N881AS

Service difficulty reports · 206

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 = 'N881AS' 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 ASOA201100564Sill · corrodedLEFT PRESSURE FLOOR SILL AND ALL ANGLES HAVE CORROSION BETWEEN FS 409+128 AND FS 559.0. ACCOMPLISHED STEP 1 OF REO 601R-53-41-1391 IAW REO 601R-53-41-1391. DID NOT EXCEED MAX. REPORTED DEPTHS IAW REO 601R-53-41-1391. COMPLIED WITH STEP 2 OF REO NDT REPAIRMar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100563Sill · corrodedRT PRESSURE FLOOR SILL AND SILL ANGLES HAVE CORROSION BETWEEN FS 409+128 AND FS 559.0. ACCOMPLISHED STEP 1 OF REO 601R-53-41-1391 IAW REO 601R-53-41-1391 DID NOT EXCEED MAX REPORTED DEPTH IAW REO 601R-53-41-1391. COMPLIED WITH STEP 2 OF REO. PERFORMED NDT.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100562Floor Support · crackedFS 484, FLOORBEAM ANGLE ON THE OTBD SIDE OF PRESSURE FLOORBEAM LBL 27 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100561Floor Support · crackedFS 484 FLOORBEAM ANGLE ON THE OTBD SIDE OF PRESSURE FLOORBEAM RBL 27 IS CRACKED. INSTALLED NEW ANGLE AT FS 484, RBL 27 IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100560Isolator · brokenISOLATOR BROKEN ON FWD FACE OF 621 BULKHEAD APPROX 20" ABOVE FLOOR AT LBL 9 AND RBL 9. R & R ISOLATOR FWD FACE 621 BULKHEAD LBL 9 AND RBL 9 IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201100559Unknown · corrodedCORROSION ON RBL 9 AT FS 559+96 FLOORBEAM. TRIMMED OUT FLOORBEAM IAW SRM 53-00-43, PG 201. PERFORMED EDDY CURRENT INSPECTION, NO INDICATIONS FOUND. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-00-43.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA201100558Floor Support · corrodedFLOOR SUPPORT AT LBL 27, FS 621 TO FS 574, HAS CORROSION AROUND FASTENER HOLES. COMPLIED WITH EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100557Cargo Track · corrodedCARGO SEAT TRACK CORRODED LBL 9 . R & R CARGO SEAT TRACK IAW AMM 20-21-00-910-801.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100556Floorbeam · crackedFLOOR SUPPORT CLIP AT FS 280 LBL 9 OTBD SIDE IS CRACKED APPROX .500". REMOVED AND INSTALLED FLOOR SUPPORT CLIP AT FS 280 LBL 9 OTBD SIDE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100555Floorbeam · crackedFLOOR SUPPORT CLIP AT FS 280 RBL 9 OTBD SIDE IS CRACKED. R & R NEW FLOOR SUPPORT CLIP AT FS 280 RBL 9 OTBD SIDE IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100554Floorbeam · corrodedFLOORBEAM & CAP ARE CORRODED AT FS 349 BETWEEN RBL 27 & RBL 45. FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 101, SHT 3. REPAIRED IAW REO 601R-53-21-1262.Mar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100553Seat Track · corrodedSEAT TRACK AT LBL 9 BETWEEN FS 364.00 CORRODED ON FWD END. FOUND OUT OF LIMITS IAW SRM 53-21-49. SEAT TRACKS AT LBL 9 AND RBL BETWEEN FS 364 AND FS 399.55 ARE AND REQUIRE REPLACEMENT. REPLACE SEAT TRACKS AT LBL 9 AND RBL 9 BETWEEN FS 364 AND FS 399.5. REMar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100552Floorbeam · corrodedFLOORBEAM & CAP ARE CORRODED FS 349 BETWEEN LBL 27 AND LBL 45. REMOVED CORROSION IAW SRM 51-21-06. MATERIAL REMOVED WAS .003" TO .004", NOT EXCEEDING 10 PERCENT IAW SRM 53-00-00, FIG 102. TREATED, PRIMED & PAINTED AERA IAW SRM 51-21-11. CLASSIFIED AS A MINOMar 23, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100536Angle · crackedRT 621-625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE 621-625 OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Mar 22, 2011 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100535Angle · crackedLT 621-625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE 621-625 LT SIDE PN 601-35012-51 OBLIQUE ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Mar 22, 2011 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100525Frame · crackedFRAME IN AFT EQUIPMENT BAY AT FS 700 S9R IS CRACKED AT BOTTOM RIVET APPROX 1"L. REPAIRED FRAME IAW SRM 53-00-15, REPAIR NR 2 AND REO 601R-53-61-4017.Mar 18, 2011 · N881AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201001570Bulkhead · crackedWHILE PERFORMING AWL2 53-41-124, FOUND A SUSPECT CRACK LOCATED AT FS 409+128 PRESSURE BULKHEAD FWD FACE COMING FROM LOWER EDGE OF THE INBD U CHANNEL AT LBL 27.00. CRACK GOES UP AND PAST FIRST LOWEST FASTENER HOLE (BUT NOT PAST THE NEXT FASTENER HOLE UP) THAT AOct 14, 2010 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001106Flashlight · inoperativeBOTH CAPT & F/O FLASHLIGHTS INOP. REPLACED CAPT & F/O BATTERIES IN FLASHLIGHT AND OPS CHECK GOOD AS REQUIRED IAW AMM 25-60-01. ACFT OK FOR SERVICE. (CLOSED)Aug 13, 2010 · N881AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001098Cover · missingEMERGENCY EXIT AISLE ILLUMINATION LIGHT COVER, FELL OFF, RED BULB COVER MISSING. RE-LAMPED EXIT LIGHT IAW AMM 33-51-14 AND RE-SECURED CKS GOOD.Aug 12, 2010 · N881AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200901069Warning Light · illuminatedL 14TH DUCT WARNING IN FLIGHT. RAN QRH. MESSAGE REMAINED THROUGH REMAINDER OF FLIGHT. [EMERGENCY DECLARED]Oct 1, 2009 · N881AS · Cndair CL6002B19 · Central WarningSDR ASOA200900357Warning System · activatedGEAR DISAGREE UPON SELECTION OF GEAR UP. RAN QRH, LANDED UNEVENTFULLY. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.Mar 29, 2009 · N881AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA200900241Structure · crackedJOB 8749615 OPERATION 96 / LT FS 718 CRACKED ABOVE AND BELOW STG 11.Feb 24, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900228Angle · damagedJOB 8749615 OPERATION 133 / LT FS 559.0 CAP ANGLE HAS AN INDICATION NOTED AT LBL 18.0 APPROX .2 INCHES IN LENGTH 80 PERCENT FSH AND RT FS 559.0 WEB HAS AN INDICATION NOTED AT WL 58.70 APPROX .1 INCH IN LENGTH 25 PERCENT FSH FS 559.0. FAILED NDT INSPECTION. COFeb 20, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900227Post · damagedJOB 8749615 OPERATION 162 / LT FS 409.0+128 LBL18 I/B VERTICAL POST AT WL 69.0 HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH 60 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. FABRICATED AND INSTALLED VERTICAL POST AS PER SAMPLE IAW SRM 51-24-16 AND DFeb 20, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900225Post · damagedJOB 8749615 OPERATION 160 / RT FS 409.0+128 RBL 18 I/B VERTICAL POST AT WL 69.0 HAS A INDICATION NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. FABRICATE NEW POST AND INSTALLED IAW SRM 51-Feb 20, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900219Repair · crackedJOB 8749611 OPERATION 245 / LEFT FS 484 FLOOR SUPPORT CRACKED 1 INCH LONG UNDER CABIN FLOOR PANEL 261DLF. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059.Feb 19, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900218Repair · crackedRIGHT FS 484 INTERCOSTAL CRACKED 1 INCH LONG UNDER CABIN FLOOR PANEL 262DRF. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059.Feb 19, 2009 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800705Light · inoperativeEMERGENCY FLOOR TRACK LIGHTING AT 5CD INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT 5CD IAW AMM 33-51-01. OPS CHECK GOOD. (B)May 30, 2008 · N881AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200701366Handle · crackedMAIN PAX DOOR OUTER HANDLE CRACKED.Sep 17, 2007 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200701226Pressure Panel · crackedFS 621 PRESSURE WEB IS CRACKED AROUND LINTEL FITTING. REPAIRED FS 621 PRESSURE WEB AT LINTEL FITTING IAW REO 601R-53-61-1230; REO 601R-53-61-2312; AND ASA EC/TC REO 601R-53-61-2312; EC/TC REO 601R-53-61-1230.Aug 20, 2007 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200701210Angle · crackedRIGHT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED NEW OBLIQUE ANGLE PER CRJ 200 SRM 51-42-20, AND REO 601R-53-61-422.Aug 17, 2007 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701209Angle · crackedLEFT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11.Aug 17, 2007 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701208Fitting · crackedFS 280 AT RBL 9 O/B CLIP CRACKED. REWORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 51-25-16, 51-25-16, 51-42-21, & REO PL601R-53-11-926.Aug 17, 2007 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701207Fitting · crackedFS 280 AT LBL 9 I/B & O/B CLIPS CRACKED. ALL WORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 51-25-06, 51-25-16, 51-42-06, 51-42-13, 51-42-21, & 51-42-02.Aug 17, 2007 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200701238Placard · unknownEMERGENCY ESCAPE HATCH NEEDS THE FOLLOWING EXTERIOR PLACARDS EMERGENCY EXIT (INSTRUCTION PLACARD), OPEN PLACARD, ARROW INDICATION PLACARD AND CLOSED PLACARD.Aug 16, 2007 · N881AS · Cndair CL6002B19 · Placards and MarkingsSDR TRAX200701204Support Angle · crackedPAX DOOR IS CRACKED ON THE INNER AFT SUPPORT ANGLE 35.3 INCHES FROM LWR EDGE OF DOOR. CRACK IS APPROX 1.5 INCH LONG. REWORK DONE AS REFERENCED IN CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-42-13, & 51-42-22.Aug 16, 2007 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200700170Switch · unknownA -STEERING INOP- CAUTION MESSAGE AFTER T/O. FOLLOWED QRH, MESSAGE WENT OUT WITH NWS SWITCH OFF. STEERING RE-SET WITH SWITCH AFTER LANDING. EMERGENCY DECLARED.Feb 4, 2007 · N881AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR TRAX200601103Web · crackedLEFT BOX BEAM LOWER WEB CRACKED IN RADIUS.Dec 10, 2006 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200601085Beam · crackedRIGHT BOX BEAM CRACKED AT FWD INBOARD SIDE. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 NDTM 51-20-06, REO 601R-53-61-366, REO 601R-53-61-366 PER CRJ 200 NDTM 51-20-06, REO 601R-53-61-366 REV. F CM20420, REO 601R-53-61-366 CM20420, AND REO 601R-53-61-366.Dec 6, 2006 · N881AS · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200601084Frame · crackedLEFT FS 640 CRACKED. FLT 4454 CX. REPAIRED IAW CRJ 200 NDTM 51-20-06, REO 601R-53-061, SB 601R-53-061 PER CRJ 200 NDTM 51-20-06, REO601R-53-061, REO 601R-53-061, REO601R-53-061, REO601R-54-005, AND REO601R-53-061.Dec 6, 2006 · N881AS · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200600579Step · crackedA/S/D BOTTOM STEP CRACKED AT ATTACHMENT BRACKETAug 4, 2006 · N881AS · Cndair CL6002B19 · Entrance StairsSDR TRAX200600343Odor · detectedSMELL OF SMOKE IN COCKPIT NOTICED ON DESCENT. A/C SWAP TO 884, FLT 4608 DEL 180 MINS.Jun 8, 2006 · N881AS · Cndair CL6002B19 · Air Distribution SystemSDR TRAX200600222Bracket · crackedA/S/D AFT. CABLE COUNTER BALANCE ANCHOR BRACKET CRACKEDMay 15, 2006 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200600150Bulb · inoperativeFOUND PAX DOOR EMERG EXIT LIGHT HAS BULBS INOP.Apr 29, 2006 · N881AS · Cndair CL6002B19 · Emergency LightingSDR ASOA06345Seal · out of positionDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE FOUND THE PASSENGER DOOR SEAL OUT OF THE CHANNEL AND REINSTALLED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Mar 24, 2006 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA06291Angle · crackedDURING A HANGAR INSPECTION, THE RT SIDE FS 640 REINFORCING ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE RT SIDE FS 640 REINFORCING ANGLE IAW SRM. (K)Mar 9, 2006 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05980Battery Pack · dischargedDURING A HANGAR CHECK IN MCN, THE EMERGENCY LIGHTS AT THE PASSENGER DOOR AND OVERHEAD IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 14, 2005 · N881AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05326Step · brokenDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINT REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K)Apr 8, 2005 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA04945Step · crackedDURING AN A CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 28, 2004 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA04517Clip · crackedDURING A C-CHECK IN MCN, THE RIGHT INBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD CLIP AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M)Jul 18, 2004 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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