N5683A
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
DETECTOR FAULT ILLUMINATES ON CARGO FIRE TEST. COMPLETED TEST ON SYSTEM A&B CARGO FIRE TEST. OPS CHECK GOOD. IAW AMM 26-23-00.
LOWER FUSELAGE, MAIN WHEEL WELL, BS 727, LBL 16 - 49, FUEL LINE FITTING CRACKED, FOUND DURING PERFORMANCE OF ITEM 1-23. REPLACED FUEL FEED LINESHROUD DRAIN AT LOWER FUSELOAGE MAIN WHEEL WELL STA 727 FROM LBL16 TO LBL 49 IAW B737-/00 AMM TASK 20-50-11-910-810 PARAG 2D STEP (20) PAGE 89 TABLE 238
UPPER FUSELAGE, PASSENGER COMPARTMENT, FORWARD ENTRY DOOR SLIDE COVER WITH SHARP EDGES AND PEELING PAINT. IAW B737-84P BAC 5300-1 SECTION 11.2.2 REV K DATED 05-11-2018 SRM 51-20-01-0G-0 PARAG 5G REV 25 DATED 11-10-2025 AND SOPM 20-41-02 PARAG 6 REV 158 DATED 11-01-2025
FWD ENTRY AREA, FWD ENTRY DOOR L1, ESCAPE SLIDE COVER FWD RETAINER CLIP WITH SOLID RIVETS LOOSE. REPLACED SOLID RIVETS IAW B737-84P SRM 51-40-02-0G-0 PARAG 4E,4B REV 25 DATED 11-10-2025 AND AIPC 25-66-00-141 REV 98 DATED 02-15-2026
FWD ENTRY AREA, GALLEY SERVICE DOOR R1, ESCAPE SLIDE RETAINER GIRT BAR CLIPS ARE DEFORMED 2EA. (WORK IN PROGRESS)
FWD ENTRY AREA ,GALLEY SERVICE DOOR R1, ESCAPE SLIDE COVER WITH LENS CRACKED. REPLACED FWD ENTRY AREA GALLERY SERVICE DOOR R1 ESCAPE SLIDE COVER LENS IAW B737 SOPM 20-50-12 PAGE 8, PARAG 6Y REV 58, DATED 07/01/2025. SATISFACTORY CONDITION.
REPLACED RETAINER GIRT BAR CLIPS P/N: 65C16820-12 (2EA) IAW B737-800 BCF SRM 51-10-02-06-0 PARAG 4 ATTACHED WITH SOLID RIVETSIAW B737-800 BCF SRM 51-40-02 PARAG 4E AND 4B REV 25 DATED 11-10-2025 AND REFERENCE AIPC 25-66-00-14 SHEET 02 REV 98 DATED 02-15-2026
DEFECT 793137: @FL 300 LITTLE FIRE STARTED AT THE TP LEFT CORNER OF R1 WINDOW LED TO CRACKED WINDSHIELD, PERFORMED QRH IT MELTED ON SOME POINT, AND IT KEEPED CRACKING THROUGH THE REMAINING FLIGHT. - - RESOLUTION: RMEVOED AND REPLACED R1 WINDOW IAW AMM56-11-11. OP[S AND LEAK CHECK GOOD. PERFORMED LAND VERIFY AND CDS TEST IAW AMM22-11-00-700-801 AND 31-62-00-730-801 ALL SYSTEMS TEST GOOD. OK FOR SERVICE. (EMERGENCY DECLARED - AIR RETURN TO RIC, ARRIVED SAFELY )
DURING PREFLIGHT HEARD AN ELECTRICAL POP AND SAW ELECTRICAL FLASH SOMEWHERE NEAR MASTER CAUTION AND VISOR, AFTERWARDS SMELLED ELECTRICAL BURNING FOR A MOMENT. DURING INSPECTION BEHIND CAPTAIN GLARESHIELD COVER, FOUND LH FWD WINDOW HEAT WIRE PINCHED WITH EXPOSED COPPER WIRE; REPAIRED WIRE PER SWPM 20-3-12. PERFORMED WINDOW HEAT OPS CK PER AMM 30-41-00. OPS CHECK GOOD NO FAULTS NOTED. WIRE NUMBER W2108-1002-18 BELOW L1 WINDOW.
EMP# 6434 AFT CARGO COMPARTMENT FROM 727 TO 847 AT RBL21 ZEE CHANNEL WITH CORROSION. EMP# 168 QC# 25 RII# QC25 REPAIRED ZEE CHANNEL FROM 727 TO STA 847 AT RBL21 IAW B737-800 BCF SRM 53-00-53-2R-6 REPAIR 6 REV 19 (10-01-2024)(SPLICE LOCATED AT STA 727E AND STA 727E+8)
UPPER FUSELAGE MAIN CARGO CABIN, AFT ENTRY AREA, AT STA 986.5 LBL AND RBL 43 FLOOR STRUCTURE WITH CORROSION AROUND FASTENER HOLE. PERFORMED PERMANENT REPAIR AT FLOOR BEAM UPPER CHORD FLANGE STA 986.5 AT LBL43 AND RBL 43 IAW COOPESA EO# COO-EO-2024-19509 REV 00 (02/20/2024) AUTHORIZATED BY ENGINEERING TASK CARD EN-53SCA-11327 REVV (02/20/2024) AND ENG-53SCA-11328 REV 00.
UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE BETWEEN BS 663 TO BS 640 LH UPPER AILERON CONTROL CABLE WITH CORROSION. REPLACED UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE BETWEEN BS 663 TO BS 640 LH UPPER AILERON CONTROL CABLE I.A.W B737-800 AMM TASK 20-10-91-000-801 STEP 2.E.(1). THRU (7). AND AMM TASK 20-10-91-400-801 STEP 3.E. AND AMM TASK 27-11-00-820-801 STEP 2.H. SATISFACTORY CONDITION
UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE AREA AT BODY STATION 540 CENTER FUEL TANK STIFFENERS WITH CRACK AT FOLLOWING POSITIONS. RBL AND LBL7, 15, 32, 41 AND 53. REPLACED STIFFENERS P/N: 111A2401-1 (5EA) AND P/N: 111A2401-2 I-A-W B-737-800 BCF S-R-M 51-10-02-06-0 PARAG 9 REV 19 (N/10/2024) AND BOEING DRAWING 111A2000 ON STA 540 AND FOLLOWING POSITIONS RBL7, 15,32,41 AND 53 AND LBL7,15,32,41 AND 53.
LOWER FUSELAGE, BETWEEN STA 727A AND 727B AND BETWEEN STR 27LH AND 27RH, SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM STA 727A AND STA 727B BETWEEN STR 27R AND STR27L DUE TO BLEND OUT AREA NOT PERMITTED IAW COOPESA EO# COOO-EO-2024-19545-ROO (02/27/2024) AUTHORIZATED BY ENGINEEERING AUTHORIZATION 53-0175 REV 00 (02/27/2024) AND BOEING REPAIR AND DEVIATION RECORD RDR# COO-SCA-24-0107-07B THIS REPAIR IS CATEGORY A
LOWER FUSELAGE MAIN WHEEL WELL LEFT SIDE FWD BULKHEAD LOWER WEB ANGLE WITH CRACK AT LBL 24.92. REPLACED ANGLE P/N 111A1308-7 IAW B737-800 SRM 51-10-02-0G-0 PAR 9
LOWER FUSELAGE MAIN WHEEL WELL RIGHT SIDE, FWD BULKHEAD LOWER WEB WITH CRACK AT RBL 9. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE MAIN W/W R/H SIDE FWD BULKHEAD LOWER WEB AT RBL 9 IAW B737-800 BCF SRM TASK 57-10-10-1A-2 A/D2 PARAGRAPH 2.C (4)(A)6)D) AND SRM 51-70-04-2R-10 REPAIR 10 FIG 201 REV 19 DATED 11/10/2023
LOWER FUSELAGE MAIN WHEEL WELL LEFT SIDE FWD BULKHEAD LOWER WEB WITH CRACK AT LBL 40.00. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE MAIN WW LH SIDE FWD BULKHEAH LOWER WEB AT LBL 40 IAW B737-800 BCF SRM TASK 57-10-10-1A-2 A/D 2 PARAGRAPG 2.C (4)(A)6)D) AND SRM 51-70-04-2R-10 REPAIR 10 FIG 201 REV 19 DATED 11/10/2023
EMP# 6268 LOWER FUSELAGE MAIN WHEEL WELL RIGHT SIDE FWD BULKHEAD LOWER WEB ANGLE WITH CRACK AT RBL 24.92. EMP# 168 QC# 25 REPLACED ANGLE P/N 111A1308-9 IAW B737-800 SRM 51-10-02-0G-0 PAR 9
LOWER FUSELAGE RIGHT MAIN WHEEL WELL PRESSURE FLOOR STRUCTURE WITH CORROSION ARROUND GROUND STUD #G310DC LOCTED AT BS 717 RBL 30. PERFORMED PERMANENT REPAIR AT SPANWISE STIFFENER, PRESSURE FLOOR STA 716 AT RBL 30 IAW COOPESA E.0 # COO-EO-2024-19510-ROO DATED 02/21/2024, DOCUMENTED ON SUN COUNTRY EA# 53-0174 REV 00 AND DOCUMENTED ON FAA FORM 8100-9-REF ID# COO-SGA-24-0105-06C.
DEFECT 717600: L1 ESCAPE SLIDE PACK BUSTLE LOOSE. - - - RESOLUTION: INSTALLED GIRT BAR INTO RETAINING CLIPS REF AMM 25-66-01. READY FOR SERVICE.
DEFECT 743511: L1 DOOR OPENED WITH SLIDE ARMED, SLIDE PACK PARTIALLY PULLED FROM COVER. RESOLUTION: REINSTALLED SLIDE AND COVER ON L1 DOOR IAW TASK 25-66-01-400-801
DEFECT 725095: FOUND L1 DOOR GUIDE ARM MISSING HARDWARE. RESOLUTION: INSTALLED L1 DOOR GUIDE ARM HARDWARE IAW AMM 52-11-21 OPS CHECK GOOD.
DEFECT WORK ORDER N/R-N/R-00001: FOUND R/H EMERGENCY EXIT LIGHTS INOP. RESOLUTION: REMOVED AND REPLACED THE R/H EMERGENCY LIGHTS BATTERY PACK REF. AMM 33-51-06. OPS CHECK GOOD.
DEFECT: LE TRANSIT LIGHT ILLUMINATED ON APPROACH. RESOLUTION: R&R #8 IB SLAT PROX SENSOR OPS CHECK GOOD REF AMM 27-88-11 ACCOMPLISHED BITE CHECK OF FSEU NO FAULTS NOTED REF FIM 27-88 TASK 804 OK FOR SVC.
DEFECT: INFLIGHT "ANTISKID INOP" LIGHT ILLUMINATED. RAN QRH PROCEDURE 14-1. RESOLUTION: PERFORMED AACU BITE REF FIM 32-42 TASK 801. FOUND FAULT VLV2, CLEANED CONNECTOR, PERFORMED NEW BITE, NO FAULTS FOUND
NR 1 RADIO PANEL SMOKING IN FLIGHT. DIVERSION TO IFP. SOURCE OF SMOKE DETERMINED ON NR 1 ACP, NR 1 ADF SELECTOR AND INDICATOR LIGHT. REMOVED AND REPLACED NR 1 ACP, REF AMM 23-51-02. CHECKS GOOD. PERFORMED GVI OF SURROUNDING AREA, WIRING, AND CIP'S D00131 AND D00133 @ P8 AREA. NO FURTHER DEFECTS NOTED, OK FOR SERVICE.