# Service difficulty reports: N17321, cancelled Oct 8, 2009

A list on [N17321, cancelled Oct 8, 2009](https://openairdocs.org/deregistered/N17321-2009-10-08.md).

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

- [SDR CALA0600535](https://openairdocs.org/sdr/CALA0600535.md): Keelbeam · corroded · Dec 20, 2006 · N17321 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND RIGHT KEEL BEAM SEGMENT CORRODED AT STA 500C+10 THROUGH STA 540. THE KEEL BEAM SECTION WAS REMOVED AND A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, REPAIR 3.
- [SDR CALA0600534](https://openairdocs.org/sdr/CALA0600534.md): Shear Tie · cracked · Dec 20, 2006 · N17321 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND A.5 INCH CRACK IN SKIN SHEAR TIE AT STA 500D BETWEEN S28R AND S28L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600527](https://openairdocs.org/sdr/CALA0600527.md): Keelbeam · corroded · Dec 18, 2006 · N17321 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED AT STA 727-727A, S27L. THE CORRODED SECTION OF LT KEEL BEAM WAS REPLACED IAW SRM 53-60-12.
- [SDR CALA0600526](https://openairdocs.org/sdr/CALA0600526.md): Frame · corroded · Dec 18, 2006 · N17321 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND CHORD CORRODED AT STA 227, BL 0 TO RBL 6, S28L TO S28R. A REPAIR WAS INSTALLED IAW ECRA 5311-01285.
- [SDR CALA0600522](https://openairdocs.org/sdr/CALA0600522.md): Web · corroded · Dec 15, 2006 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB BELOW LT TIEDOWN RAIL CORRODED AT STA 727A - 727B, S25L. THE WEB WAS REPLACED IAW ECRA 5310-04596.
- [SDR CALA0600516](https://openairdocs.org/sdr/CALA0600516.md): Attach Fitting · corroded · Dec 13, 2006 · N17321 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A FORWARD BAGGAGE BIN BELT FRAME CLIP CORRODED AT STA 500B, RBL 7 TO LBL 4. DOUBLER AND FILLER WAS INSTALLED IAW SRM 53-00-07 AND 51-40-02.
- [SDR CALA0600209](https://openairdocs.org/sdr/CALA0600209.md): Fire Loop · failed · Jun 12, 2006 · N17321 · Boeing 7373T0 · Fire Detection
  > THE AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE TO IAH FROM ATL. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO BHM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE WAS UNABLE T
- [SDR CALA0600199](https://openairdocs.org/sdr/CALA0600199.md): Control Panel · faulty · Jun 3, 2006 · N17321 · Boeing 7373T0 · Fire Detection
  > THE OVHT/DET LIGHT ILLUMINATED WITH CORRESPONDING AFT B DET ON DESCENT INTO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION FOUND NO EVIDENCE OF FIRE. THE CARGO FIRE SUPPRESSION CONTROL PANEL WAS FOUND AT FAULT. THE CONTROL PANEL WAS REMOVED AND REPL
- [SDR CALA0500311](https://openairdocs.org/sdr/CALA0500311.md): Wire · chafed · Sep 13, 2005 · N17321 · Boeing 7373T0 · Light System Wiring
  > THE EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED INTERMITTENTLY WHILE IN CRUISE PORTION OF FLIGHT. MAINTENANCE FOUND WIRES W1150-513 AND -512 CHAFING IN FORWARD CLOSET AREA WHILE REFERENCING WIRING DIAGRAM 33-51-21. THE WIRES WERE REPAIRED AND OPERATION OF
- [SDR CALA0400639](https://openairdocs.org/sdr/CALA0400639.md): Stringer · corroded · Sep 15, 2004 · N17321 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25L CORRODED AT STA 867-907 IN AFT BAGGAGE BIN. THE CORROSION WAS REMOVED AND A REPAIR SECTION OF STRINGER WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0400634](https://openairdocs.org/sdr/CALA0400634.md): Angle · cracked · Sep 12, 2004 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN ANGLE ON INTERCOSTAL AT FORWARD AND AFT SCREW HOLES OF CABIN FLOOR STRUCTURE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 53-30-51.
- [SDR CALA0400633](https://openairdocs.org/sdr/CALA0400633.md): Floorbeam · corroded · Sep 11, 2004 · N17321 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 986.5, LBL 45 TO RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-00-51, FIGURE 202 AND ECRA 5310-03851.
- [SDR CALA0400632](https://openairdocs.org/sdr/CALA0400632.md): Frame · corroded · Sep 11, 2004 · N17321 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 480, RBL 11. REPAIRED FRAME IAW SRM 53-00-07, FIGURE 206.
- [SDR CALA0400631](https://openairdocs.org/sdr/CALA0400631.md): Pan · corroded · Sep 10, 2004 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT SIDE FLOOR PAN FOR VANITY FILL/DRAIN LINE CONNECTIONS CORRODED I/B OF Z-ANGLE BETWEEN STA 986.5 AND 1016. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0400629](https://openairdocs.org/sdr/CALA0400629.md): Floorbeam · corroded · Sep 9, 2004 · N17321 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 967, LBL 35 TO RBL 35. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51, FIGURE 202, PAGE 207.
- [SDR CALA0400255](https://openairdocs.org/sdr/CALA0400255.md): Skin · dented · Mar 18, 2004 · N17321 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 1080, WL 192, RBL 8. THE AREA WAS REPAIRED IAW SRM 53-00-01 AND 51-21-41.
- [SDR CALA0300014](https://openairdocs.org/sdr/CALA0300014.md): Skin · cracked · Jan 16, 2003 · N17321 · Boeing 7373T0 · Electrical/Electronic Compartment Doors
  > INSPECTION FOUND A 1/2" CRACK IN E&E DOOR OUTER SKIN AT R/H SIDE. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-00-01.
- [SDR CALA0300013](https://openairdocs.org/sdr/CALA0300013.md): Shear Tie · corroded · Jan 16, 2003 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 500D O/B OF STRINGER 27L. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 203.
- [SDR CALA0300010](https://openairdocs.org/sdr/CALA0300010.md): Keelbeam · corroded · Jan 13, 2003 · N17321 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM CORRODED AFT OF STA 500D INSIDE AIR CONDITIONING DISTRIBUTION BAY. A KEEL BEAM REPAIR WAS INSTALLED IAW SRM 53-30-12.
- [SDR CALA0300009](https://openairdocs.org/sdr/CALA0300009.md): Floor Support · cracked · Jan 12, 2003 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN CENTER FLOOR SUPPORT BETWEEN STA 500D AND 520. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300008](https://openairdocs.org/sdr/CALA0300008.md): Web · cracked · Jan 12, 2003 · N17321 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1" CRACK IN CENTER FLOOR WEB AT STA 500D-520. A REPAIR WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0300007](https://openairdocs.org/sdr/CALA0300007.md): Floorbeam · cracked · Jan 12, 2003 · N17321 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1" CRACK IN RADIUS OF FLOORBEAM ON AFT SIDE OF STA 540 UNDER EXPANSION JOINT AT R/H I/B SEAT TRACK. REPAIRED IAW ECRA 5320-01406.
- [SDR CALA0001616](https://openairdocs.org/sdr/CALA0001616.md): Stringer · cracked · Oct 20, 2000 · N17321 · Boeing 7373T0 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN RT WING STRINGER AT WS 505.00 AFT TOP STRINGER. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW ECRA 5720-01818.
- [SDR CALA0001602](https://openairdocs.org/sdr/CALA0001602.md): Skin · cracked · Oct 19, 2000 · N17321 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK AT SCREW HOLE OF FUSELAGE SKIN, STA 380, BL 0. REPAIRED IAW ECRA 5330-02894.
- [SDR CALA0001570](https://openairdocs.org/sdr/CALA0001570.md): Beam · cracked · Oct 13, 2000 · N17321 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A 0.20 INCH CRACK IN AFT EDGE OF L-1 DOOR (EDGE BEAM) JUST I/B OF 7TH FROM TOP STOP FITTING. REPAIRED IAW ECRA 5211-01045.
- [SDR CALA0001538](https://openairdocs.org/sdr/CALA0001538.md): Floorbeam · corroded · Oct 10, 2000 · N17321 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 53-LBL 53. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9901433](https://openairdocs.org/sdr/CALA9901433.md): Frame · cracked · Oct 24, 1999 · N17321 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR FRAME AT LOWER FORWARD CORNER. THE FORWARD CARGO CORNER DOOR FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9801904](https://openairdocs.org/sdr/CALA9801904.md): Channel · cracked · Oct 4, 1998 · N17321 · Boeing 7373T0 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 10 INCH CRACK IN AFT CHANNEL INSIDE NR 1 PYLON ABOVE LOWER AFT FAIRING. A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9601478](https://openairdocs.org/sdr/CALA9601478.md): Skin · fretting · Oct 13, 1996 · N17321 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE AT DORSAL FIN ASSEMBLY FORWARD RIGHT AND LEFT SKIN FRETTING WHERE SEAL RIDES. FABRICATED AND INSTALLED DOUBLER PER SRM 53-00-01 FIG 201 SHEETS 1 TO 3.
- [SDR CALA9601477](https://openairdocs.org/sdr/CALA9601477.md): Skin · cracked · Oct 11, 1996 · N17321 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN UNDER NUMBER 3 VHF ANTENNA CRACKED JUST AFT OF STATION 727D. INSTALLED FILLER AND DOUBLER PER SRM 53-00-01.
- [SDR CAL960188](https://openairdocs.org/sdr/CAL960188.md): Circuit Breaker · popped · Feb 23, 1996 · N17321 · Boeing 7373T0 · Landing Gear Position and Warning
  > FLT NR 1645 - EWR - WHEN GEAR WAS EXTENDED FOR LANDING AT PHX, THREE GREEN GEAR INDICATION LIGHTS WERE NOT RECEIVED. THE NOSE GEAR AIR/GROUND CIRCUIT BREAKER WAS FOUND POPPED DURING A TOWER FLYBY. THE CIRCUIT BREAKER WAS RESET AND PANEL INDICATED THREE GREEN
- [SDR CAL950270](https://openairdocs.org/sdr/CAL950270.md): Eel Wiring · broken · Apr 13, 1995 · N17321 · Boeing 7373T0 · Emergency Lighting
  > EWR - FLT 135 - THE MID CABIN EMERGENCY AISLE LIGHTING WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND BROKEN WIRING, AND A BLOWN FUSE ON BATTERY CHARGER. THE BROKEN WIRES WERE SPLICED AND THE BATTERY CHARGER FUSE WAS REPLACED. OPERATION O

## 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 = 'N17321' AND deregistration_id = 'N17321-2009-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17321-2009-10-08/reports

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