N716CK

Part: DOOR — UNSECURE (ZONE 800) · airframe 105,187 hrs · 18,302 cycles

DOOR FWD OVHD EICAS ON LANDING. SECURED DOOR IAW AMM 52-21-00. ACFT OK FOR SERVICE.

Part: TRANS RECTIFIER — INOPERATIVE (NR 1) · airframe 105,156 hrs · 18,297 cycles

100281155: MULTIPLE ELECTRICAL FAILURES. ACTION TAKEN: T/S & FOUND DC 1 DIST P6 C/B POPPED IAW B747 WDM 24-54-12. REMOVED & REINSTALLED #1 TRU IAW B747-400 AMM 24-32-01. MSG CLEARED, OPS CHECK FAILED. 100281156: #1 TRU FAIL. ACTION TAKEN: REMOVED & REPLACED #1 TRU IAW B747-400 AMM 24-32-01. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE INDICATION (ENGINE) · airframe 104,242 hrs · 18,150 cycles

DOOR FLIGHT DECK OVERHEAD ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGE. OPENED OVERHEAD HATCH. INSPECTED HATCH AND FOUND NO DEFECTS IAW BOEING AMM 52-21-00.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 102,061 hrs · 17,795 cycles

CRACK FOUND IN STIFFENER AT STA 266 AND WL 180 ON OB SIDE OF NWW R/H SIDE WALL PANEL DURING NDT INSPECTION.

Part: STIFFENER — CRACKED (ZONE 800) · airframe 102,061 hrs · 17,795 cycles

POSSIBLE CRACK ON FWD CARGO DOOR, FWD DOORSIDE LIFT LINK MOUNT STIFFNER.

Part: STIFFENER — CRACKED (ZONE 800) · airframe 102,061 hrs · 17,795 cycles

CRACK ON FWD CARGO DOOR, AFT DOORSIDE LIFT LINK MOUNT STIFFNER.

Part: WARNING LIGHT — FALSE INDICATION (DOOR) · airframe 98,640 hrs · 17,249 cycles

COCKPIT EMERGENCY HATCH INDICATION OPEN DURING FLIGHT. PERFORMED INSPECTION/OPERATIONS CHECK IN ACCORDANCE WITH B747-400 AMM 52-21-00 NO DEFECTS NOTED INDICATION NO LONGER PRESENT OPERATIONS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 98,078 hrs · 17,158 cycles

DOOR FLIGHT DECK OVERHEAD ADVISORY MESSAGE. PERFORMED OPERATIONS CHECK IAW B747-400 AMM 52-21-00. MESSAGE CLEARED.

Part: SKIN — DAMAGED (UNKNOWN) · airframe 95,812 hrs · 16,811 cycles

R/H UPPER FUSELAGE BETWEEN STR 11R AND 13R B.S. 2638.0 - 2658.0 SKIN DAMAGE

Part: STRINGER — DAMAGED (UNKNOWN) · airframe 95,812 hrs · 16,811 cycles

DAMAGE STR 12R FROM B.S. 2638.0 TO 2658.0 AT AFT END FLANGE.

Part: FLANGE — CRACKED (UNKNOWN) · airframe 95,812 hrs · 16,811 cycles

CRACKED AFT FLANGE AT B.S. 2638.0 RIB FROM WL-307.0 TO 317.0 REF. TO STR. 12R

Part: WARNING LIGHT — FALSE ACTIVATION (ESCAPE HATCH) · airframe 94,373 hrs · 16,567 cycles

DOOR FLIGHT DECK OVERHEAD UPON LANDING PERFORMED OPERATIONS CHECK OF FLIGHT DECK OVERHEAD CREW ESCAPE DOOR IN ACCORDANCE WITH BOEING 747-400 AMM 52-21-00. ALLCHECKS GOOD

Part: REVEAL — CRACKED (BS 2237 S25L) · airframe 93,855 hrs · 16,491 cycles

CRACK AT L5 DOOR FWD REVEAL AT STA 2237 STR 25L

Part: DOUBLER — CRACKED · airframe 93,855 hrs · 16,491 cycles

CRACK FOUND IN R/H UPPER LOBE DOUBLER RADIUS DETAIL AT STA 2517 - 2518 AND STRINGER 3R

Part: FLOOR SUPPORT — CRACKED (BS 240) · airframe 93,855 hrs · 16,491 cycles

MAIN DECK FLOOR SUPPORT UPPER CORD @ STA 240 WL 199.80 , 30 INCHES TO LT OF BBL-0 IS DAMAGED ( CRACKED )

Part: FLOORBEAM — CORRODED (BS 460 LBL79) · corrosion level 2 · airframe 93,855 hrs · 16,491 cycles

SURFACE CORROSION FOUND ON FLOOR BEAM UPPER CHORD AT STATION 460 LBL79 LEFT SIDE BY  L1 ENTRY

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 93,855 hrs · 16,491 cycles

SHEAR TIE AT STA. 1000, WL 200, LBL 33.99 WAS FOUND TO BE CRACKED.

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 93,855 hrs · 16,491 cycles

SHEAR TIE AT STA 1000, WL 200, RBL 57.50 WAS FOUND TO BE CRACKED.

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 93,855 hrs · 16,491 cycles

SHEAR TIE AT STA. 1000, WL 200, RBL 33.99 WAS FOUND TO BE CRACKED.

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 93,855 hrs · 16,491 cycles

SHEAR TIE AT STA. 1000, WL 200, RBL 75.92 WAS FOUND TO BE CRACKED.

Part: FLOORBEAM — CRACKED (BS 240) · airframe 93,855 hrs · 16,491 cycles

MAIN DECK FLOOR SUPPORT UPPER CORD @ STA 240  WL 199.80 , 20 INCHES TO THE LT OF BBL-0 IS DAMAGED ( CRACKED )

Part: WEB — WORN (LT ELEVATOR) · airframe 93,855 hrs · 16,491 cycles

LH OB ELEVATOR IB CLOSE OUT RIB WORN

Part: FLOORBEAM — CRACKED (BS 240) · airframe 93,855 hrs · 16,491 cycles

MAIN DECK FLOOR SUPPORT UPPER CORD @ STA 240 WL 199.80 , 30 INCHES TO LT OF BBL-0 IS DAMAGED ( CRACKED )

Part: WEB — WORN (RT ELEVATOR) · airframe 93,855 hrs · 16,491 cycles

RH OB ELEVATOR IB CLOSE OUT WEB WORN

Part: PIN — STUCK (ESCAPE HATCH) · airframe 87,746 hrs · 15,486 cycles

FLIGHT DECK UPPER ESCAPE HATCH LATCH PIN GETTING STUCK WHEN HATCH IS OPENED

Part: SEAT TRACK — WORN (BS 1770) · airframe 85,700 hrs · 15,141 cycles

AFT PIT SEAT TRACK APPROXIMATELY STA 1770 LBL 24.75 HAS EVIDENCE OF WEAR.

Part: SEAT TRACK — DAMAGED (BS 1775) · airframe 85,700 hrs · 15,141 cycles

SEAT TRACK HAS EVIDENCE OF DAMAGE AT APPROXIAMTELY BS 1775 RBL 24.75.

Part: FLOORBEAM — CORRODED (BS 2240) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

CORROSION ON MAIN DECK FLOOR BEAM STA 2240 LBL 40 TO 100.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 85,700 hrs · 15,141 cycles

L1 DOOR AFT LOWER STOP PIN FITTING IS CRACKED.

Part: STIFFENER — CRACKED (BS 310) · airframe 85,700 hrs · 15,141 cycles

CRACKS NOTED ON STIFFENER ON NWW TOP AT APPROXIMATELY STA 310 LBL 10.

Part: PANEL — CORRODED (BS 1920) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

BS 1920 AT APPROX LBL 9 UPPER TORQUE BOX PANEL HAS AREA OF POSSIBLE CORROSION.

Part: STIFFENER — CRACKED (BS 310) · airframe 85,700 hrs · 15,141 cycles

CRACK NOTED ON STIFFENER ON TOP OF NWW AT APPROXIMATELY STA 310 RBL 10.

Part: BULKHEAD WEB — CRACKED (BS 1480) · airframe 85,700 hrs · 15,141 cycles

WEB CRACKED AT STA 1480 BULKHEAD LBL 110 WL 150.

Part: SEAT TRACK — CORRODED (BS 1698) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

MAIN DECK SEAT TRACK HAS EVIDENCE OF CORROSION AT STA 1698, BBL 100 LEFT.

Part: SEAT TRACK — CORRODED (BS 1730) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

MAIN DECK SEAT TRACK HAS EVIDENCE OF CORROSION AT STA 1730, BBL 100 LEFT.

Part: FLOORBEAM — CORRODED (BS 980) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

MAIN DECK FLOOR BEAM UPPER CHORD SHOWS EVIDENCE OF CORROSION AT STA 980, BBL 95 LEFT.

Part: SEAT TRACK — CRACKED (BS 990) · airframe 85,700 hrs · 15,141 cycles

CRACKED SEAT TRACK APPX STA 990 LBL 98.

Part: SEAT TRACK — CORRODED (BS 800-820) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

EVIDENCE OF CORROSION ON SEAT TRACK AT STA 800-820 RBL 33.

Part: SEAT TRACK — CORRODED (BS 664) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

MAIN DECK SEAT TRACK AT STA 664, BBL 12 LEFT HAS CORROSION.

Part: SEAT TRACK — CORRODED (BS 776) · corrosion level 2 · airframe 85,700 hrs · 15,141 cycles

MAIN DECK SEAT TRACK AT STA 776, BBL 10 LEFT SHOWS EVIDENCE OF CORROSION.

Part: FITTING — CRACKED (LONGERON) · airframe 85,700 hrs · 15,141 cycles

RIGHT LONGERON EXTENTION FITTING HAS 1/4" LONG CRACK AT BS 1480 WL 150 RBL 110.

Part: SEAT TRACK — WORN (BS 1480) · airframe 85,700 hrs · 15,141 cycles

EVIDENCE OF WEAR ON SEAT TRACK AT NUT CLIP STA 1480 RBL 99.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

CORROSION AT RT HORIZ STAB STA 143.6 AT STR 9 TO 10 ON SKIN UPPER SURFACE.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

EVIDENCE OF CORROSION ON RT HORIZ STAB NEAR BLADE SEAL MATING SURFACE AT STAB STA 143.6 STR 2 TO 3 UPPER SKIN.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

CORROSION AT RT HORIZ STAB STA 143.6 AT STR 7 TO 8 SKIN UPPER SURFACE.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

CORROSION ON RT HORIZ STAB SKIN UPPER SURFACE STAB STA 143.6 AT STR 13.

Part: FUSE PIN — CRACKED (RT MLG) · airframe 78,844 hrs · 14,012 cycles

RT MLG SUPPORT BEAM FUSE PIN HAS CRACK INDICATION AT GREASE HOLE ON INNER PIN FOUND WITH SURFACE HFEC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

MAIN DECK SEAT TRACK HAS CORROSION ON FLANGE STA 1500 LBL 98.58.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT STA 1500, RBL 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

EVIDENCE OF CORROSION ON MAIN DECK SEAT TRACK STA 640 TO 660 RBL 10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT STA 1620, BBL 10 LEFT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,844 hrs · 14,012 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT STA 1620, BBL 5 RIGHT.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 78,844 hrs · 14,012 cycles

LAV SMOKE DETECTOR FAILS OPS CHECK.

Part: SKIN — CORRODED (LT WING) · airframe 95,897 hrs · 23,931 cycles

LT WING LOWER SKIN HAS CORROSION ON UPPER SURFACE AT LES 884. (S)

Part: BRACKET — CORRODED (BS 1350) · corrosion level 2 · airframe 95,897 hrs · 23,931 cycles

CORROSION ON ATTACH ANGLES ON INBOARD AND OUTBOARD SIDE OF BRACKET AT BS 1350, LBL 78, WL 139. (S)

Part: BULKHEAD — CORRODED (BS 1241) · corrosion level 1 · airframe 95,897 hrs · 23,931 cycles

CORROSION ON CANTED BULKHEAD LOWER AFT CORD AT BS 1241, LBL 95. (S)

Part: ANGLE — CORRODED (BS 1446) · corrosion level 2 · airframe 95,897 hrs · 23,931 cycles

RT BODY WHEEL WELL LONGERON BOX ANGLE IS CORRODED AT STA 1446, RBL 120, WL 113. (S)

Part: SKIN — DAMAGED (BS 2030 S34R) · airframe 95,897 hrs · 23,931 cycles

EXTERNAL FUSELAGE SKIN IS DAMAGED AT AFT SIDE OF BULK CARGO DOOR CUTOUT AREA AT STA 2030, STR 34R. (S)

Part: STIFFENER — CORRODED (BS 1366) · airframe 95,897 hrs · 23,931 cycles

CORROSION ON LT OVERWING LONGERON BOX FRAME STIFFENER. (S)

Part: FRAME — CORRODED (BS 1297) · airframe 95,897 hrs · 23,931 cycles

CORROSION ON FRAME ABOVE RT OVERWING LONGERON AT BS 1297, RBL 121, WL 160. (S)

Part: SKIN — DENTED (E/E DOOR) · airframe 95,897 hrs · 23,931 cycles

FWD E&E DOOR HAS SMALL DENT AT L/E ON SKIN. (S)

Part: ATTACH ANGLE — CORRODED (MLG) · airframe 95,897 hrs · 23,931 cycles

CORROSION FOUND ON ATTACH ANGLE OF LANDING GEAR SUPPORT BEAM AT STA 1350, RBL 35. (S)

Part: ANGLE — CORRODED (BS 1379) · airframe 95,897 hrs · 23,931 cycles

INSIDE LONGERON BOX TEE ANGLE AT WL 113, STA 1379, RBL 115 CORRODED. (S)

Part: FRAME — CORRODED (BS 1315) · airframe 95,897 hrs · 23,931 cycles

CORROSION ON DOUBLER ON TOP OF RT OVERWING LONGERON AT BS 1315, RBL 123, WL 158. (S)

Part: SKIN — CORRODED (LT WING) · airframe 95,897 hrs · 23,931 cycles

LT WING SKIN AT WS 993 TO WS 995 HAS CORROSION. (A)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,897 hrs · 23,931 cycles

LT WING LOWER SKIN CORRODED AT APPROX 1300. (A)

Part: BULKHEAD — CHAFED (NR 2 PYLON) · airframe 95,448 hrs · 23,848 cycles

NR 2 PYLON HYDRAULIC PRESSURE LINE FITTING CHAFED ON AFT SIDE OF NAC STA 221.9 BULKHEAD.

Part: WEB — CRACKED (NLG WW) · airframe 95,448 hrs · 23,848 cycles

NOSE WHEEL WELL RT SIDE STA-285 WL-160 WEB CRACKED .75 INCH UNDER BONDED STRAP.

Part: BULKHEAD — GOUGED (NR 4 PYLON) · airframe 95,008 hrs · 23,773 cycles

NR 4 PYLON UPPER FORWARD ENGINE MOUNT BULKHEAD CHORD NAC STA 128.95 HAS A DEEP GOUGE ON INBOARD SIDE JUST AFT OF CHORD BEND RADIUS AT NOSE COWL FORWARD FAIRING LATCH FITTING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 95,008 hrs · 23,773 cycles

FORWARD BILGE SEAT TRACK IS CRACKED BETWEEN STA 540 & 560, RBL 45.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 94,153 hrs · 23,613 cycles

EMERGENCY EXIT SIGN ABOVE UPPER DECK RIGHT ESCAPE DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,801 hrs · 23,544 cycles

EMERGENCY LIGHT ABOVE UPPER DECK EXIT DOOR INOP.

Part: FILTER — CONTAMINATED (EVC) · airframe 93,234 hrs · 23,441 cycles

AT 8000', IDLE THRUST EGT NR 4 AT 874 DEGREES CELSIUS AND N2 AT 43 PERCENT. ALL OTHER INSTRUMENTS NORMAL. ACCOMPLISHED ENGINE STALL IN FLT (ABNORMAL EGT) CHECKLISTS. ATTEMPTED RESTART WITH RAPID RESTART PROCEDURE QRH-69. RESULTED IN DUPLICATE INDICATIONS. ACCOMPLISHED QRH-79, AGAIN. RESTART SECOND ATTEMPT USING QRH-69, SUCCESSFUL. DURING SAME PERIOD, NR 1 ENGINE EXPERIENCED SAME INDICATIONS, PERFORMED QRH-79. DECISION MADE TO NOT ATTEMPT A RESTART. COMPLETED QRH-67. LANDED SAFELY. WINDMILL OIL PRESSURE UP 5 PSI. PERFORMED WINDMILL INSPECTION IAW B747 MM 72-00-00. NO DEFECTS NOTED. PERFORMED LEAK CHECK OF FILTER AND CHIP DETECTORS IAW B747 MM 71-00. NO LEAKS NOTED. PERFORMED FIM PROCEDURES IAW B7

Part: ENGINE — FLAMED OUT (NR 4) · airframe 92,658 hrs · 23,335 cycles

FLT LEVEL 34.0 NR 4 ENG FLAMED OUT, DESCENDED TO F.L 280. RESTARTED ENG - ALL PARAMETERS NORMAL. ENG RESTARTED ON FIRST ATTEMPT. CLIMBED TO FL 340 ENG OPERATES NORMAL. PERFORMED ENG FLAME OUT INSPECTION IAW MM 71-00-42 P-118. PERFORMED ENG WINDMILL INSPECTION IAW MM 72-00-00 P-682R. NO DAMAGE OR DEFECTS FOUND. NR 4 ENGINE OPS CHECKS NORMAL IAW MM 71-00-00 P-235.

Part: LIGHT — INOPERATIVE (BS 405) · airframe 92,013 hrs · 23,205 cycles

UPPER DECK EMERGENCY LIGHT INOP AT UPPER DECK SERVICE DOOR.

Part: SIGN — NO TEST (EMERGENCY EXIT) · airframe 91,662 hrs · 23,140 cycles

FOUND UPPER DECK EXIT SIGN AND SLIDE LIGHT X325 WILL NOT TEST.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 91,634 hrs · 23,135 cycles

NR 1 HYD LOW LIGHT FOR SYS NR 1 ILLUMINATED. NR 1 HYD SYS QTY WAS 2 GALS WHEN ADP TURNED OFF AND ADP DEPRESSURIZED. ON POST FLT, FOUND NR 1 ADP BLOWOUT DOOR OPEN AND SKYDROL LEAK FROM ACCESSORY PANEL. REPLACED NR 1 HYD SYSTEM RETURN LINE IAW AMM 29-11-00.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 91,305 hrs · 23,070 cycles

NR 2 PYLON NAC STA 221.9 FRAME CRACKED AT FWD I/B UPPER CORNER.

Part: BULKHEAD — CHAFED (NR 2 PYLON) · airframe 91,305 hrs · 23,070 cycles

NR 2 PYLON STA NAC 221.9 BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION.

Part: STIFFENER — CRACKED (BS 2658) · airframe 90,915 hrs · 22,997 cycles

BS 2658 BULKHEAD STIFFENER CRACKED AT LBL 30, WL 277.

Part: RIB — CHAFED (RT WING) · airframe 90,915 hrs · 22,997 cycles

RIGHT WING L/E RIB AT FSSI 1022 IS CHAFED.

Part: RIB — CHAFED (RT WING) · airframe 90,915 hrs · 22,997 cycles

RIGHT WING L/E RIB AT FSSI 887 IS CHAFED.

Part: BOLT — LOOSE (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

EXTERNAL FUSELAGE RT SIDE OVERWING FITTING HAS A BOLT LOOSE AT STA 1346, WL 156.

Part: SKIN — CORRODED (BS 2210) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FUSELAGE SKIN HAS CORROSION AROUND LT OUTFLOW VALVE CUTOUT AREA AT STA 2210, STR 43L.

Part: SEAT TRACK — CORRODED (BS 910) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN DECK SEAT TRACK HAS CORROSION AT STA 910, RBL 11.33.

Part: STIFFENER — CORRODED (BS 1480) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

CORROSION ON TOP OF BS 1480 BULKHEAD HORIZONTAL STIFFENER WEB AT LBL 48, WL 118.

Part: FRAME — CRACKED (BS 2080) · airframe 90,915 hrs · 22,997 cycles

BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, RBL 18.

Part: FRAME — CRACKED (BS 2080) · airframe 90,915 hrs · 22,997 cycles

BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, LBL 18.

Part: BULKHEAD — GOUGED (BS 2360) · airframe 90,915 hrs · 22,997 cycles

MAIN CABIN STA 2360 PRESSURE BULKHEAD WEB FORWARD SIDE IS GOUGED AROUND FASTENER ADJACENT TO STR 24R.

Part: SKIN — DAMAGED (BS 2484) · airframe 90,915 hrs · 22,997 cycles

EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 2484, BETWEEN STR 22L & 23L.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 4 PYLON INTERNAL RT SIDE LOWER FRAME IS CRACKED AT NAC STA 236.

Part: BULKHEAD — CORRODED (BS 2360) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN CABIN STA 2360 BULKHEAD LOWER FORWARD CHORD IS CORRODED IN HOLES AT STRINGER END FITTING STR 48L.

Part: FITTING — CORRODED (BS 2360) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FUSELAGE STRINGER END FITTING IS CORRODED AT AFT SIDE OF STA 2360 BULKHEAD, STR 48L.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

EXTERNAL FUSELAGE SKIN HAS CORROSION AT STA 600, ABOVE STR 6R.

Part: FRAME — CRACKED (FRAME) · airframe 90,915 hrs · 22,997 cycles

BULK PIT BS 2140 FUSELAGE FRAME WEB CRACKED AT RBL 18.

Part: DOUBLER — DAMAGED (NR 3 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 3 PYLON I/B EXTERNAL SKIN DOUBLER AT NAC STA 221 ABOVE REAR ENGINE MOUNT HAS DAMAGE.

Part: STIFFENER — CRACKED (NR 4 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 4 PYLON MID SPAR WEB LOWER SIDE STIFFENER CRACKED AT O/B END IN RADIUS AT NAC STA 231.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

BS 2360 BULKHEAD HAS DENTS AT LBL 7.5, WL 347.

Part: STRINGER — CRACKED (HORIZ STAB) · airframe 90,915 hrs · 22,997 cycles

LEFT HORIZONTAL STAB UPPER STR 4 CRACKED AT STAB STA 260.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

BS 2360 BULKHEAD HAS DENTS AT RBL 54, WL 313.

Part: STRINGER — BENT (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FUSELAGE STRINGER IS BENT AT STA 1930, STR 1R.

Part: BULKHEAD — CRACKED (NR 3 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 3 PYLON REPAIR STOP DRILLED 2" VERTICAL CRACK ON THE AFT ENGINE MOUNT BULKHEAD UPPER I/B AFT FLANGE RADIUS.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

AFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.

Part: SKIN — DAMAGED (NR 4 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 4 PYLON I/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED FROM NAC STA 215 TO 236.

Part: SKIN — DAMAGED (NR 1 NACLELLE) · airframe 90,915 hrs · 22,997 cycles

NR 1 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED NAC STA 180 TO 230.

Part: SKIN — DENTED (BS 2600) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE SECTION 48 SKIN HAS A DENT AT BS 2600 JUST AFT AND BELOW TAIL JACKING POINT MOUNT AREA.

Part: SKIN — DAMAGED · airframe 90,915 hrs · 22,997 cycles

NR 4 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED AT NAC STA 190.

Part: BULKHEAD — DENTED (BS 2360) · airframe 90,915 hrs · 22,997 cycles

FOUND BS 2360 BULKHEAD HAS A DENT AT RBL 50, WL 242.5.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FUSELAGE STRINGER END FITTING IS CORRODED AT STA 1480, STR 47R.

Part: SKIN — CORRODED (BS 1715 S21L) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND EXTERNAL FUSELAGE SKIN IS CORRODED AT STA 1715, STR 21L AROUND L4 DOOR CUTOUT AREA.

Part: STIFFENER — CRACKED (NR 4 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 4 PYLON INTERNAL FORWARD BULKHEAD HORIZONTAL STIFFENER IS CRACKED AT NAC STA 180.

Part: FITTING — ELONGATED (BS 2360 S11R) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER END FITTING HAS ELONGATED HOLE AT STA 2360, STR 11R.

Part: FITTING — CORRODED (BS 2360) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 38R.

Part: FITTING — CORRODED (BS 2360) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 48L.

Part: FITTING — CORRODED (BS 2360 S17L) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 17L.

Part: FITTING — CORRODED (BS 2360 S26R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 26R.

Part: FITTING — CORRODED (BS 2360 S42R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 42R.

Part: FITTING — CORRODED (MLG) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND LT WING LANDING GEAR BEAM O/B END FITTING HAS CRACKS AND CORROSION INDICATIONS.

Part: CHANNEL — CRACKED (BS 760) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK BS 760 TENSION TIE AFT CHANNEL CRACKED AT LT SIDE UPPER RADIUS.

Part: SKIN — DAMAGED (NR 3 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 3 PYLON SKIN HAS SEVERAL AREAS OF DAMAGE FROM NAC STA 180 TO 236.

Part: FLOORBEAM — CORRODED (BS 400) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FLOORBEAM UPPER CHORD IS CORRODED AT STA 400, LBL 16 TO 53.

Part: SKIN — CORRODED (WS 360LT) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND LT WING UPPER SKIN BULGING AND RIVETS PULLED ABOVE FRONT SPAR AT WS 360.

Part: FRAME — CRACKED (BS 980 S10L) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FUSELAGE FRAME CRACKED AT WIRE STANDOFF NEAR STR 10L.

Part: FRAME — CRACKED (BS 2100) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME WEB CRACKED AT CUTOUT AT BS 2100, RBL18.

Part: SKIN — CORRODED (BS 1241) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND CORROSION ON INTERIOR OF FUSELAGE SKIN AT BS 1241, BELOW STR 11L. REPAIRED SKIN IAW B747 SRM 53-30-03 FIG 47.

Part: SPAR — CHAFED (NR 1 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 1 PYLON HAS NUMEROUS DINGS AND CHAFE AREAS ON MIDSPAR WEB AT NAC STA 221 TO 199.

Part: STRINGER — CORRODED (BS 1740 S47R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND CORROSION ON O/B FLANGE OF STR 47R FWD OF BS 1740.

Part: FLOORBEAM — CRACKED (BS 480) · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK FLOORBEAM UPPER CHORD CRACKED AT BS 480, RBL 62.

Part: BULKHEAD — WORN (NR 1 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 1 PYLON NAC STA 221 BULKHEAD WORN AROUND HYDRAULIC FITTING.

Part: FLOORBEAM — MISDRILLED (BS 640) · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK FLOORBEAM HAS DOUBLE DRILLED HOLE AT BS 640, LBL46.

Part: STRINGER CLIP — CORRODED (BS 600 S41R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND STRINGER CLIP CORRODED AT BS 600, STR 41R.

Part: FLOORBEAM — CRACKED (BS 2220 S26L) · airframe 90,915 hrs · 22,997 cycles

MAIN DECK FUSELAGE FRAME TO FLOORBEAM ATTACH ANGLE CRACKED AT BS 2220, STR 26L.

Part: FRAME — BENT (BS 1880 S12R) · airframe 90,915 hrs · 22,997 cycles

FUSELAGE FRAME INNER FLANGE BENT AT BS 1880, STR 12R. FRAME REPAIRED IAW B747 SRM 51-40-03 FIG 1.

Part: FITTING — CORRODED (RT WING MLG) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

RT WING LANDING GEAR BEAM O/B END FITTING HAS CRACK AND CORROSION INDICATIONS.

Part: FRAME — DAMAGED (BS 2220 S26L) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME DAMAGED AT BS 2220, STR26L. REPAIRED FRAME IAW B747 SRM 51-40-03 FIG 1.

Part: FRAME — BENT (BS 1840 S14R) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME INNER FLANGE BENT AT BS 1840, STR14R. REPAIRED FRAME IAW B747 SRM 51-40-03 FIG 1.

Part: FLOORBEAM — CORRODED (BS 600) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK FLOORBEAM AT BS 600 UPPER CHORD CORRODED RBL 3 TO LBL 63.

Part: SEAT TRACK — CORRODED (BS 680-700) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

UPPER DECK SEAT TRACK AT RBL 65.31 CORRODED BS 680 TO BS 700.

Part: FLOORBEAM — CORRODED (BS 540) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK FLOORBEAM AT BS 540 CORRODED BL 0.0 TO LBL41.

Part: SEAT TRACK — DAMAGED (FUSLEAGE) · airframe 90,915 hrs · 22,997 cycles

F/E'S INBOARD SEAT TRACK HAS ELONGATED LOCK HOLES.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

PILOT'S FORWARD INBOARD SEAT TRACK WEB CRACKED.

Part: STRINGER — CRACKED (BS 1260 S10R) · airframe 90,915 hrs · 22,997 cycles

FOUND STR 10R CRACKED AT BS 1230.

Part: FRAME — DAMAGED (BS 1740) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME IS DAMAGED AT STA 1740, BETWEEN STR 13R AND 14R.

Part: FLOORBEAM — DAMAGED (BS 480) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FLOORBEAM WEB DAMAGED AT BS 480, LBL20 TO LBL 90. FLOORBEAM REPAIRED IAW B747 SRM 53-10-07 FIG 18.

Part: FLOORBEAM — CORRODED (BS 460) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK FLOORBEAM FRAME CORRODED AT BS 460, RBL 85.

Part: STRINGER — CRACKED (BS 2055 S15L) · airframe 90,915 hrs · 22,997 cycles

FOUND STR15L CRACKED AT BS 2055.

Part: SKIN — BULGED (BS 530-540) · airframe 90,915 hrs · 22,997 cycles

FOUND EXTERNAL FUSELAGE SKIN IS BULGING AT STA 530 TO 540, STR 40R.

Part: SHEAR TIE — CRACKED (BS 2160) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 2160 I/B OF STR42L. REPAIRED SHEAR TIE IAW B747 SRM 53-10-04 FIG 41.

Part: FLOORBEAM — CORRODED (BS 520) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FLOORBEAM SPLICE CORRODED AT BS 520, LBL63.

Part: FRAME — CORRODED (BS 800) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FORWARD BILGE FUSELAGE FRAME UPPER FLANGE IS CORRODED AT STA 800, LBL 12.

Part: SEAT TRACK — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK SEAT TRACK CORRODED AT LBL 12 BETWEEN BS 1460 AND 1480.

Part: FLOORBEAM — DAMAGED (BS 960) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FLOORBEAM UPPER CAP HAS HOLE DAMAGE AT BS 960, LBL 48.5.

Part: FRAME — CRACKED (BS 540 S22-23L) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME IS CRACKED AT STA 540, BETWEEN STR 22L AND 23L.

Part: DOUBLER — DAMAGED (BS 1810) · airframe 90,915 hrs · 22,997 cycles

FOUND EXTERNAL FUSELAGE AFT CARGO DOOR LOWER FORWARD CORNER DOUBLER IS DAMAGED AT STA 1810.

Part: STRINGER — CRACKED (BS 1845 S14R) · airframe 90,915 hrs · 22,997 cycles

FOUND STR 14R CRACKED AT BS 1845.

Part: FRAME — CRACKED (BS 2060) · airframe 90,915 hrs · 22,997 cycles

FUSELAGE FRAME IS CRACKED AT STA 2060, STR 29L.

Part: FRAME — CRACKED (BS 1320 S9L) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME IS CRACKED AT STA 1320, STR 9L.

Part: ATTACH ANGLE — CRACKED (BS 460) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FUSELAGE FRAME TO SILL FRAME ATTACH ANGLE IS CRACKED AT STA 460, WL 280 ABOVE R-1 DOOR.

Part: FRAME — CRACKED (BS 1335 S9L) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME IS CRACKED AT STA 1335, STR 9L.

Part: STIFFENER — CRACKED (BS 410) · airframe 90,915 hrs · 22,997 cycles

E/E COMPARTMENT (BILGE AREA) FUSELAGE FRAME VERTICAL STIFFENER IS CRACKED AT STA 410, LBL 12.

Part: SHEAR TIE — CRACKED (BS 960 S23-24R) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 960 BETWEEN STR 23R AND STR 24R.

Part: SKIN — DAMAGED (BS 1770) · airframe 90,915 hrs · 22,997 cycles

FOUND EXTERNAL FUSELAGE SKIN LAP SEAM IS DAMAGED AT STA 1770, STR 34R.

Part: SPAR — CRACKED (NR 3 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 3 PYLON LOWER SPAR WEB CRACKED AT OUTBOARD NAC STA 229. REPAIRED WEB IAW B747 SRM 54-10-03 FIG 23.

Part: SKIN — CORRODED (BS 2360 S23-24L) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

EXTERNAL FUSELAGE SKIN BUTTSPLICE IS CORRODED AT STA 2360, BETWEEN STR 23L AND 24L.

Part: SPAR — CRACKED (NR 3 PYLON) · airframe 90,915 hrs · 22,997 cycles

NR 3 PYLON HORIZONTAL SPAR WEB CRACKED AT NAC STA 234. REPAIRED WEB IAW B747 SRM 54-10-03 FIG 23.

Part: SKIN — CORRODED (BS 1975) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN CABIN FUSELAGE SKIN IS CORRODED AT STA 1975, RT SIDE WINDOW BELT AREA.

Part: STRINGER CLIP — BENT (BS 1880) · airframe 90,915 hrs · 22,997 cycles

FOUND STRINGER CLIP BENT AT BS 1880, STR 12R.

Part: STRINGER — CORRODED (BS 2160 S50R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

CORROSION ON STR 50R AT BS 2160.

Part: WEB — CORRODED (BS 1680-1700) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

AFT PIT BS 1680 TO 1700 TORQUE BOX UPPER WEB CORRODED AT RBL 10.

Part: STRINGER — GOUGED (BS 340) · airframe 90,915 hrs · 22,997 cycles

FUSELAGE STRINGER IS GOUGED AT STA 340, STR 6L.

Part: SKIN — DAMAGED (BS 2742) · airframe 90,915 hrs · 22,997 cycles

EXTERNAL EMPENNAGE SKIN DOUBLER DAMAGED AT BS 2742, WL 272. REPAIRED SKIN IAW B747 SRM 53-30-03 FIG 1A.

Part: FRAME — CORRODED (BS 900) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FORWARD PIT FUSELAGE FRAME UPPER FLANGE CORRODED AT BS 900, LBL 58.

Part: SKIN — CORRODED (BS 1866-1868) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

CORROSION ON FUSELAGE LAP SEAM AT STR 46R BETWEEN BS 1866 AND 1868.

Part: STRINGER — CORRODED (BS 2160 S51L) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

CORROSION ON STR 51L AT BS 2160.

Part: SEAT TRACK — CORRODED (BS 480-720) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

UPPER DECK SEAT TRACK CORRODED AT LBL 46.65 BETWEEN BS 480 AND 720.

Part: FLOORBEAM — CORRODED (BS 900) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FWD PIT FLOORBEAM CORRODED AT BS 900, LBL 50 TO LBL 60.

Part: FRAME — CORRODED (BS 2200 S42R) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

CORROSION ON FUSELAGE FRAME LOWER CHORD AT BS 2200 ABOVE STR 42R. REPAIRED CHORD IAW B747 SRM 51-40-04.

Part: STRINGER CLIP — DAMAGED (BS 1600 S39R) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER CLIP IS DAMAGED AT STA 1600, STR 39R. CLIP REPLACED IAW B747 SRM 51-30-02.

Part: STIFFENER — BENT (BS 1480) · airframe 90,915 hrs · 22,997 cycles

AFT BILGE VERTICAL STIFFENER ON AFT SIDE OF BS 1480 BULKHEAD IS BENT AT RBL 38, WL 132.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FORWARD BILGE FUSELAGE FRAME UPPER FLANGE CORRODED AT BS 860, LBL 32. FRAME REPAIRED IAW B747 SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

UPPER DECK SEAT TRACK CORRODED AT LBL 29.99, BS 540 TO 740. SEAT TRACK REPAIRED IAW B747 SRM 53-10-01 FIG 1.

Part: SEAT TRACK — CORRODED (BS 480-740) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND UPPER DECK SEAT TRACK IS CORRODED AT STA 480 TO 740, LBL 65.31.

Part: SHEAR TIE — CORRODED (BS 1700 S50-51L) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME SHEAR TIE IS CORRODED AT STA 1700, BETWEEN STR 50L AND 51L. REPAIRED IAW B747 SRM 53-10-04, FIG 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN DECK SEAT TRACK CORRODED AT LBL 33, BS 460 TO 500. REPLACED SEAT TRACK FROM BS 460 TO 510 AT ORIGINAL SPLICES IAW B747 SRM 51-30-05 AND 51-30-02.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

MAIN DECK FLOORBEAM WEB DAMAGED AT BS 500, RBL 78. REPAIRED WEB IAW B747 SRM 53-10-07 FIG 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FWD CARGO PIT FLOORBEAM UPPER CHORD CORRODED AT BS 900, LBL 50 TO LBL 60.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN DECK FLOORBEAM CORRODED AT BS 480 LBL 36 TO LBL 93.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN DECK SEAT TRACK STRAP CORRODED AT BS 517, RBL 33. REPLACED STRAP IAW B747 SRM 53-10-05 FIG 33.

Part: CLIP — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

UPPER DECK CREW DOOR LOWER SUPPORT RAIL CLIP DAMAGED AT BS 440, STR 13R. REPLACED CLIP IAW B747 SRM 51-30-05 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

MAIN DECK SEAT TRACK HAS CORROSION BS 864, LBL 76. REPLACED SEAT TRACK AT LBL 76 FROM BS 830 TO 870 AT EXISTING SPLICES IAW B747 SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1900) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK SEAT TRACK HAS CORROSION AT BS 1900, LBL12. REPLACED SEAT TRACK AT LBL 12 BETWEEN BS 1890 AND 1950 AT ORIGINAL SPLICES IAW B747 SRM 51-30-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK SEAT TRACK SPLICE AT BS 870, LBL76 HAS AREA OF CORROSION. REPLACED SPLICE IAW B747 SRM 51-30-05 AND 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 460, LBL34, STR 44L. REPAIRED SHEAR TIE IAW B747 SRM 53-10-04 FIG 4.

Part: STIFFENER — CRACKED (BS 280-300) · airframe 90,915 hrs · 22,997 cycles

NOSE WHEEL WELL UPPER SKIN STIFFENER CRACKED AT LBL10 BETWEEN BS 280 AND 300. STIFFENER REPLACED IAW B747 SRM 51-30-05 AND 51-30-02.

Part: SHEAR TIE — CRACKED (BS 560 S38-39L) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE SHEAR TIE CRACKED AT BS 560 BETWEEN STR 38L AND STR 39L. SHEAR TIE REPAIRED IAW B747 SRM 53-10-04 FIG 3.

Part: SKIN — DENTED (BS 560 S39L) · airframe 90,915 hrs · 22,997 cycles

FOUND DENT IN FUSELAGE SKIN AT BS 560 STR 39L. DENT REPAIRED IAW B747 SRM 53-30-03 FIG 17.

Part: SKIN — DENTED (BS 534 S43-44R) · airframe 90,915 hrs · 22,997 cycles

FOUND DENT IN FUSELAGE SKIN APPROX BS 534 BETWEEN STR 43R AND STR 44R. SKIN REPAIRED IAW B747 SRM 53-30-03 FIG 17.

Part: STIFFENER — CRACKED (BS 1500 S39R) · airframe 90,915 hrs · 22,997 cycles

FOUND VERTICAL STIFFENER ON BS 1500 FUSELAGE FRAME FWD SIDE IS CRACKED AT TOP ABOVE STR 39R. STIFFENER REPLACED IAW B747 SRM 51-20-01 AND SRM 51-30-02.

Part: STRINGER — CORRODED (BS 760-820) · corrosion level 2 · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER 45L CORRODED AT BS 780. STRINGER REPAIRED IAW B747 SRM 53-10-03.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 90,915 hrs · 22,997 cycles

FOUND MAIN DECK FLOORBEAM WEB DAMAGED AT BS 280 LBL10. WEB REPAIRED IAW B747 SRM 51-40-02 FIG 1.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FOUND BS 1680 SHEAR TIE BETWEEN STR 46R AND STR 47R DAMAGED. REPAIRED SHEAR TIE IAW B747 SRM 53-10-04 FIG 3.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER CLIP DAMAGED AT BS 1600 ABOVE STR 41R. CLIP REPLACED IAW B747 SRM 51-30-05.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FOUND BS 1680 SHEAR TIE BETWEEN STR 46R AND STR 47R DAMAGED. REPAIRED SHEAR TIE IAW B747 SRM 53-10-04 FIG 3.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 90,915 hrs · 22,997 cycles

FOUND FUSELAGE STRINGER CLIP DAMAGED AT BS 1600 ABOVE STR 41R. CLIP REPLACED IAW B747 SRM 51-30-05.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,886 hrs · 22,991 cycles

UPPER DECK EMERGENCY LIGHT UNDER MEDALLION WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY UNDER MEDALLION. OPS CHECK GOOD IAW BOEING 747 M/M 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,886 hrs · 22,991 cycles

UPPER DECK EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY ON UPPER DECK. OPS CHECK GOOD IAW BOEING 747 M/M 33-51-07.

Part: BATTERY — DISCHARGED · airframe 89,573 hrs · 22,734 cycles

AFTER T/O, SMELL OF SMOKE IN COCKPIT. LOSS OF BATTERY VOLTAGE - BATTERY OVERHEAT. RETURNED TO HNL. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY CHARGER IAW B747 MM 24-30-00. OPS CHECK GOOD.

Part: SMOKE — DETECTED (COCKPIT) · airframe 89,563 hrs · 22,731 cycles

AFTER T/O SMELLED SMOKE BACK SIDE OF P6 PANEL. NO VISUAL - CLEARED ON CLIMB OUT. FOUND AND CLEANED LINT AND DUST. AIRCRAFT REMAINED POWER FOR SEVERAL HOURS ON GROUND. NO SMOKE SMELL NOTICED.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 87,497 hrs · 22,325 cycles

NR 2 ENGINE COMPRESSOR STALLED IN FLT AT FL26,600 FT. EPR DECREASED AND EGT INCREASED. RETARDED THRUST LEVER, EGT DECREASED, PEAK EGT 895 DEGREES. PERFORMED ENGINE STALL INFLT CHECK. PERFORMED RAPID RESTART CHECK. N1 RPM DID NOT INCREASE AFTER RESTART WITH THRUST LEVER. PERFORMED IN FLT ENG. FAILURE/SHUTDOWN QRH-67.