N894UP, cancelled Apr 4, 2018

Service difficulty reports · 455

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 = 'N894UP' AND deregistration_id = 'N894UP-2018-04-04'
  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 UPS09854259Attach Angle · crackedINSPECTION TYPE: SV LT ELEVATOR STA 200.238 DOUBLER ATTACHED ANGLE IS CRACKED AND DENTED, REPAIRED IAW DWG 5700911 AND SRM 51-01-21.Dec 19, 2008 · N894UP · Doug DC873F · Elevator StructureSDR UPS08854221Skin · damagedINSPECTION TYPE:SV EVAL REPAIR DOUBLER INSTALLED AT STATION 161 UPPER SURFACE OF FUSELAGE SKIN JUST AFT OF NOSE RADOME SURVEY SEQUENCE 894-F1-43. REPAIRED IAW DC8 SRM 53-02-0 FIG 001 D SHEET 3.Dec 14, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08854006Skin · crackedINSPECTION TYPE:N/A L1 DOOR HOLD OPEN LATCH AT FS 16 BETWEEN LONGERONS L-15L AND L-16L CRACK AT LOWER AFT CORNER OF PRODUCTION TRIMOUT. THE CRACK AND EXISTING STOP DRILL MEASURES 0.70 INCH LENGTH. COMPLIED WITH EO DC8-5330-31311-A.Nov 22, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853645Skin · unknownINSPECTION TYPE:SV INSTALL EXTERNAL SKIN DOUBLERS AT STA -88 TO -50 AND -29 TO 7 L21R. INSTALLED DOUBLERS IAW SRM DC-8 53-02-01 FIG 007.Oct 16, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853679Doubler · unknownINSPECTION TYPE:SV (REPAIR STA -45 LBL 33 DOUBLE FILLER) REPAIR PER DAC DWG SR0830026 REF UPS NRC 188379. REPLACED FINGER AND SPLICE DOUBLERS IAW SR 08530026 REV A.Oct 15, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853654Doubler · unknownINSPECTION TYPE:SV STA 904 OCTAGON DOUBLER REINSTALL DOUBLER. INSTALLED DOUBLER 51-01-08 AND DALFORT XEA X8-53-298.Oct 15, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853675Rib · crackedINSPECTION TYPE:SV RT WING OUTBOARD L/E LOWER RIB CRACKED AT XFS 835. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. MANUF AND INSTALLED REPAIR IAW DC8 SRM 51-1-8AND SRM DC8 SRM 51-01-20D-0.Oct 7, 2008 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS08853673Rib · crackedINSPECTION TYPE:SV RT WING L/E LOWER RIB CRACKED AT XFS 829. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. FABBED AND INSTALLED REPAIR IAW DC8 SRM 51-03-00-0, AND SRM 51-01-20D-0 DC8.Oct 7, 2008 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS08853676Fastener · deformedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT WING INBOARD FLAP INBOARD EDGE WEB EXT REPAIR DOUBLER HAS 2EA DEFORMED FASTENER. REPLACED FASTENERS IAW DC8 SRM 51-01-21.Oct 6, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853677Skin · misrepairedINSPECTION TYPE:SV RT LWR LEADING EDGE DOUBLER STA XFS 524 NEEDS VALIDATION. DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-19 AREA PREVIOUSLY REPAIRED & AND ADDED EXTRA ROW OF FASTENERS IAW DC8 SRM 57-2-1 TR 57-95 AND SRM 51-1-21.Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853674Stop · missingINSPECTION TYPE:SV LT FWD NLG DOOR BUFFER STOP MISSING. REPLACED FWD NLG DOOR BUFFER STOP IAW DC8 MM 32-22-01-5.Oct 5, 2008 · N894UP · Doug DC873F · Landing Gear DoorsSDR UPS08853650Doubler · unknownINSPECTION TYPE:SV RT UPPER LEADING DOUBLER NEEDS VALIDATION AT STA XFS627 FAIL APP H ST STEP 5 894-W4-12 REPAIRED IAW 57-2-1 AND 51-01-04.Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853647Doubler · unknownINSPECTION TYPE:SV RIGHT LEADING EDGE DOUBLER NEEDS VALIDATION AT STA XFS 455 FAILED APPH STEP 5 894-W4-07. REPLACED DOUBLER IAW DC8 SRM 57-2-1 FIG 38.Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853636Skin · unknownINSPECTION TYPE:SV RT UPPER LEADING EDGE DOUBLER NEEDS VALIDATION AT STA 325 FAILS APPEN DIX "H" STEP 5 SURVEY SEQ 894-W4-5. REMOVED AND REPLACED REPAIR PER DC 8 SRM 57-2-1 FIG 38 TR 57-85.Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853623Skin · misrepairedINSPECTION TYPE:SV RT WING LEADING EDGE LOWER DOUBLER I/B SIDE OF NR 4 PYLON NEED VALIDATION AT STA XFS 500. DOES NOT MEET CRITERIA IN APPENDIX H STEP 5. 894-W4- 32 AREA PREVIOUSLY REPAIRED FEF SRM 57-3-1 T/R 57-83.Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853619Skin · misrepairedINSPECTION TYPE:SV RT LOWER LEADING EDGE DOUBLER I/B SIDE NR 3 PYLON AT STA XFS 225 DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-31 AREA PREVIOUSLY REPAIRED FEF DC8 SRM 57-2-1 TR 57-83 FIG 14A.Oct 5, 2008 · N894UP · Doug DC873F · Nacelle/Pylon Miscellaneous StructureSDR UPS08853618Structure · misrepairedINSPECTION TYPE:SV RT WING LOWER L/E DOUBLER REPAIR NEEDS VALIDATION FOR REPAIR AT STA XFS 747.600. DOES NOT MEET CRITERIA IN APPENDIX H STEP 1 SURVEY SEQ 89 4-W4-17. PREVIOUSLY REPAIRED IAW DC8 SRM 57-2-1 FIG 2H PG 15.Oct 5, 2008 · N894UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS08853671Flap · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLAP REPLACED ON NR 188423.Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853670Flap · misrepairedINSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOVED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21.Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853605Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853603Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853565Structure · misrepairedINSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 57-2-1 FIG 2H CLASS B.Oct 3, 2008 · N894UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS08853553Skin · misrepairedINSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION REPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED.Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853648Doubler · unknownINSPECTION TYPE:SV STA-53 TO -89 RBL TO RBL 42 DOUBLER NEEDS VALIDATION FOR REPAIR 894-F 3-11. REPAIRED BY SR08530026 AND SRM 53-2-1.Oct 2, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853651Doubler · damagedINSPECTION TYPE:SV EXT DOUBLER AFT LOWER DOOR CUTOUT BS 50.5 TO 55 L30L TO 1 INCH BELOW L 29L NEED VALIDATION FOR REPAIR. REPAIRED SRM 53-02-00 FIG 13.Oct 1, 2008 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS08853695Doubler · damagedINSPECTION TYPE:SV BS 659 TO 719.5 L35L TO L35R EXT DOUBLER LOWER BELLY NEED VALIDATION FOR REPAIR. REPAIRED IAW EO DC8-5300-3I587.Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853682Doubler · damagedINSPECTION TYPE:SV EXT DOUBLER BS 1279.5 TO 1299.5 AT L35R CENTERLINE NEED VALIDATION FOR REPAIR REF SEQ 894-FA-57. REMOVED, FABBED AND REPLACED DOUBLER IAW BOEING ROD SKETCH 99-01-20-004 REV IR AND UPS EO DC8-53-20422.Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853652Doubler · damagedINSPECTION TYPE:SV EXT WINDOW DOUBLER BS 1400 TO 1421 1.5 ABOVE L14R TO 1.5 BELOW L17R NEEDS VALIDATION FOR REPAIR. REPAIRED BY SRM 51-3-0 AND EO DC 5320-31585.Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS08853599Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR. EFN 8941997-55. ORIGINAL N/R 5 34204 LEFT CUSP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. REMOVED DOUBLER VERIFIED CRACK STOP DRILLED IAW SRM 53-02-00-0. REINSTALLED DOUBLER AND VERIFIED REPAIR CSep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853598Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE EFN 89419971055 ORGINIAL N/R 534204 LEFT CUP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. VERFIED REPAIR COMPLIES WITH SRM 53-02-00 FIG 23.Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853585Cusp Web · crackedINSPECTION TYPE:SV REMOVE REPAIR AND REPLACE WITH SRM REPAIR EFN 89419971080 ORIGINAL N/R 534358 CUSP MEMBRANE CRACKED BETWEEN LIGHTENING HOLES FS 80. UPON INVESTIGATION FOUND REPAIR MISSING ONE ROW OF FASTENERS, ADDED ROW 3 RIVETS AS IAW SRM 53-02-00. FOUNSep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853568Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR ORGINIAL N/R 534146 RIGHT CUSP MEMBRANE CRACK EXTENDING FROM STOP DRILL TO AFT OF FS 1600. INSTALLED DOUBLER AS PER SRM 51-21-01.Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853567Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE ORIGINAL N/R 534909 LEFT LOWER CUSP MEMBRANE CRACKED, DENTED AND CORRODED BETWEEN FS 400-420. UPON INVESTIGATION FOUND DAMAGE WAS REMOVED AND VALIDATED REPAIR WAS A ACCOMPLISHED REF DC8 SRM 53-02-00 FIG 25.Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853550Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS CRACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2.Sep 29, 2008 · N894UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS08853586Fitting · crackedINSPECTION TYPE:SV BATH TUBE FITTINGG AT L33R-L34R IS CRACKED. REPAIR AS PER IAW DC8 SRM 51-03-02.Sep 27, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853552Skin · damagedINSPECTION TYPE:SV FLUSH SKIN REPAIR CUT BS 88 TO 14 BETWEEN L31L AND L27L NEEDS VALIDATION. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 53-02-01 FIG 007.Sep 26, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853664Skin · damagedINSPECTION TYPE:SV FUSELAGE EXTERIOR SKIN STA 50 L21R BULGING AND FASTENER HEAD SHEARED. REMOVED FASTENERS STA FS 70 TO FS 50 L19R TO L21R AND FS 50 TO FS 30 IAW DC 8 SRM 51-1-21. REMOVED DOUBLER FROM STA 7 TO STA 70 L20R-L21R. FABBED AND INSTALLED DOUBLER Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853661Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED INBOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2.Sep 23, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853660Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2.Sep 23, 2008 · N894UP · Doug DC873F · Trailing Edge FlapsSDR UPS08853622Repair · corrodedINSPECTION TYPE:SV LOWER FUSE-INT, BATHTUB FITTING REPAIR ANGLE HAS CORROSION AT FS 1180, BETWEEN L33R-L34R JUST INBOARD OF AFT CARGO DOOR CUTOUT LOWER EDGE. REPLACED REPAIR ANGLE IAW DC8 SRM 51-30-00-0-1 AND 53-02-00-0 FIG 002D.Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853563Skin · damagedINSPECTION TYPE:SV FLUSH REPAIR BS 151, 8 INCHES BELOW L21L HAS CLOSE FASTENER SPACING. ACCOMPLISHED IAW DALFORT AVIATION REPAIR XEA X8-53-706 AND REFERENCE DC8-73F SRM 53-2-0 FIG 1C PG 10 10 OF 14.Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853667Fastener · looseINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS LOOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A.Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853666Fastener · brokenINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00.Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853665Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRUDING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0.Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853504Skin · damagedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER REPAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00.Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS08853680Web · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89420061026. ORIG NR 994522 L33R STA 1 160 TO STA 1220 UPPER WEB HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABBED, AND INSTALLED NEW DOUBLER AND FASTENERS IAW REO G12470.Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853668Doubler · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971256 ORIG NR 535436 PREVIOUS REPAIR DOUBLER AND TRIPLER ON LONG 33L ARE CORRODED STA 1185-1295. REMOVED AND INSTALLED REPAIR DOUBLER IAW ROD SKETCH 97-05-06-006 AND SRM 51-30-01-00. ACTUAL REPAIR FOUNDSep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853656Web · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89419911026. ORIGINAL NR 303033. CORROSION REPAIR TO WEB AND ANGLE AT AFT PASS DOOR FS 1615-1625. REPAIR SATISFIES INTENT AND GUIDELINES OF DC8 SRM 53-2-0 FIG 001D. RF TS 894UP-20-20265.Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS08853655Door Frame · damagedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971106 ORIG NR 534710 R-1 DOOR AFT DOOR JAMB REPAIR FOR ELONGATED HOLES (FUSELAGE FRAME). EXISTING REPAIR ACCOMP IAW DWG UPS DC8-53A-011A. RFTS N894UP-12-2027.Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Main, StructureSDR UPS08853649Door Frame · damagedINSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 89419971107 ORGINIAL N/R 534711 R-1 DO OF FORWARD DOOR JAMB REPAIR FOR ELONGATED HOLES. REPAIRED BY ANGLE AND WEB REF DC8 51--21 EO DC8 5310-11728B AND DWG 53 DC8 53A-011-REV A.Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Main, Structure
Back to N894UP, cancelled Apr 4, 2018