# Service difficulty reports: N14324, cancelled Jul 13, 2011 A list on [N14324, cancelled Jul 13, 2011](https://openairdocs.org/deregistered/N14324-2011-07-13.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 3 · 115 reports - [SDR CALA2009100500585](https://openairdocs.org/sdr/CALA2009100500585.md): Logic Card · malfunctioned · Oct 2, 2009 · N14324 · Boeing 7373T0 · Landing Gear Position and Warning > ON DESCENT WITH POWER AT IDLE, ONLY NOSE UNSAFE LIGHT ILLUMINATED. AFTER SELECTING GEAR DOWN NO INDICATION EITHER RED OR GREEN. RAN QHR CONSULTED WITH IAH MX. RESET AIR/GND C/B AND ALL INDICATIONS NORMAL. REMOVED AND REPLACED M988 AND M982 LG LOGIC CARDS. - [SDR CALA2009080400426](https://openairdocs.org/sdr/CALA2009080400426.md): Light · inoperative · Aug 4, 2009 · N14324 · Boeing 7373T0 · Emergency Lighting > LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED SOCKET ASSY, LAMP AND LENS ASSY. OPERATIONAL CHECKS GOOD. - [SDR CALA2009012800064](https://openairdocs.org/sdr/CALA2009012800064.md): Charger · inoperative · Jan 27, 2009 · N14324 · Boeing 7373T0 · Emergency Lighting > FIRST CLASS EMERGENCY EXIT ROW AISLE LIGHTS INOPERATIVE. PERFORMED TROUBLESHOOTING PER MM 33-51-02, REPLACED FORWARD BATTERY PACK AND CHARGER, OPERATIONAL CHECKS GOOD. - [SDR CALA0700513](https://openairdocs.org/sdr/CALA0700513.md): Strap · cracked · Sep 12, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN STRAP ON RT SIDE OF FUSELAGE AT STA 1156, S13R BELOW HORIZONTAL STABILIZER. THE STRAP WAS REPAIRED IAW ECRA 5331-01344. - [SDR CALA0700512](https://openairdocs.org/sdr/CALA0700512.md): Skin · cracked · Sep 12, 2007 · N14324 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A 0.35 INCH CRACK AT LIGHTENING HOLE IN C-1 CARGO DOOR INTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5232-01090. - [SDR CALA0700507](https://openairdocs.org/sdr/CALA0700507.md): Stringer · cracked · Sep 8, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 360. A STRINGER SPLICE WAS INSTALLED IAW ECRA 5311-01354. - [SDR CALA0700506](https://openairdocs.org/sdr/CALA0700506.md): Shear Tie · cracked · Sep 8, 2007 · N14324 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND A.5 INCH CRACK IN SHEAR TIE AT STA 947 BELOW S25R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700504](https://openairdocs.org/sdr/CALA0700504.md): Keelbeam · corroded · Sep 7, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Keel > INSPECTION FOUND LEFT KEEL BEAM CORRODED JUST AFT OF STA 540 ON THE O/B FACE. THE CORRODED SECTION OF THE KEEL BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-60-12. - [SDR CALA0700503](https://openairdocs.org/sdr/CALA0700503.md): Stringer · corroded · Sep 6, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND AFT CARGO STRINGER 26L CORRODED AT STA 727E + 11 INCHES. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS SPLICED IN IAW SRM 53-00-03. - [SDR CALA0700502](https://openairdocs.org/sdr/CALA0700502.md): Frame · cracked · Sep 6, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK IN FRAME O/B OF LEFT KEEL BEAM AT STA 520, S27L TO S28L. THE CRACK WAS LOCATED AT THE SECOND FASTENER HOLE FROM THE BOTTOM. - [SDR CALA0700487](https://openairdocs.org/sdr/CALA0700487.md): Frame · corroded · Sep 2, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT STA 807 BETWEEN S27L AND S27R, LBL 6 TO RBL 6. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02. - [SDR CALA0700485](https://openairdocs.org/sdr/CALA0700485.md): Web · cracked · Sep 2, 2007 · N14324 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A.25 INCH CRACK IN C-2 DOOR LOWER BEAM NR 5 WEB. THE CRACK WAS AT A FASTENER HOLE NEAR FORWARD STOP FITTING AND OUTER T-CHORD. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700484](https://openairdocs.org/sdr/CALA0700484.md): Structure · cracked · Sep 2, 2007 · N14324 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A.5 INCH CRACK AT FORWARD AND AFT CORNERS OF C-2 DOOR LOWER T-CHORD. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700483](https://openairdocs.org/sdr/CALA0700483.md): Fitting · cracked · Aug 31, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN FRAME TO STRINGER CLIP AT STA 847, S27L, LBL 3. A NEW CLIP WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0700482](https://openairdocs.org/sdr/CALA0700482.md): Shear Tie · corroded · Aug 31, 2007 · N14324 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 BETWEEN STRINGER 26L AND 27L, LBL 5 TO LBL 15. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07, FIGURE 201. - [SDR CALA0700481](https://openairdocs.org/sdr/CALA0700481.md): Skin · cracked · Aug 31, 2007 · N14324 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 2. - [SDR CALA0700479](https://openairdocs.org/sdr/CALA0700479.md): Fitting · corroded · Aug 30, 2007 · N14324 · Boeing 7373T0 · Nacelle/Pylon, Attach Fittings > INSPECTION FOUND NR 2 ENGINE LT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629. - [SDR CALA0700478](https://openairdocs.org/sdr/CALA0700478.md): Fitting · corroded · Aug 30, 2007 · N14324 · Boeing 7373T0 · Nacelle/Pylon, Attach Fittings > INSPECTION FOUND NR 2 ENGINE RT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629. - [SDR CALA0700477](https://openairdocs.org/sdr/CALA0700477.md): Shear Tie · corroded · Aug 30, 2007 · N14324 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 JUST I/B OF S27L, LBL 8. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07. - [SDR CALA0700476](https://openairdocs.org/sdr/CALA0700476.md): Skin · cracked · Aug 30, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1" CRACK IN SKIN JUST AFT OF STA 727E, S24L. A DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31. - [SDR CALA0700474](https://openairdocs.org/sdr/CALA0700474.md): Frame · cracked · Aug 30, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 500D ONE INCH ABOVE S13R. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700473](https://openairdocs.org/sdr/CALA0700473.md): Skin · cracked · Aug 30, 2007 · N14324 · Boeing 7373T0 · Cargo/Baggage Doors > INSPECTION FOUND A.25 INCH CRACK IN C-1 CARGO DOOR SKIN AT HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01. - [SDR CALA0700472](https://openairdocs.org/sdr/CALA0700472.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700471](https://openairdocs.org/sdr/CALA0700471.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.5 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700470](https://openairdocs.org/sdr/CALA0700470.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK IN FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700469](https://openairdocs.org/sdr/CALA0700469.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK IN FRAME AT STA 380 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700468](https://openairdocs.org/sdr/CALA0700468.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700467](https://openairdocs.org/sdr/CALA0700467.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700466](https://openairdocs.org/sdr/CALA0700466.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700465](https://openairdocs.org/sdr/CALA0700465.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. - [SDR CALA0700464](https://openairdocs.org/sdr/CALA0700464.md): Frame · cracked · Aug 29, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.75 INCH CRACK AROUND RIVET IN FRAME AT STA 807 ABOVE S9L. REPAIR PARTS WERE INSTALLED IAW ECRA 5310-04650. - [SDR CALA0700463](https://openairdocs.org/sdr/CALA0700463.md): Frame · corroded · Aug 28, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT STA 947, S26R TO S27R. THE FRAME WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700461](https://openairdocs.org/sdr/CALA0700461.md): Stringer · corroded · Aug 28, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 26R CORRODED AT STA 986.5. A STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0700456](https://openairdocs.org/sdr/CALA0700456.md): Pressure Panel · cracked · Aug 25, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Bulkhead > INSPECTION FOUND A 1 INCH CRACK IN UPPER PRESSURE DECK IN MLG WHEEL WELL AT STA 664, RBL 38. REPAIRED IAW SRM 53-60-51, FIGURE 201. - [SDR CALA0700455](https://openairdocs.org/sdr/CALA0700455.md): Stringer · corroded · Aug 24, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND S27L CORRODED AT STA 957. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. - [SDR CALA0700454](https://openairdocs.org/sdr/CALA0700454.md): Fitting · corroded · Aug 24, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND SKIN CLIP CORRODED AT STA 986.5 BETWEEN S24R AND S25R. THE SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700453](https://openairdocs.org/sdr/CALA0700453.md): Web · cracked · Aug 24, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.75 INCH CRACK IN UPPER WEB FORWARD OF L-2 DOOR AT STA 947 AFT OF S11L. REPAIRED IAW SRM 51-10-02. - [SDR CALA0700451](https://openairdocs.org/sdr/CALA0700451.md): Stiffener · corroded · Aug 22, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED ON LOWER END, BOTH SIDES, STA 1016 FRAME ASSEMBLY. THE CORRODED SECTION OF APB CHANNEL STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C28106-1 AND EA 5310-04045, REV A, O - [SDR CALA0700450](https://openairdocs.org/sdr/CALA0700450.md): Gusset · cracked · Aug 21, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN RADIUS OF NOSE WHEEL WELL GUSSET AT AFT END OF NLG ACTUATOR SUPPORT FITTING, NWW STA 251, BL 0. THE GUSSET WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0700449](https://openairdocs.org/sdr/CALA0700449.md): Angle · cracked · Aug 21, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 291 JUST BELOW S11R. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00. - [SDR CALA0700446](https://openairdocs.org/sdr/CALA0700446.md): Fitting · cracked · Aug 20, 2007 · N14324 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.25 INCH CRACK IN STRINGER TIE AT STA 727E, S3R. THE STRINGER TIE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0700444](https://openairdocs.org/sdr/CALA0700444.md): Stringer · cracked · Aug 20, 2007 · N14324 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C + 5. REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03, FIGURE 201, REPAIR 1. - [SDR CALA0600537](https://openairdocs.org/sdr/CALA0600537.md): Oven · overheated · Dec 9, 2006 · N14324 · Boeing 7373T0 · Buffet/Galleys > THE FORWARD GALLEY 103 OVEN WAS UNUSUALLY HOT AND HAD AN ELECTRICAL ODOR PRIOR TO STARTING IT. THE CIRCUIT BREAKER WAS PULLED. THE OVEN WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. - [SDR CALA0600062](https://openairdocs.org/sdr/CALA0600062.md): Frame · corroded · Feb 14, 2006 · N14324 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND SURFACE CORROSION ON FRAME AT STA 794, S27R. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201. - [SDR CALA0600061](https://openairdocs.org/sdr/CALA0600061.md): Cargo Track · cracked · Feb 13, 2006 · N14324 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND A 2 INCH CRACK IN RT AFT CARGO TRACK BETWEEN STA 747-767, RBL 14. A NEW SECTION OF CARGO TRACK WAS SPLICED IN IAW SRM 53-00-53, FIGURE 201. - [SDR CALA0600060](https://openairdocs.org/sdr/CALA0600060.md): Cargo Track · damaged · Feb 13, 2006 · N14324 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND THE LT CARGO TRACK CORRODED AT LOCK DOWN FITTING AND APPROXIMATELY TWO INCHES OF THE I/B FLANGE BROKEN OFF AT STA 789 LBL 17. A NEW SECTION OF CARGO TRACK WAS SPLICED IN IAW SRM 53-00-53, FIGURE 201. - [SDR CALA0600059](https://openairdocs.org/sdr/CALA0600059.md): Skin · cracked · Feb 13, 2006 · N14324 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin > INSPECTION FOUND A.5 INCH CRACK AT FORWARD UPPER CORNER OF NR 2 ENGINE PYLON O/B ACCESS PANEL. AN INTERIM REPAIR HAD BEEN INSTALLED PREVIOUSLY AND THE ITEM WAS PLACED ON DIP. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204. - [SDR CALA0600044](https://openairdocs.org/sdr/CALA0600044.md): Structure · cracked · Feb 9, 2006 · N14324 · Boeing 7373T0 · Nacelle/Pylon, Main Frame > INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON I/B AFT HORSE COLLAR AT LOWER NUT PLATE. THE AFT HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0600043](https://openairdocs.org/sdr/CALA0600043.md): Shear Tie · corroded · Feb 9, 2006 · N14324 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND SKIN CLIP CORRODED AT STA 807, S28L. THE SKIN CLIP WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0500207](https://openairdocs.org/sdr/CALA0500207.md): Lock Actuator · malfunctioned · Jul 1, 2005 · N14324 · Boeing 7373T0 · Landing Gear Retraction/Extension System > MLG EXTENDED INSTANTLY WHEN GEAR HANDLE WAS PLACED DOWN ON APPROACH. NLG EXTENDED AFTER MLG EXTENDED DOWN AND LOCKED. MAINTENANCE UNABLE TO DUPLICATE FAULT. NLG LOCK ACTUATOR REMOVED AND REPLACED AS PRECAUTIONARY MEASURE IAW MM 32-33-31. OPERATIONAL CHECKS Next page: https://openairdocs.org/deregistered/N14324-2011-07-13/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 = 'N14324' AND deregistration_id = 'N14324-2011-07-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14324-2011-07-13/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.