N822SY

Part: BULB — INOPERATIVE (ZONE 200) · airframe 62,689 hrs · 28,212 cycles

EMERGENCY EXIT LIGHT AT 15F INOPERATIVE. R & R EMERGENCY EXIT WINDOW LIGHT BULB AT 15F IAW: 33-21-00, OPS CHECKED GOOD.

Part: SIGHT GLASS — CLOUDY (ZONE 800 SLIDE) · airframe 62,498 hrs · 28,166 cycles

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

Part: COVER — BROKEN (ZONE 200) · airframe 62,498 hrs · 28,166 cycles

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

Part: WINDOW — DEBONDED (SLIDE COVER) · airframe 62,498 hrs · 28,166 cycles

DISBONDED & OPAQUE WINDOWS (4 EAS) OF PRESSURE GAUGE OF ALL SCAPE SLIDE PACKS. OPEN

Part: FRAME — CRACKED (ZONE 200) · airframe 62,498 hrs · 28,116 cycles

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.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 62,498 hrs · 28,166 cycles

BROKEN COVER OF EXIT EMERGENCY LIGHT OF DOOR L1. OPEN

Part: WINDOW — DEBONDED (SLIDE COVER) · airframe 62,498 hrs · 28,166 cycles

DISBOND WINDOW OF L1 AND R2 ESCAPE SLIDE COVERS. OPEN.

Part: COVER — DEBONDED (DOOR SLIDE) · airframe 62,498 hrs · 28,166 cycles

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.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 62,498 hrs · 28,166 cycles

DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, FWD CEILING EMERG LIGHT DONT TURN ON. EMERGENCY LIGHTS, FWD CEILING EMERG LIGHT BULB WAS REPLACED PER B737-800 AMM. 33-51-03-960-801.

Part: LIGHT — NO TEST (ZONE 200) · airframe 62,498 hrs · 28,166 cycles

DURING OPS CHECK OF THE EMERGENCY LIGHTS, FWD CEILING EMERG LIGHT DONT TURN ON. OPEN.

Part: DOOR — FAULTED (ZONE 800) · airframe 61,641 hrs · 27,734 cycles

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.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 61,641 hrs · 27,734 cycles

2L DOOR ESCAPE SLIDE EMREGENCY LIGHT INOP. - RESOLUTION: RELAMPED 2L EMERGENCY SLIDE LIGHT. OPS CHECKS GOOD.REF AMM 33-51-04

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 61,641 hrs · 27,734 cycles

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

Part: BULB — INOPERATIVE (ZONE 200) · airframe 61,641 hrs · 27,734 cycles

#!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.

Part: COVER — DETACHED (ZONE 800) · airframe 60,414 hrs · 27,257 cycles

DEFECT 733939: 14 ABC EMERGENCY EXIT HANDLE COVER NOT ADHEARING TO AIRCRAFT. RESOLUTION: REPLACED WORN VELCRO REF AMM 52-22-00.

Part: COVER — DETACHED (ZONE 800) · airframe 27,257 hrs · 16,018 cycles

DEFECT 733939: 14 ABC EMERGENCY EXIT HANDLE COVER NOT ADHEARING TO AIRCRAFT. RESOLUTION: REPLACED WORN VELCRO REF AMM 52-22-00.

Part: COFFEEMAKER — SMOKE (ZONE 900) · airframe 60,361 hrs · 27,236 cycles

DEFECT 733921: AFT COFFEE C/B PULLED DUE TO SMOKE. - - RESOLUTION (IN PROGRESS)

Part: UNKNOWN — FUMES (CABIN) · airframe 59,429 hrs · 26,805 cycles

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

Part: UNKNOWN — FUMES (CABIN) · airframe 59,429 hrs · 26,805 cycles

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

Part: SELECTOR VALVE — FAULTED (MLG) · airframe 26,678 hrs · 59,202 cycles

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.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 59,038 hrs · 26,617 cycles

DEFECT 703565 LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED AT FLAPS 5. QRH CHECKLIST ACCOMPLISHED. SLAT #4 SHOWED AMBER - RESOLUTION: (IN PROGRESS)

Part: CONNECTOR — DISCONNECTED (EXTERIOR LIGHT) · airframe 58,873 hrs · 26,560 cycles

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.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,873 hrs · 26,560 cycles

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.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,668 hrs · 26,489 cycles

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.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,438 hrs · 26,399 cycles

CAPT L1 WINDOW ARCED DURING DESCENT WINDSHIELD CRACKED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,575 hrs · 26,029 cycles

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.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,326 hrs · 25,911 cycles

SUPPLEMENTAL SCNA20230420132S MAINTENANCE REMOVED AND REPLACED ESCAPE SLIDE. P/N 5A337-7 S/N BNG4621 POSITION: R1

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,326 hrs · 25,911 cycles

DOOR SLIDE FAILED TO INFLATE TODAY DURING TRAINING. THE THREADS WHERE THE INFLATION LINE ATTACHES TO ARE COMPLETELY STRIPPED OUT.

Part: NONE — NONE · airframe 57,023 hrs · 25,814 cycles

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.

Part: PRESSURE SYSTEM — INOPERATIVE · airframe 56,210 hrs · 37,182 cycles

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.

Part: FLAP SYSTEM — INTERMITTENT · airframe 55,642 hrs · 25,310 cycles

DEFECT: FLAP ASSYMETRY INDICATION AFTER RETRACTION. RESOLUTION: R&R FLAP POSITION INDICATOR PER AMM 27-58-02. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF POSITION · airframe 55,881 hrs · 25,410 cycles

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.

Part: SENSOR — CONTAMINATED (NLG) · airframe 51,400 hrs · 23,704 cycles

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.

Part: SUPPORT — DAMAGED (FLAP ACCESS PANE) · airframe 49,911 hrs · 23,185 cycles

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.

Part: PANEL — DELAMINATED (LEADING EDGE) · airframe 49,911 hrs · 23,185 cycles

PANEL 521PB LOWER LEADING EDGE DAMAGED. REPAIRED DELAMINATED EROSION STRIP ON PANEL 521 PB IN REF TO B737-800 SRM 57-4-01.

Part: STRUCTURE — CORRODED (BS 328) · airframe 49,911 hrs · 23,185 cycles

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

Part: PRESSURE DECK — CRACKED (BS 663.75) · airframe 49,911 hrs · 23,185 cycles

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.

Part: LOCK PLATE — GOUGED (BODY FAIRING) · airframe 49,911 hrs · 23,185 cycles

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).

Part: FLOORBOARD — BROKEN (BS 344-380) · airframe 49,911 hrs · 23,185 cycles

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).

Part: PLATE — MISSING (BODY FAIRING) · airframe 49,911 hrs · 23,185 cycles

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)

Part: PANEL — DELAMINATED (WING LE) · airframe 49,911 hrs · 23,185 cycles

PANEL 621DB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621DB IN REF TO B737-800 SRM 57-41-01.

Part: PANEL — DELAMINATED (WING) · airframe 49,911 hrs · 23,185 cycles

PANEL 521 DB DELAMINATION. REPAIRED DELAMINATION ON EROSION STRIP ON PANEL 521 DB IN REF TO B737-800 SRM 57-41-01.

Part: SUPPORT — DAMAGED (FLAP ACCESS PANE) · airframe 49,911 hrs · 23,185 cycles

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.

Part: FAIRING — DAMAGED (WIND TO BODY) · airframe 49,911 hrs · 23,185 cycles

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.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 49,911 hrs · 23,185 cycles

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).

Part: STRIP — GOUGED (BODY FAIRING) · airframe 49,911 hrs · 23,185 cycles

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).

Part: PANEL — DELAMINATED (WING LE) · airframe 49,911 hrs · 23,185 cycles

PANEL 621JB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621 JB IN REF. TO B737-800 SRM 57-41-01.

Part: UNKNOWN — MALFUNCTIONED (ENTRY DOOR) · airframe 48,710 hrs · 22,744 cycles

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.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 47,355 hrs · 22,330 cycles

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.

Part: SCUFF PLATE — CRACKED (R2 DOOR) · airframe 47,355 hrs · 22,330 cycles

THE R2 SCUFF PLATE HAS A CRACK AT THE RADIUS OUTBOARD SIDE AT THE AFT END. REPAIRED CRACK. INSTALLED R2 SCUFF PLATE.

Part: DOOR SILL — CORRODED (BS 891-1005) · airframe 47,355 hrs · 22,330 cycles

CORROSION FOUND UNDER L2 DOOR SCUFF PLATE. REMOVED AND REPLACED DAMAGED LOW SILL (CHORD) AT 2-2 DOOR AREA STA 891 TO 1005.

Part: SCUFF PLATE — CORRODED (R1 DOOR) · airframe 47,355 hrs · 22,330 cycles

CORROSION FOUND UNDER R1 DOOR SCUFF PLATE. REMOVED AND REPLACED ANGLE UNDER R1 DOOR SCUFF PLATE.

Part: INSULATION — DAMAGED (THRUST REVERSER) · airframe 44,987 hrs · 21,411 cycles

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.

Part: FRAME — CRACKED (BS 360) · airframe 44,644 hrs · 21,292 cycles

FOUND FRAME BS 360 CRACKED BETWEEN STRINGERS 7R AND 8R COMMON TO PSU RAIL SUPPORT FASTENER HOLES. REMOVED DAMAGE AND REPAIRED.