# Service difficulty reports: N12349, cancelled Dec 31, 2008

A list on [N12349, cancelled Dec 31, 2008](https://openairdocs.org/deregistered/N12349-2008-12-31.md).

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

- [SDR CALA0800636](https://openairdocs.org/sdr/CALA0800636.md): Charger · faulty · Jun 25, 2008 · N12349 · Boeing 7373T0 · Emergency Lighting
  > ROWS 12 - 20 EMERGENCY SEAT LIGHTS INOPERATIVE. FOUND CHARGER PART NUMBER RPS1-B AT FAULT, LOCATED IN CEILING CENTER AREA BETWEEN AFT GALLEYS. REMOVED AND REPLACED BATTERY CHARGER PER AMM 33-51-51. OPERATIONAL CHECKS GOOD.
- [SDR CALA0600182](https://openairdocs.org/sdr/CALA0600182.md): Skin · cracked · May 22, 2006 · N12349 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.58 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AROUND FORWARD LIGHTENING CUTOUTS SPRING COMPARTMENT. A REPAIR WAS INSTALLED IAW ECRA 5232-01075.
- [SDR CALA0600181](https://openairdocs.org/sdr/CALA0600181.md): Intercostal · cracked · May 22, 2006 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN INTERCOSTAL AT STA 294, S12L FORWARD OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.
- [SDR CALA0600180](https://openairdocs.org/sdr/CALA0600180.md): Stringer Splice · cracked · May 22, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.75 INCH CRACK IN STRINGER SPLICE CHANNEL AT STA 360, S14L AFT OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.
- [SDR CALA0600179](https://openairdocs.org/sdr/CALA0600179.md): Pan · cracked · May 21, 2006 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 0.8 INCH CRACK IN C-2 DOOR PAN AT FORWARD MID SECTION. THE DOOR PAN WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA0600176](https://openairdocs.org/sdr/CALA0600176.md): Fitting · cracked · May 21, 2006 · N12349 · Boeing 7373T0 · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION -X- BRACE RT FORWARD LOWER CORNER FITTING. THE FITTING WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0600172](https://openairdocs.org/sdr/CALA0600172.md): Beltframe · corroded · May 20, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT BELT FRAME STA 794, S25R - S22R, LOWER SIDE AT C-2 DOOR CUTOUT, STRAP AND REPAIR DOUBLER HAVE SOME CORROSION BY NUT PLATES. REPAIRED BELT FRAME IAW SRM 53-60-53.
- [SDR CALA0600171](https://openairdocs.org/sdr/CALA0600171.md): Pan · cracked · May 20, 2006 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN C-1 DOOR PAN LOWER FORWARD CORNER NEXT TO UPLATCH HOOK, STA 440-500, S17R TO S27R. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02, STEP 8 AND SRM 51-40-02, STEP 4 AND 5.
- [SDR CALA0600168](https://openairdocs.org/sdr/CALA0600168.md): Keelbeam · cracked · May 17, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND A 1 INCH CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 201, PAGE 205.
- [SDR CALA0600165](https://openairdocs.org/sdr/CALA0600165.md): Stiffener · corroded · May 10, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND RT CHANNEL STIFFENER CORRODED AT LOWER APB STA 1016, RBL 1. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106 AND EA 5310-04045, REV A, OPS 2.
- [SDR CALA0600161](https://openairdocs.org/sdr/CALA0600161.md): Bulkhead · corroded · May 9, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1014 BETWEEN S27R AND S27L. THE AREA WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA0600160](https://openairdocs.org/sdr/CALA0600160.md): Floorbeam · corroded · May 9, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 4 TO LBL 36. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-51.
- [SDR CALA0600156](https://openairdocs.org/sdr/CALA0600156.md): Seat Track · corroded · May 8, 2006 · N12349 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED AT STA 907 TO 947.5, LBL 25. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600155](https://openairdocs.org/sdr/CALA0600155.md): Frame · cracked · May 8, 2006 · N12349 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.25 INCH CRACK IN LEFT MAIN FRAME BELOW MAIN DECK AT STA 616, LBL 60 TO LBL 61. THE MAIN FRAME WAS REPAIRED IAW ECRA 5311-01158.
- [SDR CALA00128](https://openairdocs.org/sdr/CALA00128.md): Sensor · intermittent · Apr 25, 2005 · N12349 · Boeing 7373T0 · Landing Gear Position and Warning
  > LANDING GEAR UNSAFE LIGHT CAME ON THEN INTERMITTENT AFTER LEVEL AT FL35. REPLACED NLG SENSOR PER AMM 32-61-51.
- [SDR CALA0400640](https://openairdocs.org/sdr/CALA0400640.md): Access Panel · cracked · Sep 17, 2004 · N12349 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.
- [SDR CALA0400636](https://openairdocs.org/sdr/CALA0400636.md): Seat Track · cracked · Sep 14, 2004 · N12349 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202.
- [SDR CALA0400552](https://openairdocs.org/sdr/CALA0400552.md): Charger · inoperative · Jun 26, 2004 · N12349 · Boeing 7373T0 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-51, PAGES 201-207. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS GOOD.
- [SDR CALA2000266](https://openairdocs.org/sdr/CALA2000266.md): Spoiler · May 7, 2002 · N12349 · Boeing 7373T0 · Spoilers
  > #3 SPOILER DENTED AND CRACKED.75X.75 INCHES JUST FWD AND OB OF ACTUATOR ATTACH POINT. INSTALLED DOUBLER PER SRM 57-70-01, FIG 204.
- [SDR CALA0200242](https://openairdocs.org/sdr/CALA0200242.md): Web · corroded · Apr 25, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200239](https://openairdocs.org/sdr/CALA0200239.md): Web · corroded · Apr 25, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION UNDER FLANGE OF VERTICAL THRESHOLD WEB AT AFT BAGGAGE BIN DOORWAY FROM STA 767-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200232](https://openairdocs.org/sdr/CALA0200232.md): Channel · corroded · Apr 21, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 794, LBL 3 AND RBL 3. CHANNEL BEAM REPAIRS WERE INSTALLED AT EACH LOCATION IAW SRM 53-00-53, FIGURE 201.
- [SDR CALA0200231](https://openairdocs.org/sdr/CALA0200231.md): Channel · corroded · Apr 21, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHANNEL CORRODED IN AFT BAGGAGE BIN AT STA 794, RBL 8. REPAIRED IAW SRM 53-00-53.
- [SDR CALA0200230](https://openairdocs.org/sdr/CALA0200230.md): Channel · corroded · Apr 21, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5" RBL 3. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.
- [SDR CALA0200229](https://openairdocs.org/sdr/CALA0200229.md): Channel · corroded · Apr 21, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 727D+5", RBL 8 AND LBL 8. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW ECRA 5320-01603.
- [SDR CALA0200228](https://openairdocs.org/sdr/CALA0200228.md): Floor Support · corroded · Apr 21, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5, LBL 12. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.
- [SDR CALA0200224](https://openairdocs.org/sdr/CALA0200224.md): Floor Support · corroded · Apr 20, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200223](https://openairdocs.org/sdr/CALA0200223.md): Floorbeam · corroded · Apr 20, 2002 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT STA 312. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0200219](https://openairdocs.org/sdr/CALA0200219.md): Floorbeam · corroded · Apr 19, 2002 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER T CAP CORRODED AT FASTENER HOLES, STA 294.5, LBL 20 TO RBL 58. REPAIRED IAW SRM 53-10-51.
- [SDR CALA0200217](https://openairdocs.org/sdr/CALA0200217.md): Web · cracked · Apr 18, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3" CRACK IN WEB AT R/H SIDEWALL FLOOR BETWEEN STA 559 AND 578. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0200216](https://openairdocs.org/sdr/CALA0200216.md): Floorbeam · corroded · Apr 18, 2002 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM T-CAP CORRODED AT FASTENER HOLES, STA 344. REPAIRED IAW SRM 51-10-51.
- [SDR CALA0200212](https://openairdocs.org/sdr/CALA0200212.md): Stringer · cracked · Apr 17, 2002 · N12349 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING AT STA 500C. A NEW STRINGER WAS INSTALLED IAW SRM 53-30-03 AND 53-00-03.
- [SDR CALA0200211](https://openairdocs.org/sdr/CALA0200211.md): Mount · corroded · Apr 16, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT O/B LAV MOUNT CORRODED AT STA 1012, LBL 38. THE LAV MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200210](https://openairdocs.org/sdr/CALA0200210.md): Channel · corroded · Apr 16, 2002 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT O/B CHANNEL OF WEB CORRODED AT STA 986.5-1006, LBL 38. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200206](https://openairdocs.org/sdr/CALA0200206.md): Stringer · corroded · Apr 15, 2002 · N12349 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0001321](https://openairdocs.org/sdr/CALA0001321.md): Skin · cracked · Aug 25, 2000 · N12349 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 0.4 INCH CRACK IN ABB DOOR INTERIOR SKIN AT LIGHTENING HOLE EDGE. THE EXISTING REPAIR DOUBLERS WERE REMOVED AND A NEW SINGLE DOUBLER REPAIR WAS INSTALLED IAW ECRA 5230-01571.
- [SDR CALA0001320](https://openairdocs.org/sdr/CALA0001320.md): Skin · gouged · Aug 25, 2000 · N12349 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT BAGGAGE BIN DOOR EXTERIOR SKIN GOUGED. THE SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA9801163](https://openairdocs.org/sdr/CALA9801163.md): Channel · corroded · Jun 24, 1998 · N12349 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR Z-CHANNEL CORRODED AT STA 294-328. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9801161](https://openairdocs.org/sdr/CALA9801161.md): Panel · corroded · Jun 24, 1998 · N12349 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 847-867. THE TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9801158](https://openairdocs.org/sdr/CALA9801158.md): Seat Track · corroded · Jun 23, 1998 · N12349 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT FS 328-344. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA9801147](https://openairdocs.org/sdr/CALA9801147.md): Floorbeam · corroded · Jun 21, 1998 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT FS 294.5, RBL 8. THE FLOORBEAM CAP WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9801146](https://openairdocs.org/sdr/CALA9801146.md): Floor Track · corroded · Jun 20, 1998 · N12349 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 294.5. THE FLOOR TRACK WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-00-52.
- [SDR CALA9701804](https://openairdocs.org/sdr/CALA9701804.md): Corroded · corroded · Dec 30, 1997 · N12349 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION ON FLOORBEAM/TRACK TIEDOWN IN AFT PIT AT STA 947, LBBL 17.2. A NEW TRACK TIEDOWN WAS SPLICED IN IAW SRM 53-00-53, FIGURE 202.
- [SDR CALA9600794](https://openairdocs.org/sdr/CALA9600794.md): Light · inoperative · Jun 8, 1996 · N12349 · Boeing 7373T0 · Emergency Lighting
  > THE L-2 DOOR EMERGENCY SLIDE EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.
- [SDR CAL960385](https://openairdocs.org/sdr/CAL960385.md): Nose Link · broken · Mar 23, 1996 · N12349 · Boeing 7373T0 · Leading Edge Slat Control System
  > EWR - FLT 0725 - THE NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD PANEL AND FORWARD PANEL LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED WITH THE FLAPS RETRACTED WHILE IN CLIMB. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE NR 2 KRUGER FLAP NOSE L
- [SDR CAL950948](https://openairdocs.org/sdr/CAL950948.md): O-Rings · cut · Oct 23, 1995 · N12349 · Boeing 7373T0 · Turbine Engine Accessory Drive
  > GSO - FLT 0171 - THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO GSO. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE CREW REPORTED LOSING LESS THAN 8.5 PSI OIL PRESSURE. MAINTENANCE FOUND THE NR 2 ENGINE ANGLE GE

## 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 = 'N12349' AND deregistration_id = 'N12349-2008-12-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12349-2008-12-31/reports

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