# Service difficulty reports: N314FL, cancelled Aug 30, 2004

A list on [N314FL, cancelled Aug 30, 2004](https://openairdocs.org/deregistered/N314FL-2004-08-30.md).

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

- [SDR F3LA200300178](https://openairdocs.org/sdr/F3LA200300178.md): Floorbeam · corroded · Dec 16, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CAP, LBL 17 TO RBL 13. REPAIRED UPPER CHORD ON STA 947 PER EA B3-53R-10228.
- [SDR F3LA200300176](https://openairdocs.org/sdr/F3LA200300176.md): Intercostal · corroded · Dec 13, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL, STA 328-344, LBL 10, FWD GALLEY. INTERCOSTAL FOUND TO BE OUT OF LIMITS PER SRM 51-10-51. MATERIAL ID FOR NEW INTERCOSTAL WAS BAC 1505-100403 PER BOEING DRAWING 65-48834. COVER PLATE WAS 2024-T3.
- [SDR F3LA200300175](https://openairdocs.org/sdr/F3LA200300175.md): Mount Bracket · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage Main, Attach Fittings
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON GIRT BAR MOUNT AT STA. 344, LBL 60. REPLACED GIRT BAR MOUNT BRACKET SRM 51-36-01 AND 51-40-02.
- [SDR F3LA200300173](https://openairdocs.org/sdr/F3LA200300173.md): Floor Support · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON UPPER CHORD FLOOR SUPPORT IN AFT GALLEY, STA 986.5 TO STA 1006, LBL 31. REPLACED CHORD PER SRM 51-40-02 AND REINSTALLED FLOOR SUPPORT ASSY PER SRM 51-40-02.
- [SDR F3LA200300172](https://openairdocs.org/sdr/F3LA200300172.md): Mount · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON GALLEY MOUNT AT STA 990, RBL 32. REPLACED GALLEY MOUNT PER SRM 51-40-02.
- [SDR F3LA200300171](https://openairdocs.org/sdr/F3LA200300171.md): Intercostal · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL STA 947 - 967, LBL 16. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51 AND 51-40-02.
- [SDR F3LA200300170](https://openairdocs.org/sdr/F3LA200300170.md): Intercostal · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 952, LBL 25. REPLACED INTERCOSTAL FROM STA 947 - 967, LBL 24.5, WL 208, PER SRM 51-40-2, 53-60-5 FIG 101 AND 51-4-5.
- [SDR F3LA200300169](https://openairdocs.org/sdr/F3LA200300169.md): Intercostal · corroded · Dec 11, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND FLOORBOARD HOLE ON INTERCOSTAL AT STA. 950, LBL 46, WL 208. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-60-51, FIG. 1, SRM 51-40-02, AND EA B3-53R-10228.
- [SDR F3LA200300174](https://openairdocs.org/sdr/F3LA200300174.md): Web · broken · Dec 10, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED WEB BEHIND MOP SILL AT STA. 294.5, RBL 56, BROKEN. INSTALLED REPAIR PARTS FOR TYPICAL WEB REPAIR IAW SRM 51-70-13, PAGE 3, FIG. 1, SHEET 3 AND NEW ANEL PER SRM 51-40-02.
- [SDR F3LA200300167](https://openairdocs.org/sdr/F3LA200300167.md): Galley Track · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON GALLEY TRACK, STA. 344, LBL 20-23. REPAIRED GALLEY TRACK IAW SRM 53-00-52.
- [SDR F3LA200300166](https://openairdocs.org/sdr/F3LA200300166.md): Angle · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE ON MOP SILL SUPPORT ANGLE, STA. 326, LBL 57. REPLACED ANGLE UNDER MOP SILL IAW SRM 51-40-02.
- [SDR F3LA200300165](https://openairdocs.org/sdr/F3LA200300165.md): Sill · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON L-1 MOP SILL, STA 312-344. REPLACED L-1 MOP SILL PER SRM 51-40-02.
- [SDR F3LA200300164](https://openairdocs.org/sdr/F3LA200300164.md): Angle · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND 3 NUT PLATES BELOW MOP SILL, STA 344-360, LBL 60. REPLACED REINFORCING ANGLE UNDER L-1 MOP SILL PER SRM 51-40-02.
- [SDR F3LA200300163](https://openairdocs.org/sdr/F3LA200300163.md): Floorbeam · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 328, RBL 49. REMOVED SECTION OF FLOORBEAM AND INSTALLED NEW UPPER CAP END REPAIR AND SPLICES PER EA 03-531-10225.
- [SDR F3LA200300162](https://openairdocs.org/sdr/F3LA200300162.md): Floorbeam · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CAP AT STA 986.5, LBL 45 TO RBL 12, UPPER AND LOWER SURFACES. REPLACED FLOORBEAM UPPER CAP PER EA B3-53R-10237.
- [SDR F3LA200300161](https://openairdocs.org/sdr/F3LA200300161.md): Floorbeam · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 344, LBL 13. REPLACED FLOORBEAM UPPER CAP PER EA B3-53R-10237.
- [SDR F3LA200300160](https://openairdocs.org/sdr/F3LA200300160.md): Floorbeam · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 294.5, RBL 38.5. FABRICATED AND INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51.
- [SDR F3LA200300157](https://openairdocs.org/sdr/F3LA200300157.md): Intercostal · corroded · Dec 5, 2003 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 996, BL 0. REMOVED OLD INTERCOSTAL FROM STA 986.5 TO STA 1006, BL 0. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA B3-53R-10242 AND SRM 51-40-02.
- [SDR F3LA200300159](https://openairdocs.org/sdr/F3LA200300159.md): Web · cracked · Dec 4, 2003 · N314FL · Boeing 73736E · Nacelle/Pylon Miscellaneous Structure
  > DURING C-CHECK, INSPECTION REPORTED NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING WEB CRACKED AND PULLED FASTENERS AT STIFFENER. REPLACED WEB ON NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING PER SRM 51-40-02 AND EA B3-54R-10217.
- [SDR F3LA200300158](https://openairdocs.org/sdr/F3LA200300158.md): Floorbeam · corroded · Dec 4, 2003 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM UPPER CHORD AT STA 312, BL 0. REMOVED DAMAGED UPPER T-CHORD AT STA 312, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51 AND 51-40-02.
- [SDR F3LA200300122](https://openairdocs.org/sdr/F3LA200300122.md): Controller · inoperative · Jun 22, 2003 · N314FL · Boeing 73736E · Cabin Pressure Controller
  > AIR TURN BACK. FLIGHT CREW REPORTED ALTITUDE WARNING HORN SOUNDED WHILE CLIMBING THROUGH 23,000 FT. STARTED DESCENT TO 10,000 FT. COMPLETED CHECKLIST AT 10,000 FT. IN MANUAL MODE AND AIRCRAFT STARTED PRESSURIZING. DECLARED AN EMERGENCY AND AIRCRAFT LANDED W
- [SDR F3LA200200398](https://openairdocs.org/sdr/F3LA200200398.md): Skin · cracked · Dec 29, 2002 · N314FL · Boeing 73736E · Wing, Plate/Skin
  > INSPECTION REPORTED APPROXIMATELY A 7 INCH CRACK IN THE RT WING L/E JUST ABOVE AND OUTBOARD OF NR 4 SLAT ACTUATOR. PERFORMED INTERIM REPAIR PER SRM 51-70-14, PAGE 7, PARA 8. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK. AREA WILL BE REINSPECTED EVERY
- [SDR F3LA200200196](https://openairdocs.org/sdr/F3LA200200196.md): Fan · inoperative · Jul 15, 2002 · N314FL · Boeing 73736E · Air Distribution Fan
  > FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DEN. REPLACED TURBOFAN, PERFORMED PRESSURIZATION SYSTEM OPERATIONAL TEST AND CHECKED OKAY.
- [SDR F3LA200200122](https://openairdocs.org/sdr/F3LA200200122.md): Fairing · delaminated · Apr 4, 2002 · N314FL · Boeing 73736E · Nacelle/Pylon, Plate/Skin
  > DURING C-2 CHECK, INSPECTION REPORTED DELAMINATION ON TOP INSIDE DUCT OF NR 1 ENGINE INBOARD THRUST REVERSER MID STREAM FAIRING AND METAL MISSING. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 54-737-041 AND SRM 51-10-02.
- [SDR F3LA200200119](https://openairdocs.org/sdr/F3LA200200119.md): Angle · corroded · Mar 26, 2002 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT AFT BULKHEAD LOWER TEE ANGLE. REPLACED TEE ANGLE PER MM 51-10-02 AND DRAWING 65-4931.
- [SDR F3LA200200117](https://openairdocs.org/sdr/F3LA200200117.md): Panel · corroded · Mar 25, 2002 · N314FL · Boeing 73736E · Cargo Compartments
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TRANSITION PANEL AT STA 847 TO 867, LBL 24. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 53-60-53 AND 51-40-02.
- [SDR F3LA200200116](https://openairdocs.org/sdr/F3LA200200116.md): Floorbeam · corroded · Mar 21, 2002 · N314FL · Boeing 73736E · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED FLOORBEAM AT R-2 DOOR CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 53-60-51 AND 53-00-51 FIG 203.
- [SDR F3LA200200115](https://openairdocs.org/sdr/F3LA200200115.md): Strap · corroded · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED SPLICE STRIP CORRODED BETWEEN FLOOR PANELS NR 1 AND NR 2 IN AFT CARGO COMPARTMENT. FABRICATED AND INSTALLED REPLACEMENT FLOOR JOINT STRAP PER SRM 51-10-02.
- [SDR F3LA200200114](https://openairdocs.org/sdr/F3LA200200114.md): Floor Panel · corroded · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL NR 3 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL PER SRM 51-20-01.
- [SDR F3LA200200113](https://openairdocs.org/sdr/F3LA200200113.md): Floor Panel · corroded · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Floor Panel
  > DURING C-2 CHECK, INSPECTION REPORTED JOINT BETWEEN PANELS 3 AND 4 IN AFT CARGO COMPARTMENT CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 53-60-53.
- [SDR F3LA200200112](https://openairdocs.org/sdr/F3LA200200112.md): Stringer · corroded · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Main, Longeron/Stringer
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRINGER AT STA 793, LBL 3. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53.
- [SDR F3LA200200111](https://openairdocs.org/sdr/F3LA200200111.md): Stringer · corroded · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Main, Longeron/Stringer
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRINGER AT STA 793, RBL 3. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53.
- [SDR F3LA200200110](https://openairdocs.org/sdr/F3LA200200110.md): Panel · cracked · Mar 16, 2002 · N314FL · Boeing 73736E · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD LOWER DOOR FRAME PANEL CRACKED. FABRICATED AND INSTALLED REPLACEMENT PANEL AND DOUBLER PER SRM 51-40-2.
- [SDR F3LA200200109](https://openairdocs.org/sdr/F3LA200200109.md): Skin · cracked · Mar 14, 2002 · N314FL · Boeing 73736E · Fuselage Main, Plate/Skin
  > DURING C-2 CHECK, INSPECTION REPORTED CRACKS IN SHEET METAL AFT OF FWD CARGO COMPARTMENT DOOR. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-13.
- [SDR F3LA200200077](https://openairdocs.org/sdr/F3LA200200077.md): Controller · failed · Feb 26, 2002 · N314FL · Boeing 73736E · Cabin Pressure Controller
  > AIR TURNBACK. FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE DURING CLIMBOUT. REPLACED CABIN PRESSURE CONTROLLER AND OUTFLOW VALVE, PERFORMED OPERATIONAL TEST AND SYSTEM CHECKED OKAY.
- [SDR F3LA00189](https://openairdocs.org/sdr/F3LA00189.md): Detector · illuminated · Aug 14, 2000 · N314FL · Boeing 73736E · Overheat Detection
  > DEN - FLT 522 - AIR RETURN. FLIGHT CREW REPORTED LT WING/BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE PERFORMED WING/BODY OVERHEAT TEST AND FOUND SYSTEM SLOW TO RESPOND. REPLACED COMPARTMENT OVERHEAT MODULE. INSPECTED LT AIR CO

## 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 = 'N314FL' AND deregistration_id = 'N314FL-2004-08-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N314FL-2004-08-30/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.