# Service difficulty reports: N14347, cancelled Mar 21, 2013

A list on [N14347, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14347-2013-03-21.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 · 80 reports

- [SDR CALA0700576](https://openairdocs.org/sdr/CALA0700576.md): Battery Pack · inoperative · Oct 14, 2007 · N14347 · Boeing 7373T0 · Emergency Lighting
  > EMERGENCY EXIT SIGN IN ADT GALLEY CENTER ASSOCIATED WITH CUSTOMER CALL LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT. FOUND PROBLEM PIN NR 2 ON PWR SUPP CONNECTOR. REPINNED AND REPLACED BATTERY PACK AND POWER SUPPLY.
- [SDR CALA0700563](https://openairdocs.org/sdr/CALA0700563.md): Skin · cracked · Oct 4, 2007 · N14347 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. THE CRACKED AREA OF SKIN WAS CUTOUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-00-01 AND 51-20-01.
- [SDR CALA0700603](https://openairdocs.org/sdr/CALA0700603.md): Skin · cracked · Oct 3, 2007 · N14347 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND CRACKS IN THE INNER SKIN OF THE AFT CARGO DOOR AT LIGHTENING HOLES ABOVE THE DOOR HANDLE CUTOUT. THE SKIN WAS REPAIRED IAW ECRA 5232-01092.
- [SDR CALA0700561](https://openairdocs.org/sdr/CALA0700561.md): Web · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AND STRINGER 12L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700560](https://openairdocs.org/sdr/CALA0700560.md): Stringer Clip · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 11L FORWARD SUPPORT CLIP. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700559](https://openairdocs.org/sdr/CALA0700559.md): Web · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 15L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700558](https://openairdocs.org/sdr/CALA0700558.md): Web · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700557](https://openairdocs.org/sdr/CALA0700557.md): Web · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 303.9 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362.
- [SDR CALA0700556](https://openairdocs.org/sdr/CALA0700556.md): Intercostal · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 TO 303.9 AT STRINGER 10L O/B SUPPORT ANGLE FOR WEB. WEB INTERCOSTALS WERE INSTALLED IAW ECRA 5311-01361.
- [SDR CALA0700555](https://openairdocs.org/sdr/CALA0700555.md): Stringer Clip · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 10L ANGLE CLIP. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01361.
- [SDR CALA0700552](https://openairdocs.org/sdr/CALA0700552.md): Support · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN L-1 DOOR AFT SIDE SUPPORT CLIP AT STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700551](https://openairdocs.org/sdr/CALA0700551.md): Support · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE FORWARD SUPPORT CLIP AT STA 360, S15L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700550](https://openairdocs.org/sdr/CALA0700550.md): Support · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STA 360 SUPPORT CLIP AT STRINGER 8L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363.
- [SDR CALA0700549](https://openairdocs.org/sdr/CALA0700549.md): Stringer · cracked · Oct 2, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STRINGER 15L AT STA 360. REPAIRED IAW ECRA 5311-01363.
- [SDR CALA0700548](https://openairdocs.org/sdr/CALA0700548.md): Skin · cracked · Oct 1, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D +3 BELOW STRINGER 23R. A DOUBLER WAS INSTALLED IAW ECRA 5330-03730 AND SRM 53-00-01, FIGURE 201, REPAIR 31.
- [SDR CALA0700545](https://openairdocs.org/sdr/CALA0700545.md): Pan · cracked · Oct 1, 2007 · N14347 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR FORWARD UPPER PAN AT PULLEY BRACKET ATTACH POINT. THE FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700544](https://openairdocs.org/sdr/CALA0700544.md): Door Frame · cracked · Oct 1, 2007 · N14347 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR AT FORWARD LOWER PAN PULLEY BRACKET. THE LOWER FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700547](https://openairdocs.org/sdr/CALA0700547.md): Shear Tie · corroded · Sep 30, 2007 · N14347 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 947 BETWEEN STRINGERS 23L AND 24L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700553](https://openairdocs.org/sdr/CALA0700553.md): Skin · delaminated · Sep 29, 2007 · N14347 · Boeing 7373T0 · Rudder, Plate/Skin
  > INSPECTION FOUND LT SIDE OF RUDDER T/E SKIN DELAMINATED AT STA 175.0. THE DELAMINATION MEASURED 0.4"L X 0.2"W. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5540-01243.
- [SDR CALA0700546](https://openairdocs.org/sdr/CALA0700546.md): Skin · cracked · Sep 27, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.8 INCH CRACK IN R-1 DOOR CUTOUT AFT LOWER CORNER OUTER SKIN, STA 328-344, S16R TO S17R. A REPAIR WAS INSTALLED IAW SRM 53-10-01, REPAIR 2, FIGURE 201.
- [SDR CALA0700542](https://openairdocs.org/sdr/CALA0700542.md): Pan · cracked · Sep 27, 2007 · N14347 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A.75 INCH CRACK IN L-1 DOOR PAN ON AFT SIDE AT 5TH DOOR STOP FROM BOTTOM. THE DOOR PAN WAS REPAIRED IAW ECRA 5210-01954.
- [SDR CALA0700540](https://openairdocs.org/sdr/CALA0700540.md): Skin · cracked · Sep 27, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN INTERIOR SKIN AT 4TH DOOR STOP FROM BOTTOM OF L-1 DOOR, STA 312, S13L. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210-01954.
- [SDR CALA0700538](https://openairdocs.org/sdr/CALA0700538.md): Keelbeam · corroded · Sep 25, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND O/B SPLICE CORRODED ON RIGHT KEEL BEAM FORWARD OF STA 727, RBL 7, IN AFT BAG BIN. THE SPLICE WAS REMOVED AND A NEW SPLICE ANGLE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0700537](https://openairdocs.org/sdr/CALA0700537.md): Skin · cracked · Sep 25, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK WITH CREASE IN SKIN AT STA 900 BETWEEN S23R AND S24R. THE DAMAGED AREA OF SKIN WAS REMOVED AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0700532](https://openairdocs.org/sdr/CALA0700532.md): Floorbeam · corroded · Sep 23, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AT FORWARD ENTRY STA 344, BL 0. REPAIRED FLOORBEAM IAW SRM 53-10-51.
- [SDR CALA0700528](https://openairdocs.org/sdr/CALA0700528.md): Stringer · corroded · Sep 22, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 22L CORRODED AT STA 1013. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700524](https://openairdocs.org/sdr/CALA0700524.md): Floorbeam · corroded · Sep 18, 2007 · N14347 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED NEAR FOWRD ENTRY DOOR AT STA 312, BL 0 TO LBL 10. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600290](https://openairdocs.org/sdr/CALA0600290.md): Stringer · corroded · Aug 2, 2006 · N14347 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 21L CORRODED ON UPPER FLANGE AT STA 897. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0600281](https://openairdocs.org/sdr/CALA0600281.md): Skin Panel · cracked · Jul 30, 2006 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2" CRACK IN BOTTOM SKIN PANEL BETWEEN KEEL BEAMS AT STA 685, S29L TO S29R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-60-12, REPAIR NR 2.
- [SDR CALA0600278](https://openairdocs.org/sdr/CALA0600278.md): Web · corroded · Jul 30, 2006 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB AT L-1 DOOR CORRODED FROM STA 312-350, LBL 62. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-10-15 AND 51-10-15.
- [SDR CALA0600275](https://openairdocs.org/sdr/CALA0600275.md): Seat Track · corroded · Jul 29, 2006 · N14347 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT I/B CABIN SEAT TRACK CORRODED AT STA 847, RBL 24. A REPAIR WAS INSTALLED IAW SRM 53-60-52.
- [SDR CALA0400147](https://openairdocs.org/sdr/CALA0400147.md): Skin · dented · Feb 21, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 400 BETWEEN S17L AND S18L. REPAIRED IAW ECRA 5331-01139.
- [SDR CALA0400145](https://openairdocs.org/sdr/CALA0400145.md): Skin · gouged · Feb 20, 2004 · N14347 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND NR 3 MID FLAP OUTBOARD L/E SKIN GOUGED JUST FORWARD OF EXHAUST GATE. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5752-01144.
- [SDR CALA0400144](https://openairdocs.org/sdr/CALA0400144.md): Stiffener · corroded · Feb 20, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD LOWER WEB AND STIFFENER CORRODED JUST AFT OF FS 1016, S23L. REPAIRED IAW ECRA 5311-01186.
- [SDR CALA0400142](https://openairdocs.org/sdr/CALA0400142.md): Skin · cracked · Feb 20, 2004 · N14347 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND 0.2 INCH CRACKS AT THREE FASTENERS IN NR 3 SLAT LOWER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.
- [SDR CALA0400141](https://openairdocs.org/sdr/CALA0400141.md): Support Fitting · cracked · Feb 20, 2004 · N14347 · Boeing 7373T0 · Nacelle/Pylon, Attach Fittings
  > INSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLON STA 279.5. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400135](https://openairdocs.org/sdr/CALA0400135.md): Attach Fitting · cracked · Feb 19, 2004 · N14347 · Boeing 7373T0 · Nacelle/Pylon, Attach Fittings
  > INSPECTION FOUND A.25 INCH CRACK IN NR 2 PYLON PANEL 5842 FORWARD ATTACH RAIL. THE ATTACH RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400132](https://openairdocs.org/sdr/CALA0400132.md): Skin · dented · Feb 17, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 875 BELOW S19R AFT OF C-2 DOOR. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 210.
- [SDR CALA0400131](https://openairdocs.org/sdr/CALA0400131.md): Attach Angle · cracked · Feb 17, 2004 · N14347 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND A 1.2 INCH CRACK IN NR 2 FLAP TRACK FAIRING ATTACH ANGLE. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0400126](https://openairdocs.org/sdr/CALA0400126.md): Attach Angle · corroded · Feb 16, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND ATTACH ANGLE FOR FLOOR PANEL AROUND GEAR DOWNLOCK VIEWER CORRODED AT AFT ATTACH ANGLE, BS 270, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01172.
- [SDR CALA0400124](https://openairdocs.org/sdr/CALA0400124.md): Web · cracked · Feb 16, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.25 INCH CRACK IN C-2 DOOR OPENING LOWER FORWARD SILL WEB AT STA 787. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400123](https://openairdocs.org/sdr/CALA0400123.md): Cargo Track · corroded · Feb 15, 2004 · N14347 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT BAGGAGE BIN TIE DOWN RAIL CORRODED AT FASTENER HOLES FROM STA 787-847. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-00-53.
- [SDR CALA0400115](https://openairdocs.org/sdr/CALA0400115.md): Angle · corroded · Feb 14, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE ATTACHED TO FORWARD WALL OF NOSE WHEEL WELL CORRODED AT STA 227, RBL 14. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400114](https://openairdocs.org/sdr/CALA0400114.md): Skin · dented · Feb 13, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 324 JUST BENEATH S20R. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.
- [SDR CALA0400112](https://openairdocs.org/sdr/CALA0400112.md): Hinge · cracked · Feb 13, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 1 INCH CRACK IN R-2 DOOR HINGE HOUSING AT LOWER SURFACE, STA 954, RBL 55, WL 230. THE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400111](https://openairdocs.org/sdr/CALA0400111.md): Floorbeam · corroded · Feb 13, 2004 · N14347 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO FLOORBEAMS UNDER CROSS STRAP CORRODED AT STA 767 + 6, RBL 8, RBL 3, AND LBL 3. REPAIRS WERE INSTALLED IAW ECRA 5320-01603.
- [SDR CALA0400107](https://openairdocs.org/sdr/CALA0400107.md): Intercostal · cracked · Feb 12, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 4 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL UNDER TRANSITION PANEL AT STA 928, RBL 26. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400106](https://openairdocs.org/sdr/CALA0400106.md): Web · corroded · Feb 12, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT WEB RT SIDE ADJACENT TO RUBBER MEMBRANE AT APB, STA 1016, RBL 0 TO RBL 48, CORRODED. A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0400098](https://openairdocs.org/sdr/CALA0400098.md): Web · corroded · Feb 9, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR WEB IN RT AFT LAV AREA CORRODED AT FS 1019, RBL 28. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400097](https://openairdocs.org/sdr/CALA0400097.md): Web · cracked · Feb 9, 2004 · N14347 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN SHEAR WEB PANEL FORWARD OF STA 578, S17L. THE WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-13. THE WEB WAS REINSTALLED IAW SRM 51-41-02.

Next page: https://openairdocs.org/deregistered/N14347-2013-03-21/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 = 'N14347' AND deregistration_id = 'N14347-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14347-2013-03-21/reports

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