDER THE TWO CLIPS ON FS 349 IAW CRJ 200 SRM 51-21-06.Apr 11, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200700516Fitting · crackedRIGHT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW RIGHT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 11, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700515Fitting · crackedLEFT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW LEFT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 11, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700509Support Bracket · crackedCARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET CRACKED (MARKED). REMOVED AND REPLACED CARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET PER CRJ 200 SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 10, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700491Skin · crackedVERTICAL L/E UPPER CORNER CRACKED ON RIGHT SIDE. CUT AWAY DAMAGED AREA (C/W STEPS 1AND 2) IAW REO 601R-55-32-165 CB7015474. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 8, 2007 · N856AS · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR TRAX200700493Floor Skin · corrodedCORROSION ON RIGHT PRESSURE FLOOR FROM FS 460 TO FS 513. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.Apr 8, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700492Floor Skin · corrodedCORROSION ON LEFT SIDE PRESSURE FLOOR SKIN FROM FS 460 TO FS 513. [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.Apr 8, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700500Floor Support · corrodedSTA 280 FWD AND AFT FLOOR SUPPORT ANGLES CORRODED AT BL 0. REMOVED FWD FLOOR SUPPORT ANGLE REF CRJ200SRM 51-42-06, AFT FLOOR SUPPORT ANGLE WILL BE REPAIRED ON N/R-00090 W/O 55779. PSP19749 10APR07. INSTALLED NEW FWD FLOOR SUPPORT ANGLE PER CRJ 200 SRM 51-42Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700498Beam · corrodedMINOR SURFACE CORROSION STA 349 TRANSVERSE BEAM LOWER SURFACE LT SIDE AT LBL 36 (MARKED). REMOVED AND BLENDED UNDER TEFLON STRIP AND ON THE UNDERSIDE OF 349 AT LBL 36, FOUND TO BE WITHIN LIMITS, .059 MATERIAL REMAINING PER CRJ 200 SRM 53-00-00. SEALED AND INApr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700484Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AT RBL 9. BEGAN REMOVING FASTENERS THROUGH LT AND RT STA 280 WEB AND RELATED STRUCTURE AS PER CRJ 200 SRM 51-42-00 AND REO 601R-53-11-926. EWB 702040900. CONTINUED REMOVAL OF ASSOCIATED PARTS. MADE CUT AND REMOVED CRACKED / CApr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700482Sill · corrodedMINOR SURFACE CORROSION RT SIDE FLOOR SILL RBL 36 STA 349 (MARKED). REMOVED SURFACE CORROSION IAW CRJ SRM 51-21-06. 04/08/2007. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700481Fitting · corrodedFLOOR SUPPORT STRINGER AFT CLEAT (CUT OUT CUP FOR HANDRAIL ARM) CORRODED. BLENDED AND REMOVED AFT CUP, FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00 BAT 23167. DRILLED UP NEW AFT CUP REF CRJ-200 SRM 51-42-06, AND ADDED NEW NUT PLATES. INSTALLED NEW CUPApr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700499Beam · corrodedSTA 349 TRANSVERSE BEAM RT SIDE CORRODED AT RBL 36 (MARKED). REMOVED CORROSION IAW CRJ200 SRM 51-21-06.Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700497Stringer · corrodedFLOOR SUPPORT STRINGER AT PAX DOOR SILL CORRODED AND MISSING NUT PLATES (MARKED). BLENDED AND REMOVED STRINGER AND AFT CUP BOTH FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00. DRILLED UP NEW PAX DOOR SILL REF CRJ-200 SRM 51-42-21, AND CRJ-200 SRM 51-42-0Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR TRAX200700485Fitting · crackedSTA 280 RBL 9 AND LBL 9 INBOARD CLIPS CRACKED.Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200700483Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AT LBL 9.Apr 7, 2007 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700475Support Beam · crackedRT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD INBD NUT PLATE FOR ACCESS PANEL [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.Apr 6, 2007 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR TRAX200700474Support Beam · crackedLT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD IB NUT PLATE FOR ACCESS PANEL. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.Apr 6, 2007 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR TRAX200700224Light · inoperativeAFT EMERGENCY FLOOR LIGHT INOP.Feb 13, 2007 · N856AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200700140Unknown · unknownAFTER ROTATION -STEERING INOP- CAUTION. AFTER LANDING ROLLOUT TURNED ON NWS PER MX CTL. STEERING INOP MSG CAME ON AGAIN. EMERGENCY EQUIPMENT ON STANDBY. FLTS 4785, 4762 CX.Jan 31, 2007 · N856AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR TRAX200700108Light · brokenFLOOR LEVEL LIGHTS BETWEEN 6CD BROKEN.Jan 17, 2007 · N856AS · Cndair CL6002B19 · Emergency Lighting
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