N672UP

Part: ENGINE — POWER LOSS (NR 3)

INSPECTION TYPE:N/A IFSD - AT FL360 AT CRUISE NR 3 ENG ROLLED BACK, CHECK FUEL PANEL ENG HAD PRESS VIA X FEED. ENG STILL ROLLING BACK. PLACED IGN TO FLT START, TEMP STARTED TO OVERTEMP. SHUT ENG DOWN. DESCENDED TO 28000. DID INFLIGHT RESTART AND ENG STARTED. PERFORMED INSPECTING OF NR 3 PER MM 71-00-42 AND 71-00-45 AND MM 71-00-00, 72-00-00. RAN ENG PER MM 71-00-00, 71-00-46. NO DEFECT NOTED, OK FOR SERVICE.

Part: HOSE — BURNED (WATER DRAIN)

INSPECTION TYPE:A CK DURING INSPECTION OF EO FOUND WATER DRAIN TUBE CRUSHED AND BURNED. ALSO, FOUND EVIDENCE OF BURNED INSULATION BLANKET REF EO B747-3670-27749B. ORDERED NEW HOSE ON REQ A940808. WORKING WITH ENG ON INSULATION. REPLACE HOSE ASSY PER B747-3070-27749.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SLIDE LIGHT INOP. REMOVED & REPLACED POWER SUPPLY MODULE X327 REF WD 33-51-12 AND MM 33-51-04, OPS CHECK GOOD.

Part: WATER SEPARATOR — CRACKED (NR 3 PACK)

ATB - AFTER T/O, NR 3 PACK WOULD NOT OPERATE. ZERO AIRFLOW. NO FUNCTION. SWITCHES AND C/B'S RECYCLED. TRIED IN MAN/AUTO. NO HELP. NOTE: ISOLATION A BLEED VALVES OPEN WITH NORMAL DUCT PRESSURE. T/S PERFORMED. FOUND NR 3 PACK WATER SEPARATOR FROZEN UP. WATER BAG CLEANED AND RE-INSTALLED. F/C NR 3 PACK AS PER MM 21-50-00. FOUND NR 3 WATER SEPARATOR DRAIN LINE WITH SMALL CRACK. DRAIN LINE TEMP REPAIR PERFORMED. DEFERRED UNDER D353304.

Part: PANEL — CRACKED (LT WING)

LEFT WING LOWER T/E PANEL HAS 5 FT CRACK. A/C IS OOS. [SUP 05-21-07] REMOVED PANEL FROM A/C. SENT TO SHEETMETAL SHOP. PANEL REINSTALLED IAW EO B747-5720-6416E.

Part: DOOR — MALFUNCTIONED (NLG)

NOSE GEAR DOORS OPENING DURING FLIGHT. REMOVED AND REPLACED NOSE GEAR DOOR SEQUENCE VALVE. OPS CHECK NORMAL. OK FOR CONTINUED SERVICE.

Part: UNKNOWN — UNKNOWN (ANTI SKID SYS)

DURING LANGING GEAR ROLL AT APPROX 95 KNOTS APPLIED MAXIMUM BRAKING EFFORT (BRAKE PEDALS PUSHED TO END OF THROW) AND THE ANTI SKID DID NOT CYCLE. ACCOMPLISHED HYD BRAKE SYS. ADJ/TEST MM 32-41-00. NO FAULT NOTED. ALL SATISFACTORY. CHECKED CABLE TENSIONS PER MM 32-41-00. CABLE TENSION CHECKED OK. TAXIED AIRCRAFT AND TESTED BRAKES. NO FAULTS NOTED WITH ALL SYSTEMS.

Part: BRAKE — STIFF (MLG)

BTB - APPLIED MAX BRAKING EFFORT AT 15 KNOTS GROUND SPEED. A/C CAME TO A SLOW GENTLE STOP. BRAKE PEDAL TRAVEL AND RESISTANCE IS INCONSISTANT WITH NORMAL BRAKING FEEL. T/S HYD BRAKE SYS IAW MM 32-41-00. CLEANED AND LUBED CABLE QUADRANTS. OPS CHECK NORMAL. A/C HAS NORMAL RESPONSE METERING VALVES INSTALLED.

Part: BRAKE — FAILED (MLG)

INSPECTION TYPE:N/A BTB - BRAKES BOTTOMED OUT DURING TAXI. BLED BRAKE SYS IAW 32-41-00. CK'D CABLE TENSION IAW AMM 32-41-00, PG 501. CABLE TENSION CKS GOOD. TAXIED A/C BRAKES OPERATE NORMAL IAW AMM 32-41-00 PG 1. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A AFT EMERGENCY LIGHT IN MAIN ENTRY DOOR INOP. RELAMP, NO HELP. REMOVED AND REPLACED BATTERY PACK PER CHAPTER 33. OPS CHECKS OK.

Part: SKIN — PUNCTURED (BS 203) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX- BS 203 RBL 3" EXTERIOR SKIN FOUND PUNCTURED, CRACK LENGTH 1/2". FX EXTERIOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 1, JUST BETWEEN BS 195 AND 208 STR -1L AND STR -1R.

Part: SEAT TRACK — CORRODED (FWD CARGO BAY) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT SEAT TRACK FOUND CORROSION AT STA 980 LBL 25. FWD CARGO COMPT BS 930 TO BS 980 LBL 25 AREA TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT STR 32R BETWEEN BS 2200 TO BS 2220 FOUND 1EA HOLE CRACK AS MARKED (AFTER SKIN TRIMMED OFF) CRACK LENGTH .125 INCH. AFT OF BULK CARGO COMPT BETWEEN BS 2181 TO BS 2220 STR 32R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (BS 460 S15L) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT SIDE BS 460 STR 15 STRINGER FASTENER HOLE CRACK FOUND RUNNING TO UPPER EDGE AND RUNNING DOWNWARD APPROX .25 INCH, CRACK LENGTH .5 INCH. M/D LEFT BS 460 STR 15L STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CORRODED (BS 1800-1820) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D AFTER BS 1800-1820 RIGHT WINDOW FORGING REMOVED FOUND STR 22R AFTER END CORRODED. CORROSION BLEND OUT 0.080 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 51873 FOR WORKING DETAIL.

Part: STRINGER — CORRODED (BS 1760-1780) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D AFTER BS 1760-1780 RIGHT WINDOW FORGING REMOVED FOUND STR 22R FWD END CORRODED AS MARKED. CORROSION BLEND OUT 0.039 X 1 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CORRODED (BS 1920-1940) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D AFTER BS 1920 TO BS 1940 RIGHT WINDOW FORGING REMOVED, STR 22R FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.040 X .5 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 AND 51-30-02 REFER NRC51873 FOR WORKING DETAIL AFTER COR BLENDED. ORIGINAL THICKNESS 0.104 INCH.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 980 RBL 11 SEAT TRACK O/B FLANGE FOUND CORROSION. M/D BS 950-1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: SUPPORT FITTING — CRACKED (FWD CARGO BAY) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 RBL 25. CRACK LENGTH 2 INCHES. FWD CARGO COMPT AT BS 980 RBL 25 AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RBL 11 SEAT TACK I-BEAM BS 1740-1760 LWR SPLICE CORRODED. M/D BS 1740-1760 RBL 11 SEAT TRACK I-BEAM LWR SPLICE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: ANGLE — CORRODED (BS 1480) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT LBL 25. CORROSION BLEND OUT 0.053 X .5 X 2 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FITTING — CRACKED (BS 980) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 LBL 45. CRACK LENGTH 4 INCHES. FWD CARGO COMPT BS 980 LBL 45 AFT FIXED STOP SUPPORT FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1850 LBL 33 SEAT TRACK I/B FLANGE FOUND CORRODED. M/D BS 1830-1870 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT STRINGER FOUND CORRODED AT STA1640 S40R. AFT CARGO COMPT BS 1632 TO BS 1648 STR 40R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER CLIP — CORRODED (BS 1860 S43R) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT - STRINGER CLIP FOUND CORRODED AT STA1860 S43R INSIDE OF TORQUE BOX. CORROSION BLEND OUT 0.040 X .5 X .5 INCH EXCEED SRM LIMIT. STRINGER CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2040-2060 RBL12 TIE DOWN TRACK FLANGE AREA LWR FACE FOUND CORROSION AS MARKED. M/D BS 2030-2130 RBL 11-33 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: FITTING — CRACKED (NR 3 NACELLE) · airframe 76,834 hrs · 22,085 cycles

NR 3 PYLON FWD B/H I/B HANGER FTG AREA FASTENER REMOVED UPPERR HOLE AT T/R SYNC LOCK MOD HFEC INSP FOUND WITH CRACK INDICATION, CRACK LENGTH 0.030". NR 3 PYLON FWD BULKHEAD CHORD REPLACED AS PER SRM 51-10-01 P9.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C NR 2 PYLON UPPER WING CAVITY O/B FRAME AT NAC STA 237 TOP CORNER AREA CRACKED AS RED MARKED. NR 2 PYLON AT NAC STA 237 O/B FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND SRM 51-30-02.

Part: BEAM — CRACKED (DOOR) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LT MED NR 4 FWD VERTICAL BEAM INTERIOR LOWER CORNER FOUND CRACKED. LT MED NR 4 FWD VERTICAL BEAM LOWER CORNER AREA REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT FLOOR SUPPORT FOUND CRACKED AT STA 1775 RBL 40. AFT CARGO COMPT FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1, JUST AT STA 1775 RBL 40 AREA.

Part: SKIN — CORRODED (BS 2200-2220) · airframe 76,834 hrs · 22,085 cycles

AFT BULK CARGO COMPT FX SKIN FOUND CORRODED BTN BS 2200 TO BS 2220 STR 33R TO 34R AS MARKED. CORROSION BLEND OUT 0.035" BY 1/2" BY 4" EXCEED SRM LIMIT. FX BS 2193 TO BS 2217 BTN STR 31R TO STR 34R SKIN REPAIRED AS PER SRM 53-30-03 FIG 17.

Part: INTERCOSTAL — DEFORMED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB FOUND DEFORMED BETWEEN BS 2220 AND BS 2240 STR 40R AS MARKED. AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST AT BS 2220 AND BS 2240 STR 40R AREA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BELOW FLOOR BILGE AREA SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 1740 STR 44L TO STR 47L (3EA). AFT CARGO COMPT BS 1740 BETWEEN STR -43L TO STR 47L AREA SHEAR TIE REPAIRED AND TIE CLIPS 5EA REPLACED AS PER SRM 53-10-04 FIG 42.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SUPPORT FITTING — CRACKED (BS 980) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LWR SURFACE FOUND CRACK AT STA 980 RBL 45. CRACK LENGTH 2 INCHES. FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: ANGLE — CORRODED (BS 1480) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT RBL 25. CORROSION BLEND OUT 0.060 X .5 X 3 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1960 STR 3L FRAME ATT TIE CLIP FOUND CRACK. M/D BS 1960 STR 3L FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT CARGO COMPT - LEFT FLOORBEAM LOWER SURFACE FOUND SURFACE CORROSION AT STA 1820 LBL 42 TO LBL 45 ANCHOR NUT AREA. CORROSION BLEND OUT 0.041 X 2 X 3 INCHES EXCEED SRM LIMIT. AFT CARGO COMPT - LEFT FLOORBEAM REPAIRED AT BS 1820 LBL 20 TO LEFT MOST O/B AS PER SRM 51-40-04 FIG 2.

Part: STRINGER — CRACKED (BS 2177 S28R) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CRACK AT BS 2177 STR 28 RIGHT AS MARKED. CRACK LENGTH 1.25 INCH. AFT OF BULK CARGO COMPT FX STRINGER S28R AT BS 2177 AREA REPAIRED AS PER RS R53-62-35735 AND UPS ENGINEERING FILE NR 747-53-20377.

Part: STRINGER — CRACKED (BS 2177) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT, FX STRINGER FOUND CRACK AT BS 2177 S46R AS MARKED, CRACK LENGTH 2". FX BS 2150 TO BS 2185 STR 46R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CORROSION CRACK AT BS 2177 STR 48 RT AS MARKED. AFT OF BULK CARGO COMPT - FX STRINGER 48R REPAIRED AS PER SRM 53-10-03 FIG 1, JUST BETWEEN BS 2150 AND 2185 AREA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D - BS 1760 FLOOR SUPPORT PLATE RBL 50-55 CORRODED. CORROSION BLEND OUT 0.045 X .5 X 1 INCH EXCEED SRM LIMIT. SUPPORT PLATE REPLACED AS PER SRM 53-40-00.

Part: STRINGER — DEFORMED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT STRINGER WEB FOUND DEFORM AT STA 2020-2040 S39L. BULK CARGO COMPT STRINGER WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST AT STA 2020-2040 S39L AREA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT LWR SURFACE FOUND CORROSION AT STA 2039 TO STA 2100 CENTER LINE TO RBL 2. BULK CARGO COMPT FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 AT STA 2030 TO STA 2160 RBL 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2240 LBL 33 SEAT TRACK CROWN FOUND CRACKED APPROX 3 INCHES LONG. M/D BS 2240 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST BETWEEN BS 2230 AND BS 2280.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2040 LBL 85 FLOORBEAM FOUND CORRODED. M/D BS 2040 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1 JUST BETWEEN LBL 43 AND LBL 118 LT MOST O/B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C AFT COMPT - RIGHT STA 1580 FRAME AFT FACE UPPER EDGE AT S39 TO S40 CRACKED. AFT CARGO COMPT BS 1580 AT STR 39R STRINGER STR 39R-40R AREA FRAME REPAIRED AS PER SRM 53-10-04 FIG 69.

Part: STRINGER — CORRODED (BS 2150-2160) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CORRODED AT STA 2150 TO 2160 S31L. CORROSION BLEND OUT 0.080 X .375 X 1.5 INCH EXCEED SRM LIMIT. STRINGER 31L REPAIRED AS PER SRM 53-10-03 FIG 2, JUST BETWEEN BS 2156 AND BS 2170.

Part: FLOOR SUPPORT — CRACKED (BS 1525-1535) · airframe 76,834 hrs · 22,085 cycles

FOUND RBL117 FLR SUPPORT BS 1525-1535 CRACKED, CRACK LENGTH 7/8". BS 1525-1535 RBL117 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RBL 11 SEAT TRACK BS 1760 - 1780 LT SPLICE CRACKED. M/D RBL 11 SEAT TRACK LT SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST BETWEEN BS 1760 AND BS 1780 AREA.

Part: SEAT TRACK — CORRODED (BS 957-964) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT RIGHT SIDE SEAT TRACK LWR SURFACE FOUND CORROSION AT STA 957 TO 964 RBL 45. CORROSION BLEND OUT 0.045 X .5 X 7 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 5, JUST AT RBL 45 BETWEEN BS 930 AND 967.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1000 RBL 33 SEAT TRACK SUPPORT FOUND CRACKED. M/D BS 1000 RBL 33 SEAT TRACK SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: LONGERON — CORRODED (RT MLG WW) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C L/G - RIGHT WLG W/W OVERWING LONGERON WEB UPPER SURFACE AT BS 1258-1261 FOUND CORROSION AND CRACKED. CORROSION BLEND OUT 0.055 X .5 X 3 INCHES EXCEED SRM LIMIT. L/G - RIGHT WLG W/W OVERWING LONGERON WEB REPLACED AT BS 1254-1264 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RBL 97 SEAT TRACK BS 1500-1584 CORRODED. CORROSION BLEND OUT 0.040 X .75 X 3 INCHES EXCEED SRM LIMIT. M/D SEAT TRACK REPAIRED AT BS 1480-1590 RBL 97 AS PER SRM 53-10-05 FIG 1A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2152 LBL100 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X .5 X 1 INCH EXCEED SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2, JUST AT LBL 100 BETWEEN BS 2130 AND 2160.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2040-2140 RBL 98 SEAT TRACK CROWN ATT BOLTS AREA FOUND CORRODED. CORROSION BLEND OUT 0.070 X .75 X 3 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A, JUST AT RBL 98 BETWEEN BS 2090 AND 2150.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2180 S25R FRAME ATT TIE CLIP FOUND CRACKED. M/D BS 2180 S25R FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT STRINGER CLIP FOUND CORRODED AT STA 2060 S28L. CORROSION BLEND OUT 0.030 X .5 X .5 INCH EXCEED SRM LIMIT. BULK CARGO COMPT STRINGER CLIP REPLACED AT STA 2060 S28L AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT BLG ACTUATOR UPPER SUPPORT FITTING I/B LUG BORE FOUND CRACKED. CRACK LENGTH 0.25 INCH. LEFT BLG ACTUATOR UPPER SUPPORT FITTING REPLACED IAW UPS EO B747-5340-0994-D APP 8.4 TO 8.6.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT FOUND CORRODED AT STA 2100 AND STA 2140 LBL 55. BULK CARGO COMPT FLOOR SUPPORT REPAIRED AT BS 2090-2160 LBL 55 AS PER SRM 51-40-04 FIG 2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO RIGHT BS 760-780 S34R FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 4 INCHES EXCEED SRM LIMIT. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 745 STRINGER S35L FOUND CRACK. CRACK LENGTH .25 INCH. FWD CARGO COMPT STA 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 840-845 S37R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 830 TO BS 850 STR 37R AREA REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 800 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 745 S39L. FWD CARGO COMPT BS 740-770 STR 39L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 945 S35R. FWD CARGO COMPT BS 930 TO BS 950 STR 35R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 845 S35L. CRACK LENGTH .5 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 820-840 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO RT BS 760-780 STRINGER S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 780-800 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CORROSION AT STA 780 S35L. CORROSION BLEND OUT 0.041 X .75 X 2 INCHES EXCEED SRM LIMIT. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 800-820 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 820-840 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FRAME — CRACKED (BS 2180 S25-26R) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2180 STR 25-26R FRAME CRACKED. CRACK LENGTH .5 INCH. M/D BS 2180 STR 25-26R FRAME REPAIRED AS PER RS R53-62-35728 AND UPS EO B747-5310-26045.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 500 S32R I/B CLIP FOUND CRACKED AS MARKED. FWD CARGO BS 500 S32R I/B CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 780-800 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 800-820 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 820 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 790 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D - BS 2320 STR 18-19L FRAME FOUND CRACK. M/D BS 2320 STR 18-19L FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: SHEAR TIE — CRACKED (BS 700) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO RT BS 700 STR 30R TIE CLIP FOUND CRACKED AS MARKED, CRACK LENGTH 1/4". FWD CARGO RT BS 700 STR 30R TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER CLIP — CORRODED (BS 1980) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT FRAME ATT STRINGER CLIP FOUND CORROSION AT STA 1980 RBL41 STR 45R. CORROSION BLEND OUT 0.050" BY 1" BY 1" EXCEED SRM LIMIT. BULK CARGO COMPT FLOOR SUPPORT FRAME ATTACH STRINGER CLIP REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02 JUST AT BS1980 R13L AND S45R.

Part: DOUBLER — CORRODED (MLG WW) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C L/G - LT WLG W/W AT BS1245 LBL0 HYD TUBE CUTOUT DOUBLER FOUND CORRODED CRACKED. CORROSION BLEND OUT 0.045" BY 1/2" BY 4" EXCEED SRM LIMIT. DOUBLER REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 1800 S22-23R) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1800 STR 22-23R FRAME I/B CHORD FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 1800 STR 22-23R FRAME I/B CHORD REPAIRED AS PER RS R53-62-35721 AND UPS EO B747-5310-26036.

Part: STRINGER — CRACKED (BS 900-910 S28L) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 900 AND STA 910 S28L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 890-950 STR 28L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2180 STR 13R FRAME ATT TIE CLIP FOUND CRACK. M/D BS 2180 STR 13R FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2320 STR 20-21R FRAME FOUND CRACK. M/D BS 2320 STR 20-21R FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO LT BS 540 STRINGER S31R TIE CLIP FOUND CRACKED AS MARKED. FWD CARGO RT BS 540 STRINGER S31R TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT FRAME STRINGER CLIP FOUND CORROSION AT STA 980 S37L. CORROSION BLEND OUT 0.037 X .5 X .5 INCH EXCEED SRM LIMIT. FWD CARGO COMPT STA 980 S37L STRINGER CLIP REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1920 STR 12-13R FRAME I/B CHORD FOUND CRACK. M/D BS 1920 STR 12-13R FRAME I/B CHORD REPAIRED AS PER SRM 53-10-04 FIG 87.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 880 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO BS 500 S33R CLIP FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 500 STR 33R TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CORRODED (BS 920-930 S28L) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CORROSION AT STA 920-930 S28L. CORROSION BLEND OUT 0.035 X .5 X 10 INCHES EXCEED SRM LIMIT. STRINGER 28L REPAIRED AS PER SRM 53-10-01 FIG 1, JUST BETWEEN BS 890-950.

Part: FRAME — CRACKED (BS 2140 S25-26L) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 2140 STR 25-26L FRAME FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 2140 BEWTEEN STR 25-26L FRAME REPAIRED AS PER RS R53-62-35726. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-62-35726 AND UPS EO B747-5310-26041.

Part: PANEL — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1010-1090 CTR SHEAR PANEL EDGE FOUND CORRODED. CORROSION BLEND OUT 0.035 X .5 X 20 INCHES EXCEED SRM LIMIT. SHEAR PANEL REPLACED AS PER MM 20-51-01 AND PILOT HOLES REPAIRED AS PER RS R53-41-35733 AND UPS ENGINNERING FILE 747-53-20388.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1954-1958 STR 1R STRINGER END FOUND CRACK. M/D BS 1920-1958 STR 1R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 4 TABLE 3.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1000 RBL 11 SEAT TRACK LOWER SPLICE FOUND CORROSION. CORROSION BLEND OUT 0.030 X .5 X 1 INCH EXCEED SRM LIMIT. M/D BS 1000 RBL 11 SEAT TRACK LOWER SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1961-1964 STR 1R STRINGER END STRINGER SPLICE FITTING FOUND CORROSION. CORROSION BLEND OUT 0.080 X .375 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1954-1966 STR 1R STRINGER SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 1732-1738 STR 2L STRINGER END SPLICE FOUND CORROSION. M/D BS 1732-1748 STR 2L STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER SPLICE — SCRATCHED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX - MEC LT TUNNEL STA 300 S28AL STRINGER SPLICE FOUND SCRATCH MARK. FX - MEC LT TUNNEL BS 300 STR 28AL STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: VERTICAL BEAM — CRACKED (NLG WW) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C NWW TUNNEL RT BS 320 VERTICAL BEAM WEB WL 190 STAND OFF HOLE FOUND CRACKED. NWW RT TUNNEL BS 320 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX - KEEL BEAM FAIRING SUPPORT LOWER SURFACE FOUND CORROSION AT STA 1405 TO STA 1416 LBL 16. CORROSION BLEND OUT 0.017 X .5 X 10 INCHES EXCEED SRM LIMIT. SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: BEAM — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C NWW RT TUNNEL BS 300 VERTICAL BEAM WEB WL 190 STAND OFF HOLE FOUND CRACKED. NWW RT TUNNEL BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX REAR BODY FAIRING SUPPORT LWR SURFACE FOUND CORROSION AT STA 1520 TO STA 1525 CENTER SUPPORT. BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C NWW TOP PANEL AREA FOUND 1EA STIFFENER CRACKED AT BS 290 RBL 20 AS MARKED. NWW TOP PANEL AREA 1EA STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: PLATE — MISREPAIRED (BS 800) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D LEFT BS 800 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D LEFT BS 800 TENSION TIE ATTACHED STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35710. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35710 AND UPS EO B747-5310-25925.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1460 LBL 16 TO RBL 16. CORROSION BLEND OUT 0.029 X 1 X 10 INCHES EXCEED SRM LIMIT. FX KEEL BEAM PANEL SUPPORT REPLACED AT STA 1460 LBL 16 TO RBL 16 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1427 LBL 16 TO RBL 16. CORROSION BLEND OUT 0.025 X .5 X 10 INCHES EXCEED SRM LIMIT. FX - KEEL BEAM PANEL SUPPORT REPLACED AT STA 1427 LBL 16 TO RBL 16 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: TENSION TIE — CRACKED (BS 940) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D LEFT BS 940 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE AFT CHANNEL RUNNING UP THRU THICKNESS APPROX 0.060 INCH, CRACK LENGTH 0.060 INCH. M/D LT BS 940 TENSION TIE LT AFT CHANNEL REPAIRED AS PER RS R53-25-35712. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35712 AND UPS EO B747-5310-25927.

Part: PLATE — MISREPAIRED (BS 780) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D LEFT BS 780 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D LEFT BS 780 TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35713. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35713 AND UPS EO B747-5310-25938.

Part: PLATE — MISREPAIRED (BS 900) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RIGHT BS 900 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 900 TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35715. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35715 AND UPS EO B747-5310-25936.

Part: PLATE — MISREPAIRED (BS 800) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RIGHT BS 800 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 800 TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35710. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35710 AND UPS EO B747-5310-25925.

Part: PLATE — MISREPAIRED (BS 920) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RIGHT BS 920 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 920 TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35716. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35716 AND UPS EO B747-5310-25932.

Part: TENSION TIE — CRACKED (BS 780) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RIGHT BS 780 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE CHANNEL RUNNING UP AND DOWN APPROX .0625 INCH CRACK LENGTH .125 INCH. M/D RIGHT BS 780 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35713, CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35713 AND UPS EO B747-5310-25938.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LT BS 980 STR 38L AT DRAG SPLICE FITTING AREA FOUND 1EA FASTENER HOLE CRACKED AT SKIN APPROX .0625" RUNNING DOWNWARD. SKIN REPAIRED AS PER SRM 53-30-03 FIG 60. JUST BETWEEN BS 950 & 987 STR 37L TO 39L / OVERLAPPED SKIN REPAIRED AS PER SRM 53-30-03 FIG 12, BETWEEN BS 968.5 & 984 STR 39L AREA.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP INBOARD FWD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.

Part: TENSION TIE — CRACKED (BS 920 S8-9L) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D BS 920 STR 8-9L TENSION TIE LEFT O/B AFT CHANNEL FOUND CRACK. CRACK LENGTH .125 INCH. M/D BS 920 STR 8-9L TENSION TIE LEFT O/B AFT CHANNEL REPAIRED AS PER RS R53-25-35716. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35716 AND UPS EO B747-5310-25932.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP LWR AFT INBOARD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.

Part: TENSION TIE — CRACKED (BS 840) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE FWD CHANNEL (CRACK LENGTH 0.060"). M/D LEFT TO RIGHT TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02 & UPS EO B747-5310-23715 APPENDIX B REFER HX NRC AFF502047 FOR WORKING DETAIL.

Part: PANEL — DELAMINATED (LT WING) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT WING INBOARD TRAILING EDGE MID FLAP LWR OUTBOARD AFT PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.

Part: TENSION TIE — CRACKED (BS 840) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D LEFT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT FWD CHANNEL APPROX 0.060" RUNNING UP. M/D LEFT TO RIGHT TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02 & UPS EO B747-5310-23715 APPENDIX B.

Part: FRAME — CRACKED (BS 920) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT BS 920 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA FASTENER HOLE CRACKED AT FRAME APPROX 0.040" RUNNING UPWARD AND DOWNWARD. M/D LEFT BS 920 FRAME 1EA HOLE OVERSIZED BY INCREMENTS TO 0.247" DIA. CRACK FREE INSPECTED BY HFEC PER NTM PART 6 51-00-00 FIG 16, FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APPENDIX B.

Part: TENSION TIE — CRACKED (BS 840) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D- RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TIE CLIP APPROX 0.040 INCH RUNNING UP. M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION TIE CLIP REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C LEFT WING - NOSE UPPER CHORD ATT ANGLE AT WS 1112 FOUND CRACKED. CRACK LENGTH 1.125 INCH. LEFT WING NOSE UPPER CHORD REPAIRED AS PER SRM 57-20-03 FIG 7.

Part: FRAME — CRACKED (BS 840) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C M/D - RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 2EA HOLES CRACK AT FRAME (0.040" & 0.060"). M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION I/B & O/B 2EA HOLES OVERSIZED BY INCREMENTS TO 0.309" DIA. CRACK FREE INSPECTED BY HFEC PER NTM PART 6 51-00-00 FIG 16, FASTENERS INSTALLED AS PER UPS EO B747-5310-23715 APP B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX STA 1171 FAIRING SUPPORT FRAME FOUND CORRODED AT LBL 49. FX BS 1171 LBL 49 FAIRING SUPPORT REPAIRED AS PER SRM 53-50-04 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C FX STA 1171 FAIRING SUPPORT FRAME FOUND CORRODED AT RBL 12 AS MARKED. FX BS 1171 FAIRING SUPPORT FRAME UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 76,834 hrs · 22,085 cycles

INSPECTION TYPE:C WAN#1068883 - REPLACE MAIN DECK CENTER SHEAR FLOOR PANEL P/N: 65B16351-12 LOCATED BTN BS1170 AND BS1253 LBL11 TO RBL11. CENTER SHEAR FLOOR PANEL REPAIRED AS PER BOEING MES 1-276210464-1 AND -2 AND RS R53-41-35733. REPEAT INSPECTION ON ALL PILOT HOLES IS REQUIRED UNTIL THE FLOOR SHEAR PANELS ARE REPLACED AND REFER UPS ENGINEERING FILE NO.747-53-20388.

Part: SKIN — PUNCTURED (FS 1800 S37R) · airframe 76,733 hrs · 22,063 cycles

PUNCTURE IN FUSELAGE, STA 1800 FWD OF AFT CARGO DOOR. REPAIRED FUSELAGE SKIN AT STA 1800, S-37R-S-38R IAW SAA EA NR 747- 5330-01-A0553, UPS EO B747-5330-25724-A. THIS REPAIR IS AN ALTERNATE MEANS OF COMPLIANCE TO AD 2004-07, AD 2006-22-09, WITH REPEAT INSPECTIONS AT EVERY 1,500 FLIGHT CYCLES, AND FAA FORM 8100-9

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT UPPER DECK DOME LIGHT ASSY INOP. REMOVE AND REPLACED BATTERY ASSEMBLY IAW MM 33-51-07.

Part: ENGINE — SHUTDOWN (NR 3)

NR 3 ENG SHUT DOWN DUE TO AN OIL FILTER BYPASS LIGHT AND SPIKE IN OIL TEMP. AN EMERGENCY WAS DECLARED. REMOVED OIL FILTER DIFFERENTAIL PRESSURE SWITCH ON NR 3 ENGINE PER B747 MM 79-35-01. THIS CLEARS M333490. ENGINE RUN & LEAK CHECK COMPLIED WITH. CLOSING LP 663744.

Part: LIGHT — INOPERATIVE (ENTRY DOOR)

INSPECTION TYPE:A FWD EMERGENCY DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT AISLE, OPS CHECKS GOOD.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 75,650 hrs · 21,773 cycles

NOSE WHEEL WELL LT SIDE PANEL WEB FOUND CRACK AT BS 270 WL 170 APPROX 1/8". CRACKED WEB REPAIRED AS PER SRM 53-10-04 FIG 116, UPS MPI NR P18507 ISSUED TO CARRY OUT REPEAT INSPECTION INTERVAL PER SRM 53-10-04 PG 708 FIG 116.

Part: LINK — CRACKED (NR 1 PYLON) · airframe 74,588 hrs · 21,545 cycles

INSPECTION TYPE:AD NR 1 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG EXCEEDED LIMIT. NR 1 ENG REAR MOUNT THRUST LINK REPLACED AS PER EO B747-7120-22596-A ON APPENDIX-F. ENG REMOVED AND REINSTALLED AS PER UPS TASK CARD TC 5000.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

UPPER DECK SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM 33-51-05 OPS CK OK.

Part: WEB — CORRODED (A/C BAY) · airframe 73,825 hrs · 21,397 cycles

FX AIR CONDITIONING BAY REAR FIXED FAIRING INTERIOR ANGLE FOUND CORROSION AT STA 1241 LBL 50 O/B GROUND AIR SUPPLY VALVE AREA. CORROSION BLEND OUT 0.090 BY 0.75 BY 2.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, WEB AND INTERIOR ANGLE REPAIRED AS PER SRM 51-40-02 FIG 1 AND 51-40-04 FIG 1.

Part: SPAR — CRACKED (LT WING) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE: C, LT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE AT WS 392 CRACK RUNNING AFT APPROX 0.080 INCH. LEFT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE REPAIRED AT WS 392 AREA AS PER HX RS R57-25-35337 & UPS EO B747-5730-22494-A.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. M/D BS 640-770 LBL 98 TIE DOWN TRACK CROWN AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.060 BY 1 BY 5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, TRACK REPAIRED AT BS 640-770 LBL 98 AS PER SRM 53-10-05 FIG 1A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 760 LBL 80 HANDLING SUPPORT FTG FOUND CORRODED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CORRODED (LT WING) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE: C, AFT T/E PANEL REMOVED FOR RECTIFICATION WING UPPER SKIN LWR SURFACE FOUND CORRODED AT WS 390. CORROSION BLEND OUT 0.131 X 1.25 X 2.5 INCHES EXCEED SRM 57-30-01 FIG 1 LIMITS, LEFT WING UPPER SKIN LOWER SURFACE REPAIRED AT WS 390 AREA AS PER HX RS R57-25-35337 & UPS EO B747-5730-22494-A.

Part: SPAR — CRACKED (FUSLEAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE: C, RT SIDE OF BS 1241 UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 HOLE FOUND CORRODED CRACKED AT SPAR CHORD HORIZONTAL FLANGE LWR SURFACE WITH DEPTH 0.060 INCH & LENGTH 0.050 INCH APPROX. RIGHT BS 1241 UPPER CHORD BOLT HOLE NR 5 REPAIRED AS PER EO B747-5740-17032-C.

Part: FITTING — CRACKED (RT WING) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE: C, RIGHT WING UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 FASTENER HOLE FOUND CRACK AT INTERNAL SPLICE FITTING (CRACK LENGTH .25 INCH). RIGHT WING INTERNAL SPLICE FITTING BOLT HOLE NR 5 REPAIRED AS PER HX RS R57-18-35333 & UPS EO B747-5710-22476-A.

Part: FLOORBEAM — DEFORMED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C . AFT CARGO - STA 1580 BL 0 FRAME UPPER CHORD DEFORMED. AFT CARGO BAY, BS 1580 LBL 16 TO RBL 16 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2 REF NRC NR 6699.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

AFT CARGO STA 1640 RBL 28 FRAME LWR SHEAR TIE RIVET HOLE EDGE FOUND CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FRAME — CORRODED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 35 FRAME UPPER CHORD LWR SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.022 BY 1.5 BY 2 IN. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

CARGO BAY, STA 2180 RBL 58 FRAME UPPER CHORD LWR SURFACE FOUND CRACKED. CRACK LENGTH 1.25 IN . CORROSION BLEND OUT N/A. CARGO BAY STA 2180 RBL 58 IN FRAME REPAIRED AS PER SRM 53-10-04 FIG 66.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. AFT CARGO, LT BS 1560 WL 118 LBL 33 TO LBL 50 FRAME UPPER CHORD LWR SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.036 BY 2 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FRAME — CORRODED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 42 FRAME UPPER CHORD LWR SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.022 BY 1.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: STRUCTURE — CRACKED (AFT CARGO BAY) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. AFT CARGO - STA 1580 RBL 7 FRAME UPPER CHORD JUST UNDER ROLLER TRACK FOUND CRACKED. CRACK LENGTH 0.75. AFT CARGO BAY BS 1580 LBL 16 TO RBL 16 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FRAME — CHAFED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 37 FRAME UPR CHORD LWR SURFACE CHAFING. REFER NRC NR 6784 FOR WORK DETAIL BS 1600 RBL 8. RT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

AFT CARGO LT BS 1900 STR 43L FRAME WEB STRINGER CUTOUT SUSPECTED CRACKED. CRACK LENGTH 0.5 IN. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 42.

Part: FITTING — CRACKED (RT WING) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C RIGHT WING STA 1241 UPPER REAR SPAR SIDE OF BODY SPLICE FITTING NR 4 HOLE FOUND CRACK & COR AT INTERNAL SPLICE FITTING. RIGHT WING BS 1241 BOLT HOLE NR 4 HOLE REPAIRED AS PER SB B747-5740-17032.

Part: FRAME — CRACKED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

AFT CARGO, STA 1560 RT FRAME UPR FLANGE FOUND CRACK JUST BELOW SLOPE PANEL SUPPORT, CRACK LENGTH 2.0 IN. AFT CARGO BAY BS 1560 BTN STRINGER 36R - 38R FRAME REPAIRED AS PER SRM 53-10-04 FIG 66 DETAIL 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 540-580 LBL 27, SEAT TRACK CORRODED. CORROSION BLEND OUT 0.051 BY .375 BY 4 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C FX - LT STA 1241 FORGING TO KICK FITTING BOLT HOLES FOUND CORRODED (FINAL HOLE SIZE: 1.173 INCH). FORGING BOLT HOLE REPAIRED AS PER HX RS R53-43-35324 & UPS ENGINEERING FILE 747-53-20264.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO BAY BS 1680 STR 30R LWR AREA FOUND CORRODED. CORROSION BLEND OUT 0.032 BY 1 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2 AT BS 1671 TO BS 1690 STR 30R AREA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, LT BS 340 UPPER DECK FLOORBEAM TO FRAME JUNCTION AREA FOUND 1 EA HOLE CRACK AT FLOORBEAM WEB THRU THICKNESS RUNNING I/B, CRACK LENGTH 0.040 IN. FLOORBEAM WEB REPAIRED AT LBL 45 IN TO LT O/B AREA AS PER SRM 53-10-07 FIG 11.

Part: FRAME — CRACKED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO BS 1500 FRAME FOUND CRACKED JUST BELOW MOST RT HAND ROLLER TRACK AS MARKED. CRACK LENGTH 3 IN. AFT CARGO BAY FRAME AT BS 1500 STR 40R AREA REPAIRED AS PER HX RS NR R53-62-35329 AND UPS EO NR B747-5310-22463-A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

LT BS 340 UPPER DECK FLOORBEAM TO FRAME FUNCTION AREA FOUND 1EA HOLE CRACK AT FLOORBEAM UPPER CHORD APPROX 0.040 IN RUNNING DOWNWARD. CRACK LENGTH 0.040 INCH. CORROSION BLEND OUT N/A. LT BS 340 UPPER DECK FLOORBEAM UPPER CHORD REPAIRED AT LBL 35 TO LT MOST O/B AREA AS PER SRM 53-10-07 FIG 23.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 910 RBL 11-33 LATERAL HAT SECTION FWD FLANGE FOUND CRACKED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, LATERAL HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. U/D, BS 520 TO 600 RBL 10 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 BY 0.5 BY 2.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4 AT BS 520 TO 610 RBL 10 INCH AREA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 520-600 RBL 47 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.048 BY 0.5 BY 3.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, AFT CARGO, LT BS 1520 FRAME SHEAR TIE FOUND CORRODED AT STR 33L TO STR 34L. CORROSION BLEND OUT 0.029 BY 0.75 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SHEAR TIE ATTACH BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1520 STR 33L - 34L AREA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. U/D BS 400 RBL 11-14 FLOORBEAM UPPER CHORD FOUND SLIGHT CORROSION. CORROSION BLEND OUT 0.038 BY 0.5 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1 AT BS 400 RBL 7 - 18"AREA.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

RT BS 340 U/D FLR BEAM TO FRAME FUNCTION AREA FOUND 1EA HOLE CRACK AT FLOORBEAM WEB THRU THICKNESS RUNNING I/B, CRACK LENGTH 0.125 IN. FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. U/D, BS 400, RBL 0-6 FLOORBEAM UPPER CHORD FOUND SLIGHTLY CORRODED. CORROSION BLEND OUT 0.040 BY 0.875 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 640 RBL 47 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.040 BY 0.5 BY 1.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. U/D, BS 540 TO 630 RBL 28 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.049 BY 0.5 BY 4 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 540-630 RBL 28 AREA.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C , AFT CARGO, LT BS 1596 TO 1602 STR -35L STRINGER FOUND CORRODED. CORROSION BLEND OUT 0.038 BY 0.5 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 JUST BETWEEN BS 1590 AND 1610 STR 35L AREA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. U/D, BS 530-580 RBL 65 IN SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.042 BY 0.3750 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 530-590 RBL 65 AREA.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

SHEAR PNL AT BS 1170 TO BS 1260, LBL 11 - RBL 11 EDGE CORRODED AND DELAMINATION. CORROSION BLEND OUT 83 BY 22 BY 0.010 IN. SHEAR PNL REPAIRED AS PER HX RS NR R-53-20-35335 AND UPS EO NR B747-5320-22500-A.

Part: STRUCTURE — CRACKED (CREW DOOR) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, U/D CREW DOOR LWR BEAM WEB CTR CRACKED, CRACK LENGTH 0.375 IN. U/D CREW DOOR LOWER BEAM WEB CENTER AREA REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. FWD CARGO BAY LT SUPPORT FRAME INNER CHORD FOUND CRACKED AT STA 940 STR 34L HI LOCK CUTOUT AREA, CRACK LENGTH 0.625 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

STA 518-523 LBL 47 INCH SEAT TRACK CORROSION. CORROSION BLEND OUT 0.033 BY 0.5 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C LH BS 914 STR -39L FOUND OUTER SKIN CORROSION AT TOP ROW FASTENER LOCATION MATER LOSE APPROX 15 PERCENT. CORROSION BLEND OUT 0.010 BY 1.0 BY 25 IN. EXCEED SRM 53-30-01 FIG 1 LIMITS. SKIN REPAIR AS PER SRM 53-30-03 FIG 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, U/D STA 521-522 LBL 66 SEAT TRACK CORROSION. CORROSION BLEND OUT 0.030 BY 0.375 BY 1 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D TRACK REPAIRED AT BS 480-610 LBL 66 AREA AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

STA 550-590 LBL 47 IN SEAT TRACK CORROSION. CORROSION BLEND OUT 0.030 BY 0.25 BY 3.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRAP — CORRODED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

FWD CARGO FRAME AT BS 960 STR 34L FOUND UPPER REINFORCEMENT STRAP CORRODED. CORROSION BLEND OUT 0.52 BY 0.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FWD CARGO BAY BS 960 FRAME ATTACH STRAP REPLACED AT BETWEEN STR 31L TO 39L AREA AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

STA 783 LBL 11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.019 BY 0.75 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723- BS 857 LBL 11 AREA WORK DETAIL REF NRC NR 6006.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, U/D STA 544-562 LBL 66 SEAT TRACK CORROSION. CORROSION BLEND OUT 0.059 BY 0.5 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480-610 LBL 66 TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 800 TO 840 LBL 11 SEAT TRACK NECK FOUND CORRODED. CORROSION BLEND OUT 0.052 BY 1.0 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723 TO BS 857 LBL 11 AREA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 980 LBL 11 TO 33 FLOORBEAM CORRODED. CORROSION BLEND OUT 0.043 BY 1.0 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 900 LT FRAME O/B FLANGE FOUND CRACKED BTN S-12L AND S-13L. CRACK LENGTH 0.4375 IN. CORROSION BLEND OUT N/A. BS 900 LT FRAME O/B FLANGE BETWEEN STR 12L AND 13L AREA REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 760 LBL 65 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.055 BY 0.5 BY 2.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: BRACKET — CORRODED (KEELBEAM BOX) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE: C, FX KEELBEAM BOX INTERIOR SUPPORT ROD ATTACH BRACKET FOUND CORROSION AT STA 1240 LBL 3 BOX TOP AREA. CORROSION BLEND OUT 0.051 X .5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1240 LBL 3 AREA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C M/D BS 640 STR 24L FRAME FOUND CRACKED, CRACK LENGTH 0.5 IN. M/D BS 640 FRAME REPAIRED AT S23L TO S26L AREA AS PER RS NR R53-22-35316 AND UPS ENGINEERING FILE NR 747-53-20254.

Part: FRAME — CRACKED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, FWD CARGO FRAME AT BS 960 STR 40R FOUND UPPER CHORD CRACKED, ALSO EXTEND TO WEB, CRACK LENGTH 3 IN. FWD CARGO BAY BS 960 S40R AREA FRAME REPAIRED AS PER HX RS NR R53-22-35325 AND UPS ENGINEERING FILE NR 747-53-20259.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

BS 540-660 LBL 28 INCH SEAT TRACK CORRODED. CORROSION BLEND OUT 0.050 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

FX LT TUNNEL STR 41 AFT END CRACKED BETWEEN STA 260-280, CRACK LENGTH 0.75 IN. FX BS 260-280 STR 41L STRINGER REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. FWD CARGO FRAME AT BS 760 STR 34R FOUND UPPER CHORD CRACKED. CRACK LENGTH 0.5 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: FRAME — CRACKED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. FWD CARGO FRAME AT BS 920 STR 34L FOUND UPPER CHORD CRACKED, CRACK LENGTH 2.75 IN. FWD CARGO BAY FRAME REPAIRED AT BS 920 STR 34L - 37L AREA AS PER SRM 53-10-04 FIG 52.

Part: WEB — CRACKED (CARGO BAY) · airframe 73,825 hrs · 21,397 cycles

BULK CARGO, BS 1960 STR 36L TO STR 37L FRAME WEB AND INNER CHORD FOUND CRACKED, CRACK LENGTH WEB 5 IN, CHORD 1.5 IN. BULK CARGO, BS 1960 STR 36L TO STR 37L FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 66 AND INNER CHORD REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. BS940 S22L FRAME FOUND CRACKED, CRACK LENGTH 0.5 IN. CABIN BS 940 BETWEEN STR 22L - 23L FRAME O/B FLANGE REPAIRED AS PER HX RS NR R53-22-35322 AND UPS ENGINEERING FILE NR 747-53-20258.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

U/D BS 600 TO 660 LBL 47 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.040 BY 1.0 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, M/D, BS 2320 RT STR 26R TO 28R FRAME INNER CHORD FOUND CRACKED, CRACK LENGTH 3 IN. FRAME REPAIRED AS PER HX RS NR R53-82-35327 AND UPS EO NR B747-5310-22462-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, U/D BS 520 TO 670 LBL 10 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.040 BY 1 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520 TO BS 670 LBL 10 TRACK REPAIRED AS PER SRM 53-10-05 FIG 4.

Part: FRAME — CRACKED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. FWD CARGO, FRAME AT BS 900 STR -34L FOUND UPPER CHORD TO FRAME WEB CRACKED, CRACK LENGTH 0.75 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,825 hrs · 21,397 cycles

TIE DOWN TRACK BS 1483 RBL 97 CORRODED. CORROSION BLEND OUT 0.080 BY 0.75 BY 1.25 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (FWD CARGO) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C. FWD CARGO, FRAME AT BS 880 STR 34L FOUND UPPER CHORD CRACKED, CRACK LENGTH 1.875 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: FLOORBEAM — CRACKED (AFT CARGO) · airframe 73,825 hrs · 21,397 cycles

AFT CARGO BAY BS 1800 BL 0 AND FLOORBEAM UPPER FLANGE CRACKED. CRACK LENGTH 2.5 IN. AFT CARGO BAY BS 1800 LBL 22 TO RBL 40 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: RIB — CRACKED (TE FLAPS) · airframe 73,825 hrs · 21,397 cycles

INSPECTION TYPE:C, RHW NR 22 VC FLAP I/B ARM I/B SUPPORT RIB CRACKED AT D HOLE AREA. CRACK LENGTH 0.4375 IN. SUPPORT RIB LINKAGE ATT BOSS TIME LIMITED REPAIRED CARRIED OUT AS PER RS NR R57-41-35323 AND UPS EO NR B747-5740-22465-A.

Part: FUSE — BLOWN (EMERGENCY LIGHT)

AFT EMERGENCY LIGHT IN L1 DOOR INOP. TROUBLESHOT & FOUND BATTERY LOW FUSE BLOWN & BULB INOP. REPLACED BATTERY FUSE & RELAMPED IAW MM 33-51-00. OPS CHECK NORMAL AT THIS TIME.

Part: LIGHT — INOPERATIVE (EMERGENCY SIGN)

EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE DOOR INOP. REMOVED POWER PACK JPV 95678. REPLACED CREW SERVICE DOOR EMERGENCY EXIT SIGN BATTERY PACK PER MM 33-51-00. TESTS GOOD.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, RAP ITEM N672 46-05 CRACK AT BS 1785 - 1792 STR 23L - 25L REMOVE FOR FURTHER ACTION. REPLACED REPAIR DOUBLER PER RS R52-32-35109 RELATED AREA SIDE CARGO DOOR RIGGING AND OPERATION CHECK DONE PER MM 52-32-00. SATISFACTORY AND EO B747-5230-19954-A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, DURING WORK ACCOMPLISH FOR RAP, ITEM N672-46-28 AT BS 1960-1975 STR 45R-47R EXISTING PATCH FOUND NOT MATCH WITH SRM 53-30-03 FIG 19 AS PROVIDED BY CUSTOMER RE-DO THE REPAIR REQUIRE. EXPANDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 48 AT FX STA 1960 TO STA 1980 BETWEEN STR 45R AND STR 47R AREA SUBSEQUENT INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 48 SHT 9 TABLE II & SHT 13 TABLE III. THIS REINSPECTION WILL BE CONTROLLED BY EO B747-5330-13494-H.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, RAP ITEM N672UP 42-11 AT BS 680-703 STR 40R-41R AREA, REPAIR DOUBLER HAS LESS THAN 3 ROW FASTENERS FOR REPAIR AFTER NDT DEFINED CUTOUT RE-DO THE REPAIR REQ'D. BS 680-703 STR 40R-41R AREA DOUBLER REMOVED & DISCARDED AS PER SRM 51-30-02 BS 678-689 & BS 692-704 STR 40R-41R EXTENDED DOUBLER INSTALLED REPAIR AS PER SRM 53-30-03 FIG 1 & ZERO-TIME FASTENERS INSTALLED AS PER SRM 51-10-01 PG 11 AT STR 40R-41R AREA CLASSIFIED A CATEGORY-A REPAIR.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C BS 1241 RIGHT BULKHEAD SPLICE STRAP AFT HOLE CRACK FOUND RUNNING AFT APPROX .125 INCH. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107 BS 1241 RIGHT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2200 STR 44 FRAME AFT ATT STIFFENER FOUND CORROSION. AFT OF BULK CARGO COMPT RT STA 2200 STR 44 FRAME AFT ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION BLEND OUT DEPTH 0.020 , WIDTH 1 & LENGTH 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITATION.

Part: SKIN — DAMAGED (AFT CARGO DR.) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, EO 747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING RAP INSPECTION, ITEM N672-46-24, BS 1840-1860 STR 42R AFT CARGO DOOR LWR EDGE REPAIR DOUBLER HAS LESS THAN 2 ROWS OF FASTENER BEYOND THE DAMAGE AREA. THIS REPAIR IS CLASSIFIED AS PER -D- REPAIRED. EXPANDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR. MID LOWER EDGE AT BS 1840-1860 STR 42R AREA REPEAT INSPECTION REQ'D SRM 52-30-06 FIG 1 SHT 12 TABLE II. (REPEAT INSPECTION PER EO B747-5330-13494-H).

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2220 IN BETWEEN STR 40 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.071 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. ANGLE REPAIRED PER SRM 51-40-03 FIG 2. CIC APPLIED IAW EO M-5100-2780-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D- RT STA 2240 FLOORBEAM LOWER SECTION FOUND CORRODED IN BETWEEN RBL 6 AND RBL 40. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 LIMITS. STA 2240 RBL 30 FLOORBEAM LOWER SECTION REPAIRED AS PER SRM 51-40-04 FIG 2. CIC APPLIED IAW CPM53-10-17.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2180 - 2200 STRINGER L51 FOUND CRACKED. DEFECTIVE AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 14.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT CARGO COMPT - LT STA 1680 IN BETWEEN STR 45 AND STR 46 SHEAR TIE FOUND CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 45L AND STR 46L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- LT STA 2160 STRINGER 40 STIFFENER ANGLE FOUND CRACKED. AFT OF BULK CARGO LT STA 2160 FRAME AT STRINGER 40 STIFFENER ANGLE REPLACED AS PER SRM 51-10-01 PG 8.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 708,710 hrs · 20,783 cycles

INSPECTION TYPE:C EO747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING MARK ACCOMPLISH, TAR 106855 REPAIR AGAIN AT BS 1905-1913 STR 42R AFT CARGO DOOR AFT EDGE AREA WHICH MAY INTERFERE WITH THE EXISTING REPAIR AT ITEM N672-46-26, BS 1915-1920 STR 41-42R. EXPENDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR AFT LWR CORNER BS 1905-1920 STR 41R-42R AREA. REPEAT INSPECTION REQUIRED AS PER SRM 52-30-06 FIG 1 SHT 12 TABLE II. REPEAT INSPECTION IS REQUIRED PER EO B747-5330-13494-H.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C DURING REPAIR ASSESSMENT PROGRAM ACCOMPLISH, ITEM N672-41-08 AT BS 447-463 STR 42R-44R 2 LAYERS REPAIR DOUBLER FOUND SINCE THE OUTER DOUBLER IS ONLY 0.040 INCH THK WHICH WILL CREATE KNIFE-EDGE CONDITION, RE-DO THE REPAIR REQUIRE. EXISTING DOUBLER REMOVED & DISCARDED AS PER SRM 53-30-03 FIG 1. HFEC INSPECTED AT THE REPAIR AREA FASTENER HOLES, NO CRACK REVEALED. NEW EXTENDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 1. SUBSEQUENCE INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 1 TABLE IV (REPEAT INSPECTION PER EO B747-5330-13494H).

Part: FRAME — CRACKED (SECTION 41) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, SECTION 41, FS 250 BETWEEN STR 40L - 41L, FRAME WEB CRACKED BS 260 CANTED BULKHEAD WEB SEGMENT BETWEEN STR 38L AND STR 41L. REPLACED AS PER HX RS R-53-13-35101 AND UPS ENGINEERING FILE NUMBER 747-53-20167.

Part: SHEAR TIE — CRACKED (AFT CARGO BILGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT CARGO BILGE AREA - FS 1680, STR S47L - 48L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 47L AND STR 48L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, FX SKIN BUTT JOINT SPLICE STRAP OVAL HOLES FOUND AFTER REPAIR PATCH REMOVED AT FS 2180- 2181 ON BOTH SIDE OF STR 50R. FX SKIN BUTT JOINT SPLICE STRAP REPAIRED AT BS 2180-2181 ON BOTH SIDE OF STR 50R AREA AS PER RS R-53-61-35105 AND UPS ENGINEERING FILE 747-53-20169 ISSUED.

Part: SHEAR TIE — CRACKED (AFT CARGO BILGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1700, STR 49L - 50L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1700 BETWEEN STR 49L AND STR 50L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT CARGO BILGE AREA - FX 1820, STR 44R - 46R SHEAR TIES CORRODED. BS 1820 TO 1820, STR R44-R46 CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 0.5 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. FLANGE REPAIRED REFER SRM 53-10-04 FIG 3 AND CIC APPLIED IAW EO M-5100-2780-E.

Part: SHEAR TIE — CRACKED (AFT CARGO BILGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1720, STR 49R - 51R SHEAR TIES CRACKED. AFT CARGO COMPT BS 1720 STR 49R - STR 51R SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C S-7L STRINGER FOUND CRACK AT STA 1349 STR 7L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5.

Part: REVEAL — CRACKED (R4 DOORWAY) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D- R4 DOOR CUTOUT FWD REVEAL CRACK, BETWEEN STRINGER 17 & 18 (BS 1662-1664, STR R17, R18). REPLACED DOOR CUTOUT FWD REVEAL PER SRM 51-10-01 PG 8. DOOR RIGGING & ADJUSTMENT DONE RESULT: SATISFACTORY PER MM 52-10-00.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C BS 1241 LEFT BULKHEAD SPLICE STRAP AFT HOLE FOUND CRACKS AT FWD AND AFT SIDE. BS 1241 LEFT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D - BS 960 TO 980 LT STR 2AL STRINGER FOUND CRACK. BS 960 - BS 980 STR 2AL STRINGER REPAIR CARRIED OUT IAW SRM 53-10- 03 FIG 4.

Part: PANEL — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D- BS 1238 - 1265 LBL 75.92 - 95.58 CLOSEOUT PANEL CRACKED. REPAIRED CLOSEOUT PANEL PER EO 747-5310-2758 APP-C. ALL RELATED STEPS RESTORED TO NORMAL CONFIGURATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C BS 1438 S-13 / S-14R FRAME CRACKED. BS 1438 BETWEEN S13R AND S14R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1.

Part: FITTING — CORRODED (NR 4 PYLON) · airframe 70,871 hrs · 20,783 cycles

NR 4 PYLON DIAGONAL BRACE UNDERWING FITTING, HOLE NR 10 I/B ROW MOST AFT CORROSION FOUND ON BACKUP FITTING BORE AREA. DEFECTIVE AREA FASTENER HOLE CORROSION REPAIR CARRIED OUT AS PER HX RS R57-24-35102 AND EO B747-5740-19955-A. FINAL HOLE 0.562 INCH TO CLEAN UP CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C STA 1700 FRAME FOUND CRACK BETWEEN S-10 / S-11L. BS 1700 BETWEEN STR 10L AND STR 11L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1.

Part: FITTING — CORRODED (NR 3 PYLON) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, NR 3 PYLON DIAGONAL BRACE FWD ATTACH FITTING BASE AREA PITTING CORROSION FOUND. NR 3 PYLON DIAGONAL BRACE ATTACH FITTING LOWER SURFACE CORROSION REPAIR CARRIED OUT AS PER HX RS R-54-54-35098. (FAA 8110-3 DATED FEB 5, 2004 & EO B747-5440-19929-A APPROVED).

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C BS 960 LT BETWEEN STR 7L AND 6L SHEAR TIE FOUND CRACK. BS 960 LT FRAME BETWEEN S6L AND 7L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C BS 1241 RT CANTED PRESSURE DECK FITTING AFT HOLE FOUND CRACK APPROX 0.030 INCH RUNNING DOWN. BS 1241 RT CANTED P/D FITTING AFT BOLT HOLE REPAIRED PER RS R53-41-35107 & ENG'R FILE 747-53-20170, REPAIR IS CONSIDERED A TIME-LIMITED REPAIR 2 YEARS/1500 FLT CYCLES WHICHEVER COMES FIRST, AT WHICH TIME CANTED FITTING SHOULD BE REPLACED. SPLICE STRAP SHOULD BE REPLACED WITHIN 2 YEARS OF CRACK DISCOVERY, DUE TO CRACK WAS DISCOVERY DURING PRESENT MAINTENANCE.

Part: ATTACH ANGLE — CRACKED (SHEAR TIE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO COMPT - LT STA 900 IN BETWEEN STR 43 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CRACKED. FWD CARGO COMPT BS 900 BETWEEN STR 43L AND STR 44L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D- BS 2240 TP 2270 LBL 80 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8. CIC APPLIED IAW CPM53-10-17.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 980 IN BETWEEN STR 41 AND STR 42 FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52 AT FWD CARGO COMPT RT STA 980 BETWEEN STR 41 AND STR 42.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D - BS 2150 RBL 108 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM LIMIT.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, FWD CARGO COMPT- LT STA 720 - STA 740 STRINGER 47 FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E.

Part: CHANNEL — CORRODED (MAIN DECK) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D- BS 2315 LBL 11 TO LBL 38 HAT SECTION FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 8. P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM53-10-17.

Part: FORGING — CORRODED (WINDOW) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D- BS 1560-1580 LT WINDOW FORGING AFT EDGE ATT SKIN FOUND CORROSION REVEALED. BS 1560-1580, STR L19-L22 CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM 53-30-01 FIG 1 LIMIT. WINDOW FORGING REPAIRED PER RS R-53-61-35104 & UPS ENGINEERING FILE 747-53-20164, CIC APPLIED IAW CPM 53-10-47.

Part: CHANNEL — CORRODED (MAIN DECK) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D- BS 2320 TO 2350 LBL 40 HAT SECTION FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED PER SRM 51-10-01 PG 8 & P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM 53-10-17.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C NR 4 PYLON - LOWER CAVITY NEAR NAC STA 211 RT VERT SUPPORT RIB CRACKED. NR 4 PYLON - LOWER CAVITY NEAR NAC 221 RT VERTICAL SUPPORT FRAME REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: SKIN — CHAFED (EMPENNAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C EMP- RT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 , STR 2R TO 3R VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2R-3R AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2329-2360 STR 2R-4R. BS 2280-2310 STR 2R-3R SKIN REPAIRED AS PER SRM 53-30-03 FIG 1. (UPS MPI ASSIGNED FOR REPEAT INSPECTION).

Part: STRAP — CRACKED (RT WLG WW) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C RIGHT WLG W/W - BS 1241 SPLICE STRAP AFT HOLE CRACK. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107, RIGHT STA 1241 SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).

Part: SKIN — CHAFED (EMPENNAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C EMP- LT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 STR 2L TO STR 3L VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2L-4L AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2290-2310 STR 2L-3L & BS 2330-2360 STR 2L-4L. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 (UPS MPI ASSIGNED FOR REPEAT INSPECTION).

Part: WEB — CRACKED (NR 2 PYLON) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, NR 2 PYLON - LWR WEB CRACKED THRU AFT RT LONGITUDINAL STIFFENER APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LATERALLY. LWR SPAR WEB 5 LOCATIONS CRACK END BY STOP HOLE PRILLED AS PER SRM 54-10-03 FIG 2. NDT INSP NIL CRACKS AND PERFORMED A PERMANENT REPAIR AS PER SRM 54-10-03 FIG 2 AT NAC STA 213 COMBINED REPAIRED AT SAME AREA REF TO NRC UE56196.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C NR 2 PYLON - LWR WEB CRACKED THRU FASTENERS AFT OF PNEU DUCT CUTOUT APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LONGITUDINALLY. LWR SPAR 5 LOCATIONS CRACK END BY STOP DRILLED HOLES PER SRM 54-10-03 FIG 2 NDT CONFIRMED NIL CRACKS AND PERFORMED A PERMANENT REPAIRED AS PER SRM 54-10-03 FIG 2 AT NAS STA 213.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO COMPT- RT STA 790- STA 810 STRINGER 46 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED PER HX RS R53-21-35100 & UPS ENGINEERING FILE 747-53-20168. CIC APPLIED IAW EO M-5100-2780-E.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO COMPT- LT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER TRIMMED OUT AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE:C M/D- BS 380 RT STR 25R FRAME FOUND CRACKED. REPAIRED FRAME PER RS 53-12-35103 AT BS 380 STR 25R AREA AND EO B747-5310-19928-A.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D - BS 270 LT STR 26L VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,871 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D- BS 270 RT STR 26R VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1.

Part: MODULE — INOPERATIVE (MLG LIGHTS)

ATB ON RETRACTION OF GEAR AFTER TAKEOFF THE RED GEAR AND DOOR OPEN LIGHTS WOULD NOT EXTINGUISH. THE RED GEAR LIGHT REMAINS ILLUM AND GEAR DOOR OPEN LIGHT ILLUM. BASED ON SOUND AND FEEL AT LEAST ONE DOOR AND OR GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRACTION ABLE TO DUPLICATE PRIMARY DISPLAY RED WARNING LIGHT GEAR, TROUBLESHOOT LOGIC MODULE BOX FOUND CARD FILE PRIMARY CARD A-13 PER MM 32-61-16. RETRACTED GEAR SEVERAL TIMES, OPS CHECKED GOOD.

Part: GCU — MALFUNCTIONED (E/E BAY)

INSPECTION TYPE:N/A DURING SHUTDOWN ON ENG 2 & 3 DURING TAXI IN BTB NR 2 OPENED. WHEN CLOSURE ATTEMPTED THE KW OUTPUT ON GEN 4 SPIKED TO 60+ KW AND BTB REOPENED. ALSO SMELLED SLIGHT ODOR OF ELECTRICAL SMELL/BURN. REMOVED AND REPLACED NR 2 GCU.

Part: ACTUATOR — INTERMITTENT (RT MLG DOOR)

DURING GEAR RETRACTION RED GEAR LIGHT AND RED DOOR LIGHT ILLUMINATED RE CYCLED NO HELP PREFORMED EMERGENCY PROCEDEURE I/A/W QRH-NO HELP R ETURNED TO BASE. F/E PANEL SHOWED RT WING DOOR OPEN IN BOTH PRI + ALT. RESEQUENCE NO HELP. REPLACED RT WING GEAR DOOR ACTUATOR (PRECAUTIONARY) FOR INTERMITENT GEAR DOOR LIGHT. GARY ABBOTT 00263 5-3-03 / CK'D REQ OF RH WING GEAR DOOR EQUENCE VLV PER MM 32-32-02 OPS NORMAL 99432 5-3-03 ONT/ SEE L OG 059864 ITEM 1 FOR CONTINUATION.

Part: LIGHT — INOPERATIVE (CABIN)

AFT MAIN DECK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM-33-51-07 OPS CK OK

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN ENTRY DOOR R1 FWD EMERG LIGHT INOP. RELAMPED, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP MAIN DECK CEILING AT STA 640 LT SIDE. R&R BATTERY ASSY, OP CHECK OK.

Part: STIFFENER — CORRODED (WING)

A STIFFENER CORRODED CENTER SECTION REAR SPAR. LBS. 85.6 HAS CORROSION. APPROX. 11 INCHES LONG. NEXT TO FUEL PUMP APERATURE. REMOVED VERTICAL STIFFNER PER SRM 51 30 02 39550/ INSTALLED NEW STIFFNER PER SRM 51 10 01 REPLACEMENT OF PART. REF LOG 914476 ITEM 1 &2 FOR FINAL INSTALLATION OF REMAINING FASTNER

Part: LENS — CRACKED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT LENS CRACKED ON FWD LIGHT AT UPPER DECK CREW SERVICE DOOR. REPLACED LENS ASSY LIGHT OPS CK OK.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP MAIN DECK CEILING AT STA 580 LT SIDE. REPLACED BATTERY ASSY, OP CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP, UPPER DECK ABOVE SUPERNUMERARY SEATS LT SIDE. REPLACED BATTERY PACK OPS CK OK.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT LG W/W OVERWING LONGERON SPLICE FITTING ATTACH SIX MOUNT BOLTS, NUTS AND BOLTS FOUND CORROSION AFTER FITTING REMOVE AT STA 1355. LT LG W/W OVERWING LONGERON SPLICE FITTING ATTACH SIX MOUNT BOLT HOLE OVERSIZED. NDT INSPECTED NO CRACK & NO COR. ALL SIX BOLTS & NUTS REPLACED AS PER BOEING DWG 65B15254 SHT 2, SRM 51-30-03 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK BS 520 - 570 RBL 50 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - BS 1000 - 1020 LBL 97 SEAT TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT 53-10-01. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, COCKPIT BS 340 RBL 10 - 20 FLOOR BEAM UPPER CHORD CORRODED. CORROSION REMOVED IAW 51-10-01 EXCEED SRM LIMIT 53-10-07 FIG 16.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT LG W/W STA 1355 S33L OVERWING LONGERON UPPER FUSELAGE SKIN FOUND CORROSION. SKIN FOUND CORRODED AT LOCATION BS 1355 TO 1355, STR L33 TO L33. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SKIN REPLACED AS PER SRM 51-10-01. HX RS NR R53-41-34892, UPS EO NR M5100-2780-E.

Part: PLATE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT LG W/W STA 1241 CANTED B/H DRAIN TUBE FITTING COVER PLATE FOUND CRACK AT LBL 98. LT LG W/W STA 1241 CANTED B/H DRAIN TUBE FITTING COVER PLATE REPLACE AS PER SRM 51-10-01 PG 8 AND FASTENERS INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CRACKED (L3 DOOR) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D L3 DOOR UPPER HINGE SKIN CUTOUT CRACKED. SKIN REPAIRED AS PER SB 747-52-2144 FIG 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, UPPER DECK BS 700-710 LBL 28 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C U/D - BS 440 RBL 20-40 FLOOR BEAM FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT, UPPER CHORD REPAIRED AS PER HAECO RS NR R53-15-34883 & UPS AUTH NR 747-53-20100.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT LG W/W STA 1241 CANTED PRESSURE DECK BULKHEAD 2EA TENSION BOLT HOLES FOUND CORROSION AS RBL 75. RT LG W/W STA 1241 CANTED PRESSURE DECK 2EA TENSION BOLT HOLES OVERSIZED PER SRM 51-30-05. NDT CONFIRMED NO CRACK AND NO CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK BS 480 BL 0 - RBL 35 FLOORBEAM CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT UPPER BEAM REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK BS 680 LBL 28 SEAT TRACK LIP FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C U/D - BS 440-460 LBL 0 - RBL 50 FLOOR SUPPORT AND WEB FOUND CORR. BLEND OUT EXCEEDS SRM LIMIT, FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C U/D - BS 680-710 LBL 46 SEAT TRACK CROWN FOUND CORROSION. COR BLEND OUT EXCEEDS SRM LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, UPPER DECK BS 670-710 LBL 8 SEAT TRACK FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, UPPER DECK BS 420 RIGHT STR S9AR, S8AR AND S6AR FRAME INNER CHORD ATTACH ANGLE FOUND CRACK AS MARKED. UPPER DECK BS 420 RIGHT STR S9AR, S8AR AND S6AR FRAME INNER CHORD ATTACH ANGLES REPLACED AS PER SRM 51-10-01 PG 8.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT MLG W/W PRESSURE DECK LWR SPLICE ANGLE FWD TIP BETWEEN BS 1402 & 1403 , RBL 74 & 77. CORRODED AROUND 2EA HI-LOCK HEADS. SPLICE ANGLE REPLACED AS PER 51-10-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, UPPER DECK BS 400 RBL 80 FLOOR SUPPORT FOUND CRACKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT LG W/W I/B PRESSURE DECK TO VERTICAL WEB ATTACHMENT SHEAR TIE FITTING AT BS 1416 RBL 1 AREA UPPER FLANGE CRACKED. RT LG W/W I/B PRESSURE DECK TO VERTICAL WEB AT BS 1416 RBL 1 STIFFENER ATT CRACKED FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C FUSELAGE KEEL BEAM TOP PANEL INTERNAL HEAVY CORROSION FOUND AT BS 1250-1330. WEB FOUND CORRODED AT LOCATION BS 1250 TO 1330, RBL 8. CORROSION BLEND OUT EXCEEDED SRM LIMIT. WEB REPLACED AS PER SRM 51-10-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT MLG W/W PRESSURE DECK LWR SPLICE ANGLE TIP BETWEEN BS 1402 & 1403, RBL 56 & 59. CORRODED AROUND 2EA HI-LOCK HEADS. SPLICE ANGLE REPLACED AS PER SRM 51-10-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 10 FOUND CRACK AT EXTENSION FITTING, APPROX 0.09 RUNNING FWD. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 10 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, UPPER DECK BS 560 - 580 LBL 30 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.030 INCH. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 74753A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT WEB SPLICE PLATE , APPROX 0.02 INCH RUNNING O/B. LT 1480 BULKHEAD WEB SPLICE PLATE NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT WEB SPLICE PLATE, APPROX .125 INCH, RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-3A2390 FIG 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, COCKPIT - BS 340 LBL 100 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION REMOVED IAW 51-10-01, CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C COCKPIT BS 340 - 360 CTR INTERCOSTAL WEB ATT ANGLE CRACKED. ATT ANGLE REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RH LG W/W BS 1241 CANTED BULKHEAD FOUND CORROSION AT RBL 75-77 WL 166-167. BULKHEAD FOUND CORRODED AT LOCATION BS 1241 TO 1241 WL 166 TO 167, RBL R75 TO R77. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BULKHEAD REPLACED AS PER SRM 51-10-01 HX RS NR R53-48-34885. UPS EO NR 747-53-20101.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C BS 340 UPPER DECK FLOORBEAM UPPER CHORD, THREE FASTENER HOLES CRACKED, REVEALED AT LBL 18, RBL 15 & RBL 46 RESPECTIVELY. UPPER DECK BS 300 FLOORBEAM LBL 18 & RBL 15 CRACKED HOLE REF NRC 7305 SECTIONAL REPLACED FROM RBL 20 TO LBL 40 AS PER SRM 53-10-07 FIG 23, RBL 46 CRACKED FASTENER HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D, PLAN C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK BS 520 - 540 LBL 65 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 6.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 18 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.030 RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 18 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C BS 360 UPPER DECK FLOORBEAM UPPER CHORD, 2 FASTENER HOLES CRACK REVEALED AT RBL 28 & RBL 43 RESPECTIVELY. UPPER DECK BS 360 RBL 28 CRACKED HOLE CRACK REMOVED AS PER EO B747-5320-12407-C APPENDIX D. NO NECESSARY REPAIR. RBL 43 CRACKED FASTENER HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D PLAN C.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C BS 380 UPPER DECK FLOORBEAM UPPER CHORD, 1 FASTENER HOLE CRACK REVEALED AT RBL 60, RUNNING AFT APPROX .0625 INCH LENGTH. UPPER DECK BS 380 FLOORBEAM RBL 60 CRACKED HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D PLAN A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 5 HOLE FOUND CRACK AT EXTENSION FITTING RUNNING AFT APPROX 0.06. RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 5 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 23 HOLE FOUND CRACKED AT WEB SPLICE PLATE RUNNING I/B APPROX 0.06. THE WEB SPLICE PLATE REPLACED DUE TO HOLE OVERSIZED AND EXCEEDED LIMIT AS PER SB 747-53A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.04 INCH RUNNING FWD. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 17 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.020 INCH RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 17 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD HOLE NR 1 FOUND CRACK AT FUSE SKIN APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD FUSE SKIN NR 1 BOLT HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING I/B AFT APPROX 0.09. RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 24 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT BULKHEAD CHORD, APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD CHORD NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 8 FOUND CRACK AT EXTENSION FITTING APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 9 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C W/W KEEL BEAM RT ATTACHED FIXED PANEL AT BS 1438-1464 WL 91 FOUND PANEL OUTER SKIN SURFACE HAS CORRODED SURROUNDING PANEL EDGE AREA AND PANEL DOOR HINGE CUTOUT AREA. CORROSION BLEND OUT EXCEEDED SRM LIMIT, FIXED PANEL REPLACED AS PER SRM 51-10-01.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT BULKHEAD WEB APPROX 0.03 INCH RUNNING O/B. LT BS 1480 BULKHEAD WEB NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT OUTER CHORD SPLICE FITTING APPROX 0.02 INCH RUNNING I/B. LT BS 1480 BULKHEAD OUTER CHORD FITTING NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT LG W/W O/B PRESSURE DECK LWR FACE AT BS 1416 LATERAL O/B NR 2 RIVET HOLE AREA CRACKED TO EDGE. SECTION OF PRESSURE WEB AT RT LG W/W O/B FROM STA 1400 TO 1438 RBL 110 TO MOST O/B AREA REPLACED AS PER SRM 51-10-01 PG 8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C FUSELAGE - AFT CARGO DOOR AFT CUTOUT FOUND PREVIOUSLY TRIMMED SKIN AT STA 1920 BETWEEN S39R-S40R. FUSELAGE AFT CARGO DOOR AFT CUTOUT AT STA 1920 BETWEEN S39R-S40R SKIN REPAIR AS PER SRM 53-30-03 FIG 17.

Part: RIB — CORRODED (LT WING) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT WING L/E RIB AT L/E SLAT 1309.15 ROTARY ACTUATOR MOUNTING HOLES NR 1, 7 BORE CORROSION FOUND. RIB FOUND CORRODED AT LOCATION L/E SLAT 1309.15 TO 1309.15. CORROSION BLEND OUT EXCEEDED SRM LIMIT RIB REPLACED PER SRM 51-10-01, 57-41-34886, UPS EO NR 747-5740-17509.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK BS 550 LBL 50 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C UPPER DECK STA 420-440 BL 0 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT EXTENSION FITTING. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER BS 747-53A2390 FIG 11.

Part: BULKHEAD — CRACKED (NR 3 NACELLE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C CRACK FOUND ON NR 3 NACELLE STRUT REAR MOUNT BULKHEAD AFT O/B WEB APPROX .5 INCH LONG AND STOPPED AT FASTENER HOLE. NR 3 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34880 UPS EO NR 747-54-20029.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING I/B APPROX 0.09 AND O/B APPROX .125. THE WEB SPLICE PL ATE CHANGED AS PER SB 747-53A2390. REFER HX RS R-53-43-34884 AND UPS EO B747-5310-17499-A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AT WL 180 RBL 70. FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 6.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT LG W/W O/B, OVERWING LONGERON BETWEEN BS 1436 AND 1446 I/B LWR SURFACE CORRODED AS MARKED. LONGERON FOUND CORRODED AT LOCATION BS 1436 TO 1445 LBL L118 TO L122 CORROSION BLEND OUT EXCEEDEDS SRM LIMIT REPLACED AS PER SRM 51-10-01. HX RSRS NR R53-43-34882, UPS EO 747-53-20104.

Part: BULKHEAD — CRACKED (NR 4 NACELLE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C CRACKS FOUND ON NR 4 NACELLE STRUT REAR MOUNT FWD AND AFT WEBS. NR 4 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34881 & UPS ENGINEERING FILE NUMBER 747-54-20030.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C LT LG W/W O/B BS 1438 WEB LWR END ADJACENT OVERWING LONGERON I/B AREA HEAVY CORROSION FOUND. CORROSION BLEND OUT EXCEEDED SRM LIMIT, FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C RT BS 2231 FRAME Y STR 24 & STR 25 FOUND 2EA FASTENER HOLES CRACKED AT REVEAL. RT BS 2231 FRAME BETWEEN STR 24R TO STR 25R 2EA FASTENER HOLES CRACKED AT REVEAL REPAIRED AS PER SRM 53-10-04 FIGURE 115.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - STA 506 LBL 70 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. O/B SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, M/D - FLOOR SUPPORT FOUND CORRODED AT STA 240 LBL 4 - LBL 5. CORROSION REMOVED IAW 51-10-01, CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, M/D BS 540 S24L FRAME FOUND CRACKED. M/D BS 540 S24L FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - SEAT TRACK FLANGE FOUND CORRODED AT STA 480-500 RBL 85. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - STA 476-480 LBL 32 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BS 460-510 LBL 32 SEAT TRACK REPLACED AS PER SRM 51-10-01.

Part: PANEL — WORN (NR 3 PYLON) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C NR 3 PYLON - O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT WORN AT FWD PORTION. NR 3 PYLON O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT REPAIRED AS PER SRM 54-30-03 FIG 35 AND FIG 36.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D BS 320 S-13AL TIE CLIP FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01 PG. 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - FLOOR SUPPORT FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - BS 360 S23R FRAME FOUND CRACKED. M/D BS 360 S23R FRAME REPAIR CARRIED OUT AS PER HX RS NR R53-12-34879 AND UPS EO B747-5310-17492-A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - BS 1220 LBL 112 BELOW FLOOR, INTERCOSTAL WEB FOUND CRACKED. M/D - BS 1220 LBL 112 BELOW FLOOR INTERCOSTAL WEB CRACK STOP DRILLED AND REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - BS 390 S-14R WEB FOUND CRACKED. M/D BS 380-400 STR 14R WEB REPAIRED AS PER SRM 53-10-04 FIG 55.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D - BS 260 LBL 30 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK I/B FLANGE REPAIRED AS PER SRM 53-10-05 FIG 16.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C, M/D BS 360 S-24A FRAME DOUBLER FOUND CRACKED. M/D BS 360 STR 24AL FRAME DOUBLER REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: DOUBLER — CRACKED (R1 DOOR) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D R1 DOOR LOWER HINGE SKIN DOUBLER FOUND CRACKED. SKIN REPAIRED AS PER SB 747-52-2144 FIG 4.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C M/D L1 DOOR UPPER HINGE SKIN DOUBLER FOUND CRACKED. DOOR SKIN REPAIRED AS PER SB B747-52-2144 FIG 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C FUSELAGE - AFT CARGO DOOR FWD CUTOUT SKIN PORTION TRIMMED OFF AT BS 1810 STR 39R-40R. FUSELAGE SKIN REPAIRED AS PER SRM 53-30-03 FIG 19.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 68,213 hrs · 20,211 cycles

INSPECTION TYPE:C INSPECT SPEED TAPE TWO .25 INCH HOLES LOCATED O/B & FWD OF THE WATER SERVICING PANEL PER SRM 51-40-09 FIG 1 SHT 3. FIBERGLASS REPAIRED AS PER SRM 51-40-15 FIG 7 AT EXT SURFACE.

Part: WEDGE — CRACKED (T/E FLAP)

INSPECTION TYPE:PFLT LT INBOARD MID FLAP IS CRACKED IN TWO PLACES. REPAIRED DAMAGED AREAS OF MID FLAP T/E WEDGE IAW EO B747-5750-17190A. ACCOMPLISH PERM REPAIR OF PART REPLACEMENT NO LATER THAN C-CHECK.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 67,366 hrs · 20,043 cycles

INSPECTION TYPE: NR 3 PYLON INTERNAL FRAME FOUND CRACKED JUST O/B OF PYLON VALVE AREA. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: SEAL — LEAKING (EXIT DOOR)

INSPECTION TYPE:PFLT RIGHT EMERGENCY EXIT DOOR LEAKING WATER, WATER DRIPPING FROM CEILING ON MAIN DECK, COMING FROM DOOR. CLEANED AND INSPECTED SEAL, NO DEFECTS NOTED.

Part: SPAR — CRACKED (RT WING) · airframe 66,446 hrs · 19,830 cycles

INSPECTION TYPE:SP RIGHT WING REAR SPAR HAS A 1.5 INCH CRACK IN AFT WING SPAR WEB AT STA 1238 REF DMI D-226421. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-10-05 FIG 2.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHT AT STAIR WELL IS INOP. REPLACED EMERGENCY LIGHT ASSY AT TOP OF STAIRWELL TO UPPER DECK. CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN UPPER DECK RT CENTER EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT ASSY UPPER DECK RT CENTER CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHT INOP AT STA 2650 ON RT SIDE MAIN DECK. REPLACED EMERGENCY LIGHT ASSY AT STA 2350 RT CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHT INOP AT STA 350 ON RT SIDE MAIN DECK. REPLACED EMERGENCY LIGHT ASSY AT STA 2350 RT.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT STA 600 MAIN DECK RT SIDE. REPLACED EMERGENCY LIGHT ASSY AT STA 600 RT MAIN DECK. CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT STA 600 MAIN DECK RT SIDE. REPLACED EMERGENCY LIGHT ASSY AT STA 600 RH MAIN DECK, CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT AT STAIR WELL IS INOP. R&R EMERG LT ASSY AT TOP OF STAIRWELL TO UPPER DECK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERG LIGHT AT STAIRWELL INOP. REPLACED EMERG LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERG LIGHT INOP STA 2350 RT SIDE MAIN DECK. REPLACED EMERG LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERG LIGHT INOP STA 2350 RT SIDE MAIN DECK. REPLACED EMERG LIGHT ASSY.

Part: FLOOR SUPPORT — CRACKED (E/E BAY) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE:C LOWER NOSE AREA E&E. LONGITUDINAL FLOOR SUPPORT TEE SECTION CRACKED AT BS410 LBL20 TEE SECTION REPLACED IAW SRM 51-30-02

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, FWD CARGO HOLD. FUSELAGE FRAME CRACKED AT BS 960 STR 31 RT. FRAME REPAIRED IAW QUERY NOTE 21/01

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, FWD CARGO HOLD. CRACK ON INNER FLANGE OF FUSELAGE FRAME AT BS 500 S37-38 LT. REPAIR CARRIED OUT IAW EO B747-5310-14356-A

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, AFT CARGO HOLD. CORROSION ON FRAME WEB AT BS 1940 AT STR. 43 LT. FRAME WEB REPAIRED IAW Q/NOTE 24/01

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, FWD CARGO HOLD. CRACKING DUE TO CORROSION BULGE ON WEB OF FUSLAGE FRAME BS 680 ST 39-40 LT. FRAME WEB REPAIRED IAW QUERY NOTE 21/01

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, CRACK ON STRAP AT AFT AIDE OF FRONT PRESSURE BULKHEAD AT LBL AND RBL 25. CHORD REPLACED IAW EO B747-5310-3279-D

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 2180 S 25 LT. REPAIR CARRIED OUT IAW QUERY NOTE NO.10/01

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK FRAME WEB IS CRACKED AT CUT OUT FOR STR. AT BS 2120 STR 25 LT. REPAIR CARRIED OUT IAW QUERY NOTE NUMBER 10/01

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE:C CORROSION ON UPPER DECK SEAT TRACK AT BS 530 - BS 580 RBL 64. SEAT TRACK REPLACED IAW SRM 53-10-05

Part: BRACKET — CRACKED (HORIZONTAL STAB) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE:C TAIL. CRACK IN ANGLE BRACKET ON RT HORIZONTAL STAB REAR SPAR AT STAB STA . 580 NEW BRACKET FABRICATED AND FITTED IAW SRM 51-30-02

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, UPPER DECK FLOOR. CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 520 LBL 46 TO LBL 64 CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS. REPAIRS ACCOMPLISHED IAW SRM 53-10-07

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 360 S14 RT. REPAIR CARRIED OUT IAW QUERY NOTE 8/01

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. FRAME WEB IS CRACKED AT CUT OUT FOR STRINGER AT BS 360 S17 LT. REPAIR CARRIED OUT IAW QUERY NOTE 8/01

Part: WINDOW — CRACKED (COCKPIT) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, COCKPIT NR 3 RT WINDOW IS CRACKED. NR 3 RT COCKPIT WINDOW REPLACED IAW MM 56-11-02

Part: WINDOW — CRACKED (COCKPIT) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, COCKPIT NR 2 RT WINDOW IS CRACKED. NR 2 RT WINDOW REPLACED IAW MM 56-11-02

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1140 RBL 58. SKIN REPAIRED IAW QUERY NOTE 12/01

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1009 LBL 88. SKIN REPAIRED IAW QUERY NOTE 12/01

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, RT WING MLG WW. CORROSION ON 1265 FRAME OUTER CHORD AT THE OVER WING LONGERON OUTER CHORD.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, LT MLG WW. CORROSION ON TOP CHORD OF LT OVERWING LONGERON A T BS 1241 LONGERON REPAIRED IAW DRAWING NO. 144U3542

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. CORROSION ON UPPER SURFACE OF CENTER WING SKIN AT BS 1241 RBL 25. CORROSION REWORKED IAW Q/NOTE 12/01

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1080 LBL.92 SKIN REPAIRED IAW QUERY NOTE 12/01

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. CORROSION ON EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN AT BS 1100 LBL 92. SKIN REPAIRED IN ACCORDANCE WITH QUERY NOTE 12/01

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,819 hrs · 19,473 cycles

INSPECTION TYPE: C, MAIN DECK. CORROSION ON UPPER SURFACE OF CENTER WING AT BS 1140 RBL 45. SKIN REPAIRED IAW QUERY NOTE 12/01

Part: DOOR — UNSECURE (AFT CARGO DOOR)

INSPECTION TYPE:N/A, ATB- UNABLE TO PRESSURIZE IN AUTO OR MANUAL MODE AFTER TAKEOFF. A/C PRESURRIZED ON LANDIND. *S/D* SECURED AFT LOWER CARGO DOOR LATCH LOCK HANDLE AND VENT DOORS PERFORMED CARGO DOOR TEST, NO FAULTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERG LIGHT LOCATED AT CEILING FWD OF CREW STEP LADDER INOP REMOVED AND REPLACED EMERG LIGHT ASSY

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, L1 DOOR FWD EMERGENCY EXIT LIGHT IS INOP. TIGHTENED RECEPTICLE WIRE LIGHT, OP CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS ABOVE UPPER DECK SERVICE DOOR DO NOT WORK. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:C, EMERGENCY LIGHTS ABOVE UPPER DECK SERVICE DOOR DO NOT WORK. REMOVED AND REPLACED BATTERY PACK PER MM 33-54-1, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, MAIN ENTRANCE DOOR UPPER FWD EMERGENCY LIGHT OUT. RELAMPED, OPS CHECK GOOD.

Part: WEB — CRACKED (NR 1,2,3 PYLONS)

INSPECTION TYPE:N/A, NR 1, 2 AND 3 PYLON WEB CRACKED. *S/D* REPAIRED PER SRM 51-10-01 PYLON NR 1 LOG PAGE 460751 NR 2 LP 460759, NR 3 LP 460752.

Part: LIGHT — INOPERATIVE (CABIN)

BULB IN EMERGENCY LIGHT IN CEILING BY SIDE EXIT DOOR INOP. RELAMPED EMERGENCY LIGHT IN CEILING BY SIDE EXIT DOOR.

Part: FRAME — CRACKED (NR 3 PYLON)

INSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED FWD END OF DIAG BRACE FWD ATTACH FITTING, I/B SIDE APPROX PYLON STA 292, APPROX 2 INCH LONG, FROM BOTTOM END OF FRAME. *S/D* REMOVED DAMAGED RIB (P/N 65B90411-604) AND REPLACED WITH RIB (P/N 65B90411-604) AND BONDING ADHESIVE IAW SRM 51-30-02. HOT BOND OF RIB ACCOMPLISHED IAW B747 SRM 51-40-06.

Part: FITTING — CRACKED (NR 3 PYLON)

INSPECTION TYPE:N/A, NR 3 PYLON STRUCTURE FWD OF DIAGONAL BRACE FITTING IS CRACKED AROUND HI-LOK. *S/D* STOP DRILLED CRACK ENDS TO .250 IAW SRM 54-10-05 FIG 2 SHT 2. INSTALLED WEB REPAIR IAW SRM 54-10-03 FIG 2.

Part: FRAME — CRACKED (NR 3 PYLON)

INSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED, FWD END OF DIAG BRACE FWD ATTACH FITTING, O TB SIDE, APPROX PYLON STA 292. THE CRACK IS APPROX 1.5 INCH LONG, FROM BOTTOM END OF FRAME.

Part: LONGERON — CORRODED (BS 1245)

INSPECTION TYPE-C, CORROSION REPAIR TO OVERWING LONGERON OUTER CHORD AT BS 1241 RT SIDE. THE 2.75 CRACK ON LONGERON FWD END AT BS 1245 CRACK HAS NOW EXTENDED TO 3.75. CRACK FOUND PROPAGATED TO 3.75 REPAIRED IAW BOEING DRAWING 144U3542 AND EO B747-5310-0523.

Part: BEAM — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING SPOILER SUPPORT BEAM UPPER CHORD CRACKED AT I/B END. MODED ANGLES AND SPLICED IN A NEW SECTION OF CHORD IAW SRM 51-40-03 AND SB 747-57-224.

Part: SPAR — CORRODED (WS 1320)

INSPECTION TYPE-C, CORROSION ON INNER SPAR SKIN EXTENSION RT WING STATION 1320 JUST O/B OF JACKING POINT. REMOVED CORROSION.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, CREW UPPER DECK EMERGENCY DOOR UPPER DOOR FRAME LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (UPPER DECK)

2 UPPER DECK EMERGENCY LIGHTS INOP, REMOVED LIGHTS. REMOVED AND REPLACED ONE EMERGENCY LIGHT PACK, RESEATED ONE. BOTH OPS CK GOOD ON TEST.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT IN CEILING ABOVE STAIRWELL WILL NOT SHUT OFF. REMOVED AND REPLACED LIGHT ASSY, CK OK.

Part: CONNECTOR — FAILED (FLIGHT DECK)

INSPECTION TYPE-N/A, FLIGHT DECK EMERGENCY EXIT CEILING LIGHT INOP. FOUND BAD CONTACT, ADJUSTED AS REQUIRED, F/C OK. THIS CLOSES M-143122 (REF LOG PAGE 991265).

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, REF DMI M141399 RT PASSENGER AISLE EMERGENCY EXIT LIGHT INOP. REPLACED RT AISLE LIGHT ON UPPER DECK, TESTS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT AT EMER EXIT AISLE WILL NOT STAY ON. REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, WITH EMERGENCY LIGHTS SELECTED ON, LIGHT OVER STAIRWELL AND RIGHT SIDE OF C/L LOOKING FORWARD NEAR COURIER SEATS ILLUMINATED AND THEN EXTINGUISHED. REMOVED AND REPLACED EMERGENCY LIGHT BATT PAC IN LIGHT OVER STAIRWELL, OPS CK OK. DEFERRED RT SIDE OF CEILING LOOKING FORWARD NEAR COURIER SEATS EMERGENCY LIGHTS PER MEL 33-13 UNDER CONTROL NR M141399.

Part: FIRE WARNING — ACTIVATED (COCKPIT)

INSPECTION TYPE-N/A, DURING CRUISE MOMENTARY MASTER FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. UNABLE TO DETERMINE THE SOURCE, ALL FIRE SYSTEMS TESTED NORMAL. DID NOT OCCUR AGAIN. INSPECTED FIRE WARNING LOGIC CARDS, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHT INOP ABOVE 1ST OFFICERS FWD INSTRUMENT PANEL. REMOVED AND REPLACED BULB, NO HELP. REMOVED AND REPLACED F/O'S FLOOD LIGHT ASSY, FLOOD LIGHTS AND EMERGENCY LIGHT OPS CHECK GOOD.

Part: ENGINE — OIL LOSS (NR 1)

ATB - NR 1 ENGINE IFSD DUE TO LOSS OF ENG OIL NR 1 ENGINE SHUT DOWN AT 13,000 FEET FOR LOSS OF OIL TO 1 GAL PILOTS LOW OIL PRESS LIGHT ON AND OIL TEMP AT 140 DEGREES. REMOVED NR 1 ENGINE PER T/C 5000, TRIM AND RAN ENG PER T/C 5016, 5025 ALSO INSTALLED ENGINE PER T/C 5000 ALL SYSTEMS CK'D GOOD M/M 71-00-00.

Part: SUMP DRAIN — LEAKING (FUSELAGE)

ON TAKEOFF A VERY STRONG SMELL OF FUEL WAS DETECTED IN COCKPIT AND UPPER DECK ODOR LASTED ABOUT 5 MINUTES. FOUND (2) SUMP DRAINS LEAKING (REF ITEMS 1 AND 2) RESULTING IN FUEL ENTERING INTO THE BODY FAIRINGS AND A/C BAY CLEANED AND SECURED GROUND SERVICE CONNECTOR DOOR (REF EO B747-2120- 9566A). RAN PACKS AND RECIRC FAN NO FUEL ODORS DETECTED.

Part: FIRE WARN LIGHT — FALSE WARNING (COCKPIT)

INSPECTION TYPE:N/A, MASTER FIRE WARNING LIGHT ILLUMINATED AND FIRE BELL SOUNDED MOMENTARILY ON 3 SEPARATE OCCASIONS IN FLIGHT. NO SOURCE OR OTHER SUPPORT INDICATIONS OBSERVED. RESEATED ALL FIRE WARN CARDS, OPS CK ENGINE, CARGO FIRE, SMOKE WARNING SYS AND OPS CK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

BACKGROUND EMERGENCY LIGHT OUT ON F/O'S SIDE. REMOVED AND REPLACED BULB AS REQUIRED, F/C GOOD.

Part: PLATE — CRACKED (BS 140)

INSPECTION TYPE: C. FOUND WEB FLOOR STRUCTURE PLATE CRACKED AT BS 140 LBL 40. REPAIRED WEB FLOOR STRUCTURE PLATE BETWEEN BS 140 AND 150 LBL. 40 ACC. SRM 51-40-02.

Part: TRUSS FITTING — CRACKED (BS 1880)

INSPECTION TYPE: C. FOUND IN AFT CARGO COMP. THE FWD TRUSS FITTING CRACKED IN THE EDGE FROM LATCH SUPPORT STRUCTURE POS. NR 14. REPLACED BOTH LATCH SUPPORT AND TRUSS FITTINGS ACC. EO B747-5340-0191A APPX. D AT POS. NR 14 (INSTALLED/REPLACED PER TOPKIT 63B12792-13).

Part: SEAT TRACK — CRACKED (BS 990)

INSPECTION TYPE: C. MAIN DECK INTERIOR BS 990 RBL 98 SEAT TRACK CORRODED/CRACKED. REPAIRED SEAT TRACK FROM BS 990 TO 1070 RBL 98 I.A.W. SRM 53-10-05 FIG. 34.

Part: FRAME — SEVERED (BS 1660)

INSPECTION TYPE: C. FUSELAGE FRAME BS 1660 IS 75 PERCENT SEVERED BETWEEN STR 13 AND 14 LT. REPLACED FRAME AT BS 1660 LT FROM STR 13 TO STR 17 ACCORDING SRM 51-30-02 AND SIM 65B01777-401.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE: C. FOUND CORROSION BETWEEN THE UPPER FRONT SPAR CHORD AND UPPER WING SKIN AT RT ILES 847.50. REMOVED FASTENERS ON WING SKIN ACC. SRM 51-30-02. REMOVED CORROSION ON WING SKIN ACC. SRM 51-10-01 WING SKIN OUT OF LIMITS ACC. SRM 57-30-01 FIG. 1. REPAIRED WING SKIN ACC KLM DFX 96-241. APPROVED PER UPS EFN 747-57-0347.

Part: SEAT TRACK — CORRODED (BS 440/475/500)

INSPECTION TYPE: C. SEAT TRACK LBL 11.33 IS CORRODED AT BS 440, 475 AND 500. DAMAGE EXCEEDED ALLOWABLE LIMITS IAW SRM 53-10-01. REPLACED SEAT TRACK PARTLY FROM BS 390 TO BS 520 IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 980)

INSPECTION TYPE: C. FOUND DURING REPLACEMENT OF BSTA 1000 LOWER CHORD (EO B747-5310-5301E) CORROSION ON WEB OF FRAME BSTA 980 NEAR STR 46 LT AFT SIDE OF FRAME. CORRODED PART OF WEB IS OUT OF LIMITS ACC. SRM 53-10-01 ITEM 1 NOTE B. REMOVED CORRODED PART OF WEB, CUT OUT IS 2 SQUARE INCH. REPAIRED FRAME ACC. SRM 53-10-04 FIG. 52 DETAIL 2.

Part: TRUSS FITTING — CRACKED (BS 650)

INSPECTION TYPE: C. FWD CARGO COMP. LOWER DOORWAY SILL. FOUND TYPE 'B' CRACK IN LOWER FLANGE OF FWD TRUSS FITTING OF POS. NR 7 LATCH SUPPORT FITTING. REPLACED BOTH LATCH SUPPORT AND TRUSS FITTINGS P/N TOPKIT 63B12792-20 ACC. EO B747-5340-0191 APPX. D AT POS NR 7.

Part: FRAME — DENTED (BS 1740)

INSPECTION TYPE-C, AFT CARGO COMP, DURING INSPECTION PER EO B747-5310-0180D, FOUND DENTS IN FRAME INNER FLANGE AND DEFORMED FRAME WEB AT BS 1740, BETWEEN S-38 AND 40RT. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-0.

Part: SHEAR TIE — CRACKED (BS 1540)

INSPECTION TYPE: C. FRAME TO SKIN SHEAR TIE BS 1540 HAS EDGE CRACK BETWEEN STR 21 AND 23 LT. REPLACED SHEAR TIE AT BS 1540 STR 21 AND STR 23 LT ACC SRM 51-30-02.

Part: SHEAR TIE — BENT (BS 1060)

INSPECTION TYPE: C. FOUND SHEAR TIE BENT AT BS 1060 BETWEEN STR 2 AND 3 RT. REPAIRED SHEAR TIE AT BS 1060 AT STR 2 AND 3 RT, ACCORDING SRM 51-20-01.

Part: FLOOR BEAM — DAMAGED (BS 380)

INSPECTION TYPE: C. SEVERAL SMALL HOLES DRILLED IN FLOOR BEAM UPPER CHORD AT BS 380 BETWEEN LBL 61 AND LBL 81. REPAIRED FLOOR BEAM UPPER CHORD ON BS 580 BETWEEN LBL 61 AND LBL 81 ACCORDING SRM 51-40-04 FIG.1.

Part: SHEAR TIE — CRACKED (BS 1540)

INSPECTION TYPE: C. AT BS 1500 AND 1540 SHEAR TIE CRACKED BETWEEN STR 21/22 RT. REPLACED SHEAR TIE AT BS 1500 AND 1540 BETWEEN STR 21/22 RT ACC. SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 220-250)

INSPECTION TYPE: C. FOUND CORROSION ON SEAT RACK ON BS 220 TO BS 250 AT RBL 52. REMOVED CORROSION AT SEAT TRACK ON BS 220 TO BS 250 AT RBL 52 ACC SRM 51-10-01 CORROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED SEAT TRACK FROM BS 210 TO BS 290 ACC. SRM. 53-10-05 FIG. 1.

Part: FRAME — CRACKED (BS 1500)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE BS 1500, S-40RT. STOP DRILLED CRACK AND REPAIRED FRAME INNER FLANGE ACC SRM 53-10-04 FIG 66.

Part: BULKHEAD CHORD — CRACKED (BS 1000)

INSPECTION TYPE: C. FWD CARGO COMPARTMENT: AFTER HFEC INSPECTION, FOUND BULKHEAD CHORD STA 1000 CRACKED BETWEEN STR 46/47 RT, CRACK LENGTH APPROX. 40MM. REPLACED LWR CHORD SEGMENT AT BS 1000 ACC. EO B747-5310-5301-E PER SALES ORDER NR 69494-20.

Part: WEB — CORROSION (BS 280)

INSPECTION TYPE: C. CORROSION BETWEEN WEB AND FLOOR BEAM UPPER CHORD AT BS 280 BETWEEN RBL 20 AND LBL 20. CORROSION ON WEB AT LBL 10 OUT OF LIMITS AFTER REWORK. REPAIRED I.A.W. SRM 51-40-02 FIG. 1.

Part: GATE ASSY — CORRODED (MED 5 LT)

INSPECTION TYPE: C. FOUND LOWER GATE OF DOOR 5 LT CORRODED. DAMAGE EXCEEDED ALLOWABLE LIMITS IAW SRM 52-00-02. REPLACED LOWER GATE OF DOOR 5 LT IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 460)

INSPECTION TYPE: C. SEAT TRACK CORRODED AT BS 460 AT RBL 90. REMOVED CORROSION ON SEAT TRACK ACC. SRM 510-10-01. CORROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED SEAT TRACK FROM BS 410 TO BS 460 AT RBL 90 ACCORDING SRM 53-10-05.

Part: CHORD — CORRODED (BS 220)

INSPECTION TYPE: C. FOUND CORROSION ON UPPER CHORD AT BS 220 AT LBL 59. REMOVED CORROSION ON UPPER CHORD ON BS 220 LBL 59 ACC. SRM 51-10-01. CORROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED UPPER CHORD FROM LBL 58 TO LBL 82 ACC. SRM 53-10-07 FIG. 8.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE: C. MED NR 5 LT FWD FRAME WEB CRACKED WL 250 APPROX. REPLACED FRAME WEB AT MED 5 LT WL 250 APPROX. ACCORDING SRM 51-30-02.

Part: WEB — DAMAGED (BS 2160)

INSPECTION TYPE-C, FOUND A HOLE IN WEB AT STA 2160 LT LOWER SIDE IN BULK CARGO COMPARTMENT. REMOVED DAMAGED SECTION OF WEB AND REPAIRED WEB ACC TO SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE: C. MED 5 RT FORWARD FRAME WEB CRACKED WL 250 APPROX. REPLACED WEB AT MED 5 RT WL 250 APPROX. ACCORDING SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 255)

INSPECTION TYPE-C, SEAT TRACK AT BS 255 AT LBL 53 IS CORRODED, CORROSION BEYOND LIMITS. REPLACED DAMAGE SEAT TRACK FROM BS 310 AT LBL ACC SRM 53-10-05 FIG 1.

Part: SEAT TRACK — CORRODED (BS400/440)

INSPECTION TYPE: C. SEAT TRACK RBL 11.33 CORRODED AT BS 400 AND BS 440. REPAIRED SEAT TRACK AT BS 370 TO BS 410 RBL 11.33 ACC. SRM 53-10-05 FIG. 1.

Part: DOUBLER — MISINSTALLED (BS 310)

INSPECTION TYPE: C. EXISTING REPAIR INCORRECT. INSTALLED ACC. EO B747-5330-1431C APPX 9.6 STEP 4 AND APPX. 8.5 STEP 2 AT BS 310 STR 8A LT. INSTALLED DOUBLER AT BS 310 STR 8A LT ACC TO EO B747-5330-1431 APPX. 8.5 AND APPX. 8.6.

Part: SKIN — CORRODED (BS 1100)

INSPECTION TYPE: C. EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN BS 1100 RBL 117 SKIN CORRODED. REWORKED CORROSION IAW SRM 51-10-01. DAMAGE AFTER REWORK OUT-OF-LIMITS IAW SRM 57-30-01. REPAIRED CENTER WING UPPER SKIN IAW KLM DFX 96-243/EFN 747-57-0346 AND REF. UPS-AMS-96-0262RE.

Part: FILLER — CORRODED (BS 1240)

INSPECTION TYPE: C. CENTER SECTION UPPER SKIN: BS 1240 LT REAR SPAR UPPER SPLICE PLATE FILLER CORRODED. REMOVED CORROSION AT BS 1240 LT REAR SPAR UPPER SPLICE FILLER ACC. SRM 51-10-01, OUT-OF-LIMITS ACC. SRM 53-10-01. REPLACED FILLER ACC. SRM 51-10-10.

Part: SEAT TRACK — CRACKED (BS 1000/1265)

INSPECTION TYPE: C. MAIN DECK INTERIOR: BETWEEN BS 1000 AND BS 1265 RBL 33 SEAT TRACK CORRODED/CRACKED. CORROSION CRACKS EXCEEDING AND ALLOWABLE LIMITS I.A.W. SRM 53-10-01. REPLACED SEAT TRACK I.A.W. SRM 53-10-05 FIG.34.

Part: SKIN — CORRODED (BS 1100)

INSPECTION TYPE: C. EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN BS 1100 RBL 93 SKIN CORRODED. REWORKED CORROSION IAW SRM 51-10-01. DAMAGE AFTER REWORK OUT-OF-LIMITS IAW SRM 57-30-01. REPAIRED CENTER WING UPPER SKIN IAW DFX 96-243/EFN 747-57-0346 AND REF. UPS-AMS-96-0262RE.

Part: SEAT TRACK — DAMAGED (BS 1100)

INSPECTION TYPE: C. MAIN DECK INTERIOR: BS 1100 RBL 11, SEAT TRACK CROWN DAMAGED. REPAIRED SEAT TRACK FROM BS 1090 TO BS 1110 AT RBL 11 ACC. SRM 53-10-05 FIG. 34.

Part: SMOKE DETECTOR — FAILED (AFT CARGO COMPT)

LOWER CARGO LT BLINKED ON BRIEFLY ACCOMPANIED BY A BELL. ALL OTHER INDICATIONS WERE NORMAL. REMOVED AND REPLACED 6 AFT SMOKE DETECTORS, OPS CHECK GOOD.

Part: HANDLE — OUT OF POSITION (CARGO DOOR)

INSPECTION TYPE N/A, LOWER AFT CARGO DOOR WARNING LIGHT ILLUMINATED AT ROTATION. FOUND HANDLE IN THE UNLOCKED POSITION. INSPECTED AND OPERATED LOWER AFT CARGO DOOR HANDLE, NO DEFECTS NOTED.

Part: DECK HEATER — MALFUNCTIONED (COCKPIT)

CREW REPORTED STRONG ELECTRICAL SMELL BEGAN DURING DESCENT. ISOLATED TO RT UPPER DECK HEATER. NO ABNORMAL INDICATIONS, BUT BURNING SMELL RECURRED WITH RT UPPER DECK HEATER ON. DEFFERED RT UPPER DECK HEATER, M 10789 ASSIGNED PER MEL SEQ NR 21-18-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

MAINTENANCE REPORTED, CREW SERVICE DOOR 2 EMERGENCY EXIT LIGHTS INOP AT TOP OF DOOR FRAME. REMOVED AND REPLACED BATTERY PACK.

Part: EEL WIRE — BROKEN (CARGO DECK)

WHILE IN 'A' CHECK, MAINTENANCE FOUND MAIN CARGO DECK RT OVERHEAD FWD EMERGENCY LIGHT INOP. FOUND BROKEN WIRE, REPAIRED SAME, CHECKS OK.

Part: SKIN — DENTED (BS 2598)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND A DEEP DENT IN THE FUSELAGE SKIN JUST INBOARD FWD OF AFT JACKPOINT BODY STATION 2598. MAINTENANCE CHECKED THE DENT PER SRM 53-30-01 AND FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER AT STA 2598 AROUND JACKPOINT PER SRM 53-30-03 FIGURE 1A.

Part: FRAME — DENTED (BS 1760)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1760 RT AT STR 10 AND 11 RT. FOUND DENTS OUT OF LIMITS ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 AND UPS EFN NR 747-53-0733.

Part: T-CHORD — CRACKED (BS 560)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FWD LOWER CARGO COMP T-CHORD CRACKED AT 'B' STA 560 LBL 48 AND AT 'B' STA 560 LBL 27 WL 120. REPLACED T-CHORD ACC SRM 53-10-07, CHORD REPAIRED ACC UPS EFN 747-53-0729.

Part: FLOORBEAM — CORRODED (BS 2200)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND INTERNAL BODY STA 2200 RBL 33 TO RBL 75 FLOORBEAM BADLY CORRODED. REWORKED CORROSION ACC SRM 51-10-01 AND REPLACED UPPER CHORD ACC SRM 53-10-07.

Part: FRAME — DENTED (BS 1860)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1860 RT AT STR 13 TO 14 RT. FOUND DENTS OUT OF LIMIT ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 UPS EFN NR 747-53-0733.

Part: FRAME — DENTED (BS 1800)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1800 RT AT STR 10 AND 11 RT. FOUND DENTS OUT OF LIMITS ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 AND UPS EFN NR 747-53-0733.

Part: REVEAL — CRACKED (BS 2240)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER REVEAL DOOR 5 RT AT STA 2240. REPAIRED UPPER REVEAL DOOR ACC UPS EO 747-53-0730.

Part: FRAME — CRACKED (BS 2702)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND APU COMPT FRAME CRACKED 1.5 INCHES LONG, LT SIDE AT BS 2702 WL 313. CRACK OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FRAME AT BS 2702 WL 313 IAW SRM 51-40-03, FIG 3.

Part: FLOORBEAM — CORRODED (BS 1500)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT THE FLOOR BEAM BETWEEN LBL 98 AND LBL 75, STA 1500. FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM IAW SRM 53-10-07, FIG 12, AT LBL 75 TO 98 AT BS 1500.

Part: FLOORBEAM — CORRODED (BS 1580)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FLOORBEAM CORRODED RBL 33.99, STA 1580 FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FLOORBEAM IAW SRM 53-10-07, FIG 12, AT 33.99 RBL STA 1580.

Part: FLOORBEAM — CRACKED (BS 460)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 460 STR 13A RT FLOORBEAM HAS CRACK ON FORWARD FACE OF WEB 1 INCH LONG AT THE UPPER SIDE OF THE WEB. CRACK OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FLOORBEAM WEB ACC SRM 53-10-07, FIG 11, AT BS 460, STR 13A RBL 90.

Part: STRINGER — CRACKED (BS 2140-2160)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BETWEEN STA 2140 - 2160, STR 27 RT CORROSION AND CRACKS. REMOVED CORROSION AND STOP DRILLED CRACKS ACC TO SRM 51-10-01. REPAIRED STRINGER ACC TO SRM 53-10-03, FIG 2.

Part: STRINGER — CORRODED (BS 982)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STR 67R ON BSTA 982 IS CORRODED. CORROSION IS OUT OF LIMITS ACC SRM 53-10-01, FIG 1, DETAIL 1. REMOVED CORRODED PART AT BSTA 970 AND REPAIRED STRINGER ACC SRM 53-10-03, FIG 1 DETAIL 1. MATERIAL EXISTING STRINGER IS 0.090 INCH 7075T6.

Part: STRINGER — CRACKED (BS 1740)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STRINGER END CRACKED AND CORRODED AT BSTA 1740, RT SIDE STR 32 (UNDER SPLICE). REPAIRED STR 32 AT BSTA 1740, RT PER SRM 53-10-03.

Part: FLOORBEAM — CORRODED (BS 1580)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT FLOORBEAM BETWEEN LBL 98 AND LBL 75, STA 1580. FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM IAW SRM 53-10-07, FIG 12, FROM LBL 98 TO 75, STA 1580.

Part: FRAME — CRACKED (BS 1640)

WHILE IN AMSTERDAM FOR-C CHECK, MAINTENANCE FOUND FRAME CRACKED ON TOP OF BSTA 1640 NEAR STR 29 (JUST ABOVE STRINGER CLIP). CRACK IN FRAME AT BSTA 1640 NEAR STR 29 RT, REPAIRED PER SRM 51-40-03, FIG 7.

Part: WEB — CRACKED (BS 1620-1640)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND WEB PLATE ON RBL 11.33 STA 1620 TO 1640 CORRODED AND CRACKED. CORROSION AND CRACK OUT OF LIMITS ACC SRM 53-10-01. REPLACED WEB IAW SRM 51-10-01, AT BS 1620 TO 1640 RBL 11.33.

Part: FLOORBEAM — CORRODED (BS 2220)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2220 RBL 65 CORROSION IN TOP FLANGE OF FLOORBEAM. CORROSION ON UPPER CHORD OUT OF LIMITS ACC SRM 53-10-01. REPLACED UPPER CHORD FROM RBL 44 TO RBL GD ACC SRM 53-10-07.

Part: FLOORBEAM — CORRODED (BS 2140)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND THE FUSELAGE FLOORBEAM BADLY CORRODED AT STA 2140 RBL 33. RENEWED FLOORBEAM AT STA 2140 RBL 11 TO RBL 99 ACC SRM 53-10-01.

Part: STRINGER — CRACKED (BS 1965)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACKS IN STRINGER UNDER STRINGER END FITTING BS 1965, S-30 LT. REMOVED DAMAGED PART OF STRINGER FROM BS 1965 TO BS 1985 AND REPAIRED STRINGER ACCORDING SRM 53-10-03 FIG 1.

Part: FLOORBEAM — CORRODED (BS 2240)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2140 RBL 95 TO RBL 105 FLOORBEAM CORRODED. CORROSION AT FLOORBEAM RBL 95 TO RBL 105 STA 2140 OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM ACC 53-10-07.

Part: STRINGER — CRACKED (BS 1940)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND AT 'B' STA 1940 RT SIDE STRINGER 34 CORRODED AND CRACKED. CORROSION AND CRACK WHERE OUT OF LIMITS PER SRM 53-10-07. REPAIRED STR 34 AT 'B' STA 1940 PER SRM 53-10-03 FIG 2.

Part: STRINGER — CRACKED (BS 1500-1520)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT STR 33 BETWEEN 'B' STA 1500 TO 1520, CORRODED AND CRACKED. CORROSION AND CRACK ARE OUT OF LIMITS PER SRM 53-10-07. REMOVED DAMAGE STR PARTS FROM 'B' STA 1510 TO 1530 AND REPAIRED ACC SRM 53-10-03 FIG 1.

Part: SEAT TRACK — CORRODED (BS 2000-2060)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2160 - BS 2000 RBL 98 WEB PANEL AND SEAT TRACK CORRODED. REPAIRED WEB PANEL IAW SRM 51-40-02, FIG 1. REPLACED SEAT TRACK IAW SRM 51-10-01.

Part: FRAME — CRACKED (BS 2040)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STR 29 AT BS 2040 LT CORRODED AT FRAME LOCATION. NO CORROSION FOUND IN STRINGER, BUT A CRACK ON FRAME WEB AT DESCRIBED LOCATION, DUE TO CORROSION. STOP-DRILLED CRACK AND REMOVED CORROSION ACC SRM 51-10-01 AND REPAIRED WEB ACC SRM 53-10-04, FIG 39.

Part: D-BEAM — CRACKED (RT WING)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT WING WBL 470 D-BEAM CRACKED IN FRONT OF PYLON 3. D-BEAM REPAIRED ACC SRM 57-30-04.

Part: STRINGER — CORRODED (BS 982)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND END OF STR 47R ON BSTA 902 IS CORRODED, CORROSION IS OUT OF LIMITS, ACC. SRM 53-10-01, FIG. 1, NOTE-B. REPAIRED STRINGER FROM 970 TO BSTA 984 ACC. SRM. 53-10-03, FIG. I, DETAIL I, MATERIAL EXISTING STRINGER IS 0.90 INCH 7075T6.

Part: SKIN — DAMAGED (NR 4 PYLON)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PYLON NR 4 NAC: STA 225, SKIN DAMAGED BY WEAR ON TOP OF PYLON, OUTBOARD SIDE. SKIN REPAIRED ACC: S.R.M. 54-30-03 FIG 17A.

Part: WEB PLATE — CRACKED (BS 1620-1640)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND WEB PLATE ON RBL 11.33 STA 1620 AND 1640, CORRODED AND CRACKED. CORROSION AND CRACK OUT OF LIMITS ACC SRM 53-10-01. REPLACED WEB IAW SRM 51-10-01, AT BS 1620 TO 1640 RBL 11.33.

Part: BLKHD WEB — CRACKED (NR 2 PYLON)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PYLON NR 2 CRACKED, ON THE AFT BULKHEAD LWR SIDE WEB. CRACK WAS OUT OF LIMITS ACC SRM 54-10-01 FIG 1 PAGE 4. WEB HAS BEEN REPAIRED ACC SRM 51-40-02.

Part: EEL BULB — INOP (CABIN)

WHILE ON GROUND, MAINTENANCE CREW FOUND FWD LWR ENTRANCE DOOR AFT EMER LAMP OUT. RELAMPED, OPS CK NORMAL.

Part: EEL BULBS — FAILED (FLIGHT DECK)

MAINTENANCE REPORTED, CREW SVC DOORWAY EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK.

Part: EEL BULBS — FAILED (FLIGHT DECK)

MAINTENANCE REPORTED, CREW SVC DOOR SILL EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, EMERGENCY BATTERY PACK FAILED, LOCATED OVER C/P EMER EXIT. REPLACED BATTERY PACK.

Part: EEL — INOPERATIVE (FLIGHT DECK)

PILOT REPORTED THAT IN HKG, SEVERAL EMERGENCY LIGHTS UNDER THE INST GLARESHIELD ARE BURNED OUT. FILAMENTS REPLACED. LIGHTING OK.

Part: EEL — FAILED (FLIGHT DECK)

PILOT REPORTED SEVERAL EMER LIGHTS UNDER INSTRUMENT GLARESHIELD ARE BURNED OUT. CENTER BULBS ON BOTH ENDS. F/O,FAR RIGHT BULB. RELAMPED EMERGENCY LIGHTING. OPS CHECK GOOD.