# Service difficulty reports: N14609, cancelled Aug 7, 2009

A list on [N14609, cancelled Aug 7, 2009](https://openairdocs.org/deregistered/N14609-2009-08-07.md).

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

- [SDR CALA0700442](https://openairdocs.org/sdr/CALA0700442.md): Attach Fitting · cracked · Aug 18, 2007 · N14609 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN ATTACHMENT CLIP AT STA 360, S11L. A REPAIR WAS INSTALLED IAW ECRA 5311-01352.
- [SDR CALA0700432](https://openairdocs.org/sdr/CALA0700432.md): Frame · cracked · Aug 13, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 867 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700429](https://openairdocs.org/sdr/CALA0700429.md): Frame · cracked · Aug 13, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 827 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700433](https://openairdocs.org/sdr/CALA0700433.md): Beltframe · cracked · Aug 12, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN BELT FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700431](https://openairdocs.org/sdr/CALA0700431.md): Frame · cracked · Aug 12, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT STA 827, S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700430](https://openairdocs.org/sdr/CALA0700430.md): Frame · cracked · Aug 12, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT STA 867 BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700425](https://openairdocs.org/sdr/CALA0700425.md): Frame · cracked · Aug 12, 2007 · N14609 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT BRACKET ATTACH RIVET, STA 787, S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.
- [SDR CALA0700417](https://openairdocs.org/sdr/CALA0700417.md): Floorbeam · corroded · Aug 10, 2007 · N14609 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT STA 986.5, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGE 201-204.
- [SDR CALA0600319](https://openairdocs.org/sdr/CALA0600319.md): Battery Pack · discharged · Aug 3, 2006 · N14609 · Boeing 737524 · Emergency Lighting
  > INSPECTION REPORTED THAT -HALF- OF THE PASSENGER CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING A S-CHECK IN EWR. A NEW BATTERY PACK WAS INSTALLED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0500131](https://openairdocs.org/sdr/CALA0500131.md): Floorbeam · corroded · Apr 26, 2005 · N14609 · Boeing 737524 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT STA 986.5 AND LBL 43. INSTALLED DOUBLER PER ECRA 5321-01211.
- [SDR CALA0500088](https://openairdocs.org/sdr/CALA0500088.md): Floorbeam · corroded · Mar 25, 2005 · N14609 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND THE MAIN CABIN FLOORBEAM CORRODED AT STA 986.5, LBL 43. REPAIRED IAW ECRA 5321-01211.
- [SDR CALA0500077](https://openairdocs.org/sdr/CALA0500077.md): Seat Track · corroded · Mar 18, 2005 · N14609 · Boeing 737524 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 360-375, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0300512](https://openairdocs.org/sdr/CALA0300512.md): Wire Harness · broken · Sep 3, 2003 · N14609 · Boeing 737524 · Light System Wiring
  > INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 12ABC DUE TO A BROKEN WIRE. THE EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS WAS REPLACED. OPERATION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS RESTORED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-
- [SDR CALA0300511](https://openairdocs.org/sdr/CALA0300511.md): Skin · gouged · Sep 3, 2003 · N14609 · Boeing 737524 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN REPAIR PLATE GOUGED AT STA 980 UNDER L-2 DOOR. THE REPAIR PLATE WAS REMOVED AND A NEW REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, PAGE 204-206.
- [SDR CALA0200556](https://openairdocs.org/sdr/CALA0200556.md): Keelbeam · worn · Nov 21, 2002 · N14609 · Boeing 737524 · Fuselage Main, Keel
  > INSPECTION FOUND DEEP WEAR ON KEEL BEAM AT BS 710-727, RBL 8 (LOWER FILLET PANEL ATTACH FLANGE). A FILLER AND STRAP REPAIR WAS INSTALLED IAW ECRA 5311-01143.
- [SDR CALA0200554](https://openairdocs.org/sdr/CALA0200554.md): Web · cracked · Nov 15, 2002 · N14609 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2" CRACK IN MAIN DECK WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0000719](https://openairdocs.org/sdr/CALA0000719.md): Floorbeam · gouged · May 19, 2000 · N14609 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM GOUGED IN SEVERAL PLACES AT BS 986, RBL 15 - RBL 30. A REPAIR WAS INSTALLED IAW ECRA 5360-01040.
- [SDR CALA9900568](https://openairdocs.org/sdr/CALA9900568.md): Sensor · out of adjust · May 23, 1999 · N14609 · Boeing 737524 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WHEN RETRACTING FLAPS THE TAKEOFF WARNING HORN SOUNDED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR GAP OUT OF TOLERANCE. THE SENSOR WAS ADJUST

## 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 = 'N14609' AND deregistration_id = 'N14609-2009-08-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14609-2009-08-07/reports

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