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
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
FWD GALLEY EMERGENCY ESCAPE COVER WITH INSPECTON LENS BROKEN. OPEN
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"
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.
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.
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
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 .
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
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.
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.
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.
LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG.
LH HORIZONTAL STABILIZER FRONT SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT LH HORIZONTAL STABILIZER REAR SPAR LOWER LUG.
RH HORIZONTAL STABILIZER REAR SPAR LOWER LUG BUSHING DAMAGED. REPLACED BUSHINGS AT RH HORIZONTAL STABILIZER REAR SPAR LOWER LUG.
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".
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".
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".
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
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".
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".
UPPER FUSELAGE, AT STA 727J+8",LBL 44", SEAT TRACK, FLANGE WITH ELONGATE HOLE
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.
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".
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".
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.
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
RH WING REAR SPAR FUEL BOOSTER CUTOUT LOWER AREA WITH CORROSION. REPAIRED
REPAIRED WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB UPPER SECTION.
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.
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.
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
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
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
DEFECT 716420: FOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING RESOLUTION: (IN PROGRESS)
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.
#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.
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.