N825SY
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
R-1 DOOR SLIDE, GILT BAR SKIRT IMPROPERLY STOWED. PERFORMED ADJUSMENT R-1 DOOR SLIDE, GILT BAR SKIRT IAW AMM 25-66-01
L1 DOOR SLIDE GIRT BAR SKIRT IMPROPERLY STOWED (WORK IN PROGRESS)
AFTER TAKEOFF FWD GREEN RIGHT GEAR LIGHT REMAINED ILLUMINATED. OVHD GEAR LIGHTS WERE EXTINGUISHED. REMOVED AND REPLACED R/H GEAR DOWNLOCK SENSOR S0073. SENSOR ADJUSTMENT AND OPS TEST CHECKS GOOD. REF AMM 32-61-31. (EMRGENCY DECLARED)
R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-06. OPS CHK GOOD
AFT RIGHT OVERWING DOOR EMERGENCY LIGHTS INOP FOUND BROKEN WIRE ON AFT R/H OVERWING EXIT WINDOW LIGHT, REMOVED AND REPLACED AFT R/H OVERWING WINDOW LIGHT ASSY REF AMM 33-21-00.
L1 DOOR EXTERIOR EMERGENCY DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK REF 33-51-06. NO HELP. CHECKED FOR POWER AT CONNECTOR D11072. NO VOLTAGE. REMOVED AND REPLACED BATTERY POWER SUPPLY REF AMM 33-51-06. NO HELP. BUT NOW FOUND 6.5 VDC AT CONNECTOR D11072. CLEANED CONTACTS AT FWD ESCAPE SLIDE LIGHT SOCKET, OPS CHK GOOD.
CREW REPORTED, THE LT FWD EMERGENCY OVERWING EXIT DOOR LANYARD POUCH HANGING DOWN. INSTALLED TWO STUDS FOR LT FWD OVERWING EXIT DOOR LANYARD IAW AMM 52-22-51. OK FOR SERVICE.
SEAT BACK METAL PROTRUDING AND POCKET TORN. OPEN
L1 ESCAPE SLIDE VERY LOOSE WHEN DISARMED AND GIRT BAR IS IN RETAINER CLIP. TIGHTENED L1 SLIDE GIRT BAR HOLDER REF AMM 25-61-06
L1 WINDOW FRAME CRACK - PERMANENT REPAIR - LH - - C/W BY ATS 80761C ACCOMPLISHED SB 737-53-1336 REV 1 DATED OCT 23, 2014
CENTER EMERGENCY EXIT LENS BROKEN - R & R CENTER EMERGENCY EXIT ROW LENS IAW AMM 33-51-01
L1 DOOR SLIDE GIRT BAR RETAINING LOOPS LOOSE IN COVER, REMOVED SLIDE IAW AMM 25-66-01 TO TIGHTEN RIVETS ON GIRT BAR RETAINING LOOPS IAW SRM 51-40-02. INSTALLED SLIDE IAW AMM 25-66-01.INSPECTED SLIDE WHEN ITS INSTALLED REF AMM 25-66-01.
DEFECT 714466: EXPERIENCED 4 INNTERMITTENT , AFT CARGO FIRE ALERTS FROM 37,000 FT TO 8000 FT. LONGEST OF 10 SECOND DURATION. ALWAYS WENT OUT ON ITS OWN. - RESOLUTION: PERFORMED FIM 26-16 TASK 801 NO DEFECTS NOTED. REMOVED AND REPLACED AFT CARGO CEU IN REF. TO AMM 26-16-02 OPS CHECK GOOD. OKAY FOR SERVICE.
DEFECT 796983: 2L SLIDE HOUSING COVER BROKEN. RESOLUTION: REAPPLIED 2L SLIDE HOUSING COVER REF AMM 25-66-00 OK FOR SERVICE
DEFECT 796963: 1R DOOR BRACKET FOR GIRT BAR LOOSE. RESOLUTION: FOUND DEBRIS IN GIRT BAR BRACKET AND ON GIRT BAR REMOVED CLEANED AND REINSTALLED REF AMM 25-66-01. OPS CHECK GOOD OK FOR SERVICE.
ON APPROACH WITH FLAPS 30, GEAR EXTENDED, HYD B QTY WAS 69-70% AND PRESSURE AT 2870. AILERONS BEOND 10-15 DEGREES OF BANK WERE VERY STIFF AND HARD TO GET BEOND. CONTROLS REMAINED STIFF ON ROLL OUT UNTIL FLAPS RETRACTED. LUBRICATED AILERON POGO QUADRANT PER AMM 12-22-11, FOUND AILERON CONROL FORCE TO BE WITHIN LIMITS PER FIM TASK 27-11 TASK 804
CRACK AT WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB ON STA 663 BTW LBL 31.83 AND LBL 45.64. REPAIRED PER B737-800 SRM 57-10-10 REPAIR 3 PAR 5 AND REPAIR 6.
RH WING TE FIXED UPPER PANEL BTW #7 GROUND SPOILER AND #8 FLIGHT SPOILER DAMAGE. FIXED UPPER PANEL BETWEEN #7 GROUND SPOILER AND #8 FLIGHT SPOILER (W.S. 278.50) ON BOTTOM SIDE OF PANEL WAS REPAIRED PER B737-800 SRM 51-70-05-2R-0 REPAIR GENERAL WITH REFERENCE TO B737-800 SRM 57-51-01-2RT-1 REPAIR 1 PAR 4. B. TA- BLE 201.
12D EMERGENCY EXIT LIGHT COMING OFF FLOOR. SECURED FLOOR PROXIMITY LIGH AT ROW 12D REF AMM 33-51-15. OK FOR SERVICE
DEFECT 7533444: 12D EMERGENCY EXIT LIGHT COMING OFF FLOOR. RESOLUTION: SECURED FLOOR PROXIMITY LIGH AT ROW 12D REF AMM 33-51-15. OK FOR SERVICE.
CRACK ON INNER SKIN OF FWD CUTOUT AT EXTERNAL POWER RECEPTACLE DOOR.INNER SKIN OF FWD CUTOUT AT EXTERNAL POWER RECEPTACLE DOOR WAS REPAIRED PER B737-800 SRM 53-10-15-2R-5 REPAIR 5
FLAPS LOCKED AT 25 DEGREES PRIOR TO LANDING. PERFORMED FIM 27-51 TASK 801. NO ACTIVE FAULTS. PERFORMED OPS CHK OF TE FLAPS REF AMM 27-51-00. NO FAULTS NOTED.
DEFECT 763214: 1L BOARDING DOOR SLIDE IS EXPOSED AND COMING OUT BY GIRT BAR. - - - RESOLUTION: RE-STOWED L1 SLIDE PER AMM TASK 25-66-01. A/C OK FOR SERVICE.
DEFECT 715333: GIRT BAR AT DOOR 1L WILL NOT STAY STOWED IN DISARMED POSITION. RESOLUTION: ADJUSTED GIRT BAR LATCH PER AMM 12-25-41. OPS CHECK GOOD.
DEFECT WORK ORDER N/R-00003 EXTERIOR RH AFT R2 DOOR EMERG LIGHT INOP. RESOLUTION: RE-LAMPED R2 DOOR EMERGENCY EXIT LIGHT. REF AMM 33-51-04.
DEFECT: SPD LIM AMBER INDICATION ON CA PFD AFTER TAKE-OFF WITH INTERMITTENT STICK SHAKER. LOW SPEED LIMIT TAPE CAME UP TO 280 KIAS. RESOLUTION: ACOMPLISHED DFCS BITE. FOUND #1 SMYD FAULTED 3 TIMES ON LAST FLT LEGRPLACED #1 SYMD PER AMM 27-32-42 SND TESTED PER AMM 27-32-00-740-803. ALSO REPLASED CAPT'S SIDE AOA SENSOR. PRECAUTIONARY PER AMM 34-21-05 AND TESTED PER 34-21-05-730-801
DEFECT: SPD LIM AMBER INDICATION ON CA PFD AFTER TAKE-OFF WITH INTERMITTENT STICK SHAKER. LOW SPEED LIMIT TAPE CAME UP TO 280 KIAS. RESOLUTION: ACOMPLISHED DFCS BITE. FOUND #1 SMYD FAULTED 3 TIMES ON LAST FLT LEGRPLACED #1 SYMD PER AMM 27-32-42 SND TESTED PER AMM 27-32-00-740-803. ALSO REPLASED CAPT'S SIDE AOA SENSOR. PRECAUTIONARY PER AMM 34-21-05 AND TESTED PER 34-21-05-730-801
DEFECT: DOOR 1L GIRT BAR BRACKET ON DOOR SWIVELS BACK AND FORTH WHEN BAR IS NOT INSTALLED MX NOTIFIED 8340. RESOLUTION: REMOVED SLIDE FROM DOOR AND SECURED GIRT BAR CLAMP TO SLIDE COVER . REINSTALLED SLIDE ON DOOR PER AMM 25-66-07.
FWD ENTRY DOOR (1L) LHS GIRT BAR BRACKET LOOSE. RESOLUTION: REPLACED GIRT BAR ASSY REF M/M 25-66-00
CORROSION FOUND IN NUTPLATE @STA. 986.5, LBL 43, WL 208. CORROSION FOUND OUT OF LIMITS @ STA. 986.5, LBL 43 WL 208 PER SRM 53-70-51-1A-1, FIG 104. REPAIRED STA. 986.5 FLOOR BEAM PER SRM 53-70-51-2R-4, FIG 204.
CORROSION FOUND ON SHEAR WEB @STA. 986.5, RBL 44, WL 208. CORROSION FOUND TO BE OUT OF LIMITS @ STA. 986.5, RBL 44, WL 208 PER SRM HAS NO LIMITS. MACHINED REPLACEMENT SHEER WEB PER PO 839525-SCA. LOCATED AND DRILLED REPLACEMENT SHEAR WEB PER SRM 51-40-05-0G-0 AND DWG # 147A5712-42. REMOVAL OF DAMAGED SHEAR WEB AND INSTALLATION OF REPLACEMENT SHEAR WEB ACCOMPLISHED ON CUST CARD # 00026
CORROSION FOUND ON SHEAR WEB AROUND NUTPLATE @STA. 1016, LBL 37, WL 208. REMOVED AND REPLACED SHEAR WEB @ STA 1016, LBL 37, WL 208 IAW SRM 51-10-02-0G-0 AND BOEING DWG'S 140A9870 REV A AND DWG 147A7500 REV
CORROSION FOUND ON SHEAR WEB @STA. 986.5, LBL 44, WL 208. REMOVED DAMAGED SHEAR WEB @ STA 986.5 LBL 44 AND INSTALLED NEW WEB PER .B737 S.R.M 51-40-02-0G PARA 4.B, 7,D REV 73 AND DWG # 147A5700 REV. B
CORROSION FOUND ON FLOOR SUPPORT @STA. 947+11, LBL 49, WL 208. CORROSION ON FLOOR SUPPORT STA 947+11 LBL 49 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM. REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW FLOOR SUPPORT P/O# 839922/1 I.A.W. SRM 51-40-02-0G-0 REV: 73 AND BOEING DWG 147A5650 REV: A.
CORROSION ON INTERCOSTAL ( FLEX SEAL WEB) ,FWD SIDE OF AFT PRESSURE BULKHEAD AT STA1028, RBL 28, WL209. INTERCOSTAL FOUND DAMAGE OUT OF LIMITS PER IAW-SRM. 53-80-08-1A-1, 4F DETAIL D REV 73. REMOVED AND REPLACED NEW REPLACEMENT INTERCOSTAL IAW-B-737-SRM-51-40-02, DWG 148A0922