N39415

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 53,324 hrs · 18,985 cycles

DOOR 1R GIRT BAR BRACKET LOOSE AND WILL NOT RETAIN GIRT BAR CLEANED DEBRIS FROM RETAINERS AT DOOR 1R, ARMED AND DISARMED SLIDE PER AMM 25-66-01. NO FAULTS NOTED, OK TO CONT.

Part: SKIN — DAMAGED (R/H HORZ STAB) · airframe 49,474 hrs · 17,443 cycles

REPAIR R/H HORZ STAB LWR SKIN CUTOUT TO ACCESS RIB DAMAGE AT STAB STA 120.3 REPAIR AND EXT.LFEC INSP.WITH REPEAT INSP EVERY 9,000 FLT CYCLES REPAIRED SKIN IAW SRM 55-10-01-2R-11. REQUIRES DIP IAW TABLE 204. INSP THRESHOLD 56,000 TOTAL FLT CYCLES DETAILED VISUAL ADD EMP:U241494,U347296,U245894 VERIFIED

Part: SKIN — DAMAGED (L/H HORZ STAB) · airframe 49,474 hrs · 17,443 cycles

REPAIR L/H HORZ STAB LWR SKIN CUTOUT TO ACCESS RIB DAMAGE AT STAB STA 138.70 AND EXT.LFEC INSP.WITH REPEAT INSP EVERY 9,000 FLT CYCLES REPAIRED SKIN IAW SRM 55-10-01-2R-11. REQUIRES DIP IAW TABLE 204. INSP THRESHOLD 56,000 TOTAL FLT CYCLES DETAILED VISUAL INSP ADD EMP:U397695,U245894,U236064 VERIFIED

Part: LIGHT — INOPERATIVE (SEAT ROWS 15,20,) · airframe 48,956 hrs · 17,244 cycles

AISLE EMERGENCY EXIT SEAT MOUNTED LIGHTS DO NOT ILLUMINATE AT CONSECUTIVE SEAT ROWS 15,20, & 21 AND CONSECUTIVE SEAT ROWS 27,28,29,30, AND 31. ADDED PART BATTERY CHARGER P/N D717-02-030 FOUND FUSE BAD AT BATTERY CHARGER M1694 AND REPLACED, SEAT ROWS 15,20, &21 WORK CORRECTLY, AWAITING BATTERY TO PLACE IN POSITION M1673 AFT GALLEY AREA OVERHEAD. PARTS USED: 99-3351-3-0009,QTY :1 REPLACED BATTERY PACK PER AMM TASK 33-51-06-960-805. EMERGENCY LIGHTS CHECK GOOD. PARTS USED: 99-3351-3-0015,QTY :1

Part: ADIRU — UNKNOWN (LEFT SIDE) · airframe 48,777 hrs · 17,167 cycles

IRS 1 FAILED IN FLIGHT REMOVED AND REPLACED ADIRU 1 REF AMM 34-21-01/401. OPS TEST OK. REQUIRES CAT III TEST. PARTS USED: 29-3421-9-0010,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1925837 SN OFF 3729 UNIT, ADIRU, AI OFF 29-3421-9-0010 3729 ON 29-3421-9-0010 2018

Part: SENSOR — FAILED (TE FLAPS) · airframe 42,982 hrs · 15,037 cycles

TRAILING EDGE FLAP ASSYMETRY. FLAPS STUCK AT 5 WITHIN 1 NEEDLE WIDTH OF EACH OTHER. ELECTRICALLY DROVE THE FLAPS TO 15 VIA ALTERNATE METHOD. IPC REFERENCE # IPC 27-59-01-05 27-53258. REPLACED TE FLAP NO. 1 SKEW SENSOR. REF FIM 27-51-TASK801, 27-59-00-730-80 AND IPC 27-59-01-05 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1171975 SN OFF 3713 OIL SERVICE ACCOMPLISHED AT FLL FOR FLT 2386 ON 12 JUL 00:41:21 ENGINE 2: 02 ADDED BY U085211 ENGINE 3: ENGINE 4: APU: SENSOR, FLAP, S OFF 29-2759-9-0002 3713 ON 29-2759-9-0002 3198 ENGINE 1: 02 ADDED BY U085211 ADD EMP:U077202 ADDITIONAL TECH ADDED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,750 hrs · 13,501 cycles

EMERGENCY OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK EMER PWR AND OPS CHECK GOOD, REF AMM 33-51-06-960-805. ACCOMPLISHED THE INSPECTION OF OVERWING EMERGENCY EXIT LIGHTS OPERATION. REF AMM 33-51-06-960-805.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,644 hrs · 11,551 cycles

ROW 8 AISLE WHITE EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS. OPS CHECKED GOOD.

Part: COVER — MISSING (CABIN) · airframe 33,616 hrs · 11,538 cycles

SEAT 20C EMERGENCY LIGHT LENS COVER MISSING RPL EMERGENCY LIGHT.

Part: LIGHT — UNKNOWN (CABIN) · airframe 33,547 hrs · 11,510 cycles

L2 DOOR EMERGENCY LIGHT INOPERATIVE. RESET AC POWER. THE EMERGENCY LIGHT OPS CHECKED GOOD. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,547 hrs · 11,510 cycles

SEAT 12C EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS. OPS CHECK GOOD, OK FOR SERVICE.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 32,924 hrs · 11,298 cycles

EMERGENCY EXIT SIGN IN THE AFT GALLEY WAS LOOSE. SECURED THE SIGN.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 32,859 hrs · 11,272 cycles

EMERGENCY EXIT SIGN FWD OF THE AFT GALLEY DETACHED FROM THE CEILING. SECURED THE SIGN.

Part: LIGHT — BROKEN (SEAT 8C) · airframe 32,273 hrs · 11,024 cycles

EMER PROX LIGHT SEAT FLOOR SEAT 08C BROKEN CYCLED EMERG LTS ON AND OFF AND REINSTALLED HOUSING TO SEAT. OPS CKS GOOD.

Part: FUSE — FAULTY (CABIN) · airframe 32,236 hrs · 11,012 cycles

EMERGENCY LIGHTS INOP ROWS 15,20 AND 21. REPLACED FUSES PER AMM 33-51-06-960-804.

Part: UNKNOWN — ODOR (GALLEY) · airframe 32,206 hrs · 11,001 cycles

F/A REPORT ELECTRIC ODOR AFT GALLEY AREA. OPS CHECKED ALL ELECTRICAL ITEMS IN AFT GALLEY. ALL CHECKED GOOD. NO FAULTS NOTED, NO SMOKE OR ELECTRICAL ODORS. OK.

Part: LIGHT — LOOSE (SEAT 24C) · airframe 32,029 hrs · 10,931 cycles

SEAT 24C EMERGENCY EXIT LIGHT NOT ATTACHED TO SEAT. SECURED NEW EMERGENCY LIGHT SHROUD AT SEAT 24C

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 31,841 hrs · 10,857 cycles

VERIFIED CRACK USING HFEC IAW NDT MANUAL PART 6, 51-0 0-00-23 AND FOUND A 1 INCH CRACK AT RT HSS 129.5, PARALLEL TO RIB AND INBD OF DRAIN HOLE. REPAIRED IAW SRM 55-10-01 REPAIR 11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,078 hrs · 10,593 cycles

EMERGENCY EXIT LIGHTS AT RIGHT SEATS 22-27 INOP. REPLACED BATTERY PACK AT SEAT 27 RT, REFERENCE AMM TASK 33-51-06-960-805. OPERATIONAL CHECK SATISFACTORY.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 24,479 hrs · 8,278 cycles

RIGHT HORIZONTAL STAB LOWER SKIN REQUIRES CUT OUT FOR ACCESS TO RIB 1 & 2 REPAIRS STATION 92.70. REPAIRED LOWER SKIN IAW ECRA 5510-02528.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,479 hrs · 8,278 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 138.7 FWD OF REAR SPAR. 1 1/4" CRACK MARKED IN BLACK MARKER CONFIRMED WITH HFEC 737 PART 6 51-00-00-23. CUT OUT DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02526. INITIATED DIP TO PERFORM DETAIL VISUAL & LFEC INSPECTION 56000 FLIGHT CYCLES AFTER INSTALLATION & INTERVALS OF 9,000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01, REPAIR 11 TABLE 204.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,479 hrs · 8,278 cycles

SEAT TRACK FASTENER HOLE CRACKED AT STATION 727B LBL 45.5 IAW NDT PAR 6 51-00-00-16. REPAIRED SEAT TRACK STATION 727B AT LBL 45.5 IAW ECRA 5320-02481 & EA 5320-02076 REV G OP 3.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,479 hrs · 8,278 cycles

SEAT TRACK FASTENER HOLE CRACKED AT STATION 727B, RBL 45.5 IAW NDT PART 6 51-00-00-16. REPAIRED SEAT TRACK STATION 727B AT RBL 45.5 IAW ECRA 5320-02482 & EA 5320-02076 REV G OP 4.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,479 hrs · 8,278 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 147.9 & 17" FWD OF REAR SPAR. 1" CRACK MARKED IN BLACK MARKER CONFIRMED WITH HFEC IAW NDT 737 PART 6,51-00-00-23. CUT OUT DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02524. INITIATED DIP TO PERFORM A DETAIL VISUAL & LFEC INSPECTION 56,000 FLIGHT CYCLES AFTER INSTALLATION & AT INTERVALS OF 9,000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01 REPAIR 11 TABLE 204. QC IAW ECRA 5510-02524 LT HORIZONTAL LOWER SKIN REPAIR SRM 55-10-01 REPAIR 11 TABLE 203.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,479 hrs · 8,278 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 101.9 & 11" FWD OF REAR SPAR. 3/4" CRACK MARKED IN BLACK MARKER CONFIRMED WITH HFEC NDT 373 PART 6, 51-00-00-23. CUT OUT DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02525. INITIATED DIP TO PERFORM DETAIL VISUAL & LFEC INSPECTION AT 56,000 FLIGHT CYCLES AFTER INSTALLATION & INTERVALS OF 9,000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01 REPAIR 1 1 TABLE 204.

Part: LATCH — UNSECURE (L1 DOOR) · airframe 17,735 hrs · 6,017 cycles

DOORS LIGHT ILLUMINATED ON TAKEOFF ROLL. REJECTED APPROX 140KIAS, DUE TO F/A SCREAMING. L1 DOOR REPORTED NOT LATCHED COMPLETELY - CD LATCH ENGAGEMENT REF AMM 52-11-00-820-802, ALL LATCH ENGAGE IN LIM, DOOR OPS CHECKED GOOD. PERFORMED HIGH ENERGY STOP INSPECTION, AMM 05-51-07, CHECKED GOOD.

Part: APU — FAULTED · airframe 16,040 hrs · 5,392 cycles

WHILE SWITCHING FROM ENGINE BLEED TO APU BLEED IN PREPARATION FOR A BLEED OFF TAKEOFF, A THICK DARK SMOKE CAME OUT OF VENT SYS, PERFORMED APPROVED SMOKE IN COCKPIT/CABIN CHECK LIST. PERFORMED INSPECTION IAW AMM 05-51-26,FAULT WITH APU 49-94299, FAIL ATTEMPED START. RAN BOTH ENGS.AND PACKS, ISOLATION CLOSED NO BLEED OR PACK DISCREPANIES, REF L.P. 7280560/61 FOR APU PLACARD AND DIP TO REPLACE FILTERS. FAULT DATA FAULT CODE 1: 49-94299 FAULT COMMENTS : STARTER GENERATOR OIL FILTER SHOWS CLOGGED.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 14,843 hrs · 4,945 cycles

SUPPORT TASK LT HORIZ STABILIZER LOWER INNER SPAR SKIN BY STA 157.50 FOUND .500 CRACK LOCATED 23.5 " AFT OF FWD SPAR SKIN REPAIRED IAW SRM 55-10-01, REPAIR 11. PERFORM INITIAL INSP 56000 FLT CYC AFTER REPAIR, THEN REINSPECT EVERY 9000 FLT CYC IAW SRM 55-10-01 REPAIR 11 STEP 5 TABLE 204 OF PAGE 216.