N919CA

Part: SKIN — CRACKED (ZONE 200) · airframe 115,632 hrs · 17,381 cycles

DURING A CHECK AT RKSI, WHILE PERFORMING FCD 744-53-0076 R2, 250 FLIGHT CYCLE (FC) REPETITIVE INSPECTIONS FOR SCRIBE LINE FINDINGS ON SB 747-53A2563 LIMITED RETURN TO SERVICE (LRTS) PROGRAM, IT WAS DISCOVERED THAT SKIN PANEL 33L WITH P/N: 65B04135-343 HAVE 02 EACH 0.5 INCH CRACKS. PERMANENT REPAIR WAS ACCOMPLISHED IAW MSG MUA-MUA-25-0057-15B AND BOEINGREPAIRSKETCH_MUA-MUA-25-0057-12C REFERENCE COMMUNICATION SYSTEM MESSAGE NUMBERS FOR CASE #06216788, AND APPROVED ON 8100-9

Part: ENGINE — FAULTED (NR 4) · airframe 112,734 hrs · 16,909 cycles

DURING TAKE-OFF ROLL, SHORTLY AFTER SELECTING "TOGA", ENGINE NUMBER 4 SHOWED RED EGT INDICATION AS AIRCRAFT VEERED SIGNIFICANTLY TO THE LEFT. LOW SPEED (APPROXIMATELY 40 KTS.) RTO CARRIED OUT. ENGINE NUMBER 4 WAS DETERMINED UNSERVICEABLE AND REPLACED PRIOR TO FURTHER OPERATIONS.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 112,724 hrs · 16,908 cycles

WHILE PERFORMING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL. EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION - M5057 STA 717 LBL 8

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 112,724 hrs · 16,908 cycles

WHILE PERFORMINNG OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PIPLOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER TO POSITON M5055 STA 610 LBL 88.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 112,724 hrs · 16,908 cycles

FOUND CRACK ON SEAT TRACK BETWEEN STA 980 AND STA 1000 LBL 75 (MAIN DECK)

Part: SEAT TRACK — CRACKED (ZONE 20) · airframe 122,724 hrs · 16,808 cycles

FOUND CRACKON SEAT TRACK FWD CARGO STA 580, RBL 24

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 122,724 hrs · 16,808 cycles

MAIN DECK BETWEEN STA 980 AND STA 1000 RBL 75 FOUND CRACK ON SEAT TRACK.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 112,724 hrs · 16,908 cycles

WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTS, POWER PACK AND ATTENDANT SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION M5056 STA LBL 6

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 112,724 hrs · 16,908 cycles

DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5056 AT BS 663, LBL 8, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 112,724 hrs · 16,908 cycles

DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5057 AT BS 717, LBL 8, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 112,724 hrs · 16,908 cycles

DURING SCHEDULED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, POWER PACKS, AND ATTENDANT PANEL, BATTERY POWER SUPPLY M5055 AT BS 610, LBL 88, DOES NOT SUPPLY POWER. POWER SUPPLY BATTERY PACK REPLACED AND OPERATIONALLY CHECKED WITH NO DEFECTS.

Part: RELAY — BROKEN (B FIRE LOOP) · airframe 111,838 hrs · 16,763 cycles

ENGINE INDICATING CREW ALERTING SYSTEM (EICAS) MESSAGE "FIRE MN DK MID". - BENT PIN DISCOVERED ON LOOP B RELAY R5168 CAUSING INTERMITTANT LOOP B FIRE WARNING INDICATION. REPLACED RELAY R5168. LOOP B FUNCTIONS NORMAL PER AIRCRAFT MAINTENANCE MANUAL 26-10-00. DEFERRED MAIN DECK CARGO FIRE WARNING LOOP A SYSTEM PER MEL 26-14-01-02.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 109,855 hrs · 16,454 cycles

DURING SCHEDULED A-CHECK MAINTENANCE, AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHT SYSTEM RESULTED IN FINDING OF INOPERATIVE LIGHT BULB AT THE UPPER DECK STAIRS POSITION. REMOVED AND REPLACED LAMP. OPS GOOD IAW AMM 33-51-00. OPS GOOD.

Part: COWLING — DAMAGED (ZONE 400) · airframe 108,798 hrs · 16,297 cycles

#4 ENGINE INBOARD THRUST REVERSER TRANSLATING COWL DAMAGED BEYOND LIMITS. REPAIRED PER FVCI ENGINEERING ORDER #23075-1.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 106,498 hrs · 15,911 cycles

SEAT TRACK ON M/D STA 1265-1480, RBL 11.33 WAS FOUND BROKEN AND NO APPLICABLE REPAIR IN 747-400SF SRM. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22089-4, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 06, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVL7995.

Part: COWLING — DENTED (ZONE 400) · airframe 106,498 hrs · 15,911 cycles

IT WAS DISCOVERED (3 EA.) ELONGATED FASTENER HOLES IN THE OUTER SKIN OF THE RIGHT CORE COWL (P/N 224-2302-545, S/N 0619) CURRENTLY INSTALLED ON AIRCRAFT N919CA LOCATED AT APPROXIMATE NAS STA. 307.00, THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22089-3, REV 8, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 06, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN5780.

Part: ACCESS PANEL — ELONGATED (ZONE 400) · airframe 106,498 hrs · 15,911 cycles

DURING SCHEDULED INSPECTION, 2EA FASTENER HOLES ON 462ER DOOR ASSY (P/N: 311 U2060-110) C/T NO.2 PYLON RHS WERE FOUND ELONGATED. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22089-5, REV A, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JUNE 29, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN5749.

Part: COWLING — WORN (ZONE 400) · airframe 106,498 hrs · 15,911 cycles

WEAR DAMAGE WAS FOUND ON NO.3 ENG RH CORE COWL (P/N:224M4761-539, S/N: 1099) FWD FRAME EXISTING REPAIR. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-7, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JUNE 29, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVL7326.

Part: PYLON — DAMAGED (ZONE 400) · airframe 106,498 hrs · 15,911 cycles

IT WAS DISCOVERED AN ELONGATED FASTENER HOLE IN THE NO.2 PYLON INBOARD SKIRT PANEL FAIRING, P/N 311U2170-99, AT NAG STA 354. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-10, REV A, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 05, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN2910.

Part: SKIN PANEL — DENTED (ZONE 100) · airframe 106,498 hrs · 15,911 cycles

DURING ROUTINE MAINTENANCE IN HHN (KIRCHBERG, GERMANY), MAINTENANCE DISCOVERED TWO DENTS WITH GOUGES AT STA 5QO-520, S-22L-23L. CATEGORY 8 REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC'S ENGINEERING ORDER 22032-2, REV D, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 07, 2022, DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVL1246.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 106,498 hrs · 15,911 cycles

SEAT TRACK (P/N: 65B38272-1) ON CABIN MAIN DECK STA 1481 -1766, LBL 11.33 WAS FOUND BROKEN, THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-9, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 06, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN5020.

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 106,498 hrs · 15,911 cycles

BULKHEAD WEB (P/N: 6B815085-1077) WAS FOUND CRACKED AT STA 1480 BETWEEN WL140 AND WL 152. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-6, REV LR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JUNE 30, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN0591.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 106,498 hrs · 15,911 cycles

DURING ROUTINE INSPECTION, L/H BS1140 FRAME WEB & FRAME FOUND CRACK. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-07 REPAIR 2, REV 115. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN4056.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 106,498 hrs · 15,911 cycles

DURING ROUTINE INSPECTION, TENSION TIE - L/H BS 1180 FWD CHANNEL (REPAIRED PART) FOUND CRACK. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-40-30-2R-2 REPAIR 2, REV 54. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN3561.

Part: SHEAR WEB — CRACKED (ZONE 300) · airframe 106,498 hrs · 15,911 cycles

IT WAS FOUND 2 EA CRACKS ON THE VERTICAL STABILIZER T/E BEAM RHS WEB (P/N: 173U1010-31) APPROX.AT RUD STA 307 AND RUD STA 332. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-8, REV IR, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JUNE 28, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN6291 AND KVN6234.

Part: FRAME — CRACKED (ZONE 200) · airframe 106,498 hrs · 15,911 cycles

DURING INCORPORATION OF NAL FCD NO. 744-53-0061 R1 (SB 747-53A2450 REV 8) TO DO INSPECTION OF #5 MED LEFT, SECTION 46 BS 2231 FRAME, STR 15L THROUGH 15R, 1 EA HOLE WAS FOUND CRACKED ON LH FRAME INNER CHORD (P/N: 65B01849-51) FWD FLANGE AND STRAP (P/N: 65B01849-47) AT S-16L AND 1 EA HOLE WAS FOUND CRACKED ON RH FRAME STRAP (P/N: 65B01849-48) AT S-16R, CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH HAECO XIAMEN'S ENGINEERING NOTES EB-53-2854, REV ORIGINAL, WHICH WAS APPROVED BY FAA FORM 8100-9 DATED ON JULY 06, 2022. DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVN3587 AND KVN3579.

Part: PANEL — CRACKED (ZONE 400) · airframe 106,498 hrs · 15,911 cycles

IT WAS DISCOVERED CRACKS IN THE NO. 1 PYLON SKIRT BEAM OUTBOARD PANEL ASSEMBLY NEAR NAC STA 329. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-1, REV 8, WHICH WAS APPROVED BY FAA FORM 8110-3 DATED ON JULY 07, 2022, DETAILS WERE DOCUMENTED IN HAECO XIAMEN'S NRC KVL3416

Part: POWER SUPPLY — INOPERATIVE (DOOR EMER OPEN) · airframe 102,959 hrs · 15,344 cycles

UPPER DECK RIGHT DOOR EMERGENCY BOTTLE SQUIB BATTERY TEST INOPERATIVE. - REMOVED AND REPLACED UPPER DECK DOOR BOTTLE SQUIB BATTERY IAW B747-400 AIRCRAFT MAINTENANCE MANUAL 52-23-14.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 102,498 hrs · 15,256 cycles

REFER TO LP 43984-3 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1620, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 1620 IAW FVCI EO #21077-1 REV. IR. THIS REPAIR IS TEMPORARY AND WILL BE REPLACED AT NEXT "C" CHECK.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 102,498 hrs · 15,256 cycles

REFER TO LP 43984-1 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1540, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 1540 IAW FVCI EO #21077-1 REV. IR. THIS REPAIR IS TEMPORARY AND WILL BE REPLACED AT NEXT "C" CHECK.

Part: HYDRAULIC LINE — CRACKED (NR 1 HYD SYSTEM) · airframe 102,357 hrs · 15,234 cycles

REFERENCE NATIONAL AIRLINES AML 44070-1: DURING TAXI, SMELLED BAD HYDRAULIC ODOR AND RETURNED TO GATE. FOUND HYDRAULIC LEAK IN SYSTEM #1 HYDRAULIC LINE, LEFT SIDE FUSELAGE AT BS 900. REPLACED SUBJECT HYDRAULIC LINE WITH TEMP "FLEXIBLE" HYDRAULIC LINE IAW B747-400 AMM 20-11-05. NO LEAKS NOTED.

Part: FMC — FAILED (RIGHT) · airframe 101,456 hrs · 15,107 cycles

DISCREPANCY: LP 43593 - AIRCRAFT ENCOUNTERED A FAULT IN THE RIGHT FLIGHT MANAGEMENT COMPUTER (FMC). SIMULTANEOUSLY WITH THIS FAULT, AN AUTO-PILOT (A/P) CAUTION ILLUMINATED WITH AN UNCOMMANDED "NOSE DOWN" PITCH IN THE AIRCRAFT WITH THE A/P ENGAGED. IMMEDIATE ACTIONS: A/P WAS DISCONNECTED AND NOSE DOWN CONDITION CORRECTED. NO FURTHER ISSUES DURING THE REMAINDER OF THE FLIGHT. CORRECTIVE ACTION: THE RIGHT FMC WAS REPLACED WITH OPS CHECK NORMAL, AND THE A/P SYSTEM WAS WAS FUNCTIONALLY TESTED THROUGH ALL PARAMETERS WITH NO ISSUES NOTED.

Part: ACCESS PANEL — MISSING (NR 1 NACELLE) · airframe 1,000,020 hrs · 14,891 cycles

UPON WALK-AROUND, FOUND NR 1 PYLON ACCESS PANEL 452FR MISSING. INTERIM ACTION: INSTALLED INTERIM REPAIR, AS PER GMM 13.1.3. ITEM APPROVED FOR ACI, AS PER GMM 3.8.11 AND GMM 13.1.3. ITEM TRANSFERRED TO DMI 200006-600 CAT "ACI", DUE AT NEXT STATION WITH ADEQUATE MAINTENANCE SUPPORT AND MATERIALS. RESOLUTION: INSTALLED NR 1 PYLON PANEL 452FR, AS PER B747-400 AMM 20-51-01. DMI NR 200006-600 CLEARED.

Part: RELAY — INOPERATIVE (ZONE 100) · airframe 98,581 hrs · 14,688 cycles

FLAPS CONTROL EICAS MESSAGE DISPLAYED ON FINAL APPROACH. PERFORMED GO AROUND, COMPLETED CHECKLIST AND LANDED WITHOUT INCIDENT. - CENTRAL MAINTENANCE COMPUTER MESSAGES 27600, 27601, AND 27602 FOUND ACTIVE, FLAP CONTROL UNIT LEFT, RIGHT, AND CENTER FAIL. REMOVED AND REPLACED RELAYS R07632 AND R07633. OPS CHECK NORMAL IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 27-51-00. EICAS MESSAGES CLEARED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 98,470 hrs · 14,673 cycles

FUSELAGE SKIN DAMAGED SECTION 48, BODY STATION 2655 TO 2689, STRINGER 5L TO 11L - ACCOMPLISHED MAJOR REPAIR OF DAMAGE IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. ENGINEERING ORDER CONTROL NUMBER 20138 REVISION A DATED APRIL 15, 2020, DATA APPROVED ON FAA FORM 8110-3 CONTROL NUMBER 20138 DATED APRIL 16, 2020.

Part: VALVE — STUCK (FUEL SYSTEM) · airframe 96,734 hrs · 14,358 cycles

DURING REFUELING, THE RIGHT HAND SURGE TANK STARTED VENTING FUEL. - FOUND NUMBER 4 MAIN TANK REFUEL VALVE STICKING IN THE PARTIALLY OPEN POSITION. EXERCISED THE VALVE MANUALLY AND SYSTEM OPERATIONAL CHECK WAS NORMAL IN ACCORDANCE WITH B747-400 AIRCRAFT MAINTENANCE MANUAL 28-21-00.

Part: SPOILER — DAMAGED (LT WING NR 6) · airframe 96,278 hrs · 14,285 cycles

PARTS DEPARTING AIRPLANE REPORTING - NUMBER 6 SPOILER PANEL FOUND DAMAGED, WITH PIECES MISSING. - NUMBER 6 SPOILER PANEL WILL BE REPLACED, PRIOR TO NEXT DEPARTURE.

Part: FLOOR PANEL — GOUGED (ZONE 200) · airframe 96,004 hrs · 14,243 cycles

AFTER MAIN DECK CARGO WAS OFF LOADED FOUND DAMAGE ON THE LEFT HAND SIDE OF MAIN DECK CARGO FLOOR PANELS FROM STATION 900 TO 1600. ACCOMPLISHED TIME LIMITED REPAIR OF MULTIPLE FLOOR PANELS IN THE MAIN CARGO DECK BETWEEN STATIONS 960 TO STATION 1640, WATER LINE 199.8, LEFT OF BUTT LINE 93, IN ACCORDANCE WITH ENGINEERING ORDER CONTROL NUMBER 19341 REVISION IR.

Part: LIFE RAFT — LOW PRESSURE (CABIN) · airframe 95,903 hrs · 14,228 cycles

UPPER DECK LIFE RAFT REMOVED DUE TO LOW PRESSURE - INSTALLED SERVICEABLE LIFE RAFT PER AIRCRAFT MAINTENANCE MANUAL 25-62-01.

Part: WINDOW — BROKEN (BS 750) · airframe 95,549 hrs · 14,165 cycles

ON POST FLIGHT INSPECTION FOUND WINDOW OUTER PANE ON RIGHT SIDE AT STATION 750 BROKE. REMOVED AND REPLACED MIDDLE AND OUTER WINDOW PANES IN ACCORDANCE WITH B747-400 AMM 56-21-01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 93,968 hrs · 13,885 cycles

RIGHT UPPERDECK EMERGENCY EXIT DOOR BATTERY FOUND WITH LOW VOLTAGE. - REMOVED AND REPLACED RIGHT UPPERDECK EMERGENCY EXIT DOOR POWER SUPPLY BATTERY IN ACCORDANCE WITH B747-400 AMM 33-51-06. OPERATTIONAL TEST FOUND SATISFACTORY.

Part: STRINGER — CRACKED (LE SLAT) · airframe 95,752 hrs · 13,841 cycles

NUMBER 20 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.

Part: STRINGER — CRACKED (LE SLAT) · airframe 95,752 hrs · 13,841 cycles

NUMBER 7 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED VARIABLE CAMBER FLAP ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 27-81-02.

Part: RIB — CRACKED (RT WING) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND LEADING EDGE SUPPORT RIB FOUND CRACKED 0.70 INCHES AT ILES 330. REPLACED RIB PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.

Part: STIFFENER — CRACKED (LT WING) · airframe 95,752 hrs · 13,841 cycles

LEFT HAND WING INTERIOR OF PANEL 511CTA, INBOARD CORNER VERTICAL STIFFENER HAS 1.5 INCH CRACK. REPLACED VERTICAL STIFFENER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.

Part: RIB — CRACKED (RT WLG DOOR) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND WING LANDING GEAR INBOARD WHEEL WELL DOOR, FORWARD EDGE FOUND 1 EACH 1.2 INCH CRACK. REPAIRED PER DRAWING 52-18298-1 REVISION NEW, DATED OCTOBER 08, 2018.

Part: WEB — CRACKED (RT WING) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND LEADING EDGE SUPPORT WEB LOWER FLANGE FOUND CRACKED 0.50 INCHES AT WING LEADING EDGE STATION 330.0. REPLACED WEB PER STRUCTURAL REPAIR MANUAL 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 95,752 hrs · 13,841 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE LEFT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 1 EACH 0.125 INCH CRACK WAS DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MODIFICATION/SMALL REPAIR.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 95,752 hrs · 13,841 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2651 REVISION 1 STATION 2403.6 TO STATION 2524.4, UPPER LOBE DOUBLER AT THE FUSELAGE VERTICAL STABILIZER ATTACH FITTINGS INSPECTION, A 2 INCH CRACK WAS DISCOVERED ON THE RIGHT HAND SIDE, FROM STATION 2519 TO 2521 - ACCOMPLISHED PART 3 - UPPER LOBE DOUBLER REPAIR OF SERVICE BULLETIN 747-53A2651 REVISION 1, WITH NO DEVIATIONS.

Part: STRAP — CRACKED (FUSELAGE) · airframe 95,752 hrs · 13,841 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 2 EACH 0.125 INCH CRACKS WERE DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MODIFICATION/SMALL REPAIR.

Part: SKIN — DEFORMED (RT WING) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND WING LEADING EDGE SKIN OUTBOARD OF LANDING LIGHT HAS TILTED FASTENERS. REPAIRED PER STRUCTURAL REPAIR MANUAL 57-41-01-2R-5.

Part: FILLER — CRACKED (FUSELAGE) · airframe 95,752 hrs · 13,841 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 3 EACH 0.10 INCH CRACKS WERE DISCOVERED ON FILLER. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MODIFICATION/SMALL REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,752 hrs · 13,841 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2416 REVISION 3. FUSELAGE CENTER SECTION BODY STATION 1265 FRAME INSPECTION, REPAIR, AND MODIFICATION, FLOOR INTERCOSTAL. FRAME INNER CHORD ON RIGHT SIDE WAS FOUND CRACKED. ACCOMPLISHED MODIFICATION PER SERVICE BULLETIN 747-53A2416 REVISION 3.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND WING TRAILING EDGE CAVITY PANEL SUPPORT BEAM AFT END ATTACH BRACKET CRACKED. REPLACED BRACKET PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.

Part: SKIN — DAMAGED (RT WING) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND WING LEADING EDGE SKIN RIVETS LOOSE AND HOLES ELONGATED AT ILES 693.5. REPAIRED PER FLIGHT VEHICLES CONSULTING DRAWING NUMBER 57-18290-1 DATED 10/05/2018.

Part: STRINGER — CRACKED (LE SLAT) · airframe 95,752 hrs · 13,841 cycles

NUMBER 20 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.

Part: SKIN PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP HAS 2 EACH AREAS OF CORROSION ON LOWER SKIN PANEL. CORROSION CLEANUP OUTSIDE OF STRUCTURAL REPAIR MANUAL LIMITS. REPLACED RIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP PER AIRCRAFT MAINTENANCE MANUAL 27-51-05.

Part: STRINGER — CRACKED (LE SLAT) · airframe 95,752 hrs · 13,841 cycles

NUMBER 7 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 95,752 hrs · 13,841 cycles

UPPER DECK RIGHT HAND DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY SUPPLY ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 31-31-04. LIGHT OPERATES NORMAL.

Part: SKIN — WORN (LT BLG DOOR) · airframe 95,752 hrs · 13,841 cycles

LEFT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18303-1.

Part: SKIN — DAMAGED (RT BLG DOOR) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18315-1.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 95,752 hrs · 13,841 cycles

EMERGENCY LIGHTS L1853, L1854, AND L5735 ARE INOPERATIVE (MAIN DECK LEFT DOOR). REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-04. LIGHTS OPERATE NORMAL.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 95,752 hrs · 13,841 cycles

RIGHT HAND UPPER DECK DOOR SLIDE RESERVOIR HAS LOW PRESSURE. RESERVOIR REPLACED PER AIRCRAFT MAINTENANCE MANUAL 25-68-02.

Part: SIGN — DAMAGED (CABIN) · airframe 95,752 hrs · 13,841 cycles

UPPER DECK EMERGENCY EXIT SIGN DAMAGED. REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-00.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 92,480 hrs · 13,743 cycles

NUMBER 3 ENGINE INBOARD THRUST REVERSER SLEEVE DAMAGED, WITH HONEYCOMB EXPOSED AT THE 9 O'CLOCK POSITION. - INTERIM REPAIR OF NUMBER 3 ENGINE INBOARD THRUST REVERSER TRANSLATING SLEEVE ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. DRAWING NUMBER 54-17069-1.

Part: WEB — CRACKED (RT WING) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT A D CHECK INSPECTION, FOUND RIGHT WING TRAILING EDGE SUPPORT RIB WEB CRACKED AT INBOARD SIDE OF THE NR 7 GROUND SPOILER. - REMOVED AND REPLACED RIGHT WING TRAILING EDGE SUPPORT RIB WEB IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER CHORD CRACKED AT APPROXIMATE HTSA BUTT LINE 421 OUTBOARD END. REPAIRED LEFT HORIZONTAL STABILIZER LOWER CHORD IN ACCORDANCE WITH SRM 51-70-12.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-9 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB CRACKED. - REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-019 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-013 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-17 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER TIP RIB CRACKED. REPAIRED THE RIB IAW SRM 51-70-11.

Part: WEB — GOUGED (RT ELEVATOR) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT OF D CHECK INSPECTION FOUND RIGHT HAND OUTBOARD ELEVATOR INBOARD WEB GOUGED. REMOVED AND REPLACED RIGHT HAND OUTBOARD ELEVATOR INBOARD WED IN ACCORDANCE WITH SRM 51-40-02.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT OF D CHECK INSPECTION FOUND RIGHT HAND OUTBOARD ELEVATOR NR 3 HINGE BEARING LOOSE IN FITTING. REMOVED AND REPLACED RIGHT HAND OUTBOARD ELEVATOR NR 3 HINGE FITTING AND BEARING IN ACCORDANCE WITH AMM 27-31-03.

Part: FITTING — WORN (THRUST REVERSER) · airframe 89,251 hrs · 13,055 cycles

DURING A D CHECK INSPECTION, FOUND THE NR 4 ENGINE OUTBOARD THRUST REVERSER WILL NOT LATCH DUE TO OUTBOARD THRUST REVERSER FORWARD END HANGING TO LOW. REPLACED HINGE FITTING BEARING AND REPAIRED THRUST REVERSER CENTER HINGE FITTING IAW EO MAS-J217-N919CA-007.

Part: BALLSCREW — BRINELLED (HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

DURING INSPECTION REQUIRED BY AD 2006-10-02 FOUND HORIZONTAL STABILIZER BALLSCREW TO HAVE INDICATIONS OF BRENELLING IN THE NEUTRAL ZONE AREA OF THE BALLSCREW THREADS. REMOVED AND REPLACED HORIZONTAL STABILIZER BALLSCREW IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL CHAPTER 27-41-06.

Part: SKIN PANEL — LOOSE (RT HORIZ STAB) · airframe 89,251 hrs · 13,055 cycles

RIGHT HAND HORIZONTAL STABILIZER LOWER SURFACE AT STATION 440 JUST AFT OF LEADING EDGE HAS REPAIR WITH AREA OF PEELING PAINT AND POSSIBLE LOOSE FASTENERS. REMOVED AND REPLACED PREVIOUS REPAIR IN ACCORDANCE WITH SRM 55-10-01-2R-6. APPLIED PAINT TOP COAT.

Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND BULK CARGO DOOR SCUFF PLATE CRACKED. PERFORMED WELD REPAIR OF BULK CARGO DOOR SCUFF PLATE IN ACCORDANCE WITH ENGINEERING INSTRUCTIONS MAS-J217-N919CA-002-1 AND SRM 53-00-15-2R-15 REPAIR 5.

Part: STRAP — CRACKED (TENSION TIE) · airframe 89,251 hrs · 13,055 cycles

TENSION TIE STRAPS AT BS 1140 LEFT HAVE TWO CRACKS. REMOVED AND REPLACED THE TENSION TIE STRAPS IAW SRM 51-40-02 PAGES 4-7 AND SB 747-53A2507 REVISION 2.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 89,251 hrs · 13,055 cycles

DURING "D' CHECK INSPECTION FOUND EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN BODY STATION 720-741 AND STRINGERS 46 LEFT AND 47 LEFT WITH CRACK. - REMOVED AND REPLACED EXTERNAL FUSELAGE SKIN DOUBLER AT BODY STATION 720-741 BETWEEN STRINGERS 46 LEFT AND 47 LEFT IN ACCORDANCE WITH SRM 53-00-01 FIGURE 201.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER AND LOWER FLANGE CRACKED AT PANEL OPENING FOR ACCESS PANEL 336QBL AT LEFT HAND HORIZONTAL STABILIZER TIP OTBD AFT CORNER. REMOVED AND REPLACED THE CHANNEL IAW DRAWING 65B03710 AND SRM 51-40-02.

Part: STRAP — CORRODED (RT WING) · corrosion level 2 · airframe 89,251 hrs · 13,055 cycles

DURING "D' CHECK INSPECTION FOUND RIGHT WING LEADING EDGE AT 640 ILES UPPER CHORD STRAP WITH CORROSION. REMOVED AND REPLACED RIGHT WING UPPER CHORD STRAP AT 640 ILES IN ACCORDANCE WITH DRAWING NUMBER 65B14548 AND SRM 51-40-02.

Part: FRAME — CRACKED (BS 1160) · airframe 89,251 hrs · 13,055 cycles

PREVIOUS TENSION TIE ATTACH LOCATION AT BS 1160 FRAME WEB HAS TWO PREVIOUS FASTENER HOLES CRACKED. ACCOMPLISHED OVERSIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 89,251 hrs · 13,055 cycles

TENSION TIE AT BS 1120 CRACKED. PERFORMED OVER SIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 89,251 hrs · 13,055 cycles

TENSION TIE AT BS 1160 RIGHT SIDE, FOUND CRACKED. REPAIRED IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 89,251 hrs · 13,055 cycles

TENSION TIE AT BS 1200 FRAME CRACKED. ACCOMPLISHED OVERSIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: PIN — WORN (CARGO DOOR) · airframe 89,251 hrs · 13,055 cycles

MAIN DECK SIDE CARGO DOOR MID FRAME FORWARD LATCH PIN WORN. REMOVED AND REPLACED MAIN DECK SIDE CARGO DOOR LATCH PIN IAW AMM 52-32-24.

Part: PIN — WORN (DOOR LATCH) · airframe 89,251 hrs · 13,055 cycles

MAIN DECK SIDE CARGO DOOR MID FRAME AFT LATCH WORN. REMOVED AND REPLACED THE LATCH PIN IAW AMM 52-32-24.

Part: PIN — WORN (DOOR LATCH) · airframe 89,251 hrs · 13,055 cycles

MAIN DECK SIDE CARGO DOOR FORWARD LATCH PIN WORN. REMOVED AND REPLACED THE LATCH PIN IAW SERVICE BULLETIN 747-52A2294 REVISION 4.

Part: ANGLE — CRACKED (NR 4 NACELLE) · airframe 89,251 hrs · 13,055 cycles

NR 4 NACELLE FIREWALL LOWER SURFACE CRACKED IN THE FAIRING SUPPORT ANGLE. REMOVED AND REPLACED NR 4 NACELLE IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1200) · airframe 89,251 hrs · 13,055 cycles

BS 1200 LEFT FRAME TENSION TIE ATTACH POINT CRACKED. PERFOMED OVERSIZE HOLE REPAIR OF CRACKED FASTENER HOLES IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: FRAME — CRACKED (BS 1160) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT OF AD 2016-05-12, SERVICE BULLETIN 747-53A2507 REVISION 2, FOUND BS 1160 PREVIOUS TENSION TIE ATTACH POINT WITH 2 FASTENER HOLES CRACKED. ACCOMPLISHED PARTIAL FRAME SEGMENT REPLACEMENT IAW SRM 53-40-07, REPAIR 3.

Part: FITTING — LOOSE (ZONE 100) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT OF INSPECTION REQUIRED BY AIRWORTHINESS DIRECTIVE, 2012-07-07 AND SERVICE BULLETIN 747-53A2835 REVISION 1, FOUND AFT CARGO DOOR NR 1 LATCH FITTING PIN LOOSE IN THE FITTING. ACCOMPLISHED REPAIR OF THE AFT CARGO DOOR ATTACH FITTING IN ACCORDANCE WITH SRM CHAPTER 53-00-90-2R-1.

Part: FRAME — CRACKED (BS 1200) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT OF AD 2016-05-12, AND SERVICE BULLETIN 747-53A2507 REV 2, FOUND BS 1200 LEFT FRAME TO HAVE 9 EACH FASTENER HOLES TO HAVE CRACK INDICATIONS AND 3 FASTENER HOLES ON THE TENSION TIE CHANNEL WITH CRACK INDICATIONS. ACCOMPLISHED OVERSIZE FASTENER HOLE REPAIR AT ALL CRACKED FASTENER LOCATIONS IAW SERVICE BULLETIN 747-53A2507 REVISION 2.

Part: SKIN — CHAFED (NR 4 NACELLE) · airframe 89,251 hrs · 13,055 cycles

DURING A D CHECK INSPECTION, FOUND THE NR 4 ENGINE OTBD CORE COWL WITH WEAR GROOVE AT PRE-COOLER EXHAUST DUCT OPENING. REPAIRED IAW EO MAS-J217-N919CA-004.

Part: LONGERON — DAMAGED (NR 4 COWLING) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION FOUND NUMBER 4 ENGINE INBOARD CORE COWL RIVET PULLED THROUGH LOWER EDGE. REMOVED AND REPLACED LOWER AFT SECTION AND DAMAGED FASTENERS IN ACCORDANCE WITH ENGINEERING DISPOSITION EO MAS-J217-N919CA-008 REV IR AND SRM 51-40-02.

Part: FRAME — CRACKED (BS 1200) · airframe 89,251 hrs · 13,055 cycles

BS 1200 FRAME AT TENSION TIE ATTACH, FOUND TO HAVE 9 FASTNER HOLES WITH CRACK INDICATIONS AND THE TENSION TIE CHANNEL WAS FOUND TO HAVE 3 FASTENER HOLES WITH CRACK INDICATIONS. - PERFOMED OVERSIZE HOLE REPAIR AT ALL CRACKED FASTENER HOLE LOCATIONS IN ACCORDANCE WITH BOEING SERVICE BULLETIN 747-53A2507 REVISION 2. PERFOMED POST OVERSIZE HOLE REPAIR HFEC INSPECTION OF 12 EACH FASTENER HOLES AND THEY WERE CONFIRMED TO BE CRACK FREE.

Part: DUCT — CHAFED (NR 2 NACELLE) · airframe 89,251 hrs · 13,055 cycles

DURING A D CHECK INSPECTION, FOUND THE NR 2 ENGINE INBOARD CORE COWL WITH WEAR GROOVE AT PRE-COOLER EXHAUST DUCT OPENING. REPAIRED CORE COWL PRE-COOLER EXHAUST DUCT IAW EO MAS-J217-N919CA-004.

Part: FLAP — PUNCTURED (RT WING) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND, RIGHT HAND INBOARD MID FLAP, FORWARD LOWER FACE OF AFT WEDGE WITH 3 EACH PUNCTURES. REPAIRED DAMAGED AREAS OF RIGHT HAND INBOARD MID FLAP, FORWARD LOWER FACE OF WEDGE IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 57-53-01 AND 51-70-07.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 89,251 hrs · 13,055 cycles

DURING "D' CHECK INSPECTION FOUND SCRAPE AND DENT IN FUSELAGE BELLY SKIN AT BODY STATION 820 LEFT OF BUT LINE 2 INCHES BETWEEN STRINGERS 46 LEFT AND 47 RIGHT. REPAIRED DAMAGED FUSELAGE SKIN BY INSTALLING EXTERNAL DOUBLER IN ACCORDANCE WITH SRM 53-00-01 REPAIR 1

Part: FLAP — DELAMINATED (RT WING) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND, RIGHT HAND, INBOARD, AFT FLAP, FORWARD FACE HAS AREA WITH 3 EACH DENTS WITH DELAMINATION. REPAIRED DENTED AND DELAMINATED AREAS OF RIGHT HAND INBOARD AFT FLAP, FORWARD FACE IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 57-53-01 AND 51-70-07.

Part: BEARING — CORRODED (NR 3 PYLON) · corrosion level 2 · airframe 89,251 hrs · 13,055 cycles

NR 3 PYLON OUTBOARD DUAL SIDE BRACE UPPER BEARING RACE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE BEARING IAW SERVICE BULLETIN 747-54A2218.

Part: SUPPORT RIB — CHAFED (THRUST REVERSER) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND, NUMBER 4 ENGINE OUTBOARD THRUST REVERSER, FIRE SUPPORT RIB WITH WEAR DAMAGE. REPAIRED RIB BY INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 78-32-02.

Part: FITTING — CRACKED (RT WING) · airframe 89,251 hrs · 13,055 cycles

RIGHT WING TRAILING EDGE SUPPORT ROD ATTACH FITTING CRACKED AT OUTBAORD SIDE OF THE NR 8 GROUND SPOILER. REMOVED AND REPLACED FITTING IAW SRM 51-40-02

Part: STIFFENER — CRACKED (RT WING) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND RIGHT WING TRAILING EDGE VERTICAL STIFFENER CRACKED ON UPPER END AT OUTBOARD SIDE OF #8 SPOILER. REMOVED AND REPLACED RIGHT WING TRAILING EDGE VERTICAL STIFFENER IAW SRM 51-40-01.

Part: BATTERY PACK — DEPLETED (ZONE 800) · airframe 89,251 hrs · 13,055 cycles

RIGHT UPPER DECK DOOR FAILS BATTERY CHECK AND PRESSURE CARTRIDGE TEST DC VOLTS LOW. REMOVED AND REPLACED BATTERY POWER PACK IAW AMM 52-23-14.

Part: FLAP — CHAFED (LT WING) · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND, LEFT HAND OUTBOARD FORE FLAP WITH DAMAGE ON OUTBOARD LEADING EDGE. REPAIRED LEFT HAND OUTBOARD FORE FLAP LEADING EDGE IAW STRUCTURAL REPAIR MANUAL CHAPTER 57-53-01 REPAIR 1 AND 51-70-07.

Part: DUCT — DAMAGED (APU) · airframe 89,251 hrs · 13,055 cycles

DURING ACCOMPLISHMENT D CHECK INSPECTION FOUND APU COOLING AIR DUCT WITH 3/4 INCH HOLE. REPAIRED APU COOLING AIR DUCT IN ACCORDANCE WITH ENGINEERING INSTRUCTIONS EO MASJ217-N919CA-006 AND AMM 21-51-12.

Part: LINK — CORRODED (RT WING) · corrosion level 2 · airframe 89,251 hrs · 13,055 cycles

DURING "D" CHECK INSPECTION FOUND, RIGHT WING LEADING EDGE CAVITY RIB SUPPORT LINK CORRODED AT AFT END, WING STATION OLES 1522. REMOVED AND REPLACED RIB SUPPORT LINK IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 AND AIRCRAFT MAINTENANCE MANUAL 20-51-01

Part: FAIRING — DENTED (LT WING TE FLAP) · airframe 87,066 hrs · 12,614 cycles

NR 3 T/E FLAP MOVEABLE FAIRING HAS 5.5" LONG BY 1.5" HIGH BY 0.040" DEEP DENT ON OTBD SIDE, 52" AFT OF L/E, 32" DOWN FROM TOP. REPAIRED IAW ERO 5750ERO2110, REV IR, DATED 01/07/2016 REF FAA FORM 8110-3 008-884-16-2110 FOR DATA APPROVAL.

Part: SKIN — DAMAGED (BS 163) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 163.7, STRINGER 30L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: SKIN — DAMAGED (BS 164) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 164.5, 1.1 BELOW STR 26L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: SKIN — DAMAGED (BS 220-240) · airframe 86,928 hrs · 12,567 cycles

FOUND FORWARD FUSELAGE TO HAVE LIGHTNING STRIKE DAMAGE 2 LOCATIONS AFT OF RADOME LT SIDE BETWEEN BS 220-240, STR 30L. ACCOMPLISHED REPAIRS OF LIGHTNING STRIKE DAMAGE IAW THE MFG INSTRUCTIONS PROVIDED IN SERVICE REQUEST 4-3075414030, MESSAGE MUA-MUA-15-0074-05B. INSTALLED OVERSIZE FASTENER AND BLEND OUT OF SKIN.

Part: FAIRING — CRACKED (NR 4 NACELLE) · airframe 86,928 hrs · 12,567 cycles

FOUND NR 4 PYLON INBD SIDE, SKIRT FAIRING TO HAVE 1 CRACK 8" IN LENGTH. REPAIRED DAMAGED AREA IAW ERO 5450 ERO2105, REV A.

Part: SKIN — DAMAGED (BS 187) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 187, STRINGER 28L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: SKIN — DAMAGED (BS 206) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 206, STR 28L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTENER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: FAIRING — DENTED (ZONE 400) · airframe 86,928 hrs · 12,567 cycles

NR 3 PYLON OTBD HYDRAULIC ACCESS BAY DOOR HAS 1 DENT. DENT LENGTH 3". ACCOMPLISHED MAJOR REPAIR IAW ASI SOLUTIONS EO 5410ERO2105, REV IR.

Part: SKIN — DAMAGED (BS 193) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 193, 3" ABOVE STRINGER 30L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: SKIN — DAMAGED (BS 187) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 187, 4.2" ABOVE STR 28L. REPAIRED LIGHNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: SUPPORT BEAM — CRACKED (ZONE 600) · airframe 86,928 hrs · 12,567 cycles

TWO CRACKS FOUND ON NR 8 SPOILER SUPPORT BEAM WEB. 1 CRACK 1.250" ON RT SIDE OF SUPPORT BEAM WEB AND 1, 1" CRACK ON LT SUPPORT BEAM WEB. R & R NR 8 SUPPORT BEAM IAW SRM 51-41-02.

Part: SKIN — DAMAGED (BS 206) · airframe 86,928 hrs · 12,567 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 206.5, 4.5" ABOVE STRINGER 28L. REPAIRED LIGHTNING STRIKE DAMAGE BY INSTALLATION OF SOLID FASTNER IAW SRM 53-00-01-2R-9, REPAIR 9.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 86,291 hrs · 12,451 cycles

DURING DAILY SERVICE CHECK FOUND RT UPPER DECK DOOR 6 VOLT BATTERY EMERGENCY OPENING TEST SWITCH WILL NOT TEST. SWAPPED LT AND RT BATTERY PACKS PROBLEM FOLLOWED. REINSTALLED BATTERY PACKS IN ORIGINAL POSITION. TRANSFERRED DISCREPANCY TO DEFERRED MAINTENANCE ITEM 2467 IAW MEL 52-23-01-01.

Part: STIFFENER — CRACKED (LT WING) · airframe 85,990 hrs · 12,400 cycles

LEFT WING T/E RIB BETWEEN OTBD FLAP AND INBD AILERON VERTICAL STIFFINER WORN AND LOWER ATTACH BRACKET CRACKED. 1 EACH CRACK APPROXIMATE LENGTH .750". R & R VERTICAL STIFFINER AND BRACKET IAW SRM 51-40-02, PARA 4 AND 7.

Part: SKIN — CRACKED (RT WING) · airframe 85,990 hrs · 12,400 cycles

RIGHT WING L/E UPPER PANEL COMPOSITE REPAIR ON AFT OTBD CORNER IS CRACKED AND DISBONDED. PERFORMED INTERIM REPAIR IAW ENGINEERING REPAIR ORDER 5730ERO2052.

Part: STIFFENER — CRACKED (LT WING) · airframe 85,990 hrs · 12,400 cycles

STIFFINER BRACKET CRACKED ON LT WING T/E OTBD OF INBD AILERON. 1 EACH CRACK, APPROXIMATE LENGTH .500". R & R STIFFINER BRACKET IAW SRM CH 51-40-02.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN DECK) · airframe 85,711 hrs · 12,340 cycles

FIRE WARNING, MAIN DECK AFT ACTIVATED SEVERAL TIMES DURING FLIGHT. VERIFIED THERE WAS NO FIRE. ALSO, CARGO ZONES 10-16 MAIN DECK STATUS MESSAGES. MAINTENANCE PERFORMED FAULT ISOLATION MANUAL 26-14, TASK NR 804, NO FAULTS NOTED STATUS MESSAGES CLEARED.

Part: DETECTION SYS — MALFUNCTIONED (SMOKE DETECTION) · airframe 85,718 hrs · 12,341 cycles

MAIN DECK FIRE WARNING ACTIVATED MULTIPLE TIMES DURING CRUISE FLIGHT. VERIFIED NO FIRE OR SMOKE OBSERVED ON MAIN DECK. R & R CARD A6 IAW AMM 26-10-01. R & R SMOKE DETECTORS 16B1, 16B2 11A1 AND 15B2 IAW AMM 26-14-01. SYSTEM CHECKS GOOD.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 85,504 hrs · 12,301 cycles

GROUND LEVEL INSPECTION OF UPPER FUSELAGE IAW WC 53-872-01-01, FINDS LIGHTNING STRIKE DAMAGE AT STATION 620 & STRINGER 29 LT. REPAIRED FUSELAGE SKIN AT STATION 620 STRINGER 29 LT IAW SRM 53-00-01-2R REPAIR 14.

Part: SKIN PANEL — BURNED (FUSELAGE) · airframe 85,504 hrs · 12,301 cycles

GROUND LEVEL INSPECTION OF UPPER FUSELAGE IAW WC 530872-01-01 FINDS LIGHTNING STRIKE DAMAGE AT STATION 580 & STRINGER 30 LT. REPAIRED FUSELAGE SKIN AT STATION 580 STRINGER 30 LT IAW SRM53-00-01-2R REPAIR 14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 85,504 hrs · 12,301 cycles

GROUND LEVEL INSPECTION OF UPPER FUSELAGE IAW WC 53-872-01-01 FINDS LIGHTNING STRIKE DAMAGE AT STATION 680 & STRINGER 27 LT. REPAIRED FUSELAGE SKIN AT STATION 680, STRINGER 27 LT IAW SRM 53-00-01-01-2R REPAIR 14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,504 hrs · 12,301 cycles

OPERATIONAL CHECK OF EMER LIGHTING IAW WC 33-050-01-01 UPPER DECK CEILING LIGHTS INOPERATIVE. REPLACED FAULTED CEILING EMER LIGHTS, LAMPS, BETWEEN STATIONS 400 & 760 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: STRIP — DELAMINATED (LT WING) · airframe 85,150 hrs · 12,239 cycles

LEFT WING T/E CONDITION STRIP OTBD OF FUEL JETTISON NOZZLE, WBL 1135 IS DETACHED AT INBD END, AND DISBONDED AT OTBD END, WBL 1169. PERFORMED INTERIM REPAIR OF LT WING T/E LIGHTNING CONDITION STRIP IAW INSTRUCTIONS IN EO 5750ERO1995.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 84,060 hrs · 12,055 cycles

HOT ELECTRICAL ODOR IN THE COCKPIT. PERFORMED VISUAL INSPECTION AT LOWER FORWARD CARGO FANS, NO DEFECTS FOUND. CLEANED INLET FILTERS ON LOWER CARGO FANS 1 AND 2 IAW AMM 21-26-10. OPS CHECKED GOOD. NO ODORS OBSERVED, REF FIM 2100-810.

Part: SKIN — DENTED (FUSELAGE) · airframe 83,515 hrs · 11,940 cycles

LOWER FUSELAGE SKIN DOUBLER AT STATION 720, FOUND DENT WITHIN 1 INCH RT EDGE. LOWER FUSELAGE SKIN REPAIRED IAW SRM 53-00-01 FIGURE 201 REPAIR 1.

Part: SUPPORT — CORRODED (BODY FAIRING) · corrosion level 2 · airframe 83,515 hrs · 11,940 cycles

BODY FAIRING PANEL SUPPORT AT BS 880 BL 18 LT FOUND CORROSION AT EXISTING REPAIR. INSPECTION CARRIED OUT IAW MPD TASK 53-804-01.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 83,515 hrs · 11,940 cycles

DURING ACCOMPLISHMENT OF AD 2003-10-06, SB 747-53A2448, HIGH FREQUENCY EDDY CURRENT. INSPECTION OF THE AFT CARGO DOOR CUT OUT, FOUND CRACK IN THE SKIN OF THE UPPER FWD CORNER. CRACK LENGTH .250 INCHES.

Part: SKIN — CRACKED (RT WING) · airframe 83,515 hrs · 11,940 cycles

LEADING EDGE SKIN OTBD OF OTBD LANDING LIGHT LENS ON RT WING AT ILES 330 FOUND 1.25 INCH CRACK. REPLACED CRACKED WEB IAW SRM 51-40-02.

Part: PANEL — PUNCTURED (MAIN DECK) · airframe 83,515 hrs · 11,940 cycles

MAIN DECK BALL MAT PANEL AT STATION 1860 - 1920 RT OF BL FOUND PUNCTURED. REPAIR CARRIED OUT IAW EO 5330ERO1879.

Part: PANEL — DENTED (MAIN DECK) · airframe 83,515 hrs · 11,940 cycles

MAIN DECK BAL MAT PANEL AT STATION 1780 - 1840 LT OF BL 75 - 98 FOUND DENTED. REPAIRED DAMAGE IAW EO 5330ERO1879.

Part: BEAM — CRACKED (RT WING) · airframe 83,515 hrs · 11,940 cycles

RIGHT LE TO FRONT SPAR CAVITY NOSE BEAM LOWER CHORD AT ILES 697 FOUND 1.5 INCH CRACK. REPAIRED IAW DWG 5730D1877.

Part: OIL SYSTEM — LEAKING (APU) · airframe 83,515 hrs · 11,940 cycles

OIL ODOR IN CABIN & COCKPIT. REMOVED OIL CONTAMINATION FROM AIR CONDITIONING SYS & PNEUMATIC SYS. CAUSE OF PROBLEM FOUND TO BE INTERNAL OIL LEAK FROM APU. R & R APU.

Part: STRUCTURE — MECHANIC ERROR (FUSELAGE) · airframe 83,515 hrs · 11,940 cycles

WHILE ACCOMPLISHING AD 98-07-15 SB 747-53A2396 FOUND SHORT EDGE MARGIN & SHORT PITCH CONDITIONS ON LT & RT SIDES. ACCOMPLISHED DOUBLER INSTALLATION IAW SB 747-53A2396.

Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 83,515 hrs · 11,940 cycles

NUMBER 2 ENG LT COWL AFT CORNER FOUND FASTENER HOLES ELONGATED. REPAIRED COWL IAW EO 5430ERO1878.

Part: PANEL — DENTED (MAIN DECK) · airframe 83,515 hrs · 11,940 cycles

MAIN DECK BAL MAT AT STATION 1860-1920 LEFT OF BUTTLINE 79-98 DENTED ON EDGE OF PANEL NEAR BALL TRANFER UNITS. REPAIR CARRIED OUT PER ASI SOLUTIONS ENGINEERING ORDER 5330ERO1879 APPROVED BY 8110-3 NO. 232-884-14-1879.

Part: PANEL — DEPARTED (RT WING) · airframe 83,461 hrs · 11,922 cycles

UPON LANDING INTO OAIX, THE TOWER NOTIFIED THE FLIGHT CREW THAT A PIECE OF WING WAS FOUND ON THE RUNWAY. POST FLIGHT INSPECTION REVEALED RT WING UPPER PANEL PN 65B11629-30 WAS MISSING.

Part: RELAY — DEFECTIVE (FIRE WARNING) · airframe 83,352 hrs · 11,875 cycles

PRIOR TO DESCENT MAIN DECK FIRE WARNING EICAS MSG DISPLAYED. SYS WAS CURRENTLY DEFERRED. FIRE WARNING DISAPPEARED AT 10000' FOOT ON DESCENT. AFTER FLIGHT FOUND FAULTY RELAY R 5187. REPLACED RELAY SYS, CHECKED GOOD.

Part: DOOR — INOPERATIVE (ZONE 800) · airframe 82,815 hrs · 11,700 cycles

RIGHT UPPER DECK ESCAPE DOOR INOPERATIVE ELECTRICALLY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 82,782 hrs · 11,688 cycles

FOUND EMERGENCY EXIT BATTERY PACKS WITH NO VOLTAGE. REPLACED BATTERY PACKS EMERGENCY EXIT LIGHTS TEST GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 82,454 hrs · 11,584 cycles

ON DAILY SERVICE CHECK, FOUND RT UPPER DECK DOOR EMERGENCY OPENING SYS FAILS TEST USING 6 VOLT BATTERY TEST, TASK 52-023-00-01.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN DECK) · airframe 82,095 hrs · 11,437 cycles

MAIN DECK FORWARD FIRE WARNING ACTIVATED DURING FLIGHT. ON ABOUT 5 SECONDS THEN EXTINGUISHED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 80,928 hrs · 11,138 cycles

RT UPPER DECK DOOR EMERGENCY BATTERY DOES NOT TEST.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 80,180 hrs · 10,951 cycles

RIGHT WING FUEL PANEL FORWARD FIXED PANEL FOUND CRACKED. CRACK LENGTH 1".

Part: SPLICE PLATE — CRACKED (NLG WW BLKHD) · airframe 80,180 hrs · 10,951 cycles

NLG WHEEL WELL BS 400 RT AFT CORNER SKIN SPLICE PLATE HAS 5 CRACKS. CRACK LENGTH .030". REF AD 2010-26-07, S/B 747-53A2305.

Part: DRIP TRAY — CRACKED (BS 460) · airframe 80,180 hrs · 10,951 cycles

MAIN ELECTRICAL CENTER LT OTBD DRIP SHEILD CRACKED, LOCATED AT BS 460. REF AD 2011-16-06, SB 747-25A3588. CRACK LENGTH 2".

Part: BULKHEAD — CRACKED (NLG WW) · airframe 80,180 hrs · 10,951 cycles

NLG WHEEL WELL BS 400 LT AFT CORNER SKIN CHORD FOUND CRACKED. CRACK LENGTH .3". REF AD 2012-26-07, S/B 747-53A2305.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 80,180 hrs · 10,951 cycles

RIGHT WING FUEL PANEL LATCH ANGLE FOUND CRACKED. CRACK LENGTH .5"

Part: SPLICE PLATE — CRACKED (NLG WW BLKHD) · airframe 80,180 hrs · 10,951 cycles

NLG WHEEL WELL BS 400 LT AFT CORNER SKIN SPLICE PLATE FOUND CRACKED. 2 EACH CRACKS, CRACK LENGTH .3", REF AD 2012-26-07, S/B 747-53A2305.

Part: CARGO TRACK — BROKEN (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

AFT CARGO COMPARTMENT AT BS 1910 LT AND RT RETRACTABLE GUIDE RAIL, TWO HOOK PLATES FOUND BROKEN.

Part: RESERVOIR — PRESSURE LOSS (EMERGENCY EXIT) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK RT EMERGENCY EXIT DOOR POWER OPENING RESERVIOR PRESSURE LOW.

Part: GROMMET — BROKEN (ESCAPE REEL) · airframe 80,180 hrs · 10,951 cycles

COCKPIT EMERGENCY DECENT DEVICE BLUE GROMMET FOUND BROKEN.

Part: LIFE RAFT — PRESSURE LOSS (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK LIFE RAFT AT BS 660 LT SIDE FOUND PRESSURE BELOW LIMITS.

Part: BRACKET — CRACKED (ZONE 600) · airframe 80,180 hrs · 10,951 cycles

RIGHT WING LANDING GEAR STRUT DOOR LOWWER SECTION FIXED FAIRING MID BRACKET FOUND CRACKED. CRACK LENGTH 1".

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 80,180 hrs · 10,951 cycles

RT WING NR 7, MOVEABLE FLAP FAIRING OTBD FORWARD ANGLE FOUND CRACKED IN 2 PLACES.

Part: BRACKET — CRACKED (ZONE 600) · airframe 80,180 hrs · 10,951 cycles

RT WING T/E CAVITY AT WING BS 280 BRACKET FOUND CRACKED, CRACK LENGTH .5".

Part: RETAINER — CRACKED (ZONE 500) · airframe 80,180 hrs · 10,951 cycles

LEFT WING STRUT DOOR LOWER SECTION FIXED FAIRING RETAINER FOUND CRACKED. CRACK LENGTH 1".

Part: BEAM — CRACKED (ZONE 400) · airframe 80,180 hrs · 10,951 cycles

NR 2 PYLON OTBD SKIRT FAIRING BEAM L/E CRACKED. 4 CRACKS EXTEND FROM FASTENER HOLE. CRACK LENGTHS .8"

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK BS 1180 RT SIDE TENSION TIE FORWARD CHANNEL CRACKED. CRACK LENGHT .035".

Part: GUIDE — CRACKED (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

FORWARD LOWER CARGO COMPARTMENT STA 580-600 LT SIDE GUIDE FOUND CRACKED. CRACK LENGTH 1".

Part: SKIN — CRACKED (BS 400) · airframe 80,180 hrs · 10,951 cycles

NLG WHEEL WELL BS 400 LT AFT CORNER SKIN PANEL FOUND CRACKED. REF AD 2010-26-07, SB 747-53A2305. CRACK LENGTH 2.5" LONG FASTENER HOLE CRACK .030"

Part: WEB — CRACKED (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

FORWARD CARGO BS 570, RBL 45-50 WEB FOUND CRACKED. CRACK LENGTH .5".

Part: SEAL DEPRESSOR — CRACKED (ZONE 800) · airframe 80,180 hrs · 10,951 cycles

FORWARD LOWER CARGO DOOR SEAL DEPRESSOR FOUND CRACKED. CRACK LENGTH 2".

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

AFT LOWER CARGO COMPARTMENT AT STA 1580, RT OF BUTT LINE 58 ROLLER TRAY FOUND CRACKED, CRACK LENGTH 1".

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

FORWARD CARGO COMPARTMENT STA 570 RT OF BUTT LINE 50" CARGO TRACK FOUND CRACKED. CRACK LENGTH IS 2".

Part: PLATE — CRACKED (ENGINE) · airframe 80,180 hrs · 10,951 cycles

ENGINE FUEL NOZZLE SPLASH PLATE FOUND RADIAL CRACK, CRACK LENGTH .516".

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK STA 1180, RT TENSION TIE AT FRAME WEB FOUND 1 EA HOLE CRACKED. REF AD 2007-23-18 SB 747-53A2507. CRACK HOLE CRACK LENGTH .035"

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK BS 1180 LT TENSION TIE FORWARD CHANNEL FOUND 1 EA CRACK. REF AD 2007-23-18, SB 747-53A2507. CRACK LENGTH .035"

Part: PRESSURE PANEL — CRACKED (ZONE 100) · airframe 80,180 hrs · 10,951 cycles

LT LANDING GEAR WHEEL WELL CANTED PRESSURE DECK CLOSEOUT PANEL FOUND CRACKED. REF AD 2003-01 SB 747-51A2057. CRACK LENGTH 1".

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

BS 2598, FOUND CRACKED.

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 80,180 hrs · 10,951 cycles

UPPERDECK BS 1140 TENSION TIE AT FRAME WEB FOUND 1 EACH HOLE CRACK AND 2ND HOLE CRACK AT FAILSAFE.

Part: BATTERY — DISCHARGED (ESCAPE SLIDE) · airframe 79,326 hrs · 10,720 cycles

RT UPPER DECK EMERGENCY SLIDE-BATTERY TEST INOPERATIVE. (FOUND DURING ROUTINE COMPANY 24/48 HOUR SERVICE CHECK.)