# Service difficulty reports: N14325, cancelled Mar 21, 2013

A list on [N14325, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14325-2013-03-21.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 · 64 reports

- [SDR CALA0800843](https://openairdocs.org/sdr/CALA0800843.md): Wire · pinched · Aug 31, 2008 · N14325 · Boeing 7373T0 · Light System Wiring
  > EMERGENCY PATH LIGHTING AT ROW 24 FOUND WIRE PINCHED BETWEEN SEAT TRACK COVER AND TRACK. REMOVED AND REPLACED SEAT HARNESS EMERGENCY SEAT LIGHTS ROW 24. ALL LIGHTS OPS CHECK NORMAL.
- [SDR CALA0700596](https://openairdocs.org/sdr/CALA0700596.md): Service Panel · corroded · Oct 19, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION AND 3 POPPED RIVETS AT FORWARD EDGE OF LAV SERVICE PANEL, STA 986.5, RBL 25. A REPAIR WAS INSTALLED IAW ECRA 5331-01355.
- [SDR CALA0700586](https://openairdocs.org/sdr/CALA0700586.md): Skin · corroded · Oct 15, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FWD CARGO FUSELAGE SKIN HAS CORROSION AT STA 500C+18 LBL-17. SKIN REPAIR PER SRM 53-00-01 REPAIR 31 FIG 201.
- [SDR CALA0700584](https://openairdocs.org/sdr/CALA0700584.md): Stringer · corroded · Oct 15, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > AFT BAG BIN STA 867 STRINGER 26 RT HAS CORROSION. INSTALLED REPAIR PER SRM 53-00-03 FIG 201.
- [SDR CALA0700585](https://openairdocs.org/sdr/CALA0700585.md): Stringer · corroded · Oct 14, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STA 500C S26L CORROSION. INSTALLED REPAIR AT S26L STA 500C IN FWD CARGO IAW SRM 53-00-03 REPAIR 1.
- [SDR CALA0700581](https://openairdocs.org/sdr/CALA0700581.md): Frame · corroded · Oct 12, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Frame
  > STA 227 LBL 5 TO RBL 5 FRAME CORRODED. REPAIR ACCOMP PER ECRA 5311-01366.
- [SDR CALA0700580](https://openairdocs.org/sdr/CALA0700580.md): Bracket · cracked · Oct 12, 2007 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > ANGLE BRACKET CRACKED STA 348-351 STR 16L. REMOVED & REPLACED BRACKET PER ECRA 5311-01364.
- [SDR CALA0700579](https://openairdocs.org/sdr/CALA0700579.md): Bracket · cracked · Oct 12, 2007 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > ANGLE BRACKET CRACKED STA 351 STR 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01364.
- [SDR CALA0700578](https://openairdocs.org/sdr/CALA0700578.md): Angle · cracked · Oct 12, 2007 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED STA 348-350 STR 16L. REMOVED & REPLACED ANGLE PER ECRA 5311-01364.
- [SDR CALA0700577](https://openairdocs.org/sdr/CALA0700577.md): Skin · cracked · Oct 12, 2007 · N14325 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENG PYLON CRACKED AT ACCESS PANEL 5727. INSTALLED DOUBLER PER ECRA 5430-01230.
- [SDR 0700573](https://openairdocs.org/sdr/0700573.md): Door Frame · cracked · Oct 10, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Structure
  > C-1 DOOR CUTOUT FED FRAME CRACKED AT LWR STOP PAD MOUNT. REMOVED AND REPLACED PER SRM 51-40-02.
- [SDR 0700572](https://openairdocs.org/sdr/0700572.md): Stringer · corroded · Oct 10, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER 27L HAS CORROSION ON IT AT STA 500C+18 LBL. REPAIRED STRINGER PER SRM 53-00-03.
- [SDR 0700571](https://openairdocs.org/sdr/0700571.md): Frame · cracked · Oct 10, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Frame
  > FWD CARGO LWR FRAME HAS CORROSION ON FED SIDE AT STA 500D LBL 16 TO LBL 21. REPLACED FWD CARGO LWR FRAME PER SRM 53-00-07.
- [SDR 0700569](https://openairdocs.org/sdr/0700569.md): Door Frame · cracked · Oct 9, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Structure
  > C-2 DOOR CUTOUT FWD FRAME HAS CRACK. REPLACED FWD FRAME PER SRM 51-40-02 BOEING DRAWING 65-47959.
- [SDR 0700568](https://openairdocs.org/sdr/0700568.md): Frame · cracked · Oct 8, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Frame
  > UPPER FRAME SECTION STA 440 STR 17R-14R HAS CRACK AT FASTENER HOLE. REPLACED UPPER FRAME AT STA 440 IAW SRM 51-40-02.
- [SDR CALA0700562](https://openairdocs.org/sdr/CALA0700562.md): Shear Tie · cracked · Oct 3, 2007 · N14325 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND A.5 INCH CRACK IN LEFT FRAME SHEAR TIE AT STA 500D BETWEEN STRINGERS 10L AND 11L. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW BOEING DRAWING 69-73057 AND SRM 51-40-02.
- [SDR CALA0700488](https://openairdocs.org/sdr/CALA0700488.md): Charger · inoperative · Sep 2, 2007 · N14325 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND THE LAST 4 SEAT MOUNTED EMERGENCY LIGHTS OUT. THREE BATTERY CHARGERS IN THE AFT GALLEY WERE REMOVED AND REPLACED IAW AMM 33-51-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY.
- [SDR CALA0700272](https://openairdocs.org/sdr/CALA0700272.md): Skin · cracked · May 27, 2007 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D-727E, S22R-24R, AT AFT EMERGENCY LIGHT. THE SKIN WAS REPAIRED IAW ECRA 5330-03682.
- [SDR CALA0700260](https://openairdocs.org/sdr/CALA0700260.md): Sign · inoperative · May 24, 2007 · N14325 · Boeing 7373T0 · Emergency Lighting
  > THE RIGHT OVERWING ESCAPE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED IAW REFERENCE TO SWP 20-13-12 AND BRUCE WDM 33-50-00.
- [SDR CALA0600289](https://openairdocs.org/sdr/CALA0600289.md): Skin · cracked · Aug 1, 2006 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN BELOW EMERGENCY LIGHT AT STA 727D-727E, S22L TO S24L. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03560 AND A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 24 MONTHS OR 6,000 FLIGHT CYCLES WHICHEVER COMES F
- [SDR CALA0600092](https://openairdocs.org/sdr/CALA0600092.md): Skin · cracked · Mar 20, 2006 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3.375 INCH CRACK IN FUSELAGE SKIN AFT OF AFT CARGO DOOR AT STA 867, S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, DETAIL X, FIGURE 201, REPAIR 31, PAGE 231.
- [SDR CALA0500378](https://openairdocs.org/sdr/CALA0500378.md): Actuator · inoperative · Oct 28, 2005 · N14325 · Boeing 7373T0 · Landing Gear Actuator
  > WHEN THE GEAR HANDLE WAS PLACED DOWN ON FINAL APPROACH, THE NLG DID NOT EXTEND. THE CHECKLIST WAS RUN AND THE GEAR WAS EXTENDED MANUALLY WITH THREE GREEN LIGHTS RECEIVED. THE AIRCRAFT LANDED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR I
- [SDR CALA0500336](https://openairdocs.org/sdr/CALA0500336.md): Skin · cracked · Oct 7, 2005 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201.
- [SDR CALA0500183](https://openairdocs.org/sdr/CALA0500183.md): Door Frame · corroded · Jun 2, 2005 · N14325 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND SKIN BULGED AND RIVET HEADS STRESSED AT STA 360 AND S28L. THE E&E DOOR CUTOUT BEAM LOWER T-CHORD WAS FOUND CORRODED. THE T-CHORD WAS REPAIRED IAW ECRA 5311-01229.
- [SDR CALA0500180](https://openairdocs.org/sdr/CALA0500180.md): Skin · cracked · Jun 2, 2005 · N14325 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.75 INCH CRACK IN C-1 DOOR INNER SKIN AT CENTER LIGHTENING HOLES. A DOUBLER WAS INSTALLED IAW ECRA 5232-01063.
- [SDR CALA0500182](https://openairdocs.org/sdr/CALA0500182.md): Skin · cracked · May 27, 2005 · N14325 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01.
- [SDR CALA0500170](https://openairdocs.org/sdr/CALA0500170.md): Door Frame · corroded · May 26, 2005 · N14325 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CORRODED ON I/B SIDE AT STA 794, L26R TO L27R. THE CORRODED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-70-11.
- [SDR CALA0500162](https://openairdocs.org/sdr/CALA0500162.md): Door Frame · corroded · May 23, 2005 · N14325 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND THE R-2 AFT DOOR FRAME CORRODED AT STA 996, RBL 48. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0500161](https://openairdocs.org/sdr/CALA0500161.md): Gate · corroded · May 23, 2005 · N14325 · Boeing 7373T0 · Service Doors
  > INSPECTION FOUND THE R-2 DOOR LOWER GATE CORRODED ON INTERIOR AND EXTERIOR SURFACE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0500158](https://openairdocs.org/sdr/CALA0500158.md): Floorbeam · corroded · May 22, 2005 · N14325 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 48 TO RBL 48. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA0400060](https://openairdocs.org/sdr/CALA0400060.md): Skin · gouged · Jan 25, 2004 · N14325 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW SRM 51-70-16.
- [SDR CALA0400055](https://openairdocs.org/sdr/CALA0400055.md): Skin · cracked · Jan 23, 2004 · N14325 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 57-43-01.
- [SDR CALA0400050](https://openairdocs.org/sdr/CALA0400050.md): Floor Support · cracked · Jan 21, 2004 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 2 AND AT LBL 2. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300548](https://openairdocs.org/sdr/CALA0300548.md): Bulkhead · corroded · Sep 21, 2003 · N14325 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 1016 JUST LEFT OF BL 0. REPAIRED WEB IAW SRM 53-80-08 AND BOEING DRAWING 65C28106.
- [SDR CALA0100760](https://openairdocs.org/sdr/CALA0100760.md): Skin · dented · Aug 13, 2001 · N14325 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND THREE DENTS IN C-2 DOOR SKIN AT TEN INCHES FROM AFT SIDE AND FROM FIVE INCHES ABOVE PAINT LINE TO THIRTEEN INCHES ABOVE PAINT LINE. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA0100748](https://openairdocs.org/sdr/CALA0100748.md): Floor Support · corroded · Aug 8, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN CENTER FLOOR SUPPORT CORRODED AT STA 727D, RBL 18. A NEW SUPPORT AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-20-01.
- [SDR CALA0100732](https://openairdocs.org/sdr/CALA0100732.md): Splice · cracked · Aug 2, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRINGER 4L SPLICE CRACKED AT STA 907. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 203.
- [SDR CALA0100729](https://openairdocs.org/sdr/CALA0100729.md): Web · cracked · Jul 31, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1/4" CRACK IN STRESS WEB AT FLOORBEAM ATTACH POINT, STA 312, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100727](https://openairdocs.org/sdr/CALA0100727.md): Skin · gouged · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED AT FORWARD END ON DORSAL FIN MOUNT AREA. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100726](https://openairdocs.org/sdr/CALA0100726.md): Floor Support · corroded · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0100723](https://openairdocs.org/sdr/CALA0100723.md): Angle · corroded · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 944-991.5. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100722](https://openairdocs.org/sdr/CALA0100722.md): Fitting · corroded · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY MOUNTS CORRODED AT STA 946.5, LBL 14 AND RBL 8. THE GALLEY MOUNTS WERE REMOVED AND REPLACED IAW SRM 53-10-03.
- [SDR CALA0100721](https://openairdocs.org/sdr/CALA0100721.md): Fitting · corroded · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOOR AFT GIRT BAR LATCH MOUNT CORRODED. THE GIRT BAR LATCH MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-00.
- [SDR CALA0100720](https://openairdocs.org/sdr/CALA0100720.md): Angle · cracked · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1INCH CRACK IN WEB ANGLE AT STA 927-947.5, BL 0. THE WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100719](https://openairdocs.org/sdr/CALA0100719.md): Floor Support · corroded · Jul 30, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLES, STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100707](https://openairdocs.org/sdr/CALA0100707.md): Floor Support · cracked · Jul 27, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100706](https://openairdocs.org/sdr/CALA0100706.md): Floorbeam · corroded · Jul 27, 2001 · N14325 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 21 TO LBL 35. A CAP WAS INSTALLED ON BEAM IAW ECRA 5310-03851, REV A.
- [SDR CALA0100691](https://openairdocs.org/sdr/CALA0100691.md): Floorbeam · corroded · Jul 25, 2001 · N14325 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM SECTIONS CORRODED AT STA 967, RBL 17.5 AND AT STA 986.5, RBL 16 TO LBL 46. THE FLOORBEAM SECTIONS WERE REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0100681](https://openairdocs.org/sdr/CALA0100681.md): Web · corroded · Jul 25, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED AT STA 1020, LBL 23 AND AT STA 1016, RBL 7 - LBL 16. A NEW WEB WAS INSTALLED ON LEFT OF CENTER BBL 0 TO LBL 38 AND A NEW WEB WAS INSTALLED ON RIGHT OF CENTER BBL 0 TO RBL 38 IAW SRM 53-10-3.
- [SDR CALA0100680](https://openairdocs.org/sdr/CALA0100680.md): Support · corroded · Jul 25, 2001 · N14325 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT AFT LAV WALL SUPPORT CORRODED AT STA 1013, LBL 5 AND H STRAP CORRODED AT STA 1012, LBL 5, UNDER LAV WALL SUPPORT. THE SUPPORT AND STRAP WERE REMOVED AND REPLACED IAW SRM 53-10-3.

Next page: https://openairdocs.org/deregistered/N14325-2013-03-21/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 = 'N14325' AND deregistration_id = 'N14325-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14325-2013-03-21/reports

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