N847AS, cancelled Jul 30, 2018

Service difficulty reports · 150

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 = 'N847AS' AND deregistration_id = 'N847AS-2018-07-30'
  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 ASOA2015111614061Door Frame · damagedAC EXTERIOR POWER RECEPTACLE DOOR LANDING DAMAGED. CUT AWAY THE DAMAGED PORTION OF THE DOOR LANDING, PN:600-33042-145 AS SHOWN ON SHEET 2 IAW GREO 601R-53-11-009, REV A. FABRICATED DOOR LANDING REPAIR JOGGLE PLATE, PN:601R-53-11-009 -1, FROM 2024-T3, .050", BNov 16, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2015072813444Door Frame · crackedPAX DOOR FRAME IS CRACKED . REPLACED THE DOOR FRAME IAW SRM TR 51-32, AND DWG 601R31902.Jul 28, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2015072413443Frame · corrodedFOUND WEB OF FRAME AT FS 559+96 TO HAVE MAJOR CORROSION BETWEEN STR 26L AND 26R. CUTOUT SECTION OF FRAME BETWEEN STR 25L AND 25R IAW SRM 53-00-15, REPAIR NR 1, STEPS 5.A, 1-5 &7. FABRICATED AND INSTALLED REPAIR SPLICES AND FRAME DOUBLER IAW SMM 53-00-15.Jul 24, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072013442Floor Support · crackedLEFT SIDE CARGO FLOOR LANDING PLATE HAS CRACKS AT FS 589.00 AND FS 605.00 ORIGINATING FROM RIVET HOLE. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B.Jul 20, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071613441Intercostal · crackedBS 621 - 625 INTERCOSTAL ANGLE AT STRINGER 14R IS CRACKED. REMOVED THE INTERCOSTAL ANGLE AND INSTALLED A NEW ANGLE IAW SRM 51-40-11 AND 51-42-21.Jul 16, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071613440Bulkhead Web · crackedFOUND THE BS 621 REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 127. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.Jul 16, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015071613439Bulkhead Web · crackedFOUND BS 6210REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT RBL 27.5, WL 85, APPROXIMATELY 5 INCHES IN LENGTH. INSTALLED ISOLATION BRACKETS AT BS 621, RBL 27.50 IAW SRM 51-42-06. COMPLIED WITH ECTC REO 601R-53-61-1285 AND GREO 601R-53-6Jul 16, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015071513438Angle · corrodedLOWER PAX DOOR SILL BS 310 - 349 FOUND CORRODED OUT OF LIMITS IAW SRM 53-00-00. REMOVED THE DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. LOCATED AND DRILLED A NEW DOOR SILL ANGLE IAW SRM 51-40-11. INSTALLED THE DOOR SILL ANGLE IAW SRM 51-42-06 AJul 15, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071513437Bracket · crackedLEFT AILERON, ANGLE BRACKET BETWEEN BOTH CENTER HINGE ATTACHMENTS IS CRACKED. INSTALLED A FABRICATED ANGLE IAW SNIEO 601R3035S03.Jul 15, 2015 · N847AS · Cndair CL6002B19 · AileronsSDR ASOA2015071413436Floorbeam · corrodedFLOORBEAM ANGLE BS 349 IS CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-2642, REV.Jul 14, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015071413435Floor Support · corrodedLEFT FLOOR SUPPORT IS CORRODED AT BS 310. REPAIRED IAW REO:601R53-00-530, REV A.Jul 14, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313434Intercostal · corrodedINTERCOSTAL BS 349 - 364, STRINGER 27R CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-06. REPAIRED IAW EA 32-2015-307.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313433Intercostal · corrodedINTERCOSTAL BS 364 - 349 STR 27L CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-06. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-42-06, 51-42-21.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313432Skin · corrodedCORROSION FORMING ON EXTERNAL SKIN ALONG STRINGER 27, BS 559+80 - 559+112. COMPLIED WITH EA 32-2015-293.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015071313429Frame · corrodedFS 319 FRAME IS CORRODED FROM STR 25L TO 25R. REMOVED CORRODED LOWER FRAME SECTOR FS 319 IAW SRM 51-42-06, 51-42-21. PN 601R32003-61. LOCATED AND DRILLED UP NEW SERVICEABLE LOWER FRAME SECTOR PN 601R32003-61 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE LOWERJul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015071313428Frame · corrodedFS 364 FRAME IS CORRODED FROM STR 25L TO 25R. REMOVED FS 364 LOWER FRAME SECTOR IAW SRM 51-42-06. INSTALLED REPAIRED LOWER FS 364 FRAME IAW SRM 51-42-06.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015071313427Frame · corrodedFS 333 FRAME IS CORRODED FROM STR 25L TO 25R. REMVOED CORRODED LOWER FRAME SECTOR, FS 333 IAW SRM 51-42-06, 1-42-21 PN 601R32004-55. LOCATED AND DRILLED UP NEW SERVICEABLE LOWER FRAME SECTOR FOR FS 333, PN 601R32004-55 IAW SRM 51-40-11. INSTALLED NEW SERVICJul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015071313426Frame · corrodedFS 349 FRAME IS CORRODED FROM STR 25L TO 26R. REMOVED LOWER FRAME SECTOR PN 601R32005-69 IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE 601R32005-69 IAW SRM 51-42-06, 51-42-21. LOWER FRAME SECTOR PN 601R32005-69 IS OUT OF LIMITS. CORROSION OVERLAPS Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015071313425Intercostal · corrodedINTERCOSTAL AT FS 394 JUST TO THE LT OF STR 27 IS CORRODED. REMOVED CORRODED INTERCOSTAL PN 601R31049-11 IAW SRM 51-42-06. FOUND TO BE OUT OF LIMITS. CORROSION OVERLAPPED MORE THAN 1 ELEMENT IAW SRM 53-00-00, FIG 102. REPLACED INTERCOSTAL WITH NEW SERVICEAJul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313424Floor Support · corrodedRT SIDE CABIN FLOOR SILL HAS 3 AREAS OF CORROSION AROUND NUTPLATE HOLES FROM FS 559+16 TO FS 559+32. COMPLIED WITH REO 601R-53-00-526, REV DATED 5/22/13. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV DATED 05/22/2013 AS WRITTEN.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313423Floor Support · corrodedLT SIDE PRESSURE FLOOR SILL IS CORRODED AT 6 SPOTS AROUND NUTPLATE HOLES FROM FS 439 TO FS 559. COMPLIED WITH REO 601R-53-41-666. COMPLIED WITH REPAIR FOR CORROSION ON PRESSURE FLOOR SILL BETWEEN FS 409+128 AND FS 559 IAW REO 601R-53-41-666.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313422Floor Support · corrodedRIGHT SIDE CABIN SIDE SILL IS CORRODED AT 8 NUTPLATE HOLES FROM FS 349 TO FS 394. COMPLIED WITH REO 601R-53-00-530, REV A DATED 10/7/14. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313421Floor Support · corrodedLEFT CABIN SIDE SILL IS CORRODED AROUND 5 NUTPLATE HOLES FROM FS 349 TO FS 394. COMPLIED WITH REO 601R-53-00-530. ONE AREA AT FS 353 FOUND TO BE OUT OF LIMITS, REQUIRES ENGINEERING. COMPLIED WITH STS, EA 26-2015-091 AND REO: 601R-53-00-530, REV A FROM FS 35Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313420Door Sill · corrodedCARGO DOOR SILL PLATE IS CORRODED AROUND NUTPLATE HOLES FROM FS 574 TO FS 621. COMPLIED WITH REO 601R-53-00-526, REV. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015071313419Plate · corrodedSERVICE DOOR STEP PLATE HAS CORROSION ALL ALONG THE BOTTOM INBD EDGE. REMOVED AND LOCATED NEW SERVICEABLE STEP PLATE. DRILLED AND INSTALLED NUTPLATES IAW SRM 51-42-06 AND 51-40-11.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Service DoorsSDR ASOA2015071313418Angle · crackedFS 625, LT UPPER OBLIQUE ANGLE IS CRACKED. REMOVED IAW SRM 51-42-21. INSTALLEDIAW SRM 51-42-21 AND PAINTED SRM 51-21-16.Jul 13, 2015 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014090511185Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRACK BS 349- 559. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.Sep 3, 2014 · N847AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014090511184Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.Sep 3, 2014 · N847AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013012902923Floor Support · corrodedFLOOR SUPPORT AND DOUBLER CORRODED AT FS 319.70, RBL 42. REMOVED RT FLOOR SUPPORT FS 310.00 TO FS 319.70 IAW SRM 51-42-06 FOR REPAIR OR REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT, IAW SRM 51-40-11. INSTALLED IAW SRM 51-42-06, 7 51-42-13. Jan 13, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902922Bulkhead · crackedINDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 36, WL 78 APPROX .300 IN LENGTH AT 100/5 FULL SCREEN HEIGHT. REPAIRED FS 631 BULKHEAD AT LBL 36 & WL 78 IAW REO 601R-53-61-4765.Jan 11, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013012902921Bulkhead · crackedINDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 27.50, WL 141 APRROX .150 IN LENGTH AND 55 PERCENT FULL SCREEN HEIGHT. COMPLIED REO 601R-53-61-1546 AND REO 601R-53-61-1541 REV D DATED 10/31/2011.Jan 11, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013012902920Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH W/O 276849 AND REO 601R-52-11-513.Jan 10, 2013 · N847AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013012902919Angle · crackedFS 484.00, ANGLE AT RBL 27 IS CRACKED. REPAIRED ANGLE IAW REO 601R-53-41-059.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902918Angle · crackedFS 484.00 ANGLE AT LBL 9 IS CRACKED. R & R ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902917Angle · crackedFS 484.00, ANGLE AT LBL 27 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902915Bracket · corrodedSERVICE DOOR CUTOUT TEE BRACKET IS SEVERELY CORRODED AT FS 319.70, WL 70.60. REMOVED FITTING IAW SRM 51-42-21 FOR REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE SERVICE DOOR FITTING IAW SRM 51-40-11 & INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-21.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013012902914Floorbeam · crackedFLOORBEAM ANGLE CRACKED AT FS 280, LBL 9 INBD AND OTBD. R & R CRACKED FLOORBEAM ANGLE AT FS 280, LBL 9 INBD AND OTBD IAW SRM 51-42-21. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD ANGLE IAW REO 601R-53-11-926.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2013012902913Floorbeam · corrodedCARGO FLOORBEAM HAS CORROSION AROUND FASTENER HOLES AT FS 589, BETWEEN LBL 9 AND LBL 27. REMOVED CAP STRIP BETWEEN LBL 9 AND LBL 27 IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 589 FLOORBEAM CAP STRIP PN 601R35031-165 BETJan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2013012902912Floor Support · corrodedRT FLOOR SILL HAS CORROSION AROUND FASTENER HOLDS BETWEEN FS 559+80 AND FS 589. BLENDED CORROSION IAW SRM 51-21-00. SRM HAS NO ALLOWABLE LIMITS. AMOUNT OF CORROSION REMOVED 0.011", REO 601R-53-00-505.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902911Floor Support · corrodedLT FLOOR SILL HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 559+96 AND 559+112. BLENDED CORROSION IAW SRM 51-21-06, SRM HAS NO ALLOWABLE LIMITS SUBMITTED FOR REPAIR DISPOSITION, AMOUNT REMOVED 0.011". C/W REO 601R-53-51-214.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013012902910Frame · corrodedFS 605, FRAME CORRODED BETWEEN STRINGERS 26L AND 26R. R & R FS 605 FRAME FROM STR 25L TO STR 22R IAW REO 601R-53-61-4763 USING SRM 53-00-15, SHEET 2 REPAIR NR 1 FRAME SPLICE REPAIR.Jan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013012902909Fitting · crackedCO-PILOTS WINDSHIELD SIDE POST LOWER AFT, OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM CO-PILOTS WINDSHIELD SIDE POST IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER AFT OTBD FITTING, ON CP-PILOTS WINDSHIELD SIDJan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013012902908Fitting · crackedPILOTS WINDSHIELD SIDE POST LOWER AFT OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM PILOTS WINDSHIELD SIDE POST IAW SRM CH 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER AFT OTBD FITTING, PN 601R33235-3S ON PILOTS WINDSJan 9, 2013 · N847AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013012902907Door · misinstalledRT OVERWING EMERGENCY EXIT EXCEEDED FORCE TO OPEN. ON FURTHER INVESTIGATION, FOUND LT AND RT EMERGENCY EXIT DOORS INSTALLED IN WRONG LOCATION. FUNCTION TEST GOOD IAW AMM 52-21-00-720-801.Jan 7, 2013 · N847AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA2012101602353Lamp · burned outCEILING AFT EMERGENCY FLOOD LIGHT INOPERATIVE. LAMPED CEILING EMERGENCYH AFT FLOOD LIGHT IAW AMM 33-51-16.Oct 12, 2012 · N847AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201677Coalescer Bag · odorACFT HAS STRONG FUEL ODOR DURING DESCENT. R & R WATER SEPARATOR COLESCER ON LT AND RT PACKS IAW AMM 21-51-13, OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.May 23, 2012 · N847AS · Cndair CL6002B19 · Humidity Control SystemSDR ASOA201201229Bulkhead · crackedBULKHEAD CRACKED AT FS 202 BY PARKING BRAKE CABLE. WORK COMPLETED IAW EC/TC REO 601R-53-11-563 AND STARTED DRILLING OUT FASTENERS FOR REPAIR NR 1 IAW EC/TC REO 601R-53-11-563. COMPLIED WITH NDT HFEC INSP ON 202 BULKHEAD, VERIFIED SEVERAL CRACKS, MARKED THE EApr 7, 2012 · N847AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201200877Latch · lack of lubeON PASSENGER DOOR, TEE HANDLE INDICATOR SHOWS LOCKED WHEN DOOR IS OPEN AND F/A IS HAVING DIFFICULTY OPENING AND CLOSING THE DOOR. LUBRICATED PASSENGER DOOR LATCH MECHANISM. PERFORMED OPS TEST OF THE PAX DOOR LATCH MECHANISM IAW AMM 52-11-21. OPS CHECKED GOODFeb 23, 2012 · N847AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102169Lamp · burned outAFT CENTER CEILING EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS. REPLAMPED AFT CENTER CEILING EMERGENCY EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-51-00.Nov 12, 2011 · N847AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101870Lamp · burned outLT OVER WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING AFT EM LIGHT W/A SERVICEABLE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Oct 7, 2011 · N847AS · Cndair CL6002B19 · Emergency Lighting
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