N822SY
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
L2 EMERGENCY SLIDE LIGHT INOP R AND R L2 EMERGENCY SLIDE LAMP IAW AMM 33-51-04 OPS CHECK GOOD
12 DEF EMERGENCY PATH LIGHTING LIFTED FROM FLOOR. TRIPPING HAZARD. SECURED PHOTOLUMONESCENT LIGHT STRIP. REF AMM 33-51-15
L2 DOOR SLIDE HANGS BELOW BOTTOM OF DOOR. MAY CATCH WHEN OPENING OR CLOSING DOOR. REMOVED SLIDE FROM DOOR AND RE-INSTALLED FLAP ON BOTTOM OF SLIDE. SLIDE RE-INSTALLED REF: AMM 25-66-01 OK FOR SERVICE
L2 DOOR GIRT BAR CLIP LOOSE SLIDE FALLING OUT OF CLIP. ADJUSTED 2L CIRT BAR CLIPS REF. AMM 25-66-00. ITEM OKAY FOR SERVICE.
EMERGENCY EXIT LIGHT AT 15F INOPERATIVE. R & R EMERGENCY EXIT WINDOW LIGHT BULB AT 15F IAW: 33-21-00, OPS CHECKED GOOD.
CRACK ON FRAME STA 312 & S-6L AT PASSENGER CABIN . FRAME BS 312, S6L AT PASSENGER CABIN WAS REPAIRED PER SRM 53-10-07-2R-1 REPAIR 1.
BROKEN COVER OF EXIT EMERGENCY LIGHT OF DOOR L1. OPEN
DISBONDED & OPAQUE WINDOWS (4 EAS) OF PRESSURE GAUGE OF ALL SCAPE SLIDE PACKS. OPEN
DISBONDED & OPAQUE WINDOWS (4 EAS) OF PRESSURE GAUGE OF ALL SCAPE SLIDE PACKS. WINDOWS (4 EAS) OF PRESSURE GAUGE OF ALL SCAPE SLIDE PACKS WERE BONDED PER BOEING SOPM 20-50-12 AND CLENED PER B737-800 AMM 25-00-00
BROKEN COVER OF EXIT EMERGENCY LIGHT OF DOOR L1. COVER OF EXIT EMERGENCY LIGHT OF DOOR L1 WAS REPLACED PER B737-800 AMM 33-51-01
DISBOND WINDOW OF L1 AND R2 ESCAPE SLIDE COVERS. OPEN.
DISBOND WINDOW OF L1 AND R2 ESCAPE SLIDE COVERS. WINDOW OF L1 AND R2 ESCAPE SLIDE COVERS WERE BONDED PER BOEING SOPM 20-50-12.
DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, FWDÂ CEILING EMERG LIGHT DONT TURN ON. EMERGENCY LIGHTS, FWD CEILING EMERG LIGHT BULB WAS REPLACED PER B737-800 AMM. 33-51-03-960-801.
DURING OPS CHECK OF THE EMERGENCY LIGHTS, FWDÂ CEILING EMERG LIGHT DONT TURN ON. OPEN.
R/H AFT OVERWING EMERGENCY EXIT DOOR MISSING. DOOR SWINGS OUT...INJURY CAN OCCURE) REF AIPC 11-23-01-02E. - RESOLUTION: REPLACED MISSING PLACARD ON EXTERIOR OVERWING EXIT 15DEF IN REG AMM 11-23-01-890-801.
EMERGENCY LIGHTS AT 2R DOOR SLIDE,OVERDOOR,AFT CEILING, AND AFT TWO AILSE R/H SIDE ARE INOP. - RESOLUTION: REPLACED POWER SUPPLY BATTERY PACK.EMEERGENCY LIGHTS OPS CHECK GOOD. REF AMM 33-51-06
2L DOOR ESCAPE SLIDE EMREGENCY LIGHT INOP. - RESOLUTION: RELAMPED 2L EMERGENCY SLIDE LIGHT. OPS CHECKS GOOD.REF AMM 33-51-04
#!1 RIGHT EMERGENCY EXIT LIGHT FAILED, BULB WAS REPLACED REF AMM 33-51-01 - ROW 14 PLACARD ILLUMINATION LAMP ASSY. WAS RELAMPED AND A NEW FUSE INSTALLED TO NO EFFECT. SUSPECT BAD BALLEST ASSY P/N: 70-0366-11. REF CMM 33-21-43. AIPC 33-21-00-68.
DEFECT 733939: 14 ABC EMERGENCY EXIT HANDLE COVER NOT ADHEARING TO AIRCRAFT. RESOLUTION: REPLACED WORN VELCRO REF AMM 52-22-00.
DEFECT 733939: 14 ABC EMERGENCY EXIT HANDLE COVER NOT ADHEARING TO AIRCRAFT. RESOLUTION: REPLACED WORN VELCRO REF AMM 52-22-00.
DEFECT 733921: AFT COFFEE C/B PULLED DUE TO SMOKE. - - RESOLUTION (IN PROGRESS)
ISSUE WAS REPORTED IN ALB: FLIGHT ATTENDANTS COMPLAINED ABOUT FUMES IN THE MID CABIN. SYMPTOMS INCLUDE HEADACHE, NAUSEA, IRRITATED EYES AND THROAT. A/C WAS FERRIED TO MSP: THIS AIRCRAFT HAS BEEN INSPECTED FOR THE PURPOSE OF A FERRY FLIGHY FROM ALB TO MSP , AND NO KNOWN CONDITIONS EXIST THAT WOULD MAKE THIS AIRCRAFT UNSAFE.FERRY FLIGHT IS AUTHORIZED PER GMM VOL 6 (870) MAINTENACE FERR FLIGHT A&P 4799089. RESOLUTION IN MSP: PERFORMED FIM 21-00 TASK 806 NO ABNORMAL FUMES THROUGHOUT THE CABIN. OK FOR SERVICE
ISSUE WAS REPORTED IN ALB: FLIGHT ATTENDANTS COMPLAINED ABOUT FUMES IN THE MID CABIN. SYMPTOMS INCLUDE HEADACHE, NAUSEA, IRRITATED EYES AND THROAT. - THE A/C WAS FERRIED TO MSP: THIS AIRCRAFT HAS BEEN INSPECTED FOR THE PURPOSE OF A FERRY FLIGHT FROM ALB TO MSP , AND NO KNOWN CONDITIONS EXIST THAT WOULD MAKE THIS AIRCRAFT UNSAFE.FERRY FLIGHT IS AUTHORIZED PER GMM VOL 6 (870) MAINTENACE FERR FLIGHT A&P 4799089. - RESOLUTION IN MSP: PERFORMED FIM 21-00 TASK 806 NO ABNORMAL FUMES THROUGHOUT THE CABIN. OK FOR SERVICE
ON TAKE OFF GEAR FAILED TO RETRACT. 3 RED 3 GREEN RAN QRH GOT 3 GREEN NO RED AND LANDED. NO PINS FOUND INSTALLED AFTER LANDING. JCD 9056. TROUBLESHOT TO LANDING GEAR SELECTOR VALVE AND LANDING GEAR TRANSFER VALVE. ALL REMOVED AND REPLACED IAW B737 AMM 32-31-51, 32-31-71, AND 32-32-00. ALL ON ATS WO 729012 N/R-00001.
DEFECT 703565 LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED AT FLAPS 5. QRH CHECKLIST ACCOMPLISHED. SLAT #4 SHOWED AMBER - RESOLUTION: (IN PROGRESS)
DEFECT: WO 77532 NRC00357: LEFT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS INOP (BULB NO HELP). - RESOLUTION: UPON FURTHER INVESTIGATION FOUND CONN. D12036 NOT CONNECTED. RE CONNECTED PER WDM 33-51-13 AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.
DEFECT W/O 77532 NRC-00356: MULTIPLE EMERGENGY EXIT LIGHTS INOP. - RESOLUTION: REMOVED, REPLACED, AND PERFORMED GOOD TEST OF M1676 AND M1694 PER AMM 33-51-06-960-805. ALL INTERIOR EMERGENCY EXIT LIGHTS NOW WORK.
DEFECT 83606 NRC 00005: - BATTERY PACK AT ROW 21 DEF INOP. - - RESOLUTION: R&R EMERGENCY LIGHT BATTERY PACK AT ROW 21 DEF REF AMM 33-51-06.
CAPT L1 WINDOW ARCED DURING DESCENT WINDSHIELD CRACKED
DEFECT 687495: L1 SAFETY STRAP COULD NOT BE SECURED IN PLACE WHEN DOOR IS ARMED DUE TO WRONG PLACEMENT OF SCREW. - - - RESOLUTION: REPOSITIONED SAFETY STRAP AS NEEDED REF AMM 52-11-31. CHECKS GOOD. OK FOR SERVICE.
SUPPLEMENTAL SCNA20230420132S MAINTENANCE REMOVED AND REPLACED ESCAPE SLIDE. P/N 5A337-7 S/N BNG4621 POSITION: R1
DOOR SLIDE FAILED TO INFLATE TODAY DURING TRAINING. THE THREADS WHERE THE INFLATION LINE ATTACHES TO ARE COMPLETELY STRIPPED OUT.
DEFECT 716036: ESCAPE SLIDE AT L-1 DOOR, GERT BAR STOWAGE BRACKET LOOSE. RESOLUTION: ADJUSTED ESCAPE SLIDE L-1 DOOR GIRT BAR STORAGE BRACKET REF AMM 25-66-01 OK FOR SERVICE.
DEFECT: L AND RIGHT BLEED PRESSURE AT "0" AFTER TAKEOFF. CABIN ALT AT "4000" WHILE LEVELED OFF. RESOLUTION: DCPC BITE PROCEDURE, NO CURRENT FAULTS. LAST LEG HISTORY FAULT LO INFLOW/ HI LEAK. REF FIM 21-31 TASK 801. FOUND 3 C/B'S TRIPPED. P6-4 A5&A7&B7. (BLEED AIR VALVES.) RESET C/B'S AND ACCOMPLISHED ENGINE BLEED AIR TEST PER AMM 36-00-00-860-804. ALL CHECKS GOOD. CABIN PRESSURIZED NORMALLY ON GROUND WITH NO FAULTS NOTED. A/C IS OKAY FOR CONTINUED SERVICE.
DEFECT: FLAP ASSYMETRY INDICATION AFTER RETRACTION. RESOLUTION: R&R FLAP POSITION INDICATOR PER AMM 27-58-02. OPS CHECK GOOD.
DEFECT 720489: HAD MECHANIC CHECK GIRT BAR AFTER IT SLIPPED SIDEWAYS ON DOOR OPENING . RESOLUTION: CHECKED AND SECURED GIRT BAR AS PER B737 AMM TASK 25-66-01-000-804 OPS CHECKS NORMAL AC OK FOR SERVICE.
LANDING GEAR WOULD NOT RETRACT AFTER T/O. PSEU BITE NO FAULTS FOUND. PERFORMED FIM 32-30 TASK 813 LANDING GEAR CONTROL LEVER LOCK-NO FAULT FOUND, CHECKS NORMAL. FIM STATES INTERMITTANT FAULT, PSEU SELF TEST PASS REF FIM 32-09 TASK 801. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER MODULE FOR PRECAUTIONARY PURPOSES REF AMM 32-31-11. CLEANED NOSE LANDING GEAR AIR/GROUND SENSORS DUE TO HEAVY GREASE. LANDING GEAR CONTROL SYSTEM CHECKS NORMAL REF AMM 32-31-00. OK FOR SERVICE.
PANEL 194AL WING TO BODY FAIRING PANEL IS DAMAGED. REMOVED DAMAGE ON PANEL 194AC RUB STRIP ALL WORK DONE IAW B737-800 SRM 53-60-70 ALLOWABLE DAMAGE I STEP 4.D FIG, 108 D. D. NO FURTHER ACTION REQUIRED.
PANEL 621JB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621 JB IN REF. TO B737-800 SRM 57-41-01.
PANEL 621DB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621DB IN REF TO B737-800 SRM 57-41-01.
PANEL 521PB LOWER LEADING EDGE DAMAGED. REPAIRED DELAMINATED EROSION STRIP ON PANEL 521 PB IN REF TO B737-800 SRM 57-4-01.
PANEL 521 DB DELAMINATION. REPAIRED DELAMINATION ON EROSION STRIP ON PANEL 521 DB IN REF TO B737-800 SRM 57-41-01.
PANEL 643AB FLAP SUPPORT #7 FWD ASSY. ACCESS PANEL DAMAGED. REPAIRED PANEL 613AB FLAP SUPPORT #7 FWD ASSY ACCESS PANEL IN REF. TO B737-800 SRM 57-53-70.
PANEL 644AB FLAP SUPPORT #8 FWD ASSY. ACCESS PANEL DAMAGED. REPAIRED PANEL 644AB FLAP SUPPORT #8 FWD ASSY IN REF TO B737-800 SRM 57-53-70.
A GOUGE ON THE BASE STRIP ON FORWARD OF RIGHT HAND BODY FAIRING PANEL #192CR-2. (DOT NO. SKN 004). INSTALLED NEW BASE PLATE P/N 149A7185-3 IAW B737-800 SRM 51-40-02 STEP. 4.B.(1-5).
BASE BACK PLATE FOR THE LOCK IS MISSING FROM THE PLATE STRIP ON FORWARD RIGHT HAND SIDE BODY FAIRING PANEL 192CR-2. (DOT NO. SKN 003). REMOVED & REPLACED DOUBLER & BASE PLATE P/N'S 149A7185-3 & 149A7247-5 @ FAIRING PANEL 192 CR-2 R/H IAW B737-800 SRM 51-40-02 STEP 4.B.(1-5) & STEP 9.B.(1-6)
BASE LOCK PLATE AT FWD CORNER OF PANEL # 192CR-2 ON A BODY FAIRING RIGHT SIDE HAS A GOUGE. (DOT NO. SKN 002). INSTALLED NEW BASE PLATE P/N 149A7185-3 IAW B737-800 SRM 51-40-02 STEP 4.B.(1-5).
L/H ENGINE O/R T/R HAS A HOLE PUNCTURED INTO SKIN AT ABOUT 11 OCLOCK POSITION (AFT), FOUND ON INCOMING DAMAGE INSPECTION OF AIRCRAFT. REPAIRED L/H ENGINE OUTBOARD T/R SKIN AT 11 O'CLOCK POSITION (AFT) IAW B737-800 SRM 54-30-01 REPAIR 2 STEP 4 AND C AND IAW B737-800 AMM 51-21-99 STEP 3(C).
STA 328, RBL 48, HAS CORROSION AT SCREW HOLE. DOT008. REMOVED CORROSION AND FABRICATED REPAIR STRAP ON STA. 328 RBL 48. ALL WORK DONE IAW B737-800 SRM 51-10-02, 53-10-51, 51-40-05 AND AMM 51-21-41, 51-21-72
STA 344 TO 380, L/H FLOOR BOARD IS BROKEN. P/N 141A5810-183. DOT 002. REPAIRED L/H FLOOR BOARD P/N 141A5810-183 AT STA 344 TO 380 IAW B737-800 SRM 53-00-50 REPAIR 1 STEP 3 (A-O) AND B737-800 SRM 53-00-50 REPAIR GENERAL STEP 5 (M).
STATION 663.75 SECTION 44 PRESSURE DECK ABOVE MAIN WHEEL WELL JUST INBOARD OF RBL 45 6 INCHES BELOW FLOOR BOARD CRACKED. REPAIRED CRACKED BOARD AT STA 663.75 SECTION 44 PRESSURE DECK ABOVE MAIN WHEEL WELL JUST INB AT RBL 45, 6 INCHES BELOW FLOOR BOARD. ALL WORK DONE IAW B737-800 SRM 51-10-10 REP. 3 ALTERNATIVE 2 PARA 5 STEP B, AMM 20-50-11-910-801, SRM 51-40-02, SRM 51-10-10 REPAIR 3 ALTERNATIVE 2 PARA 5 STEP 0, SOPM 20-44-02 PAR 6, AMM 28-11-00 PAR 4, AMM 28-11-00 2 (D) 5 AND 6 AMM 29-00-00-790-801.
CABIN WOULD NOT PRESSURIZE BECAUSE MAIN ENTRY DOOR NOT FULLY CLOSED AND NO DOOR OPEN LIGHT. MX NOTIFIED. INSPECTED L1 DOOR AND OPERATED DOOR MULTIPLE TIMES. DOOR OPERATED NORMAL. OK FOR SERVICE.
THE R2 SCUFF PLATE HAS A CRACK AT THE RADIUS OUTBOARD SIDE AT THE AFT END. REPAIRED CRACK. INSTALLED R2 SCUFF PLATE.
CORROSION FOUND UNDER L2 DOOR SCUFF PLATE. REMOVED AND REPLACED DAMAGED LOW SILL (CHORD) AT 2-2 DOOR AREA STA 891 TO 1005.
CORROSION FOUND UNDER R1 DOOR SCUFF PLATE. REMOVED AND REPLACED ANGLE UNDER R1 DOOR SCUFF PLATE.
UNDER FLOOR PANEL 241AEF, LIGHT CORROSION IN TWO SPOTS AT STATION 1016, THE LE OF THIS PANEL ON TOP OF STATION CAP, MARKED WITH TWO STREAMERS NEAR AFFECTED AREAS. REMOVED AND REPLACED O/B STRAPS #147A5714-3 AND 147A5714-5 AT STATION 10/6.
DURING NR 2 ENGINE T/R INSPECTION FOUND UPPER INSULATION BLANKET ON THE RT T/R WITH TWO HOLES IN THE OUTER METAL SHEET ONE HOLE EXCEEDED DAMAGE LIMITS. REMOVED INSULATION BLANKET CLEANED AND PREPPED THE AREA FOR NEW INSULATION BLANKET. INSTALLED NR 2 ENG RT T/R INSULATION BLANKET.
FOUND FRAME BS 360 CRACKED BETWEEN STRINGERS 7R AND 8R COMMON TO PSU RAIL SUPPORT FASTENER HOLES. REMOVED DAMAGE AND REPAIRED.