N108AX, cancelled Aug 3, 2011

Service difficulty reports · 38

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 = 'N108AX' AND deregistration_id = 'N108AX-2011-08-03'
  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 CNMA20100003Access Door · leakingAT 370 FL COULD NOT CONTROL CABIN CLIMB IN AUTO, STANBY, OR MANUAL CLIMBING AT 1000 FT IAW MIN HAD TO DESCENT TO MAINTAIN 9500 FT CABIN AT FL 290. FOUND FWD AVIONICS DOOR LEAKING, RESET DOOR & PRESSURIZED ACFT TO 5 PSID & INSPECTED ALL DOORS ACFT OK FOR CONTIJan 28, 2010 · N108AX · Doug DC1030 · Electrical/Electronic Compartment DoorsSDR CNMA20090015Fuel Tank · leakingRT WING LEAKING FUEL IN FLIGHT.Jul 13, 2009 · N108AX · Doug DC1030 · Fuel StorageSDR CNMA20090055Seat Track · corrodedLIGHT CORROSION ON SEAT TRACK (N6) LT UNDER THRESHOLD PAX DOOR 4 LT REMOVE THRESHOLD PLATE AND DRAIN VALVES ON DOOR NR 4 LT OK DONE AS AMM 53-10-01, REV 81. REMOVE CORROSION IAW SRM 51-21-01, VOL II, REV 93 PERFORMED AS REQUIRED MAX DEPTH 2.5 MM OUT OF SRM LIAug 8, 2008 · N108AX · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CNMA20090054Skin · dentedDENT ON FUSELAGE SKIN STA 729 - LONGERON 43. PERFORM REPAIR IAW SRM 53-20-00 FIG SH3, REV 45, VOL I, OK PERFORM REPAIR AS REQUIRED.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/SkinSDR CNMA20090053Floorbeam · corrodedCORROSION ON FLOOR SUPPORT AT STA 815 X19. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG ADA7326 AND 7548 AND SRM 51-35-01, STEP 1, VOL II, REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090052Floorbeam · corrodedLIGHT CORROSION ON FLOORBEAM AT STA 859 X-72. REMOVED CORROSION IAW SRM 51-21-01, ERV 94, VOL II OUT OF LIMITS. REPLACED PN ADD 7160-2 IAW SRM 51-35-01, VOL II, REV 94, STEP 1 (REF DWG ADD 7163).Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090051Floorbeam · corrodedCORROSION ON FLOOR SUPPORT TEE AT AFTER PRESSURE BULKHEAD, STA 2007. X-40 - X-60, AND X 20. PERFORMED REPAIR IAW SRM 53-40-00, FIG 16, REF 94, VOL I.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090050Support · crackedGALLEY SUPPORT CORRODED AT STA 459 XX24. REPLACED PN ACA7366-501 IAW DWG ACA7365 AND SRM51-35-01, VOL II, REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090049Fitting · corrodedCORROSION ON FITTING GALLEY AT STA 879, X44. REMOVED CORROSION IAW SRM 51-21-24 VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3.5 MM. FABRICATED PN AWD7743-503, REF DWG AWD 7743 AND INSTALL NEW PN IAW SRM 51-31-03, VOL II, REV 94, PAGES 1 THRU 66 AS Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Attach FittingsSDR CNMA20090048Floorbeam · corrodedLIGHT CORROSION ON FLOOR SUPPORT AT STA 815 X-18. FABRICATED AND INSTALLED NEW PN ADA7326-1 IAW DWG 7696 AND ADA7548 AND SRM 51-35-01 STEP 1, VOL II REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090047Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT STA 859 - 893 X73. REPLACED PN ADA7160-1 IAW DWG ADA7160 AND DWG 7163 AND MM 20-50-02 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090046Floor Support · corrodedLIGHT CORROSION ON FLOORBEAM SUPPORT BETWEEN STA 1820-1887 X36. REMOVED BEAM IAW SRM 51-31-01 VOL II REV 94. FABRICATED PN AGA7085-1 ED INSTALLED IAW DWG ASA 7127 AND MM 20-50-02 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090045Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1871-2007 AND X=107.25. REMOVED CORROSION IAW SRM 51-21-01 V II REV 94 DIMENSIONS OUT OF LIMITS (120 X 50 X 2,3 MM). REPLACED PN NRA6222-9 IAW DWG NFA6222. INSTALLED PN AFA7789-535 IAW SRM 51-35-01 AND 51-33-01 V II INSTEAug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)SDR CNMA20090044Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1902 - 2007 AND X=75.25. CORROSION REMOVED IAW SRM 51-21-01 V G REV 94 DIMENTIONS ARE OUT OF LIMITS (240 X 8T X 2,4 MM) FABRICATED AND INSTALLED TRACK PN AGA7086-506 IAW DWG AGA7086 AND DWG ASA 7127 AND MM 205002 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)SDR CNMA20090043Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1887-2007 AND X=27.50. REMOVED BEAM IAW SRM 51-31-01, VOL II, REV 94 AND MM 20-50-02 REV 81. FABRICATED PN ASA7087-1 IAW DWG ASA7087 AND INSTALLED IAW DWG AGA7127 AND MM 20-50-02 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Structure (General)SDR CNMA20090041Skin · crackedHFEC INSP ON HS IAW J/C 10AD-904 SB 455-18. FOUND ONE CRACK INDICATION 37MM LENGTH ON OUTER SECTION UPPER AFTER SKIN PANEL RT SIDE. PERFORMED STOP DRILL AS REQUIED IAW SB A55-18 STEP 11C PAG 7 REV 6. FOR REPLACEMENT SEE ODL PGO-067.Aug 8, 2008 · N108AX · Doug DC1030 · Horizontal Stabilizer, Plate/SkinSDR CNMA20090042Cargo Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1931.500 -2007 AND X=8.50. REMOVED BEAM IAW SRM 51-31-01 VOL I REV 94 AND MM 20-50-02 REV 81. FABRICATED PN AGA7088-1 IAW DWG ASA7088 AND INSTALLED IAW DWG ASA7127 AND SRM 51-35-01 VOL II REV 94 AND MM 20-50-02 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CNMA20090041ADoor Frame · crackedFWD CARGO NEAR DOOR JAMB PANEL NR 127AR CRACKED. REMOVED PANEL 127AR AMM 20-50-02 REV 81. WELD PER DPS 10225 INSTALLED PANEL 127AR IAW MM 20-50-02 REV 81.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, StructureSDR CNMA20090040Stiffener · corrodedCTR WHEEL WELL AFT CLOSING BULKHEADS WITH A STIFFENER CORRODED. REPLACED PN AYB7080-9, REF DWG BOE AYB 7080 IAW SRM 51-35-01, REV 94, VOL I, STEP 9.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, BulkheadSDR CNMA20090039Support · corrodedNR 2 GALLEY SUPPORT CORRODED AT STA 465 RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 4 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01 VOL II REV 94 (PAGES 1 - 66Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090038Support · corrodedNR 2 GALLEY SUPPORT CORRODED AT STA 435, RT AND LT SIDE. REMOVED CORROSION IAW SRM 51-21-01, VOL II, REV 94 WITHOUT LIMITS DEPTH MATERIAL REMOVED 3 MM. FABRICATED PN AWD7743-503 REF DWG AWD7743 AND INSTALLED NEW PN IAW SRM 51-33-01, VOL II, REV 94 (PAGE 1 TAug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090037Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN STA 440 / 453, XO. FABRICATED AND INSTALLED NEW PN ACA7374-1 IAW DWG ACA7374 AND 7365 AND SRM 51-35-01 V I REV 94 STEP 1.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090036Support · crackedCTR CARGO DOOR EXTERNAL FAIRING SUPPORT CRACKED (AFT POSITION). PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2, REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Cargo/Baggage DoorsSDR CNMA20090035Floorbeam · crackedCTR CARGO COMPT, FLOOR STRUCTURE, AT STA 1523 (FWD BULKHEAD) NR 4 ANGULARS CRACKED. OPEN PANELS 183JE-183FE FWD BULKHEAD CTR CARGO COMPARTMENT IAW AMM 20-50-02 REV 81. PERFORM REPAIR IAW SRM 53-00-01, FIG 8, SHI REV 93 VOL I OK DONE. CLOSE PANELS 183JE, 189Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090034Floor Support · crackedAFT CARGO COMPT FLOOR SUPPORT STRUCTURE AT STA 1921 LT SIDE ANGULAR CRACKED. PERFORMED REPAIR IAW SRM 53-00-01, FIG 8, SHT 1, REV 94 (VOL I).Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090033Panel · damagedPYLON NR 2 PANEL, 457BT DAMAGED. REPAIRED IAW SRM 54-00-01, FIG 1A SHEET 1 REV 94 VOL J.Aug 8, 2008 · N108AX · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CNMA20090032Beam · crackedCTR CARGO COMP STA 1781 NR 3 LT BEAM OF ZONE PLENUM CRACKED. REMOVED BEAM IAW MM 20-50-02 REV 81. PERFORMED DRILL NEW BEAM IAW DWG AF)7011-3. REPLACED BEAM IAW AMM 20-50-02 REV 81 AND INSTALLED ALL OMNI DIRECTIONAL ROLLERS.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, StructureSDR CNMA20090031Floorbeam · crackedCTR CARGO COMP FLOOR UNLOAD BEAM CRACKED AT STA 1690 (UPPER FLANGE) PERFORMED REPAIR IAW SRM 53-70-00 FIG 3 REV 93 VOL J. PERFORMED PAINTING IAW SRM 51-21-02 VOL II REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Floor BeamSDR CNMA20090030Structure · crackedRT OTBD FLAP INBD RIB CLOSURE HAS AN ANGULAR CRACK. REMOVED RT OTBD FLAP, INBD T/E SECTION. REMOVED ALL SCREWS SIZED IAW SRM 51-31-01 VOL 2 REV 93. REMOVED RT OTBD FLAP INBD SECTION T/E IAS MM 20-50-02 REV 81. FABRICATED PN ARC1951-6 IAW DWG ARC1951 AND INSAug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090029Panel · crackedLT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090025Panel · crackedLT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090028Support · crackedLT OTBD FLAP, INBD HINGE STRUCTURE UNDER PANEL 535JL, SUPPORT CRACKED. REPLACED SUPPORTS CRACKED UNDER PANEL 535JL IAW SRM 51-35-01 VOL II REV 93.Aug 8, 2008 · N108AX · Doug DC1030 · Wing Miscellaneous StructureSDR CNMA20090027Panel · crackedLT OTBD FLAP, INBD HINGE PANEL 535JL CRACKED. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VII PERFORMED WELD IAW DPS10225. REINSTALLED OLD REPAIR IAW SRM 51-35-02 VII 4REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090026Panel · delaminatedLT INBD FLAP, OTBD HINGE, PANEL 541JL UNGLUED. PERFORMED REPAIR IAW DWG ARC 2541.Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090024Panel · crackedLT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090023Structure · dentedDENT AT STA 1853.93 LONG 47 REPAIR NEXT C CHK. PERFORMED SANDING AS REQUESTED AS DPS 9.316. PERFORMED REPAIR IAW SRM 53-20-00, FIG 6 (SHT 3) V.I. REV 93. PERFORMED PAINTING OF REPAIRED AREA IAW SRM 51-21-02 VOL 2 REV 94.Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090022Skin · dentedDENT 30 INCH, FWD OF R1 DOOR SILL - DENT 6 INCH LONG WITHIN LIMITS IAW SRM VOL I-53-20-00 PERFORM PERMANENT REPAIR. REMOVED DUCT IAW 20-50-02 AND MANIFOLD AIR CONDITIONING IAW 21-10-00. PERFORM CUTOUT SKIN DAMAGE IAW SRM 53-20-00 FIG 6, REV 93, VOL I. MADE Aug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/SkinSDR CNMA20090021Skin · dentedUNDER RT PITOT TUBE HAS FUSELAGE DENT PERFORM PERMANENT REPAIR. REMOVED ELECTRICAL EQUIPMENT TO ACCESS ZONE. REMOVE BRACKET AS AMM 77-13-01 (TRANSDUCER NOT INSTALLED). REMOVED DUCT AS MM 21-26-00 REV 81. PERFORM STRIPPING AS REQUESTED IAW DPS 9.316. PERFAug 8, 2008 · N108AX · Doug DC1030 · Fuselage Main, Plate/Skin
Back to N108AX, cancelled Aug 3, 2011