N69311, cancelled May 18, 2010

Service difficulty reports · 92

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 = 'N69311' AND deregistration_id = 'N69311-2010-05-18'
  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 CALA2009101900634Battery · dischargedR-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED BATTERY FOR R-1 DOOR EMERGENCY LIGHTS, OPS GOOD.Oct 19, 2009 · N69311 · Boeing 7373T0 · Emergency LightingSDR CALA2009012300054Skin · crackedFOUND 1.5 INCH LONG SKIN CRACK AT FUSELAGE OUTER SKIN AT 3 INCHES AFT OF STATION 727E AND S-24R. INSTALLED DOUBLER REPAIR, ALL HOLES WERE ZERO TIMED PER SRM 53-00-01, REPAIR 31, PROCEDURE 5. PLACED ON DIP TO INSPECT REPAIR AT 60,000 FLT CYCLES, AFTER REPAIR Jan 22, 2009 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA2009012200052Skin · crackedAFT LEFT FUSELAGE SKIN CRACKED AT APPROX STATION 747 FOUR STRINGERS BELOW LOWER LAP JOINT, CRACK 1.5 INCH LONG. PERFORMED HF EDDY CURRENT IAW NAT 51-00-00 PART 6. REPAIRED PER SRM 53-00-01, REPAIR 31, PROCEDURE V.Jan 21, 2009 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700364Attach Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN H-STRAP ON FUSELAGE STRUCTURE STA 312 L-1 DOOR LOWER HINGE ATTACH FITTING. A REPAIR WAS INSTALLED IAW ECRA 5311-01342.Jul 17, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Attach FittingsSDR CALA0700361Skin · corrodedINSPECTION FOUND SKIN STRAP CORRODED AT STA 1006, S27R, BL 0 TO RBL 8. THE CORRODED SECTION OF SKIN STRAP WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01327.Jul 16, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700359Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.Jul 15, 2007 · N69311 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous StructureSDR CALA0700358Structure · corrodedINSPECTION FOUND CHORD CORRODED AT STA 227.8, RBL 9 TO LBL 9. A LOWER O/B CHORD REPAIR WAS INSTALLED IAW ECRA 5311-01340.Jul 15, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700354Attach Fitting · crackedINSPECTION FOUND A .5 INCH CRACK AT AFT END OF ATTACHMENT CLIP, STA 294-309, S10L. THE CLIP WAS REPLACED IAW ECRA 5311-01337.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700353Strap · crackedINSPECTION FOUND A .5 INCH CRACK IN H-STRAP AT THE UPPER L-1 DOOR HINGE ATTACH FITTING, STA 312. THE H-STRAP WAS REPLACED IAW ECRA 5311-01337.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700352Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN STUB FRAME FOR L-2 DOOR UPPER HINGE AREA, STA 947.5, S11L. THE FRAME WAS REPAIRED IAW ECRA 5311-01335.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700351Web · crackedINSPECTION FOUND A 1 INCH CRACK IN WEB JUST FORWARD OF L-2 DOOR AT STA 942, S11L. THE CLOSE OUT WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01335.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700350Attach Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK AT I/B CORNER OF ATTACHMENT CLIP, STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01339.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700349Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL WEB AT RIVET LOCATED AT STA 294.5, S12L. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01339.Jul 12, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700347Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED ON FORWARD END BETWEEN STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 11, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700343Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S27R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW MM 51-40-02.Jul 10, 2007 · N69311 · Boeing 7373T0 · Fuselage Internal Mounting StructureSDR CALA0700348Flap Track · corrodedINSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORROSION IN THE BORE WAS REAMED, SHOT PEENED, PLATED AND A SLEEVE BUSHING WAS INSTALLED IAW CMM 57-53-15, PAGE 16, FIGURE 6 AND SOPM 20-42-10 AJul 7, 2007 · N69311 · Boeing 7373T0 · Trailing Edge FlapsSDR CALA0700341Gusset · crackedINSPECTION FOUND A 2 INCH CRACK IN NOSE WHEEL WELL GUSSET AT END OF NLG DRAG BRACE. THE GUSSET WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 7, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700339Door Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 440, S17R TO 24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 6, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, StructureSDR CALA0700338Pan · crackedINSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941.Jul 6, 2007 · N69311 · Boeing 7373T0 · Passenger/Crew DoorsSDR CALA0700344Fitting · corrodedINSPECTION FOUND STRINGER 17R END FITTING CORRODED JUST BELOW FLOOR LINE AT STA 1016. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 3, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700335Fitting · corrodedINSPECTION FOUND STRINGER 27R END FITTING CORRODED IN BOLT HOLES AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700334Fitting · corrodedINSPECTION FOUND STRINGER 27L END FITTING CORRODED IN BOLT HOLES, STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-12.Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700333Angle · corrodedINSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD FACE LOWER CHORD ANGLE CORRODED AT STA 1016 FROM S27L T0 S27R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jul 1, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700331Door Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 440. THE FORWARD FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 30, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, StructureSDR CALA0700330Pressure Panel · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02.Jun 29, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, BulkheadSDR CALA0700329Web · corrodedINSPECTION FOUND WEB CORRODED FROM STA 986.5 TO 1006, S21R. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40-02.Jun 28, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700327Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 986.5, LBL 43. THE CORRODED T-CHORD SECTION OF BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 27, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0700326Floorbeam · corrodedINSPECTION FOUND SURFACE CORROSION AROUND SCREW HOLES ON FLOORBEAM AT STA 1016 FROM LBL 30 TO LBL 34, S19L-S21L. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.Jun 27, 2007 · N69311 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0700324Fitting · crackedINSPECTION FOUND A 0.65 INCH CRACK IN CLIP AT STA 616, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 26, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700323Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN CLIP AT STA 597, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 26, 2007 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0600005Spar · corrodedINSPECTION FOUND THE LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CORRODED FROM STAB STA 196.2 TO 200.3. THE LT HORIZONTAL STABILIZER ASSEMBLY WAS REMOVED AND REPLACED MM 27-41-11, PAGE 401, FIGURE 401.Jan 10, 2006 · N69311 · Boeing 7373T0 · Horizontal Stabilizer, Spar/RibSDR CALA0600002Skin · crackedINSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.Jan 8, 2006 · N69311 · Boeing 7373T0 · Nacelle/Pylon, Plate/SkinSDR CALA0400683Skin · crackedINSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090.Oct 22, 2004 · N69311 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0300525Keelbeam · corrodedINSPECTION FOUND LIGHT CORROSION ON O/B FLANGE OF LEFT KEELBEAM FROM BS 663-727. INSTALLED REPAIR IAW ECRA 5311-01167.Sep 11, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, KeelSDR CALA0300529Floorbeam · corrodedINSPECTION FOUND CORROSION ALONG THE ENTIRE UPPER SECTION OF FLOORBEAM AT STA 967. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142.Sep 5, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300514Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING UPPER AFT INBOARD T/E PANEL OUTBOARD SUPPORT FITTING. A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 51-10-02.Sep 5, 2003 · N69311 · Boeing 7373T0 · Trailing Edge FlapsSDR CALA0300513Cargo Track · corrodedINSPECTION FOUND LT TIE DOWN RAIL CORRODED AT FASTENERS ON LOWER SURFACE AT STA 947 IN THE AFT CARGO COMPARTMENT. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53.Sep 4, 2003 · N69311 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0300510Frame · corrodedINSPECTION FOUND CORROSION ON FRAME AT STA 793 BETWEEN S26R AND S25R IN AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-40-02.Sep 3, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0300509Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.Sep 3, 2003 · N69311 · Boeing 7373T0 · Nacelle/Pylon, Main FrameSDR CALA0300507Bracket · crackedINSPECTION FOUND A .2500 INCH CRACK IN VHF RIGHT FORWARD SUPPORT AFT CARGO COMPARTMENT BRACKET AT STA 727D. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-02.Aug 30, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300506Shear Tie · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN SKIN SHEAR TIE CORRODED AT STA 460, S28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHEAR TIE WERE INSTALLED IAW SRM 53-00-07.Aug 30, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, StructureSDR CALA0300505Floor Panel · crackedINSPECTION FOUND A 1 INCH AND .5000 INCH CRACK IN AFT BAGGAGE BIN FLOOR PANEL 1536X AT STA 794.5-807. A DOUBLER WAS INSTALLED AT EACH CRACK LOCATION IAW SRM 53-30-53.Aug 29, 2003 · N69311 · Boeing 7373T0 · Fuselage Floor PanelSDR CALA0300504Door Frame · crackedINSPECTION FOUND A 7.5 INCH CRACK IN FORWARD BAGGAGE BIN WEB AT FORWARD LOWER DOOR JAMB, STA 440. A NEW SECTION OF WEB WAS INSTALLED IAW SRM 51-70-13.Aug 29, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, StructureSDR CALA0300503Support · crackedINSPECTION FOUND A .5000 INCH CRACK IN RT WING UPPER MOST I/B T/E PANEL SUPPORT. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02.Aug 29, 2003 · N69311 · Boeing 7373T0 · Wing Miscellaneous StructureSDR CALA0300502Galley Track · corrodedINSPECTION FOUND NR 3 GALLEY I/B AFT MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.Aug 28, 2003 · N69311 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0300501Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616. A DOUBLER ANGLE WAS INSTALLED IAW ECRA 5311-01158.Aug 27, 2003 · N69311 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0300500Stiffener · gougedINSPECTION FOUND RT WING NR 6 FLAP TRACK FAIRING I/B STIFFENER GOUGED. THE STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-02.Aug 27, 2003 · N69311 · Boeing 7373T0 · Trailing Edge FlapsSDR CALA0300498Bracket · corrodedINSPECTION FOUND CORROSION ON CORNER BRACKET O/B OF DOOR CUTOUT RT AFT CORNER FWD ACC COMPT, STA 219. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.Aug 26, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300497Floor Support · corrodedINSPECTION FOUND UPPER AND LOWER SURFACE OF FLOOR SUPPORT CORRODED BETWEEN STA 967 AND 986.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.Aug 26, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300494Angle · corrodedINSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT BS 947-986, LBL 48. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.Aug 25, 2003 · N69311 · Boeing 7373T0 · Fuselage Miscellaneous Structure
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