# Service difficulty reports: N14307, cancelled Aug 19, 2004

A list on [N14307, cancelled Aug 19, 2004](https://openairdocs.org/deregistered/N14307-2004-08-19.md).

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

- [SDR CALA0400109](https://openairdocs.org/sdr/CALA0400109.md): Battery Pack · inoperative · Feb 12, 2004 · N14307 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND L-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51.
- [SDR CALA0400108](https://openairdocs.org/sdr/CALA0400108.md): Battery Pack · inoperative · Feb 12, 2004 · N14307 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51.
- [SDR CALA0300458](https://openairdocs.org/sdr/CALA0300458.md): Slide · unserviceable · Aug 10, 2003 · N14307 · Boeing 7373T0 · Escape Slide
  > INSPECTION FOUND THE L-2 DOOR EMERGENCY SLIDE PRESSURE LOW. THE EMERGENCY ESCAPE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.
- [SDR CALA0300240](https://openairdocs.org/sdr/CALA0300240.md): Skin · cracked · May 11, 2003 · N14307 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A CRACK IN THE AFT CARGO DOOR INNER SKIN. THE SKIN WAS REPAIRED IAW ECRA 5232-01027.
- [SDR CALA0300200](https://openairdocs.org/sdr/CALA0300200.md): Floorbeam · corroded · Apr 17, 2003 · N14307 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND NUT PLATE HOLE AT STA 344, LBL 35. REPAIRED ONE FLANGE OF THE FLOORBEAM UPPER CHORD IAW SRM 53-10-51, FIGURE 206, SHEET 4.
- [SDR CALA0300082](https://openairdocs.org/sdr/CALA0300082.md): Pressure Panel · cracked · Mar 2, 2003 · N14307 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A.5 INCH CRACK IN PRESSURE DECK WEB AT STA 664, RBL 30. REPAIRED PRESSURE WEB IAW SRM 53-60-51.
- [SDR CALA0300080](https://openairdocs.org/sdr/CALA0300080.md): Pressure Panel · cracked · Mar 1, 2003 · N14307 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND A 2 INCH CRACK IN PRESSURE DECK AT BS 664, LBL 30. REPAIRED IAW ECRA 5360-01078.
- [SDR CALA0200247](https://openairdocs.org/sdr/CALA0200247.md): Rudder · cracked · Apr 27, 2002 · N14307 · Boeing 7373T0 · Rudder Structure
  > WHILE AIRCRAFT WAS IN HOLD FOR PAINT JOB AT VENDOR FACILITY THE RUDDER SUSTAINED DAMAGE. INSPECTION FOUND THAT THE RUDDER LOWER WEB HAD AN 8" CRACK WITH A HOLE AND SHORTER CRACKS EMANATING FROM IT. THE LEFT LOWER SKIN OF RUDDER HAD TWO CRACKS IN SAME AREA. THE
- [SDR CALA0101027](https://openairdocs.org/sdr/CALA0101027.md): Spar Cap · corroded · Dec 12, 2001 · N14307 · Boeing 7373T0 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND R/H HORIZONTAL STABILIZER AFT UPPER SPAR CAP CORRODED ON TOP SIDE O/B END UNDER T/E SKIN PANEL. REPAIRED IAW ECRA 5510-01611.
- [SDR CALA0101026](https://openairdocs.org/sdr/CALA0101026.md): Web · cracked · Dec 12, 2001 · N14307 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A 2" CRACK IN L-1 DOOR LOWER FORWARD WEB AT LOWER FORWARD STOP FITTING. THE CRACK WAS STOP DRILLED. A DOUBLER AND RADIUS BLOCK REPAIR WAS INSTALLED IAW ECRA 5265-01005 REV D AND ECRA 5210-01461.
- [SDR CALA0101025](https://openairdocs.org/sdr/CALA0101025.md): Plate · cracked · Dec 9, 2001 · N14307 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 4" CRACK IN #1 I/B PYLON NUTPLATE STRIP BETWEEN PANEL #5742 AND #5743. THE NUTPLATE STRIP WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 54-50-71.
- [SDR CALA0101023](https://openairdocs.org/sdr/CALA0101023.md): Track · corroded · Dec 8, 2001 · N14307 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO L/H O/B FLOOR TRACK CORRODED AT STA 727-727C. THE FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-53 AND 53-00-53.
- [SDR CALA0101020](https://openairdocs.org/sdr/CALA0101020.md): Skin · cracked · Dec 4, 2001 · N14307 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND L-1 DOOR SKIN AT AFT INTERIOR EDGE CRACKED AT 4TH AND 5TH STOP FROM BOTTOM. THE CRACKS WERE 1" LONG. THE CRACKED AREAS WERE REMOVED AND A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-70-11, FIGURE 1.
- [SDR CALA0101014](https://openairdocs.org/sdr/CALA0101014.md): Beltframe · corroded · Nov 28, 2001 · N14307 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD BAGGAGE BIN BELTFRAME CORRODED AT STA 500, AFT SIDE, O/B, S27R. REPAIRED BELTFRAME IAW SRM 53-00-09, FIGURE 203, PAGE 207-209.
- [SDR CALA0000215](https://openairdocs.org/sdr/CALA0000215.md): Switch · inoperative · Feb 29, 2000 · N14307 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM LGA. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE M991 AIR SENSING SQUAT SWITCH AT FAULT. THE SWITCH WAS REMOVED AND REPL
- [SDR CALA9900697](https://openairdocs.org/sdr/CALA9900697.md): Skin · cracked · Jun 17, 1999 · N14307 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.75 INCH CRACK IN C-2 DOOR SKIN AT DOOR HANDLE CUTOUT. A REPAIR WAS INSTALLED IAW SRM 52-00-01.
- [SDR CALA9900670](https://openairdocs.org/sdr/CALA9900670.md): Frame · cracked · Jun 14, 1999 · N14307 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN CAPTAIN'S WINDOW FRAME. REPAIRED IAW ECRA 5330-02824.
- [SDR CALA9900666](https://openairdocs.org/sdr/CALA9900666.md): Intercostal · cracked · Jun 11, 1999 · N14307 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 178 STRINGER 19L AND A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT STA 178 STRINGER 19R. THE INTERCOSTALS WERE REMOVED AND REPLACED IAW ECRA 5310-01968.
- [SDR CALA9900650](https://openairdocs.org/sdr/CALA9900650.md): Intercostal · corroded · Jun 4, 1999 · N14307 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT STA 986 TO 1006, WL 208, LT SIDE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9900591](https://openairdocs.org/sdr/CALA9900591.md): Support · corroded · May 31, 1999 · N14307 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 FROM BL 0 TO RBL 70. REPAIRED IAW SRM 53-10-51.
- [SDR CALA9900587](https://openairdocs.org/sdr/CALA9900587.md): Floorbeam · corroded · May 31, 1999 · N14307 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 50 TO LBL 30. REPAIRED IAW SRM 53-10-51.
- [SDR CALA9900584](https://openairdocs.org/sdr/CALA9900584.md): Seat Track · corroded · May 28, 1999 · N14307 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 344-360, LBL 40. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.
- [SDR CALA9800828](https://openairdocs.org/sdr/CALA9800828.md): Hyd Line · leaking · May 9, 1998 · N14307 · Boeing 7373T0 · Hydraulic System, Main
  > B-SYSTEM HYDRAULIC FAILURE. ENGINE NR 2 LOW PRESSURE WARNING. FOUND LINE BETWEEN B-SYSTEM HYDRAULIC SYSTEM PUM TO ACOUSTIC FILTER LEAKING. REPLACED LINE.
- [SDR CALA9601338](https://openairdocs.org/sdr/CALA9601338.md): Circuit Card · malfunctioned · Sep 27, 1996 · N14307 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AT ALTITUDE AND REMAINED ON. WHEN THE GEAR HANDLE WAS LOWERED, THE RED LIGHT STAYED ON AND THE GREEN LIGHT DID NOT COME ON. A MANUAL GEAR EXTENSION WAS PERFORMED AND A VISUAL CHECK THROUGH THE VIEW PORT SHOWED STRIP
- [SDR CALA9601330](https://openairdocs.org/sdr/CALA9601330.md): Lock Sensor · inoperative · Sep 26, 1996 · N14307 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE AIRCRAFT HAD A HISTORY OF THE NLG RED UNSAFE LIGHT COMING ON IN FLIGHT. THE M983 LOGIC CARD HAD BEEN REPLACED PREVIOUSLY, BUT THE PROBLEM WAS REPEATED. MAINTENANCE REMOVED AND REPLACED THE R374 LATCHING RELAY AND THE NOSE GEAR LOCK SENSOR. SYSTEM FUNCTI
- [SDR CALA9601275](https://openairdocs.org/sdr/CALA9601275.md): Shimmy Damper · failed · Sep 7, 1996 · N14307 · Boeing 7373T0 · Shimmy Damper
  > THE AIRCRAFT BEGAN TO BOUNCE UP AND DOWN SOON AFTER LANDING. THE BOUNCING STOPPED AFTER THE AIRCRAFT SLOWED TO 100 KNOTS, BUT THEN PULLED TO THE LEFT. THE AIRCRAFT WAS STOPPED AND TAXIED OFF THE RUNWAY. MAINTENANCE FOUND THE RT MLG SHIMMY DAMPER HAD FAILED
- [SDR CALA9601044](https://openairdocs.org/sdr/CALA9601044.md): Intercostal · corroded · Jul 19, 1996 · N14307 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 967, LBL 17.61 AND RBL 17.61. A REPAIR WAS PERFORMED IAW ECRA 5320-01443.
- [SDR CAL950219](https://openairdocs.org/sdr/CAL950219.md): Wire · chafed · Mar 20, 1995 · N14307 · Boeing 7373T0 · Hydraulic Power System Wiring
  > IAH - FLT 0501 - SYSTEM 'B' ELECTRIC PUMP LOW PRESSURE LIGHT ILLUMINATED AT CRUISE ALT ELEC PUMP FAILED AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ELECTRIC PUMP WIRE CHAFED. INSULATED WIRE AND REPOSITIONED, RESET PUMP OPS
- [SDR CAL950133](https://openairdocs.org/sdr/CAL950133.md): O-Ring · leaking · Feb 16, 1995 · N14307 · Boeing 7373T0 · Hydraulic System, Main
  > IAH - FLT 1638 - THE A-HYDRAULIC SYSTEM QUANTITY BEGAN TO DECRASE IN FLIGHT. THE LEAKAGE STOPPED WHEN THE A-SYSTEM WAS ISOLATED BY TURNING THE SYSTEM-1 FLIGHT CONTROL TO STANDBY RUDDER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAIN

## 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 = 'N14307' AND deregistration_id = 'N14307-2004-08-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14307-2004-08-19/reports

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