N823SY
Registered owner: SUN COUNTRY INC, MN (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.
58 reports on file, 2017-03-05 – 2026-08-03.
Part: CARPET — UNSECURE (ZONE 200) · airframe 56,662 hrs · 32,137 cycles
ROW 1 BULKHEAD CARPET IS COMING LOSE TRIPPING HAZARD AT THE FRONT. RESECURED CARPET PER 25-00-00
Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 56,556 hrs · 32,085 cycles
ROW 16-21 ABC EMER LIGHT POWER SUPPLY FAILED TEST. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06, OPS CHECKED GOOD.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 56,556 hrs · 32,085 cycles
L1 OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 OVERWING EMERGENCY LIGHT IAW AMM 33-51-04 OPS CHKD GOOD.
Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 56,556 hrs · 32,085 cycles
FLIGHTDECK EMERGENCY LIGHT ABOVE DOOR FAILED TO TEST. R & R EMERGENCY POWER SUPPLY IAW AMM 33-51-06 OPS CHKD GOOD.
Part: FIRE DETECTOR — FAULTED (ZONE 100) · airframe 56,451 hrs · 32,039 cycles
AFT CARGO FIRE DETECTOR FAULT. OPS CHKECKED CARGO FIRE DETECTION SYSTEM IAQ AMM 26-16-00. OPS CHK GOOD. OK FOR SERVICE
Part: LIGHT — DETACHED (ZONE 200) · airframe 56,262 hrs · 31,964 cycles
SEAT AREA 12 DEF-EMERGENCY PATH LIGHTS LIFTED FROM THE FLOOR. SECURED EMER PATH LIGHTS REF AMM 33-51-15 OK FOR SERVICE
Part: STRINGER — MECHANIC ERROR (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
MISDRILLED STR 2R AT STA 500 + 3.900. ACCOMPLISHED PERMANENT REINFORCING STRINGER REPAIR AT STA 500 TO STA 500B, STRINGER 2R AS PER B737 SRM 53-00-03-2R-3 REPAIR 3, NEW STRINGER SECTION P/N BAC1498-153. 0.040" AND STRINGER SPLICES P/N 69-78188-36, P/N 69-78188-37, 0.050" THIS REPAIR IS CATEGORY "B", THE THRESOLD FOR THE STAR OF SUPPLEMENTAL INSPECTIONS IS 22.500 FLIGHT CYCLES AFTER THE INSTALLATION ON THIS REPAIR, DO REPETITIVE INPSECTION EVERY 1600 FLIGHT CYCLES AFTER THE THRESHOLD HAS BEEN REACHED I.A.W B737 SRM 53-00-03-2R-3 REPAIR 3 PARAGRAPH "5".
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
DENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 6'' AND 0.25'' ABOVE STR4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION BOEING MESSAGE #XTV-SCA-26-0015-03C AND XTREME RES #014944-12-1
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
FUSELAGE SKIN RT SIDE BS 500G + 8.5'' BETWEEN S7R GALLEY R2 DOOR DENT WAS FOUND. XTREME W.O 014944 - NRC053: FUSELAGE SKIN R/H SIDE STA 500G + 8.5'' BETWEEN STRG 7R DENT WAS FOUND .
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,493 cycles
FUSELAGE SKIN R/H SIDE STA 380 + 2'' BETWEEN STRG 6R GALLEY DOOR DENT WAS FOUND. ACCOMPLISHED PERMANET REINFORCING REPAIR DOUBLER ALUMINUM 2024TS 0.040" IN, TRIPLER REPAIR 0.063"IN, STRUCTURAL FILLER 0.080" IN, TEAR STRAP 0.050"IN AND TAPER FILLER 0.050"IN ALL REPAIR PARTS FROM 2024-T3 CLAD SHEET, AT FUSELAGE STA 380+2"IN AND 0.40"IN BELOW IF THE ST 6R AS PER BOEING MESSAGE XTV-SCA-0019-11B AND XTREME RES #014944-11-4, THIS REPAIR IS CATEGORY "A" NO FURTHER ACTION IS REQUIRED.
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
FUSELAGE SKIN, DENT WAS FOUND AT STA 500 + 0.50'' AND 0.25'' BELLOW STR 2R. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.040" TRIPLER REPAIR 0.063", STRUCTURAL FILLER 0.080" TEAR STRAP 0.050" AND TAPER FILLER 0.050" AND 0.250" BELLOW STR 2R, AS PER BOEING MESSAGE XTV-SCA-26-0020-10B AND XTREME RES #014944-15-2, THIS REPAIR IS CATEGORY "A" NO FURTHER ACTION IS REQUIRED.
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
DENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 14'' AND 0.25'' ABOVE STR 4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION, MESSAGE # XTV-SCA-26-0015-03C AND XTREME RES # 014944-12-1
Part: SKIN — DENTED (ZONE 200) · airframe 56,209 hrs · 31,943 cycles
FUSELAGE SKIN DENT WAS FOUND AT STA 440 + 8'' AND 2.50'' BELLOW STR 3L. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AND STRUCTURAL FILLER AT FUSELAGE SKIN STA 440 + 8" AND 2.50" BELLOW STR 3L PER BOEING MESSAGE: XTV-SCA-26-0018-03B. XTREME RES # 014944-13-1, FORM EP 7.04, RO DATED: 09/15/2025. THIS REPAIR IS CATEGORY "B" INSPECTION REQUIREMENTS PRIOR TO THE INSPECTION THRESHOLD OF 50.000 TOTAL FLIGHT CYCLES.
Part: HYDRAULIC SYSTEM — OVERSERVICED (ZONE 100) · airframe 55,786 hrs · 31,789 cycles
FLIGHT ATTENDANTS NOTICED AN ODOR THROUGH 10,000 FT COMING OIUT OF AIR VENTS. STILL THERE AFTER SHUTDOWN. APPEARS TO BE ELECTRCAL IN NATURE. FOUND HYD QUANITY OVER SERVICED DRAINED. PERFORMED FIM 20-00 TASK 806 NO ODOR IN CABIN ON START UP HAD HYD SMELL IN VENTS SMELL VENT AWAY AFTER OIL CONTAMINATION REMOVAL 21-00-00.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 55,745 hrs · 31,775 cycles
EMERGENCY AREA LIGHT INOP AT ROW 12DEF. REMOVED AND REPLACED EMERGENCY AREA LIGHT LAMP IAW AMM 33-51-03-960-801. OPS CHECK GOOD. A/C OK FOR SERVICE
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,609 hrs · 31,729 cycles
EMERGENCY EXIT LIGHT ON LEFT OVERWING ILLUMINATE EVEN THOUGH THE SWITCH IS OFF AND WE CAN NOT GET THE LIGHT SO TURN OFF. REPLACED LT OVERWING EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
Earlier reports · 2017–2025 · 42 reports
2025
Part: BRAKE — OVERHEATED (ZONE 700) · airframe 55,494 hrs · 31,686 cycles
OUTER LEFT MAIN GEAR BRAKE IS SMOKING DURING WALK AROUND. PERFORMED BRAKE INSPECTION REF AMM 32-41-41 NO DEFECTS NOTED OK FOR SERVICE
Part: VIEW PORT — UNSECURE (ZONE 800) · airframe 55,247 hrs · 31,575 cycles
FORWARD ENTRY DOOR SLIDE VEIWING WINDOW FOR BOTTLE PRESSURE IS NOT SECURE. REMOVED SLIDE ASSY FROM DOOR AND REMOVED SLIDE FROM COVER ASSY IAW AMM 25-66-01. BONDED VIEWING WINDOW TO SLIDE COVER REF SOPM 20-50-20. RE INSTALLED SLIDE INTO COVER AND INSTALLED DOOR SLIDE ASSEMBLY ON TO DOOR IAW AMM 25-66-01. RII OF SLIDE INSTALL INTO COVER AND SLIDE INSTALLATION ON DOOR COMPLETE.
Part: VIEW PORT — DETACHED (ZONE 800) · airframe 55,150 hrs · 31,506 cycles
L1 SLIDE VIEWING WINDOW DETACHED. REATTACHED L1 DOOR SLIDE VIEWING WINDOW REF AMM 25-66-01
Part: SIGHT GLASS — DETACHED (ZONE 800) · airframe 54,845 hrs · 31,366 cycles
L1 DOOR MOUNTED ESCAPE SYSTEM SIGHT GLASS WINDOW DETACHED. SECURED L1 DOOR ESCAPED SLIDE SIGHT GLASS COVER REF AMM 20-30-11
Part: CIRCUIT BREAKER — FAILED (ZONE 200) · airframe 54,839 hrs · 31,364 cycles
LIGHTING EMER CHRG CIRCUIT BREAKER IS POPPED RESET UNDER ADVISEMENT OF MX CONTROL AND IT POPPED AGAIN. R & R AFT EMERGENCY CHRG CIRCUIT BREAKER IAW AMM 24-21-41. OK FOR SERVICE
Part: ELECTRONIC UNIT — ACTIVATED (ZONE 100) · airframe 54,586 hrs · 31,238 cycles
AFT CARGO FIRE WARN INDICATION DISCHARGED 1 BOTTLE. (DECLARED EMERGENCY). R & R AFT CARGO FIRE BOTTLE IAW AMM 26-23-01 R & R CEU IAW AMM 26-16-02. OK FOR SERVICE
2024
Part: UNKNOWN — ODOR (COCKPIT) · airframe 53,044 hrs · 30,520 cycles
DEFECT 757099: BURNING ELECTRICAL SMELL COMING FROM L2 SLIDING WINDOW ELECTRICAL CONNECTOR AREA. RESOLUTION: PERFORMED OPERATIONAL AND VISUAL INSPECTION. NO ARCHING OR VISIBLE DAMAGE IAW AMM 30-41-00-00-801. NO DEFECTS FOUND AT THIS TIME. A/C OK FOR SERVICE.
Part: LIGHT — BROKEN (CABIN) · airframe 52,839 hrs · 30,402 cycles
WORK ORDER 80108 NR00019: BROKEN LH / RH EMERGENCY LIGHT AND RH NO SMOKE / BELT SIGNAL LENS AT AFT GALLEY SERVICE. - - RESOLUTION: (IN PROGRESS)
Part: FASTENER — MISSING (ZONE 800) · airframe 52,748 hrs · 30,360 cycles
L/H AFT OVERWING EMERGENCY EXIT ASIST STRAP HOLDER MISSING FASTENERS. REINSTALLED STRAP HOUSING PER AMM 52-22-00
Part: COVER — STUCK (ZONE 800) · airframe 52,748 hrs · 30,360 cycles
L/H AFT EMER OVERWING ASIST STRAP HOLDER COVER STUCK ON. RESECURED COVER PER AMM 52-22-00
Part: HEATER — ODOR (L2 WINDOW) · airframe 52,522 hrs · 30,267 cycles
BURNING ELECTRICAL SMELL WITH NO SMOKE COMING FROM L2 COCKPIT WINDOW ( ELECTRICALLY HEATED WINDSHIELDS; NO. 2 WINDOW ). DUE TO REPLACEMENT OF WINDOW IN DEFECT 780433, MEL 30-11-2 IS CLEARED. L2 WINDOW HEAT OKAY FOR SERVICE
Part: TRIM SYSTEM — FAULTED (STAB) · airframe 52,217 hrs · 30,133 cycles
STAB TRIM INOP IN FLIGHT. PERFORMED FIM 27-41 TASK 804. FOUND STAB TRIM MOTOR TO BE BAD. R&R STAB TRIM MOTOR REF AMM 27-41-71. OPS CHECK GOOD. PERFORMED LAND VERIFY TEST PER LLM REQUIREMENTS REF AMM 22-11-00-700-806, TEST PASSED.
Part: MOTOR — FAILED (STAB TRIM) · airframe 52,217 hrs · 30,133 cycles
STAB TRIM MOTOR INOP INFLIGHT. - - RESOLUTION: PERFORMED FIM 27-41 TASK 804. FOUND STAB TRIM MOTOR TO BE BAD. R&R STAB TRIM MOTOR REF AMM 27-41-71. OPS CHECK GOOD. PERFORMED LAND VERIFY TEST PER LLM REQUIREMENTS REF AMM 22-11-00-700-806, TEST PASSED.
Part: OVEN — ODOR (AFT GALLEY) · airframe 51,777 hrs · 29,915 cycles
AFT LH OVEN SMELLS OF ELECTRICAL WHEN ON. L/H AFT OVEN OPS CHK GOOD REF AMM 25-31-01
Part: FUEL SYS — UNKNOWN (RT FUEL TANK) · airframe 51,388 hrs · 29,774 cycles
DEFECT 710819: - - WHILE CLIMBING OUT OF RSW USING CTR TANK FUEL, RH TANK QTY BEGAN TO DECREASE. BY LEVEL OFF FUEL HAD DECREASED FROM 8800 TO 7800. CREW RAN QRH 12.6 FUEL LEAK ENG AND DIVERTED TO JAX. MECH REPORTED FUEL UNDER #2 AFTER SHUTDOWN. - - RESOLUTION: (IN PROGRESS)
Part: PROBE — FAULTED (FUEL SYSTEM) · airframe 51,388 hrs · 29,774 cycles
WHILE CLIMBING OUT OF RSW USING CTR TANK FUEL, RH TANK QTY BEGAN TO DECREASE. BY LEVEL OFF FUEL HAD DECREASED FROM 8800 TO 7800. CREW RAN QRH 12.6 FUEL LEAK ENG AND DIVERTED TO JAX. MECH REPORTED FUEL UNDER #2 AFTER SHUTDOWN. R&R FUEL PROBES F7, F9, F10 FOR R/H FUEL TANK FUEL INDICATION OPS CHECKS GOOD, IAW AMM 28-41-21-000-801.
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,062 hrs · 29,659 cycles
DEFECT 744555: PIECE OF SLIDE COMING OUT OF 1R DOOR. - - RESOLUTION: SECURED/ ADJUSTED 1R DOOR SLIDE REF AMM 25-66-01.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,794 hrs · 29,523 cycles
DEFECT WO 82365 - - LOWER R/H EMERGENCY SLIDE LIGHT INOP. REMOVED AND REPLACED BAT PACK IAW AMM 33-51-06.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,794 hrs · 29,521 cycles
LOWER R/H EMERGENCY SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED BAT PACK IAW AMM 33-51-06.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,763 hrs · 29,511 cycles
DEFECT 741933 - - - DOOR 1R ESCAPE SLIDE IS FALLING OUT OF ENCLOSURE - - - RESOLUTION - INSPECTED 1R ESACPE SLIDE IAW AMM 25-66-01-200-802. REPOSITIONED GIRT. SLIDE WAS PROPERLY INSTALLED. A/C OK FOR SERVICE.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,356 hrs · 29,337 cycles
DEFECT 81143: DURING EMERGENCY BATTERY PACK CAPACITY TEST FOUND MULTIPLE LIGHTS FAILED THE DEEP CYCLE TEST. -R1 DOOR INTERNAL LOWER EXIT LIGHT FAILED TEST. -ALL L/H AISLE LIGHTS FAILED TEST. -L/H EMERGENCY EXIT ROWS 14CBA AND 15CBA UPPER AND LOWER EXIT LIGHTS FAILED TEST. -L/H OVERWING EMERGENCY EXIT FWD EXTERNAL LIGHT FAILED TEST. -R/H AISLE LIGHTS 15(FED) THROUGH 28(FED) FAILED TEST. -R2 DOOR UPPER AND LOWER EXIT LIGHTS FAILED TEST. -R2 EXTERNAL LIGHT FAILED TEST. L2 DOOR UPPER AND LOWER EXIT LIGHTS FAILED TEST. - L2 EXTERNAL LIGHT FAILED TEST. - - - RESOLUTION: REMOVED & REPLACED EMERGENCY BATTERY PACK REF AMM 33-51-06 OPS CHECK GOOD
Part: NONE — NONE · airframe 49,227 hrs · 28,825 cycles
DEFECT W/O 76910 NR00001: EMERGENCY LIGHTS ON FWD SECTION RH BINS ARE INOP. RESOLUTION: REMOVED, REPLACED AND PERFOMED OPS CHECK OF THE EMERGENCY LIGHT BATTERY PACK M1676 IAW B737 AMM 33-51-06-960-805. OPS CHECK GOOD.
Part: COVER — DETACHED (L2 SLIDE GAUGE) · airframe 49,108 hrs · 28,779 cycles
L2 DOOR SLIDE PLASTIC COVER OVER RAFT GAUGE FELL OFF. RESECURED DOOR SLIDE PRESSURE GAUGE IAW AMM 25-66-00
2022
Part: FLAP — OUT OF POSITION (R1 GIRT BAR) · airframe 48,806 hrs · 28,658 cycles
R1 DOOR SLIDE DOES NOT LOOK LIKE IT IS SECURE. ADVISED FA, NOT TO USE THE R1 DOOR, AFTER BLOCKED IN. FOUND GIRT BAR FLAP LOOSE SLID BACK INTO COVER. VERIFIED OPERATION CHECK. .CHECKS OK. IAW AMM ESCAPE SLIDE PACK CHECK 25-66-01-200-802.
Part: SLIDE — OUT OF POSITION · airframe 48,314 hrs · 28,407 cycles
DEFECT: 721350 DOOR 1R SLIDE SLIGHTLY SLIPPING OUT. RESOLUTION: INSP SLIDE DOOR 1R. FOUND SLIDE PACK TO BE SECURE IN HOUSING. REF AMM 25-66-01 OF FOR SERVICE
Part: LIGHT — INOPERATIVE · airframe 48,180 hrs · 28,351 cycles
DEFECT WORK ORDER N/R-00002: EMERGENCY EXIT ROW 15A LIGHT INOP. RESOLUTION: RELAMPED 15A EXIT ROW LIGHT REF AMM 33-21-00. OPS CHECK GOOD
Part: NONE — NONE · airframe 47,164 hrs · 27,899 cycles
DEFECT: CRACK DAMAGE AT THE RH #3 WINDOW FRAME WAS BEYOND ALLOWABLES. RESOLUTION: REPAIRED PER SCA SCA TC 737-53-1345-02-PART1-4-RH-1.
Part: NONE — NONE · airframe 47,164 hrs · 27,899 cycles
DEFECT: CORROSION ON UPPER FLANGE OF FLOOR BEAM STA987, RBL55, WL208. RESOLUTION: REPAIRED FLOOR BEAM STA986 LBL 50-RBL 50 IAW B737-SRM-53-70-51-2R-4 REV 74.
Part: NONE — NONE · airframe 47,164 hrs · 27,899 cycles
DEFECT: CORROSION ON UPPER FLANGE OF FLOOR BEAM STA967, LBL4-LBL20,WL208. RESOLUTION: ACCOMPLISHED REPAIR OF BS967 FLOOR BEAM UPPER "T" CHORD FROM RBL2 TO RBL32 IAW ATS ER 22-01132 REV 1R DTD 01-10-2022 AND SCA-EA-53-0101 REV 00 - 02/09/2022.
Part: NONE — NONE · airframe 47,164 hrs · 27,899 cycles
DEFECT: DURING INSPECTION OF THE BS 967 FLOOR BEAM (PN 147A5505-6), CORROSION WAS FOUND ON THE UPPER FLANGE BETWEEN LBL4 AND LBL20,WL208. RESOLUTION: ACCOMPLISHED REPAIR OF BS967 FLOOR BEEAM UPPER "T" CHORD FROM RBL2 TO LBL32 IN ACCORDANCE WITH ATS ER 22-01132, REV 1R, DTD 03/10/2022.
Part: NONE — NONE · airframe 47,164 hrs · 27,899 cycles
DEFECT: CRACK DAMAGE AT THE LH #3 WINDOW FRAME WAS BEYOND ALLOWABLE LIMITS. RESOLUTION: REPAIRED PER SCA TC 737-53-1345-02-PART1-4-LH-1.
2018
Part: COWLING — DENTED (NR 2 ENGINE) · airframe 37,825 hrs · 24,156 cycles
DURING WALK AROUND FOUND DENT IN NR 2 ENGINE INLET AT 7 O'CLOCK POSITION. REMOVED AND REPLACED NR 2 ENG. INLET COWL.
Part: RUB STRIP — DAMAGED (TE FLAP) · airframe 37,792 hrs · 24,145 cycles
DURING RON CHECK FOUND RIVETS ON OUTBOARD SIDE OF NR 3 FLAP CANOE FAIRING RUB STRIP ATTACHMENTS PULLING THROUGH. REMOVED AND REPLACED RUB STRIP, SEAL AND FASTENERS.
Part: PANEL — MISSING (FUSELAGE) · airframe 37,581 hrs · 24,072 cycles
MISSING PANEL BEHIND LEFT MAIN WHEEL WELL. INSTALLED NEW PANEL BEHIND LEFT MAIN WHEEL WELL.
2017
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,034 hrs · 23,847 cycles
R/H HORIZONTAL STAB RIB HSS 92.7 CRACKED AT STIFFNER THIRD FROM FWD SPAR. REPAIRED THE RIB.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,034 hrs · 23,847 cycles
LEFT HORIZONTAL STAB RIB HSS 92.7 HAS CRACK AT STIFFNER SECOND FROM FWD SPAR. REPAIRED THE RIB STIFFENER.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,034 hrs · 23,847 cycles
RIGHT HORIZONTAL STAB RIB HSS 92.7 CRACKED AT STIFFNER FORTH FROM FWD SPAR. REPAIRED THE RIB.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,034 hrs · 23,847 cycles
RIGHT HORIZONTAL STAB RIB HSS 92.7 CRACKED AT STIFFNER SECOND FROM FWD SPAR. REPAIRED THE RIB.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,034 hrs · 23,847 cycles
LEFT HORIZONTAL STAB RIB HSS 92.7 HAS CRACK AT THIRD STIFFNER FROM FWD SPAR. REPAIRED THE RIB.
Part: WINDOW FRAME — CRACKED (L1) · airframe 36,644 hrs · 23,689 cycles
POSSIBLE CRACK L1 WINDOW FRAME UPPER LEFT CORNER. REPAIRED THE R1 WINDOW FRAME.
Part: WINDOW FRAME — CRACKED (R1 WINDOW) · airframe 36,644 hrs · 23,689 cycles
SUSPECTED CRACK AT THE R1 WINDOW FRAME UPPER RIGHT CORNER. FOUND THE CRACK IN THE R1 WINDOW FRAME OTBD, UPPER CORNER. PREFORMED NDT, HFEC AND CONFIRMED THE WINDOW FRAME IS CRACKED. REPAIRED.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,873 hrs · 23,010 cycles
THE LT FWD OVERWING EXTERIOR EMER LIGHT IS INOP. RELAMPED LT FWD OVERWING EXTERIOR EMERGENCY LIGHT.