N47414

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 55,253 hrs · 19,808 cycles

DOOR 1R ESCAPE SLIDE HAS EXTRA SLIDE MATERIAL HANGING DOWN FROM THE GIRT BAR TO THE PACK. ADJUSTED DOOR 1R GIRT REF AMM 25-66-01-400-804. ADJUSTED WHILE ON DOOR.

Part: GIRT BAR — UNPACKED (ZONE 800) · airframe 54,917 hrs · 19,677 cycles

MATERIAL ON 1R DOOR SLIDE IS DRAGGING. REPACKED DOOR SLIDE GIRT BAR MATERIAL IAW AMM 25-66-01-000-804.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,624 hrs · 19,546 cycles

ON TAKEOFF AND DESCENT BAD ODOR SUSPECTED FROM PACKS PERFORMED IDLE CHECK BOTH PACKS RUNNING AUTO AND HIGH FIVE MINUTES NO SMELLS. RAN BOTH ENGINES FIRST RUN AND ONE AT 75% AND TWO AT 90% FOR FIVE MINUTES., POWER UP TO N1 84% AND N2 93% FIVE MINUTES NO SMELLS NOTED IDLE COOL DOWN FIVE MINUTES WALK. CABIN AGAIN NO SMELLS. PACKS CYCLED FULL COLD, AND FULL WARM DURING TEST.AMM 71-05-TASK 807.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 53,735 hrs · 19,173 cycles

REF LOG PAGE 4418928 ODOR IN FLT DECK. AIRCRAFT IS RESTRICTED TO CLASS 1 & CLASS 2 STATIONS. CREATING PLA REF LOG PAGE 4418928 ODOR IN FLT DECK. AIRCRAFT IS RESTRICTED TO CLASS 1 & CLASS 2 STATIONS. DISPATCH DESK: OM8.TOMC APPROVED. PLA 1203 AIRCRAFT IS RESTRICTED TO DOMESTIC CLASS 1-2 STATIONS ONLY. CLE-DEN-EWR-IAD-IAH-LAX-MCO-ORD-SFO-TPA-DSM-D CLT-JFK-LGA-PHL-RDU-DCA-ATL-FLL-RSW-MIA-MSY-ABQ-AUS-DFW-LAS-PHX- PDX-SMF-SAT-SAN-SNA-SEA. RESTRICTED TO CLASS 1 & CLASS 2 STATIONS. ORIGINAL CYCLES.LIMIT OF: 005 EXTENDED BY 004 NEW TIME REMAINING 005 ADJUSTED CYCLES TO REFLECT 5 CYCLES PER PLA NO FURTHER WRITEUPS OK TO CLOSE LP

Part: UNKNOWN — ODOR (CABIN) · airframe 53,725 hrs · 19,169 cycles

ODOR IN FLT DECK ON TAKEOFF FOR ABOUT 1 MINUTE THEN CLEARED OUT . FA IN CABIN DID NOT SMEL DEBRIEFED CREW AND THEY STATED A ACRID, POSSIBLE HYD FLUID SMELL ON PULLING TAKEOFF POWER AND SMELL DISSIPATED ON CLIMB AND THEN WAS GONE AND NEVER CAME BACK. FA€™S HAD NO SMELL IN CABIN AND RULES OUT LAV OR GALLEY ISSUE. CREW BELIEVED SMELL WAS FROM #1 ENGINE. NEED TO FOLLOW TASK 05-51-26-800-801-C1 IN AMM. BELOW IS SMOKE/ODOR IN PLANE QUESTIONARE. PER PAUL CASAL TOMC, HIGH POWER RUN WILL BE NEEDED AFTER INSPECTION HAS BEEN ACCOMPLISHED FOR ODOR IN FLT DECK. INSPECTED FLIGHT DECK CB'S AND FOUND NO TRIPPED OR ABNORMAL CB'S. INSPECTED NOSE COMPARTMENT E&E FOR ANY BURNT COMPONENTS OR DAMAGED WIRES OR TRIPPED CB'S AND NO ABORMALITIES FOUND. INSPECTED E&E COMPARTMENT FOR ANY TRIPPED CB'S OR DAMAGED OR BURNT WIRES OR COMPONENTS AND FOUND NO ABNORMALITES. REF AMM TASK 05-51-26-800-801-C1. PER TOMC, HIGH POWER RUNS WILL NOT BE REQUIRED. REF LP 4422888 AND 4422938 FOR ACTION TAKEN. REPLACED #1 PACK RECIRC FILTER PER MM 21-25-01. ACP PACK BURN OUT PER MM21-00-01 WITH ENGINES RUNNING FOR 10 MINUTES, NEVER HAD ANY FOUL SMELLS IN COCKPIT OR CABIN.

Part: LIGHT — FAULTY (SEAT 21C) · airframe 52,724 hrs · 18,778 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - RED & WHITE FLOOR PROX LIGHTS AT SEATS 15C, 20C & 21C DO NOT ILLUMINATE. REMOVED & REPLACED RED EXIT ROW FLOOR PROX LIGHT AT SEAT 21C, OPS NML, REF AMM 33-51-11-960-802.

Part: IDG — FAILED (NR 1 GENERATOR) · airframe 50,686 hrs · 17,926 cycles

GEN SOURCE LT CAME ON IN CRUISE. UNABLE TO RECONNECT GEN 1 APU GEN CONNECTED REF FIM 24-21 TASK 802, FOUND THAT THERE WAS AN INDICATION ON GCU1 BOX IN THE E&E OF IDG FAIL. BITE TESTED THE BOX AND CLEARED THE FAULT. THE IDG FAULT FIM REF IS 24-21 TASK 805 TO CONTINUE TROUBLESHOOTING. MANUALLY RECONNECTED #1 ENG IDG REF AMM 24-11-11, UNABLE TO PERFORM ENG RUN AND OPS CHECK DUE TO AIRPORT OPERATIONS. VERIFED INSTALL AND TORQUE OF NO. 1 ENGINE IDG FEEDER CABLES PER GMM 0910-05 AND AND AMM 24-11-11. NO DEFECTS PERFORMED ENGINE RUNS OPS CHECK FAIL TS IRW FIM 24-21 TASK 805 IDK FAIL LATCHED AFTER ENGINE RUN, SWAPPED GCU OPS CHECK FAIL, INSPECTED WIRING IRW FIM 24-21 TASK 805 WITH NO DEFECTS NOTED, IDG MOMENTARILY COMES ONLINE THEN FAILS, IDG REQ REPLACEMENT. REMOVED #1 ENG IDG REF AMM 24-11-11-000-801. OLD IDG LOCATED IN CENTER OF HANGER SECURED TO JACK. #1 ENGINE IDG INSTALLED REF AMM 24-11-11, FOLLOW ON MX NOT ACCOMPLISHED AT THIS TIME, IDG INITIAL SERVICING C/W PARTS USED: 29-2411-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1523056 SN OFF 0818 ENGINE RUN AND OPERATIONAL TEST OF NUMBER ONE IDG REQUIRED GENERATOR, INTE OFF 29-2411-9-0001 0818 ON 0000 GENERATOR, INTE OFF 29-2411-9-0001 0818 ON 29-2411-9-0001 2213 PARTS NOT IN STOCK. LEAK AND OPS CHECK C/W, NO DISCREPANCY NOTED ENGINE RUN GOOD

Part: THERMOCOUPLE — OUT OF RANGE (T49S3 AND T49S4) · airframe 49,085 hrs · 17,271 cycles

R ENG HAD RAPID EGT INCREASE TO CAUTION REDUCED THRUST TO 74 N1 AND STABILIZED 77-20862 AND 77-20872. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN REFERENCED FIM 71-06 TASK 804. PERFORMED A GENERAL VISUAL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. DO THE EEC BITE PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM THE EEC PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM THE EEC PERFORM A GENERAL VISUAL INSPECTION OF THE ENGINE INLET AND INSPECTION OF THE ENGINE INLET AND EXHAUST, NO DEFECTS FOUND. PERFORM A GENERAL VISUAL INSPECTION OF THE ENGINE INLET AND PROCEDURE PER FIM 73-00 TASK 801 AND CHECK FOR ANY RELATED BITE PROCEDURE PER FIM 73-00 TASK 801. BITE PROCEDURE PER FIM 73-00 TASK 801. EXHAUST. THE BOX AROUND THE EGT INDICATION WAS WHITE. EEC BITE TEST EXHAUST. MESSAGES. SHOWED EGT S3 & S4 PROBE OUT OF RANGE MAINTENANCE MESSAGES AT NBR 2 ENGINE TEMP INDICATION TEST T49.5 , FOUND NO INDICATION AT NBR 2 ENGINE TEMP INDICATION TEST T49.5 , FOUND NO INDICATION ON PROBES T49S3 & T49S4. ON PROBES T49S3 & T49S4. REMOVED AND REPLACED NUMBER 2 ENGINE EGT HARNESSES CJ10 AND J10 PER 77-21-43, REMOVED AND REPLACED EGT PROBES T49S3 AND T49S4 PER AMM 77-21-00. PENDING ENGINE RUN ASSURANCE TEST. REMOVED AND REPLACED NUMBER 2 ENGINE EGT HARNESSES CJ10 AND J10 J10 M&E P/N 29-7

Part: FILTER — LEAKING (HYD B) · airframe 49,072 hrs · 17,267 cycles

HYD B WENT FROM 93 TO 76. BELLY OF PLANE HAS HUGE DARK STREAK FROM WHEEL WELL TO APU FOUND B SYSTEM CASE DRAIN FILTER HOUSING LEAKING. R&R CASE DRAIN 00-0585-3-0455,QTY :1 00-0585-3-0440,QTY :1 40-0595-3-1976,QTY FILTER AND REPLACED ORING SEALS FOR FILTER HOUSING. PER AMM :1 29-11-41 OPS AND LEAKED CHECKED GOOD. SERVICED HYDRAULIC TO 94 PERCENT. PARTS USED: 29-2911-3-0052,QTY :1 ADD EMP:U238137

Part: SLIDE — UNKNOWN (DR 1L) · airframe 48,089 hrs · 16,910 cycles

SLIDE PACK 1L FELL OUT OF HOUSING DOOR SLIDE GIRT BAR AS ENGAGED, SLIDE DID NOT DEPLOY BUT DID COME OUT OF BUSTLE, REMOVED SLIDE FROM DOOR SLIDE IS PINNED RAR FWD LFT SLIDE REF AMM 25-66-01-400-801 PARTS USED: 29-2566-9-0007,QTY :1 ADD EMP:U49059 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1763064 SN OFF 8720 VERIFIED P/N AND INSTALLATION OF SLIDE ASSY. REF AMM 25-66-01-400-801 AND GMM 09-25-05. SLIDE, FWD/AFT OFF 29-2566-9-0007 8720 ON 29-2566-9-0007 0458

Part: NONE — NONE (NONE) · airframe 47,477 hrs · 16,682 cycles

HIGH SPEED REJECT FOR SEVERAL LARGE FLOCKS OF BIRDS CROSSING THE RUNWAY. SPEED AT REJ ECT WAS 120 OF 79MIN. CREW DEBRIEF GROSS WEIGHT 144,000LBS AND WITH THRUST REVERSE CREW ALSO NOTED MINIMUM MANUAL BRAKING USED TO STOP, MOSTLY STOP RELIED ON AUTOBRAKE FUNCTION. ACCOMPLISHED HIGH ENERGY STOP - IN CAUTION RANGE REF AMM 05-51-07-210-801 NO DAMAGE NOTED AT THIS TIME, OK TO CONTINUE. WILL OBSERVE MAX QUICKTURN TIME ON GROUND COMPLETED BIRD STRIKE INSPECTION AMM 05-51-18-210-801 NO DAMAGE NOTED ADD EMP:U386235

Part: LEVER — STUCK (NA) · airframe 46,072 hrs · 16,153 cycles

LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POS AFTER TAKEOFF. WE PINNED THE GEAR FOR GEAR CONTROL SYSTEM TEST FOR VERIFICATION. AND REMOVED THE COVER FOR THE GEAR HANDLE BOX. FOUND A SPACER ACCOMPLISHED LANDING GEAR CONTROL SYSTEM TEST. OPS CHECKED NORMAL.

Part: DOOR — WARNING LIGHT (AFT ENTRY DOORS) · airframe 45,203 hrs · 15,849 cycles

LOW SPEED REJECT 60 KIAS AFT ENTRY MASTER CAUTION. CHECKED BOTH AFTER ENTRY DOORS, BOTH CKD GOOD. DOORS SWITCHES DUPLICATE GRIPE BOTH WERE INSTACT AND NOT LOOSE. NOT DECTES DETECTED ON VISUAL INSPECTIONOF DOOR LATCHING MECHAISMS , CK''D GOOD REF AMM 52-13-00. DOOR WARNING SYS CK''D REF AMM 52-71-00 UNABLE TO

Part: SEAL — MISSING (RH I/B MAIN FLAP) · airframe 44,645 hrs · 15,638 cycles

PDA 3 RIGHT WING INBOARD MAIN FLAP OUTBD END LOWER SEAL COMPLETELY MISSING -- SEE PHOTO PHOTO ADDED INSTALLED NEW SEAL REF IPC 27-51-11-01A

Part: PANEL — MISSING (RH ELEVATOR) · airframe 43,904 hrs · 15,354 cycles

PDA 3 FOUND PANEL ON RIGHT HAND ELEV MISSING NO DAMAGE NOTED IN AREA TOCS LOG CREATED FOR THIS PDA 3 ITEM. LAS MM INSTALLED PANEL REF AMM 55-10-11-400 ON LOG PAGE 7620695. NO FUTHER DEFECTS NOTED. ARMENTA TOMC 14DEC21

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 38,591 hrs · 13,329 cycles

SEATS 26A 26B EMER PATH LIGHT PUSHED IN OUT OF ITS BASE. REPLACED EEL PIG TAIL. OP CHECKS GOOD.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 36,692 hrs · 12,604 cycles

RECEIVED FLIGHT AND SPOKE TO CAPTAIN. ON TAKEOFF, CAPT SPOKE OF HEAVY VIBRATION AFTER SELECTING GEAR UP, ALSO RECEIVED 3 GREEN AND 3 RED LIGHTS. MOVED GEAR SELECTOR TO OFF POSITON. AS PER CAPTAINS VERBAL, RESEARCHED TASK 32-30-00-810-815. ON INITIAL FLIGHTDECK INSPECTION, FOUND MANUAL EXTENSION ACCESS DOOR UNLATCHED AND AJAR. TIRE PRESSURE CHECK NORMAL AND WALK AROUND FOUND NO DISCREPANCIES. PER FIM TASK 32-51-00-810-803. IN ADDITION, PLEASE INSPECT AND TROUBLESHOOT REF L/P 8606695 FOR WORK PERFORMED. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER MODULE AND PERFORMED OPS CHECK OF MAIN GEAR NORMAL EXTENSION AND RETRACTION. OPS CHECK NORMAL AT THIS TIME. REF L/P 8606991 FOR WORK PERFORMED. PERFORMED ADJUSTMENT OF LANDING GEAR MANUAL EXTENSION ACCESS DOOR SWITCH. NO FAULTS OR DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,054 hrs · 11,252 cycles

AFT SEAT 15C EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB AND LENS. EMERGENCY LIGHT OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,813 hrs · 10,425 cycles

THE EMERGENCY ISLE PATH LIGHTING IN THE COACH SECTION IS INOP. R&R M1672 BATTERY PACK IAW AMM 33-51-06-960-805. REMOVED AND REPLACED BATTERIES M1671, M2626, M1670, AND M2503. OPS CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,813 hrs · 10,425 cycles

EMERGENCY EXIT LIGHTS INOP AT THE L1 DOOR (INSIDE AND OUT). REPLACED BATTERY PACK ON M1675 AT STA 322 WL 291 LBL 7 PER AMM 3 3-51-06-960-805. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,364 hrs · 9,889 cycles

FOUND DURING 2SVC, LEFT OVERWING EMERGENCY LIGHTS AND INSIDE CABIN FROM 22C TO 27C EMERGENCY LIGHTS INOPERATIVE. REPLACED THE OVERWING LAMPS IAW MM 33-51-04-960-801. ALL EMERGENCY LIGHTS OPS CHECK GOOD.

Part: CLAMP — LOOSE (AC BAY) · airframe 28,383 hrs · 9,549 cycles

ON TAKEOFF AT 25KTS WW FIRE LIGHT & BELL INDICATION. REJECT TAKEOFF RUN FOUND CLAMP LOOSE ON PNEUMATIC DUCT IN THE NR 2 PACK BAY, SECURED & RAN ENG HIGH POWER. OPERATIONS CHECKED GOOD WITH NO LEAKS.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LOG PAGE 9736654 ENTRY WAS MADE IN ERROR. LOWER RT HORIZONTAL STAB SKIN CRACK FOUND AT STATION 101.9, 1"LONG LOCATED 11" FROM REAR SPAR. CUT OUT DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02518 & SRM 55-10-01 REPAIR 11. A DETAIL VISUAL & LFEC INSPECTION TO BE PERFORMED AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & AT INTERVALS OF 9,000 FLIGHT CYCLES THEREAFTER. SEE ORIGINAL LOG PAGE 9736654 FOR ALL WORK PERFORMED.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LOWER LT HORIZONTAL STAB SKIN CRACK FOUND AT STATION 129.50, 1/2" LOCATED 10.5" FROM REAR SPAR. REPAIRED LT LOWER SKIN IAW ECRA 5510-02517. PLACED IN DIP TO BE INSPECTED, SKIN & DOUBLER EVERY 9000 FLIGHT CYCLES AFTER 56000 INSPECTION THRESHOLD IAW SRM 55-10-01 REPAIR 11 PAGE 217. 55-DIP 33698.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LOWER LT HORIZONTAL STAB SKIN CRACK FOUND AT STATION 147.9, 1/2" LONG LOCATED 10" FROM REAR SPAR. INSTALLED DOUBLER REPAIR IAW ECRA 5510-02517 & PLACED IN DIP TO BE INSPECTED. INSPECT AT THRESHOLD OF 56,000 FLIGHT CYCLE AFTER REPAIR INSTALL & REPEAT AT INTERVALS OF EVERY 9000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01 REPAIR 11 DIP CONTROL NR 33695.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

NUMBER 3 VERTICAL STIFFENER CRACKED ON RIB, LT HORIZONTAL STAB STATION 120.30. REPAIRED IAW ECRA 5510-02515.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LOWER RT HORIZONTAL STAB SKIN CRACK FOUND AT STATION 101.9, 1" FROM REAR SPAR. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02518 & SRM 55-10-01 REPAIR 11. A DETAIL VISUAL & LFEC INSPECTION TO BE PERFORMED AT 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & AT 9,000 FLIGHT CYCLE INTERVALS IAW SRM 5 5-10-01 REPAIR 11 TABLE 204. THIS LOG PAGE DISCREPANCY ENTRY WAS MADE IN ERROR. SEE NEW LOG PAGE 9739199 CONTROL 33691 55-DIP FOR CORRECT ENTRY. UPDATE CONTROL 33691. INSPECT AT THRESHOLD OF 56,000 FLIGHT CYCLE AFTER REPAIR INSTALL & REPEAT AT INTERVALS OF EVERY 9000 FLIGHT CYCLES THERE AFTER IAW SRM 55-10-01 REPAIR 11. DIP CONTROL 33692.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LOWER LT HORIZONTAL STAB SKIN CRACK FOUND AT STATION 129.50, 3/4" LONG LOCATED 19" FROM REAR SPAR. REPAIRED LOWER LT HORIZONTAL STATION SKIN AT STATION 129.50 IAW SRM 55-10-01 REPAIR 11.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN REQUIRES ACCESS CUT OUTS FOR STATION 92.70 RIB STIFFENERS 1 & 2 REPAIRS. DISCREPANCY SHOULD READ HAND LOWER HORIZONTAL STAB SKIN CRACKED. THIS LOG PAGE WAS CLOSED IN ERROR. SEE LOG PAGE 9739198 FOR CONTINUATION OF DIP. CUT OUT ACCESS HOLES. FABRICATED & INSTALLED REPAIR DOUBLER IAW ECRA 5510-02518 & SRM 55-10-01 REPAIR 11. A DETAIL VISUAL & LFEC INSPECTION TO BE PERFORMED AT 56,000 FLIGHT CYCLES AFTER INSTALLATION & AT INTERVALS OF 9,000 FLIGHT CYCLES THEREAFTER IAW SRM 55-10-01 REPAIR 11 TABLE 204. THIS LOG PAGE DISCREPANCY ENTRY WAS MADE IN ERROR. SEE NEW LOG PAGE 9739198 CONTROL 33692, 55-DIP FOR CORRECT ENTRY. UPDATE CONTROL NR 33692.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 24,691 hrs · 8,340 cycles

LEFT STABILIZER LOWER INTERNAL INSPAR, INBD RIB TRANSITION RADIUS STIFFENER NR 2 IS CRACKED. REPAIRED IAW ECRA 5510-02515.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,340 cycles

HFEC CRACK INDICATION AT FASTENER HOLES COMMON TO THE SPLICE STRAP ON SEAT TRACK OTBD FLANGES FWD OF FLOORBEAM STATION 727B AT RBL 24.75, AS INDICATED BY EA 5320-02076 REF F STEP 3 6. REPAIRED SEAT TRACK IAW ECRA5320-02469. SEE ENTRIES BELOW FOR ALL WORK PERFORMED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,340 cycles

HFEC CRACK INDICATION AT FASTENER HOLES COMMON TO THE SPLICE STRAP, ON SEAT TRACK OTBD FLANGES FWD OF FLOORBEAM STATION 727B AT RBL 45.5, AS INDICATED BY EA 5320-02076 REV F STEP 3.6. REPAIRED SEAT TRACK IAW ECRA 5320-02470. SEE ENTRIES BELOW FOR ALL WORK PERFORMED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,340 cycles

HFEC CRACK INDICATION AT FASTENER HOLES COMMON TO THE SPLICE STRAP, ON SEAT TRACK OTBD FLANGES FWD OF FLOORBEAM STATION 727B AT LBL 24.75, AS INDICATED BY EA 5320-02076 REV F STEP 3.6. REPAIRED SEAT TRACK IAW ECRA 5320-02468.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 24,691 hrs · 8,340 cycles

HFEC CRACK INDICATION AT FASTENER HOLES COMMON TO THE SPLICE ON SEAT TRACK OTBD FLANGE OF FLOOR BEAM STATION 727B AT BL 45.5, AS INDICATED BY EA 5320-02076 REV F STEP 3 3.6. REPAIRED SEAT TRACK IAW ECRA 5320-02467.

Part: LIGHT — DAMAGED (CABIN) · airframe 20,050 hrs · 6,830 cycles

SUPPORT TASK SEAT ROW 9ABC SEAT EMERGENCY PATH LIGHTING DESTROYED. REMOVED EPL LIGHT FIXTURE & INSTALLED NEW EPL LIGHT FIXTURE IAW CMM R1 25-22-51, OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 16,262 hrs · 5,452 cycles

RIGHT HORIZONTAL STAB LOWER SKIN STA 175.50 FOUND CRACKED .7500" LONG AND LOCATED ABOUT 10" FROM AFT SPAR. REPAIRED IAW SRM 55-10-01.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 16,262 hrs · 5,452 cycles

RIGHT HORIZONTAL STAB LOWER SKIN STA 157.10 FOUND CRACK 3/4 INCH LONG AND LOCATED ABOUT 10" FROM AFT SPAR. REPAIRED AS PER SRM 55-10-01 REPAIR 11.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 1,178 hrs · 472 cycles

FORWARD MEGAPHONE SIREN INOPERATIVE. REMOVED AND REPLACED MEGAPHONE WITH BORROWED PART FROM DELTA REF ECRA 2564-01027.