N315FL
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
34 reports on file, 2000-06-23 – 2003-09-29.
Part: SKIN — CANNING (FUSELAGE) · airframe 33,551 hrs · 17,570 cycles
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 PREVIOUS SKIN PATCHES AT STA. 340-360, STR. 19R. CUT OUT DAMAGED AREAS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-01, FIG. 229.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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 AND REPAIR SPLICES IAW SRM 53-60-51 AND EA B3-53R-10150.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 25, BETWEEN STA 967 AND 947.5, CORRODED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED LAV MOUNT AT STA. 947.5, LBL 25, CORRODED. REPLACED LAV MOUNT IAW SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT LBL 16, BETWEEN STA 967 AND 947.5, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-2, 51-40-02, 53-60-51 AND 51-20-01.
Part: STRIP — CRACKED (FUSELAGE) · airframe 33,551 hrs · 17,570 cycles
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 51-40-02 AND DRAWING 65C33971.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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, MFG DRAWING 65C34624 AND SOPM 20-41-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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, 53-60-53 AND DRAWING 69-43477.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED LONGITUDINAL INTERCOSTAL AT RBL 24 BETWEEN STA 947 AND STA 967 CORRODED.
Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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 51-10-02, 51-20-01, AND EA B3-53R-10148.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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 53-60-51.
Part: SILL — CORRODED (L2 DOOR) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED MOP SILL CORRODED INSIDE L2 DOOR SILL. REPLACED L-2 DOOR MOP SILL PER SRM 51-40-02.
Part: FRAME — CRACKED (HORIZONTAL STAB) · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED LT HORIZONTAL STABILIZER FRAME CRACKED WHERE ELEVATOR ATTACH MECHANISM ATTACHES TO HORIZONTAL STABILIZER. FABRICATED AND INSTALLED REPLACEMENT CHORD IAW SRM 51-40-2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED MIDDLE INTERCOSTAL BETWEEN FLOORBEAMS AT STA. 1006 - 986.5 CORRODED. FABRICATED AND INSTALLED INTERCOSTAL IAW EA B3-53R-10114 AND SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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 SUPPORT BEAM AND REPAIRED IAW SRM 53-00-51, FIG. 202.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 312 AND 328, LBL 12, CORRODED ON TOP. REPLACED INTERCOSTAL IAW SRM 51-10-02.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL AT APPROX. STA. 727C, RBBL 3. REPLACED DAMAGED FLOOR SUPPORT CHANNEL FROM STA. 727 - 847, RBBL 3, IAW SRM 53-60-53, 51-10-02 AND 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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 205, 51-40-02, 51-10-02 AND SOPM 20-41-02.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,551 hrs · 17,570 cycles
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.
Part: MEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 33,064 hrs · 17,277 cycles
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 BACKS TO IDLE. DECLARED AN EMERGENCY & DIVERTED. ACFT LANDED W/O INCIDENT. REPLACED NR 1 ENG FUEL PUMP, MEC, PMC & N2 ALTERNATOR. ENG OPS & LEAK CHECK GOOD. ALL PARAMETERS WITHIN LIMITS. PERFORMED A/T PLA SYNCHRO ADJ/TEST & A/T BITE TEST, NO FAULTS FOUND. PULLED MAGNETIC CHIP DETECTORS, NO DEFECTS NOTED. CHECKED CIT SENSOR TUBING & SENSOR, NO DEFECTS NOTED. PERFORMED OVERWEIGHT LANDING INSPECTION, NO DEFECTS NOTED. PERFORMED TEST FLIGHT. NO DISCREPANCIES NOTED. PERFORMED POST TEST FLIGHT WALKAROUND. NO DISCREPANCIES NOTED.
Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 32,430 hrs · 16,890 cycles
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 DECOMPRESSION. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED AFT OUTFLOW VALVE, CABIN PRESSURE CONTROLLER, AND OVERHEAD SELECTOR PANEL. PERFORMED OPERATIONAL TEST, CHECKED NORMAL. OXYGEN GENERATORS USED AT ROWS 12 DEF, 15 ABC, 16 ABC, 16 DEF, 17 ABC, 17 DEF, 18 ABC, 18 DEF, 19 DEF, 20 ABC, AND 22 ABC. REPLACED SAME.
Part: SKIN — CRACKED (NR 1 SLAT) · airframe 32,214 hrs · 16,764 cycles
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 SRM 57-45-01, 57-43-01 AND 51-30-2.
Earlier reports · 2000–2002 · 10 reports
2002
Part: OUTFLOW VALVE — BROKEN · airframe 31,149 hrs · 16,188 cycles
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 FROM THE VALVE ASSEMBLY DUE TO A BROKEN RIVET AND SLIPPED FLAPPER.MAINTENANCE REMOVED AND REPLACED THE OUTFLOW VALVE IN ACCORDANCE WITH THE REQUIREMENTS OF BOEING MAINTENANCE MANUAL 21-31-00, PAGE 201.
Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 INSTALLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-5 AND 51-30-2.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 51-40-02.
Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 FLOOR TRACKS PER SRM 53-60-53.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 51-70-11 AND 51-40-02.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 28,949 hrs · 15,123 cycles
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 AFT CORNER OF AFT CARGO DOOR AND REPAIRED PER SRM 51-50-2 AND 51-70-13.
Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 TRACK PER SRM 53-00-53.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,949 hrs · 15,123 cycles
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 INSTALLED PER SOPM 20-41-02 AND SRM 53-60-53, 51-70-11, 51-10-11.
2001
Part: PCU — MALFUNCTIONED (RUDDER) · airframe 27,439 hrs · 14,360 cycles
CLIMBOUT, 8 TO 10 UNCONTL RUDDER INPUTS, STRONG ENOUGH TO FEEL ACFT RESPOND. TURNED AUTOPILOT & YAW DAMPER ON & OFF, NO EFFECT. PROBLEM DISAPPEARED. CLIMBOUT, NR 1 ENG SURGED THRU 18,000 FT. TURNED AUTOTHROTTLE ON & OFF, NO EFFECT. REACHING 18000 FT ENG RAN SMOOTH. REPLACED RUDDER PCU, RIGGED & PERF OPS CHK OF RUDDER PCU, YAW DAMPER COUPLER & FOUND NO DISCREP & ACCOMP FLT CONTL MOVEMENT CHK. THE DFDR & CVR WERE REMOVED FOR READ OUT. NO SIGNIF RUDDER MOVEMENT OR YAW OBSERVED. READ OUT SHOWED FLUX OF NR 1 ENG BEGUN 18000' & STAB 24,000'. PERF PWR ASSURANCE CHK & BORESCOPE INSPEC OF NR 1 ENG & PERF TROUBLESHOOT FOR SURGING ENG, NO FAULTS FOUND. ACCOMP TEST FLT, NO ENG SURGE OR UNCONTL RUDDER INPUT.
2000
Part: GENERATOR — FAILED (NR 1 ENGINE)
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 FUSE PLUG MELTED ON TAXIWAY. MAINTENANCE REPLACED NR 1 AND NR 2 MAIN WHEEL AND BRAKE ASSEMBLIES, PERFORMED HIGH ENERGY STOP INSPECTION. REPLACED NR 1 VSCF GENERATOR. PERFORMED OPERATIONAL CHECK ON NR 2 GENERATOR SYSTEM PER MM 24-21-00, NO FAULTS FOUND. (X)