# Service difficulty reports: N14334, cancelled Mar 21, 2013

A list on [N14334, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14334-2013-03-21.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 · 76 reports

- [SDR CAL0700595](https://openairdocs.org/sdr/CAL0700595.md): Bracket · cracked · Oct 18, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > S-10L, UPPER HINGE, LOWER INTERCOSTAL, O/B ATTACHMENT CLIP CRACKED.75 INCH IN AT AFT BEND. REPAIRED PER ECRA 5311-01369.
- [SDR CALA0700593](https://openairdocs.org/sdr/CALA0700593.md): Bracket · cracked · Oct 17, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INTERCOSTAL ATTACH BRACKET CRACKED AT STA 294.5 STR 11L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01368.
- [SDR CALA0700591](https://openairdocs.org/sdr/CALA0700591.md): Intercostal · cracked · Oct 17, 2007 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT STA 294.5. S-16L. REMOVED AND REPLACED PER ECRA 5311-01368.
- [SDR CALA0700590](https://openairdocs.org/sdr/CALA0700590.md): Stringer · corroded · Oct 17, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > FBB STRINGER S-28R HAS SEVERE CORROSION AFT STA 500 FRAME CUTOUT DAMAGE. REPAIR PER SRM 53-00-03 FIG 201.
- [SDR CAL0700594](https://openairdocs.org/sdr/CAL0700594.md): Keelbeam · corroded · Oct 17, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Keel
  > FBB KEEL BEAM S-28R HAS CORROSION ON I/B FLANGE AROUND FASTENER HOLES AFT OF 500D. REPAIRED RT KEEL BEAM AFT OF STA 500D PER ECRA 5311-01367 AND SRM 53-30-12 FIG 201 REPAIR 2.
- [SDR CAL0700592](https://openairdocs.org/sdr/CAL0700592.md): Intercostal · cracked · Oct 17, 2007 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT STA 294.5 STR 12L. FABRICATED AND INSTALLED PER ECRA 5311-01368.
- [SDR CALA0700588](https://openairdocs.org/sdr/CALA0700588.md): Skin · cracked · Oct 16, 2007 · N14334 · Boeing 7373T0 · Cargo/Baggage Doors
  > C1 DOOR CRACKED AT EXT HANDLE CUTOUT. INSTALLED AND REPAIR DOUBLER IAW SRM 52-00-01 REPAIR 3.
- [SDR CALA0700587](https://openairdocs.org/sdr/CALA0700587.md): Skin · cracked · Oct 15, 2007 · N14334 · Boeing 7373T0 · Cargo/Baggage Doors
  > C2 DOOR CRACKED AT EXTERIOR DOOR HANDLE CUTOUT. TRIMMED OUT CRACKED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 52-00-01 FIG 201.
- [SDR CALA0700582](https://openairdocs.org/sdr/CALA0700582.md): Keelbeam · corroded · Oct 13, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Keel
  > KEELBEAM CORRODED ON I/B AND O/B FLANGES AROUND FASTENERS STA 500D-520 & O/B FLANGE STA 520. REMOVED & REPLACED FWD SEC OF LEFT KEELBEAM FROM STA 500C TO STA 540 PER SRM 51-40-02 & 53-60-12 FIG 201.
- [SDR 0700574](https://openairdocs.org/sdr/0700574.md): Door Frame · cracked · Oct 11, 2007 · N14334 · Boeing 7373T0 · Fuselage Main, Structure
  > FWD CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED FRAME PER SRM 51-40-02.
- [SDR CALA0600200](https://openairdocs.org/sdr/CALA0600200.md): Doubler · cracked · May 6, 2006 · N14334 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN SECTION 41 UPPER SKIN DOUBLER AT STA 178-196.5, S2L TO S2R. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-40-02 AND 53-10-01.
- [SDR CALA0500224](https://openairdocs.org/sdr/CALA0500224.md): Frame · corroded · Jul 18, 2005 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STA 727 BULKHEAD FRAME FLANGE CORRODED BETWEEN LEFT AND RIGHT KEELBEAM AS SEEN FROM AFT CARGO COMPARTMENT, LBL 6.3. REPAIRED IAW ECRA 5311-01232.
- [SDR CALA0500223](https://openairdocs.org/sdr/CALA0500223.md): Skin · cracked · Jul 17, 2005 · N14334 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 0.5 IN CRACK AT EDGE OF NR 1 PYLON SKIN PANEL OPENING NR 5724L UPPER FORWARD CORNER. SKIN REPAIRED IAW ECRA 5430-01204.
- [SDR CALA0500222](https://openairdocs.org/sdr/CALA0500222.md): Skin · cracked · Jul 16, 2005 · N14334 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND 0.5 IN CRACK IN 2 PLACES ON NR 1 ENGINE PYLON SKIN ON EXTERNAL SURFACE ACCESS PANEL NR 5724 CUTOUT. PYLON SKIN REPAIRED IAW ECRA 5430-01204.
- [SDR CALA0500221](https://openairdocs.org/sdr/CALA0500221.md): Keelbeam · cracked · Jul 15, 2005 · N14334 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND 1.0 IN CRACK IN LT KEEL BEAM AT STA 727 ON O/B SIDE, LBL 6.5. CRACKED SECTION OF KEEL BEAM LOWER CHORD CUT OUT AND NEW SECTION SPLICED IN IAW ECRA 5311-01230.
- [SDR CALA0500215](https://openairdocs.org/sdr/CALA0500215.md): Floorbeam · corroded · Jul 10, 2005 · N14334 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 967, RBL 38 TO LBL 0. REPLACED FLOORBEAM UPPER CHORD IAW ECRA 5311-01231.
- [SDR CALA0500209](https://openairdocs.org/sdr/CALA0500209.md): Floor Support · cracked · Jul 1, 2005 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 4 INCH CRACK IN FLOOR SUPPORT AT STA 328, LBL 11. CRACKED AREA CUT OUT AND REPAIRED IAW SRM 51-70-12, FIGURE 1, SHEET 6.
- [SDR CALA0400038](https://openairdocs.org/sdr/CALA0400038.md): Shear Tie · corroded · Jan 17, 2004 · N14334 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 927 BETWEEN S27L AND S27R IN AFT CARGO AREA. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07, FIGURE 210.
- [SDR CALA0400037](https://openairdocs.org/sdr/CALA0400037.md): Skin · corroded · Jan 17, 2004 · N14334 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 927 BETWEEN S27L AND S27R. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 202.
- [SDR CALA0400034](https://openairdocs.org/sdr/CALA0400034.md): Skin · cracked · Jan 16, 2004 · N14334 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1.25 INCH CRACK NR 2 PYLON PANEL NR 5842R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.
- [SDR CALA0400027](https://openairdocs.org/sdr/CALA0400027.md): Skin · cracked · Jan 15, 2004 · N14334 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING NR 4 SLAT SKIN LOWER SURFACE O/B OF ACTUATOR ATTACH. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 57-43-01.
- [SDR CALA0400025](https://openairdocs.org/sdr/CALA0400025.md): Intercostal · corroded · Jan 14, 2004 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL IN E&E COMPARTMENT CORRODED AT STA 227.8, BL 0 TO RBL 7. THE CORROSION WAS REMOVED AND THE INTERCOSTAL AND A STIFFENER WERE REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300536](https://openairdocs.org/sdr/CALA0300536.md): Apu · fire · Sep 18, 2003 · N14334 · Boeing 7373T0 · APU Cowling/Containment
  > APU FIRE LT ILLUMINATED WHILE AT CRUISE FLT ENROUTE. FIRE BOTTLE WAS DISCHARGED, LT EXT. FLT CONTINUED W/O FURTHER PROBLEM. MAINT INSP APU AND FOUND EVIDENCE OF SMALL FIRE AT BOTTOM REAR OF APU (EXH AREA). FIRE APPEARED TO BE CONTAINED. WIRES FROM APU EG
- [SDR CALA0100876](https://openairdocs.org/sdr/CALA0100876.md): Floorbeam · corroded · Sep 14, 2001 · N14334 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, RBL 4 TO LBL 24. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04187 AND SRM 53-00-51, FIGURE 202.
- [SDR CALA0100873](https://openairdocs.org/sdr/CALA0100873.md): Floorbeam · damaged · Sep 13, 2001 · N14334 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A NOTCH CUT INTO FLOORBEAM WEB AT STA 328, LOCATED JUST FORWARD OF RT HORIZONTAL STABILIZER PULLEY CABLE. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01694.
- [SDR CALA0100869](https://openairdocs.org/sdr/CALA0100869.md): Rib · gouged · Sep 13, 2001 · N14334 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND R/H WING L/E RIB GOUGED AROUND SCREW HOLE AT #4 SLAT(SLAT STA 30). THE SLAT RIB WAS REPAIRED IAW ECRA 5750-03584.
- [SDR CALA0100860](https://openairdocs.org/sdr/CALA0100860.md): Pan · cracked · Sep 11, 2001 · N14334 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A 0.20 INCH CRACK IN L-1 DOOR PAN AT AFT SIDE OF DOOR AT STOP SCREW BELOW CENTERING GUIDE. A DOUBLER WAS INSTALLED IAW ECRA 5210-01398.
- [SDR CALA0100859](https://openairdocs.org/sdr/CALA0100859.md): Panel · delaminated · Sep 10, 2001 · N14334 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND O/B TRAILING EDGE OF #5 SLAT PANEL DELAMINATED. THE #5 SLAT ASSY WAS REMOVED AND REPLACED IAW MM 27-81-21.
- [SDR CALA0100858](https://openairdocs.org/sdr/CALA0100858.md): Fitting · corroded · Sep 10, 2001 · N14334 · Boeing 7373T0 · Fuselage, Landing Gear Attach Fittings
  > INSPECTION FOUND RT MLG SIDE STRUT FITTING LUG CORRODED AT STA 685. THE LUG WAS REPAIRED IAW ECRA 5340-01354.
- [SDR CALA0100849](https://openairdocs.org/sdr/CALA0100849.md): Slat · dented · Sep 9, 2001 · N14334 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND #3 SLAT LEADING EDGE DENTED APPROXIMATELY 30" FROM O/B END. REPAIRED SLAT IAW SRM 57-43-01.
- [SDR CALA0100840](https://openairdocs.org/sdr/CALA0100840.md): Skin · dented · Sep 7, 2001 · N14334 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND C-1 DOOR SKIN DENTED 13 INCHES AFT OF FORWARD EDGE AND 12 INCHES FROM TOP. A DOUBLER WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA0100838](https://openairdocs.org/sdr/CALA0100838.md): Floor Support · corroded · Sep 7, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLE AFT OF STA 787, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-53.
- [SDR CALA0100836](https://openairdocs.org/sdr/CALA0100836.md): Plate · cracked · Sep 6, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3" CRACK ON UPPER WEB OF DOOR THRESHOLD PLATE AT STA 847. A NEW THRESHOLD PLATE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100834](https://openairdocs.org/sdr/CALA0100834.md): Seat Track · cracked · Sep 5, 2001 · N14334 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1/2" CRACK IN L/H I/B SEAT TRACK AT AFT HI-LOCK, STA 727B. STRAP AND FILLER WERE INSTALLED IAW ECRA 5310-04183.
- [SDR CALA0100833](https://openairdocs.org/sdr/CALA0100833.md): Seat Track · cracked · Sep 5, 2001 · N14334 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1/4" CRACK IN UPPER FLANGE OF L/H O/B SEAT TRACK AT HI-LOCK ATTACH POINT, STA 727B. A STRAP WAS INSTALLED IAW ECRA 5310-04183.
- [SDR CALA0100832](https://openairdocs.org/sdr/CALA0100832.md): Stringer · cracked · Sep 4, 2001 · N14334 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 4" CRACK IN STRINGER 10R AT STA 332. THE STRINGER WAS REMOVED AND REPLACED IAW EA 5363-01014.
- [SDR CALA0100831](https://openairdocs.org/sdr/CALA0100831.md): Intercostal · cracked · Sep 4, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 4" CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C33288 AND EA 5363-01014.
- [SDR CALA0100830](https://openairdocs.org/sdr/CALA0100830.md): Angle · corroded · Sep 4, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R/H LAV WALL & L/H LAV WALL ANGLES CORRODED AT STA 1014 RBL 4 AND LBL 4. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100829](https://openairdocs.org/sdr/CALA0100829.md): Angle · corroded · Sep 2, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ATTACH ANGLE FOR R/H AFT I/B WHEEL WELL FAIRING CORRODED ON FORWARD CURVED ATTACH POINTS. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100822](https://openairdocs.org/sdr/CALA0100822.md): Brace · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L/H AND R/H DIAGONAL BRACES CORRODED AT STA 1006-1016. NEW DIAGONAL BRACES WERE INSTALLED IAW SRM 51-10-02.
- [SDR CALA0100821](https://openairdocs.org/sdr/CALA0100821.md): Strap · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND "H" STRAP IN AFT LAV AREA CORRODED. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0100820](https://openairdocs.org/sdr/CALA0100820.md): Angle · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100819](https://openairdocs.org/sdr/CALA0100819.md): Angle · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100818](https://openairdocs.org/sdr/CALA0100818.md): Floor Support · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THREE FLOOR SUPPORTS CORRODED AT STA 950 FROM RBL 24 TO RBL 53. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03585.
- [SDR CALA0100817](https://openairdocs.org/sdr/CALA0100817.md): Floor Support · corroded · Aug 29, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947 - 967, RBL 30 AND STA 967-987, RBL 16. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03585.
- [SDR CALA0100811](https://openairdocs.org/sdr/CALA0100811.md): Seat Track · corroded · Aug 27, 2001 · N14334 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-947.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100810](https://openairdocs.org/sdr/CALA0100810.md): Mount · corroded · Aug 27, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R/H AFT O/B GALLEY MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100803](https://openairdocs.org/sdr/CALA0100803.md): Floorbeam · corroded · Aug 26, 2001 · N14334 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 312, LBL 24 TO RBL 23. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100805](https://openairdocs.org/sdr/CALA0100805.md): Angle · corroded · Aug 25, 2001 · N14334 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0100804](https://openairdocs.org/sdr/CALA0100804.md): Mount · corroded · Aug 25, 2001 · N14334 · Boeing 7373T0 · Fuselage, Equipment Attach Fittings
  > INSPECTION FOUND GALLEY FLOOR MOUNT CORRODED AT STA 292, RBL 12. A NEW GALLEY FLOOR MOUNT WAS INSTALLED IAW SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N14334-2013-03-21/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 = 'N14334' AND deregistration_id = 'N14334-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14334-2013-03-21/reports

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