N691UP

Part: CIRCUIT BOARD — FAILED (E/E BAY)

INSPECTION TYPE:N/A ON LEVEL OFF AT 11,000, ON DECENT LOWER CARGO FIRE LIGHT ILLUMINATED INTERMITTENTLY REPLACED FIRE WARING CARD "A8" ON FIRE WARNING P6 CARD FILE. TESTED LOWER CARGO FIRE WARNING IAW 26-16-00 PGS 501-504. OPERATIONAL CHECK WAS NORMAL

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT CEILING EMERGENCY LIGHT INOP R/R EMERGENCY LIGHT POWER PACK

Part: BOTTLE — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A CREW AND COURIER O2 DEPLETED IN ROUTE R AND R BOTTLES ALL REGS OP CHECK NORMAL

Part: FRAME — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE: C, LT WING CRACK FOUND ON UPPER AND LOWER CHORD AND WEB ON L/E AT ILES 1110. NEW CHORDS FABRICATED IAW EO206770 AND EO206774 AND REFITTED IAW QUERY NOTE 100/2000.

Part: STIFFENER — CRACKED (NACELLE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, NR 1 STRUT STIFFENER CRACKED AT VERT BULKHEAD NAC STA 180. NEW BRACKET FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CRACK IN FWD CARGO HOLD FLOOR SKIN AT BS 478 RBL 36. REPAIRED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (RT WING SPOILER) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING T/E SPOILER SUPPORT BEAM WEB CRACKED AFT OF 6 FLAP TRANSMISSION. REPAIR ACCOMPLISHED, SPLICE REPAIR USING 15.5 PH CRES ANGLES IAW QUERY NOTE 102/000 FORM 8110 ISSUED.

Part: FLANGE — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1453. REPAIR CARRIED OUT IAW SRM 57-20-03.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, PLEASE REPLACE CORRODED WINDOW FORGINGS AT BS 240 - 260 LT SIDE IAW SRM. WINDOW FORGING REMOVED IAW SRM 51-30-02 NEW FORGING FITTED SRM 51-30-02 & QUERY NOTE N691UP 11/2000.

Part: FORGING — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, REPLACE CRACKED WINDOW FORGING BS 1460 - 1480 RT SIDE. WINDOW FORGING REPLACED IAW SRM 51-30-02.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, VERTICAL STABILIZER T/E CRACK ON TRAILING EDGE BEAM AT FIN STA 245 RT. REPAIRED TRAILING EDGE BEAM WEB IAW SRM 55-30-06.

Part: WEB — CRACKED (RUDDER) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LOWER RUDDER L/E FAIRING, TWO WEBS CRACKED AT FOLLOWING LOCATIONS RT RUD STA 147 AND LT RUD STA 32. WEB AT RT RUD STA 147 REPAIRED IAW SRM 51-40-02 FIG 2 2. NEW WEB FABRICATED IAW EO100921 AND FITTED IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CONTROL CABIN INTERCOSTAL IS CRACKED AT BS 360 - 380 BETWEEN STR 1 AND 2 RT. CRACKED INTERCOSTAL REMOVED AND NEW INTERCOSTAL FABRICATED AND FITTED IAW SRM 51-30-02.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT HORIZONTAL STABILIZER INTERIOR CORROSION FOUND ON A RIGHT ANGLE FITTING AT STAB STA 243, BETWEEN REAR SPAR AND S1 UPPER SURFACE. PLEASE INVESTIGATE NEW FITTING, FABRICATED IAW E0100940 AND FITTED IAW SRM 51-30-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, AIR COND CRACK IN RAM AIR DUCT STIFFENER AT BS 960. NEW STIFFENER FABRICATED IAW BAC5300 AND FITTED IAW SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, APU COMPT FRAME CRACKED RT SIDE BS 2675 WL 310. FRAME REPAIRED IAW SRM 51-40-03 USING 2024 T3 .040.

Part: FLANGE — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED ON L/E RIB AT OLES 1421.35. REPAIRED RIB IAW SRM 57-20-03 FIG 1.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT OLES 1525.45 FOUND CRACKED. RIB REPLACED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE FOUND CRACKED BY NDT INSP ON L/E RIB AT OLES 1411.85. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1534.95. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — WORN (VERTICAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, TAIL VERTICAL FIN LWR L/E SECTION OF RIB WORN AT CONTACT AREA WITH DORSAL FIN. RIB REPLACED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING L/E CRACKING ON UPPER FLANGE OF L/E RIB AT OLES 1390.75. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CRACKED RIB UPPER CHORD ON LT HORZ STAB BEHIND R/SPAR AT STAB BL 39 1. CHORD REPAIRED IAW SRM 51-40-03.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, TAIL VERTICAL STABILIZER T/E BEAM SUPPORTS FOUND CRACKED AT RUD STA 132 LT, RT, 157 LT, 267 LT RT ,282 LT & RT, 307 LT & RT, 332 RT AND 367 RT. REPAIRS TO STAB (VERTICAL) T/E BEAM SUPPORTS REPAIRED IAW SRM 51-40-03 AND Q/NOTE 54/2000 CLOSURE STRIPS DE RIVETED TO ACCESS REPAIRS AND RE-INSTALLED ON COMPLETION.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT HORZ STAB REAR SPAR UPPER CHORD CORRODED AT STAB BL 380. CHORD REPAIRED IAW QUERY NOTE 56/200.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 878.55. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIBS AT ILES 928.96. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 852.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 792.55. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT ILES 964.55 L/E RIB CRACKS. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 705.55. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT L/E CRACKING ON UPPER FLANGE ON L/E RIB AT OLES 1493.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 802.6. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 964.55. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 938.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1048.25. NEW RIB INSTALLED RIB REPLACED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 802.5. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 756.95. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 1014.95. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, DOOR 4 LT REMOVED FOR REPAIR OF FWD FRAME DAMAGE. NR 4 DOOR FWD FRAME REPAIRED IAW SRM 52-10-02 FIG 13. MATERIAL AIS I301 .050 HFEC INSP ACCOMPLISHED ON CRACK ENDS REPAIR PIECE CAD PLATED.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 928.96. NEW RIB INSTALLLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE OF L/E RIB CRACKED AT ILES 756.95. REPAIR CARRIED OUT IAW SRM 57-20-03 FIG 1. FASTENERS FITTED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB ILES 878.55. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 768.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 852.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 938.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E AT ILES 928.95. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE ON L/E RIB AT ILES 889.5. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 716.08. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE ON L/E RIB AT ILES 1024.45. CRACKS REPAIRED IAW SRM 57-20-03 FIG 3 USING 2024 T3 X 0.125.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 768.45. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 974.05. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT ILES 842.96. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, DOOR NR 4 LT FWD FRAME, BETWEEN UPPER HINGE CUTOUT AND STOP NR 5 FROM TOP, IS DAMAGED. DAMAGE CLEANED UP AND WITHIN SRM LIMITS IAW SRM 53-10-01 AND AREA REPROTECTED IAW SRM 51-10-02.

Part: DOUBLER — CRACKED (NLG WW) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, NLG CRACK FOUND ON THE FWD LOWER CORNER STRUCTURE OF THE WHEEL WELL LT SIDE. CRACK EXTENDS UNDER THE LOWER CHORD OF THE BULKHEAD. CRACKS ARE PERMITTED IAW SB 747-53-2112 R3 IN UNDER SKIN DOUBLER. PREVIOUS MODIFICATION ACCOMPLISHED IAW UPS EO B747-5330-0367 SECTION 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, DOOR NR 4 RT FWD FRAME, BETWEEN UPPER HINGE CUTOUT AND STOP NR 5 FROM TOP, IS DAMAGED. DOOR REMOVED IAW SRM 52-11-01 AND ROUTED TO SHOP FOR REPAIR. FWD FRAME REPAIRED IAW SRM 52-10-02. BOTTOM FRAME FABRICATED IAW QUERY NOTE 42/2000 AND FITTED IAW BAC 5300. DOOR REFITTED IAW SRM 52-10-01.

Part: STOP — CRACKED (PAX DOOR) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, DOOR NR 2 RT DOOR STOP FITTING 4 FROM TOP ON THE FWD SIDE IS CRACKED. DOOR REMOVED IAW MM 52-11-01 AND SEND TO SHOP. REPLACED STOP FITTING IAW BAC 5300. REFITTED DOOR IAW MM 52-11-01.

Part: PIPE — CORRODED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING SURGE TANK DRAIN PIPE FLANGES FOUND CORRODED AT WS 889.5 AND WS 982 TWO PIPES IN TOTAL. TWO SURGE TANK DRAIN PIPES REPLACED IAW MM 28-21-19.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1462.85. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED FWD END OF L/E RIB AT OLES 1318.65. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT VARIOUS LOCATIONS ON L/E RIB AT OLES 1380.75. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AFT END OF L/E RIB AT OLES 1349.25. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING CRACK AT L/E RIB OLES 1267.65. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1205.6. L/E RIB REPAIRED IAW SRM 57-20-03 FIG 1.

Part: RIB — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED AT AFT END OF L/E RIB OLES 1277.15. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1483.95. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED TWO LOCATIONS ON L/E OLES 1246.35. L/E RIB REPAIRED IAW SRM 57-20-03 FIG 1.

Part: FLANGE — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED AT FWD END OF L/E RIB AT OLES 1349.25. REF NRC 44310792.

Part: RIB — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING CRACK AT LOWER FWD TIP OF L/E RIB AT OLES 1381.25. L/E RIB REPAIRED IAW SRM 57-20-03.

Part: RIB — CRACKED (RT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, RT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1277.15. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: SUPPORT FITTING — CRACKED (MLG) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, ULTRASONIC INSPECTION CARRIED OUT ON BLG RETRACT ACTUATOR SUPPORT FITTINGS, IAW NDTMPT4 53-40-02. LT FITTING CRACKED IN THE O/B EDGE OF THE I/B LUG. CRACK CONFIRMED USING HFEC. LT BLG RETRACT ACTUATOR SUPPORT FITTING REPLACED IAW EO747-5340-0994.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING CRACK ON L/E RIB AT OLES 1453.35. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 1301 BETWEEN STR 15 AND 16 RT. SHEAR TIE FABRICATED IAW SRM 51-20-01 AND FITTED IAW SRM 51-30-02.

Part: RIB — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING UPPER FLANGE CRACKED ON L/E RIB AT OLES 1390.75. NEW RIB INSTALLED IAW SRM 51-30-02.

Part: SPLICE — CORRODED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING LOWER FALSE WORK SUPPORT BEAM CRACKED AT ILES 813. REPAIR CARRIED OUT IAW SRM, QUERY NOTE 93/2000 SPLICED IN NEW SECTION OF BEAM BS 806 - 818, FAA 8110 ISSUED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 2100 BETWEEN STR 20 AND 22 LT. NEW SHEAR TIE FABRICATED IAW EO100617 AND FITTED IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (NR 4 PYLON) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, NR 4 ENG PYLON NAC STN 150 APPROX INTERCOSTAL ACROSS FWD FIRESEAL CRACKED. NEW INTERCOSTAL FABRICATED IAW EO100830 AND FITTED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 2080 BETWEEN STR 20 AND 22 LT. NEW SHEAR TIE FABRICATED IAW EO100617 AND FITTED IAW SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING T/E INTERCOSTAL TO REAR ANGLE BRACKET CRACKED AT WS 570. NEW INTERCOSTAL TO REAR ANGLE BRACKET INSTALLED IAW 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 2140 BETWEEN STR 20 AND 22 LT. NEW SHEAR TIE FABRICATED IAW EO100617 AND FITTED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 2120 BETWEEN STR 20 AND 22 LT. NEW SHEAR TIE FABRICATED IAW EO100617 AND FITTED IAW SRM 51-30-02.

Part: DOUBLER — CORRODED (LT WING) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING CORROSION ON UPPER SURFACE OF FIXED L/E BULL NOSE AT WS 397 AT UPPER T/E. REPAIR CARRIED OUT IAW Q/NOTE 35/2000 AND SRM 57-30-04 FIG 2, 0.04 301 CRES 1/2 HARD DOUBLER CAD PLATED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, UPPER DECK FRAME WEB CRACKED AT BS 580 AT STR 6, 7 AND 8. REPAIR CARRIED OUT ON FRAME WEB IAW SRM 53-10-04 FIG 54.

Part: FRAME — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, FUSELAGE EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN AND FRAME AT BS 1000 BELOW STR 37. CORROSION REMOVED IAW SRM 51-10-01 REPAIR CARRIED OUT IAW SRM 53-30-03.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, R-BODY GEAR DOOR, SKIN CRACKED AND DAMAGED AT THE UPPER AFT CORNER. NEW DOOR FITTED IAW MM 32-14-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, UPPER DECK FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 660 AT STR 7 AND 8 RT. REPAIR CARRIED OUT ON FRAME WEB IAW SRM 53-10-04.

Part: STRUCTURE — CORRODED (RT MLG DOOR) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, R-BODY GEAR INNER DOOR, CORROSION ALONG THE UPPER EDGE, EXTERNALLY. NEW DOOR FITTED IAW MM 32-14-00 REF NRC 44309520/44309103.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, UPPER DECK FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 640 STR 8 LT. REPAIR CARRIED OUT ON FRAME WEB IAW SRM 53-10-04.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 280 - 300 LT. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10 -01 & B 56-20-01. CORR REMOVED DEPTH .009. REWORK SPLICED IN SECTION OF Z-STRINGER 22 LT IAW QUERY NOTE 10/200.

Part: FORGING — CORRODED (FUELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1350 TO BS 1372 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. CORROSION REMOVED = .06. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 40/2000 WHICH IS TO INSTALL TWO DOUBLERS TO ENCIRCLE THE COMPLETE WINDOW CUTOUT. OVERSIZE HOLES TO .0156 AND PERFORM OPEN HOLE HFEC FOR CRACKS. MAINTAIN EDGE MARGIN OF 1.5D.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING AT BS 860 - 880 RT SIDE CORRODED. REWORK OF WINDOW FORGING REMOVED IAW SRM 51-30-02 CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01. DEPTH OF CORR .008. CORR AND HOLES REWORKED IAW QUERY NOTE 19 /2000 HOLES O/SIZED AND NDT INSP.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, WINDOW FORGING REMOVED FOR CORROSION AT BS 920 - 940 RT. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW 51-10-01 & 65-20-01, DEPTH OF CORR .006. REWORKED IAW QUERY NOTE 64/2000 HOLES O/SIZED AND NDT INSPECTED. FORGING REFITTED IAW SRM 51-30-02 BOEING TLEX TEL-DUB-00-00765H- REF.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1600 TO BS 1620 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH OF CORROSION REMOVED IS .010 IAW SRM 56-20-01. REFIT FORGING IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY .0156 AND PERFORM OPEN HOLE HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5D AND REFIT FORGING.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1920 TO BS 1940 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .006. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156 AND HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1394 TO BS 1416 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .066. FORGING RE-INSTALLL ED IAW SRM 51-30-02 AND QUERY NOTE 29/2000. Q/NOTE IS TO BLEND OUT CORROSION AND OVERSIZE HOLES BY .0156. PERFORM OPEN HOLE HFEC FOR CRACKS MAINTAIN MIN EDGE MARGIN OF 1.5D.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1350 - 1372 LT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01, 56-20-01 O/SIZED HOLES AND NDT INSP IAW QUERY NOTE 65/2000 DEPTH OF CORR .010. FORGING RE-INSTALLED IAW 65/2000.

Part: FORGING — CORRODED (BS969-980 LH) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 960 - 980 LT CORRODED. WINDOW FORGING REMOVED IAW 53-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01. FORGING REFITTED IAW SRM 51-30-02, CORR DEPTH .008. BLEND OUTS IAW QUERY NOTE 64/2000 O/SIZE HOLES AND NDT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK FRAME WEB CRACKED AT CUTOUT FOR NR 2 MED BS 806 STR 16 & 17. FRAME REPAIR CARRIED OUT 2024 TO ALUMINIUM REPAIR ANGLE HEAT TREA TED, NDT ALL OPEN HOLES IN STRUCT AND REBUILD IAW QUERY NOTE 52/2 000 NR 2 DOOR STOP REVEAL REPAIR.

Part: FORGING — CORRODED (CABIN WINDOW) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 580 - 600 LT SIDE CORROSION. FORGING REMOVED, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01 DEPTH OF CORR .008. FORGING REFITTED IAW SRM 51-30-02, BLEND OUTS ACCOMPLISHED IAW QUERY NOTE 63/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1480 TO BS 1500 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED =.009. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE THE HOLES BY .0156 AND PERFORM AN OPEN HOLE HFEC FOR CRACKS MAINTAIN EDGE MARGIN OF 1.5. BLENDOUT ALL CORROSION.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 880 - 900 LT CORROSION FOUND. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, DEPTH OF CORR .009. FORGING REFITTED IAW SRM 51-30-01, BLEND LIMITS IAW QUERY NOTE 64/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 2000 TO BS 2020 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED PER SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. HFEC ALL HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1800 TO BS 1820 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 920 - 900 RT SIDE. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01. CORR DEPTH .008. BLEND OUTS AND HOLE REWORK O/SIZE AND NDT INSP IAW QUERY NOTE 17/2000. FORGING RE-INSTALLED IAW 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 2180 TO BS 2200 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED PER SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C 44, CABIN WINDOW FORGINGS. CORROSION FOUND ON FORGING AT BS 200 TO BS 220 RT. FORGING REMOVED AND CORROSION CLEANED UP TO WITHIN LIMITS. CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. DEPTH OF CORROSION REMOVED .005. FORGING REPROTECTED IAW SRM 51-10-02. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 62/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1372 TO 1394 LT. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW 51-10-02 & 56-20-01, DEPTH OF CORR .009, REWORKED WINDOW O/SIZED HOLES AND NDT INSP IAW QUERY NOTE 65/2000. FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1394 TO BS 1416 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01 CORROSION REMOVED = .068. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 29/2000. CORROSION BLENDOUT OUTSIDE LIMITS BUT ACCEPTABLE PER Q/NOTE. OVERSIZE HOLES BY .0156 AND HFEC FOR CRACKS. MIN EDGE MARGIN 1.5D FAA 8110-3 ISSUED.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 600 - 620 LT. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, CORR DEPTH .006. FORGING REFITTED IAW SRM 51-30-02, BLEND OUTS IAW QUERY NOTE 63/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1520 TO BS 1540 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .007. FORGING RE-INSTALL ED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLENDOUT ALL CORROSION OVERSIZE HOLES AND PERFORM OPEN HOLE HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, LT WING W/WELL CORROSION ON THE OVERWING LONGERON BS 1266 - 1303 - 1332. NEW LONGERON WEB FITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1620 TO BS 1640 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .008. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION, OVERSIZE HOLES AND HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 700 - 720 LT CORRODED. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10- 01, CORR DEPTH .009. FORGING REFITTED IAW SRM 51-30-02, BLEND OUTS ACCOMPLISHED IAW QUERY NOTE 63/200 AND SRM 56-20-01.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1580 TO BS 1600 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .009. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION OVERSIZE HOLES BY .0156 AND HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CORROSION FOUND ON WINDOW FORGING BS 860 - 880 LT SIDE. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, DEPTH OF CORR .009. FORGING REFITTED IAW SRM 51-30-02, BLEND OUTS ACCOMPLISHED IAW QUERY NOTE 43/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C 44, CABIN WINDOW FORGINGS. CORROSION FOUND ON FORGING AT BS 220 TO BS 240 RT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. DEPTH OF CORROSION REMOVED .005. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 62/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C 44, CABIN WINDOW FORGING. CORROSION FOUND ON FORGING AT BS 560 TO BS 580 LT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .008. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 63/2000.

Part: FORGING — CORRODED (CABIN WINDOW) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 560 - 580 LT SIDE CORRODED. FORGING REMOVED, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, CORR DEPTH .008. FORGING REFITTED IAW SRM 51-300-02, BLENDED OUT IAW QUERY NOTE 63/2000.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, WINDOW FORGING CORRODED BS 900 - 920 LT SIDE. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10 -01 & 56-20-01, DEPTH OF CORR .009. BLEND OUT LIMITS IAW QUERY NOTE 64/2000. FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING AT BS 940 - 960 LT SIDE CORRODED. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, DEPTH OF CORR .010 BLEND OUTS IAW QUERY NOTE 64/20 00, FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 940 - 960 RT SIDE. BOEING TELEX TEL-DUB-00-00765H REFERS. FORGING REMOVED IAW SRM 51-30-01, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, CORR DEPTH .008. FORGING REWORKED IAW QUERY NOTE 20/20 00, BLEND OUT CORR, O/SIZE HOLES NDT INSP FORGING REFIT IAW 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, FORGING WINDOW AT BS 960 - 980 RT SIDE FOUND CORRODED. REMOVED WINDOW FORGING IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01 & 56-20-01, DEPTH OF CORR .007. BLEND OUTS AND REWORK IAW QUERY NOTE 64/2000 HOLES O/SIZED AND NDT INSP. FORGING REFITTED IAW SRM 51-30-02 BOEING TELEX TEL-DUB-00-00765H.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING BS 980 - 1000 RT CORRODED. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW QUERY NOTE 50/2000, DEPTH OF CORR .008. RE WORKED HOLES O/SIZED AND NDT INSPECTED FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1160 - 1180 RT SIDE. FORGING REMOVED IAW SRM 53-30-02, CORROSION REMOVED IAW SRM 51-10 -01 & 56-20-01, REWORK OF HOLES O/SIZED AND NDT INSPECTED IAW QUERY NOTE 64/2000, FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1394 TO BS 1416 LT. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED IAW SRM 51-10-01, DEPTH OF CORROSION REMOVED .009 IAW SRM 56-20-01 FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY 1/64 AND PERFORM OPEN HOLE HFEC TO ENSURE HOLES ARE CRACK FREE. ALSO MAINTAIN MIN EDGE MARGIN OF 1.5D

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1438 TO BS 1460 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH OF CORROSION REMOVED .008 IAW SRM 56-20-01 FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY 1/64 AND PERFORM HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5D AND REFIT FORGING.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1460 TO BS 1480 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. CORROSION REMOVED .010 IAW SRM 56-20-01. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 41/2000 WHICH IS TO OVERSIZE HOLES BY 1/64 AND PERFORM AN OPEN HOLE HFEC FOR CRACKS ON HOLES COMMON TO FORGING AND SKIN. MAINTAIN MIN EDGE MARGIN OF 1.5D.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1500 TO BS 1520 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH OF CORROSION REMOVED .010 IAW SRM 56-20-01. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 65-2000 WHICH IS TO OVERSIZE HOLES BY 1/64 ON HOLES WHICH ARE COMMON TO FORGING AND SKIN. PERFORM AN OPEN HOLE HFEC FOR CRACKS AND ENSURE A MIN EDGE MARGIN 1.5D.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1540 TO BS 1560 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH OF CORROSION REMOVED IS .009 IAW SRM 56-20-01. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 36/2000 WHICH IS TO OVERSIZE HOLES BY 1/64 AND PERFORM OPEN HOLE HFEC, ENSURE MIN EDGE MARG IN OF 1.5D ON ALL HOLES EXCEPT HOLES A, B AND C AS SPECIFIED.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1560 TO BS 1580 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH CORROSION REMOVED IS .009 IAW SRM 56-20-01. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 66/2000 WHICH IS TO OVERSIZE HOLES BY 1/64 AND PERFORM OPEN HOLE HFEC FOR CRACKS. MIN EDGE MARGIN IS 1.5D REPAIR/ALTERATION AUTHORIZATION EFN 747-53-1130.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1020 - 1040 RT SIDE. FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED AND WINDOW RE WORKED HOLES O/SIZED AND NDT INSPECTED DEPTH OF CORR .008, REWORK IAW QUERY NOTE 64/2000 & 51-10-01 & 56-20-01.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1620 TO BS 1640 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. DEPTH OF CORROSION REMOVED IS .010 IAW SRM 56-20-01. FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY .0156 AND PERFORM OPEN HOLE HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5D AND REFIT FORGING.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1416 TO BS 1438 LT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10 -01. DEPTH OF CORROSION REMOVED IS .010 IAW SRM 56-20-01 FORGING REFITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY .0156 AND PERFORM AN OPEN HOLE HFEC TO ENSURE HOLES ARE CRACK FREE AND MAINTAIN MIN EDGE MARGIN OF 1.5D.

Part: FORGING — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING IS CORRODED AT BS 1460 TO BS 1480 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01. FORGING CRACKED. NEW FORGING FITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000 WHICH IS TO OVERSIZE HOLES BY .0156 AND PERFORM AN OPEN HOLE HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5D.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1540 TO BS 1560 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .008. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION OVERSIZE HOLES BY .0156 AND PERFORM OPEN HOLE HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1600 TO BS 1620 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION, OVERSIZE HOLES AND HFEC FOR CRACKS. MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1820 TO BS 1840 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .005. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 2000 TO BS 2020 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-02 AND 56-20-01. CORROSION REMOVED = .008. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 66/2000. BLENDOUT ALL CORROSION AND OVERSIZE HOLES PERFORM HFEC ON HOLES FOR CRACKS MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1980 TO BS 2000 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED PER SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. PERFORM HFEC ON HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 2060 TO BS 2080 LT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .010. FORGING RE-INSTALLED PER SRM 51-30-02 AND QUERY NOTE 66/2000. BLEND OUT CORROSION AND OVER SIZE HOLES. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AB BS 1460 TO BS 1480 RT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED AND FORGING FOUND CRACKED. NEW FORGING FITTED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1480 TO BS 1500 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .009. FORGING RE-INSTALLED IAW SRM 51-30-02 AND QUERY NOTE 65/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES. HFEC HOLES FOR CRACKS AND MAINTAIN MIN EDGE MARGIN OF 1.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 1500 TO BS 1520 RT. FORGING REMOVED IAW SRM 51-30-02 AND CORROSION REMOVED IAW SRM 51-10-01 AND 56-20-01. CORROSION REMOVED = .008. FORGING RE-INSTALLED PER SRM 51-30-02 AND QUERY NOTE 46/2000. BLEND OUT ALL CORROSION AND OVERSIZE HOLES BY .0156. MAINTAIN MIN EDGE MARGIN OF 1.5. EXCEPT FOR 3 HOLE LOCATION WHICH HAVE AN EM OF 0.48 TO 0.5.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORROSION FOUND BS 1020 - 1040 LT. FORGING REMOVED IAW SRM 51-30-02. CORR REMOVED IAW SRM 51-10-01 & 5 6-20-01. DEPTH OF CORR .008. BLEND OUTS AND HOLE REWWORK O/SIZE AND NDT INSP IAW QUERY NOTE 64/2000. FORGING REFITTED IAW SRM 51-30-02.

Part: FORGING — CORRODED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CABIN WINDOW FORGING CORRODED AT BS 880 - 900 RT. FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW 51-10-01 & 56-20-01 CORR DEPTH .008. BLEND OUTS AND HOLES OVERSIZED, NDT INSP ACCOMP IAW QUERY NOTE 64/2000. FORGING REFITTED IAW SRM 51-30- 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, MAIN DECK FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR BS 620 STR 24 LT. REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 35, DOUBLER REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, PLEASE REMOVE FASTENERS AS REQUIRED FOR NDT INSPECTION PER EO 5310- 12070 APPENDIX C AND D. DURING INSPECTION OF 1265 FRAME, BOTH FRAMES WERE CRACKED. FASTENERS REMOVED AS PER EO 5310-12070 APPENDIX C AND D. REPAIRS CARRIED OUT IAW EO B747-5310-12070 AND EO B747-5310-13330-A. FASTENERS REMOVED REPLACED DURING REPAIR. FRAME WEBS AND INNER CHORDS WERE REPAIRED PER DRAWING 144U0053 WITH EXCEPTION FREIGHTER TYPE INTERCOSTAL WAS INSTALLED FAA 8110 ISSUED.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, PLEASE CARRY OUT REPAIRS TO OVERWING LONGERON FITTINGS LT AND RT IAW EO B747-5310-11087-A. REPAIRS CARRIED OUT PER UPS EO B747-5310-11087-A WITH DESCREPANCIES AS NOTED IN QUERY NOTE 70/2000. SPLICING IN NEW SEGMENT OF LONGERON FAA 8110-3 ISSUED.

Part: ANGLE — DAMAGED (NR 2 PYLON) · airframe 95,273 hrs · 22,812 cycles

INSPECTION TYPE:C, CARRY OUT PERMANENT REPAIR TO NR 2 PYLON AS PER EO B747-5430-12183. REPAIR CARRIED OUT IAW QUERY NOTE 15/2000. TRIM OUT RIB FLANGE AND SKIN ASSY, INST FREEZE PLUGS AND FABRICATE NEW REPAIR ANGLE AND FILLERS FROM 7075T6.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS AT THE UPPER DECK CREW SERVICE DOOR INOP AFTER A FEW SECONDS. REMOVED AND REPLACED BATTERY PACK AT UPPER SERVICE DOOR PER MM 33-51-04, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS AT THE UPPER DECK CREW SERVICE DOOR INOP AFTER A FEW SECONDS. REMOVED AND REPLACED BATTERY PACK AT UPPER DECK SERVICE DOOR PER MM 33-51-04.

Part: ACM — LEAKING (NR 1 PACK)

OIL FUMES IN FLIGHT DECK, ON TAXI, NR 2 AIR CONDITIONING PACK PRODUCED BURNING ODOR NR 1 ACM LEAKING OIL. DEFERRED NR 1 ACM INOPERATIVE PER MEL.

Part: SKIN — CRACKED (TE FLAP)

INSPECTION TYPE:N/A, LEFT O/B TRAILING EDGE FLAP WHEEL END HAD 10 INCH CRACK. REMOVED AND REPLACED AFT O/B TRAILING EDGE FLAP PER 747 MM 27-51-06, OPS CHECK GOOD.

Part: SMOKE DETECTOR — INOP (CARGO COMPT)

INTERMITTENT ZONE 5 MAIN CARGO DECK FIRE LIGHT ILLUMINATED DURING CLIMB-OUT OF PHL. DEFERRED PER MEL 26-11. REMOVED AND REPLACED B SMOKE DETECTOR AND A8 SMOKE DETECTOR CARD. OP'S CHECK GOOD PER MM 26-10-00. POSITIONS 14 TO 15A VOID. REFERENCE LOG PAGE 148290 ITEM 3 FOR OVERWEIGHT LANDING WHICH OCCURED DURING LANDING.

Part: CONNECTOR — CONTAMINATED (NR 4 ENGINE)

APPROX 2 HRS INTO FLIGHT, NR 4 START VALVE LIGHT CAME ON THE WENT OUT CAME ON AGAIN, THEN SHUT DOWN NR 4 ENGINE PER AOM. LIGHT WENT OUT. MX FOUND CONNECTORS AT START VALVE OIL SOAKED AND SHORTED. CLEANED CONNECTORS. SYSTEM OPS CHECK NORMAL. THIS CLEARS M180958.

Part: MARKER BEACON — INOP (COCKPIT)

INSPECTION TYPE:N/A, MARKER BEACON INOP.

Part: SKIN — CORRODED (LAV DUMP)

INSPECTION TYPE:N/A, FUSELAGE SKIN LT SIDE OF LAV DUMP HAS CORROSION AND POPPED HI-LOK RIVET HEADS. REMOVED CORROSION AND ACCOMPLISHED EO B747 5330 11468 A.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-N/A, SIXTH LT WING L/E RIB FROM OTBD END UPPER FLANGE IS CRACKED. REMOVED AND REPLACED L/E RIB IAW SRM 51-30-2, 51-10-6, 51-10-1.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE N/A, AFTER REMOVAL OF LT OTBD LEADING EDGE UPPER PANEL, FOUND 7TH L/E RIB FROM OTBD END, UPPER CHORD CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-30-2, 51-10-6, 51-10-1.

Part: SKIN — CORRODED (WS 1481)

INSPECTION TYPE-N/A, AFTER REMOVAL OF LT OUTBOARD L/E UPPER PANEL FOUND HEAVY CORROSSION ON WING SKIN UPPER FWD FLANGE AT STA WS 1481. REMOVED CORROSION AT WS 1481 IAW SRM 57-10-01 AND REPAIRED IAW DH SK691-165.

Part: BATTERY PACK — DISCHARGED (CABIN)

UPPER DECK ESCAPE SLIDE EMERGENCY LIGHTS INOP. REPLACED UPPER DECK ESCAPE SLIDE EMERGENCY LIGHTS BATTERY PACK.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

LT MAIN DECK CARGO SMOKE DETECT WARNING ON. VISUAL INSPECTED MAIN CARGO DECK AND NOTICED PRESENCE OF FUMES NEAR 14R PALLET POSITION. DECLARED EMERGENCY AND DIVERTED TO COLD BAY (CDB) EMERGENCY CHECK LIST PERFORMED IAW AOM. INSPECTED AREA AROUND SUSPECTED FUMES FOR DAMAGE OR REMAINING FUMES. NO DEFECTS NOTED. SUSPECT SMOKE DETECTOR 4B ERRONEOUS. DEFERRED 4B SMOKE DETECTOR PER MEL.

Part: ENGINE — FAILED (NR 2)

INSPECTION TYPE-N/A, NR 2 ENG FLAMED OUT. FOUND METAL IN LOWER RT BLEED SCREEN. REPLACED ENGINE.

Part: SKIN — CORROSION (RT WING)

INSPECTION TYPE:C RH WING LE STRUCTURE; LOWER SIDE OF UPPER INSPAR WING SKIN CORRODED FWD OF FRONT SPAR ILES 842 REMOVED FASTENERS FROM UPPER SKIN AND UPPER PANEL ACC SRM 51-30-02. REMOVED CORROSION FROM SKIN AND UPPER CHORD ACC SRM 51-10-01.OUT OF LIMITSACC SRM 57-30-01.REPAIRED UPPER SKIN AND UPPER CHORD ACC KLM DFX 97-139 APPOVED PER UPS EFN 747-57-0380.INSTALLED FASTENERS FROM UPPER SKIN/UPPER PANEL ACC SRM 51-30-02

Part: BEAM — CORROSION (CARGO DOOR)

INSPECTION TYPE:C FWD CARGO DOOR; FOUND CORROSION ON LOWER BEAM AROUND ANCHOR NUTS HOLES FROM INSIDE DOOR LINING. REWORKED AREA ACC SRM 51-10-01, OUT OF LIMITS ACC SRM 52-00-02 FIG 1. REPAIRED BEAM ACC KLM-DFX 97-147 / EFN 747-52-0062.

Part: SKIN — SCRATCHED (CARGO DOOR)

INSPECTION TYPE:C, FWD CARGO DOOR; FOUND SEVERAL SCRATCHES AT LOWER CORNER SKIN STA 567. REWORKED AREA ACC SRM 51-10-01, OUT OF LIMITS ACC SRM 52-00-02 FIG 1. REPAIRED DOOR ACC TELEX KLM-DFX 97-144 EFN 747-52-0063.

Part: SKIN — SCRATCHED (CARGO DOOR)

INSPECTION TYPE:C, FWD CARGO DOOR; FOUND SCRATCHES ON LOWER SIDE DOOR STA 608. REWORKED AREA ACC SRM 51-10-01, OUT OF LIMITS ACC SRM 52-00-02 FIG 1. REPAIRED DOOR ACC TELEX KLM-AMS 97-144 AND EFN 747-52-0063.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, UPPER DECK EMERGENCY LIGHT FOR DOOR INOP. RELAMPED, OPS CHKS OK.

Part: LOCKPIN — MISALIGNED (CREW HATCH)

INSPECTION TYPE-N/A, AIR TURNBACK AT 21,000 FEET, LOUD POP AND HISS, AIR NOISE. CABIN CLIMBING AT 400 FPM MAX CABIN ALTITUDE REACHED 7,000 FEET. CREW HATCH UNSEATED BUT REMAINED IN POSITION, REF MM 52-21-00. FOUND OVERHEAD LATCH AFT LOCKPIN MISALIGNED AND DOOR JAMMED. OPENED DOOR, CHECKED PINS AND FRAME FOR DAMAGE, NONE NOTED. CYCLED CLOSED SEVERAL TIMES, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT EMERGENCY LIGHT ABOVE STAIRWAY INOP. REMOVED AND REPLACED LIGHT, OPS CHECKS GOOD (P/N 60B50037-37) (S/N 19567) OFF, (P/N 60B50037-37) (S/N 33648) ON.

Part: ENGINE — FAILED (NR 4)

INSPECTION TYPE N/A, NR FOUR ENG FAILED AFTER LIFTOFF, NO FIRE LIGHT. FIRE SHOT OUT OF INTAKE WITH MODERATE THUMP, COMP STALL. MAX T/O EGT 907 DEGREES, ENGINE SHUTDOWN CHECKLIST COMPLETED. REMOVED AND REPLACED NR 4 ENGINE PER TASK CARD AND MAINT MANUAL. ALL LEAK CKS AND OPS CKS GOOD POWER ASSURANCE RUN GOOD. (P/N JT9D-7AH) (S/N 663023) ON, (P/N JT9D-7AH) (S/N 662203) OFF.

Part: ESCAPE SLIDE — IMPROPERLY INST (FLIGHT DECK)

INSPECTION TYPE, ESCAPE SLIDE INOP. CABLES DISCONNECTED ALSO SLIDE IS NOT ON ITS MOUNT, FWD SIDE. REINSTALLED ESCAPE SLIDE PER MM 25-68-02.

Part: LIGHT — INOPERATIVE (AFT FLGHT DECK)

INSPECTION TYPE N/A, ONE OF THE OVERHEAD LIGHTS ON THE AFT FLIGHT DECK IS BURNED OUT, WILL NOT ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH ON. REMOVED AND REPLACED AFT FLT DECK OVERHEAD EMERGENCY LIGHT PACK, CHECKS OK PER MM 33-51-00 (P/N 5136B37), (S/N 10006-372) ON, OFF (S/N 18363) OFF.

Part: RIB — CORRODED (LT HORIZ STAB)

INSPECTION TYPE: MODERATE CORROSION ON LOWER ANGLE ON RIB AT STABILIZER, BL 372 LEFT. CORRODED ANGLE REMOVED. REPAIR CARRIED OUT PER QUERY NOTE 3/3/96 AND SRM 51-40-04, FIGURE 2.

Part: SPAR — CRACKED (LT WING)

DURING PYLON MODIFICATION ON THIS A/C, AN INSPECTION OF THE LEFT WING FRONT SPAR REVEALED CRACKS AT FOUR LOCATIONS AT WING STATION 669.5. REF ATTACHED QUERY NOTE S/N 16/95 FOR DETAILS.

Part: FITTINGS — ELONGATED HOLES (LT AILERON)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, LT WING O/B AILERON, 4 ATTACHMENT FITTINGS HOLES ARE ELONGATED AT WS 1308, 1423, 1485 AND 1548. REPLACED HINGE FITTINGS IAW SRM 51-30-02.

Part: SHEAR TIES — CRACKED (BS 1980)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND 3 CRACKED SHEAR TIES AT BS 1980 BETWEEN STR 46 TO 50 LBL. REPAIRED SHEAR TIES IAW SRM 53-10-4 FIG 41.

Part: FRAME — CORROSION (BS 2000)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD OF FRAME AT BS 2000 RBL 45. REMOVED CORROSION FROM UPPER CHORD OF FRAME ACC SRM 51-10-01, WITHIN LIMITS OF SRM 53-10-09.

Part: ANGLE — CRACKED (BS 1960)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACKS IN REINFORCEMENT ANGLE IN TOP OF FRAME AT BS 1960 LBL 53. REPLACED REINFORCEMENT ANGLE AT BS 1960 LBL 53 ACC SRM 51-20-01 AND 51-30-02.

Part: SHEAR TIES — CRACKED (BS 2240)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIES ARE CRACKED AT BS 2240 BETWEEN STR 47 AND 48 RBL AND BETWEEN STR 47 AND 48 LBL. REPAIRED SHEAR TIES AT BS 2240 ACC SRM 53-10-04.

Part: CHORD — CORRODED (WS 1520)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING L/E STRIP OF RABBET AREA IS BULGED AT WS 1520, CORROSION FOUND ON UPPER CHORD. REWORKED CORROSION ON UPPER CHORD AND REPAIRED UPPER CHORD ACC TO KLM DFX 96-034 APPROVEL PER UPS EFN 747-57-0307.

Part: SHEAR TIE — CORRODED (BS 2180)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CORRODED SHEAR TIE PROFILE ON AFT SIDE OF SHEAR TIE, AT BS 2180 LBL BETWEEN STR 42 AND 43. REPLACED SHEAR TIE PROFILE ACC SRM 51-20-01 AND 51-30-02.

Part: FITTING — ELONGATED (LT AILERON)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED LT WING O/B AILERON ATTACH FITTINGS HAVE ELONGATED HOLES AT W/S 1308, 1423, 1485, AND 1548. REPLACED FITTINGS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 2080)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED 3 CRACKED SHEAR TIES IN BULK CARGO COMP. AT BS 2080 BETWEEN STR 50 TO 48 LBL AND RBL BETWEEN STR 49-50. REPAIRED PER SRM 53-10-04, FIG. 41.

Part: SHEAR TIE — CRACKED (BS 2140)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED CRACKED SHEAR TIE AT B.S. 2140, STR. 49-50 LT. REPAIRED CRACK PER SRM 53-10-04,, FIG. 1.

Part: SHEAR TIE — CRACKED (BS 2100)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 3 SHEAR TIES CRACKED AT BS 2100 BETWEEN STR 4 TO 50 LBL. REPAIRED PER SRM 53-10-04 FIG 41.

Part: STRINGER — CORROSION (BS 2150-2170)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FOUND IN BULK CARGO COMP AT BS 2156 STR 46 RBL CORROSION IN STRINGER. REPLACED STR BETWEEN BS 2150 AND 2170 IAW SRM 53-10-03 FIG 1 AND SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 2060)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 3 SHEAR TIES ARE CRACKED AT BS 2060 BETWEEN STR 48 TO 51 LBL. REPAIRED PER SRM 53-10-04 FIG 41.

Part: RIB — CRACKED (LE WING)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS IN UPPER CHORD OF L/E RIB AT O/B LEADING EDGE STATION 1534.95, 1462.85, 14653.35, 1309.15, 1237.05, 1195.55 AND 1483.95. REPAIRED PER SRM 57-20-03 FIG 1.

Part: SUPPORT TUBE — PUNCTURED (ILES 788)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HOLE IN SUPPORT TUBE AT I/B LEADING EDGE STATION 788. REPLACED SUPPORT IAW SRM 51-30-05 AND MM 20-10-13.

Part: ATTACH BEAM — CRACKED (NR 3)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND AFT PDU ATTACHMENT BEAM NR 3 CRACKED. REPAIRED PER SRM 51-40-03.

Part: RIB — CRACKED (LE WING)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER CHORD FLANGE L/E RIB AT I/B LEADING EDGE STATION 802.5, 852.45 AND 886.5. REPAIRED IAW SRM 57-20-03 FIG 1.

Part: FRAME WEB — CRACKED (BS 1840)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED CRACKED FRAME WEB UNDER UPPER CHORD AT B.S. 1840 LBL 6. REPAIRED WEB PER SRM 51-40-02.

Part: FRAME FITTING — CORRODED (BS 1960)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FRAME FITTING AT BS 1960 RBL 54. REPLACED FITTING IAW SRM 51-20-01 AND 51-30-02.

Part: SKIN — CORRODED (WS 1160)

WHILE IN AMS FOR C-CHECK, DURING RIVET INSTALLATION FOUND RT WING CORROSION ON LOWER SIDE OF UPPER WING SKIN O/B OF PYLON 4 AT WS 1160. REPAIRED IAW KLM DFX 96-040 ISSUE NR 3 APPROVED PER UPS 747-57-0309.

Part: FRAME — CORRODED (BS 1840)

WHILE IN AMS FOR C-CHECK, FOUND CRACK IN FRAME UPPER CHORD BS 1840 RT BL 32 NEAR EXISTING SPLICE. REMOVED DAMAGE UPPER CHORD AND REPAIRED CHORD ACC TO KLM DFX 96-035, ISSUE NR 4, APPROVED PER UPS EFN 747-53-0751.

Part: FRAME — CRACKED (BS 1900)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK IN FRAME UPPER FLANGE AT BS 1900, LBL 60 TO 63. STOP DRILLED CRACK AND REPAIRED FRAME UPPER FLANGE ACC TO SRM 51-40-03, FIG 1.

Part: SHEAR TIE — CRACKED (BS 1900)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACKS IN FRAME SHEAR TIES AT BS 1900 BETWEEN S-46/45 LT AND S-45/44 LT. REPAIRED SHEAR TIES IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1880)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, SHEAR TIES CRACKED AT FRAME BS 1880 BETWEEN S-48/47 RT S-51/50 RT AND S-45/44 LT. REPAIRED SHEAR TIES IAW SRM 53-10-04 FIG 3.

Part: CARGO TRACK — CRACKED (BS 1910)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACK IN CARGO TRACK LOWER SIDE UNDER END-STOP FITTING, BS 1910 RBL 45. STOP DRILLED CRACK AND REPAIRED TRACK IAW SRM 53-10-05 FIG 2.

Part: INTERCOSTAL — CRACKED (BS 1900-1915)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN INTERCOSTAL UNDER CARGO TRACK AT LBL 25 BETWEEN BS 1900/1915. STOP DRILLED IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (BS 2180)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE CRACKED AT BS 2180 LBL BETWEEN 43 AND 44. REPLACED SHEAR TIE AT BS 2180 LBL ACC SRM 51-20-01 AND 51-30-02.

Part: WEB — DENTED (BS 1840-1860)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, DENT IN UPPER WEB OF TORQUE BOX BS 1840 TO 1860 RBL 20. REPLACED UPPER WEB AND BLIND FASTENERS FOR SOLID FASTENERS PER SRM 51-30-02.

Part: FASTENERS — LOOSE (BS 1840-1860)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, LOOSE FASTENERS IN UPPER WEB OF TORQUE BOX BS 1840 TO 1860 BETWEEN RBL 25 TO 45. REPLACED UPPER WEB AND REPLACED BLIND FASTENERS FOR SOLID FASTENERS PER SRM 51-30-02.

Part: STRINGER — SCRATCHED (FS 800)

WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, FOUND SCRATCHES ON O/B TOP FLANGE STR 45 LT STA 800. REPLACED STR 45 FROM STA 790 TO 810 IAW SRM 53-10-03 FIG 1.

Part: FRAME WEB — CRACKED (BS 1760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME WEB UNDER UPPER CHORD AT BS 1760 LBL 25. REMOVED DAMAGE AND REPAIRED WEB IAW SRM 51-40-02.

Part: BRACKET — CRACKED (BS 1840)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN INTERCOSTAL BRACKET UNDER FRAME UPPER CHORD AT BS 1840 LBL 5. REPLACED BRACKET PER SRM 51-30-02.

Part: SPLICE — CRACKED (BS 1355)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SPLICE FITTING INSIDE LEFT BLG WW ON O/W LONGERON NEARLY CRACKED IN TWO, SUSPECT CORROSION CRACK. REPLACED SPLICE ACC SRM 53-10-02.

Part: STRINGER — CORRODED (BS 1965)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CORRODED, STRINGER END AT BS 1965 S-49 LT UNDER STRINGER SPLICE. REMOVED CORROSION FROM STRINGER END ACC SRM 51-10-01, OUT OF LIMITS PER SRM 53-10-01. REPAIRED STRINGER PER SRM 53-10-03 FIG 1.

Part: LONGERON — CRACKED (BS 1480)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, RT BLG WW OVERWING LONGERON CRACKED FROM BS 1480. REPAIRED IAW SRM 53-10-01 FIG 1 AND AS PER BOEING TELEX UPS- AMS -96-0038RE.

Part: FRAME — CRACKED (BS 1960)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CRACK IN WEB OF FRAME AROUND BLANKET HOLE AT BS 1960, LBL 4. REPAIRED CRACK IN WEB AT BS 1960 ACC TO SRM 51-40-02.

Part: HINGES — CORROSION (BS 820/840)

WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, CORROSION ON CEC DR. HINGE FITTINGS STA 820/840, LBL 15. REPLACED FITTINGS PER SRM 51-40-04.

Part: SHEAR TIE — CRACKED (BS 1840)

WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND CRACK IN SHEAR-TIE AT B.S. 1840 BETWEEN STR 48-47 LT. REPAIRED PER SRM 53-10-04, FIG. 3.

Part: STIFFENERS — CRACKED (BS 1780/1740)

WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND CRACKS IN STIFFENERS OF FRAME WEB UPPER CHORD AT B.S 1780 RBL AND LBL 14, AND B.S. 1740, RBL AND LBL 14. REPLACED STIFFENERS PER SRM 53-30-02.

Part: STRINGER — CORROSION (BS 980)

WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, CORROSION IN STR 42 RT, STA 980. OUT OF LIMITS, REPLACED STR 42 I.A.W. SRM 53-10-03, FIG. 1.

Part: SHEAR TIE — CRACKED (BS 1800)

WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, FOUND CRACK IN SHEAR TIE AT B-STA 1800 BETWEEN STR 48 TO 47 LT. REPAIRED AS REQUIRED PER SRM 53-10-04 FIG 3.

Part: STIFFENER — CRACKED (BS 1800)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER STIFFENER AND DEFORMATION ON LOWER STIFFENER OF FRAME AT BS 1800 LBL 14, AFT CARGO COMPARTMENT. REPLACED STIFFENERS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 1820)

WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, CRACKED SHEAR TIE STA 1820 BETWEEN STR 50 TO 49 RT. REPAIRED AS REQUIRED PER SRM 53-10-04 FIG 3.

Part: BULKHEAD — CRACKED (BS 2160)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED BULK CARGO COMP. T-CHORD ON BULKHEAD FOR CARGO FLOOR STRUCTURE IS CORRODED AND CRACKED ON HORIZ. FLANGE AT STA 2160, RBL 2, 23, AND 29. REPLACED UPPER CHORD PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 1700)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACKS IN SHEAR TIES AT BS 1700 BETWEEN S-51 LT/RT, S-48/47 AND S-47/46 RT. REPAIRED SHEAR TIES AT BS 1700 IAW SRM 53-10-04 FIG 3.

Part: STRINGER — CORROSION (BS 1740-1780)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FOUND CRACK DUE TO CORROSION ON STR FLANGE AT BS 1757, S-43 RT. REPLACED STR FROM BS 1740 TO 1780 IAW SRM 51-30-02.

Part: SKIN — DELAMINATED (BS 1700-1720)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND DELAMINATION DUE TO CORROSION ON SKIN LAP SPLICE UNDER S-46 RT BETWEEN BS 1700/1720. REMOVED EXISTING REPAIR PER SRM 51-30-02, REMOVED DELAMINATED PART OF OVERLAPPED SKIN BY EXTENDING CUTOUT TO BS 1695 AND REPAIRED LAP SPLICE IAW SRM 53-30-03 FIG 18.

Part: SHEAR TIE — CRACKED (BS 2040)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT HAS 2 SHEAR TIES CRACKED AT BS 2040 BETWEEN STR 47 TO 48 AND STR 49 AND 50 LT. REPAIRED SHEAR TIE AT BS 2040 LT ACC TO SRM 53-10-4 FIG 41.

Part: SKIN — CORRODED (WS 1280)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED RT WING L/E LOWER SKIN AND LOWER CHORD WS 1280 FOUND CORRODED. REPAIRED CHORD AND SKIN ACC KLM DFX 96-027R1 ISSUE NR 3 REPAIR APPROVED PER UPS EFN 747-57-0308.

Part: BLKHD WEB — CRACKED (BS 2160)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BS 2160 RBL 30. REPAIRED AS PER SRM 51-40-02.

Part: SHEAR TIE — CRACKED (BS 1760)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON SHEAR TIE AT BS 1760 BETWEEN S-51/50 LT. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: FRAME — CRACKED (BS 1780)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK IN OWER FRAME WEB IN BLANKET HOLE AT BS 1780, LBL 40. REMOVED DAMAGED SECTION FROM FRAME WEB AND REPAIRED WEB ACC TO SRM 51-40-02 FIG 1.

Part: SHEAR TIES — CRACKED (BS 1960)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND 4 SHEAR TIES CRACKED AT BS 1960 BETWEEN S-46 50 LT. REPAIRED CRACKED SHEAR TIES AT BS 1960 ACC TO SRM 53-10-04, FIG 41.

Part: SHEAR TIE — CRACKED (BS 1940)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT SHEAR TIE CRACKED AT BS 1940 BETWEEN STR 46 TO 47 LT. REPAIRED SHEAR TIE AT BS 1640 BETWEEN STR 46 TO 47 LT ACC TO SRM 53-10-04 FIG 41.

Part: SHEAR TIE — CRACKED (BS 2120)

WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND 2 CRACKED SHEAR TIES AT BS 2120 BETWEEN STR 45 TO 50 LBL AND BETWEEN STRINGER 49 TO 50 RBL. REPAIRED PER SRM 53-10-4 FIG 41.

Part: SHEAR TIE — CRACKED (BS 1780)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON SHEAR TIES AT BS 1780 BETWEEN S-50/49 LT AND BETWEEN S-43 RT AND DOOR SILL BEAM. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: CARGO TRACK — OUT OF LIMITS (BS 1750-1770)

WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND EXISTING BLEND-OUTS IN CARGO TRACK OUT OF LIMITS PER SRM 51-10-01 AT LBL 25 BETWEEN B.S. 1750 AND 1770. REPAIRED PER SRM 53-10-05, FIG. 5.

Part: BLKHD WEB — CRACKED (BS 145)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BSTA 2160 LBL 35. REPLACED WEB BETWEEN RBL 8 TO LBL 58, ALL TO SRM 51-40-02.

Part: FRAME WEB — DENTED (BS 1760)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DENT IN FRAME WEB UNDER UPPER CHORD AT BS 1760 LBL 52, DAMAGE OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02.

Part: FRAME WEB — CRACKED (BS 1600)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB UNDER FRAME UPPER CHORD AT BS 1600 RBL 40. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02 FIG 1.

Part: STRINGER — CRACKED (BS 1740)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED THEY FOUND CORROSION ON STRINGER-END UNDER STRINGER SPLICE AT BS 1740 S45R. CORROSION REMOVED PER SRM 51-10-01. REPLACED STRINGER PER SRM 51-30-02.

Part: FRAME WEB — CRACKED (BS 1700)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB BLANKET HOLE AT BS 1700 S-46 LT. STOP DRILLED CRACK, REPAIRED WEB IAW SRM 53-10-04 FIG 41.

Part: FRAME WEB — CRACKED (BS 1620)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB AT BS 1620 NEAR S-49/48 RT. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02 FIG 1.

Part: FRAME — CRACKED (BS 1960)

WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CRACKED WEB AT BS 1960, RBL 2 AROUND BLANKET ATTACHMENT HOLE. REPAIRED FRAME WEB AT BS 1960 RBL 2 AROUND BLANKET ATTACHMENT PER SRM 51-40-02.

Part: SKIN — CORRODED (BS 1720)

WHILE IN FOR C-CHECK IN AMS, MAINTENANCE REPORTED, CORROSION AT B.S. 1720 LT STR 34 AT LAP SPLICE. OUT OF LIMITS I.A.W. 53-30-01, REPAIRED PER SRM 53-30-03, FIG. 17.

Part: FRAME — CRACKED (BS 1860)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK AND CORROSION ON FRAME AT BS 1860, JUST UNDER SIDE GUIDE. REMOVED DAMAGED SECTION FROM FRAME UPPER CHORD AND REPAIRED FRAME ACC TO SRM 51-40-03 FIG 1.

Part: STRINGER — CRACKED (BS 460-480)

WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED FWD. CARGO COMP. STR. 39 RT BETWEEN STA 460-480, STRINGER IS CRACKED. REPAIRED PER SRM 53-10-03, FIG. 3.

Part: BATTERY — DISCHARGED (UPPER DECK)

WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK DOOR EMERGENCY LIGHT INOP. DURING TEST, ALL EXIT LIGHT CAME ON WITH EXCEPTION OF TWO WHITE LIGHTS AT UPPER DECK DOOR SILL WHICH CAME ON, THEN WENT OUT. UPPER DOOR RENDERED INOP, DEFERRED PER MEL 33-13. WHILE ON GROUND, MAINTENANCE FOUND WITH CHARGED BATTERIES OPS CK GOOD. THIS CLEARS DMI NR M99481 PLACARD REMOVED.

Part: EEL PANEL — INOP (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY LIGHT CONTROL PANEL SHOWS UNARMED IN ARM POSITION. REPLACED EMER EXIT LIGHT CONTROL PANEL. OPS CK NORMAL.

Part: PDU — MALFUNCTION (NR 4 LE FLAP)

(SUPPLEMENTAL MRR) PILOT REPORTED THAT RIGHT NR 4 LEADING EDGE FLAP DID NOT EXTEND PNEUMATICALLY DURING APPROACH. EXTENDED FLAP ELECTRICALLY PER PROCEDURE. REPLACED NR 4 RT L/E FLAP PDU PER MM 27-81-03.

Part: WARNING IND — MALFUNCTION (NLG)

PILOT REPORTED ON GEAR EXTENTION WITH PRIMARY NOSE GEAR SENSOR INOP. THE GEAR INDICATES UNSAFE ON THE PILOT'S PANEL, AND THE LANDING GEAR WARNING HORN WILL NOT SILENCE UNTIL BREAKER IS PULLED. ALT SENSOR INDICATES SAFE IN F/E PANEL. INSTALLED REPAIR IAW MM 32-61-15, P/N 69B47531-3, P/N 69B47530-7.