# Service difficulty reports: N14337, cancelled Jul 21, 2009

A list on [N14337, cancelled Jul 21, 2009](https://openairdocs.org/deregistered/N14337-2009-07-21.md).

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

Page 1 of 2 · 63 reports

- [SDR CALA0600269](https://openairdocs.org/sdr/CALA0600269.md): Stiffener · cracked · May 19, 2006 · N14337 · Boeing 7373T0 · Wing, Center Box
  > INSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL AND RBL 6.15. THE VERTICAL STIFFENER WAS REPAIRED IAW ECRA 5714-01018.
- [SDR CALA0600076](https://openairdocs.org/sdr/CALA0600076.md): Stringer · corroded · Mar 1, 2006 · N14337 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED JUST FORWARD OF STA 1016. A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0600075](https://openairdocs.org/sdr/CALA0600075.md): Web · corroded · Mar 1, 2006 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD WEB FORWARD FACE CORRODED AT LEFT AND RIGHT CHANNEL, STA 1016, BL 0. A WEB AND CHANNEL REPAIR WAS INSTALLED IAW BOEING DRAWING 65C28106.
- [SDR CALA0600074](https://openairdocs.org/sdr/CALA0600074.md): Skin · corroded · Mar 1, 2006 · N14337 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1009, S27L. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, REPAIR 31.
- [SDR CALA0600072](https://openairdocs.org/sdr/CALA0600072.md): Stringer · corroded · Feb 27, 2006 · N14337 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L IN FORWARD BAGGAGE BIN CORRODED AT STA 440-460. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, DETAIL VI.
- [SDR CALA0600070](https://openairdocs.org/sdr/CALA0600070.md): Stringer · corroded · Feb 26, 2006 · N14337 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 480-500B. A NEW SECTION OF STRINGER WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0600065](https://openairdocs.org/sdr/CALA0600065.md): Frame · cracked · Feb 21, 2006 · N14337 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME AT STA 616 JUST BELOW MAIN DECK FLOOR, LBL 0 TO LBL 60. REPAIRED FRAME IAW ECRA 5311-01158.
- [SDR CALA0600167](https://openairdocs.org/sdr/CALA0600167.md): Floorbeam · corroded · Mar 3, 2005 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 19. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04464.
- [SDR CALA0600166](https://openairdocs.org/sdr/CALA0600166.md): Floorbeam · corroded · Mar 2, 2005 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, LBL 20. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04463.
- [SDR CALA0500070](https://openairdocs.org/sdr/CALA0500070.md): Threshold · corroded · Mar 2, 2005 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR THRESHOLD DRAIN FRAME CORRODED AT STA 294-342, BL 0 TO RBL 36. A CHORD WAS INSTALLED IAW SRM 51-40-02 AND DRAWING 55-45875.
- [SDR CALA0500067](https://openairdocs.org/sdr/CALA0500067.md): Floorbeam · corroded · Feb 27, 2005 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21, RBL 36, AND RBL 49. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.
- [SDR CALA0500062](https://openairdocs.org/sdr/CALA0500062.md): Floorbeam · corroded · Feb 27, 2005 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED IN E&E COMPARTMENT ON RT SIDE ABOVE AIRFONE CONTROL BOX AT STA 312, RBL 21. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.
- [SDR CALA0500061](https://openairdocs.org/sdr/CALA0500061.md): Floorbeam · cracked · Feb 27, 2005 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1.625 INCH CRACK IN FORWARD GALLEY FLOORBEAM WEB AT STA 312, RBL 18. THE WEB WAS REPAIRED IAW ECRA 5310-04462.
- [SDR CALA0400635](https://openairdocs.org/sdr/CALA0400635.md): Skin · dented · Sep 12, 2004 · N14337 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW PART III WITHIN 50 FLIGHT CYCLES.
- [SDR CALA0400480](https://openairdocs.org/sdr/CALA0400480.md): Floorbeam · cracked · May 8, 2004 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146.
- [SDR CALA0400476](https://openairdocs.org/sdr/CALA0400476.md): Angle · cracked · May 6, 2004 · N14337 · Boeing 7373T0 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0400464](https://openairdocs.org/sdr/CALA0400464.md): Angle · cracked · May 4, 2004 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0400461](https://openairdocs.org/sdr/CALA0400461.md): Skin · cracked · May 4, 2004 · N14337 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2.
- [SDR CALA0400447](https://openairdocs.org/sdr/CALA0400447.md): Seat Track · broken · May 1, 2004 · N14337 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > THE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52.
- [SDR CALA0400444](https://openairdocs.org/sdr/CALA0400444.md): Seat Track · broken · May 1, 2004 · N14337 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > THE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0400413](https://openairdocs.org/sdr/CALA0400413.md): Charger · inoperative · Apr 24, 2004 · N14337 · Boeing 7373T0 · Emergency Lighting
  > THREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51.
- [SDR CALA0200127](https://openairdocs.org/sdr/CALA0200127.md): Skin · cracked · Mar 8, 2002 · N14337 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRINGS. A 1" CRACK WAS FOUND AT THE EDGE OF A LIGHTENING HOLE IN C-2 DOOR INNER SKIN AT PULLEY ACCESS PANEL. REPAIR DOUBLERS WERE INSTALLED IAW
- [SDR CALA0200126](https://openairdocs.org/sdr/CALA0200126.md): Skin · cracked · Mar 8, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1" CRACK IN CAPTAIN'S WINDSHIELD O/B POST OUTER SKIN AT UPPER CORNER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-01104.
- [SDR CALA0200125](https://openairdocs.org/sdr/CALA0200125.md): Skin · cracked · Mar 7, 2002 · N14337 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.25" CRACK IN C-2 DOOR INNER SKIN AT AFT LOWER CORNER. THE SKIN WAS REPAIRED IAW ECRA 5230-01650.
- [SDR CALA0200124](https://openairdocs.org/sdr/CALA0200124.md): Web · cracked · Mar 7, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1/2" CRACK IN WEB AT LIGHTENING HOLE AFT OF STA 1040 AND I/B OF TAIL COMPARTMENT ACCESS. A REPAIR WAS INSTALLED IAW ECRA 5320-01768.
- [SDR CALA0200122](https://openairdocs.org/sdr/CALA0200122.md): Spar Cap · cracked · Mar 6, 2002 · N14337 · Boeing 7373T0 · Wing Spar
  > INSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HFEC INSPECTION ON THE R/H WING REAR SPAR AT MLG BEAM ATTACH FITTING AT THE LOCATION REFERENCED IN ECR
- [SDR CALA0200118](https://openairdocs.org/sdr/CALA0200118.md): Skin · cracked · Mar 4, 2002 · N14337 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMANENT REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01584.
- [SDR CALA0200117](https://openairdocs.org/sdr/CALA0200117.md): Web · worn · Mar 2, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND C-1 AFT DOOR JAMB LOWER WEB WORN AROUND EDGES. A NEW WEB WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0200116](https://openairdocs.org/sdr/CALA0200116.md): Keelbeam · chafed · Mar 2, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LT AFT UPPER SURFACE OF KEEL BEAM FLANGE HAD WORN HOLES ON UPPER SURFACE FROM PANEL ATTACH NUTS AT STA 719-727. REPAIRED IAW ECRA 5310-03740.
- [SDR CALA0200115](https://openairdocs.org/sdr/CALA0200115.md): Skin · cracked · Mar 2, 2002 · N14337 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.
- [SDR CALA0200108](https://openairdocs.org/sdr/CALA0200108.md): Strap · corroded · Feb 27, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR H-STRAP CORRODED AT STA 1022-1026, LBL 3. A NEW H-STRAP WAS INSTALLED IAW SRM 51-10-2 AND 51-30-3.
- [SDR CALA0200107](https://openairdocs.org/sdr/CALA0200107.md): Skin · worn · Feb 27, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND UPPER FUSELAGE SKIN WORN AT STA 867, RBL 6. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 214.
- [SDR CALA0200099](https://openairdocs.org/sdr/CALA0200099.md): Floorbeam · corroded · Feb 25, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ABOVE AND BELOW NUT CLIP HOLES AT STA 986, RBL 46 TO LBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0200096](https://openairdocs.org/sdr/CALA0200096.md): Floor Support · cracked · Feb 25, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 578, BBL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-2.
- [SDR CALA0200095](https://openairdocs.org/sdr/CALA0200095.md): Collar · cracked · Feb 24, 2002 · N14337 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING NR 6 FLAP FAIRING HORSE COLLAR. A NEW COLLAR WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0200094](https://openairdocs.org/sdr/CALA0200094.md): Skin · cracked · Feb 24, 2002 · N14337 · Boeing 7373T0 · Wing Structure
  > INSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0200093](https://openairdocs.org/sdr/CALA0200093.md): Floor Support · corroded · Feb 24, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1006-1016, LBL 7 AND RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-02-01.
- [SDR CALA0200092](https://openairdocs.org/sdr/CALA0200092.md): Floor Support · corroded · Feb 23, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A RT AND LT LAV FLOOR SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 44, AND LBL 14 TO LBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200091](https://openairdocs.org/sdr/CALA0200091.md): Floor Support · corroded · Feb 23, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 986-1006. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200090](https://openairdocs.org/sdr/CALA0200090.md): Web · cracked · Feb 22, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1/2" CRACK IN WEB AT STA 270, S14R. A WEB INTERCOSTAL WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200088](https://openairdocs.org/sdr/CALA0200088.md): Stringer · cracked · Feb 22, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN STRINGER 16L AFT OF STA 500C. REPAIRED STRINGER IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0200087](https://openairdocs.org/sdr/CALA0200087.md): Floor Support · cracked · Feb 22, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 663.75, LBL 65. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200086](https://openairdocs.org/sdr/CALA0200086.md): Angle · corroded · Feb 22, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR JAMB, STA 927. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-05.
- [SDR CALA0200084](https://openairdocs.org/sdr/CALA0200084.md): Floor Support · cracked · Feb 20, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN AC BAY FLOOR SUPPORT AT STA 559, RBL 24, IN FORWARD BAGGAGE BIN. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200081](https://openairdocs.org/sdr/CALA0200081.md): Floorbeam · corroded · Feb 18, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 1016, RBL 37 TO LBL 37. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0200080](https://openairdocs.org/sdr/CALA0200080.md): Floorbeam · corroded · Feb 17, 2002 · N14337 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 967, LBL 50 TO RBL 50 AND AT RBL 18 TO LBL 18. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202.
- [SDR CALA0200079](https://openairdocs.org/sdr/CALA0200079.md): Angle · cracked · Feb 17, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3" CRACK IN ANGLE AT STA 927-947, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-03.
- [SDR CALA0200078](https://openairdocs.org/sdr/CALA0200078.md): Floor Support · corroded · Feb 16, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 951, LBL 14 TO LBL 16 AND AT LBL 18 TO LBL 24. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200077](https://openairdocs.org/sdr/CALA0200077.md): Floor Support · corroded · Feb 16, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200076](https://openairdocs.org/sdr/CALA0200076.md): Floor Support · corroded · Feb 16, 2002 · N14337 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947-967, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

Next page: https://openairdocs.org/deregistered/N14337-2009-07-21/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 = 'N14337' AND deregistration_id = 'N14337-2009-07-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14337-2009-07-21/reports

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