# Service difficulty reports: N14346, cancelled Mar 21, 2013

A list on [N14346, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14346-2013-03-21.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 · 51 reports

- [SDR CALA0800303](https://openairdocs.org/sdr/CALA0800303.md): Skin · misrepaired · Apr 4, 2008 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > SKIN REPAIR AT STA 420 TO 440 BETWEEN STR 16L TO 20L MISSING FIELD FASTENERS. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED NEW REPAIR IN REF TO SRM 53-00-01, REPAIR 31. PLACED ON DIP PER ECRA 5331-01399 ACCOMPLISH PERMANENT REPAIR BEFORE 60,000 FLT CYC
- [SDR CALA0700340](https://openairdocs.org/sdr/CALA0700340.md): Skin · cracked · Jul 6, 2007 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN SKIN AT SCREW HOLE, STA 380, S28L TO 28R. REPAIRED IAW ECRA 5330-02894.
- [SDR CALA0600133](https://openairdocs.org/sdr/CALA0600133.md): Floorbeam · corroded · Apr 14, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM 967 LBL 5. INSTALLED REPAIR STRAP PER SRM 53-00-51, FIG 201.
- [SDR CALA0600118](https://openairdocs.org/sdr/CALA0600118.md): Stringer · corroded · Apr 10, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25R CORRODED ON SIDE FLANGE AT STA 986 IN AFT BILGE AREA. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 201-207, FIGURE 201, DETAIL VII.
- [SDR CALA0600108](https://openairdocs.org/sdr/CALA0600108.md): Skin · cracked · Apr 8, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.125 INCH CRACK AT FASTENER IN FUSELAGE SKIN JUST AFT OF STA 390, S21R. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5331-01229 AND A DIP WAS INITIATED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER OCCURS
- [SDR CALA0600103](https://openairdocs.org/sdr/CALA0600103.md): Stringer · cracked · Apr 3, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK AT FASTENER HOLE IN STRINGER 15R, STA 500+10. A REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0600101](https://openairdocs.org/sdr/CALA0600101.md): Stringer · cracked · Apr 2, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND.25 INCH CRACKS (4 EACH) AROUND FASTENER HOLES IN STRINGER AT STA 428-486, S16R. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-53, FIGURE 201.
- [SDR CALA0600099](https://openairdocs.org/sdr/CALA0600099.md): Keelbeam · corroded · Mar 29, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LT KEEL BEAM CORRODED IN LT WHEEL WELL AT STA 727, S28L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 101, SHEET 4-13.
- [SDR CALA0600111](https://openairdocs.org/sdr/CALA0600111.md): Frame · corroded · Mar 27, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND CORROSION ON LOWER FRAME OF STA 227.8 BULKHEAD, LBL 6 TO RBL 6. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW ECRA 5311-01252 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER COMES FIRST.
- [SDR CALA0600097](https://openairdocs.org/sdr/CALA0600097.md): Floorbeam · corroded · Mar 27, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FORWARD CARGO FLOORBEAM FORWARD FACE CORRODED AT STA 500D, LBL 14. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201.
- [SDR CALA0600096](https://openairdocs.org/sdr/CALA0600096.md): Strip · corroded · Mar 26, 2006 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO FLOOR PANEL MOUNT STRIP UPPER SURFACE CORRODED AT STA 847, RBL 45. THE FLOOR PANEL MOUNT STRIP WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0600115](https://openairdocs.org/sdr/CALA0600115.md): Support Fitting · corroded · Mar 25, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND THE R-1 DOOR FUSELAGE TORQUE TUBE UPPER SUPPORT FITTING CORRODED AT STA 294.5, S10R TO S14R. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW ECRA 5341-01004.
- [SDR CALA0600112](https://openairdocs.org/sdr/CALA0600112.md): Frame · cracked · Mar 25, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1.5 INCH CRACK IN ABB DOOR CUTOUT FORWARD FRAME AT STA 794.3 ALONG UPPER THREE STOP PAD MOUNTS. THE FRAME WAS REPLACED IAW SRM 51-41-02.
- [SDR CALA0600091](https://openairdocs.org/sdr/CALA0600091.md): Floorbeam · corroded · Mar 20, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, RBL 12. THE CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA0600090](https://openairdocs.org/sdr/CALA0600090.md): Floorbeam · corroded · Mar 19, 2006 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 344, LBL 9. A DOUBLER WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0600149](https://openairdocs.org/sdr/CALA0600149.md): Angle · cracked · Mar 15, 2006 · N14346 · Boeing 7373T0 · Service Doors
  > INSPECTION FOUND A.75 INCH CRACK IN THE R1 DOOR UPPER/FORWARD TORQUE BOX ATTACH INTERCOSTAL MOUNT ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65-45871.
- [SDR CALA0400595](https://openairdocs.org/sdr/CALA0400595.md): Channel · corroded · Aug 11, 2004 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND HAT CHANNEL FOR VHF ANTENNA CORRODED AT STA 727D, BL 0. A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0400578](https://openairdocs.org/sdr/CALA0400578.md): Bolt · sheared · Jul 16, 2004 · N14346 · Boeing 7373T0 · Elevator Structure
  > THE LEFT O/B ELEVATOR HINGE BOLT WAS FOUND MISSING AND SHEARED OFF DURING A WALKAROUND INSPECTION. THE BOLT OR HINGE HARDWARE WAS JAMMED BETWEEN THE STABILIZER AND ELEVATOR RESULTING IN ADDITIONAL DAMAGE. THE LEFT HORIZONTAL STABILIZER, LEFT ELEVATOR, AND EL
- [SDR CALA0300470](https://openairdocs.org/sdr/CALA0300470.md): Skin · bird strike · Aug 17, 2003 · N14346 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN AND RIB AT STA 86.66 DAMAGED DUE TO A BIRD STRIKE.
- [SDR CALA0200193](https://openairdocs.org/sdr/CALA0200193.md): Trunnion · corroded · Apr 9, 2002 · N14346 · Boeing 7373T0 · Nose/Tail Landing Gear Attach Section
  > INSPECTION FOUND NLG LT AND RT MAIN TRUNNION SUPPORT FITTING BEARING SEATS CORRODED. THE CORROSION WAS REMOVED, THE AREAS WERE REWORKED AND BUSHINGS WERE INSTALLED AT EACH LOCATION IAW ECRA 5343-01006 REV A.
- [SDR CALA0200192](https://openairdocs.org/sdr/CALA0200192.md): Spar · cracked · Apr 9, 2002 · N14346 · Boeing 7373T0 · Wing Spar
  > INSPECTION FOUND A.125 INCH CRACK IN RT WING REAR SPAR UPPER CHORD AT MLG BEAM ATTACH FITTING. THE CRACKED AREA WAS REMOVED AND A FREEZE PLUG WAS INSTALLED.
- [SDR CALA0200190](https://openairdocs.org/sdr/CALA0200190.md): Skin · cracked · Apr 8, 2002 · N14346 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1/4" CRACK IN UPPER PYLON SKIN PANEL #5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV. B.
- [SDR CALA0200169](https://openairdocs.org/sdr/CALA0200169.md): Fitting · corroded · Apr 3, 2002 · N14346 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND R/H MLG FITTING AFT SPAR CASTING HOLE AT FALSE SPAR O/B ATTACH PIN CORRODED. THE CORROSION WAS REMOVED IAW ECRA 5711-01038.
- [SDR CALA0200161](https://openairdocs.org/sdr/CALA0200161.md): Skin · dented · Mar 29, 2002 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 887, S15R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.
- [SDR CALA0200160](https://openairdocs.org/sdr/CALA0200160.md): Bushing · corroded · Mar 29, 2002 · N14346 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND THE L/H AND R/H MLG(WALKING BEAM) O/B ATTACH FITTING BUSHINGS CORRODED. THE CORROSION WAS REMOVED AND A NEW BUSHING WAS INSTALLED AT EACH LOCATION IAW ECRA 5741-01017.
- [SDR CALA0200159](https://openairdocs.org/sdr/CALA0200159.md): Stringer · corroded · Mar 28, 2002 · N14346 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND APU COMPARTMENT STRINGER CORRODED AT CUTOUT JUST BELOW APU INLET. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0200157](https://openairdocs.org/sdr/CALA0200157.md): Web · corroded · Mar 28, 2002 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN WEB AT DOORWAY CORRODED, STA 796-847. A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0200150](https://openairdocs.org/sdr/CALA0200150.md): Seat Track · cracked · Mar 25, 2002 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 2" CRACK AT HI-LOCK HOLE IN R/H O/B SEAT TRACK, STA 727B. THE CRACKED AREA WAS REMOVED AND A REPAIR STRAP AND FILLER WERE INSTALLED IAW ECRA 5311-01117.
- [SDR CALA0200140](https://openairdocs.org/sdr/CALA0200140.md): Seat Track · corroded · Mar 21, 2002 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 887-947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200139](https://openairdocs.org/sdr/CALA0200139.md): Skin · cracked · Mar 20, 2002 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3" CRACK IN UPPER FUSELAGE SKIN AT STA 178, WL 243, LBL 1.5. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SOEING DRAWING #65-45800 AND SRM 51-40-02.
- [SDR CALA0200135](https://openairdocs.org/sdr/CALA0200135.md): Strap · corroded · Mar 17, 2002 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT LAV ANGLE STRAP CORRODED BETWEEN STA 986 AND 1006. A NEW ANGLE STRAP WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0200134](https://openairdocs.org/sdr/CALA0200134.md): Fitting · corroded · Mar 17, 2002 · N14346 · Boeing 7373T0 · Horizontal Stabilizer, Attach Fittings
  > INSPECTION FOUND TWO R/H FORWARD HORIZONTAL STABILIZER ATTACH FITTINGS HAD LOWER AFT AND FORWARD BUSHINGS CORRODED BETWEEN BUSHING AND LUG. AN OVERSIZED BUSHING WAS INSTALLED AT EACH LOCATION IAW CMM 55-10-10.
- [SDR CALA0200133](https://openairdocs.org/sdr/CALA0200133.md): Stringer · cracked · Mar 16, 2002 · N14346 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/8" CRACK IN STRINGER 16L AND 16R AT FASTENER AREA FWD OF LIGHT ASSEMBLY STA 500C AFT. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0200131](https://openairdocs.org/sdr/CALA0200131.md): Skin · cracked · Mar 15, 2002 · N14346 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.125" CRACK IN WHEEL WELL CENTER KEEL EXTERIOR SKIN PANEL. THE CRACK WAS LOCATED ALONG R/H SIDE BETWEEN STA 685 AND 706. A DOUBLER WAS INSTALLED AND PAINTED IAW SRM 53-60-12, FIGURE 202.
- [SDR CALA0001059](https://openairdocs.org/sdr/CALA0001059.md): Keelbeam · worn · Jul 12, 2000 · N14346 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND THE RIGHT O/B FLANGE OF THE KEEL BEAM WORN JUST FORWARD OF BS 727. THE WEAR WAS CAUSED BY LOOSE FAIRING ATTACH FASTENERS. THE WORN AREAS WERE SPOTFACED. A REPAIR STRAP AND FILLERS WERE INSTALLED IAW ECRA 5310-04031.
- [SDR CALA0000615](https://openairdocs.org/sdr/CALA0000615.md): Arm · worn · Apr 27, 2000 · N14346 · Boeing 7373T0 · Passenger/Crew Doors
  > L2 DOOR HARD TO OPEN AND CLOSE BOTH INTERNALLY AND EXTERNALLY. REPLACED SNUBBER AND GUIDE ARM PER MM 52-13-31.
- [SDR CALA9801181](https://openairdocs.org/sdr/CALA9801181.md): Angle · corroded · Jun 28, 1998 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT R-1 DOOR, STA 290 TO 294 AND 344. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00.
- [SDR CALA9801180](https://openairdocs.org/sdr/CALA9801180.md): Floorbeam · corroded · Jun 26, 1998 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 2. REPAIRED IAW SRM 53-10-51, FIGURE 205.
- [SDR CALA9801179](https://openairdocs.org/sdr/CALA9801179.md): Seat Track · corroded · Jun 26, 1998 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 328 TO 344. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-00-52.
- [SDR CALA9801178](https://openairdocs.org/sdr/CALA9801178.md): Floorbeam · corroded · Jun 26, 1998 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF FLOORBEAM AT STA 967, RBL 40 TO 50. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 202.
- [SDR CALA9801170](https://openairdocs.org/sdr/CALA9801170.md): Floorbeam · corroded · Jun 26, 1998 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 986 FROM RBL 0 TO RBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03450.
- [SDR CALA9801169](https://openairdocs.org/sdr/CALA9801169.md): Angle · corroded · Jun 26, 1998 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF R-2 DOOR THRESHOLD Z-ANGLE FROM STA 967 TO 996, LBL 48, WL 208.1. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9801168](https://openairdocs.org/sdr/CALA9801168.md): Angle · corroded · Jun 25, 1998 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE CORRODED AT FORWARD ENTRY, LT SIDE, STA 312-340. A NEW Z-ANGLE WAS INSTALLED IAW SRM 53-10-2.
- [SDR CALA9801167](https://openairdocs.org/sdr/CALA9801167.md): Floorbeam · corroded · Jun 25, 1998 · N14346 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT FORWARD ENTRY, STA 312, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9801166](https://openairdocs.org/sdr/CALA9801166.md): Angle · corroded · Jun 25, 1998 · N14346 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT Z-ANGLE CORRODED AT STA 967, LBL 46, WL 208. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9801165](https://openairdocs.org/sdr/CALA9801165.md): Seat Track · corroded · Jun 25, 1998 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-937, RBL 24. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA9801164](https://openairdocs.org/sdr/CALA9801164.md): Seat Track · corroded · Jun 24, 1998 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 917, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA9801159](https://openairdocs.org/sdr/CALA9801159.md): Seat Track · corroded · Jun 23, 1998 · N14346 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND OUTBOARD SEAT TRACK CORRODED AT STA 927, RBL 48, WL 208.1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, FIGURE 204, SHEET 1-4 AND SRM 51-30-00.
- [SDR CAL960595](https://openairdocs.org/sdr/CAL960595.md): Light · loose wire · May 13, 1996 · N14346 · Boeing 7373T0 · Emergency Lighting
  > IAH - FLT 1677 - INSPECTION FOUND EMERGENCY PATH LIGHTING AT FORWARD FIRST CLASS CLOSET INOPERATIVE. MAINTENANCE RECONNECTED LOOSE WIRE ON CONNECTOR TO LIGHT ASSEMBLY. (X)
- [SDR CAL960327](https://openairdocs.org/sdr/CAL960327.md): Uplock Sensor · out of adjust · Mar 17, 1996 · N14346 · Boeing 7373T0 · Landing Gear Position and Warning
  > IAH - FLT 8954 - THE LT MLG RED LIGHT CAME BACK ON AFTER GEAR RETRACTION. CYCLING THE GEAR WAS NO HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG UPLOCK SENSOR TARGET OUT OF RIG. THE SENSOR/TARGET WAS S

Next page: https://openairdocs.org/deregistered/N14346-2013-03-21/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 = 'N14346' AND deregistration_id = 'N14346-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14346-2013-03-21/reports

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