# Service difficulty reports: N14308, cancelled Mar 21, 2013

A list on [N14308, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14308-2013-03-21.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 · 71 reports

- [SDR CALA2009062300325](https://openairdocs.org/sdr/CALA2009062300325.md): Handle · lack of lube · Jun 22, 2009 · N14308 · Boeing 7373T0 · Landing Gear Selector
  > AT FLAPS 10 AT 2000 FT ALL SELECTED GEAR DOWN, RECEIVED LIGHT INDICATION 3 GREEN AND 3 RED STEADY, NO HORN W/ FLAPS 30 AT APROX 400 FT AGL TOO LOW GEAR, WENT AROUND. CONFERRED WITH MX. NEXT APCH AND LANDING COMPLETELY NORMAL INDICATIONS ALL AROUND. CLEANED AND
- [SDR CALA0700660](https://openairdocs.org/sdr/CALA0700660.md): Skin · cracked · Oct 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A WALKAROUND INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT STA 727D, S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03745.
- [SDR CALA0700435](https://openairdocs.org/sdr/CALA0700435.md): Skin · cracked · Aug 13, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN AFT CARGO DOOR SKIN AT AFT EDGE OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 3.
- [SDR CALA0700434](https://openairdocs.org/sdr/CALA0700434.md): Channel · cracked · Aug 13, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CHANNEL AT FORWARD LOWER STOP. REPAIRED IAW SRM 51-40-02.
- [SDR CALA0700428](https://openairdocs.org/sdr/CALA0700428.md): Intercostal · cracked · Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB UPPER HINGE INTERCOSTAL AT STA 294.5, S10L. A REPAIR WAS INSTALLED IAW ECRA 5311-01350.
- [SDR CALA0700427](https://openairdocs.org/sdr/CALA0700427.md): Intercostal · cracked · Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB LOWER HINGE INTERCOSTAL AT STA 294.5, S13L TO S14L. A REPAIR WAS INSTALLED IAW ECRA 5311-01349.
- [SDR CALA0700426](https://openairdocs.org/sdr/CALA0700426.md): Frame · cracked · Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FRAME AT DRAIN HOLE, STA 440, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA0700424](https://openairdocs.org/sdr/CALA0700424.md): Skin · cracked · Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND TWO 1 INCH CRACKS IN R-1 DOOR SKIN CUTOUT AT STA 328, S16R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01337.
- [SDR CALA0700423](https://openairdocs.org/sdr/CALA0700423.md): Skin · cracked · Aug 11, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR INNER SKIN BETWEEN LIGHTENING HOLES ABOVE HANDLE. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01089.
- [SDR CALA0700422](https://openairdocs.org/sdr/CALA0700422.md): Seat Track · cracked · Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, RBL 24.8. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.
- [SDR CALA0700421](https://openairdocs.org/sdr/CALA0700421.md): Seat Track · cracked · Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, LBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.
- [SDR CALA0700420](https://openairdocs.org/sdr/CALA0700420.md): Seat Track · cracked · Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK O/B MOUNT FLANGE AT STA 727B, RBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 55321-01492.
- [SDR CALA0700419](https://openairdocs.org/sdr/CALA0700419.md): Frame · cracked · Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK AT TWO EACH HOLES IN I/B CHORD AT STA 639, S16R TO S17R. THE INNER CHORD WAS REPLACED AND A REPAIR WAS INSTALLED IAW ECRA 5311-01347.
- [SDR CALA0700418](https://openairdocs.org/sdr/CALA0700418.md): Frame · corroded · Aug 10, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD BAGGAGE BIN FRAME CORRODED AT STA 500B BETWEEN STRINGER 25R AND S26R. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 7.
- [SDR CALA0700415](https://openairdocs.org/sdr/CALA0700415.md): Frame · corroded · Aug 9, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 947.5 BETWEEN S21L AND S21R, LBL 10 TO RBL 10. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0700452](https://openairdocs.org/sdr/CALA0700452.md): Floorbeam · cracked · Aug 7, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CRACKS TO THE LONGITUDINAL FLOORBEAM FLANGES AT STA 727B, LBL 45.5, RBL 45.5 AND RBL 24.8. REPAIRS WERE PERFORMED IAW ECRA 5321-01492.
- [SDR CALA0700411](https://openairdocs.org/sdr/CALA0700411.md): Skin · damaged · Aug 4, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A HOLE IN FUSELAGE SKIN CAUSED BY A LIGHTNING STRIKE AT STA 375, S24R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0700396](https://openairdocs.org/sdr/CALA0700396.md): Frame · cracked · Aug 3, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.
- [SDR CALA0700395](https://openairdocs.org/sdr/CALA0700395.md): Frame · cracked · Aug 3, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 827, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.
- [SDR CALA0700392](https://openairdocs.org/sdr/CALA0700392.md): Strap · cracked · Aug 2, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN WEB STRAP JUST FORWARD OF L-2 DOOR AT STA 947.5, S10L TO S11L. A NEW WEB STRAP WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0700391](https://openairdocs.org/sdr/CALA0700391.md): Keelbeam · corroded · Aug 1, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LEFT KEEL BEAM CORRODED IN A/C DISTRIBUTION BAY AT STA 500D-520. THE KEEL BEAM WAS REPAIRED IAW SRM 53-30-12, FIGURE 201.
- [SDR CALA0700387](https://openairdocs.org/sdr/CALA0700387.md): Stringer · corroded · Aug 1, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700441](https://openairdocs.org/sdr/CALA0700441.md): Door Frame · cracked · Jul 30, 2007 · N14308 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A CRACK EMANATING FROM THE DOORSTOP CUTOUT IN THE AFT EDGE BEAM OF THE L-1 DOOR. THE EDGE BEAM WAS REPAIRED IAW ECRA 5210-01944.
- [SDR CALA0700381](https://openairdocs.org/sdr/CALA0700381.md): Frame · corroded · Jul 29, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 1006 FROM S25R TO 26L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1.
- [SDR CALA0700377](https://openairdocs.org/sdr/CALA0700377.md): Stringer · corroded · Jul 27, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25L CORRODED AT REPAIR CUTOUT AFT OF STA 1006. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.
- [SDR CALA0700374](https://openairdocs.org/sdr/CALA0700374.md): Shear Web · cracked · Jul 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2.5 INCH CRACK IN LEFT SHEAR WEB FORWARD OF STA 639 FUSELAGE FRAME, LBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0700373](https://openairdocs.org/sdr/CALA0700373.md): Floorbeam · corroded · Jul 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 360, BL 0. THE CORRODED AREA WAS CUT OUT AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-30-51, FIGURE 201, REPAIR 2.
- [SDR CALA0600245](https://openairdocs.org/sdr/CALA0600245.md): Controller · inoperative · Jun 16, 2006 · N14308 · Boeing 7373T0 · Windshield/Door Rain/Ice Removal
  > THE CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE TO IAH. THE SMOKE REMOVAL CHECKLIST WAS COMPLETED AND AFTER TURNING OFF THE RECIRCULATION FAN THE SMOKE WENT AWAY. ALSO OBSERVED THAT THE RT FWD WINDOW HEAT CIRCUIT BREAKER HAD POPPED. THE CREW WAITED 10 M
- [SDR CALA0500429](https://openairdocs.org/sdr/CALA0500429.md): Shear Tie · corroded · Dec 10, 2005 · N14308 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND FRAME/SHEAR TIE CORRODED AT STA 967 BETWEEN STRINGERS 27L-27R. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 8.
- [SDR CALA0500428](https://openairdocs.org/sdr/CALA0500428.md): Frame · cracked · Dec 9, 2005 · N14308 · Boeing 7373T0 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0500371](https://openairdocs.org/sdr/CALA0500371.md): Skin · cracked · Oct 20, 2005 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727E - 747 JUST BELOW S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, DETAIL XI.
- [SDR CALA0300496](https://openairdocs.org/sdr/CALA0300496.md): Stringer · corroded · Aug 26, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 996. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0300495](https://openairdocs.org/sdr/CALA0300495.md): Stringer · corroded · Aug 25, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300493](https://openairdocs.org/sdr/CALA0300493.md): Floorbeam · corroded · Aug 25, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 500D BETWEEN S26L AND S27L, LOWER AREA. THE CORRODED AREA WAS CUT OUT AND FILLER, DOUBLER AND A SHIM WERE INSTALLED IAW SRM 53-00-07, FIGURE 203 AND 204.
- [SDR CALA0300490](https://openairdocs.org/sdr/CALA0300490.md): Seat Track · corroded · Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 296, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-40352 AND SRM 51-40-02.
- [SDR CALA0300489](https://openairdocs.org/sdr/CALA0300489.md): Floorbeam · corroded · Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294.5, RBL 41. THE FLOORBEAM UPPER CHORD SECTION WAS REMOVED AND A NEW UPPER CHORD WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0300487](https://openairdocs.org/sdr/CALA0300487.md): Floor Support · corroded · Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 947.5 TO 967 AT RBL 7 AND RBL 46. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-40-02 AND ECRA 5310-03585.
- [SDR CALA0300486](https://openairdocs.org/sdr/CALA0300486.md): Channel · cracked · Aug 24, 2003 · N14308 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND THE LT WING T/E NR 3 FLAP TRACK FAIRING AFT END U-CHANNEL CRACKED IN TWO PLACES UNDER THE TRACK. THE CRACKS WERE.25 INCH LONG. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300086](https://openairdocs.org/sdr/CALA0300086.md): Floorbeam · corroded · Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES OF UPPER CAP AT STA 1006 FROM BL 0 TO RBL 40. REMOVED AND REPLACED T-CAP IAW ECRA 5310-03851.
- [SDR CALA0300085](https://openairdocs.org/sdr/CALA0300085.md): Channel · corroded · Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHANNEL CORRODED ON UPPER SURFACE AND AT NUTPLATES AT STA 1006-1016, LBL 5 TO LBL 9. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02.
- [SDR CALA0300084](https://openairdocs.org/sdr/CALA0300084.md): Angle · corroded · Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON UPPER SURFACE OF ANGLE AT NUTPLATES, STA 1006, LBL 10. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300083](https://openairdocs.org/sdr/CALA0300083.md): Floorbeam · corroded · Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED IN AFT GALLEY AREA AT STA 967, LBL 25. REPAIRED IAW ECRA 5320-01726.
- [SDR CALA0300081](https://openairdocs.org/sdr/CALA0300081.md): Floorbeam · corroded · Mar 1, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF CAP AND AT FASTENER HOLES AT STA 1006, BL 0 TO RBL 30. THE T-CAP WAS REMOVED AND REPLACED IAW SRM 51-40-04.
- [SDR CALA0300068](https://openairdocs.org/sdr/CALA0300068.md): Frame · corroded · Feb 23, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND R/H O/B FRAME CORRODED AT STA 986, RBL 40. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0300054](https://openairdocs.org/sdr/CALA0300054.md): Pressure Panel · cracked · Feb 18, 2003 · N14308 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A.5 INCH CRACK IN PRESSURE DECK AT BS 664 - 675, LBL 30 - 35. REPAIRED IAW SRM 53-60-51, PAGE 213-221.
- [SDR CALA0300052](https://openairdocs.org/sdr/CALA0300052.md): Pressure Panel · cracked · Feb 17, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231.
- [SDR CALA0200028](https://openairdocs.org/sdr/CALA0200028.md): Skin · cracked · Jan 21, 2002 · N14308 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3/4" CRACK AT LIGHTENING HOLE CUTOUT OF FORWARD CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01014.
- [SDR CALA0200025](https://openairdocs.org/sdr/CALA0200025.md): Skin · delaminated · Jan 17, 2002 · N14308 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND L/H WING LEADING EDGE SKIN DELAMINATED AND HILOCK PULLED THROUGH SKIN BEHIND #2 SLAT AT O/B END. REPAIRED IAW ECRA 5721-01048.
- [SDR CALA0200024](https://openairdocs.org/sdr/CALA0200024.md): Skin · delaminated · Jan 17, 2002 · N14308 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND R/H WING LEADING EDGE SKIN UNDER O/B EDGE OF #5 SLAT DELAMINATED. REPAIRED IAW ECRA 5721-01048.
- [SDR CALA0200022](https://openairdocs.org/sdr/CALA0200022.md): Attach Angle · worn · Jan 17, 2002 · N14308 · Boeing 7373T0 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B.

Next page: https://openairdocs.org/deregistered/N14308-2013-03-21/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 = 'N14308' AND deregistration_id = 'N14308-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14308-2013-03-21/reports

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