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 SWIA201844221Door Frame · crackedPAX DOOR FRAME CRACKED. REPAIRED THE DOOR FRAME IAW REO.Jan 11, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201844214Structure · crackedNLG WHEEL WELL IS CRACKED. REPAIRED IAW REO.Jan 8, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201844213Door Sill · corrodedCARGO DOOR SILL CORRODED. REPLACED THE CARGO DOOR SILL IAW REO.Jan 3, 2018 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744220Fitting · crackedESCAPE HATCH FITTING CRACKED. R&R ESCAPE HATCH FITTING IAW SRM.Dec 29, 2017 · N856AS · Cndair CL6002B19 · Emergency ExitsSDR SWIA201744219Floor Support · corrodedFLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM.Dec 27, 2017 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744218Access Panel · corrodedWING ACCESS PANEL IS CORRODED. REPAIRED THE DAMAGE IAW REO.Dec 26, 2017 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA201744237Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED SKIN IAW REO.Dec 21, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744236Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.Dec 18, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744234Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.Dec 18, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744233Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.Dec 18, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744232Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.Dec 18, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744217Frame · corrodedFRAME IS CORRODED. THE REPLACED FRAME SECTOR IAW SRM.Dec 16, 2017 · N856AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201744216Angle · corrodedSERVICE DOOR ANGLE IS CORRODED. REPLACED ANGLE IAW SRM.Dec 13, 2017 · N856AS · Cndair CL6002B19 · Service DoorsSDR SWIA201744230Floor Panel · corrodedPRESSURE FLOOR PANEL CORRODED. BLENDED AREA OF PRESSURE FLOOR PANEL IAW NDTM.Dec 8, 2017 · N856AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2016082215286Battery · dischargedFOUND EMERGENCY LIGHTS SWITCH IN THE ON POSITION, EMERGENCY LIGHTS INOPERATIVE. RECHARGED EMERGENCY LIGHT BATTERY SYSTEM WITH APU GENERATOR SYSTEM FOR 60 MIN SYSTEM RESET NO FURTHER FAULTS NOTED MCC, AC OK FOR SERVICE.Aug 22, 2016 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015112514131Charger · inoperativeEMERGENCY LIGHTS ARE INOPERATIVE, REQUIRES TROUBLESHOOTING. EMERGENCY LIGHTS ARE INOPERATIVE, TROUBLESHOOTING IS REQUIRED. UPON TROUBLESHOOTING, FOUND EMERGENCY LIGHT CHARGER ASSY NR 4 UNSERVICABLE. REMOVED UNSERVICABLE CHARGER ASSY AND REPLACED WITH SERVINov 25, 2015 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015110514122Floorbeam · corrodedCORROSION ON RBL 9 FLOORBEAM AROUND SCREW HOLE AT FS 559+112 UNDER PANEL 281 ALF. REMOVED CORROSION IAW SRM 51-21-06. DURING CORROSION REMOVAL, CORROSION FOUND TO PENETRATE 100 PERCENT OF FLOOR SUPPORT STRUCTURE. COMPLIED WITH SRM 53-00-43-02 FLOOR SUPPORT Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015110514114Seat Track · corroded2 EA SHORT SEAT TRACKS ON LBL9 CORRODED BETWEEN FS 559.80 TO 574. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION REMOVED IAW SRM 51-21-06, SRM 53-51-49, STATES TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIENov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514113Seat Track · corrodedSHORT SEAT TRACK ON RBL9 CORRODED BETWEEN FS 559+80 TO 559.96. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06, SRM 53-51-49 TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIED WITH EC/TNov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514112Floor Support · corrodedCORROSION AROUND 2 SCREW HOLES ON RBL27 FLOORBEAM BETWEEN FS 589 TO 605 UNDER PANEL 282KRF. REMOVED CORROSION IAW SRM 51-21-06. EVALAUTED BLEND AREAS AROUND 2EA SCREW HOLES ON RBL27 FLOORBEAM FS589 TO 605 AND FOUND THEM TO BE OUT OF ALLOWABLE DAMAGE LIMITS INov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015110514111Seat Track · corroded2 EACH SHORT SEAT TRACKS CORRODED ON RBL9 AND BETWEEN FS 559+90 TO FS 570. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06 SRM 53-51-49 TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIEDNov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514110Floorbeam · corrodedCORROSION AROUND 3 SCREW HOLES ON RBL 9 FLOORBEAM AND PANEL 282LRF SUPPORT STRUCTURE AT FS 559.96. REMOVED CORROSION IAW SRM 51-21-06. EVALAUTED BLEND AREA AND FOUND TO BE WITHIN THE ALLOWABLE LIMITS OF REO 601R-53-00-005, FIGURE 1. COMPLIED WITH REO601R-53-Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015110514109Support · corrodedCORROSION AROUND SEVERAL SCREW HOLES UNDER PANEL 282ERF SUPPORT STRUCTURE BETWEEN RBL 9 & 27 AND BETWEEN FS 559.80 TO 559.96. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREAS AT FS 559.80 AND FS 559.96 CROSS-BEAMS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00. Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015110514108Floor Support · corrodedCARGO DOOR FLOOR SILL HAS CORROSION AROUND FLOORBOARD SCREW HOLES. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526-REV.Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015110514107Attach Fitting · crackedLT AND RT LOWER WINDSHIELD CENTER POST ATTACH FITTINGS ARE CRACKED. R & R LT & RT LOWER WINDSHIELD FITTINGS IAW SRM 51-40-11-00 AND 51-42-21-00, DWG 601R33007. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015110514106Seat Track · corrodedCORROSION FOUND ALONG RT SEAT RAIL BETWEEN FS 409-00 + 16 & 409.00 + 112, NEED TO BE EVALUATED. REMOVED RT SEAT RAIL BETWEEN FS 409.00+16-409.00+112 IAW AMM 53-01-11-000-802. LOCATED DRILLED AND INSTALLED RT SEAT RAIL AT FS 409.00+16-409.00+112 IAW SRM 51-40-Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514105Seat Track · corrodedCORROSION FOUND LT SEAT RAIL BETWEEN FS 364.00 AND 409.00+64, MARKED AND NEED TO BE EVALUATED. REMOVED LT SEAT RAIL BETWEEN FS 364.00-409.00+64 IAW AMM 53-01-11-000-802. INSTALLED LT SEAT RAIL AT 349.00-409.00 IAW AMM 53-01-11-400-802. LOCATED & DRILLED 15EANov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514104Seat Track · corrodedCORROSION FOUND ON LT SEAT RAIL BETWEEN FS 409.00+16 & 409.00+112, MARKED & NEED TO BE EVALUATED. REMOVED SEAT RAIL BETWEEN FS 409.00+16-409.00+112 IAW SRM 53-01-11-000-802. LOCATED EVERY OTHER HOLE AND DRILLED AND INSTALLED NEW SERVICABLE SEAT TRACK AT FS 40Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514103Seat Track · corrodedCORROSION FOUND LT SEAT RAIL BETWEEN FS 499.00 AND FS 449.00+85, MARKED AND NEED TO BE EVALUATED. REMOVED LT SEAT RAIL IAW SRM 53-01-11-946-003. INSTALLED 3EA SCREWS IN SEAT RAIL ON LT SIDE FROM FS 449.00+85-499.00 IAW AMM 5-01-11-400-802. INSTALLED SEAT RANov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514102Seat Track · corrodedCORROSION FOUND ON LT SEAT RAIL BETWEEN FS 559.00+80 499.00, MARKED & NEED TO BE EVALUATED. EVALAUTED SEAT RAIL AND FOUND TO BE EXFOILATED 100 PERCENT OUT OF LIMITS IAW SRM 53-21-49, 51-21-06. REMOVED UNSERIVCABLE SEAT RAIL FROM LT SIDE BETWEEN FS449-FS559.0Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514101Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS 559.00 AND 559.00+80, MARKED AND NEED TO BE EVALUATED. EVALAUTED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. CORROSION BLENDED IAW SRM 51-21-06. SRM 53-51-49 STATES TO USE SRM 53Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514100Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT LBL9 BETWEEN FS 559.00 & 559.00+80, MARKED & NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06, SRM 53-51-49 STATES TO USE SRM 53-21-49 INov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514099Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT LBL9 BETWEEN FS 394.00AND 409.00, MARKED AND NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, CORROSION BLENDED IAW SRM 51-21-06. COMPLIED WITH EC/TC 601R-53-00-485 BY FNov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514098Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT LBL9, BETWEEN FS 364.00 AND 394.00, MARKED & NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06. FABRICATED SEAT RAILS IAW GREO 601R-53Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514097Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS364, FS409.00+128 AND 559.00 AND 394.00, MARKED AND NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. CORROSION BLENDED SRM 51-1-06, 53-41-49 STATES TO USENov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514096Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT RBL9, BETWEEN FS 394.00 & 409.00+128, MARKED & NEED TO BE EVALUATED. EVALUATED SEAT TRACK CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, CORROSION REMOVED IAW SRM 51-21-06. COMPLIED WITH EC/TC 601R-53-00-485 STEPS 1Nov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514095Seat Track · corrodedCORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS 364.00 AND 394.00, MARKED AND NEED TO BE EVALUATED. SEAT TRACK AT RBL9 BETWEEN FS 364.00 AND 394.00 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-01. REMOVED CORROSION IAW SRM 51-21-06-00. REMOVED SEAT TRACK ANov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110514094Hinge · corrodedASD BOTTOM STEP HINGE ASSY CORRODED. REMOVED AND INSTALLED NEW ASD BOTOM STEP HINGE ASSY IAW AMM 52-11-04-000-808, AMM 52-11-00-400-807 DRILLED UP NEW ASD BOTTOM STEP HINGE ASSY IAW SRM 51-40-11, SRM 51-41-00. THIS REPAIR IS CLASSIFIED AS A MAJOR/MINOR REPAINov 5, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2015110414826Lug · chafedRIGHT INBD FLAP INBD HINGE LUG PLATE CHAFED, GOUGED ON INBD SIDE OF LUG. REMOVED DAMAGE AT RT INBD FLAP HINGE LUG PLATE INBD SIDE OF LUG IAW SRM 51-12-00-00, TR51-31 BLEND LENGTH 0.900" X .0700" X 0.018" D IAW SRM 57-00-00-01 LUG PLATE NOT SPECIFIED ON ALLOWANov 4, 2015 · N856AS · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA2015110414093Seat Track · corrodedSIDE WALL SEAT RAIL CORRODED AT FS 544.00-559.00+80 LT SIDE. LOCATED AND DRILLED, 42 EA, FASTENER HOLES ON NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. R & R SEAT TRACK AT RT SIDE WALL FS 544.00-559.00+80 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.Nov 4, 2015 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015110214092Angle · crackedFS 625.00 LT SIDE PRESSURE BULKHEAD CLIP CRACKED. R & R LT FS 625 PRESSURE BULKHEAD CLIP REF SRM 51-42-21.Nov 2, 2015 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015110214091Angle · crackedFS 625.00 RIGHT SIDE PRESSURE BULKHEAD CLIP CRACKED. R & R RT FS 625 PRESSURE BULKHEAD CLIP REF SRM 51-42-21.Nov 2, 2015 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015110114090Panel · damagedLIGHTNING STRIKE PANELS UNDER CABIN FLOORBOARD 231CLF REQUIRES REMOVAL TO C/W INSPECTION. REMOVED 3 LIGHTNING STRIKE PANELS UNDER 231CLF FOR INSPECTION IAW AMM 53-01-01-000-806. INSTALLED 3 LIGHTNING PROTECTION PANELS UNDER CABIN FLOORBOARD 231CLF IAW AMM 53Nov 1, 2015 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA2015102213947Flashlight · failedF/O FLASHLIGHT INOPERATIVE. REPLACED F/O FLASHLIGHT IAW AMM 25-61-00. ACFT RETURNED TO SERVICE.Oct 22, 2015 · N856AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2015091813779Unknown · odorF/A AND SEVERAL PASSENGERS REPORTED ELECTRICAL ODOR AROUND ROW 10 AND 11 ENROUTE, ACFT DIVERTED FOR MAINTENANCE. TURNED LIGHTS ON. COULD NOT SENSE ANY ELECTRICAL ODOR AROUND RO 10/11. ACFT OK FOR SERVICE.Sep 18, 2015 · N856AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA2015082613590Battery Pack · dischargedEMERGENCY LIGHTS DO NOT WORK. CHARGED EMERGENCY LIGHTS, OPS CHECKED GOOD IAW AMM 33-50-01.Aug 26, 2015 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015062613182Sign · damagedLIGHTED EXIT SIGN BY SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-13. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Jun 23, 2015 · N856AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015041012584Track · dirtyMAIN CABIN DOOR STICKING AND VERY HARD TO OPEN AND CLOSE. CLEANED TRASH OUT OF PASSENGER DOOR TRACK & CLEANED PASSENGER DOOR SEAL. OPS CHECK GOOD IAW AMM 52-11-00.Apr 6, 2015 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015012312073Acm · failedON CLIMBOUT, F/A REPORTED SMOKE IN THE CABIN PULLED UP ECS PAGE AND RT PACK WAS SHOWING 120 IN AUTO MODE. AUTO MODE WOULD NOT CONTROL TEMP SO SWITCHED TO MANUEL MODE. DECREASED TEMP AND SMOKE CLEARED. ACFT RETURNED TO DEPARTURE. R & R NR 2 ACM IAW AMM 21-Jan 19, 2015 · N856AS · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA2014032810207Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT ILLUMINATE. ALLOWED FOR THE EMERGENCY LIGHTS BATTERY PACKS TO CHARGE FOR ONE HOUR FROM APU POWER. COMPLIED WITH AN OPS TEST, OPS TESTED GOOD, ALL INTERIOR & EXTERIOR EMERGENCY LIGHTS ILLUMINATED. PROCEDURES DONE IAW AMM 33-51-00. Mar 24, 2014 · N856AS · Cndair CL6002D24 · Emergency Lighting
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