# Service difficulty reports: N17344, cancelled Mar 21, 2013

A list on [N17344, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N17344-2013-03-21.md).

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

- [SDR CALA0600288](https://openairdocs.org/sdr/CALA0600288.md): Skin · cracked · Aug 1, 2006 · N17344 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2" CRACK IN AFT CARGO DOOR INNER SKIN AT LOWER FORWARD LIGHTENING HOLE CUTOUT. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01078.
- [SDR CALA0600287](https://openairdocs.org/sdr/CALA0600287.md): Skin · cracked · Aug 1, 2006 · N17344 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.4" CRACK IN C-2 DOOR SKIN AT LIGHTENING HOLE APPROXIMATELY 21 INCHES DOWN FROM UPPER DOOR FRAME AND 18 INCHES FORWARD OF AFT DOOR FRAME. THE SKIN WAS REPAIRED IAW ECRA 5232-01077.
- [SDR CALA0600277](https://openairdocs.org/sdr/CALA0600277.md): Stringer · cracked · Jul 29, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN STRINGER 14L AT L-1 DOOR, STA 360-380. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02 AND ECRA 5311-01262.
- [SDR CALA0600276](https://openairdocs.org/sdr/CALA0600276.md): Stringer · cracked · Jul 29, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN S15L AT L-1 DOOR AFT SIDE, STA 360-380. THE STRINGER U CHANNEL WAS REMOVED AND REPLACED IAW ECRA 5311-01262.
- [SDR CALA0600272](https://openairdocs.org/sdr/CALA0600272.md): Beltframe · corroded · Jul 26, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CORRODED AT STA 500C, S26L-27L, LBL 17 - LBL 22. A SHEAR TIE REPAIR ANGLE AND FILLER WERE INSTALLED IAW SRM 53-00-07, REPAIR 1, FIGURE 201.
- [SDR CALA0600271](https://openairdocs.org/sdr/CALA0600271.md): Shear Tie · corroded · Jul 26, 2006 · N17344 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND CORROSION AROUND CLIP AT STA 500D BETWEEN S26L AND S27L, LBL 17-22. A SHEAR TIE REPAIR AND FILLER WERE INSTALLED IAW SRM 53-00-07, REPAIR 2, FIGURE 201.
- [SDR CALA0600264](https://openairdocs.org/sdr/CALA0600264.md): Shear Tie · corroded · Jul 22, 2006 · N17344 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FRAME SHEAR TIE CORRODED AT STA 867 BETWEEN S27R AND S27L, LBL 4 TO RBL 4. THE CORROSION WAS REMOVED AND A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA0600263](https://openairdocs.org/sdr/CALA0600263.md): Skin · corroded · Jul 22, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND STRINGER AND ADJACENT SKIN IN AFT BILGE AREA CORRODED AT STA 986-1006, S27L. A DOUBLER WAS INSTALLED ON THE SKIN IAW SRM 53-00-01, FIGURE 201 AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0600261](https://openairdocs.org/sdr/CALA0600261.md): Stringer Clip · cracked · Jul 21, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN S19L STRINGER TIE IN AFT BILGE AT STA 947.5. THE STRINGER TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600258](https://openairdocs.org/sdr/CALA0600258.md): Frame · cracked · Jul 21, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT BILGE FRAME CRACKED AT STA 947.5, STR 19L. REPLACED FRAME PER SRM 51-40-02.
- [SDR CALA0600257](https://openairdocs.org/sdr/CALA0600257.md): Stringer · corroded · Jul 20, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > STRINGER S-25L CORRODED ON O/B FLANGE. REPAIRED STRINGER PER SRM 53-00-03.
- [SDR CALA0600256](https://openairdocs.org/sdr/CALA0600256.md): Floorbeam · cracked · Jul 20, 2006 · N17344 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > TWO INCH CRACK ON FLOORBEAM AT STA 328 & RBL 12. REPLACED FLOORBEAM CHORD PER SRM 53-10-51, FIG 201.
- [SDR CALA0400734](https://openairdocs.org/sdr/CALA0400734.md): Stringer · corroded · Dec 3, 2004 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 385. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0200431](https://openairdocs.org/sdr/CALA0200431.md): Keelbeam · fretted · Jul 26, 2002 · N17344 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND RT KEEL BEAM TOP OF LOWER CHORD HAD WASHER MILLED INTO IT AT STA 720-727, RBL 6. INSTALLED REPAIR IAW ECRA 5310-03740.
- [SDR CALA0200426](https://openairdocs.org/sdr/CALA0200426.md): Floor Support · corroded · Jul 22, 2002 · N17344 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 792-815, L27R. A NEW CARGO FLOOR SUPPORT WAS INSTALLED IAW SRM 53-00-53.
- [SDR CALA0200425](https://openairdocs.org/sdr/CALA0200425.md): Panel · cracked · Jul 20, 2002 · N17344 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK AT EDGE OF ACCESS HOLE IN NR 1 ENGINE PYLON PANEL 5724L. INSTALLED REPAIR DOUBLER IAW ECRA 5430-01204.
- [SDR CALA0200420](https://openairdocs.org/sdr/CALA0200420.md): Floor Support · corroded · Jul 19, 2002 · N17344 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND DIAGONAL FLOOR SUPPORT CORRODED AT BS 1016, LBL 8 AND RBL 8. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-2.
- [SDR CALA0200419](https://openairdocs.org/sdr/CALA0200419.md): Stiffener · corroded · Jul 19, 2002 · N17344 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND APB FORWARD FACE LOWEST POINT CENTER STIFFENER CORRODED AT R/H AND L/H SIDE STA 1016, BL 0. STIFFENER REPAIRS WERE INSTALLED IAW SRM 51-70-11. INSPECTED CAPSULATED FASTENERS AND APPLIED LEVELING COMPOUND.
- [SDR CALA0200406](https://openairdocs.org/sdr/CALA0200406.md): Beam · corroded · Jul 18, 2002 · N17344 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND THE LT AND RT MLG SUPPORT BEAM O/B ATTACH POINTS CORRODED BETWEEN BUSHINGS. REPAIRED THE LT AND RT MLG BEAM IAW ECRA 5741-01025 AND 5741-01026.
- [SDR CALA0200404](https://openairdocs.org/sdr/CALA0200404.md): Frame · corroded · Jul 16, 2002 · N17344 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 3/4" CRACK ON BOTTOM END OF R/H MAIN FRAME AT STA 616 BELOW FLOOR. REPAIRED IAW ECRA 5311-01129.
- [SDR CALA0200403](https://openairdocs.org/sdr/CALA0200403.md): Floor Support · corroded · Jul 16, 2002 · N17344 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT AFT LAV DIAGONAL FLOOR SUPPORT CORRODED AT SCREW HOLES, BS 986-1006, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200397](https://openairdocs.org/sdr/CALA0200397.md): Stringer · corroded · Jul 14, 2002 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200396](https://openairdocs.org/sdr/CALA0200396.md): Floorbeam · corroded · Jul 14, 2002 · N17344 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, RBL 36 TO RBL 49. A REPAIR WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0200393](https://openairdocs.org/sdr/CALA0200393.md): Stringer · cracked · Jul 9, 2002 · N17344 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R AFT OF STA 500D. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0001301](https://openairdocs.org/sdr/CALA0001301.md): Skin · cracked · Aug 22, 2000 · N17344 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND THREE 1 INCH CRACKS AT LIGHTENING HOLES IN FORWARD CARGO DOOR SKIN. REPAIRS WERE INSTALLED IAW ECRA 5230-01567.
- [SDR CALA9900001](https://openairdocs.org/sdr/CALA9900001.md): Tire · failed · Jan 2, 1999 · N17344 · Boeing 7373T0 · Tire
  > A BUMP WAS FELT ON THE RT MLG WITH GEAR HANDLE IN THE UP AND OFF POSITION AFTER TAKEOFF. ALSO, THE RT MLG RED UNSAFE LIGHT WAS ILLUMINATED. THE AIRCRAFT WAS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 3 MLG TIRE HAD THROW
- [SDR CALA9801376](https://openairdocs.org/sdr/CALA9801376.md): Skin · gouged · Jul 30, 1998 · N17344 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 440, STRINGER 23R. THE GOUGE WAS BLENDED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, 51-10-02, AND 53-00-01, FIGURE 201.
- [SDR CALA9801346](https://openairdocs.org/sdr/CALA9801346.md): Floorbeam · corroded · Jul 26, 1998 · N17344 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947.5 SPAN OF BEAM, WL 208.1. A NEW SECTION OF UPPER T WAS SPLICED IN IAW ECRA 5321-01018 AND SRM 53-00-51, FIGURE 202.
- [SDR CALA9801334](https://openairdocs.org/sdr/CALA9801334.md): Floorbeam · corroded · Jul 24, 1998 · N17344 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 967, RBL 27.5 TO LBL 41.5. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.
- [SDR CALA9801324](https://openairdocs.org/sdr/CALA9801324.md): Seat Track · corroded · Jul 22, 1998 · N17344 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-947. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA9601145](https://openairdocs.org/sdr/CALA9601145.md): Det. Module · inoperative · Aug 8, 1996 · N17344 · Boeing 7373T0 · Fire Detection
  > WHILE CLIMBING THROUGH 34,000 FEET, WITH THE APU SHUT OFF, THE APU FIRE LIGHT AND BELL ACTIVATED. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED WITHIN TWO MINUTES. THE AIRCRAFT WAS DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR CAL950800](https://openairdocs.org/sdr/CAL950800.md): Fire Loop · inoperative · Sep 9, 1995 · N17344 · Boeing 7373T0 · Fire Detection
  > FLT NR 0655 - IAH - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF IAH. THE NR 2 ENGINE WAS SHUT DOWN AND THE RIGHT FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE
- [SDR CAL950610](https://openairdocs.org/sdr/CAL950610.md): Apu · malfunctioned · Jul 20, 1995 · N17344 · Boeing 7373T0 · Airborne Auxiliary Power Unit (APU) System
  > IAH - FLT 0426 - WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR CONTROL CIRCUIT BREAKER POPPED ON CLIMB-OUT OF IAH. THE CIRCUIT BREAKER WAS RESET AND THE APU VOLTAGE FLUCTUATED FROM 110V TO 115V. THE AIRCRAFT WAS RETU

## 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 = 'N17344' AND deregistration_id = 'N17344-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17344-2013-03-21/reports

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