# Service difficulty reports: N14335, cancelled Mar 21, 2013

A list on [N14335, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14335-2013-03-21.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 · 75 reports

- [SDR CALA2009042000209](https://openairdocs.org/sdr/CALA2009042000209.md): Skin · cracked · Apr 20, 2009 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > DURING C-SCAN INSPECTION FOUND 1EA 1.75 INCH LONG CRACK ON S-23LT 3 INCHES AFT OF STA 727D. INSTALLED REPAIR PER 53-00-01, REPAIR 31, FIG 201, PROCEDURE V. PLACED ON DIP PER EC/RA 5331-01399, BEFORE THE ACCUMULATION OF 60,000 TOTAL AIRCRAFT FLT CYCLES, ACCOMP
- [SDR CALA2009032400162](https://openairdocs.org/sdr/CALA2009032400162.md): Battery Pack · discharged · Mar 23, 2009 · N14335 · Boeing 7373T0 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT LEFT BATTERY PACK FOR THE L2 DOOR EMERGENCY LIGHTS.
- [SDR CALA2009031600142](https://openairdocs.org/sdr/CALA2009031600142.md): Skin · cracked · Mar 14, 2009 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > RT AFT FUSELAGE AFT OF STA 787 S-18R SHOWS CRACK APPROX 2 INCHES LONG. REPAIRED AS PER SRM REF 53-00-01 REPAIR 5.
- [SDR CALA2009031600141](https://openairdocs.org/sdr/CALA2009031600141.md): Skin · cracked · Mar 14, 2009 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > RT AFT FUSELAGE AT STA 767 S-23R C-SCAN SHOWS INDICATION OF CRACK. REPAIRED AS PER SRM 53-00-01 REPAIR 5.
- [SDR CALA0800115](https://openairdocs.org/sdr/CALA0800115.md): Intercostal · cracked · Feb 8, 2008 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > BS 294.5 STRINGER 7L INTERCOSTAL WEB CRACKED AT IB FORWARD CORNER. REMOVED AND REPLACED PER ECRA 5310-04700.
- [SDR CALA0800114](https://openairdocs.org/sdr/CALA0800114.md): Link · corroded · Feb 7, 2008 · N14335 · Boeing 7373T0 · Main Landing Gear
  > RT MAIN GEAR STABILIZER LINK HAS CORROSION AT END. REMOVED AND REPLACED RT MAIN GEAR STABILIZER LINK PER MM 57-15-00.
- [SDR CALA0800106](https://openairdocs.org/sdr/CALA0800106.md): Attach Angle · cracked · Jan 31, 2008 · N14335 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE CRACKED AT STA350 STRINGER 15L AFT SIDE OF L-1 DOOR. REMOVED AND REPLACED ANGLE PER SRM 51-40-02 AND EA 354-53-002 CAL REV 2.
- [SDR CALA0800107](https://openairdocs.org/sdr/CALA0800107.md): Seat Track · corroded · Jan 30, 2008 · N14335 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND RBL 18 HAS SIGNS OF SURFACE CORROSION. REMOVED FLOORBOARDS FOR FOM IAW SRM 51-40-02. REMOVED AND REPLACED CORRODED SEAT TRACK SECTION IAW SRM 53-00-52 FIG 201 AND SRM 51-40-02. REINSTALLED FLOORBOARDS IAW SRM 51-40-02 SEALED FLOORBOARDS PER AMM 51-30-
- [SDR CALA0500283](https://openairdocs.org/sdr/CALA0500283.md): Keelbeam · corroded · Aug 26, 2005 · N14335 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D-540, S28R. THE CORRODED SECTION OF KEEL BEAM WAS CUT OUT AND A NEW SECTION OF KEEL BEAM WAS INSTALLED IAW ECRA 5311-01236.
- [SDR CALA0500270](https://openairdocs.org/sdr/CALA0500270.md): Stringer · corroded · Aug 20, 2005 · N14335 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25R IN THE AFT BAGGAGE BIN CORRODED AT STA 867-887, RBL 27. A SECTION OF STRINGER AND DOUBLERS WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0500267](https://openairdocs.org/sdr/CALA0500267.md): Frame · cracked · Aug 18, 2005 · N14335 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616, S18L TO S19L. A FILLER AND ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01158, PAGE 1-9.
- [SDR CALA0500090](https://openairdocs.org/sdr/CALA0500090.md): Skin · cracked · Mar 30, 2005 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN DURING WALKAROUND. THE CRACK WAS LOCATED APPROXIMATELY 2.5 FEET FORWARD OF AFT CARGO DOOR AND 2.5 FEET BELOW WATER LINE AND BETWEEN STRINGERS 19R AND 20R (THREE FEET FORWARD OF STA 767). A REPAIR DOUBLER WAS INST
- [SDR CALA0400465](https://openairdocs.org/sdr/CALA0400465.md): Charger · inoperative · May 5, 2004 · N14335 · Boeing 7373T0 · Emergency Lighting
  > THE EMERGENCY LIGHTS IN FIRST CLASS CABIN AND AT FORWARD SERVICE ENTRY DOOR WERE FOUND INOPERATIVE. THE BATTERY CHARGER AT STA 338 WAS REPLACED IAW MM 33-51-51.
- [SDR CALA0400105](https://openairdocs.org/sdr/CALA0400105.md): Skin · cracked · Feb 11, 2004 · N14335 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204.
- [SDR CALA0400100](https://openairdocs.org/sdr/CALA0400100.md): Skin · delaminated · Feb 11, 2004 · N14335 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37.
- [SDR CALA0400099](https://openairdocs.org/sdr/CALA0400099.md): Skin · punctured · Feb 10, 2004 · N14335 · Boeing 7373T0 · Spoilers
  > INSPECTION FOUND RT WING NR 6 FLIGHT SPOILER PANEL PUNCTURED IN CENTER SECTION. REPAIRED SPOILER PANEL IAW SRM 57-70-1.
- [SDR CALA0400091](https://openairdocs.org/sdr/CALA0400091.md): Strap · corroded · Feb 8, 2004 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0400090](https://openairdocs.org/sdr/CALA0400090.md): Strap · corroded · Feb 8, 2004 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRAP I/B OF C-2 DOOR THRESHOLD CORRODED FROM STA 787 TO 847 IN AFT BAG BIN. REPLACED STRAP IAW SRM 51-40-02.
- [SDR CALA0400082](https://openairdocs.org/sdr/CALA0400082.md): Attach Angle · cracked · Feb 6, 2004 · N14335 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12.
- [SDR CALA0300520](https://openairdocs.org/sdr/CALA0300520.md): Fan · seized · Sep 9, 2003 · N14335 · Boeing 7373T0 · Turbine Engine Compressor Section
  > THE NR 2 ENGINE GAVE OFF A LOUD BANG FOLLOWED BY VIBRATION AND THE ENGINE SPOOLED DOWN TO IDLE. THE ENGINE NEVER DID SHUTDOWN. CREW WAS UNABLE TO GET POWER ABOVE IDLE. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENG
- [SDR CALA0300005](https://openairdocs.org/sdr/CALA0300005.md): Pressure Panel · cracked · Jan 6, 2003 · N14335 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND AN 8 INCH CRACK IN LT MAIN WHEEL WELL PRESSURE DECK WEB AT STA 664-675. THE AREA WAS REPAIRED IAW SRM 53-60-51.
- [SDR CALA0300003](https://openairdocs.org/sdr/CALA0300003.md): Skin · cracked · Jan 6, 2003 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1/4" CRACK IN BELLY SKIN AFT OF EXHAUST DUCT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.
- [SDR CALA0200587](https://openairdocs.org/sdr/CALA0200587.md): Oven · malfunctioned · Dec 15, 2002 · N14335 · Boeing 7373T0 · Buffet/Galleys
  > FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM BEHIND OVENS IN AFT GALLEY WHILE AT CRUISE EN ROUTE TO CLE. ASSOCIATED CIRCUIT BREAKERS WERE PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND
- [SDR CALA0200492](https://openairdocs.org/sdr/CALA0200492.md): Megaphone · weak · Oct 11, 2002 · N14335 · Boeing 7373T0 · Emergency Equipment
  > INSPECTION FOUND AFT PORTABLE MEGAPHONE WEAK. THE MEGAPHONE WAS REMOVED AND REPLACED.
- [SDR CALA0100961](https://openairdocs.org/sdr/CALA0100961.md): Skin · gouged · Oct 17, 2001 · N14335 · Boeing 7373T0 · Cargo/Baggage Doors
  > FORWARD BAG BIN DOOR INNER SKIN PREVIOUS REPAIR DAMAGED / GOUGED. INSTALLED REPAIR DOUBLER PER EC/RA 5230-01633.
- [SDR CALA0100957](https://openairdocs.org/sdr/CALA0100957.md): Skin · cracked · Oct 16, 2001 · N14335 · Boeing 7373T0 · Cargo/Baggage Doors
  > LIGHTING HOLES DAMAGED ABOVE COUNTER BALANCE CABLES AT A/B/B (1" CRACK). INSTALLED REPAIR AS PER EC/RA 5230-01632.
- [SDR CALA0100955](https://openairdocs.org/sdr/CALA0100955.md): Web · dented · Oct 16, 2001 · N14335 · Boeing 7373T0 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR INNER SKIN LOWER CENTER DENT AT LIGHTENING HOLE. INSTALLED DOUBLER REPAIR PER EC/RA 5230-1631.
- [SDR CALA0100949](https://openairdocs.org/sdr/CALA0100949.md): Skin · cracked · Oct 15, 2001 · N14335 · Boeing 7373T0 · Cargo/Baggage Doors
  > THIRD LIGHTENING HOLE FROM AFT END OF DOOR AND THIRD LIGHTENING HOLE FROM TOP OF DOOR HAS A CRACK. INSTALLED REPAIR PER EC/RA 5230-01630.
- [SDR CALA0100945](https://openairdocs.org/sdr/CALA0100945.md): Doubler · gouged · Oct 14, 2001 · N14335 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE PYLON UPPER LEFT SIDE OF PYLON ACCESS PANEL 5827 SUPPORT FOR PANEL HAS DEEP GOUGES. BLENDED AREA. INSTALLED DOUBLER PER EC/RA 5430-01230.
- [SDR CALA0100939](https://openairdocs.org/sdr/CALA0100939.md): Sill · corroded · Oct 10, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FORWARD LOWER SILL CORRODED AT STA 767-787, S26R. THE SILL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100938](https://openairdocs.org/sdr/CALA0100938.md): Cargo Track · corroded · Oct 10, 2001 · N14335 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT TIE DOWN CHANNEL CORRODED AROUND FASTENERS AT STA 500A-500D IN FORWARD BAGGAGE BIN. THE TIE DOWN CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100937](https://openairdocs.org/sdr/CALA0100937.md): Seat Track · cracked · Oct 10, 2001 · N14335 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 2 INCH CRACK COMING FROM HI-LOC HOLE IN BOTH THE RT AND LT O/B FLOOR TRACKS AT STA 727B. BOTH FLOOR TRACKS WERE REPAIRED IAW ECRA 5310-04202.
- [SDR CALA0100935](https://openairdocs.org/sdr/CALA0100935.md): Doubler · damaged · Oct 6, 2001 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN DOUBLER TORN IN TWO LOCATIONS AT EXHAUST DUCT ATTACH POINT IN E&E COMPARTMENT BELLY OF AIRCRAFT. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100928](https://openairdocs.org/sdr/CALA0100928.md): Floorbeam · corroded · Oct 3, 2001 · N14335 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 947.5, LBL 6 TO RBL 6. THE FLOORBEAM UPPER CAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100925](https://openairdocs.org/sdr/CALA0100925.md): Floorbeam · corroded · Oct 3, 2001 · N14335 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 294, RBL 53. THE FLOORBEAM UPPER SURFACE WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA0100921](https://openairdocs.org/sdr/CALA0100921.md): Fitting · corroded · Oct 2, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY MOUNT FITTINGS ON FLOORBEAM CORRODED AT STA 270-294, RBL 43 AND AT STA 294, RBL 12. THE TWO GALLEY MOUNT FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100919](https://openairdocs.org/sdr/CALA0100919.md): Angle · corroded · Oct 2, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FWD LAV WALL MOUNT L-ANGLES ON HAT SECTION CORRODED AT STA 302, LBL 36-56 AND AT STA 306, LBL12-43. NEW ANGLES WERE INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100920](https://openairdocs.org/sdr/CALA0100920.md): Channel · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FWD LAV WALL HAT SECTION CORRODED AT STA 306, LBL 36-56. THE HAT SECTION WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0100918](https://openairdocs.org/sdr/CALA0100918.md): Channel · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND U-CHANNEL UNDER L-1 DOOR THRESHOLD CORRODED AT STA 312-344. THE CHANNEL WAS REPLACED IAW SRM 51-40-00.
- [SDR CALA0100917](https://openairdocs.org/sdr/CALA0100917.md): Seat Track · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52.
- [SDR CALA0100916](https://openairdocs.org/sdr/CALA0100916.md): Fitting · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOOR GIRT BAR LATCH ATTACH FITTING CORRODED AT STA 344. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100915](https://openairdocs.org/sdr/CALA0100915.md): Angle · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE BELOW SCUFF PLATE AREA OF R-1 DOOR JAMB CORRODED AT STA 298-328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100914](https://openairdocs.org/sdr/CALA0100914.md): Stiffener · cracked · Oct 1, 2001 · N14335 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND AN 8" CRACK IN STIFFENER LOCATED JUST FORWARD OF HORSE COLLAR IN #6 FLAP TRACK FAIRING. THE STIFFENER WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0100913](https://openairdocs.org/sdr/CALA0100913.md): Angle · corroded · Oct 1, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOORWAY ANGLE CORRODED AT STA 312-344, LBL 60. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100912](https://openairdocs.org/sdr/CALA0100912.md): Stiffener · cracked · Oct 1, 2001 · N14335 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100911](https://openairdocs.org/sdr/CALA0100911.md): Splice · cracked · Oct 1, 2001 · N14335 · Boeing 7373T0 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 5" CRACK IN #3 FLAP TRACK FAIRING SPLICE. THE #3 FAIRING SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100908](https://openairdocs.org/sdr/CALA0100908.md): Skin · cracked · Sep 30, 2001 · N14335 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-1, FIGURE 210.
- [SDR CALA0100906](https://openairdocs.org/sdr/CALA0100906.md): Angle · cracked · Sep 28, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2" CRACK IN INTERCOSTAL UPPER ANGLE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100905](https://openairdocs.org/sdr/CALA0100905.md): Stringer · cracked · Sep 28, 2001 · N14335 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 6" CRACK IN STRINGER 10R AT STA 338. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100904](https://openairdocs.org/sdr/CALA0100904.md): Floor Support · cracked · Sep 28, 2001 · N14335 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 967-986.5, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N14335-2013-03-21/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 = 'N14335' AND deregistration_id = 'N14335-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14335-2013-03-21/reports

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