N853FT

Part: AILERON — DELAMINATED (R/H O/B WING) · airframe 83,805 hrs · 21,554 cycles

R/H OUTBD AILERON TOP CENTER HONEYCOMB PANEL TOP SKIN DELAMINATED 5' FROM I/B END, APPROX. 15" DIA. REMOVED & REPLACED R/H OUTBD AILERON PER MM 27-11-02

Part: FASTENER — MISSING (NR 3 PYLON) · airframe 81,152 hrs · 20,940 cycles

NR 3 ENG STRUT TO DIAGONAL BRACE ATTACH FITTING ON FORWARD SIDE, ONE FASTENER MISSING AND SOME FOUND LOOSE. DETAILED VISUAL INSPECTION CARRIED OUT AND MISSING AND LOOSE FASTENERS REPLACED. NDT PERFORMED AND CONFIRMED NO CRACKS PER BOEING SB 747-54-2186.

Part: FITTING — CRACKED (TE FLAPS) · airframe 80,935 hrs · 20,888 cycles

ON TAKEOFF AT CTS, ACFT HAD STRONG VIBRATION IN AIRFRAME UNTIL FLAPS REACHED FLAPS ONE POSITION. PERFORMED COMPLETE INSPECTION OF AIR WINGS TAIL AND FUSELAGE. FOUND CRACKED FITTING LT FORE FLAP ATTACH 11B. ALSO, FOUND LT FORE AND MID FLAP SEAL DAMAGED. REPLACED FITTING (P/N 654U6Q75-103).

Part: FLANGE — BROKEN (NR 2 ENGINE)

NR 2 ENG R FLANGE CRACKED AT 10 O'CLOCK POSITION. CRACKED WELDED CKD WITH FLOURESCENT LIGHT OK PER SRM 72-53-11.

Part: FLANGE — CRACKED (NR 3 ENGINE)

ENG NR 3 R AND S FLANGES RADIAL CRACKS. CRACK WELDED AND CK W FLOURESCENT LIGHT OK. REPAIRED PER MM 42-53-01..

Part: KEEL BEAM — CORRODED (BS 987)

AT BS 987 BOTTOM CENTER KEEL BEAM PANEL FOUND SURFACE CORROSION (PANEL 191GG). LEVEL 1 CORROSION REMOVED PER SRM 51-10-02.

Part: SKIN — DENTED (HORIZ STAB)

LEFT HORIZ STAB L/E SKIN DENT 4 LOCATIONS STAB STA L/E 165, 235, 3335 AND 385. SMOOTH OUT DENTS AND NDT CKD OK PER NDT DT-6, MM 51-00-00 SRM 51-10-01.

Part: FLANGE — CRACKED (NR 2 ENGINE)

NR 2 ENG S FLANGE CRACKED AT 2 O'CLOCK POSITION. CRACKED WELDED AND CKD WITH FLOURSCENT LIGHT OK PER MM 72-53-11.

Part: STRUCTURE — DAMAGED (AIRFRAME)

INBOUND TO RMS AIRCRAFT FLEW THRU INBEDDED THUNDERSTORMS AND HAIL CAUSING DAMAGE TO LEADING EDGES, L1 WINDSHIELD, RADOME AND NAV LIGHTS. PERFORMED BIRD STRIKE/HAIL CONDITION INSPECTION PER MM 5-51-13. REPLACED L1 WINDOW PER MM 56-11-01. REPLACED NAV LIGHT LENSES PER MM 33-43-03. REPLACED RADOME PER MM 53-52-01. REPAIRED DAMAGED LEADING EDGES ON HORIZ STAB PER POLAR MA 5510-07:01.

Part: HINGE — CORROSION (PASSENGER DOOR)

LEVEL 1 CORROSION FOUND ON HINGE AT NR 3 MAIN ENTRY DOOR. REMOVED CORROSION PER SRM 51-10-02.

Part: ANGLE — CRACKED (BS 1520)

FOUND ANGLE SUPPORT FITTING AT BS 1520 BL ZERO CRACKED. REPLACED ANGLE PER SRM 51-10-02 AND 51-30-02.

Part: SKIN — LOOSE (BS 2685)

FOUND FUSELAGE EXTERIOR SKIN AT BS 2685 LEFT ELEVATOR AREA LOOSE RIVETS. REPLACED RIVETS PER SRM 51-30-02.

Part: SKIN — CORRODED (BS 1960)

LEVEL 1 CORROSION FOUND ON EXTERION SKIN LOCATED AT BS 1960 RIGHT STRING 46. CORROSION REMOVED PER SRM 51-10-02.

Part: SKIN — DELAMINATED (AIR COND DOOR)

AIR CONDITIONING BAY DOOR 191E ON LEFT SIDE FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: PANEL — DELAMINATED (LEFT WING)

TRAILING EDGE WING UPPER SKIN PANEL FOUND DELAMINATED ON LEFT WING. REPAIRED PER SRM 51-40-09.

Part: SKIN — CORRODED (BS 1620)

LEVEL 1 CORROSION FOUND ON FUSELAGE EXTERIOR SKIN AT BS 15620 STR 47 LEFT TO RIGHT. CORROSION REMOVED PER SRM 51-10-02.

Part: FAIRING — DELAMINATED (RIGHT WING)

FOUND DELAMINATED CRACK ON RT WING AFT SIDE FAIRING AT BL 1120. REPAIRED CORROSION PER SRM 51-40-09.

Part: PANEL — DELAMINATED (WS 340)

FOUND DELAMINATED PANEL ON UPPER RIGHT WING AT WS 340. REPAIRED PER SRM 51-40-09.

Part: SKIN — DELAMINATED (NR 5 SPOILER)

FOUND NR 5 SPOILER SKIN DELAMINATED. REPAIRED PER SRM 51-40-05.

Part: FAIRING — DELAMINATED (NR 6 TE FLAP)

NR 6 TRAILING EDGE FLAP FAIRING FOUND HOLE. REPAIRED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (RIGHT WING)

RIGHT WING AFT SIDE FAIRING AT BL1120 FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: SKIN — CORRODED (BS 1580)

LEVEL 1 CORROSION FOUND ON EXTERIOR SKIN AT BS 1580 STR 47 LEFT TO RIGHT. REPAIRED CORROSION PER SRM 51-10-02.

Part: FAIRING — DAMAGED (NR 5 TE FLAP)

NR 5 TRAILING EDGE FLAP FAIRING FOUND HOLE AT BL235. REPAIRED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 8 TE FLAP)

FOUND NR 8 TRAILING EDGE FLAP FAIRING FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: FAIRING — DELAMINATED (NR 6 TE FLAP)

FOUND NR 6 TRAILING EDGE FLAP FAIRING DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: SKIN — PUNCTURE (BS 1960)

ON WALKAROUND, FOUND SKIN PUNCTURED 1 INCH HOLE AT ST 1960 FWD OF LOWER AFT CARGO DOOR SWITCH. REPAIRED PER SRM 53-30-03 PG 2J, TEMP REPAIR. PERMANENT REPAIR SCHEDULED NEXT C-CHECK PER COI ITEM 853-041.

Part: LINE — LOOSE (NR 4 PYLON)

NR 4 HYDRAULIC SYSTEM DROPPED BY 2 GALLONS DURING FIRST HOUR OF FLIGHT. DEPRESSURIZED SYSTEM AND LOSS STOPPED. FOUND HYD LINE IN PYLON AFT OF FIREWALL LOOSE. RESECURED AND TIGHTENED LINE. OPS AND LEAK CHECK GOOD PER MM 29-00-00 AND SERVICED FULL PER MM 12-00-00.

Part: ANGLE — CRACKED (NR 4 PYLON)

#4 PYLON AFT BULKHEAD FWD SIDE HAS AN ANGLE STOP DRILLED AND CRACK APPEARS TO BE GOING BEYOND STOP DRILL. REPAIRED PER SRM 51-14-01 AND 51-30-02.

Part: PANEL — DELAMINATED (FUSELAGE)

PANEL # 334GB HAS SMALL DELAMINATION. FABRICATED AND BONDED NEW SKINS IAW SRM 51-40-06.

Part: SKIN — GOUGED (RUDDER)

RUDDER LOWER LEFT GOUGE IN SKIN MID POINT. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 51-40-09.

Part: CANOE — DAMAGED (NR 7 FLAP TRACK)

#7 FLAP TRACK CANOE HAS U SHAPED HOLE. REPAIRED DAMAGED AREA PER SRM 51-40-15.

Part: ACTUATOR — INOPERATIVE (NR 4 ENGINE)

NR 4 ENG FAILED IN CRUISE. TRIED TO RELIGHT 2 TIMES AT 2 DIFFERENT ALTITUDES AND WOULD NOT RELIGHT. REMOVED ENGINE FUEL CONDITION MOTOR ACTUATOR PER MM 76-11-04 PG 401 TO 404. GROUND CHECK OK STATICALLY. INSPECTED FUEL PUMP FILTER, NO CONTAMINATION FOUND. LEAK CHECK OK. FIREWALL C/PS CLEANED AND CHECKED. OP CHECK FUEL CONDITION MOTOR ACTUATOR GOOD.

Part: CONNECTOR — CONTAMINATED (NR 4 ENGINE)

NR 4 ENG START VALVE OPEN LIGHT ON. RETURNED TO RAMP. FAULT T/S CARRIED OUT. SHAKE CHECK OF WIRING ON ENG STRUT PLUGS AND ENG DISCONNECT PLUGS UNABLE TO REPRODUCE DEFECT. ENG DISCONNECT PLUG D0014P DISCONNECTED AND FOUND STRUT CONNECTOR D0044J BADLY CONTAMINATED AND INSULATION ROTTEN. CHANGED CONNECTOR PER WDM 20-11-11 AND SYSTEM CHECKED OK ON ENG RUN.

Part: START VALVE — MALFUNCTIONED (NR 4 ENGINE)

ON INITIATING DESCENT, NR 4 ENG START VALVE LIGHT ILLUMINATED STEADY. WHEN HIGH STAGE LIGHT WAS OUT, START VALVE LIGHT WOULD EXTINGUISH. VALVE LIGHT ON STEADY ACCOMPANIED BY HIGH STAGE LIGHT ON. ENG SHUT DOWN ACCOMPLISHED. INSPECTED ALL COMPONENTS, NO DAMAGE TO STARTER OR VALVE. LOCKED OUT THE NR 4 ENG HI-STAGE VALVE PER DDPG 36-01-1.

Part: WINDOW — CRAZED (RT UPPER DECK)

FOUND MOST AFT WINDOW ON RT SIDE UPPER DECK CRAZED. REMOVED AND REPLACED PER MM 56-21-00.

Part: PANEL — MISSING (RT WING)

DURING CRUISE, MARKED AIRFRAME VIBRATION. REPLACED RT INBD FOREFLAP AND REPAIRED RT INBD MIDFLAP AND RT STABILIZER L/E. ALSO, REPLACED RT FLYING PANEL.

Part: ANGLE — CRACKED (AC DOOR)

FWD AIR COND ACCESS PANEL 191A FWD HINGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02.

Part: HINGE — CORRODED (BS 1020)

LEVEL 1 CORROSION AND BARE METAL AND FRETTING FOUND ON MOUNTING FLANGES FOR AIR CONDITIONING HINGE PANELS IN SEVERAL PLACES LT AND RT SIDES. REMOVED SURFACE CORROSION TREATED AND PRIMED IAW SRM 51-10-02.

Part: KEEL BEAM — CORRODED (BS 1239-1484)

INNER SURFACE AT KEEL BEAM STA 1239 TO 1484 SEEN THRU LIGHTENING HOLE BUBBLING AND FLAKING PAINT. CLEANED AREA AND PRIMED BARE METAL PER BOEING SRM 51-10-02.

Part: SKIN — PUNCTURED (RT MLG DOOR)

RT WING GEAR UPPER STRUT DOOR INNER SKIN PUNCTURED ALONG AFT EDGE OF PLACARD. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING SRM 52-80-02.

Part: SKIN — CORRODED (LT MLG DOOR)

LBG O/B DOOR INNER SKIN BULGED AT AFT EDGE. REMOVED CORROSION AND REPAIRED PER SRM 51-10-03 FABRICATED DOUBLER PER SRM 52-80-02.

Part: HINGE — CORRODED (ACM DOOR)

NR 1 ACM DOOR PANEL 191A HINGES HAVE LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-10-06. TREATED AND PRIMED IAW SRM 51-10-02.

Part: ANTENNA — CORRODED (BS 600)

LEVEL 1 CORROSION FOUND ON FWD CENTER RADIO ALT ANTENNA. CLEANED IAW STANDARD PRACTICES, OPS CHECK GOOD IAW MM 34-37-00.

Part: ROD — BROKEN (CARGO DOOR)

AFT HOOK PUSH PULL ROD BROKE WHEN OPERATING MAIN DECK CARGO DOOR. REPLACED MAIN DECK CARGO DOOR AFT HOOK PUSH PULL ROD ASSY. DUE TO HIGH NUMBER OF FAILURES, TROUBLESHOOTING FOUND DOOR RESTRAINT LOCK SOLENOID SWITCH INOP (P/N 60B00311-5). REPLACED PER MM 52-32-11.

Part: ROD — BROKEN (CARGO DOOR)

MAIN DECK SIDE CARGO DOOR AFT HOOK ACTUATING ROD SHEARED DURING OPERATION. INSTALLED MAIN DECK CARGO DOOR AFT HOOK PUSH PULL ROD PER MM 52-32-11.

Part: CONNECTING ROD — BROKEN (CARGO DOOR)

BROKEN CONNECTOR ROD FOR MAIN DECK CARGO DOOR AFT HOOK. REPLACED ROD PER M/M 52-32-11, OPERATIONAL CHECK GOOD.

Part: CSD SEAL — LEAKING (NR 4 ENGINE)

NR 4 ENGINE OIL QUANTITY STEADILY DECREASED TO ZERO FROM FULL, APPROXIMATELY 1 HOUR AFTER DEPARTURE. ENGINE SHUT DOWN WHEN OIL PRESSURE LIGHT ILLUMINATED. REPLACED NR 4 ENGINE CSD DRIVE SEAL, SEAL RETAINER O-RING, CSD INPUT AND OUTPUT SHAFT PACKING PER BOEING M/M 24-11-01 AND 72-61-07. A 5 MINUTE ENGINE RUN AT IDLE AND SLIGHTLY ABOVE SHOWS NO FURTHER LEAKAGE FROM CSD DRIVE PAD DRAIN.

Part: FITTING — DAMAGED (NR 4 PYLON)

NR 4 PYLON FORWARD DIAGONAL BRACE FITTING HAS 3 EACH DRILL STARTS. REPAIRED PER HAECO RS R54-33472.

Part: CONNECTOR — MISWIRED (FUEL SOV)

APPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF THE FIRE SWITCHES ON THE OVERHEAD PANEL. INVESTIGATION CONFIRMED THAT WIRES W629-1Q1221-20 AND 1Q1223-20 WERE SPLICED TOGETHER NEAR CONNECTOR D2316P. THE WIRING DIAGRAM SHOWED THESE WIRES AS TERMINATING IN PINS 12 AND 11 OF CONNECTOR D2316P. SIMILAR DISCREPANCIES WERE FOUND FOR EACH OF THE OTHER ENGINE SHUT OFF VALVES. THE EFFECT OF THIS MODIFICATION WAS TO BYPASS THE FUNCTION OF THE ENGINE FUEL SHUT OFF SWITCHES ASSOCIATED WITH THE ENGINE START LEVERS.

Part: CONNECTOR — MISWIRED (FUEL SOV)

APPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF THE FIRE SWITCHES ON THE OVERHEAD PANEL. INVESTIGATION CONFIRMED THAT WIRES W629-1Q1221-20 AND 1Q1223-20 WERE SPLICED TOGETHER NEAR CONNECTOR D2316P. THE WIRING DIAGRAM SHOWED THESE WIRES AS TERMINATING IN PINS 12 AND 11 OF CONNECTOR D2316P. SIMILAR DISCREPANCIES WERE FOUND FOR EACH OF THE OTHER ENGINE SHUT OFF VALVES. THE EFFECT OF THIS MODIFICATION WAS TO BYPASS THE FUNCTION OF THE ENGINE FUEL SHUT OFF SWITCHES ASSOCIATED WITH THE ENGINE START LEVERS.

Part: BEAM — CRACKED (L4 DOOR)

CRACKED L4 DOOR LOWER BEAM. REPLACED BEAM PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1414)

LEVEL 2 CORROSION KEEL BEAM LOWER ACCESS PANEL SUPPORT BS 1414 LBL 15 TO RBL 15. REPLACED PER BOEING SRM 51-10-01.

Part: PANEL — CRACKED (BS 1241)

CRACKED PANELS BS 1241 LBL 90 AND RBL 82. REPLACED PANELS PER BOEING SRM 51-10-01.

Part: WEB — CRACKED (NLG WW)

CRACK NOSE LANDING GEAR SIDE WALL WEB AT BOTH SIDE TRUNNION FITTING CUTOUT FORWARD CORNERS FOUND CRACKED. REPAIRED PER BOEING SB 53-2293 AREA 5.

Part: SUPPORT — CORRODED (BS 1447)

LEVEL 2 CORROSION ACCESS PANEL SUPPORT KEEL BEAM BOX BS 1447 LBL 15. REPLACED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1283)

LEVEL 2 CORROSION BS 1283 LBL KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT. REPLACED PER BOEING SRM 51-10-01.

Part: STRINGER — CORRODED (BS 990-993)

LEVEL 2 CORROSION S 44L BS 990 TO 993. REPAIRED PER BOEING SRM 53-10-03 FIG 1.

Part: SHEAR TIE — CORRODED (BS 900)

LEVEL 2 CORROSION SHEAR TIE IN FORWARD CARGO COMPARTMENT BS 900 RBL 0 TO 5. REPAIRED PER BOEING SRM 53-10-04 FIG 3A.

Part: DOUBLER — CORRODED (BS 976-970)

LEVEL 2 CORROSION SKIN DOUBLER BULGED UP BS 976 TO 970 S 46R. REPLACED DOUBLER PER BOEING SRM 51-10-01.

Part: STRINGER — CORRODED (BS 990-993)

LEVEL 2 CORROSION S 44R BS 990 TO 993. REPAIRED PER BOEING SRM 53-10-03 FIG 1.

Part: BULKHEAD CHORD — CRACKED (NR 4 PYLON)

CRACKED NR 4 PYLON FORWARD ENGINE MOUNT BULKHEAD CHORD AT LEFT LOWER SIDE. REPLACED PER BOEING SRM 51-10-01 AND DRAWING 65B90416 AND 65B90316.

Part: SKIN — CORRODED (BS 1241)

LEVEL 1 CORROSION, FUSELAGE BS 1241 RH SPLICE STRAP MATING AREA ON FUSELAGE SKIN CORROSION REVEALED AFT SPLICE STRAP REMOVAL. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02. SB/EO NR: 53-2283.

Part: SPLICE STRAP — CORRODED (BS 12341)

LEVEL 1 CORROSION, FUSELAGE BS 1241 LH SPLICE STRAP MATING AREA ON FORGING CORROSION REVEALED AFT SPLICE STRAP REMOVAL. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02. SB/EO NR: 53-2283.

Part: SPLICE STRAP — CORRODED (BS 1241)

LEVEL 1 CORROSION, FUSELAGE - BX 1241 RH SPLICE STRAP MATING AREA ON FORGING CORROSION REVEALED AFT SPLICE STRAP REMOVAL. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02. SB/EO: 53-2283.

Part: SKIN — CORRODED (BS 1241)

LEVEL 1 CORROSION, FUSELAGE BS 1241 LH SPLICE STRAP MATING AREA ON FUSELAGE SKIN CORROSION REVEALED AFT SPLICE STRAP REMOVAL. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02. SB/EO NR 53-2283.

Part: SEAT TRACK — CORRODED (BS 520-580)

LEVEL 2 CORROSION UPPER DECK BS 520 TO 580 LBL 45 TIE DOWN TRACK. REPLACED PER BOEING SRM 53-10-05 FIG 6.

Part: SUPPORT — CORRODED (BS 1480)

LEVEL 2 CORROSION BODY FAIRING SUPPORT RIB BS 1480 LBL 60 TO RBL 60. REPLACED SUPPORT PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 1220-1260)

LEVEL 1 CORROSION, FUSELAGE BS 1220 - 1260 STRINGER 30R FUSELAGE SKIN CORROSION REVEALED AFT SPLICE FITTING REMOVAL. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02. SB/EO #: 747-53-2283.

Part: SPAR CHORD — CORRODED (RT WING)

LEVEL 2 CORROSION RIGHT WING FRONT SPAR CAVITY AT OLES 1385 TO 1395. REPAIRED PER BOEING SRM 57-30-03 FIG 9 AND HAECO RS R-57-21-33503.

Part: SKIN — CORRODED (BS 800)

LEVEL 2 CORROSION FUSELAGE BELLY SKIN AND DOUBLER BS 800 RBL 10 TO 12. REPAIRED PER HAECO RS 53-21-33504.

Part: SUPPORT BEAM — CRACKED (RT WING)

CRACK RIGHT WING SPOILER SUPPORT BEAM MOST INBOARD PORTION. REPAIRED PER BOEING SRM 51-40-03.

Part: SUPPORT — CORRODED (BS 1295-1298)

LEVEL 2 CORROSION KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT BS 1295 TO 1298 RBL 15. REPLACED PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (BS 820)

LEVEL 2 CORROSION BELLY SKIN AND DOUBLER BS 820 RBL 10 TO 12. REPAIRED PER HAECO RS 53-21-33504.

Part: SUPPORT — CORRODED (BS 2365)

LEVEL 1 CORROSION, M/D LATERAL FLOOR SUPPORT FOUND CORROSION AT BS 2365 RBL 12 - 47. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 2310-2315)

LEVEL 1, CORROSION M/D LONG FLOOR SUPPORT FOUND CORROSION AT BS 2310 - 2315 RBL 31. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 2280)

LEVEL 1 CORROSION, M/D LATERAL FLOOR SUPPORT FOUND CORROSION AT BS 2280 LBL 32 - 75. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1063)

LEVEL 2 CORROSION ON AIR CONDITIONING BAY ACCESS PANEL SUPPORT AT BS 1063 RBL 15 TO RBL 25. REPAIRED PER BOEING SRM 53-50-04 FIG 2.

Part: SUPPORT — CORRODED (BS 2360)

LEVEL 1 CORROSION, M/D LONG FLOOR SUPPORT FOUND CORROSION AT BS 2360 LBL 60. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 2350)

LEVEL 1 CORROSION, M/D LATERAL HAT SECTION FOUND CORROSION AT BS 2350 RBL 47 - 70. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 2320-2322)

LEVEL 1 CORROSION, M/D LONG FLR SUPPORT CORROSION AT BS 2320 - 2322 LBL 65. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: RIB — CORRODED (BS 1167)

LEVEL 1 CORROSION, FUSELAGE BS 1167 RBL 9 - RBL 58 AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: RIB — CORRODED (BS 1235)

LEVEL 1 CORROSION, FUSELAGE BS 1235 LBL 9 - LBL 58 AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: RIB — CORRODED (BS 1167-1235)

LEVEL 1 CORROSION, FUSELAGE BS 1167 - BS 1235 RBL 58 AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: RIB — CORRODED (BS 1235)

LEVEL 1 CORROSION, FUSELAGE BS 1235 RBL 9 - RBL 58 AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: RIB — CORRODED (BS 1063)

LEVEL 1 CORROSION, FUSELAGE AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION ON BS 1063 RBL 15- RBL 25. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.

Part: RIB — CORRODED (BS 1106)

LEVEL 1 CORROSION, FUSELAGE AIR CONDITION BAY ACCESS PANEL SUPPORT RIB FOUND CORROSION ON BS 1106 RBL 34- RBL 37. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (RT TE MIDFLAP)

LEVEL 1 CORROSION, RHW INBD MID FLAP UPPER SKIN PANEL 677GT SURFACE CORROSION REVEALED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (RT TE MIDFLAP)

LEVEL 1 CORROSION, RHW INBD MID FLAP UPPER SKIN PANEL 677HT SURFACE CORROSION REVEALED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: ANGLE — CORRODED (BS 682)

LEVEL 1 CORROSION, FWD CARGO DOOR SILL CHORD LOWER ATT ANGLE CORROSION AT BS682 RBL 62. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1940-1960)

LEVEL 1 CORROSION, BULK CARGO FLOOR SUPPORT UPPER SURFACE FOUND FT8 CORROSION AT BS 1940 - 1960 LBL 22 AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1480)

LEVEL 1 CORROSION, FUSELAGE BS 1480 LBL 60 - RBL 60 BODY FAIRING SUPPORT RIB FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.

Part: SUPPORT — CORRODED (BS 1295-1298)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1295 - BS 1298 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.

Part: SUPPORT — CORRODED (BS 1400-1414)

LEVEL 1 CORROSION, FUSELAGE KEEL BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1400- BS 1414 RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1295)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1295 - LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.

Part: SUPPORT — CORRODED (RT WING)

LEVEL 2 CORROSION RIGHT WING LEADING PANEL LOGITUDINAL SUPPORT AT ILES 445 AND 476. REPLACED PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1265)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1265 LBL 9 - RBL 9. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1336)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1336 - LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1436-1447)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1436 - BS 1447 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.

Part: SUPPORT — CORRODED (BS 1400-1414)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1400 - BS 1414 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1414-1436)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1414 - BS 1436 RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1468)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORRODED ON BS 1468- LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1436-1447)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1436 - BS 1447 RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1436)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1436 LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1414-1436)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1414 - BS 1436 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1337)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1337 LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1458)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1458 LBL 9 - RBL 9. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1368)

LEVEL 1 CORROSION, FUSELAGE BS 1368 LBL 7, RBL 7 KEEL BEAM BOX LOWER SUPPORT RIB LOWER SURFACE FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1400)

LEVEL 1 CORROSION, FUSELAGE BS 1400 LBL 15 - RBL 15 KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1283-1295)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1283 - BS 1295 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (BS 1470)

LEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1470 - LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: BULKHEAD FITTING — CRACKED (BS 1241)

CRACK BS 1241 BULKHEAD AFT HOLE AT PASSENGER DECK FITTING, CRACK .0625 RUNNING DOWNWARD. REAMED HOLE TO 0.875 AS PER SB 53-2283, HOLE CHECKED CRACK FREE.

Part: SILL — CORRODED (BS 1808-1812)

LEVEL 1 CORROSION, AFT CARGO BS 1808-1812 STR 42R DOOR SILL WEB OUTBD FACE FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION, LHW LWR SKIN INTERIOR SURFACE IN FRONT OF FRONT SPAR CHORD FOUND CORROSION AT WING LEADING EDGE CAVITY APPROX TO OLES 1415. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SUPPORT BEAM — CRACKED (LT WING)

CRACK LEFT WING SPOILER SUPPORT BEAM WEB LOWER CHORD AT OUTBOARD OF NR 6 SPOILER AREA. REPAIRED PER BOEING SRM 51-40-04.

Part: SKIN — CRACKED (BS 2606)

A .25 INCH CRACK ON SKIN BS 2606 BETWEEN S 51R AND S 49R. REPAIRED PER BOEING SRM 53-30-03.

Part: SKIN — CORRODED (LT WING)

LEVEL CORROSION, LHW UPPER SKIN CORROSION IN FRONT OF MID SPAR (NR 12 LEADING EDGE FLAP). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION, LHW UPPER SKIN TRAILING EDGE FOUND CORROSION AT REAR SPAR CHORD TO SKIN ATTACH FASTENERS AREA IN FRONT OF NR 3 SPOILER OUTBD CORNER. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION, LHW UPPER SKIN FOUND SURFACE CORROSION IN FRONT OF NR 3 SPOILER (MID SPAR ATTACH FASTENERS). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION, RHW UPPER TRAILING EDGE PANEL FORWARD EDGE ATTACH TO WING SKIN AREA FOUND CORROSION AT NR 8 SPOILER AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION, LHW UPPER SKIN FOUND SURFACE CORROSION AT REAR SPAR CHORD TO UPPER SKIN ATTACH FASTENERS AREA (APPROX AT WBL 163). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.

Part: FITTING — CRACKED (NR 1 PYLON)

NR 1 PYLON UNDERWING DIAGONAL BRACE FITTING CRACKED AT OUTBOARD SIDE AFT RADIUS POSITION. FITTING REPLACED PER SB 57-2288.

Part: BOOST PUMP — FAILED TEST (NR 2)

DURING TEST PER AD 97-03-17, NR 2 FORWARD BOOST PUMP FAILED 500 VDC MEG CHECK READS O.5 MEG. REPLACED BOOST PUMP PER BOEING MAINTENANCE MANUAL 28-31-01, RETESTED PER SERVICE BULLETIN 747-28A2194.

Part: BULKHEAD — CRACKED (NR 3 PYLON)

ON ENGINE CHANGE FIREWALL INSPECTION FOUND 2.5 INCH CRACK ON NACELLE FORWARD TORQUE BULKHEAD, 5 SHEARED FASTENERS ON PYLON LOWER FORWARD WEB, A 1.5 INCH AND 4 INCH CRACKS ON FORWARD LOWER WEB. REPLACED PYLON WITH SERVICABLE PYLON EEPER MAINTENANCE MANUAL 54-10-01 DUE TO TIME REQUIRED TO REPAIR TORQUE BULKHEAD AND WEB. REMOVED STRUT TO BE REPAIRED PER SB 747-54A2069.

Part: ENGINE — STALLED (NR 3)

IMMEDIATELY AFTER TAKEOFF AT TAKEOFF THRUST, NR 3 ENGINE APPEARED TO STALL. EGT APPEARED TO HAVE PEAKED AT 975 DEGREES ACCORDING TO THE MAX EGT POINTER ON THE EGT GAUGE. THE THROTTLE WAS SUBSEQUENTLY RETARDED AND ALL ENGINE PARAMETERS WERE NORMAL. CONTROL TOWER IN SCL REPORTED SEEING FLAMES FROM THE ENGINE AT THE MOMENT OF THE APPARENT ENGINE STALL. ALTERNATE PROCEDURE 6-15-16 WAS CONSULTED WEATHER CONDITIONS AT SCL WERE 14 DEGREES CELSIUS, DEW POINT 11 DEGREES CELSIUS, WIND VARIABLE AT 1 KT. OBSERVED EGT PRIOR TO RETARDING THE THROTTLE WAS 930 DEGREES CELSIUS. BORESCOPE INSPECTED NR 3 ENGINE PER MAINTENANCE MANUAL 72-00-00 AND INSPECTED INLET AND EXHAUST AREA FOR DAMAGE, NONE FOUND. ENGINE TO BE REPLACE

Part: ANTI-SKID SYS — FAILED (LT MLG)

ON LANDING WITH NORMAL TOUCH DOWN, ANTI-SKID LIGHT ILLUMINATED ON PILOTS CAUTION PANEL AND ANTI-SKID LIGHTS FOR LEFT FRONT, LEFT AND RIGHT REAR LEFT BODY GEAR ON F/E'S PANEL ILLUMINATED. TOWER REPORTED SMOKE FORM LANDING GEAR ON LANDING. STOPPED AIRCRAFT ON TAXI WAY. FOUND NR 7 AND NR 8 TIRES FAILED NR'S 1, 3, 4, 5, AND 6 TIRES THERMAL DISCHARGED. PERFORMED CONDITIONAL INSPECTION PER M/M 05-51-05, 09, 16, 17, 25, AND 34. REPLACED TIRES 1, 3, 4, 5, 7, 8, 11, 12 PER M/M 32-41-01. REPLACED 7 AND 8 BRAKE PER M/M 32-45-15. REPLACED DAMAGED STRUT DOOR, BODY PANEL BETWEEN BS 1580, AND 1620, LT ADF PANEL, LT BODY GEAR HYDRAULIC LINES AND BODY GEAR ELECTRICAL HARNESS. REPLACED NR 7 AND NR 8 ANTI-SKID TRANSDUCERS

Part: TT2 SENSOR — MALFUNCTIONED (NR 1 ENGINE)

JUST PRIOR TO DESCENT, NR 1 ENG WOULD NOT RESPOND TO THROTTLE MOVEMENT BETWEEN FLIGHT LEVELS 35.0 AND 25.0. EPR .95; EGT 600 C; FUEL/FLOW 2700 N1 59 PERCENT. CREW TRIED A RAPID RESTART AT 250 KTS, NO HELP ENG ANTI-ICE ON ALL FUEL PUMPS, TRIED FUEL HEAT BOTH IGNITORS, 3 PACKS ETC (NO HELP). ENGINE STARTED TO RESPOND NORMALLY AFT FL 250 ON IT'S OWN. AFTER LANDING NR 1 (ENG) WOULD NOT SPOOL UP IN REVERSE. ALSO, ENG VERY SLOW TO SPOOL UP IN FORWARD THRUST. BLEED TT2 SENSOR, OPERATIONAL CHECK OF THROTTLE SATISFACTORY, REQUESTED CREW EVALUATION NEXT TAKEOFF. NO REOCCURENCE OF PROBLEM HKG/JFK LEGS. REMOVED AND REPLACED MAIN FUEL FILTER.

Part: FITTING — CRACKED (RT FUSELAGE)

INBOARD TRUNNION LONGERON BRIDGE FITTING FRACTURED. REPAIRED PER EA 47-5343-15-A0175 MOBILE AEROSPACE ENGINEERING.

Part: COWL — DAMAGED (NR 2 ENGINE)

NR 2 NOSE COWL - DAMAGE ON EXTERIOR FLANGE 'V' GROVE AT 90 DEGREE POSITION GOUGED AND DENT WITH A CRACK. REPAIRED PER BOEING DER 8110-3 MOBILE AEROSPACE ENGINEERING EA-47-5400-15-A0174.

Part: SKIN — DELAMINATED (LT MLG DOOR)

LEFT WING LANDING GEAR - LOWER STRUT DOOR DELAMINATED ON LOWER END BY FAIRING. REF: PA1579030151. REPLACED PER MM 32-12-06.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RIGHT WING LANDING GEAR - LOWER STRUT DOOR - DELAMINATED AT LOWER END. REPLACED PER MM 32-12-06.

Part: LATCH FITTING — CRACKED (CARGO DOOR)

FORWARD LOWER CARGO DOOR - CRACK IN NR 6 (FROM FORWARD END) LATCH SUPPORT FITTING - FORWARD LEG. REPAIRED PER SB-747-53-2200.

Part: LINK BOLT — ROTATED (NR 1 ENGINE)

NR 1 ENGINE - AFT MOUNT - INBOARD TANGENTIAL LINK BOLT HAS ROTATED. POLAR AIR WORK CARD S1-7121-002 REF AD-96-03-01 COMPLIED WITH.

Part: STRIP — CRACKED (NR 3 PYLON)

NR 3 PYLON - L/S UPPER WING TO PYLON STRIP CRACKED AT OLD WELD ABOVE ACCESS PANEL 472DL. WELDED PER BOEING SRM 51-30-02.

Part: SKIN — PUNCTURED (LT TE AFT FLAP)

L/W, I/B, AFT FLAP SMALL PUNCTURE BETWEEN 3 AND 4 CANOE. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — CORRODED (BS 960)

BELLY PANELS BS 960 BACK TO MLG, BARE AND CORROSION SPOTS. REPAIRED, TREATED AND FINISHED PER BOEING SRM 51-10-02.

Part: DOUBLER — CRACKED (BS 350)

TWO CRACKS IN DOUBLER UPPER AFT NLG, WHEEL WELL RIGHT SIDE OF RETRACT LINK. REPAIRED PER BOEING SRM 51-40-02.

Part: RIVETS — MISSING (BS 1390)

FASTENERS BETWEEN BLG DOOR ON KEEL BEAM PANELS MISSING. REPAIRED PER BOEING SRM 51-30-02.

Part: HINGE — CORRODED (BS 1800)

BARE METAL WITH SURFACE CORROSION, ALONG HINGE ASSY OF MAIN DECK CARGO DOOR ON FUSELAGE. REPAIRED PER BOEING SRM 51-10-01.

Part: THRESHOLD — CRACKED (BS 2000)

BULK CARGO DOORWAY THRESHOLD CRACKED. REPAIRED PER BOEING SRM 51-30-02.

Part: SKIN — DETERIORATED (TE MID FLAP)

R/W, I/B, MID FLAP, L/E DETERIORATED ON O/B END. REPAIRED PER BOEING SRM 51-40-15.

Part: R-RAIL — CRACKED (NR 1 ENGINE)

NR 1 ENGINE, R-RAIL CRACKED AT 170 DEGREE POSITION. REPAIRED PER PRATT AND WHITNEY 72-53-01.

Part: FAIRING — LOOSE (NR 4 PYLON)

NR 4 PYLON FAIRING ABOVE TURBINE EXHAUST CASE LOOSE AND MISSING RIVETS. REPAIRED PER BOEING SRM 51-30-02.

Part: PANEL — DENTED (RT HORIZ STAB)

DENT AND ABRASION, TOP RT STABILIZER L/E PANEL. REPAIRED PER SRM 55-10-03.

Part: SKIN — CORRODED (BS 1265-1460)

UPPER FUSELAGE HAS BARE SPOTS WITH CORROSION SURFACE BS 1265 TO 1460. REPAIRED PER SRM 51-10-01.

Part: FAIRING — CORRODED (BS 920)

LWR BODY FAIRINGS, CORROSION BY RAD ALT ANTENNAS AND CIRCULAR ACCESS COVERS. REPAIRED PER BOEING SRM 51-40-11.

Part: SKIN — CORRODED (LT FUSELAGE)

LEVEL 1 CORROSION UPPER DECK WINDOW LT SIDE. REPAIRED PER BOEING SRM 51-10-01 AND 51-10-02.

Part: SKIN — SEPARATED (NR 4 ENGINE)

NR 4 ENGINE TURBINE EXHAUST CASE OUTER SKIN PULLED FASTENERS AND SKIN SEPARATED. REPAIRED PER BOEING SRM 51-30-02.

Part: SKIN — CORRODED (BS 500)

LEVEL 1 CORROSION 2 OF 4 DME ANTENNA BASES CORRODED. REPAIRED PER SRM 51-10-01, 51-10-02 AND 51-10-06.

Part: ACCESS PANEL — CRACKED (WS 670)

ACCESS PANEL O/B OF NR 6 CANOE CRACKED. REPAIRED PER SRM 51-40-09.

Part: SKIN — GOUGED (BS 430)

LEVEL 1 DOOR GOUGE IN SKIN FORWARD OF DOOR FUSELAGE BS 430 WL 230. REPAIRED PER BOEING SRM 51-10-02.

Part: SKIN — CRACKED (PAX DOOR)

NR 1 MAIN ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED PER BOEING SRM 52-00-02 FIGURE 1 DETAIL II.

Part: FASTENERS — BROKEN (AFT CARGO DOOR)

AFT CARGO DOOR SILL LATCH PIN FITING AT BS 1840 HAS BROKEN FASTNERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.

Part: ENGINES — STALLED (NR 1/2)

*** CORRECTION***AT FLIGHT LEVEL 430, NR 1 AND NR 2 ENGINE LOW SPEED STALL, NO THROTTLE RESPONSE, AT FL 350 ALL PARAMETERS NORMAL THROUGH REMAINING FLIGHT. CARRIED OUT INLET AND EXHAUST INSPECTION CHECK, ALL CHECKED NORMAL. CHANGED FUEL FILTERS, NO CONTAMINATION FOUND. DRAINED FUEL TANKS, NO WATER FOUND. PER MAINTENANCE MANUAL 71-00-42. PER PRATT AND WHITNEY CHECKED FOR PNEUMATIC LEAKS, CHECKED OPERATION OF ISOLATION VALVES AND OPERATION OF HIGH STAGE CONTROLLERS, ALL CHECK NORMAL.

Part: LINE — WORN (LT MLG)

HYDRAULIC LEAK FROM LINE IN LEFT BODY GEAR WHEEL WELL. REPLACED LINE AND LEAK CHECKED PER BOEING MAINTENANCE MANUAL 29-00-00.

Part: LINE — CRACKED (NR 4 PYLON)

SLOW LOSS OF HYDRAULIC FLUID NUMBER 4 HYDRAULIC SYSTEM DURING FLIGHT. ENGINE DRIVEN PUMP DEPRESSURIZED AND QUANTITY HELD AT 4 GALLONS. FOUND NR 4 ENGINE DRIVEN PUMP PRESSURE LINE IN PYLON CRACKED. REPLACED LINE LEAK CHECK AND OPERATIONAL CHECK OK PER MAINTENANCE MANUAL 29-11-00.

Part: DRAIN CAP — BAD SEAL (NR 4 ENGINE)

LOSS OF OIL QUANTITY NR 4 ENGINE ON TAXI OUT. FOUND DRAIN CAP SEAL LEAKING ON KIT INSTALLED FOR ENGINE DRIVEN HYDRAULIC PUMP DEACTIVATION PER MEL 29-01 PER MAINTENANCE MANUAL 29-11-05. REPLACED CAP LEAK CHECK OK.

Part: PANEL — CRACKED (LT WING)

A 4 INCH CRACK ON LEFT WING LOWER, PANEL FORWARD OF WING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06.

Part: PANEL — CRACKED (LT WING)

A 4 INCH CRACK IN LEFT WING LOWER PANEL FORWARD OF WING LANDING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06.

Part: GUSSET — CRACKED (NR 1 PYLON)

CRACKED GUSSET NACELLE STATION 180 NR 1 PYLON AS VIEWED THOUGH ACCESS PANEL 452BL. REPLACED PER BOEING SRM 51-10-01 AND POLAR MA 5430-02:01.

Part: SKIN — CRACKED (NR 4 PYLON)

A .25 INCH CRACK ON NR 4 ENGINE PYLON INBOARD SIDE GOING INTO SCREW ABOVE HORSE SHOE PLATE NACELLE STA 222. REPAIRED PER BOEING SRM 54-30-03 FIG 35.

Part: SKIN — CRACKED (NR 1 PYLON)

CRACK IN SKIN NR 1 PYLON AT NAC STA 180 WL 152, SLOT SEAL AREA. REPAIRED PER BOEING SB 54-2034 REV 4 AND POLAR MA 5430-02:01.

Part: FAIRING — CRACKED (RT FUSELAGE)

CRACK ABOVE THE ACCORDIAN SEAL STRIKE PLATE ON RIGHT FUSELAGE BODY FAIRING. REPAIRED PER BAC SRM 51-40-09.

Part: SKIN — CRACKED (NR 2 PYLON)

CRACK APPROX .25 INCH GOING TO RIVET HOLE AT TOP AFT CORNER OF NR 2 PYLON CUTOUT FOR PANEL 463CL. DYE CHECK CONFIRMED CRACK, EDDY CURRENT CK PER BAC NDT MANUAL PART 6 AND INSTALLED DOUBLER PER BAC SRM 54-30-03.

Part: DOUBLER — CRACKED (NR 2 PYLON)

NR 2 PYLON OUTBOARD MID SPAR PIN FITTING LUG DOUBLER IS CRACKED. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-30-04.

Part: R RAIL — CRACKED (NR 1 ENGINE)

NR 1 ENGINE 'R' RAIL IS CRACKED AT THE 7 O'CLOCK POSITION. WELDED, STRESS RELIEVED, AND PEENED IAW MM 72-53-01. PART TOTAL CYCLES, 15,294.

Part: SKIN — CRACKED (NR 2 ENGINE COWL)

NR 2 ENGINE OUTBOARD CORE COWL SECOND FROM FWD LATCH CUTOUT IS CRACKED. FABRICATED NEW LONGERON AND INSTALLED IAW SRM 51-40-03.

Part: ANGLE — CRACKED (NR 4 ENGINE COWL)

NR 4 ENGINE INBOARD CORE COWL LOWER HOT SECTION ANGLE IS CRACKED IN TWO PLACES. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-01.

Part: FAIRING — CRACKED (NR 3 PYLON)

NR 3 PYLON FORWARD FAIRING AFT OUTBOARD EDGE CRACKED AND RIVETS SHEARED. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-40-03.

Part: SPAR — CORROSION (RT WING)

LEVEL 1 CORROSION ON RIGHT WING FRONT SPAR LOWER CHORD AT NR 19 LEADING EDGE FLAP PANEL WELL. REMOVED LEVEL 1 CORROSION AND TREATED AREA PER BAC SRM 57-30-01.

Part: SILL — CRACKED (NR 4 PYLON)

CRACKED SILL ON NR 4 PYLON LEFT SAILBOAT DOOR. FABRICATED AND INSTALLED SILL PER BOEING SRM 51-30-02 AND 51-10-01.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

CRACKED PRECOOLER NR 3 ENGINE NEAR HI-STAGE VALVE CONNECTION. WELD REPAIRED PER BAC 59-75.

Part: SKIN — CRACKED (RT MLG DOOR)

CRACKED INNER SKIN ON RIGHT BODY OUTBOARD DOOR. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-02.

Part: SUPPORT ROD — BROKEN (LT WING)

BROKEN ANGLED SUPPORT ROD LEFT WING NR 7 LEADING EDGE FLAP WELL. FABRICATED AND INSTALLED NEW SUPPORT ROD PER BOEING SRM 51-10-01 AND 51-30-02.

Part: FAIRING — DAMAGED (RUNWAY LIGHT)

DAMAGED LOWER AFT CORNER OF NOSE RUNWAY TURNOFF FAIRING. APPLIED FIBERGLASS OVERLAY PER BAC SRM 51-40-09.

Part: COWL — CRACKED (NR 2 ENGINE)

CRACKED NR 2 ENGINE CORE COWL STRUCTURE AT AFT BOTTOM ALIGNMENT PIN WITH PUSHED IN PIN. FABRICATED AND INSTALLED NEW COWL RIB AND ATTACH CLIPS PER BAC SRM 51-10-01.

Part: STIFFENER — CRACKED (BS 1400)

CRACKED STIFFENER ON RIGHT BODY GEAR WHEELWELL PRESSURE DECK BS 1400 RBL 100. REMOVED STIFFENER, PERFORMED HFEC INSPECTION OF AREA BELOW CRACK PER BOEING NDT MANUAL PART 6 51-00-00. NO DEFECTS NOTED. REPLACED STIFFENER WITH NEW PART PER BOEING SRM 51-10-01. MATERIAL IDENTIFICATION PER BOEING SRM 53-11-22, PAGE 143.

Part: BRACKET — CRACKED (BS 1395)

CRACKED LIGHT BRACKET IN RIGHT BODY LANDING GEAR WHEEL WELL BS 1395 RBL 90 WL 200. REPLACED LIGHT BRACKET PER BOEING SRM 51-10-01.

Part: BRACKET — CRACKED (BS 1350)

CRACKED AND BENT INBOARD FLAP TORQUE TUBE WHIP GUARD BS 1350 RBL 90. REPAIRED PER BOEING SRM 51-40-03.

Part: ANGLE — CRACKED (BS 1350)

CRACKED ATTACH ANGLES FOR RIGHT BODY LANDING GEAR TRUCK BUMPER AT LOWER WL 140 AND UPPER WL 160 BS 1350. REPLACED LOWER ANGLE PER BOEING SRM 51-10-01 AND REPAIRED UPPER PER BOEING SRM 51-30-03.

Part: TORQUE LINK — MISSING (RT MLG BRAKE)

AFTER TAKEOFF, LOST NR 1 HYDRAULIC SYSTEM FLUID. LANDING INSPECTION REVEALED RIGHT BODY GEAR LEFT FORWARD BRAKE TORQUE LINK DISCONNECTED. ADDITIONAL DAMAGE TO BODY GEAR TILT ACTUATOR HOSE, NR 10 BRAKE HOSE BOTH FORWARD AND AFT BRAKE TORQUE LINKS. BRAKE ROD BOLT FOUND ON RUNWAY. REPLACED BRAKE TORQUE LINKS, NR 10 BRAKE AND BRAKE LINE PER M/M 32-41-00, REPLACED TILT ACTUATOR LINE PER MM 20-11-05 PAGE 815. REPLACED NR 10 TIRE PER MM 32-45-00. REPLACED NR 1 EDP, CASE DRAIN FILTER, PRESSURE FILTER AND FLUSHED LINES PER MM 29-11-05, 29-11-18, 29-11-23.

Part: MODULE HOUSING — CRACKED (NR 3 HYD SYST)

NR 3 HYDRAULIC SYSTEM FLUID LOSS AFTER PUSHBACK. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODULE HOUSING CRACKED. REMOVED AND REPLACED MODULE PER BOEING MAINTENANCE MANUAL 29-11-23.

Part: ENGINE — MALFUNCTIONED (NR 4)

NR 4 ENGINE OIL QUANTITY DECREASED INFLIGHT, WHEN OIL PRESSURE BEGAN TO FLUCTUATE AND LOW OIL PRESSURE CAUTION LIGHT FLICKERED. COMPLETED THE PRECAUTIONARY ENGINE SHUT DOWN. ON GROUND RUN FOUND OIL LEAKING FROM BREATHER PORT. REMOVED AND REPLACED ENGINE PER BOEING MAINTENANCE MANUAL 71-00-02.

Part: BRACKET — BROKEN (E/E COMPT)

FORWARD CARGO E AND E COMPARTMENT RIB FOR CANNON PLUGS BETWEEN RIGHT AND CENTER SECTION SUPPORT BRACKET BROKEN. REPLACED PER BOEING SRM 51-10-01.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 2ND ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT 2ND ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.

Part: SUPPORT — BROKEN (E/E COMPT)

FORWARD CARGO E AND E COMPARTMENT MOST OUTBOARD CANNON PLUG RIB SUPPORT RIB BROKEN. REPAIRED VERTICAL SUPPORT PER BOEING SRM 51-10-01 AND SRM 51-40-03.

Part: SUPPORT — CRACKED (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, RIB WHICH HOLDS CANNON PLUGS BETWEEN LEFT AND CENTER SECTIONS, CRACKED AND BROKEN. REPAIRED PER BOEING SRM 51-10-01 AND SRM 51-40-03.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, CENTER SECTION 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, RIGHT SIDE 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR)

FORWARD CARGO DOOR, SEAL DEPRESSOR DAMAGED FORWARD LOWER SIDE. REPLACED DAMAGED SECTION PER BOEING SRM 51-10-01.

Part: BRACKET — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE OUTBOARD RIB FOR CANNON PLUGS SUPPORT BRACKET BENT. REPLACED PER BOEING SRM 51-10-01.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 3RD ROW BURNDY BLOCK SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.

Part: SUPPORT — BENT (E/E COMPT)

FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 4 TH ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.

Part: O-RINGS — CUT (NR 1 CHK VALVE)

NR 1 HYDRAULIC SYSTEM FLUID LOSS AFTER TAKEOFF. LEAK STOPPED WHEN PUMPS SHUT OFF, SYSTEM QUANTITY STABLE AT 2.5 GALLONS. EXTENDED GEAR AND FLAPS BY ALTERNATE SYSTEM. UPON APPROACH TO MIAMI HAD BODY GEAR AND NOSE GEAR STEERING AVAILABLE FOR TAXI IN. FLUID LOSS CONTINUED TO LESS THAN 1 GALLON DURING TAXI. FOUND NR 1 HYDRAULIC SYSTEM PRESSURE MODULE CHECK VALVE LEAKING. REMOVED CHECK VALVE AND FOUND O-RINGS DAMAGED VISUALLY CHECKED INNER MATING AREA, FOUND OK. REPLACED O-RINGS, OPERATIONAL AND LEAKED CHECKED OK PER BOEING MAINTENANCE MANUAL 29-11-13 AND 29-11-00.

Part: STOP FITTING — CRACKED (AFT CARGO DOOR)

AFT CARGO DOOR FRAME STRUCK BY PALLET AND DAMAGED DURING LOADING. FOUND WEB DAMAGE AT BS 1820 AT LOWER STOP FITTING, FITTING CRACKED. REPAIRED WEB AND FITTING IAW SRM 53-10-04.

Part: PANEL — CRACKED (RT TE MIDFLAP)

FOUND RIGHT WING INBOARD MIDFLAP OUTBOARD END CRACKED. REPAIRED IAW SRM 51-40-09.

Part: FITTING — CRACKED (RT MLG DOOR)

FOUND RIGHT HAND BODY GEAR OUTBOARD DOOR ACTUATOR CONNECTING ROD FITTING ON UPPER DOOR CRACKED. REPLACED ROD FITTING PER MM 32-33-28. OPS CHECK GOOD PER MM 32-33-00.

Part: PANEL — PUNCTURED (RT TE FOREFLAP)

FOUND RIGHT HAND INBOARD FOREFLAP PUNCTURED ON LOWER SURFACE NEAR CENTER. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS REPAIRS IAW SRM 51-40-15.

Part: MOUNTING PIN — CORRODED (NR 7 FLAPTRACK)

FOUND NR 7 FLAP TRACK AFT LINK MOUNTING PIN CORRODED. REPLACED PIN IAW OHM 27-51-75.

Part: PANEL — PUNCTURED (LT OB FOREFLAP)

FOUND LEFT OUTBOARD FOREFLAP PUNCTURED ON UNDERSIDE AT OUTBOARD END. REPAIRED IAW SRM 51-40-06.

Part: MOUNTING BOLTS — CORRODED (NR 1 AFT)

FOUND NR 1 AFT LINK MOUNTING BOLTS CORRODED. REMOVED AND REPLACED NR 1 TRACK AFT LINK MOUNTING BOLTS IAW OHM 27-51-75/SB 27-2280.

Part: PANEL — DELAMINATED (LT TE MID FLAP)

FOUND LEFT INBOARD MID FLAP LEADING EDGE DELAMINATED APPROXIMATELY 6 FEET FROM INBOARD EDGE. REMOVED DAMAGED SKIN, FABRICATED FILLERS AND DOUBLERS, REPAIRED AREA IAW SRM 51-40-15.

Part: BOLTS — CORRODED (FLAP TRACKS)

FOUND ALL FLAP TRACK FAIL SAFE BOLTS CORRODED. REMOVED AND REPLACED OUTBOARD TRACK FAIL SAFE BOLTS IAW MM 27-51-04. REMOVED AND REPLACED INBOARD TRACK FAIL SAFE BOLTS IAW MM 27-51-01.

Part: FLOOR PANEL — DELAMINATED (BS 500)

FOUND MAIN DECK BS 500, RBL 20, FLOOR PANEL ASSEMBLY DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-30-02.

Part: PANEL — CRACKED (LT WING FAIRING)

FOUND LEFT WING UPPER FIXED FAIRING PANEL JUST AFT OF R/S FORWARD OF MLG BEAM ASSEMBLY CRACKED. CRACK APPROXIMATELY 12 INCHES LONG. REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: PANEL — PUNCTURED (LT TE AFT FLAP)

FOUND LEFT OUTBOARD AFT FLAP PANEL PUNCTURED ON UNDERSIDE APPROXIMATELY 1 FOOT FROM OUTBOARD END. REMOVED DAMAGED AREA AND APPLIED FILLER AND DOUBLER IAW SRM 51-40-06.

Part: PANEL — DELAMINATED (LT TE AFT FLAP)

FOUND LEFT OUTBOARD AFT FLAP DELAMINATED ON UNDERSIDE AT INBOARD END. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-40-15.

Part: FAIRING — DELAMINATED (WING/BODY)

FOUND AFT WING-TO-BODY FAIRING 194BR DELAMINATED. REPAIRED FAIRING IAW SRM 51-40-14.

Part: EXH DUCT — CRACKED (NR 2 ENGINE)

FOUND NR 2 ENGINE 3.5 BLEED AIR LOWER RIGHT HAND EXHAUST DUCT CRACKED. REMOVED DUCT, WELDED IAW BAC5975, REINSTALLED DUCT IAW MM 75-32-06.

Part: PANEL — DELAMINATED (RT TE AFT FLAP)

FOUND RIGHT WING INBOARD AFT FLAP OUTBOARD UPPER STRESS PANEL DELAMINATED. REMOVED AND REPLACED STRESS PANEL IAW SRM 51-30-02.

Part: ANGLE — CRACKED (NR 1 ENG COWLING)

FOUND CRACKED BRACKET AND DAMAGED PIN AREA AT NR 1 INBOARD COWLING LOWER INSIDE CORNER AT ALIGN PIN. REPAIRED CRACKED ANGLE IAW SRM 51-40-04.

Part: SKIN REPAIR — DISBONDING (LT WING)

FOUND UPPER LEFT WING COMPOSITE REPAIR DISBONDING JUST BELOW L-3 DOOR. REPAIRED IAW SRM 51-40-09.

Part: SKIN — PUNCTURED (NR 1 ENG COWLING)

FOUND NR 1 OUTBOARD MAIN COWL SKIN PUNCTURED BETWEEN FIRST AND SECOND RIB. REPAIRED COWLING IAW SRM 54-30-03.

Part: CHAFE STRIP — CRACKED (NR 1 ENG COWLING)

FOUND NR 1 INBOARD COWLING LOWER AFT CORNER (INSIDE) HAS CHAFE STRIP CRACKED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-10-01 AND SRM 51-30-02.

Part: BRACKET — CRACKED (NR 1 ENG COWLING)

FOUND NR 1 INBOARD ENGINE COWLING LOWER FORWARD CORNER INSIDE BRACKETS AT FORWARD FRAME STIFFENER CRACKED AND DAMAGED. REPAIRED CORNER BRACKETS AND FRAME STIFFENER IAW SRM 54-14-03.

Part: PANEL — BROKEN (RT TE MIDFLAP)

FOUND RIGHT WING OUTBOARD MIDFLAP OUTBOARD LOWER CORNER BROKEN OFF. REPAIRED IAW SRM 51-40-09.

Part: LATCH MOUNT — DAMAGED (NR 2 ENGINE)

FOUND NR 2 ENGINE OUTBOARD COWL NR 3 LATCH MOUNT DAMAGED. REMOVED AND REPLACED LATCH MOUNT ANGLE IAW SRM 51-30-02.

Part: SILL PROTECTOR — CRACKED (CARGO DOOR)

FOUND AFT SILL PROTECTOR IN FRONT OF MAIN DECK CARGO DOOR HAS CRACK IN CENTER PORTION. FOUND CRACK IN SILL PROTECTOR WEB ALSO, UPON REMOVAL OF SILL PROTECTOR. REMOVED SILL PROTECTOR AND WEB IAW SRM 51-10-01. INSTALLED NEW PROTECTOR AND WEB IAW SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — CRACKED (NR 2 ENG FAIRING)

FOUND NR 2 ENGINE FORWARD FAIRING HAS CRACK IN SKIN ON INBOARD SIDE. REMOVED PREVIOUS REPAIR IAW SRM 51-30-02, INSTALLED DOUBLER AND FILLER IAW SRM 51-10-01.

Part: R RAIL — CRACKED (NR 1 ENGINE)

FOUND NR 1 ENGINE R-RAIL CRACKED AT 10 O'CLOCK POSITION UNDER PRECOOLER DOOR. REMOVED DOOR, STRESS RELIEVED IAW MM 72-53-01, FLAP PEENED R-RAIL IAW SRM 51-10-07, REINSTALLED DOOR IAW MM 36-12-01.

Part: SIGN — INOPERATIVE (CABIN)

FOUND CREW ENTRY EMERGENCY EXIT SIGN INOPERABLE. RELAMPED LIGHT FIXTURE, OPS CHECK GOOD IAW MM 33-51-13.

Part: ANTI-ICE VLV LT — MALFUNCTIONED (NR 4 ENGINE)

AIRCRAFT HAD GATE TURNBACK DUE TO NR 4 ENGINE ANTI-ICE LIGHT ON. VALVE OPS CHECKS NORMAL IAW MM 75-11-00. DEFERRED NR 4 ENGINE ANTI-ICE VALVE LIGHT PER MEL 30-04-1, DUE 31 MAY 96.

Part: TRANSFORMER — FAILED (COCKPIT)

AFTER PUSHBACK AND ENGINE START ALL FLIGHT ENGINEER PANEL LIGHTS WENT OUT AND A BURNED SMELL IN THE AREA. REMOVED AND REPLACED TRANSFORMER T-164 PER WIRING DIAGRAM MANUAL 33-12-11 TEST GOOD PER 33-12-00.

Part: CONTROL UNIT — FAILED (RUDDER)

AIRCRAFT RETURNED TO BLOCKS DUE TO RUDDER RATIO LIGHT ILLUMINATED. LOWER RUDDER STAYED IN HIGH-SPEED MODE. REMOVED AND REPLACED LOWER RUDDER RATIO CONTROL UNIT IAW MM 27-21-13.

Part: STARTER — INOPERATIVE (NR 1 ENGINE)

RETURNED TO BLOCKS DUE TO UNABLE TO START NR 1 ENGINE. REPLACED STARTER, STARTER GEARBOX MOUNT ADAPTER AND MOUNT CLAMP IAW MM 80-11-01.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND CREW SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED IAW MM 33-51-00.

Part: LIGHT — INOPERATIVE (FLT COMPT)

FOUND FLIGHT COMPARTMENT EMERGENCY LIGHT INOP. REMOVED AND REPLACED SAME IAW MM 33-51-00.

Part: RELAY — INOP (FUELING PANEL)

ON CLIMBOUT FL 20.0, LOST ALL POWER TO ENGINE FUEL PANEL, WITH NO GAUGE MOVEMENT AND NO GAUGE PRESSURE TO TEST. ON LANDING, AFTER APPROX 4 MINUTES TAXI, ALL POWER CAME BACK AND FUEL QUANTITY GAUGES RAN DOWN TO ACTUAL FUEL. FOUND FAULTY R996 RELAY AND REPLACED RELAY IAW WPM 28-21-01. ALL INDICATIONS CHECKED OK ON ENGINE GROUND RUN AND WITH AIRCRAFT IN FLIGHT MODE.

Part: PRESS INDICATOR — INOPERATIVE (NR 3 ENGINE)

AFTER PUSHBACK, NR 3 ENGINE WAS STARTED AND OIL PRESSURE INDICATOR DID NOT INDICATE. REMOVED AND REPLACED OIL PRESSURE INDICATOR IAW MM 79-32-03, OPS CHECKS GOOD.

Part: FAIRING — PUNCTURED (NR 4 TE FLAP)

FOUND NR 4 CANOE FAIRING PUNCTURED. REPAIRED IAW SRM 51-40-09.

Part: WEB — CRACKED (NR 4 PYLON)

FOUND NR 4 PYLON MIDSPAR WEB CRACKED AT APPROX NACELLE STA 205. WEB REPAIRED IAW SRM 54-10-03.

Part: SUPPORT FTG — CRACKED (LT WING MLG)

DURING SSID INSPECTION, NOTED INDICATION OF CRACK ON OUTBOARD WING GEAR SUPPORT FITTING. REMOVED FITTING AND REPAIRED PER S/B 747-57-2244. BORED TO FIRST OVERSIZE, MAG PART INSP COMPLETED, FITTING REINSTALLED.

Part: SKIN — CHAFED (BS 2658)

FOUND APU COMPT FORWARD BULKHEAD FWD SIDE CHAFED THROUGH AT STA 2658, CAUSED BY IMPROPERLY INSTALLED SHROUD AT BULKHEAD. REPAIRED DAMAGED AREA IAW SRM 53-10-04.

Part: SKIN — CORRODED (NR 9 SPOILER)

FOUND CORROSION AND SLIGHT BULGING OF PAINT AROUND RIVET HEAD FORWARD OF NR 9 SPOILER. CLEANED AND TREATED PER SRM 51-10-01.

Part: SUPPORT BEAM — CRACKED (WS 432.65)

FOUND SUPPORT BEAM CRACKED IN PREVIOUS REPAIR. REPAIRED PER SRM 51-40-03, WEB REPLACED WITH 2024-T3.040 MATERIAL.

Part: DOOR — CRACKED (AFT CARGO DOOR)

FOUND CRACK ON AFT CARGO DOOR LEFT LOWER EDGE AT STA 1880. REPAIRED IAW SRM 52-00-03.

Part: CHORD — CORRODED (BS 1351)

FOUND LEVEL 1 CORROSION AT STATION 1350 PRESSURE DECK TOP CHORD. CORROSION REMOVED, FOUND WITHIN LIMITS IAW SRM 53-10-01.

Part: FITTING — WORN (RT INBD AILERON)

FOUND BOTH FORWARD AND AFT INBOARD FAIL-SAFE FITTINGS ON RT INBOARD AILERON DUE TO LOOSE RIVETS IN PREVIOUS REPAIR. REMOVED FITTINGS, REPAIRED WEB, REINSTALLED NEW BUSHINGS AND FITTINGS IAW SRM 57-51 02A-001A AND 57-42-14-001.

Part: SLEEVE — CRACKED (NR 2 ENGINE)

FOUND TURBINE REVERSER SLEEVE CRACKED BETWEEN TWO PREVIOUS REPAIRS. REPAIRED IAW SRM 54-30-03. REPAIR INCLUDES BOTH PREVIOUS REPAIRS.

Part: PANEL — DELAMINATED (LT WING)

FOUND OVERWING PANEL ABOVE REAR SPAR WBL 244.6 TO 277 FIXED T/E DELAMINATED. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-40-09.

Part: LE SKIN — DENTED (VERTICAL FIN)

FOUND LOWER VERTICAL FIN LEADING EDGE SKIN DENTED AT STA 124 AND STA 220. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 55-30-03.

Part: STRUT DOOR — DELAMINATED (LT WING GEAR)

FOUND LEADING EDGE AREA OF LEFT WING GEAR UPPER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: PANEL — BROKEN (LT WING)

FOUND EDGE BROKEN ON UNDERWING REAR SPAR ACCESS PANEL. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-31-00.

Part: DOOR — DELAMINATED (LT WING GEAR)

FOUND LEADING EDGE OF LEFT WING GEAR LOWER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: PANEL — CRACKED (LT WING)

FOUND UNDERWING PANEL FORWARD OF LANDING GEAR DELAMINATED AND CRACKED. REPAIRED IAW SRM 51-40-09.

Part: SKIN — CRACKED (WS 570-590)

FOUND ONE INCH CRACK ON LOWER FLANGE, MIDPOINT ON LEFT WING LEADING EDGE BETWEEN STA 570 TO 590. REPAIRED CRACK PER SRM 57-40-03.

Part: STRUT DOOR — DELAMINATED (RT WING GEAR)

FOUND RIGHT HAND WING GEAR LOWER STRUT DOOR LOWER EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: ACCESS PANEL — DELAMINATED (LT WING)

FOUND 5TH POD ACCESS PANEL AT UNDERWING ROOT DELAMINATED. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-44-02.

Part: PANEL — CRACKED (LT WING)

FOUND OVERWING PANEL LEFT WING CRACKED. PANEL REPAIRED IAW SRM 51-40-09.

Part: CASCADE VANE — CRACKED (NR 3 ENGINE)

FOUND NR 3 ENGINE LEFT HAND UPPERMOST CASCADE VANE CRACKED. BLENDING CARRIED OUT AND VANE REINSTALLED AS PER MM 78-32-04.

Part: PRECOOLER MOUNT — CRACKED (NR 3 ENGINE)

FOUND NR 3 PRECOOLER LOWER AFT MOUNT CRACKED. REPAIRED AS PER MM 36-10-02.

Part: PANEL — PUNCTURED (VERT FIN)

FOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

FOUND RT INBOARD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED IAW SRM 51-40-06.

Part: FRAME — CRACKED (WS 570-590)

FOUND CRACKED FRAME IN INBOARD LEADING EDGE BETWEEN STA 570 TO 590 AT LOWER CENTER POSITION. REPAIRED IAW SRM 51-40-03.

Part: PANEL — BROKEN (WS 1351)

FOUND UNDERWING PANEL AT STA 1351 BROKEN AT FORWARD EDGE. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-31-00.

Part: WEIGHT — CORRODED (LT ELEVATOR)

FOUND LT OUTBOARD ELEVATOR WEIGHT AT STA 281.8 WITH LEVEL ONE CORROSION. REMOVED CORROSION, FOUND WITHIN LIMITS, REF SRM 51-20-03.

Part: DOOR — DELAMINATED (NR 2 AFT FAIRING)

FOUND NR 2 AFT FAIRING DOOR DELAMINATED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 54-32-01.

Part: FAIRING — CRACKED (NR 1 TE FLAP)

FOUND NR 1 T/E FLAP TRACK MOVEABLE CANOE FAIRING CRACKED AT TWO LOCATIONS. REPAIRED IAW SRM 51-40-09.

Part: BRACKET — CRACKED (APU COMPT)

FOUND APU COMPARTMENT BRACKETS AT BS 2710 TO 2716 CRACKED. REPLACED BRACKET IAW MM 51-10-03.

Part: WEIGHT — CORRODED (RT ELEVATOR)

BALANCE WEIGHT ON RT OUTBOARD ELEVATOR STA 306.8 HAD LEVEL 1 CORROSION. CORROSION REMOVED AND FOUND WITHIN LIMITS, REF SRM 51-20-03.

Part: PANEL — CRACKED (RT WING TE)

FOUND TRAILING EDGE FIXED PANEL CRACKED. REPAIRED AND REFITTED IAW SRM 57-30-O4.

Part: STRUT — BROKEN (WATER TANK)

FOUND LOWER HORIZONTAL STRUT FOR POTABLE WATER TANK BROKEN. NEW STRUT INSTALLED IAW IPC 38-11-02.

Part: PANEL — CRACKED (RT WING TE)

FOUND UPPER WING TRAILING EDGE PANEL CRACKED FORWARD OF NR 7 SPOILER. REPAIRED IAW SRM 51-40-09.

Part: MOUNTING RING — DAMAGED (WATER TANK)

FOUND MOUNTING RING FOR POTABLE WATER TANK DAMAGED. REPAIRED IAW SRM 38-10-01.

Part: PANEL — DELAMINATED (RT WING)

FOUND UPPER PANEL RIGHT WING DELAMINATED AFT OF NR 19 L/E FLAP. REPAIRED IAW SRM 51-40-09.

Part: PANEL — PUNCTURED (RT AILERON)

FOUND OUTBOARD AILERON UPPER ACCESS PANEL PUNCTURED. REPAIRED AND REINSTALLED IAW SRM 51-40-09.

Part: MOUNT PLATE — CRACKED (NR 4 TT2 SENSOR)

FOUND NR 4 TT2 SENSOR MOUNT PLATES CRACKED. PLATES REPLACED ND SENSOR, REINSTALLED AS PER MM 73-21-04. LEAK CHECK SATISFACTORY.

Part: SKIN — CORRODED (RT WING)

FOUND UPPER WING SKIN WITH LEVEL ONE CORROSION AT WBL 520 CENTER SPAR AREA. CLEANED AND TREATED, FOUND WITHIN LIMITS OF 51-10-01.

Part: SKIN — DELAMINATED (NR 8 SPOILER)

FOUND NR 8 SPOILER AFT EDGE DELAMINATED AT UPPER SKIN. REPAIRED IAW SRM 51-40-06.

Part: PANEL — CRACKED (RT WING)

FOUND FIBERGLASS PANEL FORWARD OF NR 8 SPOILER CRACKED AT WBL 353. REPAIRED IAW SRM 51-40-09.

Part: BRACKET — CRACKED (APU DOOR)

FOUND LHS APU COWL DOOR FIRE DETECTOR BRACKET CRACKED. BRACKET REPLACED AND INSTALLED IAW MM 51-10-03.

Part: SEAT TRACK — CRACKED (LT COCKPIT)

FOUND PILOT'S AFT INBOARD SEAT TRACK CRACKED, CRACK CONTAINED BY STOP HOLES ON BOTH SIDES. REPLACED SEAT TRACK IAW MM 25-11-01, OPS CHECK OK.

Part: BRACKET — CRACKED (NR 3 PYLON)

NR 3 PYLON FIRE EXTINGUISHER BOTTLE AT SUPPORT BRACKET CRACKED, ON INBOARD END. MANUFACTURED AND INSTALLED REPAIR PARTS PER BOEING SRM 54-11-03.

Part: CASCADE VANE — CORRODED (NR 3 ENGINE)

NR 3 ENGINE, OUTBOARD NR 7 AND NR 8 CASCADE VANES CORRODED. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: CASCADE VANE — CORRODED (NR 3 ENGINE)

NR 3 ENGINE OUTBOARD NR 5 CASCADE VANE HAS CORROSION AND BROKEN VANE. BLENDED BROKEN VANE AND CORRODED SURFACE PER BOEING SRM 51-10-01.

Part: PANEL — PUNCTURED (VERT STAB)

HOLE IN AFT WEB OF VERTICAL STABILIZER AT THE OPENING FOR THE UPPER RUDDER ACTUATOR. REMOVED DAMAGED AREA AND REPAIRED PER BOEING SRM 51-40-3.

Part: PANEL — DELAMINATED (HORIZ STAB)

LEFT HAND HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL, JUST OUTBOARD OF ELEVATOR ACTUATOR DELAMINATED THREE PLACES. REPAIRED PANEL IAW 51-40-06.

Part: SKIN — CORRODED (FS 759-800)

CORROSION LOWER FUSELAGE SKIN STA 750 TO 800. REMOVED CORRODED AREA AND REPAIRED IAW SRM 53-30-03.

Part: DOUBLER — CRACKED (RT MLG DOOR)

CRACKED DOUBLER, RIGHT WING GEAR FLYING DOOR LEADING EDGE. REPAIRED PER BOEING SRM 52-80-00.

Part: CASCADE VANE — CORRODED (NR 3 ENGINE)

NR 3 ENGINE, INBOARD NR 15 AND 17 CASCADE VANE CORRODED. BLENDED OUT CORROSION PER BOEING SRM 51-10-01.

Part: BRACKET — CRACKED (NR 3 ENGINE)

SUPPORT BRACKET CRACKED, NR 3 ENGINE BLEED AIR RELIEF VALVE, 9 O'CLOCK POSITION. WELD REPAIRED PER BAC5975.

Part: SKIN — DETERIORATING (RT WING LE)

RIGHT HAND WING LEADING EDGE BOTTOM AT ROOT, PREVIOUS REPAIR DETERIORATING TO COMPOSITE CORE. REPAIRED RIGHT HAND WING LEADING EDGE BOTTOM AT ROOT PER SRM 51-40-12.

Part: FAIRING — BROKEN (BS 1239)

LEFT LOWER WING TO BODY FAIRING 191KL BROKEN AND DELAMINATED. APPROX STATION 1239 AFT UPPER CORNER. REPAIRED AREA I/A/W SRM 51-40-15.

Part: EXHAUST STRUT — CRACKED (NR 2 ENGINE)

DURING B-CHECK INSPECTION, FOUND CRACKS AT EXHAUST STRUT POSITIONS 2, 3, 4, 5, 12 AND 15. ENGINE SCHEDULED FOR 100 HOUR REPEAT INSPECTIONS PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-02.

Part: BOLTS — SHEARED (UPPER RUDDER)

ON APPROACH, NR 1 HYDRAULIC SYSTEM SHOWED DECREASING QUANTITY, WENT TO ZERO AFTER LANDING. TOWED AIRCRAFT FROM RUNWAY DUE TO LOSS OF NOSE WHEEL STEERING. FOUND SHEARED BOLTS RETAINING FILTER ON UPPER RUDDER PACKAGE. REPLACED BOLTS, LEAK CHECK OK.

Part: CARD — SHORTED (COCKPIT)

ON PREFLIGHT INSPECTION SAW AND SMELLED SMOKE IN THE COCKPIT. DETERMINED THAT SMOKE WAS FROM MASTER DIM AND TEST MODULE. REPLACED CARD CHECKED OK.

Part: TE PANEL — TORN (NR 9 SPOILER)

B-CHECK INSPECTION, RIGHT WING NR 9 SPOILER HAS A 6 INCH BY 5 INCH TEAR IN TRAILING EDGE 20 INCHES FROM INBOARD EDGE. REPAIRED IAW BOEING SRM 51-10-06 AND 57-50-05. TOTAL CYCLES 18,040.

Part: SILL — CORROSION (CARGO COMPT)

B-CHECK INSPECTION, FOUND CORROSION ON FORWARD CARGO COMPARTMENT LOWER SILL (LEVEL 1). REMOVED CORROSION AND TREATED IAW WITH BOEING SRM 51-10-01. AIRCRAFT TOTAL CYCLES 18,040. (M)

Part: DOUBLER — CRACKED (NAC STA 180)

ON B-CHECK INSPECTION, FOUND CRACK IN DOUBLER PLATE NACELLE STATION 180, ON 4 PYLON INBOARD. INSTALLED REPAIR DOUBLER IAW SERVICE BULLETIN 54-2034 REV 4. TOTAL CYCLES 18,040.

Part: PANEL — DELAMINATED (NR 5 SPOILER)

B-CHECK INSPECTION, LEFT WING TOP SIDE PANEL FORWARD AT NR 5 SPOILER DELAMINATED. REPAIRED IAW BOEING SRM 51-40-06. TOTAL CYCLES 18,040.

Part: NR 3 BEARING — CRACKED (NR 3 ENGINE)

ON ARRIVAL IN LAX, POST FLIGHT INSPECTION REVEALED OIL IN TAILPIPE ON NR 3 ENGINE. AFTER TROUBLESHOOTING, FOUND OIL LEAKING NR 3 BEARING HOUSING. AIRCRAFT THREE ENGINE FERRY TO SAT FOR ENGINE CHANGE. (W)

Part: BRAKE ASSY — FAILED (NR 2 POSITION)

ON WALKAROUND FOUND NR 2 BRAKE COMING APART. REPLACED BRAKE AND WHEEL ASSEMBLY. PERFORMED INSPECTION PER BOEING MM 5-51-09, NO DAMAGE TO AXLE NOTED. (W)

Part: WIRE — FAILED (FUEL SHUTOFF)

NR 3 ENGINE FUEL SHUTOFF VALVE INTRANSIT LIGHT ON BRIGHT, ENGINE CONTINUED TO RUN. REPLACED ALL FUSELAGE FUEL SHUTOFF VALVE WIRING (PREVIOUSLY REPLACED ALL WING SHUTOFF VALVE WIRING). REPLACED FUEL SHUTOFF VALVE ACTUATOR AND INDICTION RELAY PRECAUTIONARY.

Part: FUEL SHUTOFF VLV — FAILED (NR 3 ENGINE)

FLT 81 - HNL - ON CLIMB-OUT NR 3 ENGINE FUEL SHUTOFF VALVE INTRANSIT LIGHT ILLUMINATED BRIGHT, ENGINE SHUT DOWN. REWIRED VALVE CIRCUIT WIRING FROM WING ROOT TO VALVE. REPLACED FUEL SHUTOFF VALVE ACTUATOR MOTOR. SYSTEM CHECKED NORMAL. (M)

Part: F/E MODULE CARD — DEFECTIVE (NR 3 ENGINE)

EN ROUTE FROM LAX FL 33, NR 3 ENGINE VALVE LIGHT INDICATED BRIGHT, ENGINE FAILED. AFTER FAILURE EXCESSIVE VIBRATION OCCURRED. AIRCRAFT TURNED BACK TO LAX. F/E FUEL CONTROL MODULE DEFECTIVE, REPLACED MODULE, REPLACED FUEL SHUTOFF VALVE ACTUATOR. OPERATIONAL CHECK OK. RETURNED TO SERVICE. (M)

Part: ACTUATOR — CRACKED (NR 7 SPOILER)

HYDRAULIC FLUID LEAK, RIGHT WING. LEAK FOUND TO BE NR 7 SPOILER ACTUATOR END CAP. REPLACED CAP LEAK. CHECK OK.

Part: SPOILER — DAMAGED (NR 2 POSITION)

JFK - ON CLIMB-OUT, SIGNIFICANT FLUTTER WAS FELT AND HEARD DURING LEFT AND RIGHT TURNS. THIS HAPPENED AFTER FLAP RETRACTED. APPEARED OKAY ON DESCENT. AT LAX, CHECKED FLIGHT CONTROLS FOR CORRECT FAIR POSITION AND OPERATION, CHECKED AUXILIARY STRUCTURE AND DOORS. CHECKED CORRECT OPERATION OF AILERON LOCKOUT SYSTEM, ALL CHECKED NORMAL. DURING FOLLOW-UP POST FLIGHT INSPECTION AT HNL, FOUND NR 2 SPOILER PANEL DAMAGED AND DAMAGE TO TRAILING EDGE FLAPS. REPLACED SPOILER AND ACCOMPLISHED INTERM REPAIRS TO LT OUTBOARD FLAP ASSY.

Part: ENGINE — FLAMED OUT (NR 4)

JUST PRIOR TO DESCENT INTO MIA AT FL 390, THE NR 4 ENGINE FLAMED OUT. THE ENGINE SHUT-DOWN CHECK LIST WAS COMPLETED AND THE IN-FLIGHT ENGINE START CHECK LIST WAS COMPLETED. THE FUEL FLOW INDICATED 3-400 POUNDS PER HOUR. ON THE FIRST TWO ATTEMPTS, THE FUEL FLOW DID NOT INCREASE, BUT EGT INCREASED WITH NO INCREASE IN N1 OR N2. ON THE THIRD ATTEMPT, AT APPROXIMATELY FL 320 AND 280 KNOTS, ENGINE RESTARTED. A NORMAL DESCENT AND APPROACH WAS MADE AT MIA. REPLACED NR 4 ENGINE FUEL FILTER, BOTH IGNITERS AND SUMPED ALL FUEL TANKS. ENGINE R/U NORMAL.