# Service difficulty reports: N17329, cancelled Mar 21, 2013

A list on [N17329, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N17329-2013-03-21.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 · 67 reports

- [SDR CALA0800487](https://openairdocs.org/sdr/CALA0800487.md): Skin · cracked · May 25, 2008 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > APPROXIMATELY.75 INCH SKIN CRACK NOTED RT FUSELAGE 2.5 INCH BELOW AND 15 INCH AFT OF EMERGENCY EXIT LIGHT, JUST AFT OF WHEEL WELL STATION 727E STRINGER 23R. REPAIRED IAW SRM 53-00-01 REPAIR 31.
- [SDR CALA0800312](https://openairdocs.org/sdr/CALA0800312.md): Door Frame · cracked · Apr 7, 2008 · N17329 · Boeing 7373T0 · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT DOOR CUTOUT, AFT FRAME SHOWS CRACK INDICATION WITH HFEC AT LOWER STOP UPPER AREA. REMOVED AND REPLACED FWD CARGO AFT DOOR CUTOUT FRAME PER SRM 51-40-02.
- [SDR CALA0700235](https://openairdocs.org/sdr/CALA0700235.md): Skin · cracked · May 5, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIRED IAW SRM 53-10-01. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT.
- [SDR CALA0700234](https://openairdocs.org/sdr/CALA0700234.md): Skin · cracked · May 4, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN FORWARD OF R-2 DOOR BETWEEN UPPER AND LOWER HINGES AT STA 950. THE INNER SKIN WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0700230](https://openairdocs.org/sdr/CALA0700230.md): Skin · corroded · May 4, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN BENEATH NR 1 DME ANTENNA CORRODED AT STA 460, S29L. THE CORRODED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5331-01305. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT 60,000 FLIGHT CYCLES THEN EVERY 30,000 FL
- [SDR CALA0700228](https://openairdocs.org/sdr/CALA0700228.md): Skin · cracked · May 3, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
- [SDR CALA0700227](https://openairdocs.org/sdr/CALA0700227.md): Frame · corroded · May 3, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 500 BETWEEN STRINGER 26L AND 27L. A SHEAR TIE AND FILLER WERE INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700225](https://openairdocs.org/sdr/CALA0700225.md): Skin · cracked · May 2, 2007 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR LOWER HINGE CUTOUT FWD LOWER CORNER, STA 947.5, S13R TO S14R. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01.
- [SDR CALA0500451](https://openairdocs.org/sdr/CALA0500451.md): Wire Harness · burned · Dec 16, 2005 · N17329 · Boeing 7373T0 · Electrical Power System Wiring
  > LT WING BODY OVERHEAT LIGHT, FLAP IND SHOWED RT FLAP RETRACTED, LT FLAP 0700 POSITION. PRESSURIZATION AUTO FAIL LIGHT ILLUM. EMERGENCY DESCENT. M1205 ELEMENT REMOVED & REPLACED FOR OVERHEAT CONDITION, T/E FLAP POSITION IND REPLACED FOR LOCKOUT ISSUE, PRESSU
- [SDR CALA0400744](https://openairdocs.org/sdr/CALA0400744.md): Skin · cracked · Dec 17, 2004 · N17329 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND TWO 0.3 INCH CRACKS AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01056.
- [SDR CALA0400743](https://openairdocs.org/sdr/CALA0400743.md): Skin · cracked · Dec 17, 2004 · N17329 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.3 INCH CRACK AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01057.
- [SDR CALA0400742](https://openairdocs.org/sdr/CALA0400742.md): Frame · corroded · Dec 10, 2004 · N17329 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN FORWARD CARGO PIT AT STA 500D BETWEEN S27L AND S28L. INSTALLED REPAIR IAW SRM 53-00-07, FIGURE 205.
- [SDR CALA0400737](https://openairdocs.org/sdr/CALA0400737.md): Stiffener · corroded · Dec 4, 2004 · N17329 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND APB BOTTOM CENTER STIFFENER CORRODED ON LEFT HALF, BS 1016-1020. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW ECRA 5311-01213.
- [SDR CALA0400746](https://openairdocs.org/sdr/CALA0400746.md): Angle · corroded · Dec 3, 2004 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991.5, RBL 46 TO LBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400736](https://openairdocs.org/sdr/CALA0400736.md): Seat Track · corroded · Dec 3, 2004 · N17329 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN RIGHT I/B SEAT TRACK CORRODED AT STA 328-355, BL 0 TO RBL 23. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 202.
- [SDR CALA0400735](https://openairdocs.org/sdr/CALA0400735.md): Seat Track · corroded · Dec 3, 2004 · N17329 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 328-360, RBL 48 TO LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0400733](https://openairdocs.org/sdr/CALA0400733.md): Galley Track · corroded · Dec 3, 2004 · N17329 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 275-294, RBL 43. A NEW FLOOR TRACK SECTION WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300313](https://openairdocs.org/sdr/CALA0300313.md): Strap · corroded · Jun 14, 2003 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN STRAP CORRODED BETWEEN STA 777 AND 847, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300312](https://openairdocs.org/sdr/CALA0300312.md): Floor Support · corroded · Jun 13, 2003 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 8 AND LBL 12. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5320-01603.
- [SDR CALA0300311](https://openairdocs.org/sdr/CALA0300311.md): Skin · cracked · Jun 12, 2003 · N17329 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.25 INCH CRACK ON LIP OF HOLE CUT ON O/B SIDE OF ACCESS PANEL 5727L OF NR 1 PYLON. REPAIRED ACCESS PANEL IAW ECRA 5430-01230.
- [SDR CALA0300310](https://openairdocs.org/sdr/CALA0300310.md): Pressure Panel · cracked · Jun 12, 2003 · N17329 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN MAIN WHEEL WELL PRESSURE DECK AT STA 673, LBL 31. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.
- [SDR CALA0300309](https://openairdocs.org/sdr/CALA0300309.md): Floor Support · corroded · Jun 12, 2003 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, LBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.
- [SDR CALA0300308](https://openairdocs.org/sdr/CALA0300308.md): Floor Support · corroded · Jun 11, 2003 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CORRODED AT STA 767, RBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5320-01603.
- [SDR CALA0300303](https://openairdocs.org/sdr/CALA0300303.md): Strap · corroded · Jun 10, 2003 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT STRAP CORRODED AT STA 727E, LBL 21. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0100424](https://openairdocs.org/sdr/CALA0100424.md): Arm · out of adj · Apr 26, 2001 · N17329 · Boeing 7373T0 · Passenger/Crew Doors
  > L1 DOOR WILL NOT CLOSE. ADJUSTED L1 DOOR GUIDE ARM. OPS CHECK OK.
- [SDR CALA0100231](https://openairdocs.org/sdr/CALA0100231.md): Skin · cracked · Mar 14, 2001 · N17329 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5230-01604.
- [SDR CALA0100223](https://openairdocs.org/sdr/CALA0100223.md): Skin · gouged · Mar 13, 2001 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED AT L-1 DOOR TORQUE TUBE UPPER HINGE AREA, BS 312, S13L. THE GOUGED AREA OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED.
- [SDR CALA0100222](https://openairdocs.org/sdr/CALA0100222.md): Skin · gouged · Mar 12, 2001 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 395, STRINGER 20-21R. A DOUBLER WAS INSTALLED.
- [SDR CALA0100215](https://openairdocs.org/sdr/CALA0100215.md): Frame · cracked · Mar 8, 2001 · N17329 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807 BETWEEN STRINGER 27L AND 27R. A REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0100212](https://openairdocs.org/sdr/CALA0100212.md): Web · cracked · Mar 7, 2001 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR JAMB LOWER FORWARD INSIDE CORNER WEB AT STA 440, S25. REPAIRED WEB IAW SRM 51-70-13, FIGURE 1.
- [SDR CALA0100193](https://openairdocs.org/sdr/CALA0100193.md): Rib · gouged · Mar 2, 2001 · N17329 · Boeing 7373T0 · Vertical Stabilizer, Spar/Rib
  > INSPECTION FOUND L/E RIB OF VERTICAL STABILIZER GOUGED AT STA 10-40. THE DORSAL FIN RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0100186](https://openairdocs.org/sdr/CALA0100186.md): Fitting · cracked · Mar 1, 2001 · N17329 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING MLG SUPPORT BEAM O/B ATTACH FITTING AT AFT SPAR. A NEW FITTING WAS INSTALLED IAW WORK CARD 03-5743-1-0003.
- [SDR CALA0100165](https://openairdocs.org/sdr/CALA0100165.md): Floor Support · corroded · Feb 25, 2001 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 967-986, LBL 18.32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9900145](https://openairdocs.org/sdr/CALA9900145.md): Intercostal · cracked · Feb 12, 1999 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND A REPAIR INTERCOSTAL AND REPAIR PARTS WERE INSTALLED IAW EA 5363-01014.
- [SDR CALA9900133](https://openairdocs.org/sdr/CALA9900133.md): Intercostal · cracked · Feb 11, 1999 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 947.5, BELOW CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9900132](https://openairdocs.org/sdr/CALA9900132.md): Skin · cracked · Feb 11, 1999 · N17329 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE SKIN OF UPPER WINDOW POST AT CAPTAIN'S NR 2 SLIDING WINDOW. A REPAIR WAS INSTALLED IAW ECRA 5330-02769.
- [SDR CALA9900129](https://openairdocs.org/sdr/CALA9900129.md): Panel · cracked · Feb 11, 1999 · N17329 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 1 CRACK IN LT WING NR 3 SLAT PANEL AT FASTENER I/B OF SLAT ACTUATOR. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C30133.
- [SDR CALA9701681](https://openairdocs.org/sdr/CALA9701681.md): Fuel Pump · inoperative · Nov 28, 1997 · N17329 · Boeing 7373T0 · Engine Fuel Pump
  > THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT. THE LOW IDLE LIGHT AND NR 2 GEN BUS OFF LIGHT ILLUMINATED AND THEN THE NR 2 LOW OIL PRESSURE LIGHT CAME ON. THE APU WAS STARTED AND NR 2 BUS WAS PUT ON LINE. ENGINE RESTART WAS PERFORMED, BUT THE ENGINE WOULD NOT
- [SDR CALA9700335](https://openairdocs.org/sdr/CALA9700335.md): Chord · cracked · Feb 22, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FAIL SAFE CHORD AT STA 520, RBL 24.50. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9700334](https://openairdocs.org/sdr/CALA9700334.md): Floorbeam · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 328 BETWEEN RBL 12 AND RT SIDE AND BETWEEN RBL 12 AND LT SIDE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51, FIGURE 205.
- [SDR CALA9700333](https://openairdocs.org/sdr/CALA9700333.md): Floorbeam · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 294 BETWEEN LBL 12 AND RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9700332](https://openairdocs.org/sdr/CALA9700332.md): Floorbeam · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 344 BETWEEN LBL 12 AND LT SIDEWALL. THE CORRODED AREA WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9700331](https://openairdocs.org/sdr/CALA9700331.md): Floorbeam · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 312 BETWEEN LBL 12 AND RT SIDEWALL. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9700326](https://openairdocs.org/sdr/CALA9700326.md): Support · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT LBL 12 BETWEEN B.S. 312-328 AND BETWEEN B.S. 328-344. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03439.
- [SDR CALA9700325](https://openairdocs.org/sdr/CALA9700325.md): Support · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED BETWEEN B.S. 294.5 AND 312 AT RBL 12 AND RBL 14. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-10-02.
- [SDR CALA9700324](https://openairdocs.org/sdr/CALA9700324.md): Angle · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE CORRODED BETWEEN B.S. 294.5 AND 328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA9700323](https://openairdocs.org/sdr/CALA9700323.md): Angle · corroded · Feb 21, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT L-ANGLE UNDER R-2 DOOR CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9700330](https://openairdocs.org/sdr/CALA9700330.md): Angle · cracked · Feb 20, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SUPPORT ANGLE AT STA 540, STRINGER 22. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA9700329](https://openairdocs.org/sdr/CALA9700329.md): Fairing Support · cracked · Feb 20, 1997 · N17329 · Boeing 7373T0 · Aerodynamic Fairings
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. A.25 INCH CRACK WAS FOUND IN LT WING TO BODY FAIRING SUPPORT AT STA 540, STRINGER 22. THE SUPPORTS WERE REPAIRED IAW ECRA 5350-01227.
- [SDR CALA9700328](https://openairdocs.org/sdr/CALA9700328.md): Support · cracked · Feb 20, 1997 · N17329 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, AIRCRAFT CENTERLINE, LT SIDE. THE ANGLE WAS REPAIRED IAW SRM 51-70-11.

Next page: https://openairdocs.org/deregistered/N17329-2013-03-21/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 = 'N17329' AND deregistration_id = 'N17329-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17329-2013-03-21/reports

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