N845SY
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
CABIN WRITE UP SEAT 11& 12 DEF EMERGENCY STRIP ON FLOOR PEELING OFF. INSPECTED EMERGENCY LIGHT PHOTOLUMINESCENT STRIP AT 11& 12 DEF. FOUND TO BE SECURE AND FUNCTIONAL REF AMM 33-51-15
AISLE CARPET CONNECTOR AT ROW 12 TRIPPING HAZARD. SECURED AISLE CARPET AT ROW 12 DEF. AMM 25-27-15. OK FOR SERVICE
AT DOOR 2-L AIRCRAFT SLIDE GIRT BAR HOLDER IS BENT. ADJUSTED 2L DOOR SLIDE GIRT BAR CLIP IAW AMM 25-64-000 . OK FOR SERVICE.
CORROSION ON ESCAPE SLIDE FLOOR FITTINGS OF R1, L1, R2, L2 (8EAS). ESCAPE SLIDE FLOOR FITTINGS OF R1, L1, R2, L2 (8EAS) WAS VERIFIED AND REPLACED PER B737-800 AIPC 25-66-02-01 AND AIPC 25-66-02-02. NEW MOUNT FITTINGS WILL BE INSTALLED WITH ROUTIN CARD 598-N845SY:SCX737-FLOOR MOUNTED.
CORROSION ON FLOORBEAM AT STA 986.5, RBL 42.5 AND LBL 42.5 ON PAX CABIN. :CORROSION ON FLOORBEAM AT STA 986.5, RBL 42.5 AND LBL 42.5 ON PAX CABIN WERE REPAIRED PER B737-800 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4
CRACKS ON PHOTOLUMINESCENT FLOOR PATH MARKING COVERS. PHOTOLUMINESCENT FLOOR PATH MARKING COVERS 3EAS WERE REPLACED PER IPC 33-51-05-88.
CRACK IN LOWER HOLE AT 9 HRS POSITION ON THE WEB, STA 727 AND S-18A (IN REF. CARD 737-53A1402-01-GRP1-CFG1-RH-INIT, ITEM 12: FIG. 4 - STEP 3). OPEN
CRACK ON VAPOR BARRIER (LOWER WEB) BETWEEN BSTA 663 & LBL 31.83 TO LBL 45.64, ALSO BETWEEN BSTA 663 & RBL 25.00 TO RBL 40. VAPOR BARRIER (LOWER WEB) BETWEEN BSTA 663 & LBL 31.83 TO LBL 45.64, ALSO BETWEEN BS 663 & RBL 25 TO RBL 40 WAS REPAIRED IAW SRM 51-70-04-2R-10, REPAIR 10.
EMERGENCY AREA LIGHT AT ROW 14ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY AREA LIGHT LAMP AT ROW 14ABC IAW AMM 33-51-03-960-801. OPS CHECK GOOD AT THIS TIME.
FOUND BROKEN CONNECTOR ON RT FWD EMERGENCY EXIT FWD HATCH HEATER. OPEN
L1 MAIN DOOR SLIDE NEEDS REPACKING. THE SLIDE PACK CHECKED IAW AMM 25-66-01-200-802. NO FAULTS NOTED, OK FOR SVC.
LEFT PICKLE FORK REPLACEMENT IS REQUIRED BEFORE RELEASE OF THE AIRCRAFT. COMPLIED WITH SC ENGEERING TC 737-53-1397-00-GRP53, FAS#8205
SPLICE REPAIR OF THE LEFT HAND AND RIGHT HAND STRINGER 10 FOR PICKLE FORK REPLACEMENT - RESOLUTION: COMPLETE: COMPLIED WITH SC ENGINEERING TC 737-53-1397-00-GRP53.
SPLICE REPAIR OF THE LEFT HAND AND RIGHT HAND STRINGER 14 FOR PICKLE FORK REPLACEMENT - COMPLIED WITH SC ENGINEERING TC 737-53-1397-00-GRP53
FAS# 8502 RH PICKLE FORK REPLACEMENT IS REQUIRED BEFORE RELEASE OF THE AIRCRAFT. FAS# 8205 COMPLIED WITH SC ENGINEERING TC 737-53-1397-00-GRP53.
DEFECT 707464: FORWARD 1R DOOR GIRT DOOR BRACKET IS VERY LOOSE RESOLUTION: ADJUSTED BRACKET REF AMM 25-66-01. OPS CHECK GOOD OK FOR SERVICE
1R GIRT BAR BRACKET BENT OUT OF PLACE. STRAITENED 1R GIRT BAR BRACKET. OPS CGECKS OK. REF AMM 25-66-02.
DEFECT 765219 - AILERON CONTROLS VERY HEAVY (STIFF) WHEN AUTOPILOT TURNED OFF. TAKES SIGNIFICANT CONTROL PRESSURE TO MOVE AILERONS. - RESOLUTION: REFERENCE WORK ORDER 83447 NON-ROUTINE CARD 00001, (SEE LOG PAGE 765219 ITEM 1. AILERON CONTROLS VERY HEAVY (STIFF) WHEN AUTOPILOT TURNED OFF.) CHECKED AILERON CONTROL CABLES CONDITION AND ROUTING. NO DEFECTS FOUND. CHECKED CABLE TENSIONS. WITHIN LIMITS. REF AMM 27-09-14. PERFORMED WHEEL FORCE TEST. TEST CHECKS GOOD. REF AMM 27-11-00-700-804. DURING AILERON OPERATION FOUND CENTER SUPPORT BEARING ON AILERON CENTERING MECHANISM HAS SEAL MOVING WITH MECHANISM SHAFT. SUSPECT BAD BEARING.(IN PROGRESS)
SUPPLEMENTAL: PERFORMED FIM 27-11 TASK 804 AND FOUND THE CONTROL WHEEL FORCE NORMAL FOR AILERON MOVEMENT. INSPECTED THE CAM FOLLOWER BEARING AND FOUND MINOR WEAR. REMOVED AND REPLACED BEARING REF. STEP E(1)(E). OPS CHECK GOOD AFTER REPLACEMENT.
ON SHORT FINAL WHEN TRYING TO CONTROL ROLL WITH AILERONS I COULD NOT MOVE THE CONTROL WHEEL MORE THAN 3 TO 4 UNITS WITHOUT GREAT DIFFICULTY. IMPOSSIBLE WITHOUT BOTH HANDS
CORROSION ON PLATES (2EAS) OF AFT CARGO COMPARTMENT. FOR EXCESS DAMAGE ON PLATES (2EAS) OF AFT CARGO COMPARTMENT WILL REPLACED PER B737-800 SRM 51-10-02-0G PAR 9.A REV 78-17-MAY-2023 AND THESE WERE VERYFIED AT B737-800 AIPC 25-52-10-19 ITEM 585 FOR PART NUMBER 453A2611-1 AND ITEM 590 FOR PART NUMBER 453A2611-2 AND THESE MUST BE INSTALLED WITH TASK CARD 446-N845SY:SCXOPEN/CLOSE-100
HIDDEN DAMAGE IN REF: NRC # 00107, DURING REMOVAL OF FWD CARGO RH SIDE PLATE , INTERCOSTAL BTW FRM 500G-500H CRACK WAS FOUND. INTERCOSTAL BTW FRM 500G-500H RH WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.
INITIAL INSPECTION: CRACK ON INTERCOSTAL BTW STA 344 & STA 360 BL 0 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). INTERCOSTAL BTW STA 344 & STA 360 BL 0 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX) WAS REPLACED PER B737-800 SRM 51-40-02-0G-0
INITIAL INSPECTION: CRACK ON INTERCOSTAL STA 285 BL 0 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). INTERCOSTAL STA 285 BL 0 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX) WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.
INITIAL INSPECTION: CRACK ON INTERCOSTAL STA 324 RBL 31 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). INTERCOSTAL STA 324 RBL 31 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX) WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.
INITIAL INSPECTION: CRACK ON INTERCOSTAL BTW STA 312 & STA 328 LBL 46 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX). INTERCOSTAL BTW STA 312 & STA 328 LBL 46 AT PASSENGER CABIN FLOOR STRUCTURE (CPAX) WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.
INITIAL INSPECTION: CRACK IN FRAME AT STA 312 & S-6L AT PASSENGER CABIN. FRAME AT STA 312 & S-6L AT PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-10-07-2R-1.
INITIAL INSPECTION :CORROSION ON SIDEWALL PANEL SUPPORTS FROM STA 500D TO STA 500H BTW STRINGER 23L AND STRINGER 25L AT FWD CARGO COMPARTMENT. SIDEWALL PANEL SUPPORTS FROM STA 500D TO STA 500H BTW STRINGER 23L AND STRINGER 25L AT FWD CARGO COMPARTMENT WERE REPLACED PER B737-800 SRM 51-40-02-0G-0.
INITIAL INSPECTION:CORROSION ON SIDEPLATE LH FROM STA 400 TO STA 500I STR 26L AT FWD CARGO COMPARTMENT. SIDE PLATE LH FROM STA 400 TO STA 500I STR 26 LH AT FWD CARGO WAS REPLACED PER B737-800 SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5 .
INITIAL INSPECTION:CORROSION ON SIDE PLATE RH FROM STA 500A TO STA 500I STR 26R AT FWD CARGO COMPARTMENT. SIDE PLATE RH FROM STA 500A TO STA 500I STR 26 RH AT FWD CARGO WAS REPLACED PER B737-800 SRM 51-40-02-0G-0
INITIAL INSPECTION: CORROSION ON SEVERAL POINTS OF ALL SIDEPLATE OF AFT CARGO COMPARTMENT FLOOR STRUCTURE RBL 21 BETWEEN STA 867 & 947. SIDEPLATE OF AFT CARGO COMPARTMENT FLOOR STRUCTURE RBL 21 BETWEEN STA 867 & 947 WAS REMPLACED PER B737-800 SRM 51-40-02-0G-0 PARAGRAPH 4 AND PARAGRAPH 7
INITIAL INSPECTION: CRACK ON WEB ON INTERNAL STRUCTURE AT REAR SPAR WS 280 APPROX RH WING. WEB ON INTERNAL STRUCTURE AT REAR SPAR WS 280 APPROX RH WING WAS REPLACED PER B737-800 SRM 51-40-02-0G-0
DEFECT 682464: SELECTED FLAPS 30 LE FLAP TRANSIT LIGHT DID NOT GET A GREEN LIGHT. RESOLUTION: FOUND FAULT CODES 27-51105, 27-81354. REMOVED AND REPLACED FSEU PER AMM 27-51-01. OPS CHECKS GOOD. NO FAULTS PRESENT.
DON`T PASS OPERATIONAL TEST EMERGENCY LIGHT AT EMERGENCY EXIT AREA LH S IDE AT PASSENGER CABIN PERFORMED FAULT ISOLATION OF THE EMERGENCY LIGHT AT EMERGENCY EXIT AREA LH SIDE AT PASSENGER CABIN IAW FIM 33-50 TASK 801 STEP 801.A THRU E.(2) THE BATTERY PACK FOUND DISCHARGED, PERFORMED CHARGED OF THE BATTERY PACK AS PER AMM 33-51-06-610-802, AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS AT EMERGENCY EXIT AREA LH SIDE AT PASSENGER CABIN IAW AMM 33-51-00-710-801 TEST IS GOOD.