# Service difficulty reports: N17306, cancelled Sep 23, 2004

A list on [N17306, cancelled Sep 23, 2004](https://openairdocs.org/deregistered/N17306-2004-09-23.md).

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

- [SDR CALA0300227](https://openairdocs.org/sdr/CALA0300227.md): Keelbeam · corroded · Apr 28, 2003 · N17306 · Boeing 7373T0 · Fuselage Main, Keel
  > FORWARD BAG BIN CORROSION AT STRINGER 28R STATION 500D PLUS 17 IN. REPAIR ACCOMPLISHED PER EC/RA 5310-04345.
- [SDR CALA0300242](https://openairdocs.org/sdr/CALA0300242.md): Skin · damaged · Apr 24, 2003 · N17306 · Boeing 7373T0 · Cargo/Baggage Doors
  > MAINTENANCE DISCOVERED A SMALL TRIM-OUT IN THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE. THE DAMAGED AREA WAS REPAIRED IAW ECRA 5232-01026.
- [SDR CALA0300206](https://openairdocs.org/sdr/CALA0300206.md): Web · corroded · Apr 21, 2003 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAG BIN THRESHOLD WEB CORRODED IN SEVERAL SPOTS. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300204](https://openairdocs.org/sdr/CALA0300204.md): Cargo Track · cracked · Apr 19, 2003 · N17306 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 4 INCH CRACK IN RT TIE DOWN RAIL AT STA 492. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300203](https://openairdocs.org/sdr/CALA0300203.md): Plate · corroded · Apr 18, 2003 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE NR 3 COMMUNICATION ANTENNA ATTACHMENT/MOUNTING PLATE CORRODED AROUND RIVETS NEXT TO COAX CONNECTOR AT STA 727D, BL 0. A NEW ANTENNA MOUNT PLATE WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300201](https://openairdocs.org/sdr/CALA0300201.md): Channel · corroded · Apr 18, 2003 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHANNEL CORRODED AT DRAIN MAST, STA 986-1006, L26L TO L27L. THE CHANNEL WAS REPAIRED IAW SRM 51-40-2.
- [SDR CALA0300199](https://openairdocs.org/sdr/CALA0300199.md): Structure · cracked · Apr 17, 2003 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN SUBFLOOR AT STA 1024, RBL 10. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200548](https://openairdocs.org/sdr/CALA0200548.md): Wire · shorted · Nov 13, 2002 · N17306 · Boeing 7373T0 · Emergency Lighting
  > WHEN THE EMERGENCY EXIT LIGHT SWITCH IN OVERHEAD WAS PUT IN ARM POSITION THE LIGHTS CAME ON. MAINTENANCE FOUND A SHORTED POWER WIRE AT EMERGENCY LIGHT BATTERY PACK(M9100) STA 378, REFERENCE WDM 33-51-01. REPAIRED WIRE AND EMERGENCY LIGHT OPERATION CHECKED GOOD
- [SDR CALA0100933](https://openairdocs.org/sdr/CALA0100933.md): Skin · cracked · Oct 5, 2001 · N17306 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1/4" CRACK AT LIGHTENING HOLE OF C-2 DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01629.
- [SDR CALA0100932](https://openairdocs.org/sdr/CALA0100932.md): Skin · cracked · Oct 4, 2001 · N17306 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1/2" CRACK AT LIGHTENING HOLE IN C-2 DOOR INNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01627.
- [SDR CALA0100930](https://openairdocs.org/sdr/CALA0100930.md): Fitting · cracked · Oct 4, 2001 · N17306 · Boeing 7373T0 · Fuselage, Door Hinge
  > INSPECTION FOUND A 2" CRACK IN L-2 DOOR LOWER HINGE FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100929](https://openairdocs.org/sdr/CALA0100929.md): Skin · cracked · Oct 4, 2001 · N17306 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1.25" CRACK IN R/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL AT REAR SPAR STA 129. AN INTERIM AIRWORTHY REPAIR WAS INSTALLED IAW ECRA 5510-01601. A DIP WAS ISSUED TO REINSPECT THE AREA AT INTERVALS NOT TO EXCEED 3000 FLIGHT HOU
- [SDR CALA0100923](https://openairdocs.org/sdr/CALA0100923.md): Web · cracked · Oct 2, 2001 · N17306 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3" CRACK IN C-1 DOOR FWD AND AFT LOWER WEBS. A REPAIR WAS INSTALLED AT EACH LOCATION IAW W/C JA 5230-0103006001.
- [SDR CALA0100922](https://openairdocs.org/sdr/CALA0100922.md): Frame · cracked · Oct 2, 2001 · N17306 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 4" CRACK IN C-1 DOOR AFT LOWER FRAME. A NEW FRAME WAS INSTALLED IAW W/C JA 5230-0103007001.
- [SDR CALA0100909](https://openairdocs.org/sdr/CALA0100909.md): Clip · corroded · Sep 30, 2001 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SKIN CLIP CORRODED AT STA 500D BETWEEN STRINGER 27L AND 28L. A REPAIR CLIP WAS INSTALLED IAW SRM 53-00-07, FIGURE 210.
- [SDR CALA0100903](https://openairdocs.org/sdr/CALA0100903.md): Skin · cracked · Sep 28, 2001 · N17306 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 5/8" CRACK IN #2 ENGINE PYLON SKIN ACCESS PANEL #5827R CUTOUT. REPAIRED IAW ECRA 5430-01230.
- [SDR CALA0100453](https://openairdocs.org/sdr/CALA0100453.md): Control Handle · lack of lube · May 8, 2001 · N17306 · Boeing 7373T0 · Landing Gear Selector
  > WHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO SAT THE THREE GEAR GREEN LIGHTS AND THREE RED LIGHTS ILLUMINATED. A MANUAL GEAR EXTENSION WAS PERFORMED DURING A GO-AROUND AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCI
- [SDR CALA9900541](https://openairdocs.org/sdr/CALA9900541.md): Support · corroded · May 14, 1999 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > RIGHT LAVATORY FLOOR SUPPORT CORRODED BS 1006-APB RBL18. REPLACED RIGHT AFT LAV FLOOR SUPPORT PER SRM 51-10-2.
- [SDR CALA9900493](https://openairdocs.org/sdr/CALA9900493.md): Floorbeam · corroded · May 9, 1999 · N17306 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT (CABIN) HAS CORROSION AT STA 951 RBL 47. REPLACED PER EC/RA 5310-03585.
- [SDR CALA9900491](https://openairdocs.org/sdr/CALA9900491.md): Post · cracked · May 7, 1999 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CAPTAINS WIND SHIELD OUTBOARD UPPER CORNER OF POST HAS.375 INCH CRACK. INSTALLED REPAIR DOUBLERS AND FILLER PER EC/RA 5330-02806.
- [SDR CALA9900501](https://openairdocs.org/sdr/CALA9900501.md): Angle · corroded · May 6, 1999 · N17306 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > R2 DOOR THRESHOLD Z ANGLE CORRODED STA 907 - 986. REMOVED AND REPLACED R-2 Z ANGLE PER SRM 51-10-02.
- [SDR CALA9900458](https://openairdocs.org/sdr/CALA9900458.md): Seat Track · corroded · May 2, 1999 · N17306 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > HOU - LEFT INBOARD CABIN SEAT TRACK HAS CORROSION AT STA 907 TO STA 947. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 53-00-52 FIG 204. (X)
- [SDR CALA9900459](https://openairdocs.org/sdr/CALA9900459.md): Seat Track · corroded · Apr 30, 1999 · N17306 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > HOU - CABIN SEAT TRACK LEFT OUTBOARD CORRODED AT STA 370. FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-00-52. (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 = 'N17306' AND deregistration_id = 'N17306-2004-09-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17306-2004-09-23/reports

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