# Service difficulty reports: N14320, cancelled Jun 3, 2011 A list on [N14320, cancelled Jun 3, 2011](https://openairdocs.org/deregistered/N14320-2011-06-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 85 reports - [SDR CALA0801011](https://openairdocs.org/sdr/CALA0801011.md): Cable · frayed · Oct 25, 2008 · N14320 · Boeing 7373T0 · Escape Slide > ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS ON (L-2) AFT ENTRY DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. - [SDR CALA0801010](https://openairdocs.org/sdr/CALA0801010.md): Cable · frayed · Oct 25, 2008 · N14320 · Boeing 7373T0 · Escape Slide > ESCAPE SLIDE LATCH CABLE HAS BROKEN STANDS ON (R-2) AFT SERVICE DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. - [SDR CALA0700688](https://openairdocs.org/sdr/CALA0700688.md): Skin · corroded · Nov 13, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND CORROSION ON BONDED DOUBLER AT STA 986.5 BELOW S27L. THE AREA WAS REPAIRED IAW ECRA 5311-01372. - [SDR CALA0700686](https://openairdocs.org/sdr/CALA0700686.md): Angle · cracked · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700684](https://openairdocs.org/sdr/CALA0700684.md): Angle · cracked · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700685](https://openairdocs.org/sdr/CALA0700685.md): Intercostal · cracked · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700683](https://openairdocs.org/sdr/CALA0700683.md): Stringer Clip · cracked · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Attach Fittings > INSPECTION 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. - [SDR CALA0700682](https://openairdocs.org/sdr/CALA0700682.md): Skin · corroded · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND SKIN CORRODED AT RIVET ROW, STA 967 BETWEEN STRINGERS 27R AND 27L. A REPAIR WAS INSTALLED IAW ECRA 5311-01377. - [SDR CALA0700676](https://openairdocs.org/sdr/CALA0700676.md): Frame · corroded · Nov 12, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION 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. - [SDR CALA0700675](https://openairdocs.org/sdr/CALA0700675.md): Skin · cracked · Nov 12, 2007 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin > INSPECTION 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. - [SDR CALA0700674](https://openairdocs.org/sdr/CALA0700674.md): Frame · corroded · Nov 11, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION 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. - [SDR CALA0700673](https://openairdocs.org/sdr/CALA0700673.md): Door Frame · cracked · Nov 11, 2007 · N14320 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION 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. - [SDR CALA0700672](https://openairdocs.org/sdr/CALA0700672.md): Door Frame · cracked · Nov 11, 2007 · N14320 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION 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. - [SDR CALA0700671](https://openairdocs.org/sdr/CALA0700671.md): Keelbeam · cracked · Nov 11, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Keel > INSPECTION 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. - [SDR CALA0700667](https://openairdocs.org/sdr/CALA0700667.md): Structure · cracked · Nov 9, 2007 · N14320 · Boeing 7373T0 · Horizontal Stabilizer Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700650](https://openairdocs.org/sdr/CALA0700650.md): Stringer · corroded · Nov 5, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 25L CORRODED AT STA 360. A REPAIR STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0700649](https://openairdocs.org/sdr/CALA0700649.md): Intercostal · cracked · Nov 5, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700648](https://openairdocs.org/sdr/CALA0700648.md): Stringer · corroded · Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND HEAVY CORROSION ON STRINGER 27L AT STA 986.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0700647](https://openairdocs.org/sdr/CALA0700647.md): Frame · corroded · Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT STA 500D BETWEEN STRINGERS 26L AND 27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700646](https://openairdocs.org/sdr/CALA0700646.md): Frame · corroded · Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT STA 500D, ABOVE S26L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700645](https://openairdocs.org/sdr/CALA0700645.md): Attach Fitting · corroded · Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Attach Fittings > INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R ATTACH CLIP CORRODED AT STA 747. A NEW CLIP WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0700643](https://openairdocs.org/sdr/CALA0700643.md): Frame · cracked · Nov 2, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION 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. - [SDR CALA0700651](https://openairdocs.org/sdr/CALA0700651.md): Intercostal · cracked · Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700642](https://openairdocs.org/sdr/CALA0700642.md): Skin · corroded · Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION 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. - [SDR CALA0700631](https://openairdocs.org/sdr/CALA0700631.md): Frame · cracked · Nov 1, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN MAIN FRAME AT STA 616 JUST BELOW CABIN FLOOR, S17L. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. - [SDR CALA0700629](https://openairdocs.org/sdr/CALA0700629.md): Stringer Splice · corroded · Oct 31, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA0700627](https://openairdocs.org/sdr/CALA0700627.md): Mount · cracked · Oct 29, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION 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. - [SDR CALA0700626](https://openairdocs.org/sdr/CALA0700626.md): Stringer · corroded · Oct 29, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 25R CORRODED AT STA 340-360. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1, FIGURE 201, DETAIL VII. - [SDR CALA0700628](https://openairdocs.org/sdr/CALA0700628.md): Release Mech · inoperative · Oct 29, 2007 · N14320 · Boeing 7373TO · Flight Compartment Windows > THE 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 FUNCTIONAL - [SDR CALA0700625](https://openairdocs.org/sdr/CALA0700625.md): Frame · cracked · Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE FRAME AT STA 767, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700624](https://openairdocs.org/sdr/CALA0700624.md): Frame · cracked · Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE FRAME AT STA 867, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700623](https://openairdocs.org/sdr/CALA0700623.md): Frame · cracked · Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8L AND S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700622](https://openairdocs.org/sdr/CALA0700622.md): Frame · cracked · Oct 27, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8R AND S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. - [SDR CALA0700621](https://openairdocs.org/sdr/CALA0700621.md): Floorbeam · corroded · Oct 26, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700608](https://openairdocs.org/sdr/CALA0700608.md): Stringer · cracked · Oct 24, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA0700600](https://openairdocs.org/sdr/CALA0700600.md): Angle · corroded · Oct 21, 2007 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0700597](https://openairdocs.org/sdr/CALA0700597.md): Floorbeam · corroded · Oct 21, 2007 · N14320 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 360, BL 0. REPAIRED IAW SRM 53-30-51. - [SDR CALA0600226](https://openairdocs.org/sdr/CALA0600226.md): Pin · worn · Jun 29, 2006 · N14320 · Boeing 7373T0 · Service Doors > THE 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. - [SDR CALA0600094](https://openairdocs.org/sdr/CALA0600094.md): Frame · corroded · Mar 22, 2006 · N14320 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION 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. - [SDR CALA0600093](https://openairdocs.org/sdr/CALA0600093.md): Skin · cracked · Mar 22, 2006 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin > INSPECTION 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. - [SDR CALA0500375](https://openairdocs.org/sdr/CALA0500375.md): Slide · twisted · Sep 22, 2005 · N14320 · Boeing 7373T0 · Escape Slide > R-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 WI - [SDR CALA0300675](https://openairdocs.org/sdr/CALA0300675.md): Keelbeam · corroded · Nov 22, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, Keel > INSPECTION FOUND UPPER SURFACE OF O/B FLANGE OF LEFT KEELBEAM CORRODED AT STA 720. A REPAIR WAS INSTALLED IAW ECRA 5311-01177. - [SDR CALA0300657](https://openairdocs.org/sdr/CALA0300657.md): Web · cracked · Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure > INSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002. - [SDR CALA0300656](https://openairdocs.org/sdr/CALA0300656.md): Strap · cracked · Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002. - [SDR CALA0300655](https://openairdocs.org/sdr/CALA0300655.md): Strap · cracked · Nov 20, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002. - [SDR CALA0300648](https://openairdocs.org/sdr/CALA0300648.md): Fitting · cracked · Nov 14, 2003 · N14320 · Boeing 7373T0 · Nacelle/Pylon, Attach Fittings > INSPECTION 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. - [SDR CALA0300647](https://openairdocs.org/sdr/CALA0300647.md): Strap · broken · Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND STRAP BROKEN ON BOTTOM OF BEAMS AT STA 312-328, RBL 42. THE STRAP WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA0300643](https://openairdocs.org/sdr/CALA0300643.md): Channel · corroded · Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0300642](https://openairdocs.org/sdr/CALA0300642.md): Skin · gouged · Nov 14, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION 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. - [SDR CALA0300641](https://openairdocs.org/sdr/CALA0300641.md): Skin · gouged · Nov 13, 2003 · N14320 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT STA 314, S27L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. Next page: https://openairdocs.org/deregistered/N14320-2011-06-03/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N14320-2011-06-03/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.