N7907A
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.
38 reports on file, 2020-07-01 – 2026-07-25.
Part: ACM — FAULTED (LEFT) · airframe 61,845 hrs · 43,397 cycles
ON TAXI IN GOT STRONG SMOKE ODOR AND LT PACK ILLUMINATED LT PACK TEMP GAUGE MAXED OUT. CHECKED FOR AIR SUPPLY CONTAMINATION IAW FIM 21-00 TASK 802. NO EVIDENCE OF CONTAMINATION CAN BE FOUND. LT PACK OPS SHOWED ACM NOT OPERATING.
Part: SMOKE GOGGLES — NO DISCREPANCY (ZONE 200) · airframe 61,440 hrs · 43,203 cycles
SMOKE GOGGLES REMOVED FROM INBOARD AFT FACING SUPERNUMERARY SEAT FOR USE IN F/O POSITION ( SUPERNUMERARY SEATS ) INSTALLED MISSING SMOKE GOGGLES AT AFT FACING I/B SUPERNUMERARY SEAT IN REF AMM 25-64-00 THIS CLEARS MEL 25-31
Part: LENS — BROKEN (ZONE 200) · airframe 61,190 hrs · 43,093 cycles
FWD GALLEY EMERGENCY ESCAPE COVER WITH INSPECTON LENS BROKEN. OPEN
Part: CARGO — CONTAMINATED (ZONE 100) · airframe 60,953 hrs · 42,898 cycles
FLUID SPILL IN MAIN DECK CARGO ZONE A4/A5 FOUND TO BE DEISEL FUEL ADDITIVE ROUGHLY 1/2 PINT SPILL . SPILL HAS BEEN IDENTIFIED AS NOT HAZMAT/DG SPILL HAS BEEN CLEANED USING STANDARD PROCEDURES REF SOP.810.295. AIRCRAFT IS APPROVED FOR CONTINUED OPERATIONS"
Part: STRUT — DISCHARGED (NLG) · airframe 60,890 hrs · 42,958 cycles
ON WALK AROUND NOSE LG STRUT FOUND FULLY COMPRESSED. PRECEIDING FLIGHT (3055) CREW HAD ISSUE WITH NOSE LG DISAGREE INDICATION, CREW RUN NNC WHICH FIXED AN ISSUE AND LANDED SUCCESS FULLY. TS 31882 SERVICED NOSE STRUT WITH N2 TO SERVICEABLE PRESSURE/EXTENSION PER AMM 12-15-41 NO OIL/N2 LEAK NOTED AND PERFORMED PSEU BITE PROCEDURE IAW FIM 32-09 TASK 801. NO FAULT NOTED. OK DISPLAY DURING THE TEST. ACFT OK FOR BACK TO SERVICE.
Earlier reports · 2020–2025 · 33 reports
2025
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,576 hrs · 42,810 cycles
CAPTAIN'S EMERGENCY FLASHLIGHT BATTERIES DEPLETED. R & R 2 EA BATTERIES IN CAPTANS EMERGENCY FLASHLIGHT IAW AMM 25-64-00. OPS CHECKS GOOD THIS CLEARS MEL 25-12-02.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 60,513 hrs · 42,787 cycles
L1 DOOR EMERG LIGHT DID NOT ILLUMINATE DURING EMERG BATT PACK CAP FUNC CHECK. R1 ILLUMINATED PAST 15 MIN. BATTERY RECHARGE. REPLACED BATTERY PACK IAW AMM 33-51-06, CHECKS OK
Part: PIN — MISSING (GUST LOCK) · airframe 59,839 hrs · 42,452 cycles
L1 GUST LOCK GUIDE ARM PIN AND HARDWARE MISSING INSTALLED GUIDE ARM PIN AND HARDWARE AS REQUIRED PER AMM 52-11-21 OK FOR SERVICE .
Part: REGULATOR — FAULTED (ZONE 100) · airframe 58,247 hrs · 41,739 cycles
RIGHT PACK BLEED TRIP OFF ILLUMINATED DESCENDING FROM FLT390 TO FL380. PERFORMED BLEED AIR SYS LEAK CHECK REF AMM 36-11-00 BLEED AIR REG FAILED. R/R BLEED AIR REGULATOR ASSY IAW AMM 36-11-3 LEAK AND OPS CHECK REQUIRED. DEFECT 785437: R/R RH PRE-COOLER VALVE IAW AMM 36-12-2 OPS CHECK GOOD. THIS CLEARS MEL 363-2 MDDR#129206
2024
Part: SKIN — DAMAGED (ZONE 100) · airframe 57,117 hrs · 41,118 cycles
FS400 FWD CARGO DOOR CUTOUT FWD LOWER CORNER HAS DAMAGE. RESOLUTION: ACCOMPLISHED EXTERNAL SKIN REPAIR AT RH SIDE FUSELAGE FWD CARGO DOOR CUTOUT OWER CORNER IAW BOEING SRM 53-00-01-2R-21.
Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 56,582 hrs · 40,935 cycles
WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB ATTACH ANGLE STA 663 RBL 35" AT INBOARD NUTPLATE AREA CRACKED. REPAIRED WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB ATTACH ANGLE STA 663 RBL 35" AT INBOARD NUTPLATE AREA.
Part: CARGO TRACK — NOT REPORTED (BS 500-500I) · airframe 56,582 hrs · 40,935 cycles
REPLACED FWD CARGO COMPARTMENT TIE DOWN TRACK FROM BS 500 +13 INCH TO BS 500 I, RBL 13.84 INCH. ATTACHED WITH SOLID RIVETS AND HI-LOKS IAW B737-800 SRM 51-40-02-06-0 PARA. 4B AND 51-40-02-06-0 PARA 7D(1) (5) AND BOEING DWG: 143A7500. SPLICED AT TWO PLACES FROM BS 500+ 9.125 INCH TO BS 500 +17 INCH AND BS 500 +7.250 INCH TO BS 500F +15.5 INCH RBL 13.84 INCH IAW BCF SRM 53-00-53-2R-3 REPAIR 3, FIGURE 201. NOTE: THIS IS PERMANENT CATEGORY "A" REPAIR AND FURTHER ACTION IS REQUIRED.
Part: BUSHING — DAMAGED (HORIZONTAL STAB) · airframe 56,582 hrs · 40,935 cycles
LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG.
Part: BUSHING — DAMAGED (HORIZONTAL STAB) · airframe 56,582 hrs · 40,935 cycles
LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT LH HORIZONTAL STABILIZER REAR SPAR LOWER LUG.
Part: BUSHING — DAMAGED (HORIZONTAL STAB) · airframe 56,582 hrs · 40,935 cycles
RH HORIZONTAL STABILIZER REAR SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT RH HORIZONTAL STABILIZER REAR SPAR LOWER LUG.
Part: SEAT TRACK — MECHANIC ERROR (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA 787+16", RBL 47", SEAT TRACK FLANGE WITH DOUBLE HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 787+13" - STA 787+19" COMMON RBL=45.5".
Part: SEAT TRACK — MECHANIC ERROR (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE, AT STA 747+7",LBL 1". SEAT TRACK FLANGE WITH DOUBLE HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 747+3" - STA 747+11" COMMON BL+0.
Part: SEAT TRACK — MECHANIC ERROR (BS 727H) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE, AT STA 727H+2.5",RBL `", SEAT TRACK, FLANGE WITH DOUBLE HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 727H+1" - STA 727H+6".
Part: FLOORBEAM — DAMAGED (BS 827) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA 827 LBL 32" FLOOR BEAM, UPPER FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CABIN FLOOR BEAM UPPER FLANGE SECTION STA 827 LBL 32".
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA 907+16", RBL 23.5" SEAT TRACK FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 920 - STA 926 COMMON RBL=24.75".
Part: SKIN — CRACKED (BS 540) · airframe 56,582 hrs · 40,935 cycles
FUSELAGE SKIN, STA 540 UNDER DRAG LINK ASSEMBLY AT STR S-21R + 7.250 IN, FASTENER HOLE WITH CRACK INDICATION. REPAIRED FUSELAGE SKIN BTWN STA 520 AND STA 540, STR 21R - 23R.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA787+8", RBL 60.5", SEAT TRACK, FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 787+5" - STA 787+11" COMMON RBL=61.9".
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA 807+14", RBL 44.5", SEAT TRACK FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 807+11" - STA 807+17" COMMON RBL=45.5".
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE, AT STA 787+6", RBL 44.5", SEAT TRACK, FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CARGO CABIN SEAT TRACK FLANGE SECTION BETWEEN STA 791 - STA 796 COMMON RBL=45.5".
Part: FLOORBEAM — DAMAGED (BS 948 LBL 22) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE AT STA 947.5, LBL 22, FLOOR BEAM, UPPER FLANGE WITH ELONGATED HOLE. REPAIRED MAIN CABIN FLOOR BEAM UPPER FLANGE SECTION @ STA. 947.5 LBL.22 IAW COOPESA EO # COO-EO-2024-19723-R00 DATED 04-04-2024 AND BOEING MESSAGE C00-SCA-24-0123-0813 DATED 04-2-2024 DOCUMENTED AND APPROVED ON FAA FORN 8100-9 REF: ID 202403200-135-0005 AND DOCUMENTED THE REPAIR AS CATAGORY A DATED 04-11-2024 AND ONE SUN COUNTRY A AUTHORIZATION FORM EA.53-0186 DATED 04/19/2024 THAT CLASSIFIED THIS REPAIR AS MINOR. T.C+40935, FH+56582.39
Part: SEAT TRACK — DAMAGED (BS 727J) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE, AT STA 727J+8",LBL 44", SEAT TRACK, FLANGE WITH ELONGATE HOLE
Part: STIFFENER — CRACKED (BS 540) · airframe 56,582 hrs · 40,935 cycles
UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE AREA AT BODY STATION 540 CENTER FUEL TANK STIFFENERS WITH CRACKS AT ALL POSITIONS. REPLACED SHEAR FITTINGS AT BS 540 CENTER FUEL TANK IAW B737-800 BCF SRM 51-10-02-06-0 PAR 9 AND DWG.111A20000 NEW SHEAR FITTING PN 111A2401 AT LBL.54.60, LBL. 40.87, LBL.32.40, LBL15.04, LBL.6.14 RBL.6.14, RBL.15.04, RBL.32.40, RBL.40.87 AND RBL.54.60
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 56,582 hrs · 40,935 cycles
RH WING REAR SPAR FUEL BOOSTER CUTOUT LOWER AREA WITH CORROSION. REPAIRED
Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 56,582 hrs · 40,935 cycles
REPAIRED WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB UPPER SECTION.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,226 hrs · 40,774 cycles
DEFECT 755160: - - DOOR 1L SLIDE FELL OUT OF THE DOOR. - - RESOLUTION: RE-INSTALLED L1 DOOR EVAC SLIDE PACK +COVERT IAW AMM 25-66-01 OK FOR SERVICE.
Part: WINDOW — CRACKED (R1) · airframe 56,175 hrs · 40,749 cycles
DEFECT 752097: - - R1 OVERHEAT FOLLOWED BY SPIDER CRACK ON OUTER PANE OF R1. - - RESOLUTION: (TRANSFERED LOG ITEM 752097 ITEM 1 TO W/O# 84410 N/R 00003) REMOVED R1 WINDOW REF AMM 56-11-11, BEGAN TO INSTALL NEW WINDOW, DONE THRU STEP 6 REF AMM 56-11-11. FINISHED WINDOW INSTALLATION OF R1 PER AMM 56-11-11. WINDOW HEAT OPS CHECKED PER AMM 30-41-00, OPS CHECKS GOOD. PRESSURIZATION CHECKED PER AMM 05-51-91, OPS CHECKS GOOD.
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,204 hrs · 39,905 cycles
DEFECT 735745: SPEED BRAKE ARMED LIGHT ILLUMINATES DURING APPLICATION OF RIGHT AILERON ON THE GROUND DURING FLIGHT CONTROL CHECK ( AUTO SPEED BRAKE SYSTEM - (ALL EXCEPT N820SY, N821SY, N834SY, N832SY, N834SY AND TAV A/C) - - - RESOLUTION: R&R SPEEDBRAKE ARMED SWITCH REF AMM 27-62-34. OPS CHECK GOOD. PERFORMED SPEED BRAKE CONTROL LEVER ADJUSTMENT REF AMM 27-62-00. OPS CHECK GOOD. THIS CLEARS MEL 27-7-1 MDDR# 117406 MC NOTIFIED
2022
Part: GIRT BAR — DAMAGED (R1 DOOR) · airframe 53,122 hrs · 39,415 cycles
FOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING. INSTALLED GIRT BAR RELEASE STOP ASSY REF AMM 25-66-01 THIS CLEARS MEL 25-10 MDDR#114432
Part: STOP FITTING — MISSING · airframe 53,122 hrs · 39,415 cycles
DEFECT 716420: FOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING RESOLUTION: (IN PROGRESS)
Part: NONE — NONE · airframe 53,122 hrs · 39,415 cycles
DEFECT 716420: FOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING RESOLUTION: INSTALLED GIRT BAR RELEASE STOP ASSY REF AMM 25-66-01 THIS CLEARS MEL 25-10 MDDR#114432
Part: AUTOTHROTTLE SYS — FAILED · airframe 53,089 hrs · 39,402 cycles
DEFECT : LEFT AUTO THROTTLE FAILS TO ADVANCE DURING TAKEOFF. RESOLUTION: REF LOGPAGE 71649 ITEM #2 R&R GEARBOX ASSY IAW AMM 22-31-00. THIS CLEARS MEL 22-4 MDDR# 114373.
2020
Part: SLAT SYSTEM — WARNING LIGHT · airframe 47,991 hrs · 37,405 cycles
#8 LED DID NOT EXTEND FULLY LE TRANSIT ILLUMINATED. PERFORMED FSEU BITE PER FIM 27-51 TASK 801. NO EXISTING FAULTS . PERFORMED FIM 27-88 TASK 804, NO FAULTS FOUND. VISUALLY INSPECTED SENSOR, OPERATED FLAPS SEVERAL TIMES. ALL OPS AND INDICATIONS NORMAL.
Part: SHUTOFF VALVE — MALFUNCTIONED (PARKING BRAKE) · airframe 47,903 hrs · 37,366 cycles
PARKING BRAKE ILLUMINATED AFTER TAKE OFF. CREW DECLARED EMERGENCY AS PRECAUTION. REPLACED PARKING BRAKE SHUT OFF VALVE IAW AMM 32-44-21 INSTALLATION TEST GOOD, NO LEAKS NOTED.