# N315FL: Boeing 737-75C - Status: Valid registration - Airframe: [Boeing 737-75C](https://openairdocs.org/model/boeing-737-75c) (registry code 13844DY, 149 seats) - Serial number: 30513 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: December 23, 2025 - Expires: December 31, 2032 - Mode S code: A359EC - Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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 is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315FL - Page: https://openairdocs.org/aircraft/N315FL From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Boeing 737-75C) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N315FL. ## FAA accident and incident reports None matched to N315FL. ## Service difficulty reports (34) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200300149](https://openairdocs.org/sdr/F3LA200300149), Sep 29, 2003: SKIN. CANNING. DURING C-4 CHECK, INSPECTION REPORTED OIL CANNING ON SKIN BETWEEN TWO EXISTING PATCH REPAIRS AT STA. 340-350, STR. 20R. NUMEROUS TIPPED FASTENER HEADS ON PREVIO - [SDR F3LA200300148](https://openairdocs.org/sdr/F3LA200300148), Sep 25, 2003: FLOORBEAM. CORRODED. DURING A-4 CHECK, INSPECTION REPORTED FLOOR BEAM AT STA. 947.5 CORRODED ON TOP CAP, UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED REPLACEMENT TEE CHORD CAP - [SDR F3LA200300147](https://openairdocs.org/sdr/F3LA200300147), Sep 24, 2003: MOUNT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LAV MOUNT AT STA. 947.5, LBL 25, CORRODED. REPLACED LAV MOUNT IAW SRM 51-40-02. - [SDR F3LA200300146](https://openairdocs.org/sdr/F3LA200300146), Sep 24, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 25, BETWEEN STA 967 AND 947.5, CORRODED. REPLACED INTERCOSTAL PER SRM 51-40-02. - [SDR F3LA200300145](https://openairdocs.org/sdr/F3LA200300145), Sep 24, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 16, BETWEEN STA 967 AND 947.5, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10 - [SDR F3LA200300144](https://openairdocs.org/sdr/F3LA200300144), Sep 23, 2003: STRIP. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED CAP STRIP BETWEEN STA. 344 AND 360, RBL 12 TO 24, CRACKED. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP IAW SOPM 51-40-0 - [SDR F3LA200300143](https://openairdocs.org/sdr/F3LA200300143), Sep 23, 2003: SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT. ZEE SUPPORT IN AFT CARGO COMPARTMENT FROM STA. 767 TO STA. 797.2. REPLACED ZEE SUPPORT IAW SRM 51-40-02, - [SDR F3LA200300142](https://openairdocs.org/sdr/F3LA200300142), Sep 23, 2003: SEAT TRACK. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK AT STA. 328 TO STA. 360, RBL 24, CORRODED. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-40-02, MF - [SDR F3LA200300141](https://openairdocs.org/sdr/F3LA200300141), Sep 20, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LONGITUDINAL INTERCOSTAL AT RBL 24 BETWEEN STA 947 AND STA 967 CORRODED. - [SDR F3LA200300140](https://openairdocs.org/sdr/F3LA200300140), Sep 20, 2003: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA. 951, RBL 26-46, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND COVER PLATE IAW SRM - [SDR F3LA200300139](https://openairdocs.org/sdr/F3LA200300139), Sep 20, 2003: MOUNT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED LAVATORY MOUNT AT STA. 947.5, RBL 25, CORRODED. REPLACED MOUNT IAW SRM 51-10-02 AND 51-40-02. - [SDR F3LA200300138](https://openairdocs.org/sdr/F3LA200300138), Sep 18, 2003: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED AT STA. 486.5 TO 1006, LBL 31.5. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-5 - [SDR F3LA200300135](https://openairdocs.org/sdr/F3LA200300135), Sep 17, 2003: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED MOP SILL CORRODED INSIDE L2 DOOR SILL. REPLACED L-2 DOOR MOP SILL PER SRM 51-40-02. - [SDR F3LA200300134](https://openairdocs.org/sdr/F3LA200300134), Sep 13, 2003: FRAME. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED LT HORIZONTAL STABILIZER FRAME CRACKED WHERE ELEVATOR ATTACH MECHANISM ATTACHES TO HORIZONTAL STABILIZER. FABRICATED AND I - [SDR F3LA200300133](https://openairdocs.org/sdr/F3LA200300133), Sep 12, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED MIDDLE INTERCOSTAL BETWEEN FLOORBEAMS AT STA. 1006 - 986.5 CORRODED. FABRICATED AND INSTALLED INTERCOSTAL IAW EA B3-53R-10 - [SDR F3LA200300131](https://openairdocs.org/sdr/F3LA200300131), Sep 12, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOORBEAM CAP STRIP FROM LT TO RT SIDE OF AIRCRAFT AT STA. 986.5. REMOVED DAMAGED SECTION OF FLOOR SU - [SDR F3LA200300130](https://openairdocs.org/sdr/F3LA200300130), Sep 11, 2003: INTERCOSTAL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 312 AND 328, LBL 12, CORRODED ON TOP. REPLACED INTERCOSTAL IAW SRM 51-10-02. - [SDR F3LA200300129](https://openairdocs.org/sdr/F3LA200300129), Sep 9, 2003: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT STA 312. REPLACED FLOORBEAM T-CAP AND SPLICES AT STA 312, RBL 24 TO LBL 34, PER SRM 53-10-51, FIG 20 - [SDR F3LA200300128](https://openairdocs.org/sdr/F3LA200300128), Sep 9, 2003: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT APPROX. STA. 727C, RBBL 3. REPLACED DAMAGED FLOOR SUPP - [SDR F3LA200300127](https://openairdocs.org/sdr/F3LA200300127), Sep 4, 2003: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLES ON WEB AT STA 787 TO STA 794.3. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-2. - [SDR F3LA200300125](https://openairdocs.org/sdr/F3LA200300125), Aug 30, 2003: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT DOOR SILL WEB CORRODED. REPLACED SILL WEB IAW MFG DRAWING 65-20726 AND SRM 51-40-02. - [SDR F3LA200300121](https://openairdocs.org/sdr/F3LA200300121), Jun 18, 2003: MEC. MALFUNCTIONED. AFTER DEPARTURE NR 1 ENG BEGAN TO ROLL BACK THUR RECOVERY & CONTINUED TO FLUCTUATE. FUEL FLOW & ENG FLUCTUATIONS CONTINUED UNTIL LANDING WITH AT LEAST 2 ROLL BA - [SDR F3LA200300115](https://openairdocs.org/sdr/F3LA200300115), Apr 6, 2003: OUTFLOW VALVE. FAILED. FLIGHT CREW REPORTED TOTAL LOSS OF PRESSURIZATION AT CRUISE ALTITUDE. INOPERATIVE IN STANDBY AND MANUAL. MAX CABIN ALTITUDE 18,500/2,000 FPM. NO RAPID DECOMPRES - [SDR F3LA200300095](https://openairdocs.org/sdr/F3LA200300095), Mar 3, 2003: SKIN. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED SURFACE CRACK ON NR 1 SLAT, INBD OF SLAT ACTUATOR. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER S - [SDR F3LA200200377](https://openairdocs.org/sdr/F3LA200200377), Oct 23, 2002: OUTFLOW VALVE. BROKEN. ON TAKE OFF, THE FLIGHT CREW FOUND THE CABIN PRESSURIZATION COULD NOT BE MAINTAINED. MAINTENANCE FOUND THE CHECK VALVE SEAL ON THE OUTFLOW VALVE HAD SEPARATED F - [SDR F3LA200200086](https://openairdocs.org/sdr/F3LA200200086), Feb 24, 2002: CARGO TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR TIE DOWN CORRODED AT STA 859 AND STA 772, LBL 17.2. REPLACED CORRODED AFT CARGO COMPARTMENT FL - [SDR F3LA200200085](https://openairdocs.org/sdr/F3LA200200085), Feb 24, 2002: SKIN. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO DOOR INNER SKIN CRACKED AT LIGHTENING HOLE IN LOWER AFT CORNER. STOP DRILLED CRACK AT LIGHTENING HOLE ON LOWER A - [SDR F3LA200200084](https://openairdocs.org/sdr/F3LA200200084), Feb 24, 2002: ANGLE. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED FLOOR ANGLES CORRODED IN AFT CARGO COMPARTMENT AT STA 787, STR 26R. REPLACED FLOOR STRAP BETWEEN STA 787 AND 867 PER SRM 5 - [SDR F3LA200200083](https://openairdocs.org/sdr/F3LA200200083), Feb 24, 2002: CHANNEL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED AT STA 859, LBL 3. REMOVED CORROSION AND DAMAGE, FABRICATED REPAIR ANGLE AND - [SDR F3LA200200082](https://openairdocs.org/sdr/F3LA200200082), Feb 24, 2002: CHANNEL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED AT STA 727, RBL 8.1. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 51-70- - [SDR F3LA200200081](https://openairdocs.org/sdr/F3LA200200081), Feb 24, 2002: PANEL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED RT FLOOR TO SIDEWALL TRANSITION PANEL IN AFT CARGO COMPARTMENT CORRODED, STA 727 TO STA 767, STR 26R. FABRICATED AND INSTA - [SDR F3LA200200080](https://openairdocs.org/sdr/F3LA200200080), Feb 24, 2002: CARGO TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO BAY FLOOR TIE DOWN TRACK AT STA 859, RBL 13.8, CORRODED. SPLICED IN SECTION OF AFT CARGO BAY FLOOR TIE DOWN TRAC - [SDR F3LA200100098](https://openairdocs.org/sdr/F3LA200100098), Aug 5, 2001: PCU. MALFUNCTIONED. CLIMBOUT, 8 TO 10 UNCONTL RUDDER INPUTS, STRONG ENOUGH TO FEEL ACFT RESPOND. TURNED AUTOPILOT & YAW DAMPER ON & OFF, NO EFFECT. PROBLEM DISAPPEARED. CLIMBOUT, N - [SDR F3LA00124](https://openairdocs.org/sdr/F3LA00124), Jun 23, 2000: GENERATOR. FAILED. DEN - FLT 120 - REJECTED TAKEOFF. FLIGHT CREW REPORTED NR 1 AND NR 2 ELECTRICAL BUSSES TRIPPED OFF. REJECTED AT 108,000 POUNDS AND 110 KNOTS. NR 1 MAIN WHEEL FU ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 737-75C aircraft: https://openairdocs.org/model/boeing-737-75c/aircraft.md --- 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.