# Service difficulty reports: N14358, cancelled Mar 21, 2013

A list on [N14358, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14358-2013-03-21.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 · 53 reports

- [SDR CALA0700388](https://openairdocs.org/sdr/CALA0700388.md): Fuse · inoperative · Aug 1, 2007 · N14358 · Boeing 737300 · Emergency Lighting
  > THE EMERGENCY LIGHT OVER COCKPIT DOOR WAS FOUND INOPERATIVE. THE F2 FUSE ON BATTERY PACK M1133 WAS REMOVED AND REPLACED IAW AMM 33-51-51.
- [SDR CALA0700233](https://openairdocs.org/sdr/CALA0700233.md): Fitting · cracked · May 4, 2007 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ECRA 5311-01320.
- [SDR CALA0700232](https://openairdocs.org/sdr/CALA0700232.md): Fitting · cracked · May 4, 2007 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ANGLE CLIP AT STA 351.20, S16L. REPAIRED IAW ECRA 5311-01320.
- [SDR CALA0700231](https://openairdocs.org/sdr/CALA0700231.md): Fitting · cracked · May 4, 2007 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ERCA 5311-01320.
- [SDR CALA0700226](https://openairdocs.org/sdr/CALA0700226.md): Keelbeam · cracked · May 2, 2007 · N14358 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND A 2" CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, PAGE 206, DETAIL NR 2.
- [SDR CALA0700224](https://openairdocs.org/sdr/CALA0700224.md): Frame · cracked · May 2, 2007 · N14358 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/4" CRACK IN THE FORWARD BAGGAGE BIN FORWARD FRAME AT THE FOURTH STOP PAD FROM TOP, STA 440, S13R TO S28R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700223](https://openairdocs.org/sdr/CALA0700223.md): Stop Fitting · cracked · May 1, 2007 · N14358 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A 1" CRACK IN L-1 DOOR TOP AFT STOP FITTING. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700056](https://openairdocs.org/sdr/CALA0700056.md): Skin · cracked · Feb 7, 2007 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.875 INCH CRACK IN FORWARD GALLEY DOOR CUTOUT LOWER CORNER FUSELAGE FRAME SKIN, STA 330, L17R. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5331-01286 AND A DIP WAS ISSUED TO ACCOMPLISH A REPEAT INSPECTION WITH AN INTERVAL NOT TO EXCEED 60,000
- [SDR CALA0500463](https://openairdocs.org/sdr/CALA0500463.md): Stiffener · cracked · Dec 22, 2005 · N14358 · Boeing 7373T0 · Wing Miscellaneous Structure
  > A 2 INCH CRACK WAS FOUND TO THE WING CENTER SECTION REAR SPAR AT STA 540, RBL 6.15 VERTICAL STIFFENER DURING A WALKAROUND INSPECTION. AN INTERIM REPAIR WAS INSTALLED PER EA 5714-01002, REV C, OP 8 AND ECRA 5714-01011. A DIP WAS ISSUED TO REINSPECT THE STIFFE
- [SDR CALA0500216](https://openairdocs.org/sdr/CALA0500216.md): Skin · cracked · Jul 11, 2005 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > WALK AROUND FOUND 3.5 IN CRACK IN STA 767 LOWER LAP SKIN, S25L. REPAIRED IAW SRM 53-00-01, FIGURE 229. DIP WAS ISSUED TO REINSPECT REPAIR EVERY 60,000 CYCLES.
- [SDR CALA0500111](https://openairdocs.org/sdr/CALA0500111.md): Tru · smoke · Apr 17, 2005 · N14358 · Boeing 7373T0 · Electrical Power System
  > DURING CRUISE, ELECTRICAL SMOKE IN COCKPIT AND CABIN. REPLACED NR 2 TRANSFORMER RECTIFIER PER AMM 24.
- [SDR CALA0500003](https://openairdocs.org/sdr/CALA0500003.md): Skin · cracked · Jan 8, 2005 · N14358 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A.75 INCH CRACK IN L-1 DOOR SKIN AT UPPER AFT INSPECTION HOLE. THE SKIN WAS REPAIRED IAW ECRA 5210-01812.
- [SDR CALA0400752](https://openairdocs.org/sdr/CALA0400752.md): Stringer · corroded · Dec 29, 2004 · N14358 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND RT APU TORQUE BOX CORRODED ON TOP STRINGER 14R AT AIR INLET CUTOUT, STA 1121-1156. THE UPPER APU TORQUE BOX STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400751](https://openairdocs.org/sdr/CALA0400751.md): Angle · corroded · Dec 19, 2004 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR THRESHOLD ZEE ANGLE CORRODED AT STA 907-1006, LBL 58. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400747](https://openairdocs.org/sdr/CALA0400747.md): Stringer · cracked · Dec 18, 2004 · N14358 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK AT FASTENER OF STRINGER 4L SPLICE, STA 907. REPLACED STRINGER SPLICE IAW SRM 51-10-02.
- [SDR CALA0400745](https://openairdocs.org/sdr/CALA0400745.md): Seat Track · corroded · Dec 17, 2004 · N14358 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK BELOW G-1 GALLEY CORRODED AT STA 290. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-45834.
- [SDR CALA0300674](https://openairdocs.org/sdr/CALA0300674.md): Stringer · corroded · Nov 21, 2003 · N14358 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGERS 26R AND 27R IN FORWARD CARGO AREA CORRODED AT STA 535-539. A STRINGER SECTION REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0300659](https://openairdocs.org/sdr/CALA0300659.md): Skin · lightning strike · Nov 21, 2003 · N14358 · Boeing 7373T0 · Rudder, Plate/Skin
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON RUDDER T/E APPROXIMATELY 30 INCHES BELOW STATIC WICK. REPAIRED IAW ECRA 5540-01171.
- [SDR CALA0300646](https://openairdocs.org/sdr/CALA0300646.md): Frame · cracked · Nov 14, 2003 · N14358 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME FITTING JUST BELOW CABIN FLOOR AT BOTTOM TWO FASTENERS, STA 616, W/ 200, LT SIDE. REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0300645](https://openairdocs.org/sdr/CALA0300645.md): Frame · cracked · Nov 14, 2003 · N14358 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FRAME INNER CHORD AT STA 616, WL 200, RT SIDE. THE INNER CHORD WAS REPAIRED IAW ECRA 5311-01158.
- [SDR CALA0300043](https://openairdocs.org/sdr/CALA0300043.md): Skin · cracked · Feb 6, 2003 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BETWEEN STA 727D +9.9 AND STA 727E JUST ABOVE S23L. THE SKIN WAS REPAIRED IAW ECRA 5330-03205.
- [SDR CALA0100663](https://openairdocs.org/sdr/CALA0100663.md): Stop Fitting · gouged · Jul 20, 2001 · N14358 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND C-2 DOOR FORWARD LOWER STOP FITTING GOUGED. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-2.
- [SDR CALA0100662](https://openairdocs.org/sdr/CALA0100662.md): Skin · cracked · Jul 20, 2001 · N14358 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.375" CRACK IN SKIN AT C-2 DOOR LIGHTENING HOLE ABOVE INTERIOR HANDLE. A DOUBLER WAS INSTALLED IAW ECRA 5230-01613.
- [SDR CALA0100661](https://openairdocs.org/sdr/CALA0100661.md): Frame · dented · Jul 20, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME DENTED AT STA 787, S25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1.
- [SDR CALA0100659](https://openairdocs.org/sdr/CALA0100659.md): Spar · cracked · Jul 17, 2001 · N14358 · Boeing 7373T0 · Wing Spar
  > INSPECTION FOUND A CRACK INDICATION IN NR 2 HOLE OF LT WING REAR SPAR UPPER CHORD AT GEAR BEAM CASTING ATTACH POINT. THE HOLE WAS REAMED AND THE CRACK WAS FOUND TO EXCEED 0.500 INCH MAX REAM LIMIT. THE REAR SPAR UPPER CHORD WAS REMOVED AND REPLACED FROM INBO
- [SDR CALA0100656](https://openairdocs.org/sdr/CALA0100656.md): Skin · dented · Jul 14, 2001 · N14358 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND C-2 DOOR EXTERNAL SKIN DENTED AT LOWER AFT CORNER. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0100654](https://openairdocs.org/sdr/CALA0100654.md): Skin · cracked · Jul 13, 2001 · N14358 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1.6" CRACK IN L/H HORIZONTAL STABILIZER LOWER SKIN ALONG REAR SPAR AREA AT STA 138.7. THE SKIN WAS REPAIRED IAW ECRA 5510-01586.
- [SDR CALA0100650](https://openairdocs.org/sdr/CALA0100650.md): Skin · dented · Jul 11, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 219, S23L, TEN INCHES ABOVE L/H SIDE OF FORWARD ACCESSORY DOOR AT EDGE OF BONDED DOUBLER. THE DENTED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100647](https://openairdocs.org/sdr/CALA0100647.md): Skin · dented · Jul 10, 2001 · N14358 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND TWO DENTS IN FORWARD CARGO DOOR EXTERNAL SKIN AT CENTER OF DOOR AND 14" FROM AFT EDGE OF DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA0100646](https://openairdocs.org/sdr/CALA0100646.md): Skin · cracked · Jul 10, 2001 · N14358 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN FORWARD OF AFT SPAR AT I/B ELEVATOR BALANCE PANEL. THE SKIN WAS REPAIRED IAW ECRA 5510-01585 AND SRM 55-10-01.
- [SDR CALA0100645](https://openairdocs.org/sdr/CALA0100645.md): Angle · corroded · Jul 10, 2001 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND COCKPIT FLOOR Z-ANGLE CORRODED AT BS 270, LBL 10 TO RBL 10. A REPAIR WAS INSTALLED IAW ECRA 5320-01683.
- [SDR CALA0100644](https://openairdocs.org/sdr/CALA0100644.md): Skin · dented · Jul 9, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 917, S19L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100640](https://openairdocs.org/sdr/CALA0100640.md): Skin · dented · Jul 8, 2001 · N14358 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND THREE DENTS ON C-1 DOOR EXTERNAL SKIN. THE DENTS WERE LOCATED 12 INCHES FROM FORWARD EDGE OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0100639](https://openairdocs.org/sdr/CALA0100639.md): Access Panel · cracked · Jul 8, 2001 · N14358 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL 5727. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0100637](https://openairdocs.org/sdr/CALA0100637.md): Skin · damaged · Jul 6, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN "DAMAGED" AT STA 807, S28L TO S26R. THE DAMAGE WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-00-01.
- [SDR CALA0100602](https://openairdocs.org/sdr/CALA0100602.md): Floorbeam · corroded · Jun 25, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, BL 0 TO LBL 59. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0100590](https://openairdocs.org/sdr/CALA0100590.md): Floorbeam · corroded · Jun 23, 2001 · N14358 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 49. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9901039](https://openairdocs.org/sdr/CALA9901039.md): Floorbeam · corroded · Jul 22, 1999 · N14358 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD LOWER SURFACE FORWARD AND AFT OF STA 986.5, RBL 25-35. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA9900065](https://openairdocs.org/sdr/CALA9900065.md): Wire · pinched · Jan 17, 1999 · N14358 · Boeing 7373T0 · Light System Wiring
  > ROW 7 TO 12 EMERGENCY LIGHTS INOP. FOUND WIRE PINCHED IN SEAT TRACK AT ROW 12. REPAIRED WIRE, OPS CHECK GOOD.
- [SDR CALA9701003](https://openairdocs.org/sdr/CALA9701003.md): Floorbeam · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED UNDER LEFT AFT LAV AT STA 1016. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-00-51, PAGES 207 TO 211.
- [SDR CALA9701002](https://openairdocs.org/sdr/CALA9701002.md): Angle · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE AT L-2 DOOR LOWER JAMB CORRODED FROM STA 947.5 TO 986.5. THE ANGLE WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9701001](https://openairdocs.org/sdr/CALA9701001.md): Angle · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE AT LOWER R-2 DOOR JAMB CORRODED FROM STA 947.5 TO 1006. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-30-11 AND 51-40-02.
- [SDR CALA9701000](https://openairdocs.org/sdr/CALA9701000.md): Web · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED UNDER RIGHT LAV FROM STA 1016 TO 1040. THE WEB WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9700999](https://openairdocs.org/sdr/CALA9700999.md): Floorbeam · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03450.
- [SDR CALA9700998](https://openairdocs.org/sdr/CALA9700998.md): Stringer · cracked · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECCTION FOUND A.5 INCH CRACK IN STRINGER 16L AT STA 500C. THE CRACKED AREA OF STRINGER WAS REMOVED, REPAIR DOUBLER, FILLER, AND CHANNEL WERE FABRICATED AND INSTALLED IAW ECRA 5330-02541.
- [SDR CALA9700997](https://openairdocs.org/sdr/CALA9700997.md): Frame · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME WEB AND CHORD CORRODED AT STA 1121R. THE WEB AND CHORD WERE REPLACED IAW SRM 51-10-02.
- [SDR CALA9700996](https://openairdocs.org/sdr/CALA9700996.md): Angle · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT STA 1121R, WL 240. THE ANGLE WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA9700991](https://openairdocs.org/sdr/CALA9700991.md): Web · corroded · Jun 9, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB UNDER LEFT AFT LAV CORRODED AT STA 1016 TO 1040. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9700995](https://openairdocs.org/sdr/CALA9700995.md): Angle · corroded · Jun 8, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 276R TO 300R. THE FLOOR ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA9700994](https://openairdocs.org/sdr/CALA9700994.md): Support · corroded · Jun 8, 1997 · N14358 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 228L TO 312L, LBL 26.75. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.

Next page: https://openairdocs.org/deregistered/N14358-2013-03-21/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 = 'N14358' AND deregistration_id = 'N14358-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14358-2013-03-21/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.