# Service difficulty reports: N14342, cancelled Jul 21, 2009

A list on [N14342, cancelled Jul 21, 2009](https://openairdocs.org/deregistered/N14342-2009-07-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA0800414](https://openairdocs.org/sdr/CALA0800414.md): Channel · cracked · May 6, 2008 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > DURING REMOVAL AND REPLACEMENT OF THE NR 3 VHF ANTENNA TWO CRACKS WERE FOUND ON THE ANTENNA MOUNTING CHANNEL LOCATED IN THE AFT CARGO COMPARTMENT. CHANNEL AT STATION 727C TO 727D BETWEEN S27L TO S27R FOUND WITH TWO CRACKS WAS REMOVED AND REPLACED WITH NEW CHA
- [SDR CALA0700321](https://openairdocs.org/sdr/CALA0700321.md): Wire · broken · Jun 24, 2007 · N14342 · Boeing 7373T0 · Fire Detection
  > THE APU FIRE LIGHT ILLUMINATED ACCOMPANIED BY ACTIVATION OF THE FIRE BELL WHILE AT CRUISE ENROUTE FROM SFO TO IAH. THE APU DETECTOR INOP LIGHT ALSO ILLUMINATED. THE APU FIRE EXTINGUISHING BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SAT WHERE IT LAND
- [SDR CALA0600195](https://openairdocs.org/sdr/CALA0600195.md): Floorbeam · cracked · Jun 1, 2006 · N14342 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 0.7 INCH CRACK IN FORWARD CABIN FLOORBEAM WEB AT STA 328, LBL 46. THE WEB WAS REPAIRED IAW ECRA 5321-01367.
- [SDR CALA0600178](https://openairdocs.org/sdr/CALA0600178.md): Stringer · corroded · May 21, 2006 · N14342 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600177](https://openairdocs.org/sdr/CALA0600177.md): Shear Tie · corroded · May 21, 2006 · N14342 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S26R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600173](https://openairdocs.org/sdr/CALA0600173.md): Floorbeam · corroded · May 20, 2006 · N14342 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED I/B OF LT Z-ANGLE AT STA 986.5, LBL 26-52. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03851.
- [SDR CALA0600169](https://openairdocs.org/sdr/CALA0600169.md): Seat Track · corroded · May 18, 2006 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CABIN INTERIOR RIGHT I/B FLOOR SEAT TRACK CORRODED FROM STA 907-936, RBL 15. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52.
- [SDR CALA0600243](https://openairdocs.org/sdr/CALA0600243.md): Stringer · corroded · May 17, 2006 · N14342 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND E&E COMPARTMENT STA 312-323.7 STRINGER 28R CORRODED ON BOTH SIDES AND ALONG TOP LEFT UPPER EDGE. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300424](https://openairdocs.org/sdr/CALA0300424.md): Floorbeam · corroded · Jul 20, 2003 · N14342 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED UNDER LAV-A AT STA 294.5, LBL 24.67. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-51 AND ECRA 5311-01159.
- [SDR CALA0300398](https://openairdocs.org/sdr/CALA0300398.md): Pressure Panel · cracked · Jul 19, 2003 · N14342 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE DECK AT BS 663, LBL 31. THE CRACKED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-60-51.
- [SDR CALA0300396](https://openairdocs.org/sdr/CALA0300396.md): Floorbeam · corroded · Jul 19, 2003 · N14342 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT L-2 DOOR AFT GIRT BAR ATTACH POINT, STA 986. A REPAIR WAS ACCOMPLISHED ON UPPER CHORD OF FLOORBEAM IAW ECRA 5310-03851.
- [SDR CALA0300045](https://openairdocs.org/sdr/CALA0300045.md): Solenoid · inoperative · Feb 12, 2003 · N14342 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE CREW WAS UNABLE TO RAISE THE GEAR HANDLE PAST THE OFF POSITION AFTER TAKEOFF. THE GEAR OVERRIDE TRIGGER WAS USED TO RAISE GEAR. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER LOCK SOLENOID IAW MM 32-31-31-024-001, PAGE 401-404.
- [SDR CALA2000257](https://openairdocs.org/sdr/CALA2000257.md): Angle · corroded · May 3, 2002 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CORROSION ON L-ANGLE AT STA 500D, STRINGER 26L F/B/B. REMOVED AND REPLACED ANGLE REF SRM 51-70-12.
- [SDR CALA0200255](https://openairdocs.org/sdr/CALA0200255.md): Fitting · corroded · May 2, 2002 · N14342 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > R/H MLG FITTING INNER BUSHING CORROSION ON THE BOSS. REPAIRED FITTING HOLE AND INSTALLED OVER SIZE BUSHING PER ECRA 5711-01039.
- [SDR CALA0200254](https://openairdocs.org/sdr/CALA0200254.md): Skin · cracked · Apr 29, 2002 · N14342 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0200250](https://openairdocs.org/sdr/CALA0200250.md): Skin · cracked · Apr 29, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT TWO SCREW HOLES AFT OF C/L OF AIRCRAFT STA 380. A DOUBLER WAS INSTALLED IAW ECRA 5330-02849.
- [SDR CALA0200249](https://openairdocs.org/sdr/CALA0200249.md): Angle · chafed · Apr 27, 2002 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER SURFACE OF FUSELAGE KEEL BEAM RIGHT AND LEFT LOWER ANGLES HAD WASHERS WEARING INTO THE ANGLES AT STA 710-727. THE KEEL BEAM ANGLES WERE REPLACED IAW ECRA 5310-03740.
- [SDR CALA0200246](https://openairdocs.org/sdr/CALA0200246.md): Spar · cracked · Apr 26, 2002 · N14342 · Boeing 7373T0 · Wing Spar
  > INSPECTION FOUND THE RT AND LT WING REAR SPARS HAD A 0.050 INCH CRACK INDICATION AT HOLE AT MLG BEAM ATTACH FITTINGS.
- [SDR CALA0200244](https://openairdocs.org/sdr/CALA0200244.md): Cargo Track · corroded · Apr 26, 2002 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT TIE DOWN RAIL CORRODED ON UPPER SIDE FRONT IN AFT BAGGAGE BIN AT STA 807-840. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, PAGE 204-205.
- [SDR CALA0200241](https://openairdocs.org/sdr/CALA0200241.md): Stringer · corroded · Apr 25, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 22L CORRODED AT STA 867-887. A REPAIR STRINGER WAS INSTALLED IAW SRM 53-00-03, PAGE 201 AND 204.
- [SDR CALA0200240](https://openairdocs.org/sdr/CALA0200240.md): Stringer · cracked · Apr 25, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN STRINGER 16R AND 16L AT STA 500C + 5". THE CRACKED AREA OF EACH STRINGER WAS REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-03.
- [SDR CALA0200236](https://openairdocs.org/sdr/CALA0200236.md): Beltframe · cracked · Apr 23, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/4" CRACK IN L/H BELTFRAME ANGLE AT STA 616 JUST ABOVE CENTER TANK. THE CRACKED AREA WAS TRIMMED OUT. AN ANGLE DOUBLER AND FILLER WERE INSTALLED ON FRAME IAW ECRA 5311-01121.
- [SDR CALA0200235](https://openairdocs.org/sdr/CALA0200235.md): Skin · cracked · Apr 22, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3/4" CRACK IN FUSELAGE SKIN FORWARD OF L-2 DOOR FUSELAGE TORQUE TUBE ACCESS PANEL AT STA 947 BETWEEN STRINGER 10 AND 11L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-60-01.
- [SDR CALA0200234](https://openairdocs.org/sdr/CALA0200234.md): Seat Track · corroded · Apr 22, 2002 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK HAD PITTING CORROSION AT STA 727-767. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0200227](https://openairdocs.org/sdr/CALA0200227.md): Seat Track · corroded · Apr 21, 2002 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H SEAT TRACK HAD PITTING CORROSION AT STA 847-907. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA0200215](https://openairdocs.org/sdr/CALA0200215.md): Stringer · corroded · Apr 17, 2002 · N14342 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND CENTER STRINGER ON LOWER FLOOR SIDE OF AFT PRESSURE BULKHEAD AT STA 1016 CORRODED ON LOWER END. THE STRINGER WAS REPAIRED IAW SRM 51-70-11, PAGE 1-6.
- [SDR CALA0200209](https://openairdocs.org/sdr/CALA0200209.md): Fitting · corroded · Apr 16, 2002 · N14342 · Boeing 7373T0 · Horizontal Stabilizer, Attach Fittings
  > INSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD UPPER LUG CORRODED. THE CORROSION WAS REMOVED FROM LUG IAW SRM 55-10-10.
- [SDR CALA0200208](https://openairdocs.org/sdr/CALA0200208.md): Splice · cracked · Apr 16, 2002 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN STRINGER SPLICE AT STA 907, S4L. A NEW SPLICE WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0200197](https://openairdocs.org/sdr/CALA0200197.md): Web · cracked · Apr 12, 2002 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 4" CRACK IN WEB AT STA 303.9, STRINGER 4L. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0200196](https://openairdocs.org/sdr/CALA0200196.md): Seat Track · corroded · Apr 11, 2002 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52.
- [SDR CALA0000895](https://openairdocs.org/sdr/CALA0000895.md): Skin · cracked · Jun 13, 2000 · N14342 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND INNER SKIN OF C-1 DOOR CRACKED IN THREE PLACES AT LIGHTENING HOLES. THE CRACKS WERE 1 INCH LONG. A REPAIR WAS INSTALLED IAW ECRA 5230-01555.
- [SDR CALA0000851](https://openairdocs.org/sdr/CALA0000851.md): Skin · cracked · Jun 8, 2000 · N14342 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND TWO 1 INCH CRACKS IN NR 1 ENGINE PYLON I/B SIDE ACCESS DOOR PANEL NR 5724L CUTOUT. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.
- [SDR CALA0000818](https://openairdocs.org/sdr/CALA0000818.md): Skin · cracked · Jun 3, 2000 · N14342 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT LOWER SKIN AT ACTUATOR AREA. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02586.
- [SDR CALA9900850](https://openairdocs.org/sdr/CALA9900850.md): Relay · inop · Jul 22, 1999 · N14342 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE GEAR HANDLE TRIGGER HAD TO BE PULLED TO RAISE LANDING GEAR PAST THE OFF POSITION AFTER TAKEOFF. THE FLIGHT CONTINUED TO LAX WHERE IT LANDED WITHOUT INCIDENT. THE FAULT WAS DUPLICATED ON THE GROUND. THE LANDING GEAR LEVER REMAINED LOCKED. MAINTENANCE FO
- [SDR CALA9801418](https://openairdocs.org/sdr/CALA9801418.md): Sensor · inoperative · Aug 9, 1998 · N14342 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR WOULD NOT RETRACT; THE LEVER WOULD NOT GO ABOVE THE OFF POSITION AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AIR SAFETY SENSOR AND PERFORMED ADJUSTMENT AND T
- [SDR CALA9801384](https://openairdocs.org/sdr/CALA9801384.md): Logic Cards · inoperative · Aug 2, 1998 · N14342 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE LANDING GEAR HANDLE WOULD NOT MOVE ABOVE THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE GEAR HANDLE RAISED. MAINTENANCE REMOVED AND REPLACED THE M990 AND M991 LOGIC CARDS IAW MM 32-09-20. OPERATION OF THE LANDING GEAR CON
- [SDR CALA9801187](https://openairdocs.org/sdr/CALA9801187.md): Wire · damaged · Jun 27, 1998 · N14342 · Boeing 7373T0 · Light System Wiring
  > INSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 6ABC TO 12AB. TROUBLESHOOTING FOUND A CRUSHED WIRE UNDER SEAT AT ROW 9ABC. THE WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED.
- [SDR CALA9801062](https://openairdocs.org/sdr/CALA9801062.md): Skin · dented · Jun 12, 1998 · N14342 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SMALL DENTS IN RT FUSELAGE SKIN JUST FORWARD OF STA 360 BETWEEN STRINGERS 18R AND 19R. REPAIRED IAW ECRA 5331-01024.
- [SDR CALA9801037](https://openairdocs.org/sdr/CALA9801037.md): Hinge · gouged · Jun 10, 1998 · N14342 · Boeing 7373T0 · Engine Thrust Reverser
  > INSPECTION FOUND NR 1 ENGINE INBOARD AND OUTBOARD THRUST REVERSER FORWARD HINGE POINT FORWARD LUGS GOUGED. THE HINGES WERE REPAIRED IAW ECRA 7832-01125.
- [SDR CALA9800967](https://openairdocs.org/sdr/CALA9800967.md): Door · cracked · Jun 4, 1998 · N14342 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 CRACK AT FORWARD LOWER CORNER (JUST BELOW HOLD OPEN HOOK) OF FORWARD BAGGAGE BIN DOOR. THE DOOR WAS REPAIRED IAW ECRA 5234-01004.
- [SDR CALA9800951](https://openairdocs.org/sdr/CALA9800951.md): Floorbeam · corroded · Jun 3, 1998 · N14342 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION AT FASTENER HOLES OF AFT LAV LT FLOORBEAM AT STA 1016 FROM CENTERLINE TO LBL 36. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.
- [SDR CALA9800915](https://openairdocs.org/sdr/CALA9800915.md): Skin · cracked · May 31, 1998 · N14342 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND THREE.25 CRACKS COMING FROM RIVETS IN NR 1 SLAT LOWER SKIN BETWEEN OUTBOARD MAIN TRACK AND OUTBOARD AUX TRACK. A REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C30133.
- [SDR CALA9800914](https://openairdocs.org/sdr/CALA9800914.md): Angle · corroded · May 29, 1998 · N14342 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT AFT GALLEY NEAR L-2 DOOR THRESHOLD AREA, STA 947 TO 967. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9800913](https://openairdocs.org/sdr/CALA9800913.md): Seat Track · corroded · May 29, 1998 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT INBOARD SEAT TRACK IN AFT GALLEY AT STA 947.5 CORRODED. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA9601816](https://openairdocs.org/sdr/CALA9601816.md): Axle · cracked · Dec 13, 1996 · N14342 · Boeing 7373T0 · Wheel/Ski/Float
  > WHILE TURNING ONTO THE RUNWAY FOR TAKEOFF, THE CREW FELT THE NOSE STRUT BOTTOM OUT. THE CREW IN AIRCRAFT BEHIND THEM REPORTED THAT THEY LOST A NOSE TIRE. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NOSE STRUT AXLE CRACKED. THE NOSE LOWER S
- [SDR CALA9600685](https://openairdocs.org/sdr/CALA9600685.md): Track · worn · May 20, 1996 · N14342 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A HOLE WORN THROUGH AFT CARGO FLOORBEAM TRACK ON LT SIDE. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA9600684](https://openairdocs.org/sdr/CALA9600684.md): Skin · cracked · May 20, 1996 · N14342 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 2.875 INCH CRACK IN NR 1 SLAT LOWER SKIN PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159.
- [SDR CAL960450](https://openairdocs.org/sdr/CAL960450.md): Pin · failed · Apr 9, 1996 · N14342 · Boeing 7373T0 · Trailing Edge Flaps
  > THE FLIGHT CREW REPORTED AIRFRAME VIBRATION AFTER TAKEOFF FROM PHX. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD FLAP FAIRING HAD DEPARTED THE AIRCRAFT. THE FAIRING WAS RECOVERED ON OR NEAR THE RUNWAY AT PHX

## 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 = 'N14342' AND deregistration_id = 'N14342-2009-07-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14342-2009-07-21/reports

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