N851FT

Part: ANTENNA — MALFUNCTION (WEATHER RADAR)

RADAR SYSTEM TILT APPEARS TO POINT FULL DOWN IN SYSTEMS 1 AND 2, TESTS OK. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLACED WEATHER RADAR ANTENNA REF MM 34-43-03. OPERATIONS CHECK OK. REPLACED NR 1 R/T REF MM 34-43-02. OPS CHECK NORMAL.

Part: ANGLE — CRACKED (BS 2000 & 2100)

BULK CARGO COMPARTMENT AT STA 2000/2100L ATTACH ANGLES FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51-30-02.

Part: INTERCOSTAL — BROKEN (BS 570)

FWD CARGO COMPARTMENT AT STATION 570 RBL 30 TO 35 FOUND BROKEN INTERCOSTAL. REMOVED AND REPLACED PER SRM 51-10-01 AND SRM 51-30-02.

Part: ANGLE — CRACKED (BS 1960-1980)

BULK CARGO PIT AT STATION 1960 TO 1980 BL 22L ATTACH ANGLE FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51-30-02.

Part: SEAT TRACK — CORROSION (BS 520-740)

LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK BS 520L TO 740L. REPLACED SEAT TRACK FROM BS 520L TO 740L FOR CONVIENENCE PER SRM 53-10-21 PG 45.

Part: PANEL — CRACKED (LT WING)

LEFT WING PANEL FWD OF LEFT FLYING PANEL HAS CRACK. REPAIRED PER SRM 51-40-09 AND 51-24-11.

Part: ANGLE — CRACKED (BS 1940)

BULK CARGO STA 1940 BL 22L ATTACH ANGLE FOUND CRACKED. REPAIRED PER SRM 51-01-01, 51-30-02 AND 51-40-04.

Part: SEAT TRACK — CORRODED (BS 520-720)

LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK AT BS 520R TO 720R. REPLACED FOR CONVIENENCE PER SRM 52-10-21 PG 45.

Part: INTERCOSTAL — DAMAGED (BS 1720-1740)

AFT CARGO BULK PIT BS 1720L TO BS 1740L SPACING RIB DAMAGED. REPAIRED PER SRM 51-10-01.

Part: FLOOR — DELAMINATED (BS 720)

REPLACED UPPER DECK FLOOR PANELS AT BS 720R DUE DELAMINATION. REMOVED AND REPLACED PER SRM 53-22-01, 51-10-01 AND 51-30-02.

Part: ANGLE — CRACKED (BS 1960)

BULK PIT STA 1970/1980 BL 22R ATTACH ANGLE HAS CRACK. REMOVED AND REPLACED PER SRM 51-10-01 AND SRM 51-30-03.

Part: ANGLE — CRACKED (BS 200)

BULK PIT STA 2000 STR 22 SUPPORT ANGLE CRACKED. REMOVED AND REPAIRED PER SRM 51-10-01, 51-30-02 AND 51-40-04.

Part: SUPPORT — CRACKED (BS 2020)

BULK CARGO COMPARTMENT STA 1960 BLR 34 TO STA 2020 BLR 34 FLOOR PANEL SUPPORT CRACKED. REMOVED AND REPLACED PER SRM 51-30-01.

Part: CHANNEL — CRACKED (BS 2060)

BULK CARGO AREA STA 2060L SUPPORT CHANNEL HAS CRACK AT LT SIDE. REMOVED AND REPLACED PER SRM 51-40-03.

Part: SUPPORT — CRACKED (BS 2000)

BULK CARGO PIT AT STA 2000L FLOOR PANEL SUPPORT CRACKED AT TIEDOWN AREA. REMOVED AND REPLACED PER SRM 51-30-02.

Part: STRINGER — PUNCTURED (BS 1820)

UPPER DECK AT STA 1820R STR 15R FLANGE PUNCTURED. REPAIRED PER SRM 53-10-04, 51-30-02.

Part: FRAME — GOUGED (BS 2060)

UPPER DECK FRAME AT BS 2060 STR 16L FOUND GOUGE. REPAIRED PER SRM 53-10-04.

Part: CHANNEL — CRACKED (BS 1940-2060)

BULK CARGO COMPARTMENT STA 1940 TO STA 2060R SEVERAL HAT CHANNELS CRACKED. REMOVED AND REPAIRED HAT CHANNEL PER SRM 51-10-01 AND 51-30-02.

Part: FLOOR — DELAMINATED (BS 500)

FLOOR PANEL STATION 500 TO 580 RBL 20 FOUND DELAMINATED. REMOVED AND REPAIRED PER SRM 51-10-01 AND 51-30-02.

Part: FRAME — DAMAGED (BS 1740)

MAIN CABIN FRAME STATION 1740R STR 12R FOUND DAMAGED. REPAIRED DAMAGE PER SRM 53-10-04.

Part: ANGLE — CRACKED (BS 1960)

BULK CARGO COMPARTMENT AT STATION 1960 BL 50R ANGLE FOUND CRACKED. REPAIRED PER SRM 51-10-01, 53-10-03 AND 51-30-02.

Part: SUPPORT — CRACKED (BS 2080)

BULK CARGO PIT STA 2080R FLOOR PANEL SUPPORT FOUND CRACKED. REPAIRED PER SRM 51-40-03.

Part: ENGINE — FAILED (NR 1)

DURING CLIMBOUT PASSING FL120, ACFT EXPERIENCED LOUD NOISE AND SHUDDER AND FLASH OF LIGHT FOLLOWED BY INCREASE IN NR 1 ENG EGT TO 960 DEGREES. ENGINE SHUT DOWN. DUMPED FUEL AND RETURNED TO SNN. REPLACED NR 1 ENGINE PER BMM 71-00-02 AND PAC M7100-002/M7111-001, M783-007 AND M7100-001.

Part: ENGINE — FLAMED OUT (NR 2)

NR 2 ENGINE FLAMED OUT FL350. ENG RESTART AT FL 290. RESTART NORMAL. PERFORMED FUEL CONTAMINATION CHECK PER MM 73-00-00 PG 201. VERIFIED FUEL REMAIN NR 2 TANK VIA STICK 17 AT 20.0, 10,962 LBS. SUMPED TANKS FOR EVIDENCE OF WATER, VERIFIED CONDITON MOTOR OPERATIONAL. VERIFIED FUEL PUMP PRESS PER MM 76-00-46 PROCEDURE 1. CHECKED INLET AND EXHAUST FOR FOD DAMAGE. DRY MOTORED THE WET MOTORED. ENG STARTED NORMAL. CHECK AND REPLACE FUEL FILTER, NO CONTAMINATION FOUND ALL CHECK NORMAL.

Part: WIRE — CHAFED (FE PANEL)

REJECTED TAKEOFF FROM RTA DUE TO AFT CARGO FIRE INDICATION AND FIRE BELL DURING T/O ROLL. PARKED AND INSPECTED FOR FIRE. NO SMOKE OR FIRE NOTED. TRANSFERED TO DMI NR 20623 AND 20624. REMOVED AND REPLACED SMOKE DETECTOR PANEL P-4 FOR T/S PER MM 26-16-00 DMI OK TO CONTINUE. LOWER CARGO FIRE DETECT LIGHT INTERMIT DURING TURBULENCE AND LANDING AT JFK. FOUND CHAFFED WIRE BEHIND F/E PANEL. REPAIRED WIRING PER MM 20-10-13 CHECK OK PER 26-16-00 DMI CLEARED.

Part: STRINGER — CORRODED (BS 1000)

LEVEL 2 CORROSION RIVET SHEARED AND SKIN BULGED AT BS 1000 AT S-42L. CORROSION REMOVED AND STRINGER REPAIRED PER BOEING SRM 53-10-03 FIG 1.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION LEFT WING LOWER SKIN AT NR 1 MAIN FUEL TANK INBOARD BOOST PUMP. REMOVED CORROSION AND SHOT PEENED INSTALLED A SEALANT RAMP PER BOEING TELEX PAO-HKG-98-0093TE AND HAECO REPAIR SCHEME R-57-26-33741.

Part: SKIN — DENTED (BS 2598)

DENT AFT FUSELAGE SKIN AT PREVIOUS REPAIR FORWARD AND AFT OF BS 2598 JACK POINT. REPAIRED PER BOEING SRM 53-30-03 FIG 1A.

Part: SKIN — DENTED (BS 1780-1800)

DENT IN THE LOWER FUSELAGE AT BS 1780 TO 1800 S35R TO S36R. REPAIRED PER BOEING SRM 53-30-03 FIG 1.

Part: SKIN — DENTED (SERVICE DOOR)

DENT ON UPPER DECK CREW SERVICE DOOR AFT EDGE MID PORTION. REPAIRED PER BOEING SRM 52-00-03 FIG 3.

Part: FRAME — CRACKED (BS 360)

CRACKED FRAME WEB BS 360 S-23L. REPAIRED PER BOEING TELEX PAO=HKG-98-0109RE/0099TE AND HAECO REPAIR SCHEME R-53-12-33724.

Part: FRAME — CRACKED (BS 380)

CRACKED FRAME WEB AND DOUBLER AT BS 380 S-24L. REPAIRED PER BOEING TELEX PAO-HKG-98-106TE/0116RE AND HAECO REPAIR SCHEME R-53-12-33742.

Part: STIFFENER — DEFORMED (BS 460)

DEFORMED UPPER DECK FLOORBEAM ATTACH VERTICAL STIFFENERS AT BS 460 RBL 55 AND RBL 74. REPLACED STIFFENERS PER BOEING SRM 51-10-01.

Part: SKIN — CORRODED (LT WING)

LEVEL 2 CORROSION LEFT WING LEADING EDGE SKIN PANEL AT FSSO 1486. REPAIRED PER BOEING SRM 57-30-03 FIG 4.

Part: MOUNT — WORN (NR 1 ENGINE)

NR 1 ENGINE FORWARD UPPER ENGINE MOUNT INBOARD HANGER FITTING INNERMOST LUG WAS PREVIOUSLY REWORKED AND BUSHIN MIGRATED OUT. SPOT FACED THE LUG, SHOT PEENED THE REWORKED SURFACE, REWORKED THE BUSHING AND INSTALLED WITH NEW WASHER PER BOEING TELEX PAO-HKG-98-0121RE/0105TE AND HAECO REPAIR SCHEME R-53-13-33725.

Part: CASE — CRACKED (NR 1 ENG EXH)

NR 1 ENGINE TURBINE EXHAUST CASE CRACKED, FLANGE AT 10 O'CLOCK POSITION. REPLACED CASE PER P AND W OVERHAUL MANUAL 72-00-00.

Part: FRAME — CRACKED (NR 1 PYLON)

NR 1 PYLON RIGHT FRAME AT NAC STN 168 CRACKED AND LEFT FRAME AT NAC STN 193 FOUND CHAFED. REPLACED FRAMES PER BOEING SRM 51-10-01.

Part: STRINGER — CRACKED (BS 380-400)

CRACKED STRINGER S-24L AT BS 380 TO 400. REPLACED STRINGER PER BOEING SRM 51-10-01.

Part: SKIN — DAMAGED (NR 1 PYLON)

NR 1 PYLON LEFT OUTER SKIN AT NAC STN 220 AND RT SKIN AT STN 233 FOUND DAMAGED. REPAIRED PER BOEING SRM 54-30-03.

Part: FRAME — CRACKED (BS 1375)

CRACKED FRAME WEB AT LEFT WING LANDING GEAR WHEEL WELL BS 1375 S-32L. REPAIRED PER BOEING TELEX PAO-HKG-98-0091TE/0108RE AND HAECO REPAIR SCHEME R-53-42-33743.

Part: WEB — CRACKED (BS 360-380)

MAIN DECK BS 360 TO 380 RT WEB FOUND CRACKED AT S-32R. WEB REPAIRED PER BOEING SRM 51-40-01.

Part: SKIN — CORRODED (BS 820-840)

LEVEL 2 CORROSION AT UNDERSIDE OF ANTENNA 10 AFT OF CENTER ELECTRONICS BAY DOOR CUTOUT BS 820 TO 840 S47L TO S47R. REMOVED CORROSION REPLACED DOUBLER PER BOEING SRM 53-30-03.

Part: DUCT — CRACKED (NR 2 COWLING)

NUMBER 2 ENGINE RT SIDE COWL BREATHER EXHAUST DUCT CRACKED AT FLANGE RADIUS. WELD REPAIRED PER BAC 5975 REV L.

Part: WEB — CRACKED (BS 320-340)

M/D B/S 320-340 LT SIDE FLOOR SUPPORT WEB FOUND CRACKED AT S26L AREA. FLOOR SUPPORT WEB REPLACED AS PER SRM 51-10-01.

Part: FLAP TRACK — CORRODED (LT TE MIDFLAP)

AFTER REMOVAL OF BEARING FROM L/W I/B MIDFLAP O/B SLIDING TRACK FWD ATTACH CORROSION FOUND IN BORE. TRACK REPAIRED IAW OHM 57-52-35.

Part: FAIRING — PUNCTURED (RT WING)

RIGHT WING NR 5 CANOE FAIRING TAIL CONE PUNCTURED. REPAIRED IAW SRM 51-40-15.

Part: WEB — CRACKED (LT TE FOREFLAP)

LEFT WING I/B FOREFLAP I/B WEB FOUND CRACKED. REPAIRED AS PER SRM 51-10-01.

Part: FITTING — CORROSION (LT TE FOREFLAP)

FOUND LEVEL 1 SURFACE CORROSION ON LEFT WING I/B FOREFLAP LOWER SURFACE CENTER AND O/B NR 3 SEQUENCE CARRIAGE FITTING AREA AFTER FOREFLAP REMOVAL. CORROSION REMOVED AND AREA REPROTECTED IAW SROM 51-10-01 AND 51-10-02.

Part: FAIRING — PUNCTURED (RT TE FLAP)

RIGHT WING NR 5 FLAP FIXED FAIRING FOUND 2 PUNCH HOLES. REPAIRED IAW SRM 51-40-15.

Part: COWL — DAMAGED (NR 1 ENGINE)

NUMBER 1 ENGINE LEFT SIDE COWL FORWARD UPPER EDGE DAMAGED. REPAIRED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 360-380)

MAIN DECK LEFT OUTBOARD FLOOR INTERCOSTAL FOUND CRACKED BS 360-380 S26L. INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01.

Part: ANGLE — CRACKED (LT TE MIDFLAP)

LEFT WING INBOARD MIDFLAP INNERMOST RIB AFT ATTACHMENT ANGLE FOR AFT ACCORDIAN SEAL FITTING CRACKED AT LOWER BOLT HOLE. ANGLE REPLACED IAW SRM 51-10-01.

Part: SUPPORT — DELAMINATED (LT TE FOREFLAP)

LEFT WING INBOARD FOREFLAP UPPER T/E SUPPORT DELAMINATED (INBOARD OF NR 4 FLAP TRACK). REPAIRED IAW SRM 51-40-15.

Part: INTERCOSTAL — CRACKED (BS 380-400)

MAIN DECK LEFT OUTBOARD INTERCOSTAL FOUND CRACKED BS 380-400 S26L. FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01.

Part: FAIRING — CRACKED (NR 2 PYLON)

NUMBER 2 PYLON LEFT SIDE SKIRT FAIRING AT NAC STA 153 CRACKED. REPAIRED AS PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 360-380)

MAIN DECK RIGHT OUTBOARD FLOOR INTERCOSTAL CRACKED BS 360-380 S26R. INTERCOSTAL REPLACED AS PER SRM 51-10-01.

Part: STRINGER — CRACKED (BS 520-740)

MAIN DECK STRINGER R19 HAS CRACKED STRINGER HOLES, BS 520-560, 600-620, 640-660 AND 720-740. STRINGER 19R REPLACED FROM BS 520-BS 741 AS PER SRM 51-10-01 AND 53-10-03.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION FOUND ON LEFT WING UPPER T/E WING SKIN EXTENSION AT WBL 515, OUTBOARD OF INBOARD AILERON. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01, 51-10-02.

Part: COWL — PUNCTURED (NR 2 ENGINE)

NUMBER 2 ENGINE RT SIDE COWL SKIN PUNCTURED AT 3 O'CLOCK POSITION. SKIN REPAIRED AS PER SRM 51-40-02.

Part: FITTING — RUSTY (CARGO DOOR)

AFT CARGO DOOR NR 9 LATCH FITTING FOUND RUSTY ON BORE PIN AREA. SURFACE RUST CLEANED AND LATCH FITTING REPLACED REF SB 747-52-2186.

Part: SKIN — CORROSION (LT WING)

LEVEL 1 CORROSION FOUND ON UPPER WING SKIN EXTENSION AT ILES 374. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01, 51-10-02.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

LEFT WING INBOARD FOREFLAP L/E, OUTBOARD OF NR 3 FLAP TRACK DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: STRINGER — CORRODED (BS 1580-1600)

LEVEL 1 CORROSION AT AFT CARGO COMPARTMENT STR S46R STA 1580-1600. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02.

Part: STRINGER — CORRODED (BS 1540-1560)

LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT AT STR S46R STA 1540-1560. CORROSION REMOVED AND REPROTECTED AREA PERSRM 51-10-01 AND 51-10-02.

Part: STRINGER — CORRODED (BS 1480-1500)

LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46L STA 1480-1500. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORROSION (FUSELAGE)

LEVEL ONE CORROSION FOUND ON PANEL 193KK. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SPAR WEB — CORRODED (LT WING)

LEVEL 1 CORROSION FOUND ON AFT SPAR LWR WEB AT ATTACHMENT OF BONDING LEAD OF NR 2 AFT BOOST PUMP. REPAIRED CORROSION PER SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

LEFT WING INBOARD FOREFLAP INBOARD EDGE LOWER SURFACE DELAMINATED. REPAIRED IAW SRM 51-40-06.

Part: ANGLE — CRACKED (BS 770)

FWD CARGO COMPT SUPPORT ANGLE AT STA 770 LBL 20-30, FOUND DEFORMED AND CRACKED. SUPPORT ANGLE REFORMED PER SRM 51-40-01.

Part: ANGLE — CRACKED (NR 1 PYLON)

NR 1 ENG HYDRAULIC RESERVOIR INBD AND OUTBD SUPPORT ANGLE CRACKED AT MID AREA. REPAIRED PER SRM 51-30-02.

Part: STRINGER — CORRODED (BS 1520-1540)

LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46R STA 1520-1540. CORROSION REMOVED AND REPROTECTED AREA PER SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CORRODED (BS 1480-1500)

LEVEL 1 CORROSION FOUND IN AFT CARGO COMPT AT STRINGER S40L STA 1480-1500. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORROSION (FUSELAGE)

LEVEL ONE CORROSION FOUND ON PANEL 191S. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CORRODED (BS 1480-1500)

LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46L STA 1480-1500. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — DELAMINATED (FUSELAGE)

PANEL 191P LEFT FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER SRM 51-40-15.

Part: FAIRING — BROKEN (RT VERT STAB)

RT STABILIZER ROOT UPPER FAIRING FWD EDGE BROKEN. FIBERGLASS REPAIRED PER SRM 51-40-15 AND 51-24-11.

Part: PANEL — CORRODED (L1 DOORWAY)

MAIN DECK 1L DOOR AFT CUTOUT PANEL FOUND SLIGHT CORROSION ADJACENT TO CENTER GUIDE TRACK FITTING MOUNTED AREA. CORROSION REMOVED AND REPROTECTED AREA PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DAMAGED (RT LE FLAP)

RT WING NR 16 KRUEGER FLAP CAVITY FWD CUTOUT FOUND CRACK AT ILES 542. REPAIRED IAW SRM 51-40-03 FIG 1.

Part: BULKHEAD — CRACKED (NLG WW)

LEFT AND RIGHT NLG WHEEL WELL FORWARD CORNERS CANTED BULKHEAD AND SIDEWALL LOWER CHORD FOUND CRACKED. REPAIRED AS PER SB 747-53-2112.

Part: FLOOR — CORROSION (BS 460)

LEVEL 1 CORROSION FOUND UNDER FLOOR RIGHT HAND SIDE STA 460 WBL R199.8. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORROSION (FUSELAGE)

LEVEL 1 CORROSION FOUND ON PANEL 191S. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: FRAME — CORRODED (BS 400)

FWD E/E COMPT RT CORRODED RIVETS AND FRAME AT STA 400 BLKHD FWD FACE BWL 150-118 LHR OF RH TUNNEL. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (LT WING)

LEVEL 1 CORROSION FOUND ON LT WING L/E UPPER INSPAR WING SKIN. CORROSION REMOVED AND AREA REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: STRINGER — CORRODED (BS 1500-1520)

LEVEL 1 CORROSION FOUND AT AFT CARGO COMPARTMENT STR S46R STA 1500-1520. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SPLICE — CRACKED (BS 1241)

RIGHT SIDE BS 1241 BH SPLICE STRAP CRACKED AT FWD HOLE THROUGH THICKNESS RUNNING AFT. MODIFIED PER SB 747-53-2283.

Part: SKIN — PEELING (LT ELEVATOR)

EMP - LT INBD ELEVATOR T/E O/B AREA UPPER SURFACE COATING PEELING. REPAIRED PER SRM 51-10-01, 51-10-02.

Part: COWL — DAMAGED (NR 1 ENGINE)

NR 1 ENG RT SIDE COWL 7TH FRAME FROM FRONT HAS SEGMENT OF REINFORCING PLATE MISSING AT THE UPPER MOST ENT. PLATE REPLACED IAW SRM 51-10-01.

Part: FAIRING — BROKEN (LT HORIZ STAB)

EMPENNAGE LEFT STABILIZER ROOT UPPER FAIRING FORWARD EDGE BROKEN. REPAIRED AS PER SRM 51-40-15.

Part: SKIN — DELAMINATED (TE FOREFLAP)

IB FORE FLAP O/B LWR SURFACE DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: BASE — CORRODED (RUDDER)

LEVEL 1 CORROSION FOUND UPPER RUDDER NR 1 STATIC DISCHARGER BASE. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SPAR CHORD — CORRODED (WS 822-840)

LEVEL 1 CORROSION ON RT WING LOWER CHORD SURFACE AT FSS 822-840. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (PAX DOOR)

RIVETS CORRODED FWD UPPER CORNER FWD OF NR 1 LT ENTRY DOOR. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02 AND PAINTED PER 570-26-11.

Part: FAIRING — DELAMINATED (NR 2 PYLON)

NR 2 PYLON V FAIRING IS DELAMINATED. REPAIRED IAW SRM 51-40-06 FIG 17.

Part: SPLICE — CRACKED (BS 1241)

BS 1241 LEFT SIDE B/H SPLICE STRAP CRACKED AT FWD HOLE RUNNING AFT THROUGH THICKNESS. MODIFIED PER SB 747-53-2283.

Part: FAIRING — DELAMINATED (NR 3 CANOE)

LT WING NR 3 CANOE FAIRING AREA OF DELAMINATION ON I/B SIDE. REPAIRED IAW SRM 51-40-15.

Part: BRACKET — CRACKED (BS 1335)

RT WING GEAR WW BRACKET CRACKET BELOW GEAR OPP SEQUENCE VALVE AT DOOR CUTOUT STA 1335. BRACKET REPLACED PER SRM 51-10-01.

Part: SKIN — DELAMINATED (LT TE MID FLAP)

LT WING INBOARD MID FLAP L/E DELAMINATED BETWEEN 3 AND 4 FLAP TRACKS. FIBERGLASS REPAIR PER SRM 51-40-15.

Part: BRACKET — CRACKED (RT PNEU DUCT)

PNEUMATIC DUCT RT PRESS TRANSMITTER SUPPORT BRACKET CRACKED. SUPPORT BRACKET REPLACED PER SRM 51-10-0.

Part: COWL — DISBONDED (NR 1 ENGINE)

NUMBER 1 ENG LT FAN COWL INNER SKIN IS DISBONDED AT THE BOTTOM EDGE. HOT BOND REPAIR C/OUT IAW SRM 51-40-06 FIG 17A.

Part: COWL — DISTORTED (NR 2 ENGINE)

NR 2 ENG RT SIDE LOWER CHORD IS DISTORTED AT THE GUIDE PIN ARE JUST FWD OF NR 4 U BOLT. REPAIRED IAW SRM 51-10-02, 51-10-02 AND MM 71-11-06.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION RT WING UPPER SKIN AT SEVERAL LOCATIONS FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: FAIRING — DELAMINATED (NR 1 CANOE)

LT WING NR 1 CANOE FAIRING O/B SIDE DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: COLLAR — CORRODED (NLG STEERING)

LEVEL 1 CORROSION ON NOSE LANDING GEAR COLLAR ASSY IN FRONT OF LT STEERING. AREA CLEANED AND CORROSION REMOVED PER SRM 51-10-01 AND 51-26-11.

Part: SKIN — CORRODED (BS 1168-1548)

LEVEL 1 CORROSION UPPER SKIN SURFACE SEVERAL LOCATIONS BS 1168 TO 1548. REMOVED CORROSION IAW SRM 51-10-01 AND PROTECTIVE FINISH APPLIED IAW SRM 51-14-11.

Part: CLAMP — CORRODED (NR 3 AIR DUCT)

NR 3 TRIM AIR DUCT CLAMP AROUND COUPLING INBD OF PAC VALVE CORRODED. CLAMP REPLACED IAW MM 36-11-01.

Part: STRUCTURE — CORRODED (BS 2436-2460)

LEVEL 1 CORROSION EMP COMPT BS 2436-2460 RT WL 334-350 AREA STR AND SUPPORT ROD. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: STRUCTURE — CORRODED (BS 2460-2484)

EMP CMPT STA 2460-2484 WL 366 CTR AREA SLIGHT CORROSION. CORROSION REMOVED AND REPROTECTED PER SRM 51- 10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

LT WING INBOARD FORE FLAP L/E DELAMINATED IN 3 AREAS BETWEEN NR 3 AND NR 4 FLAP TRACKS. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON RT WING LOWER SURFACE AT WBL 1140. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CRACKED (RT WING)

RT WING PANEL 671BT FOUND CRACK AT FASTENER HOLE. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION UPPER RT WING SKIN WS 614 TO 862 FRONT SPAR TO MID SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-02 AND MM 51-14-11.

Part: SKIN — DELAMINATED (LT TE MIDFLAP)

LT WING INBD MID FLAP OUTBD L/E AND LWR SURFACE DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORROSION (WS 862)

LEVEL 1 CORROSION RT WING UPPER SKIN SURFACE WS 862 TO 1168 FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: DOOR — CRACKED (RT MLG)

RT BODY GEAR DOOR 762, FOUND CRACK ON AFT FACE. DOOR REPAIRED PER SRM 51-40-03.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION RT WING UPPER SKIN FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-20 AND MM 51-14-11.

Part: SKIN — CORRODED (BS 760)

LEVEL 1 CORROSION ON RIVETS AND LIGHT SURFACE CORROSION AROUND RIVETS AT STA 760 STR 7A, 10 AND 11. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

LEFT WING INBOARD AFT FLAP OUTBOARD LOWER EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: FAIRING — DELAMINATED (NR 2 CANOE)

LT WING NR 2 CANOE FAIRING O/B SIDE DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: DUCT — CRACKED (NR 2 PACK)

NR 2 PACK DUCT CRACKED AT DISCHARGE TEMP SENSOR BOSS. DUCT REMOVED FOR WELDING PER OHM 36-10-04 REV 66. DETAILS REF FORM 8130-3.

Part: SKIN — CORRODED (BS 520-740)

LEVEL 1 CORROSIN MD BS 520-740 S19L LAP JOINT INNER SURFACE. REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: HINGE — CORRODED (CARGO DOOR)

LOWER FUSELAGE AFT CARGO DOOR HINGE SURFACE CORROSION AT FWD SIDE AND AFT SIDE. REMOVED CORROSION FROM DOOR HINGE AREA AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CRACKED (NR 1 ENGINE)

CRACKED CASCADE SUPPORT RING UPPER END. BLENDED OUT CRACK PER BOEING SRM 51-10-01 AND REPROTECTED PER 51-10-02.

Part: PANEL — DENTED (VERT STAB)

VERTICAL STABILIZER PANEL 321D DENT FOUND. REPAIRED PANEL PER SRM 51-40-01.

Part: FAIRING — DAMAGED (NR 7 TE FLAP)

RIGHT WING NR 7 T/E FLAP FWD FIXED FAIRING PUNCH MARK FOUND. REPAIRED IAW SRM 51-40-15.

Part: PANEL — DAMAGED (RT WING)

RT WING PANEL 672DB HAS 2 HOLES. REPAIRED PER SRM 51-40-15.

Part: FAIRING — DELAMINATED (LT TE FOREFLAP)

LT WING OUTBOARD FORE FLAP L/E OB OF NR 2 CANOE FAIRING DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: LONGERON — CORRODED (BS 1330-1338)

LEVEL 1 CORROSION ON RT WING WW O/B LONGERON LOWER CHORD UPPER SURFACE BS 1330-1338. CORROSION REMOVED PER SRM 51-10-01, 51-10-02.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

LEFT WING OUTBOARD FOREFLAP INBOARD LEADING EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: STRUCTURE — CORRODED (BS 340-360)

LEVEL 1 CORROSION FOUND ON MLG CAVITY AT RT SIDE BETWEEN STA 340-360 BWL 119 TO BWL 180. REMOVED CORROSION PER SRM 51-10-01 AND SRM 51-10-02. PAINTED PER MM 51-26-11.

Part: DOOR — CRACKED (APU COMPT)

APU LT COMPARTMENT ACCESS DOOR LOWER FLANGE SLIGHTLY CRACKED AND LIFTED UP BETWEEN NR AND NR 4 VERTICAL FRAME. REPAIRED DOOR FLANGE PER SRM 51-10-01 AND 51-10-02.

Part: FITTING — CRACKED (NLG DOOR)

NLG W/W RT FWD DOOR FWD HINGE FITTING FWD ANGLE FOUND CRACK. 'T' ANGLE REPAIRED FROM BS 220-280 AT RT SIDE WALL LOWER PR HX R.S. R 53-18-33745.

Part: PANEL — DELAMINATED (RT WING)

RT WING UPPER T/E PANEL FOUND DELAMINATED AT WBL 1160. REPAIRED IAW SRM 51-40-15.

Part: DOOR — CRACKED (APU COMPT)

APU LT COMPARTMENT ACCESS DOOR FWD LOWER FLANGE BENT AND CRACKED AND 1 RIVET MISSING. DOOR REPAIRED PER SRM 51-40-02.

Part: COWL — SPLIT (NR 2 ENGINE)

NR 2 ENG RT SIDE COWL INNER SKIN HEAT SHIELD IS SPLIT BETWEEN 4 AND 5 FRAME. REPAIRED PER SRM 54-30-03 FIG 14.

Part: COWL — DELAMINATED (NR 3 ENGINE)

DELIMATED LOWER EDGE FWD AND AFT CORNERS NR 3 ENGINE RT FAN COWL. REPAIRED PER BOEING SRM 51-40-06 FIG 17.

Part: PANEL — DELAMINATED (WS 528-568)

RT WING 3 EACH T/E UPPER PANEL FOUND DELAMINATED AT WS 528-568. REPAIRED IAW SRM 51-40-15.

Part: COWL — CRACKED (NR 4 ENGINE)

CRACKED NR 4 ENGINE SIDE COWL UPPER 3.5 BLEED EXHAUST. WELD REPAIRED PER BAC 5975.

Part: PRESS WEB — CORRODED (BS 1460-1480)

LEVEL 1 CORROSION ON LT BODY LANDING GEAR WW BETWEEN BS 1460-1480 ON OUTBD WALL BWL 200. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DENTED (RT ELEVATOR)

RT I/B ELEVATOR E/B UPPER SURFACE 2 DENTS. FIBERGLASS REPAIRED PER SRM 51-40-15 AND MM 51-25-11.

Part: SKIN — DISTORTED (NR 2 PYLON)

NR 2 PYLON ACCESS PANEL 463EL IS DISTORTED AT FWD END. REMOVED AND REPLACED PANEL PER MM 54-32-00.

Part: SKIN — CORRODED (NLG DOOR)

LEVEL 1 CORROSION ON NLG RT FWD DOOR 712 ON AFT TOP INSIDE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (TE AFT FLAP)

I/B AFT FLAP LWR SURFACE DELAMINATED IN 2 AREAS. REPAIRED IAW SRM 51-40-15.

Part: ANGLE — CRACKED (LT MLG DOOR)

LT WING LANDING GEAR DOOR 733 AFT LOWER ANGLE CRACKED. AFT LOWER DOOR ATTACH ANGLE REPLACED PER SRM 51-10-01.

Part: SKIN — CORRODED (BS 1940-1980)

LEVEL ONE CORROSION FOUND AFT LOWER FUSELAGE AT STA 1940-1980 STR S51L AND S50L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 1840-1860)

LEVEL 1 CORROSION ON AFT LOWER FUSELAGE SKIN AT STA 1840-1860 STR S44L. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORROSION (BS 1000)

PANEL SUPPORT BRACKET RIB CORRODED AT STA 1000 BBL 18L AIR COND BAY. REPAIRED SUPPORT PER SRM 51-40-04.

Part: BRACKET — CRACKED (NR 1 HYD RESV)

NR 1 HYD RESERVOIR LT AFT ATTACH ANCHOR NUT SUPPORT BRACKET CRACKED. REPAIRED PER SRM 51-10-01 P 18.

Part: FRAME — CRACKED (NR 1 ENGINE)

NR 1 ENG LT SIDE COWL FOURTH FRAME FROM FRONT IS CRACKED ABOVE THE LATCH. REPAIRED PER SRM 51-10-01 P 18.

Part: PANEL — DELAMINATED (RT WING)

RT WING UPPER T/E PANEL FOUND DELAMINATED AT WBL 927. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORROSION (RT MLG DOOR)

LEVEL 1 CORROSION ON RT WING GEAR WW DOOR 742 OUTSIDE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. PAINTED PER MM 51-26-11.

Part: COWL — CRACKED (NR 4 ENGINE)

CRACKED NR 4 ENGINE SIDE COWL FWD FRAME FWD OF BREATHER DUCT. REPLACED ANGLE PER BOEING SRM 51-10-01.

Part: SKIN — CORROSION (RT MLG DOOR)

LEVEL 1 CORROSION ON RT BODY GEAR DOOR 761 AFT FACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02 AND PAINTED PER MM 51-26-11.

Part: COWL — DENTED (NR 4 ENGINE)

DENT IN NR 4 ENGINE RIGHT FAN COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-40-06.

Part: LONGERON — CORRODED (WS 1284-1301)

LEVEL 1 CORROSION ON RT WING LANDING GEAR WW LONGERON BETWEEN ST 1284 AND 1301. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (RT WING)

LEVEL 1 CORROSION RT WING UPPER SURFACE BETWEEN PANEL 671CT AND 671DT. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DELAMINATED (LT ELEVATOR)

LT INBOARD ELEVATOR T/E O/B AREA UPPER SURFACE COATING PEELING OFF. FIBERGLASS REPAIRED PER SRM 51-40-15 AND 51-26-11.

Part: SKIN — DENTED (BS 2718)

BS 2718-2728 LT UPPER FUSELAGE AREA BWL 310 SLIGHT DENT. AREA SMOOTHED PER SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02.

Part: SKIN — CORRODED (BS 1920-1940)

LEVEL ONE CORROSION FOUND AFT LOWER FUSELAGE AT STA 1920-1940 STR S38R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DENTED (VERT STAB)

VERT STAB T/E UPPER AREA HAS A DENT NEAR TOP OF UPPER RUDDER. REPAIRED PER SRM 51-40-15.

Part: PANEL — DENTED (FUSELAGE)

DENT IN LOWER FORWARD FUSELAGE AT RT JACK PAD ACCESS PANEL. REPAIRED PER BOEING SRM 51-40-15 FIG 7.

Part: SKIN — CORROSION (E/E DOORWAY)

LEVEL 1 CORROSION AROUND CTR ELECTORNICS DOOR CUTOUT. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORROSION (BS 1660)

AFT LOWER FUSELAGE CORROSION AT LT LOWER BRACKET OF PANEL 193F AT STA 1660. REMOVED CORROSION FROM BRACKET AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DENTED (VERT STAB)

VERT STAB SKIN LEFT SIDE HAS DENT NEAR L/E STA 200-220 AT 2 LOCATIONS. DENT REPAIRED PER SRM 51-40-06 AND MM 51-26-11.

Part: BRACKET — CRACKED (NR 1 PYLON)

NR 1 PYLON HYD LINE SUPPORT BRACKET AT NAC ST 190 IS CRACKED. SUPPORT BRACKET REPLACED IAW SRM 51-10-01 P 18.

Part: SKIN — CORROSION (LT AILERON)

LEVEL 1 CORROSION ON LT WING OUTBD AILERON OUTBD LOWER T/E AREA. CORROSION REMOVED PER SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — DEBONDED (NR 1 PYLON)

NR 1 PYLON ACCESS PANEL 453CL IS DEBONDED, CRACKED AND RUBBER PADS ARE MISSING FROM PANEL LATCHES. REMOVED AND REPLACED DOOR PER MM 54-32-00.

Part: SKIN — DAMAGED (LT ELEVATOR)

LT INBOARD ELEVATOR OUTBD AREA T/E DAMAGED. FIBERGLASS REPAIR PER SRM 51-40-15.

Part: INLET FLAP — CORRODED (NR 3 PACK)

NR 3 A/C PACK RAM AIR INLET FLAP SHAFT BEARINGS INBD AND OUTBD CORRODED. REPLACED NR 3 PACK RAM INLET FLAP SHAFT BEARINGS IAW FAA FORM 8130-3 REF NO 001038.

Part: SKIN — CORRODED (BS 480)

LEVEL 1 CORROSION ON SKIN AT STA 480 BWL 122 RT SIDE ABOVE LAP JOINT. CORROSION REMOVED PER SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — DENTED (LT HORIZ STAB)

LT STABILIZER ROOT UPPER SURFACE T/E FIXED PANEL HAS DENTS. FIBERGLASS REPAIRED PER SRM 51-40-15 AND MM 51-26-11.

Part: PANEL — DENTED (FUSELAGE)

DENT IN LOWER AFT FUSELAGE PANEL 293E. REPAIRED PER BOEING SRM 51-40-15.

Part: SKIN — CORROSION (BS 1580-1620)

LEVEL 1 CORROSION AFT LOWER FUSELAGE AT STA 1580-1620 BOTTOM SIDE LBL 1 TO RBL 1. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: STRAP — CRACKED (WS 970)

RT WING REAR SPAR UPPER SURFACE ATT STRAP FOUND CRACK AT WS 970. REPAIRED PER SRM 51-40-15.

Part: DOOR — CORROSION (APU COMPT)

LEVEL 1 CORROSION ON APU INLET DOOR EXTERIOR SURFACE. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.

Part: BASE — CORRODED (RT ELEVATOR)

LEVEL ONE CORROSION FOUND ON RT OUTBOARD ELEVATOR NR 1, NR 2 AND NR 3 STATIC DISCHARGER BASES. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: DOOR — DENTED (E/E COMPARTMENT)

DENT MARK FOUND AT FORWARD EDGE OF CENTER E/E ACCESS DOOR. REPAIRED AS PER SRM 51-40-01. NO CRACKS FOUND.

Part: SKIN — CORRODED (BS 1940-1960)

LEVEL ONE CORROSION FOUND AT AFT LOWER FUSELAGE STA 1940-1960 STR S39R TO S40R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: COWLING — DENTED (NR 2 ENGINE)

NUMBER 2 ENGINE NOSE COWL FOUND DENTED AT 5 O'CLOCK POSITION. REPAIRED IAW SRM 51-40-06.

Part: BASE — CORRODED (LT ELEVATOR)

LEVEL ONE CORROSION FOUND ON LEFT OUTBOARD ELEVATOR NR 1, NR 2, NR 3 AND NR 4 STATIC DISCHARGER BASES. ONE BASE REPLACED, CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DENTED (CARGO DOORWAY)

AFT LOWER FUSELAGE DENT AT BULK CARGO DOOR CUTOUT UPER AFT-END. REPAIRED IAW SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

LEFT WING NR 3 SPOILER UPPER SURFACE FOUND DELAMINATED. SPOILER REPLACED IAW SRM 27-61-02.

Part: SKIN — CORRODED (BS 1960)

LEVEL ONE CORROSION FOUND AT AFT LOWER FUSELAGE STA 1960 STR S38R TO S39R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DAMAGED (RT WING)

RT WING SURFACE T/E FIXED PANEL AT I/B OF I/B AILERON SCREW MOUNTED AREA DAMAGED. REPAIRED IAW SRM 51-40-15.

Part: PANEL — CORROSION (TOILET SVC)

LEVEL 1 CORROSION ON FWD TOILET SERVICE PANEL SURFACE INSIDE. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — DAMAGED (NR 1 PYLON)

NUMBER 1 PYLON VALVE ACCESS PANEL CUTOUT DAMAGED AT AFT EDGE. ACCESS PANEL CUTOUT TRIMMED OFF AS PER SRM 51-10-01.

Part: ROD — CORRODED (LT MLG)

LT BODY GEAR WW DOOR 745 ACT MANUAL SELECTOR ROD LOWER EYE END FOUND CORRODED. REPLACED ROD PER MM 32-35-08.

Part: SKIN — DENTED (BS 2320)

AFT FUSELAGE DENT MARK AT STA 2320 STR S48L-S49L. REPAIRED PER SRM 51-10-01 AND SRM 51-10-02.

Part: SKIN — DAMAGED (NR 2 PYLON DOOR)

NR 2 ENG RT SAILPLANE DOOR INNER SKIN PUNCTURED. REPAIRED PER SRM 51-40-06.

Part: BRACKET — CRACKED (NR 1 PYLON)

NR 1 PYLON GAP PANEL AREA CLOSURE SPAR RT SIDE FAIRING AFT BRACKET CRACKED. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: COWL — DENTED (NR 3 ENGINE)

NR 3 ENG LT SIDE COWL FWD EDGE UPPER SECTION DENTED. REPAIRED IAW SRM 51-10-02.

Part: WALL — CORRODED (BS 1394-1416)

LEVEL ONE CORROSION FOUND AT LEFT BODY LANDING GEAR WHEEL WELL OUTBOARD WALL BETWEEN BS 1394 AND 1416 BWL 200. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: LINK — RUSTY (NLG STEERING)

LEVEL 1 CORROSION NOSE LANDING GEAR STEERING LINK ARM. TREATED PER BOEING OH MANUAL 20-10-01, 20-10-02.

Part: PANEL — DELAMINATED (WATER SERVICE)

DELAMINATED POTABLE WATER SERVICE PANEL. REPAIRED PER BOEING SRM 51-40-12 FIG 9.

Part: SKIN — CORRODED (BS 800)

LEVEL 1 CORROSION AT BS 800 BBL 0 FORWARD OF CENTER ELECTRONICS ACCESS DOOR. REMOVED CORROSION PER BOEING SRM 51-10-01 REPROTECTED PER 51-10-02.

Part: SKIN — DEBONDED (NR 1 PYLON)

NUMBER ONE LEFT SAILPLANE DOOR OUTER SKIN IS DEBONDED. REPAIRED IAW SRM 51-40-06.

Part: BRACKET — CRACKED (NR 1 PYLON)

NUMBER 1 PYLON CRACKED BRACKET AT MIDSPAR WEB STIFFENER AT NACELLE STA 211. BRACKET REPLACED AS PER SRM 51-10-01.

Part: SKIN — DENTED (BS 1780-1800)

DENT LOWER FUSELAGE SKIN AT BS 1780 TO 1800 S33R - S32R. REPAIRED PER BOEING SRM 51-10-02.

Part: SKIN — DENTED (BS 800)

DENT FUSELAGE SKIN BS 800 BETWEEN S43L AND S44L. REPAIRED PER BOEING SRM 51-40-01.

Part: SKIN — CORROSION (BS 1820-1840)

LEVEL 1 CORROSION FOUND AFT LOWER FUSELAGE AT STA 1820-1840 STR S45L AND S46L. REMOVED CORROSION AND REPROTECTED PER SMR 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 1060)

PANEL SUPPORT BRACKET RIB CORRODED AT STA 1060 BBL 15R AIR CONDITIONING BAY. PANEL REPAIRED PER SRM 51-40-04 FIG 1.

Part: STRINGER — CORROSION (BS 1800-1820)

LEVEL 1 CORROSION AFT LOWER FUSELAGE STA 1820-1800 STR S47L. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: COWL — DAMAGED (NR 2 ENGINE)

DAMAGED AND LOOSE NR 2 ENGINE FAN COWL SUPPORT STRUCTURE AND UPPER SKIN. REPLACED SKIN AND DOUBLER PER BOEING SRM 51-10-01.

Part: PANEL — CORRODED (FUSELAGE)

LEVEL 1 CORROSION ON PANEL 192H ON OUTER SKIN. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — BROKEN (NR 2 PYLON)

NUMBER 2 PYLON HYDRAULIC PRESSURE LINE SUPPORT BRACKET BROKEN AT NACELLE STA 186. BRACKET REPLACED IAW SRM 51-10-01.

Part: STOWAGE BIN — CRACKED (LT COCKPIT)

COCKPIT LEFT STA 370-400 EQUIP STOWAGE FOUND CRACKED IN TWO PLACES. REPAIRED AS PER MM 25-59-00.

Part: RIVET — CORRODED (BS 145-160)

SURFACE CORROSION FOUND ON 44 RIVETS AT 145-160 BWL 195 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: BULKHEAD — WORN (NR 1 PYLON)

NUMBER 1 PYLON AFT 'V' FAIRING DEBONDING, DRAIN TUBE BROKEN, FWD BULKHEAD WORN AND SEALS SPLIT. REPAIRED AS PER SRM 51-40-06.

Part: COWL — DENTED (NR 4 ENGIINE)

DENT NR 4 ENGINE RIGHT SIDE COWL OUTTER SKIN FORWARD UPPER EDGE. REPAIRED PER BOEING SRM 54-40-01 FIG 1.

Part: STRUT — CORRODED (MLG)

LEVEL 1 CORROSION ON BODY LANDING GEAR STRUT AFT SIDE BELOW UPPER TORQUE LINK. CORROSION BLENDED OUT PER OHM 20-10-01 WITHIN LIMITS PER 32-13-38.

Part: STRINGER — CORROSION (BS 1920-1940)

LEVEL 1 CORROSION AFT LOWER FUSELAGE AT STA 1920-1940 STR S25L-S24L AFT OF MAIN CARGO DOOR LOWER CORNER. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 145-160)

SURFACE CORROSION FOUND ON 52 RIVETS AT 145-160 BWL 270 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01 AND 51-10-02.

Part: SKIN — CHAFED (NR 1 PYLON)

NUMBER 1 PYLON RIGHT SAILPLANE DOOR PRESSURE RELIEF PANEL INNER SKIN IS CHAFED THROUGH. REPAIRED IAW SRM 51-40-06 AND 51-30-02.

Part: FAIRING — DAMAGED (NR 7 CANOE)

RIGHT WING NR 7 CANOE FAIRING EXTERNAL SURFACE FOUND SPONGY IN TWO LOCATIONS. REPAIRED IAW SRM 51-40-15.

Part: SKIN — CORRODED (BS 2360)

LEVEL 1 CORROSION AFT FUSELAGE AT STA 2360 LBL 40 T LBL 20. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 854)

SUPPORT BRACKETS FOR PANEL 191S AT BS 854 LBBL 5 TO RBBL 5 CORRODED. REPLACED BRACKETS PER BOEING SRM 51-10-08.

Part: SKIN — CORROSION (BS 680)

LEVEL ONE CORROSION FOUND AT STATION 680 BWL 91. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01 AND 51-10-02.

Part: STRUT — CORROSION (LT MLG)

LEVEL 1 CORROSION LEFT BODY LANDING GEAR SURFACE AT SIDE STRUT. CORROSION BLENDED PER BOEING OHM 20-10-01, 02 FOUND WITHIN LIMITS PER 32-13-38.

Part: SKIN — CORRODED (FUSELAGE)

LEVEL ONE CORROSION FOUND ON FUSELAGE SKIN FWD OF TOILET SERVICE PNL SECTION 42. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SUPPORT — CORRODED (BS 1000)

PANEL SUPPORT STIFFENER AT STA 1000 BBL 55 CORNER HAS CORROSION. REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: COWL — CRACKED (NR 4 ENGINE)

BENT/CRACKED NR 4 ENGINE RT SIDE COWL BRACKET FORWARD HOOK UPPER EDGE.

Part: SKIN — CORRODED (BS 2400-2420)

LEVEL ONE CORROSION FOUND AT AFT FUSELAGE PREVIOUS REPAIR AREA, STATION 2400-2420 RBL 0 TO RBL 4. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: FITTING — BROKEN (NR 5 CANOE)

RIGHT WING NR 5 CANOE FAIRING FORWARD OUTBOARD HINGE MOUNT FITTING BROKEN. FAIRING SUPPORT REPLACED IAW MM 27-51-44.

Part: BRACKET — CRACKED (NR 3 COWL)

NR 3 ENGINE RIGHT SIDE COWL LOWER EDGE AFT CORNER BRACKET CRACKED. REPAIRED IAW SRM 51-40-03 AND SRM 51-30-02.

Part: BRACKET — CRACKED (NR 4 COWLING)

NR 4 ENGINE LEFT SIDE COWL UPPER EDGE FWD CORNER BRACKET CRACKED. BRACKET REPAIRED AS PER SRM 54-10-03.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RIGHT WING LANDING GEAR LOWER SLAVE DOOR 743 FOUND DELAMINATED ON INSIDE. REPAIRED AS PER SRM 51-40-06.

Part: SKIN — CORRODED (BS 2340-2360)

LEVEL 1 CORROSION FOUND AFT FUSELAGE AT STA 2360-2340 RBL 60. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: BRACKET — CORRODED (BS 910)

AT BS 910 RBBL 2 AFT SECTON OF SUPPORT BRACKET CORRODED. REPAIRED PER BOEING SRM 51-40-03, 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 145-160)

SURFACE CORROSION FOUND ON 44 RIVETS AT STA 145-160 BWL 189 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: COWL — CRACKED (NR 4 ENGINE)

CRACKED NR 4 ENGINE RIGHT SIDE COWL BREATHER EXHAUST DUCT. WELD REPAIRED PER BAC 5975.

Part: FAIRING — SPONGY (NR 8 CANOE)

RIGHT WING NR 8 CANOE FAIRING EXTERNAL SURFACE FOUND SPONGY. REPAIRED IAW SRM 51-40-15.

Part: RIVETS — CORROSION (BS 145-160)

CORROSION FOUND ON 26 RIVETS AT STA 145-160 285 LT AND RT SIDE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (BS 2360)

LEVEL 1 CORROSION ON AFT FUSELAGE AT STA 2360 RBL 2O TO RBL 30. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORRODED (FUSELAGE)

AIR CONDITIONING PANEL 192AR SURFACE CORROSION ON EXTERIOR AROUND LATCHES. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: RIVETS — CORRODED (BS 145-160)

SURFACE CORROSION FOUND ON 32 RIVETS AT 145-160 BWL 205 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.

Part: STRAP — CORROSION (BS 940)

STATION 940 LT FUSELAGE NR 2 INLET PACK PHELEM LOWER LEFT SUPPORT STRAP FOUND CORRODED. REPLACED SUPPORT STRAP AS PER SRM 51-10-01.

Part: DUCT — CRACKED (NR 3 COWLING)

NUMBER 3 ENGINE RT SIDE COWL BREATHER EXHAUST DUCT CRACKED. WELD REPAIRED IAW BAC 5975 REV L.

Part: COWL — DENTED (NR 3 ENGINE)

LARGE DENT NR 3 ENGINE LEFT FAN COWL OUTER SURFACE. REPAIRED PER BOEING SRM 51-40-06 FIG 14.

Part: COWL — DENTED (NR 4 ENGINE)

LARGE DENT NR 4 ENGINE LEFT FAN COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-40-06 FIG 14.

Part: PANEL — DENTED (FUSELAGE)

DENT LOWER FUSELAGE PANEL 194D. REPAIRED PER BOEING SRM 51-40-15 FIG 7.

Part: BRACKET — BROKEN (NR 1 ENGINE)

BROKEN BRACKET NR 1 ENGINE TOP SUPPORT TO PRECOOLER ASSY. REPLACED PER M/M 72-50-00.

Part: HOUSING — BROKEN (NR 1 TR UNIT)

BROKEN NR 1 ENGINE DIAPHRAGM SEGMENT AT 9 O'CLOCK POSITION. REPLACED HOUSING ASSY PER M/M 78-31-15.

Part: HINGE — WORN (NR 4 ENG OIL DR)

NR 4 ENGINE LEFT SIDE COWL OIL TANK ACCESS DOOR DENTED AND LOWER HINGE WORN. DOOR AND HINGES REPLACED PER MM 71-11-13 AND SRM 51-10-01.

Part: COWL — DAMAGED (NR 3 ENGINE)

DAMAGED UPPER AFT CORNER NR 3 ENGINE RT FAN COWL. REPAIRED PER BOEING SRM 51-40-06 FIG 17.

Part: TIP — DENTED (LT WING)

ON WALKAROUND, FOUND DENT IN LEFT WING TIP PANEL FWD SECTION. REMOVED AND REPLACED WING TIP PER MM 57-23-01.

Part: ENGINE — FLAMED OUT (NR 4)

NR 4 ENGINE FLAMED OUT AT FL 390 DURING MODERATE TURBULENCE. ENGINE RELIT SHORTLY THEREAFTER. ALL PARAMETERS WERE NORMAL. NR 4 ENGINE INTAKE AND TAIL PIPE VISUAL CHECK NORMAL. NO METAL FOUND IAW MM 71-00-00. BORESCOPE IAW MM 72-00-00, NO DAMAGE FOUND. REMOVED AND REPLACED FUEL FILTER PER MM 72-00-00.

Part: BRACE — CHAFED (NR 1 PYLON)

LT SIDE OF DIAGONAL BRACE CHAFED FWD END OF NR 1 ENGINE PYLON. BLENDED OUT CHAFED AREA PER SRM 54-40-01.

Part: PANEL — DAMAGED (WING)

DURING APPROACH WHEN FLAPS SELECTED TO 5 A VIBRATION WAS FELT UNTIL FLAT 10 SELECTED. ALL FLIGHT CONTROL AND LANDING GEAR IND NORMAL. FOUND FLYING PANEL DAMAGED. REMOVED AND REPLACED RT FLYING PANEL AS PER MM 57-22-01. ALSO, FOUND DAMAGE TO RT I/B FOREFLAP. REMOVED AND REPLACED RT I/B FORE FLAP PER MM 217-51-02 P/N 65B02001-102.

Part: PANEL — DELAMINATED (NR 2 SPOILER)

DELAMINATION NR 2 SPOILER PANEL LOWER SKIN BY AFT EDGE. REPLACED PANEL PER BOEING M/M 27-61-02.

Part: COWL — CRACKED (NR 1 ENGINE)

CRACK IN SKIN OF NR 1 ENGINE INBOARD CORE COWL. REPAIRED PER SRM 54-30-03 AND SRM 54-30-00.

Part: PANEL — DELAMINATED (NR 5 SPOILER)

DELAMINATED NR 5 SPOILER PANEL LT WING I/B AFT CORNER. REPAIRED PER SRM 51-50-06, 51-24-11 AND MM 27-61-01.

Part: ACCESS PANEL — DELAMINATED (LT ELEVATOR)

DELAMINATED POWER PAC ACCESS PANEL ON LT ELEVATOR. REPAIRED PER SRM 51-40-06.

Part: SKIN — DELAMINATED (LT TE FLAP)

DELAMINATED LT INBOARD AFT FLAP. REPAIRED PER SRM 51-40-06.

Part: FLYING DOOR — CORROSION (RT WING)

CORROSION ON RIGHT WING FLYING DOOR. REPAIRED PER SRM 52-00-02, 51-10-06.

Part: SKIN — DAMAGED (CARGO DOOR)

GOUGE IN SIDE CARGO DOOR, SKIN LWR BOTTOM. REPAIRED PER SRM 51-10-06.

Part: RIVETS — LOOSE (RT MLG DOOR)

WORKING RIVETS ON RT BODY GEAR INBOARD STRUT DOOR. REMOVED AND REPLACED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATION OF RT WING UPPER T/E PANEL OUTBD OF FLYING PANEL. REPAIRED PER SRM 51-30-02.

Part: SPOILER — DELAMINATED (NR 12 SPOILER)

DELAMINATED NR 12 SPOILER. REMOVED AND REPLACED PER MM 27-61-02.

Part: FASTENERS — MISSING (NR1 ENG TAILPIPE)

LOOSE/MISSING FASTENERS AT 9 TO 12 O'CLOCK POSITIONS NR 1 ENGINE TAILPIPE. REMOVED AND REPLACED SRM 51-30-02.

Part: PANEL — DELAMINATED (LT HORIZ STAB)

DELAMINATION PANEL 334 6BL, LEFT HORIZONTAL STAB. REPAIRED PER SRM 51-71-00.

Part: COWL — GOUGED (NR 1 ENGINE)

GOUGE IN THE NR 1 OUTBOARD FAN COWL. REPAIRED PER SRM 51-40-06.

Part: FASTENER — DAMAGED (RT WING SPAR)

DAMAGED FASTENER RT WING FRONT SPAR INBD NR 4 PYLON. REMOVED AND REPLACED PER SRM 51-10-02.

Part: RIVETS — MISSING (NR4 ENG EXHAUST)

MISSING RIVETS ON NR 4 ENGINE EXHAUST SLEEVE AT 11-12 O'CLOCK POSITIONS. REMOVED AND REPLACED PER SRM 51-10-02.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATED PANEL UNDER L3 DOOR L/E LEFT WING. REPAIRED PER SRM 51-40-89.

Part: FASTENERS — BROKEN (BS 2362)

BROKEN FASTENER AT LEFT SIDE STATION 2362, 20 INCHES ABOVE MAIN DECK FLOOR. REMOVED AND REPLACED PER SRM 51-30-02.

Part: DUCT ASSEMBLY — CRACKED (APU)

CRACKED APU SUPPLY DUCT ELBOW. CRACKED JUST FWD OF APU. REMOVED AND REPLACED DUCT ASSY (P/N 69B40052-1) PER MM 36-11-01.

Part: COWL — DELAMINATION (NR 4 ENGINE)

DELAMINATION ON OUTBOARD CORE COWL OF NR 4 ENGINE. REPAIRED PER SRM 51-40-06.

Part: PANEL — CRACKED (LT WING)

CRACK ON UPPER T/E PANEL OUTBD NR 5 SPOILER LEFT WING, PREVIOUS REPAIR. REPAIRED PER SRM 51-40-09.

Part: BEAM — GOUGED (RT MLG)

SLIGHT GOUGE AND CHAFE ON R-BODY GEAR VERT OUTBD ATTACH BEAM. BLEND PER SRM 51-10-06.

Part: FASTENER — MISSING (LT WING SPAR)

MISSING FASTENER LT WING L/E FRONT SPAR 6 FEET FROM FUSELAGE. REMOVED AND REPLACED PER SRM 51-01-02.

Part: FASTENERS — LOOSE (NR 4 ENG COWL)

LOOSE FASTENERS ON NR 4 O/B CORE COWL AT BLEED EXHAUST. REMOVED AND REPLACED PER SRM 51-30-02.

Part: SKIN — SCRATCHED (RT HORIZ STAB)

SCRATCHES ON RT L/E HORIZ STAB. REPAIRED PER SRM 51-10-02, 55-10-01.

Part: SKIN — DENTED (FUSELAGE)

DENT/GOUGE IN FUSELAGE JUST AF OF TAIL JACK POINT. REWORKED AREA PER SRM 51-30-01 PAGE 1A. HFEC PER 51-00-00 FIG 4. NO DEFECTS NOTED.

Part: FASTENERS — DAMAGED (FUSELAGE)

DAMAGED FASTENER ON FUSELAGE SECTION 48 STA 2598. REMOVED AND REPLACED PER SRM 51-30-07.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATED UPPER T/E PANEL RT WING FWD OF NR 7/8 SPOILER. REPAIRED PER SRM 51-30-02.

Part: J-BOX — PULLED FASTENERS (RT BODY GEAR)

PULLED FASTENERS ON RT BODY GEAR J-BOX. REMOVED AND REPLACED OHM 20-50-01.

Part: TAILPIPE — TORN (NR 1 ENGINE)

TORN 2 INCH AREA ON NR 1 ENG TAILPIPE ASSY. REPARIED PER SRM 54-30-03.

Part: FASTENERS — MISSING (NR 3 PYLON)

MISSING FASTENERS .25 INCH CRACK, NR 3 PYLON INBD SLOT SEAL AREA. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FASTENERS — MISSING (NR 2 PYLON)

MISSING FASTENERS ON NR 2 PYLON INBD AFT SMALL FAIRING. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FASTENERS — LOOSE (NR 3 PYLON)

LOOSE FASTENERS NR 3 PYLON OUTBD ABOVE SLEEVE. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FAIRING — DAMAGED (WING/BODY)

DAMAGED RT WING TO BODY FAIRING NR 292AR. REPAIR PER SRM 51-40-15, SRM 51-24-11.

Part: FASTENERS — MISSING (NR 1 PYLON)

LOOSE/MISSING FASTENERS NR 1 PYLON INBD SLOT SEAL AREA. REMOVED AND REPLACED SRN 51-30-02.

Part: SKIN — DELAMINATION (RT WING)

DELAMINATION UPPER SURFACE RT WING FWD OF NR 7 SPOILER. REPAIRED PER SRM 51-40-09.

Part: COWL — MISSING FASTENER (NR 1 ENGINE)

MISSING FASTENER ON EXTERNAL SKIN OF THE NR 1 ENGINE CORE COWL. REMOVED AND REPLACED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATION ON RT WING TRAPIZODIAL PANEL BOTTOM SURFACE. REPARIED PER SRM 51-40-14.

Part: RADOME — ERRODED (FWD FUSELAGE)

ERROSION ON RADOME. REPAIRED PER BOEING SRM 51-40-115 AND 53-52-01.

Part: FASTENERS — LOOSE (NR 2 PYLON)

LOOSE FASTENERS, NR 2 ENGING PYLON UPPER OUTBD AFT EXTERNAL. REMOVED AND REPLACED PER SRM 51-30-02.

Part: RIVETS — LOOSE (NR 2 PYLON)

WORKING RIVETS OTBD LWR AFT PANEL NR 2 PYLON. REMOVED AND REPLACED PER SRM 51-30-02.

Part: SLOT SEAL — DAMAGED (NR 1 PYLON)

ELONGATED ALIGNMENT HOLE, NR 1 ENG OUTBD SLOT SEAL ASSY. REMOVED AND REPLACED PER 51-30-02 DOUBLER.

Part: FASTENERS — BROKEN (LT WING SKIN)

BROKEN FASTENERS OUTBOARD NR 2 PYLON LEFT WING UPPER LEADING EDGE. REMOVED AND REPLACED PER SRM 51-10-02.

Part: PANEL — CRACKED (LT WING)

CRACK OF PREVIOUS REPAIR UPPER T/E PANEL, FWD INBD AILERON, LEFT WING. REPAIRED PER SRM 51-50-09 AND 51-24-11.

Part: FASTENERS — LOOSE (RT LOGO LIGHT)

LOOSE/MISSING ATTACH FASTENERS ON RT LOGO LIGHT. REMOVED AND REPLACED FASTENERS PER SRM 51-10-02.

Part: PANEL — DELAMINATION (RT ELEVATOR)

DELAMINATED RT INBD ELEVATOR POWER CONTROL ACCESS PANEL NR 344. REPAIRED PER SRM 51-30-02, 51-24-11.

Part: FLYING PANEL — DELAMINATION (LT WING)

DELAMINATION ON AFT CORNER OF LT WING FLYING PANEL. REPARIED PER SRM 51-40-15.

Part: SKIN — DELAMINATION (NR 11 SPOILER)

DELAMINATED NR 11 SPOILER RT WING AT INBD T/E. REPARIED PER SRM 51-40-06, 51-40-09.

Part: FASTENERS — BROKEN (FRONT SPAR)

BROKEN FASTENERS ON UPPER LEADING EDGE FRONT SPAR INBD NR 1 PYLON. REMOVED AND REPLACED SRM 51-10-02.

Part: BRACKET — CRACKED (LT LE FLAP)

CRACKED BRACKET GROUP 1 LEADING EDGE DE-VICE LEFT WING. REPAIRED PER SRM 51-40-03.

Part: DOOR — DAMAGE (CARGO COMPT)

DAMAGE ON EXISTING REPAIR ON UPPER AFT CORNER OF THE LOWER AFT CARGO DOOR. REPAIRED PER SRM 51-30-02.

Part: FASTENER — CORRODED (WING SKIN)

CORROSION (LITE) ON FASTENERS AT NR 12 SPOILER AREA UPPER SKIN/REAR SPAR. REPAIRED PER SRM 57-30-01.

Part: SKIN — CRACKED (RT ELEVATOR)

A 4 INCH CRACK IN RT INBD ELEVATOR T/E. REPAIRED PER SRM 51-40-15 AND SRM 51-24-11.

Part: PLENUM — CRACKED (NR 2 HEAT EXCHGR)

CRACKED FIBERGLASS PLENUM ON THE NR 2 HEAT EXCHANGER. REPAIRED PER SRM 51-40-15.

Part: SKIN — DELAMINATION (LT TE FOREFLAP)

DELAMINATION LT WING INBD FOREFLAP 4 INCH AREA.

Part: SKIN — DELAMINATION (NR 10 SPOILER)

DELAMINATION ON NR 10 SPOILER AT O/B T/E. REPAIRED PER SRM 51-40-06.

Part: FASTENERS — BROKEN (RT WING SKIN)

BROKEN FASTENERS ON RT WING LEADING EDGE 15 FT FROM FROM FUSELAGE. REMOVED AND REPLACED PER SRM 51-10-02.

Part: SKIN — DELAMINATED (LT HORIZ STAB)

DELAMINATED L/HORIZ STAB LWR T/E. REPAIRED PER SRM 51-24-11 AND SRM 51-30-02.

Part: DOOR — MISSING FASTENER (NR 2 ENGINE)

LOOSE/MISSING FASTENERS ON CSD DOOR, NR 2 ENGINE OUTBOARD CORE COWL. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FAIRING — CRACKED (RT WING)

CRACKED FWD FAIRING RT WING GEAR. REPAIRED PER SRM 51-30-02, 53-30-03, 51-10-02.

Part: SKIN — GOUGE (FUSELAGE)

SEVERAL GOUGES ON FUSELAGE SKIN BELOW EMERGENCY DOOR. BLEND PER SRM 51-10-02, 53-30-01, 51-10-02.

Part: DOOR — CORROSION (RT MLG)

CORROSION (LITE SURFACE) ON RT WING GEAR DOOR CHAFED IN TWO PLACES. REPAIRED PER SRM 52-00-02.

Part: FASTENERS — BROKEN (LT WINGSKIN)

BROKEN FASTENERS LEFT WING LEADING EDGE FRONT SPAR INBD NR 1 PYLON.

Part: SKIN — CORROSION (RT WING)

CORROSION (LITE) RIGHT WING LEADING EDGE SKIN. REMOVED AND REPLACED PER SRM 51-30-02 AND SRM 52-10-01.

Part: BRACKET — BROKEN (RT MLG WW)

BROKEN BRACKET TO PANEL SUPPORT BRACE AT RIGHT MAIN LANDING GEAR OUTBOARD GEAR DOOR AREA. MANUFACTURED BRACKER FROM EXTRUDED TEE BAC1505-34393 7075 T6 MATERIAL PER BOEING SRM 51-10-01 REFERENCE SRM 53-10-22 (BOEING IDENTIFIED MATERIAL).

Part: HINGE — CRACKED (RT MLG DOOR)

CRACKED AFT HINGE AT RIGHT BODY GEAR INBOARD DOOR. REPLACED HINGE PER BOEING M/M 32-14-05.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

NR 3 ENGINE HAD A OVERHEAT ON THE BLEED VALVE. VALVE CLOSED, THROTTLED BACK, LIGHT WENT OUT. FOUND NR 3 ENGINE PRECOOLER CRACKED APPROXIMATELY 5 INCHES LONG. REMOVED AND REPLACED PRECOOLER PER M/M 36-12-01.

Part: INU — FAILED (NR 1)

NR 1 INERTIAL NAVIGATION SYSTEM FAILED AFTER TAKEOFF DISPLAY WAS BLANK WITH RED WARNING LIGHT ON. NR 3 INERTIAL NAVIGATION SYSTEM HAS ADC AND MX RQD FLASHING IN STATUS DISPLAY. AIRCRAFT RETURNED TO SIN. REPLACED NR 1 INU AND ALIGNED PER M/M 34-41-00. PLACARDED NR 3 INU PER MEL 34-27-1.

Part: FITTING — CORRODED (BS 980.8)

LEVEL 1 CORROSION, RIGHT ATTACH FITTING TO KEEL BEAM LOWER SURFACE BS 980.8 AT FASTENERS. REMOVED CORROSION PER SRM 51-10-01 FOUND WITHIN LIMITS PER SRM 51-10-02 AND 51-30-02.

Part: T CHORD — CORRODED (BS 965)

LEVEL 2 CORROSION, PANEL SUPPORT BS 965 LBL 48. REPLACED T-CHORD PER BOEING SRM 51-30-02.

Part: SKIN — DELAMINATED (LT HORIZ STAB)

DELAMINATED PANEL NR 334MB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-05.

Part: PANEL — DELAMINATED (RT HORIZ STAB)

DELAMINATED PANEL NR 344NB RIGHT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06.

Part: SKIN — DELAMINATED (LT HORIZ STAB.)

DELAMINATED PANEL NR 334NB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06 AND 55-10-12.

Part: SUPPORT — CORRODED (FUSELAGE)

LEVEL 2 CORROSION PANEL SUPPORT LOWER FUSELAGE FORWARD OF WATER SERVICE PANEL. REPAIRED PER SRM 51-40-04 AND 51-10-01.

Part: PANEL — CRACKED (LT TE FLAP)

CRACK ON INBOARD END OF LEFT WING INBOARD FLAP COVER PANEL. REPAIRED PER BOEING SRM 51-40-09 AND 51-24-11.

Part: PANEL — CORRODED (BS 980)

LEVEL 2, CORROSION LWR SURFACE STA 980, LBL 40 BODY PANEL SUPPORT. REPAIRED DAMAGED AREA FAB. REPAIR PARTS AND INSTALLED IAW BOEING SRM 51-40-04.

Part: SKIN — CORRODED (FUSELAGE)

LEVEL 2 CORROSION, LWR FUSELAGE BETWEEN NR 1 AND NR 3 ACM DOORS, PANEL. REMOVED CORROSION FROM LWR FUSELAGE BETWEEN NR 1 AND NR 3 ACM DOORS IAW BOEING SRM 51-10-01 AND TREATED AND PRIMED AREA PER BOEING SRM 51-10-02.

Part: PANEL — CORRODED (FUSELAGE)

LEVEL 1 CORROSION, LWR FUSELAGE NR 1 HEAT EXCHANGER PANEL AROUND FASTENERS. REPAIRED AREA PER BOEING SRM 51-40-11 PRIMED AND PAINTED PER BOEING SRM 51-24-11.

Part: FITTING — CORRODED (BS 968)

LEVEL 1 CORROSION, LWR SURFACE STA 968 RT FORWARD FITTING KEEL BEAM IN CENTER OF FITTING AT FASTENERS. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW BOEING SRM 53-10-01 FIG. 1 ORIG. MAT .260 NOW .224 TREATED AND PRIMED IAW BOEING SRM 51-10-06.

Part: FILL VALVE — CORRODED (BS 970)

LEVEL 1 CORROSION, LWR SURFACE STA 970 WATER SERVICE STATION WATER TANK FILL VALVE HANDLE AT MOUNT. CORROSION REMOVED FOUND TO BE WITHIN LIMITS IAW BOEING SRM 53-10-01 FIG 1, REG MAT .130 NOW .111 TREATED AND PRIMED PER SRM 51-10-06.

Part: FITTING — CORRODED (BS 980)

LEVEL 1 - CORROSION, LWR SURFACE STA 980 LEFT FORWARD ATTACH FITTING TO KEEL BEAM AROUND FASTENERS. CORROSION REMOVED PER BOEING SRM 53-30-01 WITHIN LIMITS IAW SRM 53-10-01 FIG 1 ORIG MAT .560 NOW .543 TREATED AND PRIMED IAW SRM 53-10-06.

Part: SKIN — CORRODED (BS 980)

LEVEL 1 CORROSION, LWR SURFACE STA 980 LEFT FORWARD ATTACH FITTING TO KEEL BEAM HAS CORROSION AROUND FASTENERS. REMOVED CORROSION IAW BOEING SRM 53-30-01 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 1 ORIG MAT .560 NOW .543 TREATED AND PRIMED IAW SRM 53-10-06.

Part: RADOME — DELAMINATED (FWD FUSELAGE)

NOSE RADOME HAS SEVERAL AREAS OF EXPOSED COMPOSITE AND DELAMINATION. CLEANED, SANDED AND POTTED DAMAGED AREA IAW BOEING SRM 53-50-03 AND PREP AND PAINTED SPOTS ON NOSE RADOME IAW 51-24-11.

Part: OVERHEAD PANEL — CORRODED (E/E COMPT)

LEVEL 1 - CORRODED CENTER ELECTRICAL COMPARTMENT FORWARD OVERHEAD PANEL AROUND FASTENERS AT AFT END. CORROSION REMOVED AROUND FASTENERS AT CENTER ELECTRICAL COMPARTMENT FORWARD OVERHEAD PANEL FOUND TO BE WITHIN LIMITS IAW BOEING SRM 51-10-01. TREATED AND PRIMED AREA IAW SRM 51-10-07.

Part: A13 FIRE CARD — FAILED (NR 1 ENGINE)

SHORTLY AFTER TAKEOFF, NR 1 ENGINE FIRE WARNING B-LOOP INDICATED FIRE. A-LOOP WAS INTERMITTENT CAUSING FIRE WARNING NR 1 ENGINE SHUT DOWN. MEGGED LOOPS A AND B FROM FIRE WARNING CONTROL MODULE CHECKS GOOD. CHECKED WIRING AND LOOPS ON ENGINE, CHECKED GOOD. REMOVED AND REPLACED FAULTY A13 CARD PER MAINTENANCE MANUAL 26-11-00 PAGE 201.

Part: PANEL — DAMAGED (RT WING)

ACCESS PANEL DAMAGED BETWEEN NR 5 FLAP TRACK FIXED FAIRING AND RWG UPPER STRUT DOOR. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: INU — FAILED (COCKPIT)

NR 1 INS WARNING LIGHT CAME ON IN FLIGHT (OVER 60 XFR ERROR), NR 3 INS ALREADY ON PLACARD. MADE UNSCHEDULED LANDING IN TPE. ON GATE 8 TIRES DEFLATED DUE TO OVER HEAT. REPLACED INS SYSTEM INU PER BOEING MAINTENANCE MANUAL 34-41-00. TIRES REPLACED PER BOEING MAINTENANCE MANUAL 32-45-01. OVERWEIGHT LANDING INSPECTION COMPLETED PER MAINTENANCE MANUAL 05-51-39, NO DEFECTS NOTED.

Part: BRACKET — CRACKED (LT LE FLAP)

NR 4 LEFT LEADING EDGE DRIVE UNIT SUPPORT BRACKET CRACKED BY NUT PLATE HOLES, FWD L/R SIDES. STOP DRILL CRACK AND INSTALLED FABRICATED DOUBLER AS PER BOEING SRM 51-40-03.

Part: BRACE — DAMAGED (LT/RT PYLON)

NR 4 ENG DIAGONAL BRACE CHAFED AT FWD END LT AND RT SIDES. INSPECTED AREA PER SRM 54-40-01, FOUND TO BE WITHIN LIMITS PER ZONE 2 C/W EDDY CURRENT INSP PER NDT MM 51-00-00, FOUND OK FOR SERVICE PLUS BLENDED, SHOT PEENED, TREATED AND PAINTED PER SRM 54-40-01.

Part: BRACE — DAMAGED (LT/RT PYLON)

NR 3 ENG DIAGONAL BRACE CHAFED FWD END BOTH LT AND RT SIDES. INSPECTED ARE PER SRM 54-40-01 FOUND TO BE WITHIN LIMITS PER ZONE 2, BLENDED AREA PER SRM 54-40-01 C/W EDDY CURRENT OK FOR SERVICE PER NDT MM 51-00-00, SHOT PEENED, TREATED AND PAINTED PER SRM 54-40-01.

Part: BRACE — DAMAGED (LT PYLON)

NR 1 ENG DIAGONAL BRACE CHAFED FWD END LT SIDE. INSPECTED AREA PER SRM 54-40-01, FOUND TO BE WITHIN LIMIT PER ZONE 2 AND 3. BLENDED AREA, EDDY CURRENT INSP C/W PER NDT MM 51-00-00 OK FOR SERVICE SHOT PEENED, TREATED AND PAINTED PER SRM 54-40-01.

Part: ADI — FAILED (RT COCKPIT)

DURING TAKEOFF AT APPROXIMATELY 60 TO 70 KTS, THE FIRST OFFICERS ADI ROLLED 90 DEGREES LEFT, CIWS ATT LIGHT ON AND THE GYRO FLAG WAS IN VIEW. AFTER THE ABORT THE ADI RETURNED TO NORMAL GYRO FLAG DISAPPEARED AND THE CIWS ATT LIGHT WENT OUT. NR 2 INS WAS CHECKED FOR ERROR CODES AND NONE WERE DISPLAYED. REPLACED FIRST OFFICER'S ADI OPERATIONAL CHECKED SATISFACTORY PER 34-27-00.

Part: FAIRING — DELAMINATED (NR 3 PYLON)

DELAMINATION ON NR 3 PYLON SAIL BOAT FAIRING LEADING EDGE 2 BY 15. REPAIRED PER MA 5450-01:01.

Part: SKIN — CRACKED (BS 1852)

DURING WALK AROUND INSPECTION FOUND SKIN BULGING AND A 1.50 INCH CRACK BELOW AFT CARGO DOOR APPROXIMATELY BS 1852. REPAIRED PER BOEING SRM 53-30-03 FIGURE 1. (LEVEL 2 CORROSION.)

Part: COWL — DAMAGED (NR 1 ENGINE)

DAMAGE ON UPPER AFT EDGE OF NR 1 ENGINE CORE COWL. REPAIRED DAMAGE PER BAC SRM 51-10-01.

Part: COWL — BENT (NR 2 ENGINE)

NR 2 ENGINE OUTBOARD FAN COWL UPPER FORWARD CORNER BENT AND DELAMINATED. REPAIRED PER BOEING SRM 51-30-02 AND 51-10-02.

Part: DOUBLER — CRACKED (NR 1 ENGINE COWL)

CRACK IN DOUBLER AT NR 4 LATCH NR 1 ENGINE OUTBOARD CORE COWL. REPAIRED PER BOEING SRM 51-10-01.

Part: DUCT — CRACKED (NR 3 ENGINE)

CRACKED NR 3 ENGINE COMPENSATOR DUCT. REMOVED AND REPLACED DUCT PER BOEING MAINTENANCE MANUAL 36-11-16.

Part: LATCH PIN — CORRODED (CARGO DOOR)

CORROSION ON MAIN CARGO DOOR NR 1 LATCH PIN. REPLACED PIN PER BOEING M/M 53-44-00.

Part: COWL — BENT (NR 2 ENGINE)

NR 2 ENGINE INBOARD FAN COWL UPPER FORWARD CORNER BENT AND DELAMINATED. REPAIRED PER BOEING SRM 51-30-02 AND 51-10-02.

Part: COWL — WORN (NR 2 ENGINE)

WORN NR 2 ENGINE INBOARD CORE COWL FORWARD CORNER. FABRICATED AND INSTALLED NEW FRAME SECTION AND SPLICE PER BAC SRM 51-10-01.

Part: PRECOOLER — CRACKED (NR 2 ENGINE)

CRACK ON NR 2 ENGINE PRECOOLER. WELD REPAIR PERFORMED PER BOEING SPECIFICATION 5975.

Part: SKIN — CRACKED (NR 4 PYLON)

CRACK NR 4 PYLON INBOARD SIDE JUST ABOVE AFT MOUNT (HALF MOON CUTOUT) FROM SCREW HOLE. REPAIRED PER BOEING SRM 54-30-03.

Part: SKIN — CHAFED (NR 3 ENGINE)

CHAFED THROUGH SKIN ON NR 3 ENGINE INBOARD CORE COWL AFT TOP AREA IN 2 PLACES. REPAIRED PER BOEING SRM 51-40-03.

Part: BRACKET — CRACKED (NR 3 ENGINE)

CRACKED AFT BOTTOM CORNER BRACKET. REMOVED FABRICATED AND INSTALLED NEW BRACKET PER BOEING SRM 51-10-01.

Part: PANEL — CRACKED (LT WING)

COMPOSITE PANEL OVER LEFT WING GEAR DELAMINATED AND CRACKED. REPAIRED PER BOEING SRM 51-40-09 AND 51-40-12.

Part: CONNECTOR — CONTAMINATED (RUDDER RATIO)

ON TAXI OUT AFTER FLIGHT CONTROL CHECK, RUDDER RATIO LIGHT CAME ON AND REMAINED ON. REMOVED AND CLEANED CANNON PLUGS ON BOTH UPPER AND LOWER RUDDER RATIO UNITS. PERFORMED RUDDER RATIO CHECK PER BOEING MAINTENANCE MANUAL 27-21-12, PROCEDURE GROUND CHECKS NORMAL. RUDDER RATIO SHOWS EQUAL TRAVEL ON BOTH RUDDERS, LIGHT STAYED OUT.

Part: AIR SPEED IND — READS HIGH (RT COCKPIT)

AFTER APPLICATION ON TAKEOFF, THRUST FIRST OFFICERS AIRSPEED INDICATOR INDICATED 20 KNOTS FASTER THAN CAPTAINS, INCREASED TO 85 KNOTS THEN STUCK AT THAT INDICATION. ABORTED TAKEOFF. REPLACED FIRST OFFICERS AIRSPEED INDICATOR PER BOEING MAINTENANCE MANUAL 34-13-04.

Part: AIRSPEED IND — INOPERATIVE (RT COCKPIT)

FIRST OFFICER'S AIRSPEED INDICATOR READ ZERO WHILE CAPTAIN'S ASI INDICATED 100 KNOTS. PERFORMED HIGH ENERGY STOP INSPECTION PER BAC MM 05-51-10 AND REPLACED FIRST OFFICER'S AIR SPEED INDICATOR PER BAC MM 34-13-05.

Part: PANEL — CREASED (RT WING)

RIGHT UNDERWING FIBERGLASS PANEL AFT OF OUTBOARD LANDING LIGHT HAS A CREASE APPROXIMATELY 4 INCHES LONG BY .25 INCH DEEP WING STATION 294.600. REPAIRED PER BOEING SRM 51-40-07.

Part: FUEL TANK RIBS — NOT SEALED (RT WING)

FLIGHT REPORT OF UNCOMMANDED TRANSFER OF FUEL INTO NR 4 MAIN FROM NR 4 RESERVE AND INTO NR 3 MAIN FROM NR 4 MAIN TANK. INVESTIGATION REVEALED MISSING SEALANT AT NR 4 RESERVE TANK-J NR 4 MAIN TANK RIB ABOVE NR 4 PYLON AND AT NR 3 TO NR 4 TANK RIB ABOVE NR 3 PYLON. MODIFICATION PER SB 747-54-2159 COMPLETED 3 FLIGHTS PRIOR. REMOVED OLD SEALANT, RESEALED AND LEAK CHECKED OK PER BOEING MAINTENANCE MANUAL 28-11-00.

Part: TEE FITTING — CRACKED (NR 4 FUEL TANK)

DURING INSPECTION FOR CAUSE OF FUEL MIGRATION, FOUND CRACKED TEE FITTING IN NR 4 MAIN TANK. REMOVED WELDED PER COMPONENT MAINTENANCE MANUAL 28-00-10 AND REINSTALLED TEE FITTING AND LEAK CHECKED OK.

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

CRACKED NR 3 HYDRAULIC SYSTEM FILTER MODULE. REPLACED MODULE PER BOEING MAINTENANCE MANUAL 29-11-23.

Part: BULKHEAD WEB — CRACKED (LT MLG WW)

CRACK AT APU DUCT CUTOUT AT LEFT WHEEL WELL BULKHEAD. REPAIRED WITH KIT 015M0425-1 PER BAC SERVICE BULLETIN 747-53-2309.

Part: ANGLE — CRACKED (BS 1380)

CRACKED SHEAR ANGLE AT STATION 1380 / RBL 100. REPAIRED PER BAC SERVICE BULLETIN 747 SB 2213.

Part: SKIN — CORRODED (RT HORIZ STAB)

LEVEL 1 CORROSION TOP OF RIGHT HORIZONTAL STABILIZER STA 335 RBL 260, STA 340 RBL 270, STA 310 RBL 260 TO 270, STA 260 TO 310 RBL 255.2, STA 310 RBL 260 TO 300, STA 0 TO 260 RBL 255, STA 0 TO 26 RBL 231, STA 0 TO 26 RBL 170. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 55-10-01 AND 55-10-02.

Part: STRINGER — CORRODED (BS 810)

LEVEL 2 CORROSION AT S46R BS 810 FORWARD CARGO COMPARTMENT. REPAIRED STRINGER PER BOEING SRM 53-10-03.

Part: SHEAR TIE — CORRODED (BS 760)

LEVEL 2 CORROSION FORWARD CARGO HOLD SHEAR TIE AT BS 760 BETWEEN S46L AND S47L. MANUFACTURED REPLACEMENT PART PER BOEING SRM 51-20-01 AND INSTALLED PER 53-10-04.

Part: STRINGER — CORRODED (BS 516-618)

FOUND LEVEL ONE CORROSION ON FORWARD CARGO HOLD S47L, BS 516 TO 518. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS IAW SRM 51-10-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. RIVETS REMOVED FOR ACCESS AND REINSTALLED IAW SRM 51-30-02.

Part: STRINGER — CORRODED (BS 775/785)

LEVEL 2 CORROSION S44L AT BS 775 AND 785. REPAIRED PER BOEING SRM 53-10-03.

Part: STRINGER — CORROSION (BS 1648)

LEVEL 1 CORROSION AT STRINGER 48R STA 1648. REMOVED CORROSION PER BAC SRM 51-22-00, WITHIN LIMITS PER BAC SRM 51-12-00, REPROTECTED AREA PER BAC SRM 51-21-00.

Part: STRINGER — CORRODED (BS 1678)

LEVEL 1 CORROSION STRINGER S48R BS 1678. CORROSION REMOVED PER BOEING SRM 51-22-00. FOUND WITHIN LIMITS PER 51-12-00 REPROTECTED PER 51-21-00.

Part: STRINGER — CORROSION (BS 1416)

LEVEL 1 CORROSION AT STRINGER 41 STA 1416 RBL 160. REMOVED CORROSION PER BAC SRM 51-10-03, WITHIN LIMITS PER BAC SRM 53-40-01, REPROTECTED AREA PER BAC SRM 51-21-00.

Part: SKIN — CORRODED (RT TE MIDFLAP)

FOUND LEVEL ONE SURFACE CORROSION ON INBOARD MIDFLAP ON CENTER PANEL AT JOINT TO AFT PANEL ON LOWER SURFACE RWBL 225. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 51-40-00. REPORTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.

Part: SKIN — CORROSION (RT TE MIDFLAP)

FOUND LEVEL ONE SURFACE CORROSION ON UPPER SKIN OF INBOARD MIDFLAP AT JOINT TO TRAILING EDGE FALSE WORK, RWBL 333 TO 352. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 57-50-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 700)

LEVEL 1 CORROSION ON FORWARD CARGO HOLD LATERAL FLOORBEAM UPPER CHORD UPPER SURFACE AT BS 780 RBL 15 TO RBL 23. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PROTECTED PER 51-10-02.

Part: WIRE — CHAFED (E\E COMPT)

PRIMARY DISPLAY AND CONTROL CIRCUIT BREAKER TRIPPED. REPAIRED CHAFED WIRE AT CONNECTOR IN LANDING GEAR CARD FILE DISCONNECT PANEL, OPERATIONAL CHECKED OK PER M/M 32-61-00.

Part: ENGINE — OVER TEMP (NR 1)

ON TAKEOFF ROLL, NR 1 ENGINE ROLL REACHED 942 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF, RETURNED TO GATE. ENGINE CHANGED PER BOEING MAINTENANCE MANUAL 71-00-02.

Part: DOOR — DELAMINATED (LT/RT MLG)

DELAMINATED REPAIR ON BOTH THE LEFT AND RIGHT WING LANDING GEAR FLYING DOORS. REPAIRED PER BOEING SRM 51-40-15 AND 51-40-06.

Part: R-RAIL — CRACKED (NR 4 ENGINE)

NR 4 ENGINE R-RAIL IS CRACKED CIRCUMFERENTIALLY, LIGHTENING HOLE TO LIGHTENING HOLE AT THE 5:30 POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01.

Part: CORE COWL — CRACKED (NR 3 ENGINE)

NR 3 ENGINE INBOARD CORE COWL IS CRACKED AT AFT UPPER CORNER. STOP DRILLED CRACK, FABRICATED DOUBLERS AND REPAIRED IAW SRM 54-10-03.

Part: LE SKIN — DAMAGED (NR 1 TE FOREFLAP)

SMALL HOLES IN LEFT WING NR 1 FOREFLAP ON LEADING EDGE INBOARD OF NR 1 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15 AND 51-40-11.

Part: TIP SHROUD — DELAMINATED (NR 3 ENGINE)

NR 3 ENGINE INLET FAN BLADE TIP SHROUD DELAMINATED AT 5:30 POSITION. REPAIRED DELAMINATION AND APPLIED ADHESIVE IAW SRM 72-33-01.

Part: CHANNEL — CRACKED (NR 3 ENGINE)

CRACKED CHANNEL ON NR 3 ENGINE INBOARD CORE COWL LOWER CHANNEL AT THE FORWARD MOST GUIDE PIN. REPAIRED PER BOEING SRM 51-10-01 AND 51-30-02.

Part: CHANNEL — CRACKED (NR 2 ENG COWL)

NR 2 ENGINE INBOARD CORE COWL INNER CHANNEL AFT SECTION IS CRACKED. FABRICATED PARTS AND REPAIRED IAW SRM 51-30-02.

Part: COWL — CRACKED (NR 3 ENGINE)

CRACKED CHAFE STRIP NR 3 INBOARD CORE COWL UPPER EDGE. REMOVED, FABRICATED AND REPLACED CHAFE STRIP PER BOEING SRM 51-30-02 AND 51-10-01.

Part: COWL — TORN (NR 4 ENGINE)

TEAR AT TRAILING EDGE OF NR 4 ENGINE INBOARD CORE COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-10-01, 51-30-02 AND 51-10-02.

Part: AIR DUCT — CRACKED (NR 2 ENG COWL)

NR 2 ENGINE INBOARD CORE COWL LOWER FORWARD AIR DUCT IS CRACKED. WELDED AND REINSTALLED IAW SRM 51-30-02.

Part: S-RAIL — CRACKED (NR 4 ENGINE)

NR 4 ENGINE S-RAIL HAS A RADIAL CRACKED AT 1:30 POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01.

Part: S-RAIL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE S-RAIL HAS A RADIAL CRACK AT THE 2 O'CLOCK POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01.

Part: SUPPORT PLATE — CRACKED (NR 2 ENG COWL)

NR 2 ENGINE OUTBOARD CORE COWL, LOWER FORWARD CORNER SUPPORT PLATE IS CRACKED IN THE LIGHTENING HOLE. WELDED BRACKET AND REINSTALLED IAW SRM 51-30-02.

Part: FALSE SPAR — CORRODED (RT WING)

RT FALSE SPAR FORWARD SIDE FROM WING GEAR TRUNNION ATTACH I/B TO END HAS BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02.

Part: MOUNT BRACKET — CRACKED (NR 3 ENGINE)

NR 3 ENGINE CLAMP MOUNTING BRACKET IS CRACKED FOUR INCHES FORWARD OF R-RAIL AT 6 O'CLOCK POSITION. FABRICATED NEW BRACKET AND INSTALLED IAW MM 70-50-00.

Part: LE FAIRING — DELAMINATED (LT/RT TE FLAPS)

ALL EIGHT FLAP TRACK FIXED L/E FAIRINGS HAVE HEAVY EROSION AT FORWARD END WITH SEVERAL AREAS DELAMINATED AND CRACKED. REPAIRED DELAMINATION WITH FIBERGLASS OVERLAYS AND REPAIRED EROSION IAW SRM 51-40-09 AND 51-40-11.

Part: SLOT SEAL — CRACKED (NR 1 ENGINE)

CRACKED SKIN AT NR 1 ENGINE RIGHT SLOT SEAL FORWARD END. WELD REPAIRED PER BOEING SRM 51-10-01.

Part: SKIN — CHAFED (NR 4 TE MID FLAP)

CHAFED TO CORE MATERIAL UPPER SURFACE RIGHT OUTBOARD MID FLAP NEAR OUTBOARD END. REPAIRED PER BOEING SRM 51-40-06.

Part: TR SLEEVE — CORRODED (NR 4 ENGINE)

NR 4 ENGINE HAS SURFACE CORROSION ON THRUST REVERSER SLEEVE AT RT UPPER JACKSCREW BARREL NUT HOLES. REMOVED LEVEL ONE CORROSION AND TREATED IAW SRM 51-10-01.

Part: DOOR — CORRODED (RT MLG GEAR)

RIGHTHAND OUTBOARD BODY GEAR DOOR HAS LARGE AREA OF BARE METAL WITH SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-24-11, 51-10-01.

Part: BRACKET — CRACKED (NR 3 ENGINE)

NR 2 ENGINE AIR DUCT MOUNT ANGLE BRACKET IS CRACKED AT THE 6 O'CLOCK POSITION FORWARD OF MAIN GEARBOX. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-01.

Part: PRESS DECK — CORRODED (NLG WW)

NOSE WHEEL WELL UPPER PRESSURE DECK HAS NUMEROUS SPOTS OF BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02.

Part: OVERHEAT SENSOR — BARE WIRE (NR 2 PYLON)

DURING TAXI OUT, LEFT WING OVERHEAT LIGHT ILLUMINATED. RETURNED TO BLOCKS. FOUND NR 4 LED GROUP WITH AN AIR LEAK, REPLACED SEAL IAW MM 36-11-01. FOUND SENSOR NR 2 INBOARD OF NR 2 PYLON WITH A BARE WIRE. REPAIRED SAME IAW MM 26-18-02. L/E OVERHEAT SYSTEM CHECKS GOOD IAW MM 26-18-01.

Part: CONDITION MOTOR — INOPERATIVE (NR 2 ENGINE)

NR 2 ENGINE WOULD NOT START AFTER PUSH BACK, RETURNED TO BLOCKS. REMOVED AND REPLACED NR 2 FUEL CONDITION MOTOR PER MM 76-11-04.

Part: SEAL — LEAKING (LT WING)

****CORRECTION****RETURNED TO GATE DUE TO LEFT WING L/E OVERHEAT LIGHT CAME ON DURING PUSHBACK. REPLACED LEFT WING ANTI-ICE VALVE IAW MM 30-11-03. REPLACED D-D SEALS AT NR 4 LED UNIT AT 2 INCH DUCT ASSY AND TWO NEW CLAMPS INSTALLED AT THE MANIFOLD ELBOW AND LED UNIT IAW MM 27-81-03. PRESSURE CHECK NORMAL, NO OVERHEAT LIGHTS NOTED.

Part: OVERHEAT SW — MALFUNCTIONED (LT WING)

LEFT WING LEADING EDGE OVERHEAT LIGHT CAME ON AFTER ENGINE START. REPLACED OVERHEAT SWITCH INBOARD OF NR 2 ENGINE STA 388 IAW MM 26-18-02.

Part: TR DRIVE UNIT — INOP (NR 2 ENGINE)

NR 2 REVERSER DRIVE MOTOR FAILED AD 95-16-02 INSPECTION. PLACARDED AS INOP, REMOVED AND REPLACED NR 2 DRIVE UNIT AT LAX IAW MM 78-31-02.

Part: POSITION IND — FAILED (TE FLAPS)

WHEN EXTENDING FLAPS FOR APPROACH, OUTBOARD TRAILING FLAPS SPLIT: LEFT STAYED AT 1 DEGREE, RIGHT WENT TO 5 DEGREES. EXTENDED FLAPS BY ALTERNATE SYSTEM, FLAPS EXTENDED NORMALLY. FLAP TRANSMISSION SERVICED IAW MM 12-13-13. CHECKED FLAP POSITION INDICATION SYSTEM CABLE TENSIONS AND FOUND NORMAL IAW MM 27-58-02. REPLACED OUTBOARD FLAP POSITION INDICATOR AND OPS CHECK NORMAL IAW MM 27-58-00.

Part: PT7 LINE — BROKEN (NR 4 ENGINE)

ON TAKEOFF, LOST NR 1 AND NR 4 EPR INDICATION AND NR 3 AND NR 4 GENERATOR. TAKEOFF WAS ABORTED. REPLACED NR 3 GCU, GROUND CHECK OK. FOUND NR 4 GCR RACK PLUG LOOSE, SECURED AND GROUND RUN CHECK OK. FOUND NR 4 ENGINE PT7 LOOP LINE BROKEN AT ONE O'CLOCK POSITION. REPLACED LINE, GROUND RUN OK IAW MM 77-11-15. DEFERRED REPAIR OF NR 1 EPR.

Part: COUPLING — LOOSE (NR 1 PYLON)

ON BLOCK IN, GROUND PERSONNEL SAW TAILPIPE FIRE, NR 1 ENGINE. CREW DISCHARGED FIRE BOTTLE AND MOTORED ENGINE, PUT OUT FIRE. INSPECTED ENGINE AND PYLON FOR DAMAGE, NO STRUCTURES FOUND DAMAGED. FOUND AFT-MOST FUEL FEED LINE COUPLING LOOSE AND FUEL LEAK IN NR 1 PYLON. FOUND SAFETY WIRE BROKEN AT PIG TAIL. REPLACED O-RING AND TIGHTENED COUPLING IAW MM 28-22-07, OPS AND LEAK CHECK OK. PYLON CONDUCTIVITY INSPECTION OK.

Part: SEAT TRACK — CRACKED (RT COCKPIT)

FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED AND GOUGED. REPLACED SAME IAW MM 25-11-01, OPS CHECK OK.

Part: SEAT TRACK — CRACKED (RT COCKPIT)

FOUND FIRST OFFICER'S FORWARD INBOARD SEAT TRACK CRACKED. REPLACED SAME IAW MM 25-11-01, OPS CHECK OK.

Part: SEAT TRACK — CRACKED (LT COCKPIT)

FOUND CAPTAIN'S FORWARD OUTBOARD SEAT TRACK CRACKED. REPLACED SAME, OPS CHECK OK IAW MM 25-11-01.

Part: DNLOCK ACTUATOR — FAILED (RT MLG)

NR 1 HYDRAULIC SYSTEM FAILED WHEN LANDING GEAR WAS EXTENDED, DURING FINAL APPROACH. DUE TO UNSAFE, UNCOMPLETED GEAR EXTENSION, ALT EXTENSION WAS COMPLETED WITH NO EFFECT. ACCOMPLISHED BODY GEAR NOT EXTENDED CHECKLIST AND LANDED WITHOUT FURTHER INCIDENT. RIGHT BODY GEAR DOWNLOCK ACTUATOR REMOVED AND REPLACED IAW MM 32-33-15 PG 401.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

DURING PREFLIGHT INSPECTION, PILOT'S POSITION INDICATION SHOWED CARGO DOOR OPEN, FEO'S ANNUNCIATOR INDICATED AFT CARGO DOOR OPEN. ADJUSTED DOOR LATCH SWITCH IAW MM 52-34-09 AND OPS CHECK OK.

Part: ACTUATOR — CRACKED (NR 6 SPOILER)

DURING WALKAROUND, FOUND SEPARATION OF AFT END OF NR 7 GROUND SPOILER ACTUATOR. REPLACED CRACKED ACTUATOR IAW MM 27-11-15.

Part: POSITION IND — INOPERATIVE (OUTBD FLAP)

DURING TAXI OUT, LOWERING FLAPS, OUTBOARD FLAP POSITION INDICATIONS SPLIT LT/RT. SPLIT CAUSED ASYMMETRY LOCKOUT. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR IAW MM 27-58-00, PERFORMED SEVERAL OP CHECKS AND ALL FOUND NORMAL.

Part: FUEL CONTROL — OUT OF ADJUST (NR 3 ENGINE)

DURING TAKEOFF ROLL AT 40-60 KTS, A/C VEERED TO LEFT OF CENTERLINE. BROUGHT POWER BACK ON ALL ENG'S AND ABORTED TAKEOFF. ADVANCING POWER ON ALL ENGINES EVENLY UP TO 1.30 EPR. AT THAT TIME, NR 3 ENG EPR JUMPED TO 1.53, CAUSING A/C TO VEER. A/C WAS VERY LIGHT AND INCREASED EPR AT LOW GROUND SPEED PRODUCED ASYM THRUST. RE-CHECKED RIG AND FOUND TO BE WITHIN LIMITS. FOUND NR 3 FCU OUT OF RIG, RIGGED SAME AND C/W POWER RUN. OPS CHECKS GOOD PER MM 71-00-00.

Part: ENGINE — FAILED (NR 3)

THE NR 3 OIL PRESS LIGHT CAME ON, CONFIRMED OIL PRESS LOSS BELOW 40 PSI, SHUTDOWN ENGINE. REPLACED ENGINE IAW POLAR WORK CARD M7100-002A.

Part: STRAP — CRACKED (NR 3 PYLON)

CRACK ON NR 3 PYLON ENGINE AFT MOUNT SUPPORT BULKHEAD AT THE 6 O'CLOCK POSITION. FABRICATED NEW STRAP AND INSTALLED PER BOEING SRM 51-40-00.

Part: STRAP — CRACKED (NR 4 PYLON)

CRACK ON NR 4 PYLON ENGINE AFT MOUNT SUPPORT BULKHEAD AT THE 6 O'CLOCK POSITION. FABRICATED NEW STRAP AND INSTALLED PER BOEING SRM 51-40-00.

Part: FAN — FAILED (FWD CARGO)

NR 1 RECIRCULATION FAN INOPERATIVE. FAN BLADE FOUND CRACKED AND LODGED INTO FAN HOUSING BARREL. REPLACED, BENCH CHECK OK, AND REINSTALLED.

Part: HARNESS — LOW RESISTANCE (NR 3 MAIN TANK)

NR 3 MAIN FUEL QUANTITY INDICATOR ERRATIC AT CRUISE ALTITUDE, QTY ROLLS UP ABOUT DOUBLE THE AMOUNT OF FUEL AND THEN ROLLS BACK WITH PRESS TO TEST BUTTON. TROUBLESHOT SYSTEM, FOUND READINGS BELOW M/M REQUIREMENTS, REPLACED TANK HARNESS ASSY AND TESTED PER BOEING MAINTENANCE MANUAL 28-40-01.

Part: STIFFENER — CRACKED (RT WING)

CRACKED RIB STIFFENER, RIGHT WING INBOARD AILERON, INBOARD SUPPORT. INSTALLED NEW STIFFENER PER BOEING SRM 51-40-00 AND DRAWING 65B08150-2- ITEM 9.

Part: SKIN — CORRODED (LEFT WING)

LEFT WING UPPER SKIN RABBET AREA 3, BULGE ON LEADING EDGE SKIN AT WS 685 AFT OF LEADING EDGE FLAP. CORROSION REMOVED AND AFFECTED AREA RE-PROTECTED WITH 0.050 INCH MATERIAL, REMOVAL WITHIN LIMITS PER BOEING SRM 57-30-01 PAGE 2.

Part: STIFFENER — CRACKED (NR 3 PYLON)

CRACKED STIFFENER, NR 3 PYLON NACELLE, STATION 180 INBOARD SIDE, REPAIRED PER BOEING SRM 54-1003 FIG. 15.

Part: PANEL — ERODED (RIGHT WING)

RIGHT WING UPPER SURFACE FOUND ERODED. FIBERGLASS REPAIR REQUIRED FROM WING ROOT TO WING TIP. REPAIRED PER BOEING SRM 51-40-09 FINISH RESTORED.

Part: SPAR — CORRODED (WS 1555)

RIGHT WING FRONT SPAR LOWER RABBET AREA WS 1555 T-CHORD CORRODED. REPAIRED PER BOEING SRM 57-30-03.

Part: CONNECTOR — CONTAMINATED (NR 2 ENGINE)

HUNG START ENGINE NR 2. CLEANED AND SECURED CANNON PLUG ON FUEL CONDITION ACTUATOR, SUBSEQUENT ENGINE STARTS NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 2)

AFTER PUSHBACK UNABLE TO START NR 2 ENGINE. SHUTDOWN OTHER OPERATING ENGINES, INSPECTED INSTALLATION OF START VALVE AND FUEL CONDITION ACTUATOR, ALL FOUND NORMAL. START ATTEMPT AT GATE WAS NORMAL.

Part: FUEL INDICATOR — INOPERATIVE (NR 3 FUEL TANK)

DURING TAXI AFTER LANDING, NR 3 ENGINE FLAMED-OUT. CHECKED NR 3 FUEL TANK WITH STICK AND FOUND NO FUEL IN NR 3 TANK, FUEL QUANITY INDICATOR ON PLACARD. FUELED AIRCRAFT ENGINE, RUN OK.

Part: SWITCH — FAILED (STABILIZER)

DURING TAXI FOR TAKEOFF, CONSTANT TAKEOFF WARNING. RECYCLED ALL FLIGHT CONTROLS, NO HELP. RETURNED TO BLOCKS, OPERATIONAL CHECK OK PER BOEING MAINTENANCE MANUAL 31-26-00.

Part: TE PANEL — CRACKED (WING)

A 32 INCH CRACK IN LEFT WING TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER INBOARD END. REPAIRED IN ACCORDANCE WITH BOEING SRM 51-40-09.

Part: GEAR DOOR — LOOSE (RT MLG)

REPAIR COMING LOOSE AT OUTBOARD WING GEAR DOOR AT BOTTOM FORWARD END. REPAIRED PER BOEING 747 SRM 51-40-09.

Part: ROD — CRACKED (LT WING LE)

FOUND LEFT WING LEADING EDGE SUPPORT ROD CRACKED AREA OF NR 2 LEFT LEADING EDGE PDU. REMOVED AND REPLACED SUPPORT ROD AS PER BOEING SRM 51-10-01.

Part: PANEL — CRACKED (LT WING)

FOUND .5 INCH CRACK IN TRAILING EDGE LEFT WING FIBERGLASS PANEL FORWARD OF NR 6 SPOILER. REPAIRED PANEL PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LT WING)

FOUND 32 INCH CRACK IN LEFT WING TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER INBOARD END. REPAIRED IAW BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LT WING)

FOUND 17 INCH CRACK IN TRAILING EDGE LEFT WING FIBERGLASS PANEL FORWARD OF NR 6 SPOILER CENTER HINGE. REPAIRED PER BOEING SRM 51-40-09. (M)

Part: PANEL — DELAMINATING (RT WING)

FOUND RIGHT WING BOTTOM LEADING EDGE PANEL REPAIR IS DELAMINATING AT THREE CORNERS AFT OF NR 16 LEADING EDGE JACK SCREW. REPAIRED AS PER BOEING 747 SRM 51-40-06.

Part: PLATE — CRACKED (NR 3 PYLON)

FOUND NR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02.

Part: NUT — RUSTED (RT ELEVATOR)

RIGHT ELEVATOR HINGE NUT RUSTED AND ACTUATOR ROD END RUSTED. CLEANED AND TREATED AREA PER 747 SRM 51-12-01 (LEVEL 1).

Part: PLATE — TORN (FS 603)

FLOOR PLATE TORN AT FS 603 FORWARD OF BALL MAT AREA CENTER OF FLOOR. REPLACED PLATE AS BOEING SRM 51-10-01.

Part: SKIN — GOUGED (FWD FUSELAGE)

CO-PILOTS WINDSHIELD WIPER ARM HAS GOUGED FUSELAGE SKIN IN PARKED POSITION. SMOOTH BLENDED MILD GOUGE OUT PER BOEING SRM 51-10-01, RERIGGED WIPER.

Part: PANEL — DAMAGED (RT WING LE)

FOUND DAMAGED PANEL BOTTOM OF RIGHT WING LEADING EDGE AFT OF NR 23 LEADING EDGE SLAT AT JACK POINT. REPAIRED PER BOEING 747 SRM 51-40-09.

Part: MID FLAP — WORN (LT WING)

FOUND LEFT WING OUTBOARD MID FLAP OUTBOARD END WORN DOWN TO HONEYCOMB TOP SIDE. REPAIRED PER BOEING SRM 51-40-06 AND 51-70-09.

Part: PANEL — CRACKED (WING)

FOUND 6 INCH CRACK IN FIBERGLASS PANEL FORWARD OF NR 8 SPOILER AT OUTBOARD END. REPAIRED CRACKED PANEL PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (WING)

FOUND 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF PANEL 571CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09, FIGURE 10.

Part: RIVET — POPPED (NR 9 SLAT)

RIVET HEAD POPPED ON FORWARD SPAR CAP AFT OF NR 9 SLAT (INBOARD END). REPLACED RIVET PER BOEING SRM 51-30-03. (M)

Part: PANEL — CRACKED (WING)

A 6 INCH CRACK IN FIBERGLASS PANEL FORWARD OF NR 8 SPOILER AT OUTBOARD END. REPAIRED CRACKED PANEL PER BOEING SRM 51-40-09.

Part: SKIN — GOUGED (FWD FUSELAGE)

COPILOTS WINDSHIELD WIPER ARM HAS GOUGED FUSELAGE SKIN IN PARKED POSITION. SMOOTH BLENDED MILD GOUGE OUT PER BOEING SRM 51-10-01, RERIGGED WIPER.

Part: TE PANEL — CRACKED (WING)

A .5 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FWD OF NR 6 SPOILER. REPAIRED PANEL PER BOEING SRM 51-40-09.

Part: FLOOR PLATE — TORN (FS 603)

PLATE TORN FLOOR AT STA 603 FWD OF BALL MAT AREA CENTER OF FLOOR. REPLACED PLATE AS PER BOEING SRM 51-10-01.

Part: SKIN — WORN (LT TE MID FLAP)

LEFT WING OUTBOARD MIDFLAP OUTBOARD ENG WORN DOWN TO HONEYCOMB TOP SIDE. REPAIRED PER BOEING SRM 51-40-06 AND 51-70-09.

Part: ROD END — RUSTED (ELEVATOR)

RIGHT ELEVATOR HINGE NUT RUSTED AND ACTUATOR ROD END RUSTED. CLEANED AND TERATED AREA PER 747 SRM 51-12-01, LEVEL 1.

Part: PANEL — DAMAGED (RT HORIZ STAB)

HOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01.

Part: ROD — CRACKED (LT WING LE)

LEFT WING LEADING EDGE SUPPORT ROD CRACKED AREA OF NR 2 LEFT LEADING EDGE PDU. REMOVED AND REPLACED SUPPORT ROD AS PER BOEING SRM 51-10-01.

Part: TE PANEL — CRACKED (WING)

A 17 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER CENTER HINGE. REPAIRED PER BOEING SRM 51-40-09.

Part: TE PANEL — CRACKED (WING)

A 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL LOCATED FWD OF PANEL 571 CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09 FIG 10.

Part: PLATE — CRACKED (NR 3 PYLON)

NR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02.

Part: PANEL — CRACKED (WING)

A .25 INCH CRACK IN FIBERGLASS PANEL, FWD OF NR 9 SPOILER. REPAIRED PER SRM 51-40-09.

Part: PANEL — HOLE (RT HORIZ STAB)

FOUND HOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01.

Part: RIVET — POPPED (WING)

RIVET HEAD POPPED ON FORWARD SPAR CAP AFT OF NR 9 SLAT, INBD END. REPLACED RIVET PER BOEING SRM 51-30-03.

Part: BLKHD LINER — HOLE (FS 2160)

BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD NEAR CENTER. REPAIRED AS PER BOEING SRM 51-40-02.

Part: BLKHD LINER — HOLE (BS 2160)

BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02.

Part: KEEL BEAM — CORRODED (FUSELAGE)

ADF ANTENNA MOUNT STRUCTURE IS CORRODED (LEVEL 1) LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING SRM 51-10-01, PAGES 13, 14, 15, 16 PAR 6 AND 7. (M)

Part: BLKHD LINER — DAMAGED (BS 2160)

BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02. (M)

Part: TR SLEEVE — DELAMINATED (NR 1 ENGINE)

SMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02.

Part: TR SLEEVE — GOUGED (NR 1 ENGINE)

FORWARD EDGE OF NR 1 ENGINE FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH.

Part: COWL — WORN (NR 1 ENGINE)

TOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN ONE FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07.

Part: KEEL BEAM — CORRODED (FUSELAGE)

ADF ANTENNA MOUNT STRUCTURE IS CORRODED LEVEL 1, LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01 PAGES 13, 14, 15, 16 PAR 6 AND 7.

Part: PALLET GUIDE — PEELED (BS 6631)

FORWARD CARGO COMPARTMENT STATION 663 LEFT SIDE PALLET GUIDE SUPPORT METAL PEELED BACK. REMOVED AND REPLACED PALLET GUIDE AS PER SRM 51-10-01.

Part: SKIN — PUNCTURED (LT AILERON)

SMALL PUNCTURE 1.5 BY .5 LEFT WING INBOARD AILERON LOWER SKIN ALONG OUTER EDGE. SANDED AREA APPLIED FILLER PER BOEING SRM 51-40-09.

Part: TR SLEEVE — SCRATCHED (NR 4 ENG)

SCRATCHES RIGHT SIDE NR 4 ENGINE THRUST REVERSER SLEEVE FROM 3:30 TO 4:00 POSITION. REMOVED SCRATCHES AS PER BOEING SRM 51-10-01 PAGE 11 TREATED AND PAINTED AREA.

Part: BLKHD LINER — HOLE (FS 2160)

BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD NEAR CENTER. REPAIRED AS PER BOEING SRM 51-40-02.

Part: NUTPLATE — LOOSE (ABOVE NR 2 ENG)

ONE NUTPLATE LOOSE AND ONE NUTPLATE MISSING ON TOP LEADING EDGE ACCESS PANEL ABOVE NR 2 ENGINE. REMOVED AND REPLACED NUTPLATES PER BOEING SRM 51-10-01.

Part: SKIN — LOOSE (NR 3 PYLON)

NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVITS. INSTALLED ALL MISSING AND LOOSE AS PER BOEING SRM 51-30-02.

Part: TR SLEEVE — GOUGED (NR 1 ENGINE)

FORWARD EDGE OF FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH.

Part: SKIN — BENT (BS 2040)

FUSELAGE SKIN AT AFT BULK CARGO DOOR OPENING STATION 2040 IS BENT OUTWARD. REPAIRED AS PER BOEING SRM 51-40-01, PRIMED AND PAINTED.

Part: RIVET — SHEAR (BS 2040)

RIVET HEAD SHEARED ON LAP SEAM NR 34R STATION 2040 JUST AFT OF BULK CARGO DOOR. REMOVED RIVET, NO CORROSION FOUND, CLEANED AND SEALED AREA AND REPLACED RIVET AS PER BOEING SRM 51-30-02.

Part: KEEL BEAM — CORRODED (FUSELAGE)

ADF ANTENNA MOUNT STRUCTURE IS CORRODED (LEVEL 1) LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING SRM 51-10-01, PAGES 13, 14, 15, 16 PAR 6 AND 7.

Part: SKIN — CRACKED (NR 4 PYLON)

RIVET HEAD CRACKED ON NR 4 PYLON AFT OF SLOT SEAT LEFT SIDE LOWER SECTION. REMOVED AND REPLACED DAMAGED RIVET PER BOEING SRM 51-30-02.

Part: PANEL — DAMAGED (FUSELAGE)

FIBERGLASS PANEL NR 191X IS DAMAGED AT RADIO ALTIMETER INSTALLATION HOLE BOTTOM FUSELAGE 2ND PANEL AFT. REPAIRED PER BOEING 747 SRM 51-50-09, PAINTED.

Part: PANEL — CORRODED (FUSELAGE)

AREA OF CORROSION ON FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 ACM ACCESS DOORS (LEVEL 1). REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15, PARAGRAPH 6 AND 7.

Part: SKIN — LOOSE (NR 3 PYLON)

NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS AS PER BOEING SRM 51-30-02.

Part: SKIN — WORKING RIVETS (NR 1 TR UNIT)

SMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02.

Part: SKIN — PUNCTURED (LT AILERON)

FOUND SMALL PUNCTURE (1.5 INCH BY .5 INCH) LEFT WING INBOARD AILERON LOWER SKIN ALONG OUTER EDGE. SANDED AREA AND APPLIED FILLER PER BOEING SRM 51-40-09.

Part: FIRE WALL — WORN (NR 3 PYLON)

NR 3 PYLON IN 3RD AND 4TH INSPECTION PANEL TOP HOLE HYDRAULIC PRESSURE LINE FIREWALL FITTING JAM NUT NOT INSTALLED HOLE IS WORN ELONGATED. DRESSED AND CLEANED BULKHEAD FITTING HOLE AS PER SRM 51-10-02, INSTALLED AND SECURED SHOULDER BUSHING, AND BULKHEAD FITTING.

Part: SIDE COWL — WORN (NR 1 ENGINE)

TOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN WITH FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07.

Part: SKIN — LOOSE (NR 3 PYLON)

NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS PER BOEING SRM 51-30-02. AIRCRAFT TOTAL TIME: 69560. AIRCRAFT TOTAL CYCLES: 17553.

Part: BLKHD LINER — HOLE (BS 2160)

BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LT SIDE. REPAIRED AS PER BOEING SRM 51-40-02.

Part: RIVET — SHEARED (BS 2040)

RIVET HEAD SHEARED ON LAP SEAM NR 34R STA 2040 JUST AFT OF BULK CARGO DOOR. REMOVED RIVET, NO CORROSION FOUND CLEANED AND SEALED AREA AND REPLACED RIVET AS PER BOEING SRM 51-30-02.

Part: FIRE WALL — WORN (NR 3 PYLON)

NR 3 PYLON IN 3RD AND 4TH INSPECTION PANEL TOP HOLE HYDRAULIC PRESSURE LINE FIREWALL FITTING JAM NUT NOT INSTALLED HOLE IS WORN ELOGATED. DRESSED AND CLEANED BULKHEAD FITTING HOLE AS PER SRM 51-10-02, INSTALLED AND SECURED SHOULDER BUSHING, AND BULKHEAD FITTING.

Part: PALLET GUIDE — PEELED (BS 663L)

FORWARD CARGO COMPARTMENT STATION 663 LEFT SIDE PALLET GUIDE SUPPORT METAL PEELED BACK. REMOVED AND REPLACED PALLET GUIDE AS PER SRM 51-10-01.

Part: SKIN — CRACKED (RT NLG CUTOUT)

RIGHT NOSE GEAR TRUNNION CUTOUT HAS CRACK IN FORWARD UPPER CORNER IN WHEEL WELL SKIN, CRACK IN CORNER RADIUS GOING UP UNDER DOUBLER. ITEM REVIEWED BY BOEING, DETAILED VISUAL INSPECTION TO BE PERFORMED EVERY 250 CYCLES. REFERENCED BOEING LETTER PAOE 950531.

Part: SKIN — BENT (BS 2040)

FUSELAGE SKIN AT AFT BULK CARGO DOOR OPENING STATION 2040 IS BENT OUTWARD. REPAIRED AS PER BOEING SRM 51-40-01, PRIMED AND PAINTED.

Part: SKIN — CRACKED (LT NLG CUTOUT)

LEFT NOSE GEAR TRUNNION CUTOUT HAS CRACK IN FORWARD UPPER CORNER IN W/W SKIN, CRACK IN CORNER RADIUS GOING UP UNDER DOUBLER. ITEM REVIEWED BY BOEING, DETAILED VISUAL INSPECTION TO BE PERFORMED EVER 250 CYCLES. REFERENCE BOEING LETTER PAOE 950531.

Part: SKIN — CRACKS (NR 3 DOOR)

CRACKS COMING OUT OF 4 RIVET HOLES IN VERTICAL ROW APPROXIMATELY 18 INCHES BELOW WINDOW IN NR 3 REAR DOOR SKIN, MARKED. CUT OUT DAMAGE PER BOEING SRM 52-10-00, FIG 9. INSTALLED REPAIR DOUBLER PER SRM 50-10-00, FIG 9.

Part: PANEL — CORRODED (FUSELAGE)

FOUND SMALL AREA OF CORROSION FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 AIR CYCLE MACHINE ACCESS DOORS (LEVEL 1). REMOVED CORROSION ALODINED AND PAINTED PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15 AND 16, PARAGRAPH 6, 7.

Part: SKIN — CRACKED (NR 3 DOOR)

CRACKS COMING OUT OF 4 RIVETS HOLES IN VERTICAL LINE OF RIVETS APPROXIMATELY 18 INCHES BELOW FORWARD EDGE OF WINDOW IN NR 3 REAR DOOR SKIN. CUT OUT DAMAGE PER BOEING SRM 52-10-00, FIG 9. INSTALLED REPAIR DOUBLER PER SRM 50-10-00 FIG 9.

Part: SILL — CORRODED (FWD CARGO DOOR)

FORWARD CARGO DOOR LOWER SILL UPPER LIP JUST AFT OF NR 3 ROLLER HAS AREA OF CORROSION (LEVEL 1). REPAIRED IAW BOEING SRM 51-10-01.

Part: FUEL QTY IND — MALFUNCTIONED (NR 3 ENGINE)

AT FLIGHT LEVEL 33.0 SMOOTH AIR NR 3 ENGINE HAD LOUD BANG WITH FIRE BALL GOING FORWARD SHUTDOWN ENGINE. ON GROUND FOUND FUEL TANK EMPTY PLACARDED FUEL QUANTITY SYSTEM.

Part: FAN BLADES — DAMAGED (NR 4 ENGINE)

VCP - CREW FOUND 4 DAMAGED FAN BLADES IN NR 4 ENGINE. SUSPECT BIRD STRIKE. LANDING WAS MADE IN EXTREME WEATHER CONDITION. MAINTENANCE INSPECTED NR 4 ENGINE IAW MM 71-00-00. NO OTHER DEFECTS FOUND. FOUR SETS OF FAN BLADES WERE REPLACED PER MM 72-31-01. ACFT RELEASE FOR SERVICE.

Part: START VALVE — FAILED (NR 3 ENGINE)

VCP-CCS - EN ROUTE, THE NR 3 ENGINE START LIGHT CAME ON. ENGINE SHUTDOWN AND ACFT DIVERTED TO GIG. REMOVED AND REPLACED NR 3 ENGINE START VALVE IAW MM 80-10-00, AND CHANGED NR 3 ENGINE STARTER AS PRECAUTIONARY. OPERATIONAL CHECKS NORMAL. ACFT RELEASED FOR FLIGHT.