# N313FL: 1992 Boeing 737-3L9, registration cancelled 2005-06-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 2, 2005 - Exported to: Malaysia - Status when cancelled: Valid registration - Airframe: [Boeing 737-3L9](https://openairdocs.org/model/boeing-737-3l9) (registry code 138447O) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 26442 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 10, 1999 - Certificate issued: October 29, 1999 - Last registry action: November 5, 2002 - Mode S code: A3527E - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N313FL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=313FL - Page: https://openairdocs.org/deregistered/N313FL-2005-06-02 From the FAA registry file of October 29, 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 737-3L9: https://openairdocs.org/model/boeing-737-3l9.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200500018](https://openairdocs.org/sdr/F3LA200500018), Apr 22, 2005: COVER. MISSING. AIR RETURN TO DEN, ON CLIMB-OUT, BOTH ENGINE OIL QUANTITY INDICATORS WENT TO ZERO. BOTH OIL PRESSURE INDICATORS WENT TO ZERO. BOTH LOW OIL PRESSURE LIGHTS ILLUM - [SDR F3L2005F00000](https://openairdocs.org/sdr/F3L2005F00000), Apr 22, 2005: ENGINE. LEAKING. APPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR - [SDR F3LA200500008](https://openairdocs.org/sdr/F3LA200500008), Mar 9, 2005: SILL. CORRODED. DURING C-4 CHECK INSPECTION, REPORTED L2 DOOR MOP SILL CORRODED. REPLACED L2 DOOR MOP SILL PER SRM 51-40-02. - [SDR F3LA200500010](https://openairdocs.org/sdr/F3LA200500010), Mar 8, 2005: STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT GALLEY PAN STRAP AT BS 1016, BETWEEN RBL 30 AND LBL 30. FOUND TO BE OUT OF LIMITS PER SRM 53-60-61, FIG 1 - [SDR F3LA200500009](https://openairdocs.org/sdr/F3LA200500009), Mar 8, 2005: INTERCOSTAL. CORRODED. DURING C-4 CHECK INSPECTION, REPORTED INTERCOSTAL AT BS 950, RBL 20 TO RBL 40, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REPLACED INTERCOSTAL PER SR - [SDR F3LA200500007](https://openairdocs.org/sdr/F3LA200500007), Mar 8, 2005: SILL. CORRODED. DURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02. - [SDR F3LA200400091](https://openairdocs.org/sdr/F3LA200400091), Aug 20, 2004: PRESSURE PANEL. CRACKED. FLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK - [SDR F3LA200400067](https://openairdocs.org/sdr/F3LA200400067), Jun 3, 2004: CONTROL MODULE. INOPERATIVE. ABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTRANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLA - [SDR F3LA200300123](https://openairdocs.org/sdr/F3LA200300123), Aug 1, 2003: SNUBBER. INOPERATIVE. DURING C-3 CHECK, INSPECTION REPORTED R-1 DOOR LOCK PIN INOPERATIVE. ADJUSTED SNUBBER ON R-1 DOOR PER MM 52-41-00, PAGE 504, STEP 5. - [SDR F3LA200200370](https://openairdocs.org/sdr/F3LA200200370), Oct 24, 2002: INTERCOSTAL. CORRODED. DURING C 2 CHECK, CORROSION WAS FOUND ON THE AFT CARGO PIT INTERCOSTAL SURFACE AND AROUND NUT PLATES BETWEEN STA 767 TO STA 794 AND RBL 21. NEW INTERCOSTAL WAS - [SDR F3LA200200363](https://openairdocs.org/sdr/F3LA200200363), Oct 24, 2002: FLOOR SUPPORT. CORRODED. DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND CORRODED AT STA 727D AT RBL 13.8 THE CORRODED SECTION OF TRACK WAS REPLACED BETWEEN STA 727 AN - [SDR F3LA200200372](https://openairdocs.org/sdr/F3LA200200372), Oct 23, 2002: FLOOR SUPPORT. CORRODED. DURING C 2 CHECK, CORROSION WAS FOUND OF THE AFT CARGO COMPARTMENT FLOOR TRACK AT STA 791, LBL 11.5. REMOVED AND REPLACED THE FLOOR TRACK IAW SRM 51-10-02 AND S - [SDR F3LA200200369](https://openairdocs.org/sdr/F3LA200200369), Oct 23, 2002: FLOOR SUPPORT. CORRODED. DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, RBL 2. FLOOR TRACK WAS REPLACED BETWEEN STA 727 AND STA 947, RBL 2.5 IAW SRM 51-40-05 AND - [SDR F3LA200200368](https://openairdocs.org/sdr/F3LA200200368), Oct 23, 2002: SKIN. PUNCTURED. DURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IAW SRM 51-70-10 AND REINSTALLED IAW BOEING - [SDR F3LA200200366](https://openairdocs.org/sdr/F3LA200200366), Oct 22, 2002: FLOOR SUPPORT. CORRODED. DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, LBL 3.0 FLOOR TRACK REPLACED BETWEEN STA 791 TO STA 860. LBL 3.0, IAW SRM 51-40-02 - [SDR F3LA200200371](https://openairdocs.org/sdr/F3LA200200371), Oct 20, 2002: FLOOR PANEL. CORRODED. DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS FOUND CORRODED BETWEEN STA 787 AND STA 807. AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL - [SDR F3LA200200365](https://openairdocs.org/sdr/F3LA200200365), Oct 18, 2002: TAIL CONE. DENTED. DURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-30 - [SDR F3LA200200367](https://openairdocs.org/sdr/F3LA200200367), Oct 17, 2002: SKIN. BIRD STRIKE. DURING C 2 CHECK, A BIRD STRIKE WAS FOUND ON THE RT LEADING EDGE OF THE STABILIZER BETWEEN STA 184.7 AND STA 189.2. FABRICATED AND INSTALLED DOUBLER AND FILLER - [SDR F3LA200200136](https://openairdocs.org/sdr/F3LA200200136), May 8, 2002: CONTROL CABLE. BROKEN. FLIGHT CREW REPORTED SIGNIFICANT RT ROLL TENDENCY ON FINAL APPROACH AND LANDING. CORRECTED ON TOUCHDOWN. FOUND AILERON BUS CABLE BROKEN. REMOVED RT AILERON CABL - [SDR F3LA200200120](https://openairdocs.org/sdr/F3LA200200120), Apr 1, 2002: VIDEO UNIT. SHORTED. FLIGHT CREW REPORTED ENTERTAINMENT TAPE RECORDER SMOKING EN ROUTE TO DEN. DIVERTED TO SLC AND LANDED WITHOUT INCIDENT. ISOLATED ELECTRICAL SHORT IN TAPE PLAYER. - [SDR F3LA200200105](https://openairdocs.org/sdr/F3LA200200105), Mar 1, 2002: ACTUATOR. INOPERATIVE. BLOCK TURNBACK. FLIGHT CREW REPORTED RUDDER WOULD NOT CENTER AFTER START UP AND TAXI. REPLACED RUDDER TRIM ACTUATOR AND CHECKED OKAY. - [SDR F3LA200000259](https://openairdocs.org/sdr/F3LA200000259), Nov 28, 2000: DOOR. OUT OF ADJ. DURING TAKEOFF, FLIGHT CREW REPORTED FORWARD ENTRY DOOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 75 KIAS. MAINTENANCE ADJUSTED FORWARD ENTRY DOOR PER MM 52-11- - [SDR F3LA200000260](https://openairdocs.org/sdr/F3LA200000260), Nov 24, 2000: SPRING. UNSERVICEABLE. DURING C-7 CHECK TEST FLIGHT, FLIGHT CREW REPORTED AILERONS STIFF IN MANUAL REVERSION. REPLACED AILERON CONTROL SPRING AND CHECKED OKAY. ## Other aircraft with N313FL - [Registered now](https://openairdocs.org/aircraft/N313FL): Bell Textron Canada 505, S/N 65466, built 2023 --- 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.