N578UP

Part: SLIDE — UNWANTED DEPLOY (ZONE 800) · airframe 125,751 hrs · 21,182 cycles

RIGHT UPPER DECK ESCAPE DOOR/SLIDE DEPLOYED. REINSTALLED NEW RH UPPER DECK ESCAPE SLIDE IAW AMM 25-68-01 UP TO AND INCLUDING STEP G. 9. VERIFIED SAFETY PINS REMOVED AND PROPER SYSTEM PRESSURES IAW AMM 25-68-01 AND GMM 04-02. COMPLETED REMAINING STEPS IAW AMM 25-68-01.

Part: AILERON SYS — NO DISCREPANCY · airframe 124,195 hrs · 20,939 cycles

DURING CLIMB OUT AILERON FORCE WERE A LITTLE HEAVIER THAN NORMAL AND RIGHT AILERON REQUIRED SIGNIFICANTLY MORE FORCE THEN LEFT AILERON. PERFORM ROTATIONAL TORQUE CK OF BOTH YOKES IAW AMM 27-11-00-705-091. WITH IN LIMITS.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 123,263 hrs · 20,803 cycles

FAULT - FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP AT STA 620 AND STA 690 (REPLACE). I.A.W AMM 33-51-00-715-105 REV.113 CONTINUE TO SUPPLY POWER TO THE EMERGENCY LIGHT SYSTEM FOR SUFFICIENT TIME TO CHARGE THE BATTERY PACKS FOR THE POWER SUPPLIES, THE LIGHT COME ON , CONDITION CHECK NORMAL. REVIEWED TASK PER GMM-MTX 09.05.01.09.

Part: CIRCUIT CARD — FAULTED (ZONE 100) · airframe 122,357 hrs · 20,637 cycles

DURING PRE-DEPARTURE CHECK FOUND CARGO FIRE MD ZONE 6 LOOP-A FAIL NO CURENT FAULT FOUND. C/O FIRE TEST IAW AMM 26-11-00-715-001 REV 112. CHECKED SATIS. THIS CLOSES DMI. PLACARD REMOVED.

Part: STRUCTURE — BROKEN (ZONE 100) · airframe 121,125 hrs · 20,425 cycles

LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) INSTALLED 2(EA) BALL MAT PANELS IN LWR AFT PIT AT STATIONS 1840 AND 1900 PER AMM 25-53-15-400-801, PDU OPS CHECK GOOD PER AMM SUBTASK 25-53-01-864-035-004, REPLACED 2(EA) CENTER LINE GUIDES (RETRACTABLE) PER AMM 25-54-04-424-007

Part: STRUCTURE — BROKEN (ZONE 100) · airframe 121,112 hrs · 20,423 cycles

LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) OPEN

Part: WINDOW — DELAMINATED (ZONE 200) · airframe 120,929 hrs · 20,398 cycles

CAPT€™S #1 (FRONT) WINDSHIELD DELAMINATING ON TOP SECTION OF WINDOW COMPLETED WINDOW INSLALL WITH REF TO B747 MM 56-11-01. PERFORMED WIPER OPS CHECK WITH REF TO B747 MM 30-42-00.

Part: HMU — INOPERATIVE · airframe 120,790 hrs · 20,373 cycles

ON DECENT GOT #3 GEN ELECT FAIL. THEN ENG 3 FAILED APPEARED. N1 WAS AROUND 28%. ENGINE RETURNED TO NORMAL IDLE. ENG FAIL MESSAGE LASTED ABOUT 20 SECONDS NO OTHER PROBLEMS WITH ENG. CREW REPORTS CLEAR GOOD WEATHER DURING FAULT. REF FIM TASK 71-00 TASK A72 AND 71-00 FAULT TREE FIGURE 114. PERFORMED STEPS 1 AND 21. PERFORMED #3 ENGINE FUEL SUCTION FEED OPERATIONAL TEST PER AMM 28-22-00. OPERATIONAL TEST PASS, ENGINE PARAMETERS DID NOT FLUCTUATE. R&R #3 HMU PER AMM 73-21-14, UP UNTIL INSTALLATION ITEM #I (HMU TEST). PREFORMED TEST #12 OF POWER PLANT REF. TABLE, #3 EEC ACTUATOR TEST PASS. PERFORMED IDLE LEAK CHECK OF #3 ENGINE HMU PER AMM 71-00-00-705-152-J00. LEAK CHECK GOOD. C/W GMM 04-02

Part: LIGHT — FAULTED (CABIN) · airframe 120,587 hrs · 20,334 cycles

EMER LIGHTS EICAS. RESET EMERGENCY LIGHT SWITCH. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-715-001. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 119,494 hrs · 20,130 cycles

FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE) C/W I.A.W AMM 33-51-04-902-001-001 REV.109 REPLACED THE EMERGENCY LIGHT BATTERY (M5056) AT UPPER DECK,AND PERFORMED UPPER DECK EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORY. IPC VERIFIED AND SERVICEABLE TAG NO.151742.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 119,464 hrs · 20,125 cycles

SDR FILED OPEN. FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE)

Part: SNUBBER — OUT OF LIMITS (L4 DOOR) · airframe 119,464 hrs · 20,125 cycles

FOUND L4 ENTRY DOOR SNUBBER INDICATOR OUT OF LIMIT. (REPLACE) C/W 1. I.A.W AMM 52-11-10-004-001 REV. 109 AND AMM 52-11-10-404-005 REV. 109 REPLACE SNUBBER. 2. IPC VERIFIED AND SERVICEABLE PARTS TAG NO. 983747. 3. JOB COMPLETE AND CONDITION CHECK NORMAL.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 119,464 hrs · 20,125 cycles

*MAJOR REPAIR* FAULT - CRACK - FND TENSION TIE CHANNEL FWD SIDE CRACK AT STA 1120 L/H (REPAIR) ACCOMPLISH REINFORCING REPAIR I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2 (FIGURE 201). 1.ACCOMPLISH INSPECTION I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2, TABLE 202 AT 3,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION. REPEAT INSPECTIONS EVERY 3,000 FLIGHT CYCLES, THEREAFTER.<BR>2.REPEAT INSPECTION REQUERT DEFERRAL PER DMI - SRM 53-40-30-2R-2 TABLE 202.

Part: SKIN — DENTED (UNKNOWN) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK

Part: SKIN — DENTED (NR 1 FAN COWL) · airframe 119,464 hrs · 20,125 cycles

DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) 1.REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (DIAMETER:1",DEPTH:0.0175",32.5" FROM FORWARD EDGE,25.5" FROM LOWER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE CURED AT 200°F FOR 60 MINUTES.AND BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 20 IN/HG I.A.W.747-400SF SRM 54-21-01-2R-2 REV.58.

Part: SKIN — DENTED (NR 1 FAN COWL) · airframe 119,464 hrs · 20,125 cycles

DENT - SKIN SURFACE AT 10 O'CLOCK, NR 1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.7",DEPTH:0.012",30.4" FROM FORWARD EDGE,38" FROM UPPER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE CURED AT 200°F FOR 60 MINUTES.AND BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 20 IN/HG I.A.W.747-400SF SRM 54-21-01-2R-2 REV.58.

Part: SKIN — DENTED (UNKNOWN) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 10 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK

Part: STIFFENER — CRACKED (RT ELEVATOR) · airframe 119,464 hrs · 20,125 cycles

*** SUPPLEMENTAL SDR *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W AMM 27-31-01-404-015 REV.109 STEP 3.H(14) TO 3.H(23) ADJUST R/H INBOARD ELEVATOR AND OPERATION.

Part: PANEL — DEBONDED (LT WING LE) · airframe 119,464 hrs · 20,125 cycles

LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 119,477 hrs · 20,127 cycles

CRACKED SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) INSTALLED NEW PART I.A.W. SRM 51-40-02-0G REV.58 AND BOEING DWG NO:65B15168 SH.2 REV.G AND AIPC 27-81-02-01 REV.54. I.A.W AMM 27-81-02-404-010 REV.109 STEP 3.A TO 3.E.(5), INSTALL LH WING NO. 1E VC FLAP. REVIEWED

Part: SKIN — BROKEN (LT WING LE) · airframe 119,477 hrs · 20,127 cycles

BROKEN SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) C/W 1. OK TO INSTALL PANEL NO: 521EB. 2. I.A.W AMM 20-51-01-912-008 REV.109 INSTALL PANEL NO: 521EB. 3. CONDITION CHECK NORMAL. 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB COMPLETED AND CONDITION CHECK NORMAL AND PARTS INFO ATTACHED. REVIEW

Part: FAIRING — DAMAGED (NR 8) · airframe 119,464 hrs · 20,125 cycles

NR 8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.5",AT UPPER EDGE,5" FROM AFTER EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W.747-400SF SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV.58.

Part: FAIRING — UNKNOWN (UNKNOWN) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - NO.8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) OK TO WORK

Part: SKIN — DAMAGED (LT WING) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - BROKEN - SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) OK TO WORK

Part: STIFFENER — CRACKED (ELEVATOR) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W. AMM 27-31-01-004-001 REV.109 REMOVED R/H INBOARD ELEVATOR.

Part: SKIN — CRACKED (LT WING FLAP) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - CRACK - SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) I.A.W AMM 27-81-02-004-001 REV 109 REMOVE #1E V.C FLAP

Part: SKIN — DEBONDED (LT WING LE) · airframe 119,464 hrs · 20,125 cycles

*** SDR FILED OPEN *** FAULT - LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) OK TO WORK

Part: DOOR — BINDING (UNKNOWN) · airframe 119,386 hrs · 20,111 cycles

*** SUPPLEMENTAL SDR *** MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE REPLACED ROD END ASSY. ON LOWER HINGE GUIDE ARM REF AMM 52-11-01-401. OPS NORMAL AT THIS TIME. REF BARCODE T3F18E003MVRM FOR PARTS INFORMATION.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 119,337 hrs · 20,099 cycles

MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE, OPEN

Part: TRUNNION — CRACKED (MLG) · airframe 118,551 hrs · 19,949 cycles

RIGHT AFT TRUNNION, CRACKS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 118,551 hrs · 19,949 cycles

OPEN, RIGHT AFT TRUNNION, CRACKS

Part: CARGO TRACK — DAMAGED (CARGO) · airframe 118,535 hrs · 19,945 cycles

*** MAJOR REPAIR *** DURING CARGO LOADING OPERATIONS, FOUND FWD LWR CARGO DOUBLE PALLET LOCK ASSY. SECURING RAIL BROKEN, WL-118 ST-560, RH FWD BALL-MAT.***SM26/LMX13*** **WORK WITH 25TEY**457790 INSTALLED PDU CANNON PLUG REF AMM 25-53-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 117,636 hrs · 19,769 cycles

THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) OK TO WORK. OPEN

Part: LAMP — INOPERATIVE · airframe 117,716 hrs · 19,786 cycles

*** SUPPLEMENTAL SDR *** FAULT - THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) ALL PAPERWORK C/W

Part: SKIN — CORRODED (LT WING) · airframe 119,464 hrs · 20,125 cycles

*MAJOR REPAIR* FASTENERS PULLED THROUGH SKIN, LH WING***SM40/LMX6***HGR*** 1.REPAIR PER UPS EO-89517-REQ1 REV.1. 2.JOB COMPLETED. REVIEWED

Part: ACCESS PANEL — MISSING (NR 4 NACELLE)

OUTBD PYLON NO.4 FOUND PANEL 484DR MISSING

Part: BATTERY — INOPERATIVE (UPPER DECK) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3FOUND THE L1 DOOR EMERGENCY LIGHT INOPI.A.W AMM 33-51-04-902-001-001 REV.103.02 REPLACED THE L1 DOOR EMERGENCY LIGHT BATTERY ASSY (M5170) AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST , RESULT WAS SATISFACTORY

Part: SKIN — CRACKED (NO.12 SPOILER) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK DAMAGE WAS FOUND ON NO.12 SPOILER SKIN TRAILING EDGE , 47.75' FROM OUTBD EDGE OF SPOILER 'REPAIR I.A.W B747-400SF SRM 57-70-02-2R-1 , SRM 51-70-10-2R REPAIR GENERAL , AND SRM 51-70-10-2R-4 REV.53.00

Part: SKIN — CRACKED (NO.12 SPOILER) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK DAMAGE WAS FOUND ON NO.12 SPOILER SKIN TRAILING EDGE , 47.75'' FROM OUTBD EDGE OF SPOILERREPAIR I.A.W B747-400SF SRM 57-70-02-02-1, SRM 51-70-10-2R REPAIR GENERAL , AND SRM 51-70-10-2R-4 REV.53.00

Part: NONE — CRACKED (STA 2231,S-16R) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK ON EXIST REPAIR STRAPS OF FUSELAGE FRAME AT STA 2231 , S-16RREPAIR I.A.W BOEING SR : 4-5466926736 AND UPS EO B747-5340-83276-A

Part: STRAP — CRACKED (STA 2231) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACKS ON STRAP (P/N : 65B01849-47) AT STA 2231, BETWEEN S-16L AND S-17LREPAIR I.A.W BOEING SR : 4-5465984274 AND UPS EO B747-5310-83277-A

Part: CARGO TRACK — BROKEN (STA 570,RBL 45) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3BROKEN DAMAGE ON EXISTING REPAIR CARGO TRACK IN FWD CARGO COMPARTMENT AT STA 570 , RBL 45REPAIR I.A.W BOEING SR : 4-5465659276 AND UPS EO B747-5320-83274-A

Part: TENSION TIE — CRACKED (STA 1180) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK ON TENSION TIE FWD CHANNEL NEAR RBL 70 , STA 1180REPAIR I.A.W 747-400SF SRM 53-40-2R-1 REV.53.00

Part: NONE — CRACKED (STA 1140,S-9R) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK WAS FOUND ON EXISTING REPAIR CHORD ON STA 1140, S-9RREPAIR I.A.W BOEING SR:4-5465517685 AND UPS EO B747-5340-83249-A

Part: STRINGER — CORRODED (NO.18 VC FLAP) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CORROSION DAMAGE WAS FOUND ON STRINGER (P/N : 65B10857-9) ON R/H WING NO.18 V.C FLAPREPLACE PART I.A.W. 747-400SF SRM 51-40-02-0G , REV.53.00 AND BOEING DWG 65B15170 SH 2 , REV H.

Part: SKIN PANEL — CRACKED (STA 1810) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3CRACK ON FUSELAGE SKIN ON AFT CARGO DOOR CUTOUT FWD UPPER CORNER AREA , NEAR STA 1810 , S-26RREPAIR I.A.W BOEING SR : 4-5463029978 AND UPS EO B747-5330-83248-A

Part: SKIN PANEL — DENTED (STA 540,S-31R) · airframe 114,200 hrs · 19,128 cycles

INSPECTION TYPE:C3DENT ON FUSELAGE SKIN (P/N : 65B23674-2) NEAR STA 540 , S-31RREPAIR I.A.W BOEING SR : 4-5457728268 AND UPS EO B747-5330-83219-A

Part: SKIN — NONE (FUSELAGE TAIL) · airframe 113,966 hrs · 19,072 cycles

INSPECTION TYPE:N/ASKIN DMG AT TAIL BALL STAND AFT SKIN PNL AT STA 2598 BETWEEN S-26R AND S-42RREPAIRED PER EO B747-5330-82748-A

Part: NONE — NONE (DOORS) · airframe 113,172 hrs · 18,886 cycles

INSPECTION TYPE:NAUPPER DECK LEFT EXIT DOOR EMERGENCY BATTERY FAIL TESTREF 33 51 04 INSTALLED NEW BATTERY OPS NORMAL EFF SOURCE REF IPC 33 51 04 21 FIG 620

Part: NONE — NONE (DOORS) · airframe 113,172 hrs · 18,886 cycles

INSPECTION TYPE:NAUPPER DECK LH EXIT DOOR EMERGENCY BATTERY DOES NOT TEST "OK"CYCLED POWER OPS CHECK GOOD REF M/M 33 50 00

Part: NONE — ILLUMINATED (CABIN) · airframe 113,027 hrs · 18,852 cycles

INSPECTION TYPE:N/AUPPER DECK L.H. EMERGENCY EXIT DOOR "DOOR GROUND MODE" INDICATOR LIGHT NOT ILLUMINATEDRELAMPED I.A.W. / A.M.M. 33-12-02

Part: NONE — NONE (FUSELAGE) · airframe 113,027 hrs · 18,852 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** FOUND LOWER CARGO AFT 4 LOOP B FAULT MSG ON EICAS - NOT RESETABLE. ITEM DEFERRED PER MEL 26-16-1-2-2-1 REV 24. DMP ACCOMPLISHED. PLACARD INSTALLED. DMI M758012 OPENED.R/R R4223 AFT LL CGO 4 LOOP B RELAY. OPS CHECK GOOD PER SWPM 20-81-22. THIS CLEARS M758012

Part: SMOKE DETECTOR — FAULTY (FUSELAGE) · airframe 113,027 hrs · 18,852 cycles

INSPECTION TYPE:N/ADURING PDC FOUND MULTIPLE CARGO SMOKE DETECTION FAULTS.R&R MAWEA POWER SUPPLY YMXA020 PER AMM 31-51-01 PB 401 REV 102.00. TEST OK. P/N OFF-ON: 285T0035-202, S/N OFF: D05495, S/N ON: D04587. EFF REF IPC: 31-51-01-01 ITEM 005L.

Part: SKIN — DAMAGED (BS 1780-1800) · airframe 110,385 hrs · 18,309 cycles

INSPECTION TYPE: N/A FUSELAGE SKIN REPAIR STA 1780-1800 BETWEEN S33R AND S35R DAMAGED. REPAIRED IAW EP B747-5330-76919-C.

Part: MECHANISM — INOPERATIVE (EMERGENCY EXIT) · airframe 109,251 hrs · 18,127 cycles

RT EMERGENCY EXIT DOOR DIFFICULT TO ARM IN AUTOMATIC MODE. FOUND THE RT EMERGENCY DOOR MECHANISM OUT OF ADJUSTMENT. FOUND ARM/DISARM HANDLE HARD TO AUTOMATIC POSITION. ADJUSTED AND LUBRICATED THE ARM/DISARM MECHANISM. OP CHECKED NORMAL IAW AMM 52-23-00-825.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1FOUND EXIT EMERGENCY LIGHT INOP AT U/D CEILING STA 680 AREA1.I.A.W. AMM 33-51-07-002-009,33-51-07-402-015 REV 98.00 RPL EXIT EMERGENCY LIGHT AT U/D CEILING STA 680,AND PERFORMED EMERGENCY LIGHT TEST,THE RESULT WAS SATISFACTORY.

Part: BATTERY — DISCHARGED (UPPER DECK) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1FOUND LEFT SIDE U/D DOOR EMERGENCY LIGHT INOP.1.I.A.W. AMM 33-51-04-902-001-001 REV.97.03 REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY M5057. 2.I.A.W. AMM 33-51-04-902-001-001 REV.98.00 PERFORMED EMERGENCY LIGHT BATTERY FUNCTION TEST,RESULT WAS SATISFACTORY.

Part: BATTERY — DISCHARGED (UPPER DECK) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1FOUND EMERGENCY EXIT SIGN AND SLIDE LIGHT INOP AT R/H U/D DOOR AREA.1.I.A.W. AMM 33-51-04-902-001-001 REV.97.03 REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY M5056. 2.I.A.W. AMM 33-51-04-902-001-001 REV.98.00 PERFORMED EMERGENCY LIGHT BATTERY FUNCTION TEST,RESULT WAS SATISFACTORY.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CRACKS AND CORROSION ON RH #3 ENTRY DOOR AFT LWR SIDE VERTICAL FRAME.REPAIR I.A.W. BOEING SRID :4-4741334104 AND UPS EO B747-5210-75990-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 2140-2240FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1380-1500FABRICATE THE REPLACEMENT FLOOR PANEL PER EO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1440-1500FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 420-440FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 800-860FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 2350-2370FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1** SUPPLEMENTAL SDR ** DAMAGE ON M/D CARGO FLOOR PANEL AT STA 2040-2140FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1860-1960FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1580-1660FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 2140-2240FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1380-1500FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (UPPER DECK) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON U/D CARGO FLOOR PANEL AT STA 390-410FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1DAMAGE ON M/D CARGO FLOOR PANEL AT STA 440-460FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B747-5320-42648-A

Part: FITTING — CRACKED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CRACK WAS FOUND ON FITTING (P/N:65B17069-5) OF FUSELAGE AT STA 1000, LBL 78.49.REPAIR I.A.W. BOEING SRID :4-4709861461 AND UPS EO B747-5310-75989-A.

Part: CARGO TRACK — BROKEN (CARGO BAY) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1BROKEN DAMAGE WAS FOUND ON TRACK (P/N:65B06451-50) OF FWD LOWER CARGO COMPARTMENT AT STA 571 ,RBL 24.75.REPAIR I.A.W. BOEING SRID: 4-4736408358 AND UPS EO B747-5310-75956-A.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON ANGLE(P/N:65B06894-39)ON AFT CGO FLOOR STRUCTURE,STA 1819 RBL 48.REPLACE NEW PART I.A.W. 747-400SF SRM 51-40-02-0G REV 47.00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON INTERCOSTAL(P/N:65B06277-13)OF BULK CARGO COMPARTMENT NEAR STA 1990,RBL 53.45.REPLACE NEW PART I.A.W.747-400SF SRM 51-40-02-0G REV 47.00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON INTERCOSTAL(P/N:65B06261-47)OF BULK CARGO FLOOR STRUCTURE AT STA 2040,BL 0.REPAIR I.A.W. 747-400SF SRM 53-60-53,REPAIR 1,REV 47.00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON STRAP(P/N:146U5091-35)OF BULK CARGO FLOOR STRUCTURE AT STA 2002,LBL 7 TO RBL 7.REPLACE NEW PART I.A.W. 747-400SF SRM 51-40-02-0G REV 47.00.

Part: PLATE — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON PLATE (P/N: 65B04333-95) ON AFT CGO FLOOR STRUCTURE, STA 1920 LBL 45.REPLACE NEW PART I.A.W. 747-400SF SRM 51-40-02-0G REV.47.00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON STRAP(P/N:146U5091-35)OF BULK CARGO FLOOR STRUCTURE AT STA 2018,LBL7 TO RBL 7.REPLACE NEW PART I.A.W.747-400SF SRM 51-40-02-0G REV 47.00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON INTERCOSTAL(P/N:65B06164-1)OF BULK CARGO FLOOR STRUCTURE AT STA 2000 TO STA 2040,LBL 23.REPAIR I.A.W. 747-400SF SRM 53-60-53,REPAIR 1,REV 47.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON SEAT TRACK (P/N: 65B38259-5) OF SECTION 41 MAIN DECK BETWEEN STA 420-440, LBL 82.REPLACE NEW PART I.A.W. BOEING SR 4-4740914169 AND UPS EO B747-5310-75868-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON SEAT TRACK(P/N:140U5286-7)OF SECTION 41 MAIN DECK BETWEEN STA 420-440, LBL 82.REPLACE NEW PART I.A.W. 747-400SF SRM 51-40-02-0G REV 47.00.

Part: BEAM — CRACKED (R2 DOOR) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1** SUPPLEMENTAL SDR ** CRACK ON AFT LOWER CORNER OF RH NO.2 MAIN ENTRY DOOR.REPAIR IAW BOEING SRID #4-4717681548 & UPS EO B747-5210-75931-A.

Part: BEAM — CRACKED (L4 DOOR) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1** SUPPLEMENTAL SDR ** CRACK ON FWD LOWER CORNER OF LH NO.4 MAIN ENTRY DOOR.REPAIR IAW BOEING SRID #4-4718690922 & UPS EO B747-5210-75937-A.

Part: BEAM — CRACKED (L4 DOOR) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1** SUPPLEMENTAL SDR ** CRACK ON AFT LOWER CORNER OF LH NO.4 MAIN ENTRY DOOR.REPAIR IAW BOEING SRID #4-4718543710 & UPS EO B747-5210-75935-A.

Part: BEAM — CRACKED (L4 DOOR) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1** SUPPLEMENTAL SDR ** CRACK ON AFT UPPER CORNER OF LH NO.4 MAIN ENTRY DOOR.REPAIR IAW BOEING SRID 4-4718240551 & UPS EO B747-5210-75929-A.

Part: SKIN — CORRODED (LT WING) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON UPPER SKIN(P/N:112U3101-3)OF LH WING NEAR WS 422,REAR SPARREPAIR I.A.W.747-400SF SRM 57-20-01-1A-1 ALLOWABLE DAMAGE 1,REV 47.00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CRACK WAS FOUND ON FUSELAGE SKIN(P/N:65B04190-7)NEAR STA 980,S-38L.REPAIR I.A.W. 747-400SF SRM 53-20-01,REPAIR 2 DEVIATION SUPPORT BY SRID:4-4690849262 AND UPS EO B747-5330-75624-A.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1WING TO BODY FAIRING 192ER HINGE ANGLE FOUND CORROSION.REPAIR PER UPS EO B747-5240-75992-A REV.A

Part: PANEL — CORRODED (TE FLAP) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION ON PANEL ASSY (P/N:65B08423-502)OF R/H INBD MID FLAP NEAR WBL 347.069.REPAIR I.A.W.BOEING SRID:4-4703222604 AND UPS EO B747-5750-75991-A.

Part: SPLICE STRAP — CORRODED (LT WING) · airframe 108,402 hrs · 17,999 cycles

INSPECTION TYPE:D1CORROSION WAS FOUND ON SPLICE STRAP(P/N:65B11601-7)OF L/H WING FRONT SPAR NEAR OLES 1515.REPAIR I.A.W. UPS EO B747-5710-75615-A.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 107,884 hrs · 17,915 cycles

INSPECTION TYPE:NACEILING EMERGENCY LIGHT INOP AT UPPER DECK , JUST FWD OF SUPERNUMERARY SEATS.RELAMPED CEILING EMERGENCY LIGHT AS REQUIRED REF: MM 33 51 07. OPS CHECK GOOD.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 106,365 hrs · 17,680 cycles

INSPECTION TYPE:N/AMAIN CARGO DECK POS 20L AFT LEFT FLOOR PANEL DAMAGED IN 2 PLACESMANUFACTURED NEW PANEL IAW UPS E.O. B747-5320-42648-A ON NRC 620413

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 106,365 hrs · 17,680 cycles

INSPECTION TYPE:N/A2" DIA HOLE MAIN CARGO FLOOR PNL STA 2200-2280 POS 2L FWD LT PNL 814B6554-273FABRICATED NEW FLOOR PNL PER EP B747-5320-42648-A

Part: BATTERY — NO TEST (UPPER DECK) · airframe 104,780 hrs · 17,439 cycles

RIGHT UPPER DECK DOOR EMERGENCY SYSTEM BATTERY TEST FAILED. REPLACED THE UPPER DECK DOOR EMERGENCY SYSTEM BATTERY PACK IAW AMM 52-23-14-004-001, AND AMM 52-23-14-404-005, REV 93.03, AND PERFORMED AN INSTALLATION TEST, THE TEST WAS SATISFACTORY.

Part: BATTERY PACK — NO TEST (UPPER DECK) · airframe 104,780 hrs · 17,439 cycles

FOUND THE UPPER DECK LEFT DOOR EMERGENCY SYSTEM BATTERY TEST FAILED IAW AMM 52-23-14-004-001, AND AMM 52-23-14-404-005 REV.93.03. REPLACED THE BATTERY PACK AND PERFORMED NEW BATTERY PACK INSTALLATION TEST, RESULT WAS SATISFACTORY

Part: STRUCTURE — CRACKED (BS 2598) · airframe 104,780 hrs · 17,439 cycles

A CRACK WAS FOUND AT TWO FASTENER HOLES, BS 2598, DURING PERFORMANCE OF SB 747-53A2427 RELATED TO AD 2010-14-07. REPAIRED IAW SRID 4-4288337329, AND EO B747-5310-70636-A.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 104,017 hrs · 17,321 cycles

UPPER DECK RIGHT EMERGENCY LIGHTBATTERY FAILED TO TEST. PERFORMED DMP 52-23-7. R & R THE UPPER DECK DOOR BATTERY RT . OPS CHECKED GOOD. OKAY FOR SERVICE IAW AMM 52-23-14-004-001.

Part: SKIN — CORRODED (FUSELAGE) · airframe 103,466 hrs · 17,244 cycles

CORROSION ON FUSELAGE SKIN ON UPPER FWD LT SIDE OF APU COMPARTMENT JUST AFT OF STA 2658. REPAIRED PER EO B747-5330-68999-A.

Part: LINK — DETACHED (PAX DOOR) · airframe 103,270 hrs · 17,216 cycles

MAIN DECK ENTRY DOOR OUTSIDE HANDLE WILL NOT OPEN OR CLOSE THE DOOR, INSIDE HANDLE WORKS NORMAL. FOUND ENTRY DOOR UPPER HINGE LINK HAD COME OUT OF THE UPPER BEARING. REMOVED THE BEARING, REINSERTED LINK AND REINSTALLED. IAW MM 52-11-01-401, CONFIG 2. OPS CHECKED GOOD IAW MM 52-11-01-501.

Part: LINER — DAMAGED (BS 888) · airframe 102,621 hrs · 17,123 cycles

MAIN CARGO DECK POS 6 CEILING SMOKE BARRIER DAMAGED. R & R LINER ASSY AT BS 888 IAW AMM 25-59-01-404-176.

Part: LINER — TORN (MAIN CARGO) · airframe 102,621 hrs · 17,123 cycles

MAIN CARGO DECK POS 6R SMOKE BARRIER WHERE NET COMES OUT OF SIDEWALL TORN. R & R THE LINER AT BS 900 IAW AMM 25-59-01-404-176.

Part: FLOOR SUPPORT — CORRODED (BS 1920-1970) · airframe 102,336 hrs · 17,080 cycles

INSPECTION TYPE: C4, CORRIOSION DAMAGE ON BULK CARGO FLOOR SUPPORT AT BS 1920 - 1970, RBL 55. REPAIRED IAW SRID 3-4131002048 AND EO B747-5320-67599-A.

Part: SKIN — CRACKED (BS 2658) · airframe 102,336 hrs · 17,080 cycles

INSPECTION TYPE: C4, CRACK ON FUSELAGE SKIN NEAR BS 2658, STRINGER 12R. REPAIRED IAW SRID 3-4114844072, AND EO B747-5330-67498-A.

Part: SKIN — CORRODED (BS 2658) · airframe 102,336 hrs · 17,080 cycles

INSPECTION TYPE: C4, CORROSION ON THE FUSELAGE SKIN NEAR BS 2658, STRINGERS 15L & 16L. REPAIRED THE SKIN IAW SRID 3-4114843884, AND EO B747-5330-67496-A.

Part: SKIN — DENTED (LT INBD MID FLAP) · airframe 102,336 hrs · 17,080 cycles

INSPECTION TYPE: C4, DENT ON THE LT INBD MID FLAP LOWER SKIN AT WBL 169.30. REPAIRED IAW SRM 57-53-01, REPAIR 1, REV 40, SRM 51-70-10, REPAIR 4, REV 40, AND SRM 51-70-10, REPAIR GENERAL REV 40.

Part: DOOR — BINDING (MAIN PAX) · airframe 102,016 hrs · 17,037 cycles

CREW ENTRY DOOR BINDING WHEN ATTEMPTING TO CLOSE. DOOR FELL OPEN AFTER BEING PHYSICALLY CLOSED. TROUBLESHOT IAWFIM 52-11-00-812-810, LUBRICATED HINGE IAW FIM. OK FOR CONTINUED SERVICE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,401 hrs · 16,947 cycles

LEFT UPPER DECK DOOR EMERGENCY OPEN SYSTEM, 6 VOLT BATTERY TEST SWITCH WILL NOT TEST. REPLACED THE LT UPPER DECK EMERGENCY LIGHT BATTERY IAW AMM 33-51-14.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 100,953 hrs · 16,883 cycles

BATTERY CHECK UPPER DECK LEFT DOOR INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: SLIDE — UNWANTED DEPLOY (RT SIDE) · airframe 100,764 hrs · 16,856 cycles

RIGHT ESCAPE SLIDE DEPLOYED. REMOVED AND REPLACED THE SLIDE IAW MM 25-68-01-004-001, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,470 hrs · 16,812 cycles

DURING CHECK, FOUND UPPER DECK LT SIDE EMERGENCY POWER SYS BATTERY PACK INOPERATIVE. R & R THE BATTERY PACK IAW AMM 52-23-14. TESTED GOOD, ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 100,311 hrs · 16,787 cycles

FOUND LEFT EMERGENCY POWER SYSTEM BATTERY PACK LOW, TEST FAILED. R & R THE BATTERY PACK IAW AMM 52-23-14. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (DOOR ASSIST) · airframe 100,089 hrs · 16,759 cycles

FOUND UPPER DECK DOOR EMERGENCY OPENING SYSTEMS TEST FAULT. REPLACED THE BATTERY PACK IAW AMM 52-23-14-004-001, AND AMM 52-23-14-404-005, REV.89.01 2. PERFORMED BATTERY PACK TEST IAW AMM 52-23-14-404-005, REV 89.01.

Part: BARRIER — DAMAGED (MAIN CARGO DOOR) · airframe 99,476 hrs · 16,666 cycles

FIRE BARRIER ON THE MAIN CARGO DOOR DAMAGED & TORN IN TWO LOCATIONS. REPLACED THE BARRIER IAW AMM 25-58-06.

Part: AXE — DAMAGED (CARGO DECK) · airframe 99,476 hrs · 16,666 cycles

MAIN CARGO DECK CRASH AXE BLADE DAMAGED. R & R CRASH AXE IAW AMM 25-60-00-216-005.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 98,548 hrs · 16,530 cycles

SEAT TRACK STA 588 RBL45.5 DAMAGED. REPAIRED IAW EO B747-5320-62900-A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 98,548 hrs · 16,530 cycles

FWD LWR CARGO SEAT TRACK DAMAGED STA 588 RBL24.75. REPAIRED IAW EO B747-5320-62900-A.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 98,548 hrs · 16,530 cycles

FWD LWR CARGO BEAM DAMAGED STA 571 RBL 24-RBL 45. REPLACED AND REPAIRED BEAM IAW EO B747-5320-62864-B.

Part: MECHANISM — LACK OF LUBE (EMERGENCY EXIT) · airframe 98,143 hrs · 16,465 cycles

UNABLE TO DISARM LT UPPER EMERGENCY EXIT DOOR. LUBED INNER ARM DISARM MECHANISM IAW AMM 12-21-04-603-004. OPS CHECKED OF ARM/DISARM HANDLE IAW AMM 52-23-00-715-001, CHECKED GOOD.

Part: SPAR — CORRODED (RT WING) · airframe 96,085 hrs · 16,161 cycles

CORROSION ON RT WING LOWER SPAR CHORD AT BS OLES. 1510. REPAIRED CORRODED RT WING LOWER SPAR CHORD AT BS OLES. 1510 IAW EA 747-5710-01-A6300 REV. I/R AND EO B747-5710-61018-B.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 96,085 hrs · 16,161 cycles

DAMAGE TO AFT LOWER CARGO DOOR SKIN, FWD LOWER CORNER REPAIR IAW EO B747-5230-60772-B.

Part: SKIN — PUNCTURED (BS 1780-1800) · airframe 95,557 hrs · 16,081 cycles

PUNCTURE FUSELAGE SKIN 18.0" FWD OF AFT LOWER CARGO DOOR MID SECTION ON LAP SEAM REPAIRED IAW EO B747-5330-60373-A.

Part: DOOR — INOPERATIVE (SMOKE BARRIER) · airframe 95,557 hrs · 16,081 cycles

UPPER DECK ENTRY DOOR SMOKE BARRIER SIDE ON AFT SIDE COMING LOOSE AND OUT OF TRACK ON DOOR FRAME. INSPECTED AND REMOVED SEAL AND RETAINER AND ROUTED TO S/M FOR REPLACEMENT T22710 ILLEG. INSTALLED NEW SEAL ON RETAINER AND INSTALLED ON ACFT IAW DWG 841133101.

Part: BATTERY — INOPERATIVE (SLIDE) · airframe 95,552 hrs · 16,080 cycles

RT UPPER DECK ESCAPE SLIDE BATTERY TEST DOES NOT WORK. REMOVED RT POWER SUPPLY IAW AMM 33-51-04-002-009-001. INSTALLED SERVICABLE UNIT IAW AMM 33-51-04-402-012-001. OPS CHECK GOOD EFF SOURCE REF: IPC 33-51-04-21, ITEM 626.

Part: DOUBLER — CRACKED (BS 2645-2658) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CRACK, FOUND LT FUSELAGE SKIN CRACK AT BETWEEN BS 2645 TO BS 2658, BETWEEN STR 9L TO 11L. REPAIR IAW SRID:3-3465201587 WITH APPROVED 8100-9 FORM, DATED 21MAR2016 AND EO NR B767-5330-60276-A.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION, SKIN , BETWEEN WS 834 AND WS 858 , RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR, REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION, SKIN, WS 1205, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR. REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION, SKIN, WS 917, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION SKIN, BETWEEN WS 944 AND WS 972, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR. REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION, SKIN, BETWEEN WS 724 AND WS 807, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION, SKIN , WS 655, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R. REPAIR 1, REV 35.01.

Part: SKIN — CORRODED (RT WING) · airframe 95,507 hrs · 16,073 cycles

INSPECTION TYPE:C3, CORROSION-SKIN, WS 1028, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.

Part: COVER — FAILED (ESCAPE DOOR) · airframe 94,122 hrs · 15,870 cycles

EMERGENCY DOOR ARMING LEVER HANDLE COVER FAILED AT HINGE. INSPECTED RE-ATTACHED SHIM IAW DWG 69B56837. NOTE: 1 AND HUNTSMAN. ADHESIVE 5774-ACFT. DOOR PS NORMAL AT THIS TIME. THIS CLEARS M563485. NO RESTRICTIONS AT THIS TIME. DMI REVERSED.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 93,610 hrs · 15,786 cycles

INSPECTION TYPE:CR, HW INBD AFT FLAP LOWER MAIN SKIN FOUND DAMAGED D559545. PERFORMED METAL HOT BOND REPAIR IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 3, REV 33.

Part: LIFE VEST — OPEN (FLIGHT DECK) · airframe 93,588 hrs · 15,783 cycles

PASSENGER LIFE VEST FOUND OPEN DURING CHECK. R & R LIFE VEST IAW MM 25-62-05 EFF SOURCE, REF 25-62-05-39H-005.

Part: HANDLE — MISSING (R1 DOOR SLIDE) · airframe 92,854 hrs · 15,672 cycles

ACCESS DOOR TO EMERGENCY SLIDE HANDLE MISSING ON RT UPPER DECK. REPLACED MISSING COVER IAW MM 52-23-02.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 91,652 hrs · 15,485 cycles

APPROXIMATELY 1.5" DENT IN CENTER LOWER SKIN PANEL OF RT INBD AFT FLAP. REPAIRED IAW EO B747-5750-56765-A.

Part: DOOR — FAILED (ESCAPE SLIDE)

INSPECTION TYPE: BTB, UPPER DECK ESCAPE SLIDE DOOR LT SIDE WOULD NOT ARM TO THE AUTOMATIC POSITION. R&R LEFT UPPER DECK ESCAPE SLIDE DOOR IAW AMM 25-68-01-404-005.

Part: COVER — BROKEN (PAX DOOR)

F/O SIDE DOOR ARM SLIDE SAFETY DOOR IS BROKEN OFF HINGE. SECURED THE UPPER RT SLIDE DOOR ARMING COVER AND CARRY OUT OPS CHECK IAW AMM 52-23-00-716-011 AND FOUND SATISFACTORY.

Part: SLIDE — OUT OF ADJUST (COCKPIT)

CAPTAIN`S EMERGENCY ESCAPE SLIDE DOOR WILL NOT ARM. REMOVED AND ADJUSTED POSITION OF FLOOR MOUNTED ESCAPE SLIDE IAW MM 25-68-01. SYS OPERATES NORMALLY.

Part: DOOR — OBSTRUCTED (ESCAPE SLIDE)

LEFT UPPER DECK SLIDE DOOR INOPERATIVE, UNABLE TO ARM. OPENED LT UPPER DECK DOOR, FOUND FASCIA PANEL NOT SELECTED PREVENTING DOOR FUNCTION. SECURED FASCIA PANEL. DOOR OPERATED OK IAW MM 52-23-00. OPS CK GOOD.

Part: HOOK — LACK OF LUBE (EMERGENCY EXIT)

LT EMERGENCY EXIT UNABLE TO ARM. CLEANED/LUBED SLIDE DEPLOYMENT HOOK AND MODE SELECTOR LEVER. OPS TEST IAW 52-23-00/501.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, L1 DOOR EMERGENCY LIGHT INOPERATIVE DURING TEST OF POWER SUPPLY. BATTERY PACK REPLACED AND LIGHTS TESTED NORMAL IAW AMM 33-51-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, UPPER DECK EMERGENCY LIGHTS POWER SUPPLY FOUND INOPERATIVE. BATTERY PACK REPLACED, LIGHTS TESTED NORMAL.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, RIGHT ELEVATOR L/E PANEL, FOUND CRACK. REPAIRED IAW RI RI-55-20-10719, REV A AND EO NR B747-5520-55549-A. MAJOR REPAIR.

Part: WEB — CRACKED (BS 708) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, BS 708, STRINGER 13L DOOR LOWER SILL WEB FOUND CRACKED. REPAIRED IAW RI RI-53-20-10691 REV A & EO 5330-55443-A.

Part: SUPPORT ANGLE — CRACKED (RT ELEVATOR) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, RIGHT ELEVATOR UPPER PANEL SUPPORT ANGLE FOUND CRACKED. REPAIRED IAW RI RI-55-23-10709, REV A & EO NT B747-5530-55612-A.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 90,211 hrs · 15,267 cycles

RT ELEVATOR L/E UPPER COVER RIVET, HEAD FOUND ELONGATED AT ELEVATOR STA 302.63. RIGHT SIDE ELEVATOR L/E FAIRING, BONDED SKIN, AT ELEVATOR STA 302.63 AREA REPAIRED IAW RI RI55-23-10708, REV A & EO NR B747-5520-55441-A. MAJOR REPAIR.

Part: ANGLE — CRACKED (RT ELEVATOR) · airframe 90,211 hrs · 15,267 cycles

RIGHT OTBD ELEVATOR L/E ES 281.8 WEB AND ANGLE FOUND CRACKED. REPAIRED IAW RI RI-55-23-10703, REV A & EO B747-5520-55569-A. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 2231) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, BS 2231, STR 16R, FRAME CRACKED. REPAIRED IAW RI RI-53-60-10699, REV A & EO NR B747-5340-55604-A.

Part: FRAME — CRACKED (BS 2231) · airframe 90,211 hrs · 15,267 cycles

INSPECTION DFX, FRAME BS 2231, S16-17R FOUND CRACKED. REPAIRED IAW RI RI-53-60-10699, REV A AND EO NR 5340-55604-A.

Part: REVEAL — CRACKED (R4 DOOR) · airframe 90,211 hrs · 15,267 cycles

INSPECTION TYPE:D, MAIN DECK R4 DOOR FWD LWR CUTOUT FOUND CRACKED. M/D R4 DOOR FWD LWR CUTOUT AT STA 1664 AREA REVEAL PANEL IS REPAIRED IAW SRM 53-60-15-2R-4, FIG 201, REV 29. THIS REPAIR IS A CATEGORY B REPAIR WITH 2 LAYERS OF DOUBLER 0.050", 2024T3. REPEAT INSP IS REQUIRED IAW SRM 53-60-15-2R-4, FIG 201, REV 29, TABLE II. INSP THRESHOLD 3000 FLT CYC. REPEAT INSP INTERVAL 3000 FLT CYC.

Part: ANGLE — CORRODED (BS 708) · airframe 90,211 hrs · 15,267 cycles

INSPECTION DU/D, BS 708, STRINGER 13L LT DOOR SILL WEB OTBD ANGLE FOUND CORRODED. REPAIRED IAW RI RI-53-20-10691 REV A & EO B747-5330-55443-A.

Part: FRAME — CRACKED (BS 800) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, MAIN DECK FRAME BS 800, STRINGER 17R, CRACKED ON INNER ANGLE. FRAME BETWEEN STRINGERS 16-18R REPAIRED IAW RI RI-53-20-10684, REV A & EO NR B747-5310-55577, REV A.

Part: FRAME — CRACKED (BS 800) · airframe 90,211 hrs · 15,267 cycles

INSPECTION D, LT BS 800, FRAME, STR 17 CRACKED AT INNER ANGLE. FRAME BETWEEN STRINGERS 16-18L REPAIRED IAW RI RI-53-20-10683, REV A & EO NR 5310-55578-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

INTERIM REPAIR TO MAIN CARGO DECK FLOOR PANEL, BS 292, LBL 13. REPAIRED IAW SRM 53-00-50-2R-1-4B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK BS 1310 FLOOR PANEL DAMAGED APPROX .7500 INCHES DIAMETER. REPAIRED IAW SRM 53-00-50-2R-1.

Part: SKIN — DAMAGED (RT WING TE FLAP)

RT OTBD MID FLAP HAS A HOLE IN LOWER INBD SKIN. REPAIRED IAW EO B747-5750-54723-A.

Part: RIB — CRACKED (RT WING)

RT INBD MIDFLAP COVE PANEL, OTBD RIB CRACKED AT FASTENER HOLE. REPAIRED IAW EO -54544-A.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LT EMERGENCY EXIT DOOR IN UPPER DECK BATTERY CHECK ANNUNCIATOR LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD IAW 52-23-14-706-011.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

MAIN CARGO DECK FLOOR PANEL HAS A 0.4 INCH HOLE IN UPPER SKIN AND CORE DAMAGED. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-1, PARA 4C.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

MAIN CARGO DECK FLOOR PANEL, HAS A 0.25 INCH HOLE IN TOP SKIN AND CORE DAMAGE BS 1650. REPAIRED IAW SRM 53-00-50-2R1, PARA 4C.

Part: SKIN — DAMAGED (LT WING)

LEFT WING INBD FLAP COVE PANEL LOWER SKIN DAMAGED 82 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-53168.

Part: SKIN — DAMAGED (LT WING)

LEFT WING INBD FLAP COVE PANEL LOWER SKIN DAMAGED 146 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-53170-A.

Part: SKIN — DAMAGED (LT WING)

LEFT WING INBD MID FLAP COVE PANEL PUNCTURED ON LWR SURFACE 41-62 INCHES FROM INBD EDGE OF FLAP. REPAIR IAW EO B747-5750-53171-A.

Part: SKIN — DAMAGED (LT WING)

LEFT WING INBD FLAP COVE PANEL LOWER SKIN DAMAGED 38 INCHES FROM INBD EDGE. REPAIRED IAW EO B757-5750-53169.

Part: SKIN — DAMAGED (RT WING)

RT INBD MID FLAP COVE PANEL HAS 2.0 X 1.5 HOLE. REPAIRED IAW EO B747-5750-53175-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK BS 1760 FLOOR PANEL DAMAGED, FABRICATED FLOOR PANEL IAW EO B747-5320-53159-A.

Part: FLOOR PANEL — CRACKED (BS 1910)

TWO CRACKS IN FLOOR PANEL, BS 1910. FABRICATE NEW FLOOR PANEL IAW EO B747-5320-53158-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK BS 1700, FLOOR PANEL DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO-5320-53160-A.

Part: VALVE — FAILED (LT WING FUEL)

TOWER REPORTED FUEL LEAKING AT TAKE OFF. FOUND LT WING SURGE TANK INBD PRESSURE RELIEF VALVE OPEN. INSPECTED SURGE GE TANK VENT TUBE FOR BLOCKAGE. NO BLOCKAGE. VALVE FAILS MANUAL, OPS TEST. R & R LT WING SURGE TANK INBD PRESS RELIEF VALVE.

Part: TRANSMITTER — INOPERATIVE (TE FLAPS)

CREW RECEIVED FLAP DRIVE EICAS MESSAGE, EMERGENCY DECLARED. RAN FLAPS DRIVE QRH CHECKLIST. LANDED WITHOUT INCIDENT. CHECKED CMC PRESENT LEG FAULTS FOUND MESSAGE 27771 AND CMC EXISTING FAULTS. 27650 RT OTBD RVDT FAIL. R & R RT OTBD FLAP POSITION TRANSMITTER IAW AMM 27-58-01, PG BLOCK 401, REV 7702. OPS CHECK SATISFACTORY OF RVDT IAW PG BLK 27-58-01/501.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE:C, LT WING INBD T/E FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 26.

Part: SKIN — DAMAGED (APU AREA) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE:C, APU COMPT RT SUPPORT FRAME FOUND LOOSE AT BS 2680, WL 300 TO WL 320. APU BAY RT BS 2658 TO 2701 BETWEEN WL 280-340 AREA SKIN PANEL REPAIRED IAW HX RI-53-81-10277, REV A AND EO B747-5330-51680-A, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: ACCESS PANEL — DAMAGED (NR 3 PYLON) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE: C, NR 3 PYLON PANEL 472EL LATCH CUTOUT AREA ELONGATED. REPAIRED IAW HX RI-54-57-10280, REV A AND EO B747-5420-51649-A AND CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 983) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE: C, BS 983 FLOOR SUPPORT FOUND CORRODED. REPAIRED IAW SRM 53-00-71-2R REPAIR 3, FIG 201, REV 26.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE:C, RT WING INBD T/E MID FLAP T/E COVE PANEL HAS DELAMINATION. FIBERGLASS PREPREG LAY-UP REPAIR PERFORMED IAW SRM 51-70-07, PAR5A (1), FIG 5, REV 25.

Part: KEELBEAM — CORRODED (BS 987-1050) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE: C, BS 987 TO 1050 KEEL BEAM BOX AREA SEVERAL LOCATIONS OF CORROSION. REPAIRED IAW HX RI-53-49-10282, REV A & EO B747-5310-51646-A, REPAIR CLASSIFIED AS MINOR.

Part: BEAR STRAP — CORRODED (MAIN DECK) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE:C, MAIN DECK R3 DOOR AFT UPPER CUTOUT CORNER CORRODED. REPAIRED IAW HX RI-53-41-10270, REV A AND EO B747-5330-51647-A, REPAIR CLASSIFIED AS MAJOR.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 86,320 hrs · 14,670 cycles

INSPECTION TYPE:C, MAIN DECK R3 DOOR AFT UPPER CUTOUT CORNER CORRODED. BEAR STRAP REPAIRED IAW HX RI-53-41-10270, REV A AND EO B747-5330-51647. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBOARD — DAMAGED (MAIN CARGO)

HOLE IN FLOORBOARD CENTERLINE BS 1700. REPAIRED IAW SRM 53-00-50-2R.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DOOR BATTERY TEST FAILED. R & R UPPER DECK DOOR EMERGENCY LIGHT BATTERY PACK IAW AMM 52-23-14-004-001, 52023014-404-005.

Part: PSEU — FAILED (LANDING GEAR)

AFTER TAKEOFF GEAR LEVEL WOULD NOT RETRACT. GEAR DOOR AND GEAR DISAGEE ON EICAS. PERFORM PSEU GUARD TEST FAIL. R & R PSEU AND PERFORM GUARD TEST PASSED. IAW AMC REQUEST, R & R BODY GEAR TILT ALT SW AND WING GEAR TILT PRI SW. DUE TO T/S FOUND SW FAULT. CLEAN ALL BODY AND WING GEAR SW AND NOSE GEAR SQUAT SNRS. VISUAL CHECKED NORMAL. PERFORM TILT POS SENSOR AND LEVEL SW TEST ALL FUNCTION NORMAL AND LANDING GEAR LEVEL MOVING NORMAL. NO FAULT FOUND.

Part: SWITCH — FAILED (EMERGENCY LIGHTS)

RT UPPER DECK EMERGENCY DOOR 6 VOLT BATTERY TEST FAILED P/S CHECK. REPLACED LAMP SWITCH, PRESS TO TEST CHECKS NORMAL IAW 52-23-14-6.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT AT ENTRY DOOR INOPERATIVE. LAMPED IAW AMM 33-51-07.

Part: FLOOR PANEL — DAMAGED (BS 518 RBL 9.5)

MAIN DECK FLOOR PANEL HAS 1 INCH DIA HOLE TO THE TOP SURFACE PAN. REPAIRED REF SRM 53-00 50 2R-1, PAR4C.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, LEFT WING OTBD AFT FLAP T/E WEDGE UPPER SURFACE OTBD AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A FIG 5, REV19.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:3C, RT SIDE HORIZONTAL STAB UPPER REAR SPAR HORIZONTAL SPLICE PLATE AREA WAS FOUND 2 EA FASTENER HOLES CRACKED IN SKIN LAYER. REPAIRED IAW HX RS R-55-10-37291 REV A & EO B747-5510-45851-A, ORI MATERIAL IS 7075T6511-0.313", 2 EA CRACKS AT HOLE NR 6 ARE 0.030" APPROX & 1 EA CRK HOLE NR 8 IS 0.030" APPROX, AT HOLES NR 6 & NR 8 INSTALL BACB30US8K, Y BOLTS WITH NUTS & WASHERS IAW SB 747-55A-2050, REV 1 & AT HOLES NR 5 & NR 7 INSTALL BACB30US7K, Y BOLTS WITH NUTS AND WASHER.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, LT WING OTBD T/E MID FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 19.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, BULK CARGO COMPT STA 1940 TO 2060, RBL 22.5, FLOOR PANEL SUPPORT UPPER & LOWER SURFACE FOUND SEVERAL AREA CORRODED. ORG MATERIAL IS BAC1506-2261-7075T6 & THICKNESS IS 0.050", BLENDED DEPTH IS 0.035", WIDTH 1" & LENGTH 1.5" OUT OF LIMIT, DAMAGE CUT OFF LENGTH IS 100" THIS IS A MAJOR REPAIR WITH MATL BAC1506-2261-7075T6511 AS FLOOR SUPPORT REPAIR SECTION AND 7075-0-0050IN AS REPAIR ANGLES (HEAT TREAT TO T6 CONDITION AFTER FORMING), REPAIR SIZE IS 110".

Part: FLOOR SUPPORT — CORRODED (BS 1940-2000) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, BULK CARGO COMPT STA 1940 TO 2000, RBL 45 FLOOR PANEL SUPPORT UPPER & LOWER SURFACE FOUND SEVERAL AREA CORRODED. ORG MATL IS BAC1500-6204-7075T6 & THICKNESS IS 0.040", BLENDED DEPTH IS 0.037", WIDTH 1"& LENGTH 2" OUT OF LIMIT, DAMAGED AREA CUT OFF LENGTH IS 70", THIS IS A MAJOR REPAIR WITH MATL BAC1500-6204-7075T62 AS FLOOR SUPPORT REPAIR SECTION AND 7075-0-0040IN AS REPAIR ANGLES (HEAT TREAT TO T6 CONDITION AFTER FORMING), REPAIR SIZE IS 70.5"

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, BULK CARGO COMPT STA 1920 TO 1980 LBL 22.5 FLOOR PANEL SUPPORT UPPER & LOWER SURFACE FOUND SEVERAL AREA CORRODED. ORG MATL IS BAC1506-2261-7075T6 & THICKNESS IS 0.050", BLENDED DEPTH IS 0.028", WIDTH 1"& LENGTH 1" OUT OF LIMIT, DAMAGED AREA CUT OFF LENGTH IS 70", THIS IS A MAJOR REPAIR WITH MATL BAC1506-2261-7075T6511 AS FLOOR SUPPORT REPAIR SECTION & 7075-0-0050IN AS REPAIR ANGLES (HEAT TREAT TO T6 CONDITION AFTER FORMING), REPAIR SIZE IS 70.5"

Part: FLOOR SUPPORT — CORRODED (BS 1960-2020) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, BULK CARGO COMPT STA 1960 TO 2020, LBL 53.45 FLOOR PANEL SUPPORT UPPER & LOWER SURFACE FOUND SEVERAL AREA CORRODED. REPAIR IAW HX RS R53-65-37290 REV A & EO B747-5320-45867-A. ORG MATL BAC1520-1892-7075T6511 & THICKNESS 0.063", CORRODED BLENDED AREA DEPTH 0.045", MINOR REPAIR WITH MATL BAC1520-1892-7075T6511 AS REPAIR INTERCOSTAL SECTION AND 7075-0-0080" AS REPAIR ANGLES. (HEAT TREAT TO T6 CONDITION AFTER FORMING)

Part: FLOORBEAM — CORRODED (BULK CARGO COMPT) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, BULK CARGO BAY STA 2044, LBL 54 TO RBL 54 FLOORBEAM UPPER & LOWER SURFACE FOUND SEVERAL AREAS CORRODED. REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV.19. THICKNESS IS 0.050",BLEND DEPTH IS 0.037", WIDTH 1" & LENGTH 1.5" OUT OF LIMIT IAW SRM 53-00-53 ALLOWABLE DAMAGE 1 FIG 101, REV 19, DAMAGED PARTS REPLACED WITH MFG PART, PN 69B03459-2

Part: FAIRING — PUNCTURED (LT WING TE FLAP) · airframe 81,457 hrs · 13,958 cycles

INSPECTION TYPE:C, LT WING OTBD T/E AFT FLAP OTBD L/E FAIRING PUNCTURE HOLE. FIBERGLASS PREPREG LAY UP REPAIT CARRIED OUT IAW SRM 51-70-06, PAR 5D, FIG 6, REV 19.

Part: SKIN — DENTED (LT WING TE FLAP)

LT WING INBD AFT FLAP LWR SURFACE HAS 2 DENTS. REPAIRED IAW EO B747-5750-44814-B.

Part: FLOOR PANEL — DAMAGED (BS 950L)

MAIN CARGO DECK FLOOR PANEL BS 950L DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: FLOOR PANEL — DAMAGED (BS 1550)

FLOOR PANEL HAS 1" HOLE, BS 1550. REPAIRED IAW SRM 53-00-50, REPAIR 1, PARA 4.D.

Part: SKIN — DAMAGED (LT WING TE FLAP)

LT IB AFT FLAP T/E UPPER SKIN DAMAGED. REPAIRED IAW EO B747-5750-42879-B.

Part: FLOOR PANEL — DAMAGED (BS 460)

MAIN DECK FLOOR PANEL DAMAGE AT AFT END STA 460 LBL 100. ISSUED N/R 396923 FOR REPAIR TO MAIN DECK FLOOR PANEL THIS IS A MAJOR REPAIR. ALL WORK ACCOMPLISHED ON NRC 396923 FOR REPAIR TO FLOOR PANEL. REF LP 562718 FOR REMOVAL AND INSTALL OF FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN)

MAIN DECK FLOOR PANEL DAMAGED APPROX 1.4 X .800 NEAR AFT END OF THE PANEL. REMOVED DAMAGED AND REPAIRED IAW SRM 53-00-50, REPAIR 1, PARA 4.D.

Part: WEB — CRACKED (BS 800 S22-26R) · airframe 78,259 hrs · 13,457 cycles

INSPECTION TYPE:C, CABIN R2 DOOR FWD CUTOUT WEB CRACKED BETWEEN S24R AND S25R. R2 DR FWD CUTOUT FRAME WEB REPAIRED IAW SRM 53-60-15-2R4, FIG 201. JUST AT STA 800 BTN S22R & S26R, CRACK LENGTH 0.875", 0.25" DIA STOP HOLE DRILLED, THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATL 2024T3- 0050" AS REPAIR INNER & OUTER DOUBLER, REPAIR SIZE 5.5" X 19". REPEAT INSP IAW SRM 53-60-15-2R4, REPAIR 4, FIG 201, SHT 13, TABLE 2.

Part: FLOOR SUPPORT — DAMAGED (BS 570) · airframe 76,978 hrs · 13,259 cycles

INSPECTION TYPE:C, DMI D433753 - FWD LWR CARGO COMPT BALL MAT SUPPORT BEAM AND TRACK REPAIR AT BS 570. TIE DOWN TRACK REPAIRED IAW SRM53-00-52 REPAIR 10, REV 16 & EO B747- 5320-39438-A JUST AT RBL 45.5" BETWEEN STA570 & 591, BROKEN DAMAGE 3" ,CUT OFF LENGTH 21",IT IS CLASSIFIED A MAJOR REPAIR,TOTAL OF REPAIR LENGTH 25"FLR SUPPORT CHANNEL REPLACED IAW SRM51-10-02 & INSTALLED IAW SRM51-40-02, REV 16 & EO 5320-39438A AT STA570, BTN LBL62 & RBL62.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 76,978 hrs · 13,259 cycles

INSPECTION TYPE:C, DMI D433270 - LT WING OTBD AFT FLAP DENT OTBD OF INBD CANOE FAIRING. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 2, FIG 203, REV 16.

Part: LEVER — MALFUNCTIONED (EMERGENCY EXIT)

RT EMERGENCY DOOR WILL NOT ARM TO AUTOMATIC. DEFERRED RT UPPER MAIN ENTRY DOOR IAW MEL 52-23-1-3-1. PLACARD INSTALLED. CHECK ADJUSTMENT & TEST ON ARM/DISARM LEVER OPS CHECKS GOOD IAW AMM 52-23-005. THIS CLEARS MEL.

Part: SKIN — CORRODED (BS 740 S46L)

CORRISION AT FRAME 740 S-46L. REPAIRED IAW SRM 53-00-01 REPAIR 15, DETAIL 1,

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD IAW EO B747-5320-36305.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR DAMAGED. FABRICATED NEW FLOOR.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED. FAB NEW FLOORBOARD.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED. FABRICATED NEW FLOOR BOARD.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD.

Part: FLOORBOARD — DAMAGED (UNKNOWN)

FLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD.

Part: LIGHT — INOPERATIVE (CABIN)

UPPER DECK AFT EMERGENCY CEILING LIGHT INOP. RE-LAMPED UPPER DECK AFT EMERGENCY CEILING LIGHT PER MM 33-51-07-2. OPS CK NORMAL.

Part: HINGE FITTING — CORRODED (KRUEGER FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:N/A RT WING - NR 14 K/FLAP BULLNOSE FAIRING O/B HINGE FTG CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-02 AND 51-20-01 BLENDING WITHIN LIMIT AND REF UPS EO B747-5740-33385-A.

Part: FAIRING — CRACKED (TE FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - NR 18 VC FLAP BULLNOSE FAIRING SURFACE SKIN FOUND CRACKED. RT WING NR 18 VC FLAP BULLNOSE FAIRING SKIN REPAIRED AS PER SRM 57-43-02 FIG 20 REPAIR 2 REV11, MATERIAL 202473 .056IN & REPAIR SIZE 4 .75 X 10 INCH.

Part: FITTING — CRACKED (SPOILER) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING NR 6 SPOILER LWR 'H' FTG O/B LWR AREA NR 3 HOLE FROM BOTTOM FOUND CRACKED RUNNING UPWARD AND I/B DOWNWARD CRACK LENGTH APPROX 0.040 INCH FOR BOTH CRACKS. LT WING NR 6 SPOILER LWR 'H' FTG O/B LOWER LUG REPAIRED AS PER RS R57-51-36307 REV A. REPEAT INSPECTION IS REQUIRED AS PER RS R57-51-36307 REV A. REPAIR WITH MATERIAL 7075T6.100" REPAIR ANGLE. SIZE 6.125" X 3.25" REFER NRC 50350 FOR WORKING DETAIL AND REF UPS EO B747-5740-33436-A.

Part: FITTING — CRACKED (FWD CARGO DOOR) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D FWD CARGO COMPT DOOR FWD UPPER CORNER CLIP FOUND CRACKED. FWD CARGO COMPT DOOR FWD UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: FITTING — CRACKED (FWD CARGO DOOR) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D FWD CARGO COMPT DOOR AFT UPPER CORNER CLIP FOUND CRACKED. FWD CARGO COMPT DOOR AFT UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D AFT CARGO DOOR FWD HINGE DOOR SIDE FWD UPPER CORNER CLIP FOUND CRACKED. AFT CARGO DOOR FWD HINGE DOOR SIDE FWD UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: WEB — CRACKED (RT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - ILES 1185 L/E NOSE FAIRING AFT WEB FOUND CRACKED. RT WING OLES 1185 L/E NOSE FAIRING AFT WEB REPAIRED AS PER RS R53-00-36311 REV A. REPAIR WITH MATERIAL 7075T6.063" REPAIR SIZE 5" X 6.25". UPS EO B747-5720-33425-A.

Part: WEB — CRACKED (LT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING - ILES 1185 L/E NOSE FAIRING AFT WEB FOUND CRACKED. LT WING OLES 1185 L/E NOSE FAIRING AFT WEB REPAIRED AS PER RS R57-00-36311 REV A. REPAIR WITH MATERIAL 7075T6.063" SPLICE, REPAIR SIZE 5" X 6.25". UPS EO B747-5720-33425-A.

Part: CARGO TRACK — CRACKED (FWD CARGO BAY) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D FWD CARGO RBL 45 STA 570 PALLET LOCK TRACK FOUND CRACKED. FWD CARGO COMPT BS 570 TO BS 590-875 RBL 45 TIE DOWN TRACK REPAIRED AS PER SRM 53-00-52 FIG 201 REPAIR 10 REV 11.

Part: FLAP — DELAMINATED (RT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:C RIGHT - I/B FOREFLAP TE LWR I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D FWD CARGO RBL 45" STA 570 FLOOR SUPPORT FOUND CRACKED. FWD CARGO COMPT BS 570 RBL 34.25" TO RBL 58.25" FORMER SUPPORT REPAIRED AS PER SRM 51-70-11 FIG 1 REV 11.

Part: SUPPORT — DAMAGED (KRUEGER FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING - NR 13 K/FLAP SUPPORT FRAME LWR CHORD MID AREA FOUND CORROSION CRACKED. LT WING - NR 13 K/FLAP SUPPORT FRAME LWR CHORD REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: SUPPORT — CRACKED (LT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:C LEFT WING - O/B FORE FLAP T/E LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:C RT WING O/B FORE FLAP T/E UPPER SURFACE I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.

Part: ACCESS PANEL — WORN (NR 4 ENGINE) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D NR 4 ENG - RT C-DUCT LWR FWD LATCH ACCESS PANEL FWD AND AFT EDGE WORN. NR 4 ENG RT C-DUCT LOWER FWD LATCH ACCESS PANEL FWD AND AFT EDGE REPAIRED AS PER UPS EO NO B747-7830-33315-A AND CMM 78-32-09 REPAIR 005. MATERIAL 17-7PH 0.085" AS REPAIR DOUBLER ON FWD EDGE. 17-7PH 0.032" AS REPAIR DOUBLER ON AFT EDGE WITH REPAIR SIZE H5" X 9.75" FWD AREA & 1.25" X 9.75" AFT AREA.

Part: PANEL — CORRODED (TE FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 83 INCHES AREA REPAIRED AS PER HX RS R57-55-36310 REV A AND UPS EO B747-5750-33412-A.

Part: PANEL — CORRODED (LT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCH AREA REPAIRED AS PER HX RS NO R57-55-36310 REV A & UPS EO B747-5750-33412-A.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D FUSELAGE AREA STA 1232 RBL 104 STIFFENER FOUND CRACKED. FUSELAGE BS 1152 TO BS 1232 RBL 104 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 11.

Part: SKIN — DELAMINATED (SPOILER) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - NR 7 SPOILER LWR SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 11 51-70-10 REPAIR 4 FIG 201.

Part: FITTING — CRACKED (LT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D LHW - NR 6 SPOILER LWR 'H' FTG O/B LWR LUG FOUND CRACKED. LHW NR 6 SPOILER LOWER 'H' FTG OTBD LOWER LUG REPAIRED AS PER RS NR R 57-51-36307 REV A REPEAT INSPECTIONS IN REQUIRE AS PER RS NO R 57-51-36037 REV A REPAIR WITH MATERIAL 707576 .100 INCH REPAIR ANGLE SIZE 6.125 INCH BY 3.25 INCH AND REF UPS EO NR B747-5740-33436-A.

Part: RIB — CRACKED (RT WING) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET FOUND CRACKED. RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.

Part: FITTING — CRACKED (SPOILER) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - NR 8 SPOILER 'H' FTG I/B LWR LUG FOUND CRACKED. RT WING NR 8 SPOILER 'H' FTG I/B LOWER LUG REPAIRED AS PER RS R-57-51-36307 REV A REPEAT DETAILED VISUAL INSPECTIONS IS REQUIRED AS PER RS R 57-51-36307 REV A REPAIR WITH MATERIAL 707576 .100" REPAIR ANGLE SIZE 6 X 3.125 INCH REF UPS EO B747-5740-33436-A.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D RT WING - I/B FORE FLAP TRAILING EDGE I/B LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.

Part: SEAL — DAMAGED (TE FLAP) · airframe 72,472 hrs · 12,526 cycles

INSPECTION TYPE:D DMI C397322 RT WING MISSING MID - FLAP T/E FLAP TO FUSELAGE SEAL. ORIGINAL COMPRESSION SEAL ASSY BETWEEN FROM CUSTOMER. VISUAL INSP PERFORMED SUPPORT TUBES FOUND WORN AND SUPPORT WEB CRACK FOUND. SUPPORT TUBES REPLACED AS PER SRM 57-52-01. SUPPORT WEB REPAIRED AS PER SRM 51-70-11 FIG 1, REV 11. COMPRESSION SEAL ASSY REINSTALLED & OPERATION CHK CUTOUT AS PER MM 57-52-01 AND 27-51-00.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A HOLE IN FUSELAGE 40 INCHES FWD OF LWR AFT CARGO DOOR BS 1770, BETWEEN STRINGERS 28R & 29R. FABRICATED PATCH PER EO B747-5330-31394A, AND SRM 53-00-01 OUT OF 2024 -T-3 .125 CLEANED DAMAGE ON A/C REPAIRS MATERIAL AND A/C ETCHED, ALODINE & PRIMED PER SRM 51. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REPAIR 1 DETAIL III USING HI-LOC HL111VAZ8-6 HL11VAZ8-6. SEALANT 870 BY 1/2 IAW EO B747-5330-31394A, M5100-21238B2, M-5100-19877-D. RCD C/W.

Part: SLIDE — NO TEST (LEFT SIDE)

INSPECTION TYPE:N/A WHILE ATTEMPTING UPPER DECK SLIDE DEPLOYMENT FOR FAA, LEFT SIDE SLIDE FAILED TO DEPLOY IN THE AUTOMATIC POSITION. FOUND DOOR ASSIST BOTTLE SQUIB PREVIOUSLY BLOWN. REMOVED AND REPLACED DOOR ASSIST BOTTLE. EMERGENCY ESCAPE SLIDE DEPLOYED NORMALLY DURING 2ND AUTOMATIC TEST.

Part: FRAME — CRACKED (BS 1180)

LT BS 1180 TENSION TIE FOUND CRACKED AT FRAME MORE THAN O.200 INCH. LT BS 1180 TENSION TIE FRAME REPLACED PER SRM 53-40-07.

Part: FILLER — CRACKED (FUSELAGE) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS 1140 LT TENSION TIE UPPER & LWR CLIP FILLER CRACKED. BS 1140 LT TENSION TIE UPPER & LWR CLIP FILLER REPLACED PER SRM 53-40-30 F FIG 201.

Part: TENSION TIE — CRACKED (FUSELAGE)

BS 1180 TENSION TIE LT FWD SIDE CRACKED, BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FAILSAFE — CRACKED (RH BS 1140)

INSPECTION TYPE:C RT BS 1140 TENSION TIE FAIL SAFE CHORD CRACKED ABOUT O.030 INCH. RT BS 1140 TENSION TIE FAIL SAFE CHORD REPLACED PER SRM 51-70-11.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS1180 TENSION TIE LT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-31 FIG 201.

Part: TENSION TIE — CRACKED (BS 1180)

INSPECTION TYPE:C BS 1180 TENSION TIE LT AFT SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FRAME — CRACKED (BS 1140)

INSPECTION TYPE:C RT BS 1140 TENSION TIE FRAME CRACKED MORE THAN 0.060". RT BS 1140 TENSION TIE FRAME REPLACED PER SRM 53-40-07.

Part: FRAME — CRACKED (BS 1140) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF LT BS 1140 TENSION TIE FRAME CRACKED. LT BS 1140 TENSION TIE FRAME REPAIRED PER SRM 53-40-07.

Part: TENSION TIE — CRACKED (BS 1140)

INSPECTION TYPE:C BS 1140 TENSION TIE LT AFT SIDE CRACKED. BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF LT BS 1140 TENSION TIE FRAME FAIL/SAFE CHORD CRACKED. LT BS 1140 TENSION TIE FRAME FAIL/SAFE CHORD REPLACED PER SRM 51-70-11.

Part: FRAME — CRACKED (BS 1140) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF RT BS1140 TENSION TIE FRAME CRACKED MORN THAN 0.060 INCH. RT BS 1140 TENSION TIE FRAME REPLACED PER SRM 53-40-07.

Part: TENSION TIE — CRACKED (BS 1140)

BS 1140 TENSION TIE RT AFT SIDE FOUND CRACK, BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS 1140 TENSION TIE RT AFT SIDE FOUND CRACK. BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FAILSAFE — CRACKED (BS 1140)

INSPECTION TYPE:C LT BS 1140 TENSION TIE FRAME FAIL SAFE CHORD CRACKED. LT BS 1140 TENSION TIE FRAME FAIL SAFE CHORD REPLACED PER SRM 51-70-11.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS1180 TENSION TIE LT AFT SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: TENSION TIE — CRACKED (BS 1180)

INSPECTION TYPE:C BS 1180 TENSION TIE FOUND CRACK AT RT AFT SIDE. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: TENSION TIE — CRACKED (BS 1180)

INSPECTION TYPE:C BS 1180 TENSION TIE RT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FILLER — CRACKED (FUSELAGE) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS 1140 RT TENSION TIE UPPER & LWR CLIP FILLER CRACKED. BS 1140 RT TENSION TIE UPPER & LWR CLIP FILLER REPLACED PER SRM 53-40-30 I FIG 201.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF BS 1180 TENSION TIE RT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201.

Part: FRAME — CRACKED (BS 1180) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF LT BS1180 TENSION TIE FOUND CRACKED AT FRAME MORN THAN 0.200 INCH. LT BS 1180 TENSION TIE FRAME REPLACED PER SRM 53-40-07.

Part: FRAME — CRACKED (BS 1180)

INSPECTION TYPE:C RT BS 1180 TENSION TIE FRAME CRACKED ABOUT 0.040 INCH. RT BS 1180 TENSION TIE FRAMED REPLACED PER SRM 53-40-07, REPAIR 4.

Part: FRAME — CRACKED (BS 1180) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF RT BS 1180 TENSION TIE FRAME CRACKED ABOUT 0.040 INCH. RT BS 1180 TENSION TIE FRAME REPLACED PER SRM 53-40-07 REPAIR 4.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF AFT CARGO TRACK SECTION CORRODED. CORRODED TRACK SECTION CUT AND REPLACED PER SRM 53-00-52.

Part: DOUBLER — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A LEFT BS 1120 TENSION TIE FRAME DOUBLER CRACKED ABOUT 0.030 INCH. LEFT BS 1120 TENSION TIE FRAME DOUBLER REPLACED.

Part: FRAME — CRACKED (BS 1140)

INSPECTION TYPE:C LT BS 1140 TENSION TIE FRAME CRACKED. LT BS 1140 TENSION TIE FRAME REPAIRED PER SRM 53-40-07.

Part: DOUBLER — CRACKED (BS 1120 FRAME) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF LT BS1120 TENSION TIE FRAME DOUBLER CRACKED ABOUT 0.030 INCH. LT BS 1120 TENSION TIE FRAME DOUBLER REPLACED PER 65B25837 PL AND DWG.

Part: FRAME — CRACKED (BS 1120) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF RT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1120 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07 REPAIR 1.

Part: FRAME — CRACKED (BS 1160)

INSPECTION TYPE:C RT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT .250 INCH. RT BS1160 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07. REPAIR 3.

Part: FRAME — CRACKED (BS 1120)

INSPECTION TYPE:C RT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1120 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07, REPAIR 1.

Part: FRAME — CRACKED (BS 1120)

INSPECTION TYPE:C LT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.500 INCH LT BS 1120 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07 REPAIR 1.

Part: FRAME — CRACKED (BS 1160)

INSPECTION TYPE:C LT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT 0.400 INCH. LT BS 1160 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07 REPAIR 3.

Part: FRAME — CRACKED (BS 1160) · airframe 70,344 hrs · 12,159 cycles

INSPECTION TYPE:BCF RT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1160 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07 REPAIR 3.