N884AS, cancelled Nov 26, 2019

Service difficulty reports · 162

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 = 'N884AS' AND deregistration_id = 'N884AS-2019-11-26'
  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 SWIA201743939O-Ring · failedHYD SYSTEM 3 FAILED DURING CRUISE FLIGHT. ZERO PSI. COMPLIED WITH QRH. DECLARED EMERGENCY. PERFORMED A FREEFALL EXTENSION OF LANDING GEAR. R & R THE HYD PUMP 3A AND 3B IAW AMM. R & R THE O-RING BETWEEN THE PUMP AND THE BALL ATTENUATOR. LEAK CHECKED GOOD.Nov 1, 2017 · N884AS · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA2017101243860Trunnion · damagedUPPER LEFT TRUNNION STRUCTURE ATTACHMENT HOLES, ARE OVERSIZED. STEPPED UP TRUNNION HOLES TO FIRST OVER SIZE IAW REO.Sep 13, 2017 · N884AS · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA2017101243852Floor Support · corrodedSERVICE DOOR FLOOR SUPPORT BRACKET AT BS 349 CORRODED. REMOVED AND REPLACED BRACKET IAW SRM.Sep 13, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243862Angle · corrodedSERVICE DOOR FLOOR SUPPORT ANGLE AT BS 319 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM.Sep 11, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2017101243858Floor Support · corrodedFLOOR SUPPORT AT THE PASSENGER DOOR IS CORRODED BETWEEN BS 349 AND 359. REMOVED THE CORROSION IAW REO.Sep 10, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243864Shear Tie · corrodedCORROSION ON LOWER FRAME SHEAR TIE AT BS 319. REMOVED AND REPLACED THE SHEAR TIE IAW SRM.Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2017101243863Doubler · corrodedRT GALLEY MOUNT DOUBLER FWD OF BS 319 IS CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM.Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243857Beam · corrodedRIGHT TRANSVERSE BEAM AT BS 349 IS CORRODED. REPAIRED DAMAGE AT IAW REO.Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201743855Floor Support · damagedFLOOR SUPPORT AT RBL 27 BETWEEN BS 574 - 621 DAMAGED. REPAIRED FLOOR SUPPORT IAW REO.Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243853Shear Tie · corrodedCORROSION ON LOWER FRAME BRACKET AT BS 349. REMOVED AND REPLACED LOWER FRAME BRACKET IAW SRM.Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2017101243856Floor Support · corrodedCORROSION ON THE RT FLOOR SUPPORT FROM BS 349 - 364. REPAIRED THE DAMAGE IAW REO.Sep 8, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243851Floor Support · corrodedFLOOR SUPPORT AROUND NUTPLATES BETWEEN BS 605.04 AND 574 CORRODED AT CARGO BAY DOOR. FURTHER INVESTIGATION FOUND CARGO DOOR FLOOR SUPPORT TO BE OUT OF LIMITS. IAW REO 601R-53-00-526 REV -.Sep 3, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2017101243861Frame · crackedBS 280 FRAME IS CRACKED AT STRINGER 3L. REPAIRED THE FRAME IAW REO.Aug 28, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2017101243854Channel · crackedCARGO DOOR FWD TRACK LOWER CHANNEL IS CRACKED. REMOVED AND INSTALLED A NEW CHANNEL IAW SRM.Aug 28, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743859Skin · dentedSKIN DENTED AT BS 409+64, STRINGER 15R. REPAIRED IAW REO.Aug 24, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2016060714916Lamp · burned outNR 4 EXIT, EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Jun 7, 2016 · N884AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015121114209Generator · shutdownADG DEPLOYED IN FLIGHT DUE TO INADVERTENTLY SHUTTING DOWN OF GEN 1 AND GEN 2 EMERGENCY DECLARED. ACFT RETURNED TO DEPARTURE AFTER T/O. RETRACTED ADG IAW AMM 24-23-01 AND PERFORM IDLE ENGINE RUNS IAW AMM 71-00-00 WITH IDG'S AND APU GENERATOR ONLINE. NO ABNDec 11, 2015 · N884AS · Cndair CL6002B19 · AC Generator-AlternatorSDR ASOA2015102313950Spar · damagedAFT SPAR ON RT HORIZONTAL STAB TIP FOUND TO BE DAMAGED DUE TO LIGHTNING STRIKE. CUT AWAY BURNED SECTION OF AFT SPAR AND CLEANED UP ALL SHARP EDGES ON MISDRILLED HOLE ON AFT SPAR TO THE RT OF BURN, WORK DONE REF EA EJ-CRJ255-00032. COMPLIED WITH EDDY CURRENTOct 23, 2015 · N884AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR ASOA2015070213228Angle · corrodedFS 280 J-ANGLE CORRODED. REMOVED CORRODED J-ANGLE AT FS 280 PT 600-34017-351 IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW FS 280, J-ANGLE PT 600-34017-351S IAW SRM 51-42-06 & 51-40-11.Jun 18, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213227Frame · crackedFS 605, FRAME AND PREVIOUS USED DOUBLER STRAP CRACKED AT UPPER HOLE LOCATION WHERE STANDOFF SB INSTALLED AFTER INSTALLATION AT RT STR 26 AND RT STR 27. LOCATED AND DRILLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-40-11. INSTALLJun 10, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015070213226Floorbeam · corrodedCORROSION FOUND AT NUTPLATE LOCATION AT LT FS 561.00, STR 17, BUTT LINE 36 TO 47. COMPLIED WITH EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C.Jun 8, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015070213225Skin · crackedRIGHT WING PLANK ACCESS HOLE CUTOUT FOR PANEL 650CB HAS INDICATIONS AROUND CIRCUMFERENCE OF LANDING 55 PERCENT FSH, AREA MARKED ON ACFT, FAILED NDT. REMOVED RT WING FUEL ACCESS FUEL PANEL 650CB IAW AMM TASK 28-11-01-000-802. INSTALLED RT FUEL PANEL 650CB IAWJun 5, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015070213224Angle · crackedOBLIQUE ANGLE CRACKED AT FS 622- FS 625, STR 14L ABOUT LBL 40. REMOVED OBLIQUE ANGLE IAW SRM 51-42-20. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE AT FS 622-FS 625, STR 14L, LBL 40 IAW SRM 51-42-20, SRM 51-40-11 AND SRM 51-42-06.Jun 5, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213223Intercostal · crackedINTERCOSTAL FS 621-625, STR 14L, ADJACENT TO SKIN, OTBD FLANGE IS CRACKED. REMOVED CRACKED INTERCOSTAL, PN:601R2350121-5 FROM INTERCOSTAL. IN STEP 3 IAW SRM 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL, PN:601R350121-5 IAW SRM 51-40-11. INSTALLED IT ON INJun 5, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213222Intercostal · corrodedINTERCOSTAL AT BS 349-364, STRINGER 26L IS CORRODED. BLENDED CORROSION FROM INTERCOSTAL 26L AT FS 349-364 MAXIMUM MATERIAL REMOVED .002 IAW SRM 51-21-06, 53-00-00, FIG 102.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213221Splice Plate · corrodedSPLICE PLATE AT FS 621 RH RBL 41 IS CORRODED. BLENDED CORROSION ON SPLICE PLATE AT FS 621, RBL 41 IAW REO 601R-53-61-4690. MAXIMUM MATERIAL REMOVED .009. REPAIRED FLOOR ANGLE AT FS 621.00 IAW REO 601R-53-61-4690.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070213220Skin · corrodedCORROSION ON LOWER WING PLANK HOLE, 540BB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEENING REWORKED AREA IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015070213219Skin · corrodedCORROSION ON LOWER WING PLANK HOLE, 510AB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEEN OF THE REPAIR SURFACE IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015070113218Skin · corrodedCORRROSION ON LOWER WING PLANK HOLE, 610AB IN SEVERAL AREAS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L-ROTO PEEN OF REWORKED SURFACES IAW SRM 51-24-11. C/W REO 601R-57-21-030. LEAK CHECK GOOD. C/W ECTC EO 600-57-81, C/W IAWJun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015070113217Skin · corrodedCORROSION ON LOWER WING PLANK HOLE, 640BB, IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO-PEENING OF REWORK AREAS IAW SRM 51-24-11.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015070113216Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50, WL 130 APPROX 2.0" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. UPON MILLING OF CARGO DOOR TRACK IAW REO 601R-53-61-5498. REMOVED EXCESS MATERIAL CARGO DOOR TRACK REQUIRES REPJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113215Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 JUST ABOVE WL 73.50 APPROXIMATELY 1.5 IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. C/W REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621, BULKHEAD LBL 36 IAW REO 60Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA2015070113214Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 24" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEPS 1-3 OF REO 601R-53-61-5498, REV P1. C/W REO 601R-53-61-5498 PJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113213Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 (Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113212Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 9.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHAD WEB AT BL 0 IAW REO 601R-53-61-549Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113211Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 9.5 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW SEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 9.5. C/W REOJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113210Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 18. COMPLETJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113209Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 121.43-WL 137.5 APPROXIMATELY 6.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113208Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113207Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498, P1 AT FS 621, RBL 18. C/W RJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113206Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED POSITION OF THE REAR PRESSURE BULKHEAD WEB AT BL 0 IAW REO 601R-53-61-54Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113205Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 9.50 BETWEEN WL 73.50-WL 120.43 APPROX 4.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGE PORTION OF THE REAR PRESSURE BULKHEAD WEB AT LBL 9.50 IAW REO 601R-53-61-5498.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113204Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 73.50, WL 120.43 APPROXIMATELY 12" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW REO 601R-53-61-5498 P1. INSTALLED ALJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070113203Post · crackedFS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 .250", LONG BY 60 FSH. FAILED NDT. REMOVED INBD POST, PN:601R32208-32 AND OTBD POST, PN:601R32208-156 AT FS 409+128, RBL 18 IAW SRM 51-42-06. ASSEMBLED Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070113202Attach Bracket · crackedBRACKET ATTACHING FROM STR 3L TO FS 280 IS CRACKED. REMOVED CLEAT IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015063013198Attach Angle · crackedSTR 3L ATTACHING ANGLES ARE CRACKED JUST AFT OF FS 280. REMOVED ANGLE, PN 600-31057-19 FROM STR 3L AT FS 280 IAW SRM 51-42-06. DRILLED, LOCATED AND INSTALLED NEW ANGLE, PN 600-31057-19 ON STR 3L AT FS 280.0 IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32. REMOVEJun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015061213102Post · crackedFS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 APPROXIMATELY .250" LONG BY 50 PERCENT FSH. BOTH INDICATIONS FAILED NDT. NO OTHER INDICATIONS NOTED. REPAIRED IAW EC/TC, REO:601R-53-41-889.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015060813069Post · crackedFS 409+128, BL 0 VERT POST LT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250", LONG Y 50 PERCENT FSH, FAILED NDT. REPAIRED IAW ECTC REO 601R-53-41-889.Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015063013197Frame · corrodedCORROSION ON 605 FRAME FROM STR 27 TO STR 24L. FOUND CORROSION ON FS 605, FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-0Jun 2, 2015 · N884AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA2015063013196Crossbeam · corrodedCORROSION ON CROSSBEAM AT FS 589.00 BETWEEN RBL 9 & LBL 9. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. .021" MATERIAL REMOVED. REPLACEMENT REQUIRED. REMOVED DAMAGED CAP STRIP IAW SRM 51-42-06-00. FABRICATED, LOCATED AND DRILLED NEW SERVICJun 2, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Structure
Back to N884AS, cancelled Nov 26, 2019