# Service difficulty reports: N14604, cancelled Dec 13, 2012

A list on [N14604, cancelled Dec 13, 2012](https://openairdocs.org/deregistered/N14604-2012-12-13.md).

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

- [SDR CALA2012110100716](https://openairdocs.org/sdr/CALA2012110100716.md): Skin · dented · Nov 1, 2012 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED 4 INCHES BELOW L1 DOOR BETWEEN BS 312 AND 340. REPAIRED IAW ECRA 5331-01649, REV A.
- [SDR CALA2012110100704](https://openairdocs.org/sdr/CALA2012110100704.md): Skin · dented · Oct 31, 2012 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BETWEEN BS 189 AND 195 AT BL 0. R & R DAMAGED INTERNAL BUTT SPLICE IAW DWG 65C27 793 AND SRM 51-10-02 AND SRM 51-40-02.
- [SDR CALA2012101700666](https://openairdocs.org/sdr/CALA2012101700666.md): Skin · damaged · Oct 16, 2012 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A 2.5 BY 2.5 INCH HOLE BETWEEN BS 807 AND 827 APPROX 5 INCHES BELOW STR 18 LT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW ECRA 5331-01645.
- [SDR CALA2011022500109](https://openairdocs.org/sdr/CALA2011022500109.md): Transducer · failed · Feb 24, 2011 · N14604 · Boeing 737524 · Brake Anti-Skid Section
  > ANTI SKID INOP LIGHT ON FORWARD PANEL ILLUMINATED IN-FLIGHT. WENT OUT PRIOR TO LANDING. PREVIOUS HISTORY. RAN QRH. REMOVED AND REPLACED NR 3 MAIN WHEEL TRANSDUCER IAW MM 32-42-11. OPS CHECKED GOOD. NO OTHER DEFECT NOTED AT THIS TIME. ROTABLE PARTS CHANG
- [SDR CALA2010041400136](https://openairdocs.org/sdr/CALA2010041400136.md): Frame · cracked · Apr 13, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > MAIN FRAME CRACKED STA 616 RT SIDE JUST ABOVE FUEL TANK. REPAIRED MAIN FRAME AT STA 616 RT JUST ABOVE FUEL TANK REF ECRA 5311-01487. HOWEVER, WITHIN 9000 FLIGHT CYCLES AND AT INTERVALS NOT TO EXCEED 9000 FLIGHT CYCLES THEREAFTER, PERFORM AN INSPECTION PER PA
- [SDR CALA2010041200131](https://openairdocs.org/sdr/CALA2010041200131.md): Skin · cracked · Apr 10, 2010 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK FWD ENTRY DOOR LWR HINGE CUTOUT HAS CRACK INDICATION AT 2EA FASTENERS HOLE (MARKED) JUST BELOW WL 236.68 AND FWD OF STA 303.90 REF TASK INSTRUCTION ITEM 20.0 OF EA 5330-037 36 REV B -OPERATION 03. INSTALLED REPAIR REF EC/RA 5330-04014.
- [SDR CALA2010041200130](https://openairdocs.org/sdr/CALA2010041200130.md): Skin · cracked · Apr 9, 2010 · N14604 · Boeing 737524 · Passenger/Crew Doors
  > L-1 DOOR AFT SIDE INNER SKIN & REINFORCEMENT STRIP CRACKED AT 4TH STOP PIN MOUNT FROM BOTTOM REPAIR ACCOMPLISHED PER ECRA 5210-02149.
- [SDR CALA2010040600125](https://openairdocs.org/sdr/CALA2010040600125.md): Skin · cracked · Apr 6, 2010 · N14604 · Boeing 737524 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB, LOWER T/E SKIN NEAR AFT SPAR, STAB STA 125.00 APPROX APPEARS TO BE CRACKED. TRIMMED OUT CRACKED SECTION OF SKIN AND INSTALLED FILLER AND REPAIR DOUBLER FROM STAB STA 111 TO STA 166, SEALED REPAIR AND RESTORED FINISH PER ECRA 5510-01616 RE
- [SDR CALA2010040600122](https://openairdocs.org/sdr/CALA2010040600122.md): Frame · corroded · Apr 5, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 907 BETWEEN STR 21R - STR 22R AT SKIN ATTACH POINT. INSTALLED FRAME REPAIR AT SKIN ATTACHMENT REF SRM 53-00-07, ATTACH HEAT TREAT FORM 43.0150 AND 44.0008.
- [SDR CALA2010040600120](https://openairdocs.org/sdr/CALA2010040600120.md): Beam · corroded · Apr 5, 2010 · N14604 · Boeing 737524 · Fuselage Miscellaneous Structure
  > AFT CARGO STA 907 RT AFT SIDE OF BEAM SKIN HAVE CORROSION. REPLACED SKIN SPLICE, SRM 51-40-02.
- [SDR CALA2010040600119](https://openairdocs.org/sdr/CALA2010040600119.md): Skin · corroded · Apr 5, 2010 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > STA 907 LT AFT SIDE OF BEAM, SKIN HAVE CORROSION BETWEEN STR 19 LT AND 24 LT CTN 53-310-218. REMOVED AND REPLACED SPLICE STRAP AT STA 907 STR 19-24 LT REF SRM 51-40-02.
- [SDR CALA2010040500113](https://openairdocs.org/sdr/CALA2010040500113.md): Skin · corroded · Apr 1, 2010 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT DOOR CUTOUT AFT LWR CORNER HAS DEEP CORROSION. INSTALLED REPAIR DOUBLER AT DAMAGED AREA PER SRM 53-00-01 REPAIR 32.
- [SDR CALA2010040500109](https://openairdocs.org/sdr/CALA2010040500109.md): Hinge Fitting · worn · Mar 30, 2010 · N14604 · Boeing 737524 · Spoilers
  > NR 4 GROUND SPOILER O/B HINGE FITTING WORN (ON WING). REMOVED AND REPLACED FITTING IN REF TO SRM 51-40-02.
- [SDR CALA2010032400098](https://openairdocs.org/sdr/CALA2010032400098.md): Frame · cracked · Mar 22, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 727A BETWEEN STR 8&9 RT. INSTALLED REPAIR ANGLES A&B PER EA 5310-04498 OP 02.
- [SDR CALA2010032400097](https://openairdocs.org/sdr/CALA2010032400097.md): Frame · cracked · Mar 22, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 867 BETWEEN STR 8&9 RT. REPAIRED CRACKED FRAME PER EA 5310-04498.
- [SDR CALA2010032400096](https://openairdocs.org/sdr/CALA2010032400096.md): Frame · cracked · Mar 22, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK, FUSELAGE FRAME CRACKED AT STA 827 BETWEEN STR 8 & 9 LT. REPAIRED FRAME AT STA 827 LT BETWEEN STR 8& STR 9 PER ECRA 5311-01484. DIP GENERATED ON L/P 9715509.
- [SDR CALA2010032400095](https://openairdocs.org/sdr/CALA2010032400095.md): Frame · cracked · Mar 22, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 747 BETWEEN STR 8 & 9 RT. REPAIRED FRAME AT STA 747 BETWEEN STR 8 & 9 RT. REF EA 5310-04498, DIP GENERATED ON NON-ROUTINE LG PG 9715509 SEQ N00700.
- [SDR CALA2010032200094](https://openairdocs.org/sdr/CALA2010032200094.md): Angle · corroded · Mar 21, 2010 · N14604 · Boeing 737524 · Passenger/Crew Doors
  > L1 DOOR L-ANGLE HAS CORROSION STA 312 TO 344. INSTALLED NEW L-ANGLE ON L-1 REF SRM 51-40-02.
- [SDR CALA2010032200091](https://openairdocs.org/sdr/CALA2010032200091.md): Frame · cracked · Mar 19, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 787 BETWEEN STR 8&9LT (SEE ATTACHED FORMS 44.0008). REPAIRED FUSELAGE FRAME AT STA 787 BETWEEN STR 8&9LT PER EA 5310-04498.
- [SDR CALA2010032200089](https://openairdocs.org/sdr/CALA2010032200089.md): Frame · cracked · Mar 19, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 727B BETWEEN STR 8 & 9 RT. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER ANGLES REF EA 5310-04498 (SEE ATTACHED.0008 FORMS).
- [SDR CALA2010032200088](https://openairdocs.org/sdr/CALA2010032200088.md): Frame · cracked · Mar 19, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 400 BETWEEN STR 8&9 RT (SEE ATTACHED FORMS 44.0008 AND 43.0150). TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLES PER EA 5310-04498.
- [SDR CALA2010032200087](https://openairdocs.org/sdr/CALA2010032200087.md): Frame · cracked · Mar 18, 2010 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 380 BETWEEN STR 8& 9 RT (SEE ATTACHED FORMS 44.0008 AND 43.0150). TRIMMED OUT DAMAGE, INSTALLED REPAIR ANGLES REF EA 5310-04498.
- [SDR CALA2010031800085](https://openairdocs.org/sdr/CALA2010031800085.md): Floorbeam · corroded · Mar 18, 2010 · N14604 · Boeing 737524 · Fuselage Main, Floor Beam
  > FLOORBEAM STA 986.5 LBL 11 TO LBL 31 HAS CORROSION. INSTALLED STRAP REPAIR, TREATED AND PRIMED REF SRM 53-00-51.
- [SDR CALA0700163](https://openairdocs.org/sdr/CALA0700163.md): Angle · cracked · Apr 3, 2007 · N14604 · Boeing 737524 · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE WEB L-ANGLE AT STAB STA 83.5. A REPAIR WAS INSTALLED IAW ECRA 5510-01883.
- [SDR CALA0700162](https://openairdocs.org/sdr/CALA0700162.md): Door Frame · cracked · Apr 2, 2007 · N14604 · Boeing 737524 · Fuselage Main, Structure
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB AT LOWER DOORSTOP FITTING, WL 160, S24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700161](https://openairdocs.org/sdr/CALA0700161.md): Attach Fitting · cracked · Apr 2, 2007 · N14604 · Boeing 737524 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN ATTACHMENT CLIP AFT OF L-1 DOOR AT STA 360, STRINGER 11L. THE ATTACHMENT CLIP WAS REPLACED IAW ECRA 5311-01306. A DIP WAS CREATED TO REINSPECT THE CLIP AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES.
- [SDR CALA0700160](https://openairdocs.org/sdr/CALA0700160.md): Frame · cracked · Apr 2, 2007 · N14604 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME WEB AT LOWER DOORSTOP FITTING, STA 482, WL 160, S24L. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700155](https://openairdocs.org/sdr/CALA0700155.md): Angle · corroded · Mar 28, 2007 · N14604 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-2 DOORWAY Z-ANGLE CORRODED JUST AFT OF DOORWAY AT STA 986.5, RBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600150](https://openairdocs.org/sdr/CALA0600150.md): Wire Harness · damaged · May 5, 2006 · N14604 · Boeing 737524 · Light System Wiring
  > THE EMERGENCY LIGHT AT SEAT 24 ABC WAS FOUND INOPERATIVE. THE LIGHT HARNESS WAS REPLACED IAW MM 33-51-81.
- [SDR CALA0300446](https://openairdocs.org/sdr/CALA0300446.md): Cooling Fan · failed · Aug 6, 2003 · N14604 · Boeing 737524 · Air Distribution Fan
  > AN OBJECTIONABLE ODOR WAS DETECTED BY FLIGHT ATTENDANT AND PASSENGERS JUST PRIOR TO DESCENT INTO COS. NO SIGN OF SMOKE WAS DETECTED IN CABIN OR COCKPIT. ALL ELECTRICAL SYSTEMS AND FLUID LEVELS CHECKED NORMAL. THE AIRCRAFT LANDED AT COS WITHOUT INCIDENT. MA
- [SDR CALA0100001](https://openairdocs.org/sdr/CALA0100001.md): Engine · leaking · Jan 2, 2001 · N14604 · Boeing 737524 · Turbine Engine Oil System
  > SHORTLY AFTER TAKEOFF FROM EWR SMOKE ENTERED THE CABIN AND THE LAV SMOKE DETECTORS ACTIVATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. THE SMOKE DISSIPATED RAPIDLY ONCE ON THE GROUND. THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTEN
- [SDR CALA0000230](https://openairdocs.org/sdr/CALA0000230.md): Skin · lightning strike · Mar 2, 2000 · N14604 · Boeing 737524 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO LT LOWER FUSELAGE SKIN AT STA 727-908 AT OR BELOW PAINT LINE AND AT STA 908-1016 BELOW L17L. THE DAMAGED AREA WAS REPAIRED BY BURNISHING AND INSTALLING PLUG RIVETS IAW SRM 53-00-01, FIGURE 219.
- [SDR CALA9700439](https://openairdocs.org/sdr/CALA9700439.md): Battery Charger · inoperative · Mar 26, 1997 · N14604 · Boeing 737524 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 5 TO 9. MAINTENANCE FOUND THE M1135 BATTERY CHARGER INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED, OPERATION OF THE PATH LIGHTS WAS RESTORED.
- [SDR CAL950786](https://openairdocs.org/sdr/CAL950786.md): Eel Fuse · failed · Sep 2, 1995 · N14604 · Boeing 737524 · Emergency Lighting
  > IAH - FLT 1510 - INSPECTION FOUND MIDDLE ZONE OF AISLE PATH LIGHTING INOPERATIVE. A BLOWN FUSE WAS FOUND IN THE AFT EMERGENCY PATH LIGHTING BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X)

## 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 = 'N14604' AND deregistration_id = 'N14604-2012-12-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14604-2012-12-13/reports

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