N858AS

Service difficulty reports not matched to an aircraft · 141

They name N858AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N858AS' AND registry_match IS NULL
  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 ASOA201705301633Wheel · brokenSUPPORT WHEEL BROKEN. PASSENGER DOOR ASSEMBLY REMOVED AND REPLACED, OPS CHECKED GOOD . ACFT OK FOR CONTINUED SERVICE.May 30, 2017 · N858AS · Bombdr CL6002D15 · Passenger/Crew DoorsSDR ASOA2015121814232Wire · damagedEXIT LIGHT ON F/A STATION INOPERATIVE. R & R WIRE SPLICE CONNECTOR ON EMERGENCY LIGHT, DS10LN, IAW ESPM 20-17-31. OPS TEST GOOD.Dec 18, 2015 · N858AS · Cndair CL6002B19 · Light System WiringSDR ASOA2015121714231Wire · brokenEXIT LIGHT TRIM PANEL NEXT TO GALLEY 1 HAS A BROKEN WIRE. TERMINATED FEMALE SPLICE CONNECTOR FOR EXIT LIGHT ON RT FWD DOOR TRIM IAW ESPM 20-17-31. PERFORMED OPS TEST OF EXIT LIGHT IAW AMM 33-51-00, EXIT LIGHT PASSED, OPS TEST.Dec 17, 2015 · N858AS · Cndair CL6002B19 · Light System WiringSDR ASOA2015112914227Floor Support · corrodedFLOORBEAM CAP CORRODED BETWEEN FS 554.00 +64 AND FS 559.0+45 AT RBL9. REMOVED CORROSION FROM FLOORBEAM AT RBL 9 BETWEEN FS 559.00+48-559.00+64 IAW SRM 51-21-06. REPAIR OR REPLACE BLEND AREA OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH SRM FLOOR SUNov 29, 2015 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015112914185Floorbeam · corrodedFLOORBEAM CORRODED AT FS 621.00, RBL9. REMOVED CORROSION FROM FLOORBEAM AT FS621 AT RBL9 IAW SRM 51-21-06. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43 AND SRM 53-00-00. DRILLED NEW SERIVCABLE FLOORBEAM AT RBL9, FS 559+112 TO FS 621 IAW SRM 51-40-11. Nov 29, 2015 · N858AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015112814226Floorbeam · corrodedCORROSION ON RBL 9 FLOORBEAM CAP FWD OF FS 409.00 + 16. REMOVED CORROSION ON RBL9 FLOORBEAM CAP FWD PF FS 409.00+16 IAW SRM 51-21-06. REPAIRED IAW SRM 53-00-43. FLOOR SUPPORT STRUCTURE REPAIR NR 2.Nov 28, 2015 · N858AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015112814225Seat Track · corrodedRBL9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN FS 409 +112 AND FS 394. REMOVED CORRODED SEAT TRACK AT RBL9, FS 394-FS 409+112 IAW TASK 53-01-11-000-802. DRILLED & COUNTERSUNK REQUIRED HOLES IAW SRM 51-40-11 HOLES ALODINED IAW SRM 51-21-11. INSTALLED NEW Nov 28, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112814224Seat Track · corrodedLBL9 SEAT TRACK CORRODED AND OUT-OF-LIMITS AT FS 394 TO FS 409 + 112. REMOVED SEAT RAIL AT FS 394 - FS 409+112 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL AT FS 394-FS406+112 LBL9 IAW AMM 53-01-11-400-802. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485,Nov 28, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112814179Seat Track · corrodedRBL9, SEAT TRACK CORRODED AND OUT-OF-LIMITS BETWEEN FS 364 TO 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802.Nov 28, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112814178Seat Track · corrodedLBL 9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN BS 364 - 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802.Nov 28, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714177Intercostal · corrodedBAY DOOR INTERCOSTAL AT BS 349-409 BETWEEN STR 26 AND 27L IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. INTERCOSTAL AT FS 394-FS 409 BETWEEN STR 27-26L IS OUT OF LIMITS IAW SRM 51-21-06. REMOVED IAW SRM 51-42-06. INSTALLED INTERCOSTAL AT FS 394-FS 409 BENov 27, 2015 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015112714176Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK FS409+16-409+112 HAS CORROSION. REMOVED CORROSION ON RT SIDE SEAT RAIL BETWEEN FS 409+16-409+112 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED RT SEAT RAIL AT FS409+16-409+112 IAW AMM 53-01-11-000-802Nov 27, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714175Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK FS364-409.16 HAS CORROSION. REMOVED CORROISON ON RT SIDE SEAT RAIL BETWEEN FS364-409+16 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SIDE SEAT TRACK IAW AMM 53-01-11-000-802, FABRCATED NEW SNov 27, 2015 · N858AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112414223Skin · crackedFUSELAGE SKIN IS CRACKED AT FS 235.00 S26R. RECIEVED AND COMPLIED WITH REO 601R-53-11-2844. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV C.Nov 24, 2015 · N858AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015112414222Floor Panel · crackedBS 193 ELECTIRCAL BAY FLOOR CRACKED RT SIDE. REPAIRED ELECTRICAL BAY FLOOR AT BS 193.0, RT SIDE, IAW GREO 601R-53-11-111. UPON FURTHER EVALUATION FOUND GREO 601R-53-11-111 TO NOT BE APPLICABLE TO RT SIDE FS 193 ELECTRICAL BAY FLOOR CRACK REPAIR CANCELED ECTNov 24, 2015 · N858AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2015102813980Handle · fouledF/A REPORT MAIN AIR SERVICE DOOR IS HARD TO OPEN. FOUND FOD AT MAIN PAX DOOR LEVEL HANDLE. REMOVED FOD. OPS CHECK TEST GOOD, REF AMM 52-11-21.Oct 28, 2015 · N858AS · Cndair CL6002B19 · Service DoorsSDR ASOA2015102013934Inverter · unserviceableRT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R INVERTER NR 3 IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Oct 20, 2015 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015101113886Lamp · burned outEXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD.Oct 11, 2015 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015100513869Fitting · damagedUPPER ATTACH FITTINGS HAD TOOL DAMAGE ON BOTH INBD FACES. BLENDED IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS IAW SRM 55-11-27. REPAIRED IAW REO 601R-55-11-522. CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3.Oct 5, 2015 · N858AS · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR ASOA2015030412317Sign · missingCEILING EXIT SIGN MISSING. INSTALLED CEILING EXIT SIGN IAW AMM 33-51-14.Mar 2, 2015 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014073010984Lens · missingFWD CABIN ENTRANCE EMERGENCY FLOOR FLOOD LIGHT COVER MISSING. INSTALLED LENS IAW AMM 33-51-19. OP'S CHECKED GOOD.Jul 27, 2014 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014062310715Bulb · burned outRT EXTERIOR NR 6 EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS TEST OF EXTERIOR EMERGENGY LIGHTS, REPLACED THE BULBS AS REQUIRED IAW AMM 33-51-00. OPS CHECKED GOOD.Jun 19, 2014 · N858AS · Cndair CL6002D24 · Emergency LightingSDR ASOA2014031910157Skin · damagedA HOLE IS IN THE SKIN OF THE AC RT SIDE AT THE FWD END OF THE FLAP STUB FAIRING THIS WAS FOUND WHILE GIVING AN OK TO INSTALL THE RT FLAP STABILIZER FAIRING. COMPLIED WITH REO 601R-53-41-610. COMPLIED WITH EC/TC REO 601R-53-41-610 IAW REO 601R-53-41-601.Mar 10, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014031910156Window Frame · crackedWINDSHIELD CENTER POST LOWER RT FITTING CRACKED. REMOVED FITTING ON W/S CENTER POST LWR RT SIDE IAW SRM 51-42-21. DRILLED UP NEW FITTING IAW SRM 51-40-11. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. INSTALLED FITTING IAW SRM 51-42-21 AND DWGFeb 27, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014031910155Floor Support · corrodedUPPER LT FLOOR SUPPORT FITTING CORRODED. LOCATED & DRILLED NEW UPPER LT FLOOR SUPPORT FITTING IAW DWG 601RR38672-7 & SRM 51-42-06. INSTALLED NEW SERVICEABLE FITTING IAW DWG 601R38672 & SRM 51-42-06.Feb 24, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031910154Strap · crackedLEFT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED STRAP IAW SRM 51-42-20-00 AND SRM 51-42-06-00. INSTALLED IAW SRM 51-42-06, 51-42-20 DWG 601R-10336, REV-H.Feb 20, 2014 · N858AS · Cndair CL6002B19 · Wing Miscellaneous StructureSDR ASOA2014031910153Insert · damagedFLOOR PANEL 282HRF HAS DAMAGED SCREW INSERTS. REMOVED AND INSTALLED NEW INSERTS IAW C AND D RPM 25-6000-1.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014031910152Frame · corrodedFRAME BS 349 CORRODED BETWEEN S25L AND 26R. R & R FRAME SECTOR IAW SRM 51-42-06-00, 51-42-21-00 AND DWG 601R32005. MAJOR REPAIR.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014031910151Frame · corrodedFRAME BS 333 CORRODED BETWEEN S26 - 27L. REMOVED CORROSION IAW SRM 51-21-06 AND 51-12-00. COMPLIED WITH PERMANENT REPAIR EA 12-2014-046 NDTM PT-1, 51-20-06.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014031910150Floor Support · corrodedLEFT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439-544. COMPLIED WITH ECTC REO 601R-53-41-666.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031910149Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439 - 516. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031910148Bulkhead · gougedSCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE BETWEEN LBL 18.00 & LBL 27.50 JUST ABOVE WL 73.50. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH STEP 2 OF REO 601R-53-61-2155.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014031910147Bulkhead · gougedSCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE AT RBL 36.20 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH REO 601R-53-61-2155.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014031910146Bulkhead · gougedSCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 27.50 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH REO 601R-53-61-2155.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014031910145Bulkhead · gougedSCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 18.00 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. COMPLIED WITH REO 601R-53-61-2155.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014031910144Panel · damagedSTAB TIP PANEL 343AR ERODED. REPAIRED ERODED TIP ON TAB PANEL 343AR IAW SRM 51-15-52 AND SRM 51-74-02. REPAIRED LIGHTING PROTECTION STRIP IAW D/G DOCUMENT 7101569,Feb 19, 2014 · N858AS · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR ASOA2014031910143Hinge · gougedPASSENGER DOOR HINGE FUSELAGE SIDE 15TH LUG FROM FRONT IS GOUGED. COMPLIED WITH REO 601R-53-21-814, REV. MAJOR REPAIR.Feb 19, 2014 · N858AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2014031910142Angle · corrodedPAX DOOR SILL LOWER ATTACH ANGLE MISSING. INSTALLED SILL ANGLE IAW DWG 601R-31-527-221, 51-42-21, 51-42-13, 51-42-06, SRM 51-22-00. MAJOR REPAIRFeb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031910141Strap · crackedRT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED AND REPLACED STRAP IAW SRM 51-42-20-00 & SRM 51-42-06-00 & DWG 601R10336.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Wing Miscellaneous StructureSDR ASOA2014031910140Structure · crackedTRU SHELF CRACKED LT SIDE OTBD OF SERVICING GAUGE, BS 193. COMPLIED WITH REO 601R53-11-081. RECEIVED AND COMPLIED WITH REO 601R-53-2634. MAJOR REPAIR.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014031710139Floor Support · crackedCOCKPIT FLOOR SUPPORT AFT LT CORNER CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED AND DRILLED HOLES ON NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031710138Attach Angle · crackedAFT BULKHEAD ZEE MEMBER TO SKIN ATTACH ANGLE APPEARS CRACKED. REMOVED ATTACH ANGLE AT FS 625 & STR16L IAW SRM 51-42-06 & SRM 51-42-21. REMOVED & DRILLED UP NEW ATTACH ANGLE REF SRM 51-40-11. INSTALLED ATTACH ANGLE REF SRM 51-42-06 & SRM 51-42-21 & DWG 601R3Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014031410137Lug · gougedPAX DOOR HINGE LUG 2, 5, 8, 14, 19 & 25 GOUGED. COMPLIED WITH REO 601R-52-11-1347. COMPLIED WITH ECTC REP 601R-52-11-1347. MAJOR REPAIR.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2014031410136Angle · crackedLT FS 625 ANGLE BROKEN ON T/E. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21, DWG 601R350126 AND 601-35012.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014031410135Panel · damagedPANEL 121AL HAS ERROSION DAMAGE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLETED REPAIR OF PANEL 121AL IAW SRM 51-74-02.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Standard Practices/StructuresSDR ASOA2014022710029Floorbeam · crackedUPPER RADIUS OF FLOORBEAM ANGLE CRACKED, RBL 9 BS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-21.Feb 18, 2014 · N858AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2013122009673Flashlight · intermittentCAPTAIN`S FLASHLIGHT GOES IN AND OUT. R & R FLASHLIGHT IAW AMM 25-61-02.Dec 19, 2013 · N858AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2013022803082Lamp · burned outCABIN CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT AT 4-5CD IAW AMM 33-51-16, OPS CHECKED GOOD.Feb 24, 2013 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201200504Wire · damagedLEFT 14TH STAGE BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED. REPAIRED WIRE AT LT PYLON IAW ESPM 20-16-00, PERFORMED OPS TEST OF BLEED LEAK DETECTION SYS IAW AMM 36-21-00-710-801. NO FAULT AT THIS TIME.Feb 15, 2012 · N858AS · Cndair CL6002B19 · Fire Protection System WiringSDR ASOA2012012500333Angle · corrodedAFT CORNER OF ASD ON HINGE END IS CORRODED. REMOVED AFT CORNER OF ASD AT HINGE END CORRODED. INSTALLED AFT CORNER OF ASD HINGE END IAW SRM 51-42-06, 51-42-13. REPAIR CLASSIFIED AS MAJOR.Jan 25, 2012 · N858AS · Cndair CL6002B19 · Passenger/Crew Doors
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