# N314FL: Boeing 737-36E, registration cancelled 2004-08-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 30, 2004 - Exported to: Iceland - Status when cancelled: Valid registration - Airframe: [Boeing 737-36E](https://openairdocs.org/model/boeing-737-36e) (registry code 138443A) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 25256 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 28, 2000 - Certificate issued: February 6, 2004 - Last registry action: February 6, 2004 - Mode S code: A35635 - Owner when cancelled: [Afs Investments Xliv LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XLIV%20LLC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N314FL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314FL - Page: https://openairdocs.org/deregistered/N314FL-2004-08-30 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-36E: https://openairdocs.org/model/boeing-737-36e.md ## Service difficulty reports (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200300178](https://openairdocs.org/sdr/F3LA200300178), Dec 16, 2003: FLOORBEAM. CORRODED. 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), Dec 13, 2003: INTERCOSTAL. CORRODED. 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 - [SDR F3LA200300175](https://openairdocs.org/sdr/F3LA200300175), Dec 11, 2003: MOUNT BRACKET. CORRODED. 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), Dec 11, 2003: FLOOR SUPPORT. CORRODED. 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 REI - [SDR F3LA200300172](https://openairdocs.org/sdr/F3LA200300172), Dec 11, 2003: MOUNT. CORRODED. 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), Dec 11, 2003: INTERCOSTAL. CORRODED. 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- - [SDR F3LA200300170](https://openairdocs.org/sdr/F3LA200300170), Dec 11, 2003: INTERCOSTAL. CORRODED. 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- - [SDR F3LA200300169](https://openairdocs.org/sdr/F3LA200300169), Dec 11, 2003: INTERCOSTAL. CORRODED. 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- - [SDR F3LA200300174](https://openairdocs.org/sdr/F3LA200300174), Dec 10, 2003: WEB. BROKEN. 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, F - [SDR F3LA200300167](https://openairdocs.org/sdr/F3LA200300167), Dec 5, 2003: GALLEY TRACK. CORRODED. 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), Dec 5, 2003: ANGLE. CORRODED. 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), Dec 5, 2003: SILL. CORRODED. 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), Dec 5, 2003: ANGLE. CORRODED. 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- - [SDR F3LA200300163](https://openairdocs.org/sdr/F3LA200300163), Dec 5, 2003: FLOORBEAM. CORRODED. 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 A - [SDR F3LA200300162](https://openairdocs.org/sdr/F3LA200300162), Dec 5, 2003: FLOORBEAM. CORRODED. 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 - [SDR F3LA200300161](https://openairdocs.org/sdr/F3LA200300161), Dec 5, 2003: FLOORBEAM. CORRODED. 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), Dec 5, 2003: FLOORBEAM. CORRODED. 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 53-10-5 - [SDR F3LA200300157](https://openairdocs.org/sdr/F3LA200300157), Dec 5, 2003: INTERCOSTAL. CORRODED. 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 INSTALLE - [SDR F3LA200300159](https://openairdocs.org/sdr/F3LA200300159), Dec 4, 2003: WEB. CRACKED. 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 L - [SDR F3LA200300158](https://openairdocs.org/sdr/F3LA200300158), Dec 4, 2003: FLOORBEAM. CORRODED. 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 REPA - [SDR F3LA200300122](https://openairdocs.org/sdr/F3LA200300122), Jun 22, 2003: CONTROLLER. INOPERATIVE. 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 - [SDR F3LA200200398](https://openairdocs.org/sdr/F3LA200200398), Dec 29, 2002: SKIN. CRACKED. 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, PA - [SDR F3LA200200196](https://openairdocs.org/sdr/F3LA200200196), Jul 15, 2002: FAN. INOPERATIVE. FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DEN. REPLACED TURBOFAN, PERFORMED PRESSURIZATION SYSTEM OPERATIONAL TEST AND CHECKED OK - [SDR F3LA200200122](https://openairdocs.org/sdr/F3LA200200122), Apr 4, 2002: FAIRING. DELAMINATED. 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 DAMAG - [SDR F3LA200200119](https://openairdocs.org/sdr/F3LA200200119), Mar 26, 2002: ANGLE. CORRODED. 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), Mar 25, 2002: PANEL. CORRODED. 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- - [SDR F3LA200200116](https://openairdocs.org/sdr/F3LA200200116), Mar 21, 2002: FLOORBEAM. CORRODED. 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), Mar 16, 2002: STRAP. CORRODED. 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 FL - [SDR F3LA200200114](https://openairdocs.org/sdr/F3LA200200114), Mar 16, 2002: FLOOR PANEL. CORRODED. 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), Mar 16, 2002: FLOOR PANEL. CORRODED. 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), Mar 16, 2002: STRINGER. CORRODED. 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), Mar 16, 2002: STRINGER. CORRODED. 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), Mar 16, 2002: PANEL. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD LOWER DOOR FRAME PANEL CRACKED. FABRICATED AND INSTALLED REPLACEMENT PANEL AND DOUBLER PER SRM 5 - [SDR F3LA200200109](https://openairdocs.org/sdr/F3LA200200109), Mar 14, 2002: SKIN. CRACKED. 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), Feb 26, 2002: CONTROLLER. FAILED. AIR TURNBACK. FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE DURING CLIMBOUT. REPLACED CABIN PRESSURE CONTROLLER AND OUTFLOW VALVE, - [SDR F3LA00189](https://openairdocs.org/sdr/F3LA00189), Aug 14, 2000: DETECTOR. ILLUMINATED. DEN - FLT 522 - AIR RETURN. FLIGHT CREW REPORTED LT WING/BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE PERFORMED WING/BODY OVERHEAT T --- 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.