N829SY

Part: WIRE HARNESS — BURNED (ZONE 400) · airframe 57,659 hrs · 29,657 cycles

FOUND WIRE HARNESS TO NR 2 ENG STARTER BURNED. REMOVED AND REPLACED WIRING HARNESS MW0312. REF AMM 71-51-03. WIRING HARNESS NEEDS OPS CHECKED PER SUBTASK 71-51-03-710-004-F00

Part: LIGHT — UNSECURE (ZONE 200) · airframe 57,540 hrs · 29,615 cycles

ROW 1A AND 13 ABC EMERGENCY EXIT PATH STRIP COMMING UP. SECURED THE LIGHT STRIP ON EXIT PATH LIGHT IAW AMM 33-14-00.

Part: LENS — DETACHED (ZONE 200) · airframe 57,115 hrs · 29,397 cycles

EXIT ROW EMER EXIT LIGHT MISSING FWD EXIT SIGN. FOUND LENS FOR EXIT LOCATOR SIGN IN COMPARTMENT, RESECURED AT OVERWING POSITION IN REF AMM 33-51-00. OKAY FOR SERVICE.

Part: BATTERY — NO TEST (ZONE 200) · airframe 56,804 hrs · 29,240 cycles

L1 INBD FLASHLIGHT DOES NOT FLASH ( EMERGENCY FLASHLIGHT HOLDERS/ FLASHLIGHTS; CABIN/ REMOVED AND REPLACED L1 INBD FA SEAT FLASH LIGHT BATTERY. OPS CHECK GOOD. OK FOR SERVICE REF AMM 25-64-00. THIS CLEARS MEL 25-12-1.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,646 hrs · 29,174 cycles

EMER BATTERY PACK FOR AFT SERVICE DOOR FAILED TEST - RESOLUTION: R&R EMER BATTERY PACK FOR AFT SERVICE DOOR REF AMM 33-51-06 OPS CHECK GOOD

Part: WINDOW — ARCED (ZONE 200) · airframe 55,780 hrs · 28,814 cycles

DEFECT 797038: DURING DECENT BRIGHT FLASH OF LIGHT FROM MIDDLE OF R1 WINDOW POSSIBLE ARC WITH OVERHEAT ANNUNCIATION ON OVERHEAD PANEL. REMOVED WINDOW REF AMM 56-11-11 R1 WINDSHIELD INSTALLED REF AMM 56-11-11. UP TO STEP H.(8). INSTALLED MESH , NALON CORN AND SEALED WINDOW W/ 1828B1/2 REF AMM 56-11-11. REPLACED THE R1 WINDOW ON NR# 00004, WO # 92799 PER AMM 56-11-11-400-801.

Part: FLT CONTROLS — STIFF · airframe 55,633 hrs · 28,758 cycles

DEFECT 796540: FLIGHT CONTROLS ARE ABNORMALLY STIFF. RESOLUTION: LUBED AILERON MIXER REF AMM 27-11-81 OPS TEST GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 54,209 hrs · 28,156 cycles

DEFECT 772719: ¨ON CLIMB AT FL200 HYD QUANTITY DROPPED TO 25% AFTER 2 MIN QUANTITY DROPPED TO 20%, OF SYS HYD A VERIFY HYD LEAKS AND CORRECTED FAIL.(DECLARED EMERGENCY) - - RESOLUTION: REF TO TECHOPSMX N/R 00001 FOUND LOOSE HYDRAULIC (A) SYSTEM SUPPLY LINE ON LH PYLON FAIRINGS, RECONNECT HYDRAULIC SUPPLY LINE PER B737-800 AMM 20-10-51-910-802 AND PERFORM DRY RUN PER B737-800 AMM 71-00-00-700-821-F00 AND STARTING THE ENGINES PER B737-800 AMM 71-00-00-800-808-F00 TO VERIFY LEAKS NO LEAK NOTED AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,721 hrs · 27,157 cycles

DEFECT 745003: NOTICED WINDOW HEAT ARCING ON APPROACH. TURNED OFF ACCOCIATED WINDOW HEAT(LEFT SIDE). ARCING SUBSIDED. TWO CRACKS FORMED, APPROX 20 INCHES & 15 INCHES EACH. - - - RESOLUTION: REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-11. OPS CHECK GOOD. REPLACED #2 WHCU PER AMM 30-41-11 OPS CHECK GOOD.

Part: NONE — NONE · airframe 50,626 hrs · 26,690 cycles

DEFECT W/O 74740 N/R-00001: L-1 DOOR REPORTED FEELING ABNORMAL WHEN OPENED BY FLT ATTN. RESOLUTION: L1 DOOR HAD SHEERED SCREW ON THE PIN SECRUING THE UPPER AND LOWER RADIUS LINKS TO THE GUIDE ARM. IMPROPER WASHER STACK UP WHERE THE UPPER AND LOWER RADIUS LINKS ATTACH TO THE UPPER SUPORT ARM. EXCESSIVE PLAY IN UPPER AND LOWER RADIUS LINKS MIGHT BE THE CAUSE OF REPEAT DAMAGE TO SCREWS. MISSING HARDWARE SECURING THE UPPER GUIDE ARM TO THE UPPER HINGE ARM. SUGGEST REPLACING GUIDE ARM, UPPER RADIUS LINK, AND LOWER RADIUS LINK FOR PROPER FITMENT.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 50,620 hrs · 26,688 cycles

MAIN CABIN DOOR WAS DIFFICULT TO OPEN FROM INSIDE. LUBRICATED MAIN CABIN DOOR REF AMM 52-11-00, OPS CHECK GOOD

Part: SIGN — DETACHED (CABIN) · airframe 50,594 hrs · 26,674 cycles

ROW 16 EMERGENCY EXIT SIGN FELL DURING FLIGHT. RE-ATTACHED EMER EXIT SIGN COVER. CHECKS SERVICEABLE IAW AMM 33-51-01

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 50,474 hrs · 26,596 cycles

AT THE GATE THE FLIGHT ATTENDANT COULD NOT GET THE MAIN CABIN DOOR L1 TO GO FULLY OPEN INSPECTED DOOR, LUBRICATED ROLLERS, DOOR OPERATION OK REF AMM 52-11-00.

Part: NONE — NONE · airframe 50,384 hrs · 26,554 cycles

DEFECT WORK ORDER 73571: SEVERAL EMERGENCY LIGHTS DO NOT COME ON IN THE CABIN AT THE OVERWING EXITS WHEN TESTING. RESOLUTION: REPLACED 2 LIGHT BULBS ON RH OVERWING EMERGENCY EXIT REF. AMM 33-51-04. OPS CHECK GOOD.

Part: FLOOR SPLICE — CRACKED · airframe 50,121 hrs · 26,441 cycles

DEFECT: TRANSFERRED FROM LOG PAGE 682938 ITEM 1: FOUND EVIDENCE OF CRACK DAMAGE ON FWD BULKHEAD OF WHEEL WELL PRESSURE DECK STA. 663. RBL 31.83-45.64. REF SRM 57-10-10-2R-4 FOR TYPICAL CRACK LOCATION AND REPAIR INSTRUCTION. RESOLUTION: REPAIRED BS 663 VERTICAL PRESSURE WEB RBL25-RBL45 PER B737 SRM 57-10-10-2R-3 ALTERNATIVE 2. CAT B REPAIR. REPAIR INSPECTION REQUIREMENTS PER B737 SRM 57-10-10-2R-3 TABLE 205; INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION HFEC INSPECTION, INTERVAL 36,000 FLIGHT CYCLES INITIAL WEB AND PART 1 REPAIR WEB FROM AFTSIDE , PART 3 FILLER NOT COMMON TO THE PART 2 DOUBLER FROM THE FWD SIDE PART 2 DOUBLER FROM THE FWD SIDE HORIZONTAL FLANGE OF THE LOWER ATTACH ANGLE FROM THE FWD SIDE UPPER COMPRESSION CHIRD FROM THE AFT OR FWD SIDE LFEC INTERVAL 36,000 FLIGHT CYCLES PART 3 FILLER COMMON TO THE PART 2 DOUBLER FROM THE FWD SIDE. PLACED ON GMM/MTI LOGPAGE 682294 ITE 1.

Part: BULKHEAD — CRACKED · airframe 50,121 hrs · 26,441 cycles

DEFECT: TRANSFERRED FRM LOGPAGE 682938 ITEM 1: FOUN EVIDENCE OF CRACK DAMAGE ON FWD BULKHEAD OF WHEEL WELL PRESSURE DECK STA 663 LBL 31.83-45.64. REF SRM 57-10-10-2R-4 FOR TYPICAL CRACK LOCATION AND REPAIR INSTRUCTION. RESOLUTION: REPAIRED DAMGE ON FWD BULKHEAD OF WHEEL WELL PRESSURE DECK STA. 663 LBL 31.83-45.64 PRE SRM 57-10-10-2R-3 REV 76 ALTERNATIVE 2. CAT B REPAIR. REPAIR INSPECTION REQUIREMENTS PER B737 57-10-10-2R-3 TABLE 205; INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION HFEC INSPECTION INTERVAL 36,000 FLIGHT CYCLES: INTIAL WEB AND PART 1 REPAIR WEB FROM THE AFT SIDE (ARROW 1). PART 3 FILLER NOT COMMON TO THE PART 2 DOUBLER FROM THE FORWARD SIDE (ARROW 2). PART 2 DOUBLER FROM THE FORWARD SIDE (ARROW 6). UPPER COMPRESSION CHORD FROM THE AFT OR FWD SIDE (ARROW 5) LFEC INTERVAL 36,000 FLIGHT CYCLES, PART 3 FILLER COMMON TO THE PART 2 DOUBLER FROM THE FWD SIDE (ARROW 3). PLACED GMM/MTI MDDR # 113179 LOGPAGE 682940 ITEM 2.

Part: NONE — NONE · airframe 48,882 hrs · 25,930 cycles

GIRT BAR BRACKET ON DOOR 1L BROKEN. RESOLUTION: REMOVED BOLTS AND INSTALLED RIVETS ON GIRT BAR BRACKET REF SRM 51-40-02 INSPECTION COMPLETED THIS CLEARS GMM/MTI MDDR# 110363 RII ACCOMPLISHED BY 9905 R+R SLIDE REF AMM 25-66-01

Part: NONE — NONE · airframe 48,134 hrs · 25,641 cycles

CORROSION FLOOR BEAM AT STA 986 APPROX RBL 35. EVALUATED DAMAGE ON BS 986 FLOOR BEAM RBL 35 AND REMOVED DAMAGE IN AREA OF .9"L X .5"W X .042"D. FOUND OUT OF LIMITS PER 737SRM 53-70-51-1A-1. REMOVED UPPER T CAP OF FLOOR BEAM FROM RBL 60 - LBL 60 AND REPAIRED PER SRM 53-70-51-2R-4 REPAIR 4.

Part: NONE — NONE · airframe 48,134 hrs · 25,641 cycles

CORROSION LAV FITTING ONFLOOR BEAM AT STA 947 APPROX LBL 40. REMOVED CORROSION ON BS 947.5 FLOOR BEAM LBL 40 IN AREA OF .6" X .5" X .037"D. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED FLOOR BEAM TCAP FORM LBL 9.25 TO LBL 60 AND REPAIRED PER SRM 53-70-51-2R-5.

Part: NONE — NONE · airframe 48,134 hrs · 25,641 cycles

CORROSION LAV FITTING ONFLOOR BEAM AT STA 947 APPROX LBL 40. REMOVED CORROSION ON BS 947.5 FLOOR BEAM LBL 40 IN AREA OF .6" X .5" X .037"D. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED FLOOR BEAM TCAP FORM LBL 9.25 TO LBL 60 AND REPAIRED PER SRM53-70-51-2R-5.

Part: NONE — NONE · airframe 48,134 hrs · 25,641 cycles

CORROSION FLOOR BEAM AT STA 986 APPROX LBL 35. REMOVED CORROSION ON BS 986.5 FLOOR BEAM LBL 35 IN AREA OF .7" X .7" X .059"D. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVAL OF UPPER T CUP AND REPAIR ACCOMPLISHED ON CUSTOMER CARD 00072.

Part: CABLE — UNSECURE (SPOILER) · airframe 45,880 hrs · 24,664 cycles

AFTER TAKE OFF, GEAR LEVER WOULD MOVE TO OFF POSITION, BUT NOT UP. PSEU BITE FOUND GSBV CL FAULT# 31-51001 INTERMITTANT. FOUND LOWER SLIDER SLEEVE FOR GROUND SPOILER INTERLOCK CABLE AT RT MLG HARDWARE WITH BROKEN SAFETY WIRE AND UNSECURE. SECURED IAW AMM 27-62-57, PERFORMED GSIV SENSOR CHECK, FUNCTIONAL TEST IAW AMM 27-62-61, ALL CHECKS GOOD, PERFORMED PSEU BITE IAW FIM 32-19 TASK 801, TEST PASSED, NO FAULTS. AIRCRAFT OK FOR SERVICE.

Part: SLIDE — NO TEST · airframe 44,779 hrs · 24,217 cycles

DURING SLIDE DEPLOYMENT FOR FA TRAINING, SLIDE DEFLATED QUICKLY. FOUND TEAR IN SLIDE. REMOVED AND REPLACED SLIDE IAW AMM 25-66-1. OK FOR SERVICE.