N826SY
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
R2 DOOR GIRT BAR LEFT HAND SIDE OF BAR, THE PLASTIC PIECE IS BROKEN, DEBRIS FOUND WAS FROM AN OLD PIECE. RENTENSION CLIP IS INSTALLED AND SECURED AT 2R DOOR GIRT BAR. OK FOR SERVICE REF 25-66-01.
FOUND RH AFT EMERGENCY OVERWING EXIT LIGHT INOP. R/R RH AFT EMERGENCY OVERWING EXIT LIGHT LAMP IAW AMM 33-51-04-960-801. NO HELP. R/R RH AFT EMER OVERWING EXIT LIGHT ASSEMBLY IAW AMM 33-51-04-960-802. NO HELP. SIDEWALL PANEL AND SEATS REMAIN REMOVED. REQUIRE RE-INSTALLATION. REPLACED BATTERY PACK. R/H AFT EMERGENCY OVERWING EXIT LIGHT OPS. CHECKS GOOD REF AMM 33-51-06. RESSURIZED AC AND REINSTALLED PANELS, OPS CHECK GOOD REF AMM 33-51-04
FWD RH AND LT EMERGENCY DOORS EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACE EMERGENCY BATTERY PACK IAW B737-800 MM 33-51-06 OPS CHECK GOOD ON FWD RH AND LH OVERWING DOORS EMERGENCY LIGHT IAW B737-800 MM 33-51-06.
2L LAV LOWER RIGHT INSIDE LAV TRIM BROKEN AND SHARP. RESECURED 2L LAV TRIM PIECE. REF CMM 25-43-78. OK FOR SERVICE
SMALL CRACK IN THE MIDDLE SECTION OF THE GLASS ON CAPTAINS SMOKE GOGGLES (BW #9425 MC NOTIFIED). REMOVED AND REPLACED CA SMOKE GOGGLES IN REF AMM 25-64-00. OKAY FOR SERVICE.
FOUND AREAS OF FLOOR PATH LIGHTING NOT ADHEREING TO CABIN FLOOR REAFIXED FLOOR PATH LIGHTING IAW 33-51-00. BUTT JOINT GAP REQUIRED PER ITEM 12 OF TASK CARD ST02269NY-800-14. BS 520 BUTT JOINT MARKED AT ISLE CARPET BUTT JOINT READJUSTED THE BUTT JOINT GAP AT BS 520 AND REPLACED THE LOOSE PHOTOLUMINESCENT IAW ENG TC ST02269NY-800-14.
NO SMOKING LIGHTS INOP AT THE FOLLOWING SEAT LOCATIONS: 6D, 11D, 29D, 10A, 19A RELAMPED NO SMOKING LIGHTS 6D, 11D, 29D,10A,AND 19A REF AMM 33-25-00. OK FOR SERVICE
BOTH BRAKE SMOKING ON LANDING UP TO GATE. INSP NR 1 & 2 BRAKES IAW AMM 32-41-41. NO LEAKS NOTED, SUSPECT DEICING FLUID.
LEFT FWD OVERWING EMERGENCY EXIT DOOR MAINT ASSIST STRAP MISSING TRIM RETAINING STUDS. SECURED THE LT FWD OVERWING EXIT DOOR ASSIST HANDLE TRIM ASSY. REF AMM 52-22-51.
6-12ABC EMERGENCY AREA LIGHTS FAILED CAPACITY CHECK RETEST. PER AMM 33-51-06-200-801 STEP 5 REMOVED AND REPLACED AFT POWER SUPPLY BATTERY PACK REF: 31-51-06-960-805. EMERGENCY LIGHTS CHECK GOOD.
1L DOOR SLIDE SAGS AND SEEMS TO MAKE A POPPING NOISE ON CLIMB OUT INSPECTED SLIDE PACK PER AMM 25-66-01 NO DEFECTS NOTED OK FOR SERVICE A&P 3353509
2L EMERGENCY EXIT PLACARDS (TOP AND BOTTOM) AND FLOOR EXIT LIGHTING IN THE AFT CABIN DID NOT ILLUMINATE WITH AC POWER OFF. REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.
THE EMERGENCY LIGHTING STRIP ON THE FLOOR IS NOT SECURED TO THE FLOOR ROW 12 & 13. RESECURED STRIP @ ROW 12 & 13 REF AMM 25-27-31. OK FOR SERVICE.
ON WALKAROUND FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS PUSHED OUT & LIGHT INOP. - RESOLUTION: RELAMPED L1 DOOR EMERGENCY EXIT (SLIDE) LIGHT, CHECKS GOOD. REMOVED DAMAGED LENS.
L1 DOOR SLIDE PARTIALLY DEPLOYED FROM SLIDE CANISTER. GIRT BAR WAS ARMED WHEN DOOR PARTIALLY OPENED. REF LOG PAGE 797561 ITEM 2 FOR SLIDE REPLACEMENT, REF 797561 - L1 DOOR SLIDE INSTALLED REF AMM 25-66-01 GOOD FOR SERVICE
DEFECT 797311: FORWARD ALLEY EMERGENCY CABINET EQUIPMENT DOOR LATCH STUCK. RESOLUTION: LUBED LATCH FWD GALLEY CABINET DOOR LATCH. OPS CK GOOD REF AMM 25-64-00.
DEFECT 734522: #2 FIRE EXTINGUISHING TEST FAILED. - - RESOLUTION: PERFORMED OVERHEAT DETECTION TEST, OPS CHECK GOOD. REF AMM 26-10-00 THIS CLEARS MEL 26-2-2 MDDR#127822
WORK ORDER FS240102: COROSION FOUND ON LH SIDE EXTERNAL FUSELAGE SKIN AT STA 917 BTWN STR21 AND STR22 L, LAV VENT. - - RESOLUTION: REMOVED CORROSION ON LH SIDE EXTERNAL FUSELAGE SKIN AT 917 BTWN STR 21 L STR22 L, LAV VENT IAW B737 SRM 51-10-02 EVALUATED ARE ON LH EXTERNAL FUSELAGE SKIN AT STA 917 BTWN STR21 AND STR22 L, LAV VENT,
WWORK ORDER FS 2400102: SCRATCH FOUND ON EXISTING REPAIR, L/H SIDE EXTERNAL FUSELAGE AFT OF L2 DOOR APPROX BS 1016 BTWN STR 12L AND STR 17L. - - CORRECTIVE ACTION: ACCOMPLISHED DOUBLER REPAIR AT LH SIDE EXTERNAL FUSELAGE SKIN BTWN STA 1016 TO STA 1040 BTWN STR 12L TO 17L IAW EA 24006 REV IR
CRUZ FLIGHT HYDRAULIC QTY ON SYSTEM A DROPPED TO 22%.PRESS STAYED NORMAL TILL T/R DEPLOYED. DROPPED TILL 1700 PRESS FOR A FEW SEC. REPLACED A HYD UNION AND HOSE AT LH MLG DOWNLOCK ACTUATOR OPS AND LEAK CK GOOD REF AMM 32-32-51
DOOR 1L GIRT BAR HOLDER LOOSE. REMOVED DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-66-01. SHOT NEW RIVET IN GRIT BAR HOLDER IAW SRM 51-40-02. INSTALLED ESCAPE SLIDE IAW AMM 25-66-01.
R1 GIRT BAR BRACKETS ON DOOR ARE LOOSE. - - : ADJUSTED GIRT BAR BRACKETS REF AMM 25-66-00
EXIT LIGHT ABOVE 14F FELL OFF. INSTALLED EXIT SIGN COVER REF AMM 33-51--01-960--801.
DEFECT 752823: 2L DOOR EXIT FELL OFF ON LANDING. - RESOLUTION: RESECURED EXIT SIGH LIGHT COVER IAW AMM 33-51-01.
DEFECT 752815: EXIT SIGN LEFT SIDE AFT GALLEY FELL OFF. - RESOLUTION: RESECURED LH EXIT SIGN LENS ON AFT GALLEY IAW AMM 33-51-01. OK FOR SERVICE.
WORK ORDER 77245, NR00142: HIDDEN DAMAGE: AFTER REMOVED ANGLE, CRACK ON STRINGER S-26R STA 500I WAS FOUND AT FORWARD CARGO COMPARTMENT. - RESOLUTION: STRINGER S-26R AT STA 500I IN FORWARD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R-1
DEFECT W/O 83430 NRC00006 RH AFT OVERWING EXIT EMER LIGHT INOP - - RESOLUTION: RELAMPED OUTSIDE AFT R/H OVERWING EXIT LIGHT IAW 33-51-00.
ROW 16CBA EMER LIGHT INOP. R & R ROW 16ABC EMERGENCY LIGHT HOUSING ASSY IAW AMM 33-51-00. OPS CHECK GOOD
ROW 14 CBA EMER LIGHT INOP. REPLACED LAMP IAW AMM 33-51-03. OPS CK GOOD.
ROW 12D EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LENS AT SEAT 12 D IAW AMM 33-51-03. OK FOR SERVICE.
FLIGHT SCX343: L1 DOOR SQUEAL â CREW HELD SE OF KMSP TO BURN FUEL TO GET BELOW MAX LANDING WEIGHT â FLIGHT LANDED RWY 30L AT KMSP WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER OWN POWER. (IN PROGRESS)
ON TAKEOFF, SOUND OF LEAKING AIR BEGAN DURING CLIMBOUT NEAR L2 WINDOW AND L1 DOOR. BECAME LOUDER WITH INCREASED SPEED. OVERWEIGHT LANDING 154,500 POUNDS. TOUCHDOWN AND BRAKING ALL NORMAL INDICATIONS. EMERGENCY DECLARED - CREW HELD SE OF KMSP TO BURN FUEL TO GET BELOW MAX LANDING WEIGHT â FLIGHT LANDED RWY 30L AT KMSP WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER OWN POWER - - REF WO#82270, NON-ROUTINES 1 THRU 4, L1 UPPER HINGE ARM DOOR BOLT ACCESS WAS SEALED, AND L2 WINDOW SEAL INSPECT BOTH L1 + L2 WERE LEAK CHECKED GOOD PER AMM 21-31-00.
DEFECT 770109: FA REPORTS 1 R GRIT BAR BRACKET LOOSE. - - - RESOLUTION: ADJUSTED GRIT BAR PER AMM 25-66-00.
DEFECT 769274: DOOR 1R SLIDE IS NOT STORED CORRECTLY. - - - RESOLUTION: REMOVED AND RE-INSTALLED 1R EMERGENCY SLIDE IAW AMM 25-66-01 FIT CHECK GOOD.
DEFECT 722637: R1 GIRT BAR WILL NOT STAY ATTACHED TO DOOR WHEN DISARMED. - - - RESOLUTION: ADJUSTED CLIP ON DOOR THAT SECURES GIRT BAR AS REQUIRED. OK FOR SERVICE.
DEFECT W/O 78001 NON-ROUTINE CARD 0001: AFT SERVICE DOOR (RH REAR GALLEY DOOR): EXCESSIVE DISTANCE BETWEEN GIRT BAR AND LOWER EDGE OF SLIDE COVER. RESOLUTION: REPACKED AND REINSTALLED R2 DOOR SLIDE REF AMM 25-66-01.
DEFECT 714523: EMERGENCY LIGHT( EXTERIOR L1 DOOR) DOES NOT ILLUMINATE WHEN IN ON POSITION: RESOLUTION:
DEFECT 714523: EMERGENCY LIGHT( EXTERIOR L1 DOOR) DOES NOT ILLUMINATE WHEN IN ON POSITION. RESOLUTION: RR"D BATTERY AND BATTERY [OWER SUPPLY IAW AMM 33-51-00. OPS CHECK GOOD.
DEFECT 714515: 14A EMERGENCY EXIT DOOR DOWN LIGHT INOP. RESOLUTION: (IN PROGRESS)
14A EMERGENCY EXIT DOOR DOWN LIGHT INOP. REMOVED AND REPLACED BALLAST IAW B737800 AMM 33-29-00-0960-804. OSP CHECK GOOD. NO DEFECTS NOTED.
DEFECT WORK ORDER 74176: AFT LEFT EMERGENCY LIGHTS INTERMITTENT WHEN USING AFT FA PANEL. RESOLUTION: COULD NOT DUPLICATE PER AMM 31-51-00. OPS CHECK GOOD.
DEFECT WORK ORDER 74176 : RESOLUTION: COULD NOT DUPLICATE PER AMNM 31-51-00. OPS CHECK GOOD.
DEFECT 725566: EMERGENCY AREA LIGHT AT 31ABC, CEILING, IS INOP. RESOLUTION: R AND R'D THE EMERG. AREA LAMP AT 31ABC, CEILING, IAW AMM 33-51-03. OP CHK GOOD, OK FOR SVC.
DEFECT: RH HORIZONTAL STAB RIB AT STA 92.70 #2 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB CRACK AT STA 92.70 STIFFENER PER B737 SRM 55-10-09-2R-4 REV 75.
DEFECT: RH HORIZONTAL STAB RIB AT STA 92.70 #1 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB AT STA 92.70 STIFFENER PER B737 SRM 55-10-09-2R-4 REPAIR 4 REV 75
DEFECT: LH HORIZONTAL STAB RIB AT STA 92.70 #3 STIFFENER IS CRACKED. RESOLUTION: REPAIRED #3 STIFFENER ON LH HORIZONTAL STAB RIB STATION 92.70 IAW B737-800SRM55-10-09-2R-4.
DEFECT: LH HORIZONTAL STAB RIB AT STA 92.70#2 STIFFENER IS CRACKED. RESOLUTION: REPAIRED #2 STIFFENER ON LH HORIZONTAL STAB RIB STATION 92.70 IAW B737-800SRM-55-10-09-2R-4.
DEFECT: RH HORIZONTAL STAB RIB AT STA 123.85 #3 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB CRACK AT STA 123.85 STIFFENER PER B737 SRM 55-10-09-2R-4 REV 75.
DEFECT: CRACK FOUND IN R/H HORIZONTAL STAB LWR INSPAR SKIN 134" FROM I/B EDGE AND 25" FROM L/E. RESOLUTION: REPAIRED R/H HORIZONTAL STABILIZER LOWER INSPAR SKIN 134" FROM I/B EDGE AND 25" FROM L/E IAW B737 SRM 55-10-01-2R-11 REV 75. REPAIR IS A CAT B. INSPECTION THRESHOLD 56,000 TOTAL FLIGHT CYCLES PER B737 SRM 55-10-01-2R-11 REV 75 TABLE 204.
DEFECT: REPAIRED RH HORIZONTAL STABILIZER LOWER INSPAR SKIN 98" FROM I/B EDGE AND 16" FROM L/E IAW SRM 55-10-01-2R-11 REV 75. REPAIR IS CAT B. INSPECTION THRESHOLD IS 56,000 TOTAL FLIGHT CYCLES PER SRM 55-10-01-2R-11 REV 75 TABLE 204.
***TRANSFER FROM LOG BOOK PAGE 692172 DEFECTIVE ITEM #2*** DURING WALKAROUND, FOUND POSSIBLE CRACK IN L/H HORIZONTAL STAB LOWER SKIN. RESOLUTION: REPAIRED L/H HORIZONTAL STABILIZER LOWER INSPAR SKIN I/B EDGE END 33" FROM L/E IAW SRM 55-10-01-2R-11 REV 75. REPAIR IS CAT B INSPECTION THRESHOLD 56,000 TOTAL FLIGHT SYSLES PER SRM 55-10-01-2R-11 REV 75 TABLE 204.
CABIN FLOOR STRUCTURE, SHEAR WEB STA. 1016 TO PRESSURE BULKHEAD RBL6 CORRODED. PERFORMED BLEND REPAIR IAW ATS ER 21-02631 REV IR
CABIN FLOOR STRUCTURE, STIFFENER STA. 990 RBL42 CORRODED. REMOVED AND REPLACED SUPPORT STIFFENER STA 990 RBL 32-44 IAW B737 SRM 51-40-02-0G-0 AND DWG 14A5700.
SMELLED SMOKE AT V1 F/AS CALLED WITH SMELL IN CABIN. FOUND #1 & #2 ENGINE OIL TANKS TO BE OVERSERVICED. DRAINED TO PROPER LEVELS REF MM 12-13-11. REF FIM 71-05 TASK 807 STEP B (2) RAN BOTH ENGINES AT SEVERAL POWER SETTINGS INCLUDING T.O. POWER. NO FURTHER SMOKE IN COCKPIT OR CABIN.
NUMBER 3 KRUGER FLAP, OTBD BULL NOSE, INBD HINGE POINT IS CRACKED. INSTALLED NEW BULL NOSE, STILL NEEDS TO HAVE BONDING WIRE SEALED WITH SEALANT. APPLIED SELANT AS NEEDED.
PART OF EMERGENCY LIGHTS ILLUMINATTED IN AIRCRAFT WITH SWITCH IN ARMED GARDED POSITION. OVERHEAD BIN EMERGENCY LIGHTS AT ROWS 6 & 11ABC INOP. REMOVED AND REPLACED LT AFT EMER BATTERY PACK. OK FOR SERVICE. ALSO REMOVED AND REPLACED BATTERY PACK AT LT OVER WING EXIT. PLACED ROW 6 AND 11 ABC OVERHEAD BIN EMERGENCY LIGHTS ON MEL. RELAMPED AREA LIGHTS AT ROWS 6 ABC AND 11 ABC FOR OVERHEAD BINS EMERGENCY LIGHTS. OPS TEST GOOD. THIS CLEARS MEL.