N14320, cancelled Jun 3, 2011

Service difficulty reports · 85

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 = 'N14320' AND deregistration_id = 'N14320-2011-06-03'
  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 CALA0801011Cable · frayedESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS ON (L-2) AFT ENTRY DOOR. INSTALLED NEW CABLE REF AMM 25-61-35.Oct 25, 2008 · N14320 · Boeing 7373T0 · Escape SlideSDR CALA0801010Cable · frayedESCAPE SLIDE LATCH CABLE HAS BROKEN STANDS ON (R-2) AFT SERVICE DOOR. INSTALLED NEW CABLE REF AMM 25-61-35.Oct 25, 2008 · N14320 · Boeing 7373T0 · Escape SlideSDR CALA0700688Skin · corrodedINSPECTION FOUND CORROSION ON BONDED DOUBLER AT STA 986.5 BELOW S27L. THE AREA WAS REPAIRED IAW ECRA 5311-01372.Nov 13, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700686Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700684Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN UPPER ANGLE AT S16L BETWEEN STA 348.2 AND 351.2. THE ANGLE WAS REPLACED IAW ECRA 5311-01375.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700685Intercostal · crackedINSPECTION FOUND A 5 INCH CRACK AND MISSING FASTENER HEAD IN INTERCOSTAL WEB ON STRINGER 16L AT STA 348.2. THE INTERCOSTAL WEB WAS REPLACED IAW ECRA 5311-01375.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700683Stringer Clip · crackedINSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP (BROKEN FASTENER HEADS TOO) ON STRINGER 15L AT STA 348.2. THE ATTACHMENT CLIP WAS REPLACED IAW ECRA 5311-01375.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Attach FittingsSDR CALA0700682Skin · corrodedINSPECTION FOUND SKIN CORRODED AT RIVET ROW, STA 967 BETWEEN STRINGERS 27R AND 27L. A REPAIR WAS INSTALLED IAW ECRA 5311-01377.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700676Frame · corrodedINSPECTION FOUND FRAME AND SUPPORTS CORRODED AT STA 227.8, LBL 5.7 TO RBL 5.7, S28L. THE AREA WAS REPAIRED IAW ECRA 5311-01373.Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700675Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5430-01204.Nov 12, 2007 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Plate/SkinSDR CALA0700674Frame · corrodedINSPECTION FOUND FRAME AND SUPPORT CORRODED AT STA 203.8, S28L TO S28R, RBL 5.7 TO LBL 5.7. THE FRAME CHORD AND SUPPORT WERE REMOVED AND REPLACED IAW SRM 51-40-02.Nov 11, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700673Door Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR FRAME AT FORWARD LOWER SEGMENT AT PULLEY BOLT HOLE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 11, 2007 · N14320 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0700672Door Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR UPPER FRAME AT SPLICE POINT. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 11, 2007 · N14320 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0700671Keelbeam · crackedINSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM IN RIGHT A/C BAY AT STA 540. THE KEEL BEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-60-12, FIGURE 201, PAGE 201.Nov 11, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, KeelSDR CALA0700667Structure · crackedINSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER UPPER O/B CHORD AT STAB STA 101.90. THE CRACKED AREA OF CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW IAW SRM 51-70-12.Nov 9, 2007 · N14320 · Boeing 7373T0 · Horizontal Stabilizer Miscellaneous StructureSDR CALA0700650Stringer · corrodedINSPECTION FOUND STRINGER 25L CORRODED AT STA 360. A REPAIR STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.Nov 5, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700649Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ANGLE AT STA 290 BELOW S10R FORWARD OF R-1 DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.Nov 5, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700648Stringer · corrodedINSPECTION FOUND HEAVY CORROSION ON STRINGER 27L AT STA 986.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03.Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700647Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 500D BETWEEN STRINGERS 26L AND 27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07.Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700646Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 500D, ABOVE S26L. THE FRAME WAS REPAIRED IAW SRM 53-00-07.Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700645Attach Fitting · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R ATTACH CLIP CORRODED AT STA 747. A NEW CLIP WAS INSTALLED IAW SRM 51-40-02.Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Attach FittingsSDR CALA0700643Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 847 BETWEEN STRINGER 23R AND 24R. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02, PARAGRAPH 4 AND 7 AND BAC DRAWING 65C35243.Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700651Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 280, S14R FORWARD OF R-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700642Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED JUST FORWARD OF STA 500D ABOVE S27R. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700631Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 JUST BELOW CABIN FLOOR, S17L. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700629Stringer Splice · corrodedINSPECTION FOUND STRINGER SPLICE 27L CORRODED AT STA 360. THE CHANNEL SPLICE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND AMM 51-31-00.Oct 31, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700627Mount · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 VHF ANTENNA MOUNTING BRACKET AT FORWARD CARGO BIN BETWEEN S28L AND S28R. THE MOUNTING BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.Oct 29, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700626Stringer · corrodedINSPECTION FOUND STRINGER 25R CORRODED AT STA 340-360. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1, FIGURE 201, DETAIL VII.Oct 29, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700628Release Mech · inoperativeTHE FIRST OFFICER'S SLIDING WINDOW (R2) FAILED OPERATIONAL TEST FROM OUTSIDE THE CONTROL CABIN (WINDOW DID NOT UNLOCK AND OPEN WHEN THE EXTERNAL RELEASE HANDLE WAS PULLED). THE EMERGENCY RELEASE MECHANISM WAS LUBRICATED AND THE AREA WAS CLEANED. A FUNCTIONALOct 29, 2007 · N14320 · Boeing 7373TO · Flight Compartment WindowsSDR CALA0700625Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700624Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 867, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700623Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8L AND S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700622Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8R AND S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700621Floorbeam · corrodedINSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02.Oct 26, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0700608Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C FORWARD OF WING SCANNING LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 201, FIGURE 201, REPAIR 1.Oct 24, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700600Angle · corrodedINSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1016, LBL 45. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Oct 21, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700597Floorbeam · corrodedINSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 360, BL 0. REPAIRED IAW SRM 53-30-51.Oct 21, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0600226Pin · wornTHE R-1 DOOR COULD BE CLOSED WITHOUT RELEASING THE HOLD OPEN CAM PLATE PIN. MAINTENANCE FOUND THE PIN WORN. THE DOOR RELEASE LEVER WAS REPLACED IAW MM 52-41-00. OPERATIONAL CHECKS WERE GOOD.Jun 29, 2006 · N14320 · Boeing 7373T0 · Service DoorsSDR CALA0600094Frame · corrodedINSPECTION FOUND FRAME CORRODED IN AFT BAGGAGE BIN AT FLOOR SUPPORT WEB FUSELAGE ATTACH AREA, STA 927 BETWEEN S26L AND S26R. A SHEAR TIE WAS INSTALLED IAW SRM 53-00-07.Mar 22, 2006 · N14320 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0600093Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN AT UPPER FORWARD O/B PANEL, NAC STA 224. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.Mar 22, 2006 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Plate/SkinSDR CALA0500375Slide · twistedR-1 DOOR EVACUATION SLIDE FAILED TO DEPLOY PROPERLY DURING DEPLOYMENT TEST. SLIDE INFLATED EARLY CAUSING SLIDE TO INFLATE BETWEEN DOOR & DOOR OPENING NOT ALLOWING DOOR TO COMPLETELY OPEN. SLIDE DEPLOYED SIDEWAYS INSTEAD OF FLAT. SLIDE INFLATED COMPLETELY WISep 22, 2005 · N14320 · Boeing 7373T0 · Escape SlideSDR CALA0300675Keelbeam · corrodedINSPECTION FOUND UPPER SURFACE OF O/B FLANGE OF LEFT KEELBEAM CORRODED AT STA 720. A REPAIR WAS INSTALLED IAW ECRA 5311-01177.Nov 22, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, KeelSDR CALA0300657Web · crackedINSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002.Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous StructureSDR CALA0300656Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002.Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous StructureSDR CALA0300655Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002.Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous StructureSDR CALA0300648Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 1 PYLON FORWARD FITTING AT LOWER I/B CORNER. THE NR 1 PYLON FORWARD FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.Nov 14, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Attach FittingsSDR CALA0300647Strap · brokenINSPECTION FOUND STRAP BROKEN ON BOTTOM OF BEAMS AT STA 312-328, RBL 42. THE STRAP WAS REPAIRED IAW SRM 53-10-51.Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300643Channel · corrodedINSPECTION FOUND HAT CHANNEL FOR ANTENNA CORRODED AT STA 727D +12, S27L. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02.Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300642Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 727D + 8, LBL 2. THE GOUGED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0300641Skin · gougedINSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT STA 314, S27L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.Nov 13, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin
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