N819SY

Part: SKIN — GROUND DAMAGE (ZONE 200) · airframe 56,840 hrs · 24,708 cycles

CATERING TRUCK RAILING MADE CONTACT AFT OF L2 DOOR. REPAIR THE DAMAGE ON FUSELAGE SKIN AT BS 1006 TO 1016 BETWEEN STR 14L TO 15L IAW SRM 53-70-01-2R-5, REPAIR 5, ALTERNATIVE 3.

Part: SKIN — GROUND DAMAGE (ZONE 200) · airframe 56,840 hrs · 24,718 cycles

CATERING TRUCK RAILING MADE CONTACT AFT OF L2 DOOR. REPAIR DAMAGE ON FUSELAGE SKIN AT FS 1006 TO FS 1016 BETWEEN STR 14L TO 15L IAW SRM 53-70-01-2R-5, REPAIR 5, ALTERNATIVE 3.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 56,829 hrs · 24,703 cycles

14ABC AND 15ABC EMERGENCY WINDOW FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB ON 14ABC AND 15ABC EMERGENCY WINDOW FWD EMERGENCY LIGHT REF AMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — DETACHED (ZONE 200) · airframe 56,605 hrs · 24,623 cycles

ROW 11 ABC SIDE EMERGENCY LIGHT STRIP COMING OFF THE FLOOR. SECURED THE PATH LIGHT STRIP NEAR ROW 11ABC IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 56,605 hrs · 24,623 cycles

L1 DOOR LEFT BRACKET FOR GIRT BAR IS LOOSE. ADJUSTED FORWARD GIRT BAR RETAINER CLIP ON L1 DOOR REF. AMM 25-66-01. OPS CHECKED GOOD.

Part: THRESHOLD — UNSECURE (ZONE 200) · airframe 56,154 hrs · 24,436 cycles

FWD GALLEY FLOOR RUBBER FLOOR TRIM IS RIPPED UP AND A TRIPPING HAZARD. REMOVED AND REPLACED THE CARPET TO MAT THRESHOLD IAW AMM 25-27-21.

Part: COFFEEMAKER — DAMAGED (ZONE 900) · airframe 56,121 hrs · 24,432 cycles

PLACARD ON FORWARD GALLEY COFFEE MAKER IS BENT AND SHARP. SECURED FWD. GALLEY PLACARD AT COFFEE MAKER PER AMM 11-32-00

Part: WINDOW — OVERTEMP (ZONE 200) · airframe 55,333 hrs · 24,097 cycles

WINDOW R3 OVERHEAT. SLIGHT ELECTRICAL WIRING SMELL WHEN SWITCH STAYS ON. REPLACED RCPT FOR R2 SLIDING WINDOW. REPLACED R2 WINDOW COIL CHORD. REF: WDM 30-41-11 AND SWPM 20-61-00. REF: W/O 94912 N/R 4 FOR RIGHT SIDE WHCU REPLACEMENT. OPS CHECKS GOOD. OK FOR SERVICE. REMOVED AND REPLACED RIGHT SIDE WHCU PRECAUTIONARY PER MM 30-41-11. AFTER WIRING GETS REPAIRED THE RIGHT SIDE WHCU WILL NEED OPS CHECK.

Part: SEAT — DAMAGED (ZONE 200) · airframe 54,233 hrs · 23,698 cycles

WORK ORDER 911123, NR00010 THROUGH NR00029: 4C SEAT CUSHION OUT OF POSITION - NOTED VELCRO MISSING AND FIREBLOCKING DAMAGED. REMOVED AND REPLACED SEAT CUSHIONS IAW CMM 25-22-57. OK FOR SERVCIE.

Part: COVER — CRACKED (ZONE 200) · airframe 54,016 hrs · 23,618 cycles

DEFECT 71919: 1L DOOR FLOOR LIGHT COVER CRACKED. RESOLUTION: INSTALLED NEW COVER ON THE L1 FLOOR PROXIMITY LIGHT REF AMM 33-51-14. THIS CLEARS MEL 25-10

Part: COVER — DETACHED (ZONE 800) · airframe 53,962 hrs · 23,594 cycles

DEFECT 777247: ESCAPE SLIDE PACK BUSTLE COVER FELL. RESOLUTION: SECURED SLIDE PACK PRESSURE SIGHT WINDOW REF AMM 25-66-01.

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,832 hrs · 23,537 cycles

WORK ORDER A1P190 JOB 2 ITEM 71: UPPER FUESLAGE, EXTERNAL SKIN SECTION AT STA 481 AND 1.750 INCH BELOW STR-4R SKIN WITH LIGHTNING STRIKE. - - - WORK PERFORMED: PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE. DAMAGES AT THREE LOCATIONS BETWEENSTA 460 AND STA 500A, S-4R AND S-5R (DAMAGE LOCATIONS 2,3,4) DAMAGE 2 AT STA 481 AND 1.750 INCH BELOW STR-4R IAW COOPESA EO # C00-EO-0/72024-20839-R01 DATED09/07/2024.

Part: SKIN — DAMAGED (ZONE 200)

UPPER FUSELAGE EXTERNAL SKIN SECTION AT STA 203 AND WL243 SKIN WITH LIGHTNING STRIKE (RHS) - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR BETWEEN STA200 AND STA210, WL240 AND WL250, RBL30 AND RBL40 (DETAIL A) IAW COOPESA EO# C00-EO-2024-20832-R01 DATED 9/10/2024.

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,832 hrs · 23,537 cycles

WORK ORDER A1P190 JOB 2 ITEM 70: PERFORMED FUSELAGE SKIN REPAIR BETWEEN STA 440 AND STA480, S-4R AND S-6R DUE TO LIGHTNING STRIKE IAW COOPESA EO# C00-EO-2024-20839 R01 DATED 9/07/2024.

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,832 hrs · 23,537 cycles

WORK ORDER A1P190 JOB 2: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500+3 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE DAMAGES AT THREE LOCATIONS BETWEEN STA 460 AND 500A, S-4R AND S-5R (DAMAGE LOCATIONS 2, 3, 4) DAMAGE 3 LOCATED AT STA 500 +3 AND 1.5 INCH BELOW STR-4R IAW COOPESA EO# C00-EO-2024-20839.

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,832 hrs · 23,537 cycles

UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 233 AND WL 265 (RBL 40) SKIN WITH LIGHTNING STRIKE. - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR BETWEEN STA 230 AND STA 250, WL260 AND WL270, RBL30 AND RBL40 (DETAIL B) IAW COOPESA EO #000-EO-2024-20832-RO1 DATED 09/10/2024.

Part: SKIN — DAMAGED (ZONE 200) · airframe 53,832 hrs · 23,537 cycles

WORK ORDER A1P190 JOB 2 ITEM 73: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500 + 12 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. - - WORK PERFORMED: PERFORMED FUSELAGE SKIN BLEND REPAIRS DUE TO LIGHTNING STRIKE DAMAGES AT THREE LOCATIONS BETWEEN STA 460 AND STA 500A, S-4R AND S-5R (DAMAGE LOCATIONS 2,3,4) DAMAGE 4 LOCATED AT STA 500A + 12 AND 1.5 INCH BELOW STR-4R. IAW COOPESA EO #C00-EO-2024-20839-R01 DATED 9/10/2024.

Part: SKIN — DENTED (ZONE 100) · airframe 53,812 hrs · 23,531 cycles

WORK ORDER FS240105 NR002: POSSIBLE DENT WITH 2 BLIND FASTENERS INSTALLED THRU SKIN AND STRINGER STA 440 STR 28R. - - RESOLUTION: DENT WITH CREASE ON SKIN AT STRINGER STA 440 STR 28R REPAIRED IAW EA 24009 REV IR.

Part: RIB — CRACKED (ZONE 500) · airframe 53,812 hrs · 23,531 cycles

WORK ORDER FS240105 NR001: LH WING OUTER RIB P/N 737-5274-1 #18 HOLE AS A CRACK INDICATION. - - RESOLUTION: LH WING OUT RIB P/N 737-5274-1 #18 CRAKCED HOLE WAS REPAIRED IAW EA 24007 REV IR

Part: BRACKET — LOOSE (R1 GIRT BAR) · airframe 52,597 hrs · 22,978 cycles

1R GIRT BAR DOOR BRACKET TOO LOOSE GIRT BAR FALLS OFF. ADJUSTED GRIT BAR HANGER REF AMM 25-66-01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,675 hrs · 22,630 cycles

DEFECT 770498: AFT LEFT OVEN 410 DEGREES SMOKING WHEN USED. - - - RESOLUTION: REMOVED AND REPLACED AFT L/H OVEN REF AMM 25-31-01, OPS CHECK GOOD.

Part: NONE — NONE · airframe 50,556 hrs · 22,199 cycles

DEFECT W/O 77392: CABIN EMERGENCY LIGHTS AT RH EXIT ROW 14 UPPER AND AFT LOWER RIGHT AND LEFT LOWER ROW 14 NOT ILLUMINATING. RESOLUTION: REPLACED ALL LAMPS FIXTURES REMAIN INOP.

Part: FLAP — ASYMETRIC · airframe 49,926 hrs · 21,993 cycles

DEFECT 713770: FLAP ASYMMETRY AFTER T/O ON CLEAN UP. RESOLUTION: (IN PROGRESS)

Part: SENSOR — FAULTED (NR 2 SKEW) · airframe 49,926 hrs · 21,993 cycles

FLAP ASYMMETRY AFTER T/O ON CLEAN UP. BITE CK. OF FSEU REPORTED FAULT 27-53251 FLAP 2 SKEW. FOUND SKEW SENSOR 2 OUT OF RANGE . REMOVED AND REPLACED #2 FLAP SKEW SENSOR PER AMM 27-59-01. . FUNCTIONAL CHECK OF FLSAP SKEW SYSTEM IS GOOD AND OPS CK. OF T/E FLAPS IS GOOD . MEGGERED #2 FLAP SKEW SENSOR WIRES . NO SHORTS NOTED . REMOVED AND REPLACED #2 SKEW SENSOR CONNECTOR D11816 AS A PRECAUTION.

Part: SCREW — MISSING · airframe 49,339 hrs · 21,765 cycles

DEFECT 705390: 2L AFT DOOR MISSING SCREW ON GIRT PLATE.

Part: FASTENER — MISSING · airframe 49,339 hrs · 21,765 cycles

SUPPLEMENTAL. DEFECT 705390: 2L AFT DOOR MISSING SCREW ON GIRT PLATE. RESOLUTION: REF MDDR# 113587 LOG # 705202 ITEM#1 2L THRESHOLD FASTENERS THIS CLEARS GMM/MTI MDDR# 113586. REF 2LP 705390 ITEM2 REMOVED AND REPLACED 2L THRESHOLD FASTENERS REF AMM 25-27-00. THIS CLEARS GMM/MTII# 113587

Part: ROPE — LOOSE · airframe 48,812 hrs · 21,575 cycles

DEFECT: F.O. EMERGENCY ESCAPE ROPE NOT SECURED TO A/C. MXC NOTIFIED RESOLUTION: SECURED F/O EMERGENCY ESCAPR ROPE TO AIRCRAFT REF AMM 25-61-10.

Part: FLOOR SUPPORT — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 807, STR. 24L TO 22L. RESOULTION: REPAIRED FRAME @ STA 807 STR 24L - 22L IN ACCORDANCE WITH SCA ENG-53SCA-10965 REV00 AND ATS ER 22-01698 REV IR.

Part: STRINGER — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: DAMAGE FOUND ON STRINGER 23L AT STA 727A. RESOLUTION: REPAIRED STRINGER @ STA 727A 23L IAW B737 SRM 53-00-03-2R-1 REV 75 THIS IS A CATEGORTY "A". NO FURHTER INSPECTIONS.

Part: FLOOR SUPPORT — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 727F, STR. 24L. RESOLUTION: AFT CARGO FRAME @ STA 727F, STR 24L REPAIRED PER SRM 53-60-07-2R-3 REV 75. REPAIR IS CAT B. INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION, WHICHEVER COMES FIRST PER SRM 53-60-07-2R-3 REV 75 TABLE 209.

Part: FLOOR SKIN — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727E, STR 24L TO 25L. RESOLUTION: REPAIRED FRAME @STA 727E STR 24L - 25L IAW SCA ENG-53SCA-10964 REV 00 AND ATS ER 22-01693 REV IR.

Part: FLOORBEAM — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMGE TO FRAME, AFT CARGO @STA. 727B, STR. 3R RESOLUTION: REPAIRED FRAME AFT CARGO @STA 727B, STR 23R PER SRM 53-60-07-2R-3 REV 75 REPAIR IS CAT B. INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES AFTER INSTALLATION, WHICHEVER COMES FIRST PER SRM 53-60-07-2R-3 REV 75 TABLE 206.

Part: STABILATOR — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727C, STR. 23L RESOLUTION: REPAIRED FRAME AFT CARGO @ STA 727C, STR 23L PER SRM 53-60-07-2R-3 REV 75 REPAIR IS CAT B. INSP THRESHHOLD 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION, WHICHEVER COMES FIRST PER SRM 53-60-07-2R-3 REV 75 TABLE 209.

Part: FRAME ANGLE — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727C, STR 23L

Part: FRAME ANGLE — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727B, STR 24L. RESOLUTION: REPAIRED DAMAGED FRAME @STA 727B STR 24L IN ACCORDANCE WITH B737 SRM 53-60-70-2R-3 REV 75. THIS IS A CATEGORY "B" REPAIR. INSPECTION THRESHOLD IS 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION WHICHEVER COMES FIRST IAW TABLE 206.

Part: STRINGER — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: FOUND DAMAGE TO STA 727A, STR 24L FRAMES, AFT CARGO IN AREA OF FWD FLOOR PANEL. RESOLUTION: REPAIRED FRAME @ STA 727A STR 24L IAW SCA ENG-53SCA-10962 REV00 AND ATS ER22-01560 REV IR.

Part: FLOOR SUPPORT — CRACKED · airframe 48,737 hrs · 21,546 cycles

DEFECT: DAMAGED BEAM FOUND ON FORWARD CARGO DOOR, BEAM "B" (2ND INTERNAL BEAM FROM TOP). RESOLUTION: REPAIRED DAMAGED BEAM ON FWD CARGO DOOR PER ATS ER 2201541 REV IR SCA ENG-52SCA-10961 REV 00.

Part: BULKHEAD WEB — DAMAGED (BS 1016) · airframe 44,760 hrs · 20,196 cycles

TOOL MARK FOUND C/T AFT PRESSURE WEB AT W/L 207 RT WEB JUST BELOW THE PRESSURE WEB. REMOVED .006" MATERIAL FROM .040" NOMINAL .034" REMAINING, IAW B737 SRM 53-80-08 ALLOWABLE DAMAGE. FOUND TO BE OUT OF LIMITS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,287 hrs · 19,292 cycles

MULTIPLE EMERGENCY LIGHTS OUT ON RH SIDE. REMOVED AND REPLACED 4 EA EMERLIGHT BATTERY PACKS. OPS CHECKS GOOD.

Part: SMOKE GOGGLES — BROKEN (COCKPIT) · airframe 35,790 hrs · 16,896 cycles

DURING A PREFLIGHT, FOUND BROKEN SMOKE GOGGLES ON CAPTAIN`S AND JUMPSEAT POSITIONS. REPLACED PIN ON CAPTAIN`S SMOKE GOGGLES AND FOUND TO BE SERVICABLE. REPLACED OBSERVERS SEAT SMOKE GOGGLES.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 31,591 hrs · 15,399 cycles

T/E FLAP ASYMETRY LT 2', RT 4'. FOUND FSEU FAULT CODE 27-52259-T/E FLAP SENSOR LT. REPLACED LT FLAP POSITION TRANSMITTER. OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,902 hrs · 15,181 cycles

FOUND LT OVERWING EMERGENCY LIGHTS INOPERATIVE, INTERIOR. REPLACED M1695 BATTERY PACK & CHARGER ASSY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,900 hrs · 15,180 cycles

GROUND POWER DOOR DAMAGED. REPAIRED GROUND POWER DOOR CUTOUT.

Part: BULB — ABNORMAL (EMERGENCY LIGHT) · airframe 28,593 hrs · 14,287 cycles

LEFT FWD EMERGENCY LIGHT IS INOPERATIVE. R & R BULB.