N930FD

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 67,924 hrs · 25,770 cycles

R1 SLIDE EXTERIOR EMERGENCY EXIT LIGHT INOP. SHGN 15JAN25 14:01 BNA AMM: 33-51-06-2-1 WDM: 33-51-12 PG 11 SH 1FX1 IPC: 33-51-07-100 RELAMPED R1 SLIDE LIGHT ASSY L38, NO HELP...CHECKED FOR VOLTAGE, NO POWER AT TERMINAL. CONTINUITY CHECK LIGHT ASSY THRU BULB GOOD...CONTINUITY THRU PWR SUPPLY GOOD AT TERMINAL ENDS. CONTINUITY FROM CONNECTOR PIN 9 TO GRD GOOD. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-07-2-0. OPS CHECKS GOOD. OK FOR SERVICE.

Part: GUST LOCK — DAMAGED (L1 DOOR) · airframe 67,628 hrs · 25,537 cycles

GUSTLOCK BROKEN ON L1 DOOR REPLACED THE NO 1 (LH) PASSENGER DOOR HOLD OPEN LOCK COLLAR PER ABOVE AMM. OK FOR SERVICE.

Part: FITTING — DAMAGED (RT WING) · airframe 67,437 hrs · 25,398 cycles

DURING INSP OF R/H WING OUTER-UPPER SKIN FITTINGS AND DIAGONAL BRACE FASTENNERS AND SHIM PER E 5730-E0340076 L P12 STEP:3 HOLE 14 FASTENNER FOUND SECOND OVER SIZE. REPAIR/COMPLIED WITH FEDEX EA# F-5730-T0378078 P1 TITLE: WINGS- PLATES AND SKIN- RH WING - PYLON #2 DRAG FITTING UPPER SKIN 2ND OVERSIZE FASTENERS REPAIR. MAJOR REPAIR

Part: ACTUATOR — FAILED (ZONE 700) · airframe 67,257 hrs · 25,262 cycles

AFTER TAKEOFF & GEAR RETRACT APPEARED TO COMPLETE, A SHORT BUMP NOISE & FEEL UNDER COCKPIT, BUT ALL INDS APPEARED NORMAL. ON MLG EXTENSION, A SIGNIFICANT BANG & THUD, FOLLOWED BY SLIGHT VIBRATION & NOISE, DISCONTINUED APPROACH. HAD NO NLG GREEN DOWN LIGHT, A MLG DOORS & MLG DISAGREE CAUTION EICAS MESSAGE. AFTER QRH, NO INDS CHANGED. DECLARED AN EMERGENCY & LANDED UNEVENTFULLY, BROUGHT TO A FULL STOP. TOWED TO GATE. FOUND NLG RETRACT ACTUATOR ROD END BROKEN. R&R NLG MAIN RETRACT ACTUATOR IAW AMM 32-34-01-4, LEAK CK NORMAL. R & R BOTH NLG 1 & 2 LOCKED SENSORS S10065 & S10078, ALL MLG INDICATION SYS CK NORMAL IAW AMM 32-61-03-2. R & R NLG IAW AMM 32-35-00-5 32-51-00-5-3 & WC 3205600-00-02.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 67,087 hrs · 25,145 cycles

ABOUT 2 MINUTES AFTER LEVEL OFF AT FL330, CABIN ALTITUDE MASTER WARNING MESSAGE APPEARED. ABOUT 1 MINUTE LATER, CABIN AUTO INOP MASTER CAUTION MESSAGE APPEARED. CABIN ALTITUDE CLIMBED TO ABOUT 14,000 . STATUS MESSAGES CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 APPEARED. COMPLIED WITH QRC AND QRH. FACT 25JUL23 10:37 MEM FIM: FAULT TREE 802 FIG 103 FIM: FAULT TREE 810 FIG 108 AMM: 21-31-02-4 AMM: 21-31-04-4 AT GATE EICAS DISPLAYED CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED BITE OF CONTROLLERS UING FIM 802 FIG103. ALL TEST PASSED. REMOVED AND REPLACED #2 AUTO CONTROLLER PRECAUTIONARY PER ABOVE REFERENCE.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,169 hrs · 24,504 cycles

FUSELAGE CUT-OUT FOR ACCESS DOOR 313AL AFT FRAME CORRODED. EVALUATED CORROSION AT FUSELAGE CUT-OUT FOR ACCESS DOOR 313AL AFT FRAME AND FOUND TO BE CORRODED 100% OUT OF LIMITS IAW SRM 53-00-02-1A FIG. 101 DET.II, REMOVED AND REPLACED OUTER CHORD FX148N1601-9 IAW DWG 148N1601 SH.1 REV. B, MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 66,169 hrs · 24,504 cycles

ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VTMAE TRAVELER #T22/1604260 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 66,169 hrs · 24,504 cycles

L/H LOWER LOBE FUSE SKIN AT STA. 247 AT STR23L HAS A CREASE BULGE ON FWD SIDE OF FRAME, NEEDS EVAL. EVALUATED DENT AT STA 247 S-23L, DAMAGE LOCATION IS LESS THAN 0.5" AWAY FROM FRAME AT STA 247, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101, DET. III, REPAIRED SKIN 141N3215-2 AT STA 247, S-23L IAW SRM 53-00-01-2R REPAIR 29, FIG 201 (CATEGORY B REPAIR),PART MARKED REPAIR PER GMM 07-0-1001, REPAIR LOCATION IS AT STA 247 BETWEEM S-23L TO S-26L MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,169 hrs · 24,504 cycles

FUSELAGE SKIN BETWEEN ACCESS DOOR 313AL CUT-OUT AND APU COMPARTMENT, INNER SURFACE IS CORRODED. REMOVED CORROSION FROM FUSELAGE SKIN BETWEEN ACCESS DOOR 313AL CUT-OUT AND APU COMPARTMENT INNER SURFACE IAW SRM 51-10-02-0G, 0.035" MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A, FIG 101, DET.II. REMOVED AND REPLACED 148N3611-10 SKIN IAW SRM 51-40-02-0G AND DWG. 148N8402,148N3601, MAJOR REPAIR

Part: PUMP — FAILED (HYD SYSTEM) · airframe 65,046 hrs · 23,675 cycles

EMERGENCY DECLARED. LT HYD QTY AMBER CAS FOLLOWED LT ENGINE PUMP AMBER CAS, FOLLOWED BY LT HYD RESERVOIR AND LOSS OF FLUID .01 RF SHOWING. ALTN FLAP AND ALTN GEAR EXTENSIONS. T/S FOUND HYD FLUID COMING FROM THE NR 1 ENGINE HYD PUMP SEAL DRAIN WHILE SERVICING LEFT HYD SYTEM TO FULL. REMOVED AND REPLACED LEFT ENGINE DRIVEN HYD PUMP, PER MM 29-11-05-4-1 PER MM 29-11-00-2 STEP 1E CONDITION NR 1 NOT NECESSARY TO FLUSH SYSTEM AS A RESULT OF PUMP SEAL PROBLEM. RAN ENGINE, LEAK, AND OPERATIONS CHECK OF PUMP NORMAL. CYCLED ALL FLT CONTROLS AND BRAKES. ALL SYSTEMS OPERATIONS CHECK NORMAL A/C OK FOR SERVICE. PUMP MPN 887673, S/N MX-548672 MFG VICKERS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,527 hrs · 23,340 cycles

AFT CARGO COMPT. AFT BULKHEAD INTERCOSTAL BETWEEN FLOOR BEAMS BS. 1681.8 AND BS. 1701, IS CRACKED AT FWD SIDE ON RADIOUS AT BS. 1681.8 BL-0. REMOVED INTERCOASTAL CHANNEL STA 1681.8 TO 1701 BL0 IAW B757 SRM 51-40-02. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW CHANNEL IAW B757 SRM 51-40-05, 51-40 -02 AND BOEING DWG 146N5180 REV CP AND REV -

Part: STRAP — MISSING (FUSELAGE) · airframe 64,527 hrs · 23,340 cycles

AFT CARGO COMPT. AFT BULKHEAD FLOOR BEAM BETWEEN BS 1681.8 AND BS 1701,FLOOR BEAM IS MISSING STABILIZER STRAP ON INTERCOSTAL WEB LOWER FLANGE AT BL-0. FABRICATED, LOCATED, DRILLED AND INSTALLED STABILIZER STRAP STA 1681.8 TO 1701 BL0 IAW BOEING DWG 146N5192 REV G, REV - AND B757 SRM 51-40-02

Part: LINE — LEAKING (HYD SYSTEM) · airframe 64,438 hrs · 23,277 cycles

AFTER TAKEOFF, RAISED GEAR HANDLE TO UP. RECEIVED A GEAR DOORS EICAS AND DOORS LIGHT. COMPLED WITH QRH. NO OTHER ASSOCIATED PROBLEMS. PERFORMED B757 FIM 32-09 FT804, PSEU BITE TEST, NO HISTORY FAULTS STORED OR CURRENT FAULTS PRESENT AT THIS TIME. FAULT IS NOT PRESENT ON EICAS AT THIS TIME. SUSPECT HYD LEAK ON RT GEAR WAS REASON FOR GEAR DOORS EICAS MESSAGE. TEMP INSTALLED 3 FLEX HYD LINES IN PLACE OF RIGID LINES IN ORDER TO CONTINUE T/S OTHER DISCREPANCIES. BLED THE TEMP INSTALLED LINES GOING TO THE TRUCK POSITION ACTUATOR. ERS 20-00566 IS SUBMITTED FOR APPROVAL TO USE THE 3 HYD FLEX LINES FOR REPAIR OF LEAKING RIGID LINE ON RT MLG. AWAITING RESPONSE. TEMP FLEX LINE INSTALLED FOR RT GEAR TILT ACTUATOR OK PER E.A. F-2902-T0352405 COMPLIED WITH INSTALLATION OF 3 EA HYD FLEX LINES, P/N 171141-6CR-0360, 171141-6CR-0120, AND 171141-6CR-0300, WITH 2 UNIONS MS21902-6J, IN PLACE OF RIGID LINE, P/N 271N6611-1020, ON RT MLG REF EA F-2902-T0352405 PT 1 AND B757 AMM 20-10-09-8. LEAK CHECK GOOD AT THIS TIME.

Part: CARGO — FUMES · airframe 64,020 hrs · 22,986 cycles

DURING CLIMBOUT HAD STRONG UNKNOWN FUMES IN COCKPIT FOR 2-3 MINUTES. THAN SEEMED TO BE DISSAPPATING, BUT AT LEVEL OFF AT FL 380 STARTED COMING BACK. DECLARED AN EMERGENCY AND DIVERTED. PER B757 FIM 21-00-01-3 VERIFIED ALL ENG OIL AND HYD NOT OVER SERVICED. NO EXTERNAL LEAKING. FOUND CHEMICAL SHIPMENT CAUSING STRONG ODOR. SHIPMENT REMOVED FROM AIRCRAFT A/C, OPENED FOR APROX 6 HOURS. NO FUMES NOTICEABLE. RAN A/C PER B757 JRH AND MM 71-00-00-5-3 TO CLOSE COMPRESSOR BLEED VALVES. NO FUMES ON EITHER ENG. A/C OK FOR SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 63,898 hrs · 22,905 cycles

DURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. NOTICED OUTFLOW VALVE IN FULL CLOSED POSITION WITH RIGHT PACK OPERATIVE WHICH SHOULD HAVE PRESSURIZED THE AIRCRAFT WITH NO PROBLEM. DM REMOVED AND REPLACED RT PACK FLOW CONTROL SHUTOFF VALVE. REF MM 21-51-01-2. OPS CHECK AND TESTED GOOD. RAN PACKS WITH HUFFER AT 48PSI, BOTH PACKS OPERATED NORMAL. OUTFLOW VALVE OPERATED NORMAL. AIRCRAFT GOOD FOR SERVICE. PART OFF MANUFACTURER: PNEUMATICS SYSTEMS PART OFF:396480-1, FLOW CONTROL VALVE,SERNO OFF 313`

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 63,896 hrs · 22,904 cycles

PDIS 930 21-30 7416 10MAY19 MEM OPEN U LOGPAGES:3112369 DURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. NOTICED OUTFLOW VALVE IN FULL CLOSED POSITION WITH RIGHT PACK OPERATIVE WHICH SHOULD HAVE PRESSURIZED THE AIRCRAFT WITH NO PROBLEM. /DM PART 10MAY19 16:08 MEM U IDENTIFIED PARTS (W/KIT)EQUIP COOLING OVBD MPN: 60B40041-3 CPN: 2112858 QTY: 1 PART 10MAY19 16:08 MEM U ORDER PART MPN: 60B40041-3 CPN: 2112858 QTY: 1 ICT: 915963 REMOVED AND REPLACED RT PACK FLOW CONTROL SHUTOFF VALVE. REF MM 21-51-01-2. OPS CHECK AND TESTED GOOD. RAN PACKS WITH HUFFER AT 48PSI , BOTH PACKS OPERATED NORMAL. OUT FLOW VALVE OPERATED NORMAL. AIRCRAFT GOOD FOR SERVICE. PART OFF MANUFACTURER: PART # OFF: 396480-1, FLOW CONTROL VALVE, SERNO OFF 313 REF WRI 77-15/7417 R&R'D N3 TACH TRANSMITTER. THE SPEED SENSOR CAUSED NUMEROUS ADDITIONAL WRITE-UPS.

Part: INSERT — UNSECURE (L1 DOOR) · airframe 63,586 hrs · 22,709 cycles

FOUND L1 DOOR SLIDE COVER FWD UPPER LATCH, UNLATCHED. REPAIRED POTTED INSETS REF. AMM 25-00-00-8. REINSTALLED L-1 DOOR SLIDE COVER, DOOR OPS CHECKS NORMAL REF AMM 52-11-02-4.

Part: BOTTLE — INOPERATIVE (R1 DOOR) · airframe 63,337 hrs · 22,555 cycles

ON POST FLIGHT FOUND R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE DEPLETED. REPLACED R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE PER AMM 52-11-30-4. A/C OK FOR SERVICE.

Part: SWITCH — FAILED (LE SLAT) · airframe 63,082 hrs · 22,351 cycles

ON SELECTING FLAPS 15 FROM 5, LE SLAT ASYMETERY CAUTION MESSAGE WAS RECEIVED. LE SLAT DISAGREE DISPLAYED AT THE COMPLETION OF THE QRH THE FLAPS WERE SELECTED INTO 30 POSITION VIA THE ELECTRIC. R & R THE LT INBD SLAT LOSS SWITCH IAW MM 27-81-41-4. OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — OVERSERVICED · airframe 62,997 hrs · 22,296 cycles

DURING A MAIN DECK CARGO FIRE PROTECTION CHECK, SMOKE CAME OUT BOTH FLIGHT DECK VENT DIFFUSERS. RAN QRH AND SMOKE CLEARED. OPERATED PACKS WITH ENGINES AS PNUEMATIC SOURCE IAW JRH. COULD NOT DUPLICATE SMOKE IN COCKPIT. OPERATED PACKS WITH APU AS PNEUMATIC SOURCE IAW AMM 49-11-00-2, AND 21-00-00-2. COULD NOT DUPLICATE SMOKE IN COCKPIT. PERFORMED CARGO ISOLATION OPS CHECK IAW AMM 21-51-00,504. COULD NOT DUPLICATE SMOKE IN COCKPIT. PERFORMED FIM 21-00-01-3, PROCEDURE 4, DUE TO PIREP SMOKE CLEARED AFTER QRH, PRIOR TO LANDING. NO DEFECTS NOTED. REMOVED AND REPLACED HYDRAULIC RESERVOIR PRESSURIZATION MODULE AND LEFT HYD HYDRAULIC HYDRAULIC RESERVOIR DEPRESSURIZATION VALVE AS A PRECAUTION DUE TO THE LT HYDRAULIC OVERFULL BEING DISPLAYED ON EICAS AND POST FLIGHT ODOR OF HYDRAULIC FLUID IN THE THE COCKPIT. AIRCRAFT OK FOR FLIGHT.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,996 hrs · 22,295 cycles

DURING SANDING, FOUND LEFT WING T/E OTBD AFT FLAP UPPER SURFACE TABS DELAMINATED, WS 481 AFT OF THE NR 3 SPOILER. ACCOMPLISHED PERMENANT REPAIR IAW SRM 57-53-01-2R, TABLE II, AND SRM 51-70-04, PAR 5A1.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,996 hrs · 22,295 cycles

LEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 138 - 143, ONE DENT FOUND OUT OF LIMITS. REMOVED DAMAGE, APPLIED PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,996 hrs · 22,295 cycles

LEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HAD TWO DENTS, HSS 127 - 133 AND FOUND TO BE OUT LIMITS. CUT OUT THE DAMAGE & APPLIED PERMANENT REPAIR IAW SRM 51-70-10-2R, REPAIR 3 & 4.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,996 hrs · 22,295 cycles

LEFT HORIZONTAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT SPAR HSS 124 - 130 DENTED OUT OF LIMITS. REMOVED DAMAGE, APPLIED A PERMENANT REPAIR IAW SRM 51-70-10-2R, REPAIRS 3 & 4.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,996 hrs · 22,295 cycles

LEFT HORIZONAL STAB UPPER SKIN BETWEEN AUX SPAR AND FRONT STAB 144 - 150 HAD TWO DENTS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-70-10-2R, REPAIR 3 & 4,

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 62,996 hrs · 22,295 cycles

CRACK GOING OUT FROM SKIN AFT SIDE OF THE NR 1 SLAT FROM FASTENER. COMPLIED WITH EA F-5750-T0339279 P1. FABRICATED TWO REPAIR DOUBLERS, FILLERS & INSTALLED IAW SRM 57-43-01-2R, REPAIR 4.

Part: FLOORBEAM — DAMAGED (BS 580) · airframe 62,996 hrs · 22,295 cycles

MAIN CABIN FLOORBEAM AT BS 580 FWD FLANGE, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339086, P1.

Part: FLOORBEAM — DAMAGED (BS 600) · airframe 62,996 hrs · 22,295 cycles

MAIN CABIN FLOORBEAM BS 600 FLOOR PANEL MOUNT HOLE AT APPROX. LBL 40 IS OBLONG. REPAIRED IAW EA F-5310-T0339087.

Part: FLOORBEAM — DAMAGED (BS 620) · airframe 62,996 hrs · 22,295 cycles

MAIN CABIN FLOORBEAM FWD FLANGE BS 620, LBL 40 HOLE IS OBLONG. REPAIRED IAW EA F-5310-T0339088.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,996 hrs · 22,295 cycles

MAIN CABIN FLOORBEAM ATTACH FITTING AT BS 580, LBL 45 CRACKED IN AFT UPPER FLANGE. REPAIRED IAW EA F-5310-T0338866 P1.

Part: PRESSURE SWITCH — FAILED (HYD SYSTEM) · airframe 62,654 hrs · 22,070 cycles

RECEIVED A LT HYD SYS PRESSURE EICAS MESSAGE, ALONG WITH RUDDER RATIO EICAS MESSAGE ON EXTENDING FLAPS TO 1. LEFT HYDRAULIC QTY 1.0, LEFT HYDRAULIC PRESSURE 3100 PSI. R & R THE LT HYD SYS PRESSURE SWITCH IAW AMM 29-11-17-4. LEFT HYD PRESSURE SWITCH OPS AND LEAK CHECKED NORMAL IAW AMM 29-11-00-5. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,424 hrs · 21,898 cycles

FOUND DOOR 1R EMERGENCY LIGHTS NOT COMING ON DURING TEST. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK PER AMM 33-51-07-2, OPS CHECK NORMAL. A/C OK FOR SERVICE.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,478 hrs · 21,230 cycles

RIGHT WING INBD FLAP, OTBD TE, UPPER SKIN HAS AREA OF DELAMINATION. HOT BONDED PERMANENT REPAIR ONTO RT WING I/B FLAP O/B TE UPPER SKIN IAW SRM 57-53-01-2R REPAIR 1 FIG 201 DETAIL 1 AND SRM 51-70-10-2R REPAIR 4. POST REPAIR TAP TESTED AREA IAW SRM 51-10-06-2R REPAIR 1. NO DEFECTS NOTED.

Part: SHEAR WEB — CORRODED (BS 1684-1694) · corrosion level 2 · airframe 61,478 hrs · 21,230 cycles

MAIN DECK SHEAR WEB BS 1684 - 1694, LBL 60 TO RBL 60, HAS CORRODED AREAS. REMOVED CORROSION, AND FOUND TO BE E OUT OF LIMITS IAW SRM 53-60-51-1A FIG 101 DETAIL III TABLE 102. FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 53-60-51-2R FIG 201 DETAIL 1 ALTERNATIVE 1.

Part: SHEAR PLATE — CORRODED (BS 410-440) · corrosion level 2 · airframe 61,478 hrs · 21,230 cycles

MAIN CARGO COMPARTMENT, FLOOR SHEAR PLATE CORRODED, BETWEEN BL 0 - LBL 24, BS 410 - 440. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 757-200, FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM. FOUND TO BE WITHIN LIMITS IAW SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,478 hrs · 21,230 cycles

RT INBD AFT FLAP HAS DELAMINATION AT OTBD AREA. EVALUATED AREA TO BE .025" DEPTH X2.5 ' LENGHT AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101. ACCOMPLISHED PERMANENT REPAIR TO RT I/B AFT. FLAP UPPER SKIN IAW SRM 57-53-01-2R FIG 201,TABLE II AND SRM 51-70-04-0G PAR 5A2A AND SRM 51-70-17-0G PAR 4A2.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 606 hrs · 20,599 cycles

LEFT FRONT ENTRY DOOR SLIDE LIGHT INOPERATIVE. REPLACED BULB GE 767 IAW MM 33-51-06-2-1. LIGHT OPERATIONS CHECKED NORMAL, OK FOR SVC.

Part: STOWAGE BOX — FAILED (COCKPIT) · airframe 60,425 hrs · 20,356 cycles

AT BLOCK IN POST FLIGHT CHECK FOUND CAPTAIN`S O2 MASK WOULD NOT TEST. R & R CAPTAIN`S O2 STORAGE BOX IAW MM 35-11-51-4-99. OPERATIONS & LEAKS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,385 hrs · 20,328 cycles

EMERGENCY LIGHTS UNARMED ANNUNCIATOR LT HALF UNLIT. REMOVED & RE LAMPED EMER LIGHT UNARMED ANNUNCIATOR LIGHT. OPERATIONS CHECKED GOOD IAW MM 33-13-00-2. ACFT OK TO CONTINUE.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 60,335 hrs · 20,292 cycles

UPON ARRIVAL, L1 DOOR WAS OPENED WITH THE SLIDE ARMED. SLIDE CAME OUT BUT DID NOT DEPLOY. MEL 19 NOV 14 13:59 RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 22 NOV 14 MEL 52-11-01-A. L1 DOOR SLIDE MISSING, IDENTIFY INOPERATIVE OR MISSING. REMOVED SLIDE FROM L1 DOOR & STORED BEHIND THE RCB. SLIDE DEACTIVATION PIN IS INSTALLED. ALSO, L1 DOOR POWER RESERVOIR IS DEACTIVATED. THIS WAS REQUIRED IAW AMM 25-66-01-4 FOR SLIDE REMOVAL.

Part: WINDOW — FAILED (COCKPIT) · airframe 60,043 hrs · 20,026 cycles

LEVEL AT 390, FIRST OFFICER`S WINDOWS SHATTERED. REPLACED WINDOW.

Part: SLIDE — UNSECURE (ENTRY DOOR) · airframe 59,799 hrs · 19,805 cycles

LEFT ENTRY DOOR SLIDE PARTIALLY UNSTOWED. COMPLIED WITH ESCAPE SYS INSPECTION & CHECKED IAW MM 25-66-01-6. L1 DOOR OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (R1 SLIDE LIGHT) · airframe 59,332 hrs · 19,375 cycles

R1 SLIDE LIGHT WILL NOT ILLUMINATE WHEN THE DOOR IS ARMED. REPLACED LAMPS IAW STD MAINT PRACTICES, OPS CHECKED OK.

Part: COVER — DETACHED (L1 DOOR SLIDE) · airframe 59,164 hrs · 19,217 cycles

L-1 DOOR SLIDE COVER, BOTTOM SEAL IS DETACHED FROM COVER. REINSTALLED L1 ESCAPE SLIDE COVER IAW AMM CHPT 25-66-00-2. SLIDE COVER LOCKED AND SECURED, ACFT OK FOR SERVICE. FINAL CLOSED.

Part: SHEAR TIE — CRACKED (BS 1300 S20L) · airframe 58,694 hrs · 18,736 cycles

UPON REMOVAL OF WING TO BODY SUPPORT, FOUND SHEAR TIE CRACKED AT STA 1300, STR 20L. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG NR 140N2002-1059 AND SRM 51-30-01 AND 51-40-5. INSTALLED SHEAR TIE IAW SRM 51-40-02.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 58,391 hrs · 18,552 cycles

LENS CAP ASSY ON EMERGENCY LIGHT UNARMED ANNUNCIATOR BROKEN. R & R EMERGENCY LIGHT UNARMED ANNUNCIATOR LENS CAP ASSY, DIODE/FUSE CARD AND DRAWER ASSY. OPS CHECKED GOOD WITH EMERGENCY LIGHTS ARMED/UNARMED. AMM 33-16-02-2.

Part: CONNECTOR — DAMAGED (TE FLAPS) · airframe 57,448 hrs · 18,006 cycles

PASSING 17000FT, FLAPS RETRACTED, CLEAN CONFIGURATION, RECEIVED L/E SLAT ASYM EICAS ALONG WITH T/E CAUTION LIGHT. AT DESTINATION, FLAPS COULD NOT EXTEND WITH HYD EXTENDED FLAPS IAW QRH ELE WITH ALTN FLAP SWITCH. PERFORMED BITE ON ALL 3 FSEU'S. NO CURRENT FAULTS, BUT FOUND "SLAT LOSS" ON FSEU NR1 ON LAST FLIGHT LEG. USED PROCEDURE FIM 27-81-00, FIG 105. NO GROUND FOUND AT PIN B6 ON CONNECTOR D3312B. IAW FIM, FSEU NR1 NEEDS REPLACED. R & R NR1 FSEU IAW MM 27-51-01. SYS OPERATES GOOD, WITH NO FAULTS. CAT STATUS DOWNGRADED TO CHECK III FOR ALL THREE A/P'S.

Part: FRAME — DAMAGED (ZONE 100) · airframe 57,415 hrs · 17,967 cycles

LOWER LOBE- AVIONICS COMPT FWD OF NWW- FRAME 231.25 HAS DOOR LOCK PIN IMPACT DAMAGE AT BL "0", ALSO DOOR LOCK FITTING ATTACHED TO FRAME DAMAGED. REPAIRED FRAME 231.25 BL "0" AT AVIONCS COMPT FWD OF NWW IAW EA F-5310-141195, FUSELAGE STA 231.25, LOWER LOBE FRAME INNER CHORD DAMAGE AT BL 0. CATEGORY " A ", MAJOR REPAIR.,

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 57,415 hrs · 17,967 cycles

NR 1 CARGO DOOR LOWER FRAME HAS 3 GOUGES BLENDED GOUGES ON NR 1 CARGO DOOR LOWER FRAME AND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101 DETAIL VII. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

INCOMING FASTNER HOLES IN FLOORBEAM UPPER FLANGE INTERFERS WITH 657N3332-2 SEAT TRACK INSTALLATION AT STA 620, 640, 660. RBL 58.22 AT STA 620, 640, AND 660 RBL 58.22. FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE EA 757-5335-16-F2773 REV- DATED JUL 9, 2010. MAJOR REPAIR

Part: SKIN — CRACKED (NR 7 SLAT) · airframe 57,415 hrs · 17,967 cycles

NR7 SLAT UPPER SURFACE HAS 2 EA CRACKS FOUND NR 7 SLAT TO BE OUT OF LIMITS IAW SRM 57-43-01 FIG 101. NR 7 SLAT REMOVED AND REPLACED ON WO 00047415, N01466. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — MISALIGNED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

SHORT EDGE MARGIN CONDITIONS FOUND IN 146N5044-4 FLOORBEAM UPPER FLANGE AT STA 1280, RBL 24.75 AND RBL 45.50 AT STA 1280, RBL 24.75 AND 45.5 FLOORBEAM UPPER FLANGE REPAIR WAS ACCOMPLISHED ON MAE EA 757-5365-16-F2762, REV- DATED JUN 24, 2010. MAJOR REPAIR.

Part: STRINGER — DAMAGED (ZONE 100) · airframe 57,415 hrs · 17,967 cycles

ELONGATED HOLE FOUND IN INCOMING STRINGER AT STA 437, S-22L AT STA 437, S-22L STRINGER REPAIR WAS ACCOMPLISHED ON MAE EA 757-5332-16-F2732, REV- DATED JUN 15, 2010. MAJOR REPAIR.

Part: SKIN — MISALIGNED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

2 EA OVERSIZED FASTNER HOLES ON OUTER LOWER EXTERIOR FUSELAGE SKIN AT STA 501, WL 220, LBL 70. DWG REQUIREMENT- .159 TO .165 DIAM. ACTUAL SIZE .191 2EA FASTENER HOLES ON OUTER LOWER EXTERIOR FUSELAGE SKIN PN 143N8161-2 AT STA 501, WL 220, LBL 70 WERE OVERSIZED. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 460) · airframe 57,415 hrs · 17,967 cycles

DISCREPANT FASTNER HOLE IN FLOORBEAM AT STA 460, LBL 68 AT STA 460, LBL 68. FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE EA 757-5335-16-F2740 REV- DATED JUN 17, 2010. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

1EA INCOMING FASTNER HOLE INTERFERS WITH INSTALLATION OF 657N3329-2 SEAT TRACK AT STA 640, LBL 58.22 AT STA 640, LBL 58.22 FLOORBEAM FLANGE REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE EA 757-5335-16-F2819 REV- DATED AUG 6,2010. THIS NR IS FOR TIME TRACKING PURPOSES ONLY. REF FAA FORM 8110-3, DATED SEPT 3, 2010 AND EA F-5310-141209. MAJOR REPAIR.

Part: FITTING — MISALIGNED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

POTENTIAL SHORT EDGE MARGIN CONDITIONS IN 657N3161-11 FITTING DUE TO INCOMING FASTNER HOLE LOCATIONS AT STA 1640 BETWEEN S-17L TO S-18L AT STA 1640 BETWEEN S17L TO S18L FRAME REPAIR WAS ACCOMPLISHED ON MAE EA 757-3562-16-F2757 REV- DATED JUN 22, 2010. THIS NR IS FOR TIME TRACKING PURPOSES ONLY. REF EA F-5310-142257. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

EXTERIOR SKIN UNDER ELT STA 1500-1520 SKIN IS DISTORTED COMPLIED WITH EA F-5330-142238 FUSELAGE PLATES AND SKIN-BS 1500 TO STA 1520 BETWEEN S-1 AND S-2L SKIN REPAIR. MAJOR REPAIR

Part: SKIN — DENTED (NR 9 SLAT) · airframe 57,415 hrs · 17,967 cycles

NR 9 SLAT L/E UPPER SURFACE HAS DENT REPAIRED NR 9 L/E SLAT UPPER SURFACE AT STA 594.50 APPROX 5" FWD OF T/E IAW SRM 57-43-02. FINAL REPAIR DIMENSION WAS 4" IN DIAM. CATEGORY "A" MAJOR REPAIR.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

R4 DOOR LOWER GATE, LOWER EDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG. 101 XII. REMOVED AND REPLACED R4 LOWER GATE ASSEMBLY IAW AMM 52-11-38-4. ADJUSTED R4 DOOR IAW AMM 52-11-00-5.

Part: SKIN — DENTED (BS 1520) · airframe 57,415 hrs · 17,967 cycles

REWORK- DENT WAS FOUND ON FIRST EVALUATION TO BE OUT LIMITS, WAS RE-EVALUATED AND BLOCK 26 "CORRECTIVE ACTION" STATED TO BE FOUND WITHIN LIMITS. SECOND EVALUATION DID NOT ADDRESS FIRST EVALUATION OUT OF LIMITS CONDITION "DENT IS WITHIN .5" PROXIMITY OF SHEAR TIE. ORIGINAL DISCREPANCY: EXTERNAL SKIN DENTED AT BS 1520, BETWEEN S29R/ 30. TRANSFERRED FROM N/R N00143. STRIPPED PAINT AREA, RE-EVALUATED, DENT FOUND OUT OF LIMITS IAW SRM 53-00-01, P.104, FIG 101, DETAIL 3. PROXIMITY OF DENT IS WITHIN .5" OF SHEAR TIE. DENT MEASURES L=5.7", A=1.344", Y=.042", A/Y=32. REPAIRED AREA, BS 1520, S29R/30, IAW SRM 53-00-01, P 204, TABLE 1 AND 3. CAT. "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING: INITIAL AT 37,500 FC, THEREAFTER EVERY 6,000 FC, USING HFEC.

Part: GATE — CORRODED (R1 DOOR) · airframe 57,415 hrs · 17,967 cycles

R1 DOOR LOWER GATE, LOWER EDGE HAS CORROSION. REMOVED CORROSION FROM R1 DOOR LOWER GATE AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL XII. R & R LOWER GATE ON NR N01728 IAW AMM 52-11-38. CLASSIFIED MAJOR REPAIR.

Part: GATE — GOUGED (R1 DOOR) · airframe 57,415 hrs · 17,967 cycles

R 1 DOOR LOWER GATE , FWD & AFT CORNERS HAVE GOUGES. R 1 DOOR LOWER GATE , FWD & AFT CORNERS HAVE GOUGES REMOVED GOUGES ON R1 DOOR LOWER GATE AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DETAIL XII. REPLACEMENT OF LOWER GATE ACCOMPLISHED ON NR N01728. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: GATE — CORRODED (L1 DOOR) · airframe 57,415 hrs · 17,967 cycles

L1 DOOR LOWER GATE LOWER EDGE HAS CORROSION. REMOVED L-1 DOOR LOWER GATE FOUND OUT OF LIMITS IAW SRM 51-10-02. INSTALLED L-1 LOWER GATE IAW AMM 52-11-38. PERFORMED OPERATIONAL AND ADJUSTMENT CHECKS FOUND SATISFATORY IAW AMM 52-11-00 IN C/W N00134.

Part: SKIN — DENTED (NR 7 SLAT) · airframe 57,415 hrs · 17,967 cycles

NR 7 SLAT HAS SEVERAL DENTS UPPER SURFACE. REPAIRED NR 7 SLAT IAW SRM 57-43-02, SLAT NR 7 PN 114N4005-178A, SN A2-0348, STA 341.50, BONDED 4" DOUBLER OVER DENT NR 1 DENT NR 2 IS A=.655, Y=.006, A/Y=109.1, DENT NR 2 TO BE IN LIMITS IAW SRM 57-43-02, FIG 101, DETAIL III. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1640 S5-6L) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FRAME BS 1640, BETWEEN S- 5L & S-6L GOUGED AT BS 1640 FRAME, S5-6L.

Part: SKIN — CRACKED (BS 223.5) · airframe 57,415 hrs · 17,967 cycles

DENT AT BS 223.5 ABOVE S23L , EXT FUSELAGE SKIN WAS DETERMINED " OUT OF LIMITS " AND "REWORKED TO ORIGINAL CONTOUR" BY PREVIOUS OPERATOR, SRM REQUIRES A REPAIR BE ACCOMPLISHED EVALUATED DENT. CRACK INDICATIONS NOTED PER NDTM, PT.6, 51-00-19. CRACK: 1.5", W=.002". FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. FIG.101, P.102. ACCOMPLISHED SKIN REPAIR AT BS 223.5, S23L, PER SRM 53-00-01, FIG.201, PP. 201-207. CAT. "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING: INITIAL AT 25,000 FC, THEREAFTER EVERY 6,000 FC, USING HFEC. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 755-900) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR LEFT SHEAR WEB INBD SUPPORT ANGLE, BS 755, HAS CORROSION. REMOVED CORROSION LT SHEAR WEB SUPPORT ANGLE, BS 755-900, IAW SRM 51-10-02. CHECKED LIMITS; ORIG MATL .071", LOSS: .008", REMAINING: .063". FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG.101, DETAIL 8, P.105. REMOVED SUPPORT ANGLE, INBD, LT, BS 755-900, IAW SRM 51-40-02. FABRICATED SUPPORT ANGLE USING MAT. BAC 1515-553, BATCH 0001827675, IAW DWG 143N5520-27. TREATED/PRIMED IAW SRM 51-20-01. TOPCOAT APPLIED IAW AMM 51-21-00-7. INSTALLED NEW LT, INBD, SUPPORT ANGLE, BS 755-900, IAW SRM 51-40-02. MAJOR REPAIR.

Part: WEDGE — DENTED (NR 3 SLAT) · airframe 57,415 hrs · 17,967 cycles

DENT ON NR 3 L/E SLAT UPPER SURFACE T/E WEDGE AT SLAT OSS 503.75 EVALUATED DENT ON NR 3 SLAT T/E WEDGE OSS 503.75 A=1.115 Y=.026 A/Y RATIO 42.8 FOUND TO BE OUT OF LIMITS DUE TO DELAMINATION IAW SRM 57-43-02 FIG 101 NOTE "K". REPAIRED SLAT IAW SRM 57-43-02 BONDED 4" DOUBLER OVER DENT. CLASSIFIED CATEGORY 'A' MAJOR REPAIR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,415 hrs · 17,967 cycles

RT WING INBD FLAP DENTED AT APPROX WS 369.5 LOWER SURFACE EVALUATED DENT ON RT WING INBD FLAP LOWER SURFACE WS 369.5 A=1.187 Y=.062 A/Y RATIO 19.1 FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, FIG 101, DETAIL VII. REPAIRED FLAP IAW SRM 57-53-01. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 57,415 hrs · 17,967 cycles

NR 6 SLAT LEADING EDGE HAS CREASE DENT UPPER SURFACE WS 150.5 EVALUATED DENT AND FOUND TO BE OUT OF LIMITS PER SRM 57-43-02, FIG.101, AND NOTE "K"; A=1.11, Y=.066", A/Y=16.83. REPAIRED NR 6 L/E SLAT, UPPER SURFACE, PER SRM 57-43-02, BY BONDING A 4" DOUBLER AT WS 150.50. REPAIR ACCOMPLISHED ON ASSY. REFERENCE EA F-5750-141193 FOR REPAIR TRACKING. MAJOR REPAIR

Part: ANGLE — CORRODED (R4 DOORWAY) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

R-4 DOOR CUT OUT LOWER AFT ANGLE HAS CORROSION BS 1681, STG 17R BLENDED CORROSION ON SUPPORT ANGLE, ORIG MAT .063 / MAT LOSS .023, MAT REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, PAGE 103, DETAIL II SEC C-C. RECEIVED ANGLE ON MAE TRAVELER NR T10/848990. LOCATED & DRILLED ANGLE IAW SRM 51-40-05. INSTALLED ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 315) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

FLOOR SUPPORT CHANNEL STA 315, RBL25 CORRODED. REMOVED CORROSION TO FLOOR SUPPORT CHANNEL STA 315 RBL 25.0 IAW SRM 51-10-02 , CHECKED LIMITS ORIG MAT .050 MAT REMAINING .040 LOSS .010 , FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III PAGE 103, REMOVED FLOOR SUPPORT CHANNEL IAW SRM 51-40-02, REMOVED ANGLE FOR FOM IAW SRM 51-40-02, FABRICATED NEW FLOOR SUPPORT CHANNEL ON TRAVELER T10/ 841103, LOCATED 7 DRILLED IAW SRM 51-40-02 TREATED & PRIMED & TOP COATED IAW SRM 51-20-01, INSTALLED FLOOR SUPPORT CHANNEL & ANGLE AT STA 315, RBL 25,0 PER 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 1612-1628) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR, RT SHEAR WEB INBD SUPPORT ANGLE STA 1612-1628 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS; ORIG. MATL.; .071", MATL. LOSS; .010", REMAINING; .061". FOUND TO BE OUT OF LIMITS PER SRM 53-60-13, FIG.101, DETAIL 3, P.103. REMOVED SHEAR WEB RT I/B SUPPORT PER SRM 51-40-02. FABRICATED SHEAR WEB RT I/B SUPPORT ANGLE, DRAWING 146N8722. TREATED / PRIMED PER SRM 51-20-01. INSTALLED NEW SHEAR WEB RT I/B SUPPORT ANGLE PER SRM 51-40-02. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 740 S24-25R) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

FORWARD CARGO COMPT - FRAME AT STA 740 S 24R - S25R HAS CORROSION REMOVED CORROSION PER SRM 51-20-01. CHECKED LIMITS; ORIG. MATL.; .063", MATL. LOSS; .010", REMAINING; .053". FOUND TO BE OUT OF LIMITS PER SRM 53-00-07, FIG.101, SEC. A- A, P.103. REMOVED SPLICE FOR ACCESS. RECEIVED NEW SPLICE ON TRAVELER T10/848597. CUTOUT DAMAGE PER SRM 53-00-07, P.208, FIG 201, DETAIL 3. TREATED / PRIMED NEW SPLICE PER SRM 51-20-01. COATED NEW SPLICE PER AMM 51-21-00-7. INSTALLED NEW SPLICE PER SRM 51-40-02 AND SRM 53-00-07, PAGE 208, FIG.201, DETAIL 3, REPAIR 5. MAJOR REPAIR

Part: SEAT TRACK — MISALIGNED (BS 780) · airframe 57,415 hrs · 17,967 cycles

BS 780, SEAT TRACK AT BUTT SPLICE AREA, LBL 24, EXCEEDS STEP HEIGHT TO ALLOW CARGO HANDLING SYS TO BE INSTALLED. AT BS 780, LBL 24, SEAT TRACK CROWN REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 118310114 BZ2R02, AND STAM EA 757-5335-16-F2848, DATED 08/16/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

Part: SEAT TRACK — MISINSTALLED (BS 780) · airframe 57,415 hrs · 17,967 cycles

BS 780, SEAT TRACK AT BUTT SPLICE, LBL 45, EXCEEDS STEP HEIGHT TO ALLOW CARGO SYS TO BE INSTALLED. AT BS 780, LBL 45, A SEAT TRACK CROWN REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 118310114BZ2R02, AND STAM EA 757- 5335-16-F2850, DATED 08/16/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK BS 440-640, RBL 25, HAS GOUGES, CORROSION, AND WORN PAINT FINISH. REMOVED CORROSION ON SEAT TRACK, BS 640-440, RBL 25, IAW SRM 51-10-02. CHECKED LIMITS; BEFORE: .180", AFTER: .157", LOSS: .027". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4, P102. R & R SEAT TRACK BS 440-640, RBL 25, IAW SRM 51-40-02, PN BAC 1520-792. MAJOR REPAIR

Part: FRAME — CHAFED (BS 1480 S23R) · airframe 57,415 hrs · 17,967 cycles

AFT CARGO BAY FRAME AT STA 1480 , S23R CHAFED. BLENDED CHAFE PER SRM 51-10-02 ORIG MATERIAL THICKNESS 0.063, MATERIAL LOSS 0.033, MATERIAL REMAIN 0.030 FOUND AREA OUT OF LIMITS PER SRM 53-00-07 INSTALLED REPAIR SPLICE PER SRM 51-40-02 AND 51-20-05 . FOUND OUT OF LIMITS PER SRM 53-00-07 DETAIL II FIG. 101 PAGE 107. FABRICATE REPAIR SPLICE ON TRAVELER T10/ 848596.

Part: SKIN — CRACKED (APU DOOR) · airframe 57,415 hrs · 17,967 cycles

APU DOOR 316AR SKIN CRACKED AT FWD LATCH CUTOUT DAMAGED AREA IAW SRM 52-40-01, FIG 201, P202, REPAIR NR3. PERFORMED HFEC OF CUTOUT AREA IAW NTM 51-00-19, P16, WITH NO CRACK INDICATION. FABRICATED DOUBLER/FILLER REPAIR PARTS FROM 2024-T3, .040", BATCH NR 1862684, IAW SRM 52-40-01, FIG 201, REPAIR NR3. TREATED AREA SRM 51-20-01. INSTALLED DOUBLER/FILLER REPAIR ON APU DOOR, 316AR, IAW SRM 52-40-01 FIG.201, REPAIR NR3. MAJOR REPAIR

Part: STRUCTURE — CORRODED (NR 9 SLAT) · airframe 57,415 hrs · 17,967 cycles

NR 9 L/E SLAT OTBD INNER SIDE HAS CORROSION. ACCOMPLISHED REPAIRS OF NR 9 SLAT ON EA F-5740-142234. MAJOR REPAIR.

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

E.O. F-5450-7-5003 P4 CODE B, FASTENER ON RT WING I/B SIDE LOAD FITTING , I/B AFT FASTENER HOLE FOUND CORRODED AFTER REAMING TO CALLED OUT OVER SIZE. COMPLIED WITH EA F-5720-139200, MAJOR REPAIR.

Part: BULKHEAD — CORRODED (BS 168-1720) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

AFT PRESSURE BULKHEAD SUPPORT WEB AT STATION 1680-1720 HAS CORROSION IN SEVERAL AREAS. REMOVED AFT PRESSURE BULK HEAD SUPPORT WEB OVER 20 EA AREA (PLACES) CHECKED LIMITS ON WEB, ORIG MAT .071 REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-0051 FIG 101 DETAIL III PAGE 103 , REMOVED ANGLE SUPPORT ATTACH TO WEB IAW SRM 51-40-02 . FABRICATED NEW WEB IAW DWG 146N5318 LOCATED 7 DRILLED NEW WEB IAW SRM 51-40-05. INSTALLED NEW WEB 7 ANGLE SUPPORT ATTACH TO WEB IAW SRM 51-40-02

Part: WEB — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

AFT PRESSURE BULKHEAD SUPPORT WEB AT STATION 1680-STATION1720 HAS CORROSION IN SEVERAL AREAS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

AFT PIT FLOOR SUPPORT STA 1446 - 1500 RBL 7.5 CORRODED AT NUT PLATES AND FASTENERS HOLES.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

AFT PIT FRAME EXFOLIATED STA 1500, LBL 3 TO LBL 7. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 1, P.103. REMOVED SPLICES, CLIP, TIE DOWN FITTINGS, FALSE CHORD, & FRAME, AND CUSP WEBS IAW SRM 51-40-02. LOCATED AND DRILLED NEW FRAME IAW DWG 146N1016. INSTALLED NEW FRAME AND RE-INSTALLED SPLICES, CLIP, TIE DOWN FITTINGS, FALSE CHORD, AND RE-INSTALLED CUSP WEBS IAW SRM 51-40-02 / 53-00-07 AND DWG 146N1016. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1344) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

AFT PIT FLOOR SUPPORT RBL 2.9 STA 1200 - 1344 CORRODED AT NUMEROUS FASTENER HOLES AND NUTPLATES. CORROSION REMOVAL RESULTED IN BLENDING BEYOND LIMITS IAW SRM 53-00-53 AS FOLLOWS ORIGINAL MATERIAL 0.071 BLENDED 0.020 REMAINING 0.051 PART WAS R & R IAW SRM 51-40-02 AND 51-40-05.

Part: BUSHING — DAMAGED (NR 1 PYLON) · airframe 57,415 hrs · 17,967 cycles

LT WING OTBD NACELLE WING FITTING BUSHING WITH CORROSION. R & R BUSHING IAW WINGS-FITTINGS (AD2004-12-07) NR 1 ENG PYLON OTBD SIDE LOAD FTG BUSHING OS HOLE, EA F5720-139194, DATED 12JUL10. BUSHING FABRICATED O/S ON TRAVELER T10/845494. DTA IS PENDING IAW EA F-5720-139194, AND FAA FORM 8100-9, DATED 07/30/2010. DTA MUST BE ACCOMPLISHED W/I 24 MONTHS FROM DATE OF 8100-9. (NO CORROSION NOTED; SCRATCHES ONLY). MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM STA 324, RBL 24 TO RBL60, CORROSION. REMOVED CORROSION IAW SRM 51-10-02, ORIG MATL..120", LOSS: .030", REMAINING: .090", FOUND OUT OF LIMITS IAW SRM 53-10-08, FIG 101, P 107. R & R FLOORBEAM UPPER TEE IAW SRM 51-40-02 AND SRM 51-20-05. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1525) · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK STA 1525, LBL 25 CORRODED. REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS; ORIG MATL; .920", REMAINING; .420, LOSS; .500", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, P 102, DETAIL 1. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW DWG 146N5130-1, INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. REMOVED CORROSION ON (3EA) SUPPORT BRACKETS IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 1320-1540) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK, STA 1320, RBL 25 HAS CORROSION AT INDB FASTENER HOLE. REMOVED CORROSION FROM SEATTRACK PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 10, P.102; BEFORE: .070", AFTER: .040", LOSS: .030". REMOVED SEAT TRACK BS 1320-1540, RBL 25, PER SRM 51-40-02. RECEIVED NEW SEAT TRACK MATL. BAC 1520-792, BATCH 0001864038. FABRICATED NEW TRACK PER DRAWING PL146N5130. LOCATED AND DRILLED PER SRM 51-40-05. TREATED & PRIMED PER SRM 51-21-01. INSTALLED NEW SEAT TRACK BS 1320-1540, RBL 25, PER SRM 51-40-02 AND DRAWING 146N5120. MAJOR REPAIR.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

NR 4L DOOR UPPER GATE INNER SIDE FOUND CORRODED AND MISSING LEVELING COMPOUND. R & R L4 DOOR UPPER GATE IAW AMM 52-11-28. ADJUSTMENT CHECK PERFORMED ON N/R N01545. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM CORRODED STA 1680, LBL 7 TO LBL 24. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS BEFORE: .150", AFTER: .122", LOSS: .028" / L=25", W=2.7", D= .028", FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3. ACCOMPLISHED FLOORBEAM REPAIR IAW SRM 53-00-51, FIG 201, REPAIR NR 2. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 460-480) · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM OTBD CHORD HAS CORROSION BS 460 TO BS 480 S17R. REMOVED CORROSION ON RT SIDE CREASE BEAM OB CHORD STA 455-465 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL III. REPAIRED CHORD IAW EA F-5310-141190. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: FITTING — MISSING (BS 1640) · airframe 57,415 hrs · 17,967 cycles

UNABLE TO LOCATE 657N3161-12 FITTING, AT BS 1640, RT SIDE, DWG 657N3160, SH.2, REV. D, FOR AFT PALLET FRAME MOD, SHOWS 4EA EXISTING FASTENER HOLES TO BE PICKED UP. ACFT HAS (5EA) EXISTING FASTENER HOLES. AT BS 1640, RT, S17R-S18R, RBL 63, FRAME INSTL MODIFIED, AFT PALLET, RT WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350400EZ2R02, AND MAE EA 757-5362-16-F2742, REV NEW, DATED 06/17/2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION .

Part: FLOOR SUPPORT — CORRODED (BS 660-750) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR SHEAR WEB INBD SUPPORT ANGLE, S17L, BS 660-680, HAS CORROSION AROUND FASTENER AND SCRATCH MARKS ON SEVERAL AREAS. REMOVED CORROSION IAW SRM 51-10-02; ORIG. MATL. = .090", LOSS = .015", REMAINING = .075", OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL3, PAGE 103. R & R CREASEBEAM CHORD, BS 660-750, LT, INBD, IAW SRM 51-40-02/ 51-20-05. (PN 143N8328-53).

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

LT CREASE BEAM SHEAR WEB BETWEEN STA 1600 AND 1620 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS FOUND OUT OF LIMITS ORIG- MAT .056, REMAINING .048 IAW SRM 53-00-13, FIG 101, PG 103, DETAIL III. FABED NEW WEB, TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW WEB STA 1600- 1620, STR 17L, IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK SEAT TRACK LBL 45.5,STA 870-879 GOUGE/ CHAFFED ON SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK BS 780-879, LBL 45 PER SRM 51-40-02. REMOVED GOUGE PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, P.102, FIG.101, DETAIL 2; BEFORE: .230", AFTER: .192", LOSS: .038", AT BS 879. RECEIVED NEW SEAT TRACK P/N BAC 1520- 792, BATCH 1865442. FABRICATED PER SRM 53-60-52, AND DRAWING 146N5130-2. LOCATED/DRILLED PER SRM 51-10-02. TREATED / PRIMED PER SRM 51-20-01. PART MARKED PER GMM 7-0-1001. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

LT CREASE BEAM INBD CHORD HAS CORROSION BETWEEN BS 900 TO BS 1040 STRG 17L REMOVED CORROSION PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-40-13, FIG.101, DETAIL 3, BEFORE: .070", AFTER: .050", LOSS: .020". REMOVED I/B CHORD BS 900-1040, S17L, PER SRM 51-40-02. RECEIVED NEW I/B CHORD BAC 1515-551. INSTALLED NEW I/B CHORD FROM BS 900-1040, S17L, PER SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

STA 680 FLOORBEAM, RBL 45 TO RBL 60 UPPER FLANGE CORRODED. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-00-51, P.103, FIG.101, NEW FLOORBEAM FABRICATED IAW DWG 143N5013. INSTALLED NEW FLOORBEAM. MAJOR REPAIR .

Part: SEAT TRACK — CORRODED (BS 1100-1280) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK STA 1100-1280 RBL 45 HAS GOUGES, CORROSION, AND WORN PAINT. REMOVED AND REPLACED SEAT TRACK STA 1180 -1280 RBL 45 IAW SRM 51-40-02.REMOVED CORROSION AND GOUGES IAW SRM 51-10-02 CHECKED LIMITS ORGINAL MATERIAL AT CROWN .230 MAT. REMAINING .195 MAT. LOSS .031 AT LOWEST STA 1259 FOUND OUT OF LIMITS IAW 53-00-52 PG 102 FIG. 101 DETIAL 2.RECEIVED NEW SEAT TRACK. FABRICATED IAW SRM 53-60-52 & DRAWING 14N5130-2 .LOCATED & DRILLED HOLES IAW SRM 51-10-02 ,TREATED & PRIMED IAW 51-20-01. PART MARKED AS PER GMM 7-0- 1001-1

Part: CREASE BEAM — CORRODED (STA 1345) · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM WEB STA 1345 HAS CORROSION ON LOWER SIDE. REMOVED CORROSION ON RT SIDE CREASE BEAM WEB STA 1345 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL III. R & R WEB IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 900-1075) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK, STA 900-1075, RBL 25 HAS GOUGES, CORROSION AND WORN PAINT. REMOVED SEAT TRACK IAW SRM 51-41-02. REMOVED CORROSION / GOUGES IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52. RECEIVED NEW SEAT TRACK IAW SRM 51-40-05. INSTALLED NEW SEAT TRACK STA 900- 1075, RBL 25, IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 57,415 hrs · 17,967 cycles

BS 418-440, RBL 24, SEAT TRACK GOUGED. REMOVED DAMAGED AREA ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. R & R SEAT TRACK, BS 418-440, RBL 24, IAW SRM 51-40-02. (REPLACEMENT SEAT TRACK FABBED IAW SRM 53-10-52, FIG.1, DETAIL 2). MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 660-720) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM HAS CORROSION AROUND FASTENERS LOWER FACE BS 660 TO BS 680 STG 17R. REMOVED CORROSION INNER CHORD CREASE BEAM IAW SRM 51-10-02. CHECK LIMITS INNER CHORD CREASE BEAM ORIGINAL MATERIAL .100 REMAINING .085 LESS .015. DETAIL 3, FIG 101, PAG. 105 IAW SRM 53-30-13. REMOVED CREASE BEAM IAW 51-40-02. RECEIVED CREASE BEAM INNER CHORD PN 143N8328-54, BATCH 0001860048. LOCATED AND DRILLED IAW 51-40-05. INSTALLED NUT PLATE ON CREASE BEAM IAW 51-40-02. TOP COATED SPLICES BELONGING TO STA 660-724. INSTALLED SPLICES AND INNER CHORD CREASE BEAM IAW SRM 51-40-02. CLASSIFIED AS MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK STA 1320-1540, LBL 45 HAS GOUGES, CORROSION, AND WORN PAINT FINISH. REMOVED CORROSION ON SEAT TRACK STA 1320-1540 LBL 45 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL IX. REMOVED AND REPLACED SEAT TRACK IAW SRM 51- 40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR

Part: FRAME — DAMAGED (BS 1640) · airframe 57,415 hrs · 17,967 cycles

DWG NR 657N3160-SH.2, REV D, FOR AFT PALLET FRAME MOD SHOWS 4EA. EXISTING FASTENER HOLES TO BE PICKED UP IN THE 657N3161-11 FITTING AT BS 1640, LT. ACFT HAS 5 EA EXISTING HOLES AT BS 1640, S17L/18L, FRAME REPAIR WAS ACCOMPLISHED ON MAE MOD W/C 118350399EZ2R02, AND MAE EA 757-5362-16-F2757, REV.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK REQUIRE REMOVE FOR FLOORBEAM REPLACEMENT STA 1180- 1240, LBL- 45.50. ( FOUND CORR- AFTER SEAT TRACK REMOVAL ). REMOVED CORR/ GOUGES AREA IAW SRM 51-10-02. REMOVED SEAT TRACK, FOUND OUT OF LIMITS, IAW SRM 53-00-52 PAGE 102, DETAIL I. RECEIVED NEW SEAT TRACK BAC 1520-792. INSTALLED NEW SEAT TRACK , BETWEEN STA 1180- 1240, LBL- 45.50, IAW SRM 53-60-52, AND SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK REQUIRE REMOVE FOR FLOORBEAM REPLACEMENT, STA 1180- 1240, LBL- 24.75. ( FOUND CORR/ GOUGES AFTER SEAT TRACK REMOVAL). REMOVED SEAT TRACK IAW SRM 51-40-02. REMOVED CORROSION AND GOUGES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PG 102, FIG 101, DETAIL I. RECEIVED NEW SEAT TRACK PN BAC 1520-792, LOCATED AND DRILLED HOLES IAW SRM 53-60-52, TREATED AND PRIMED IAW SRM 51-20-02. INSTALLED NEW SEAT TRACK FROM STA 1180- 1240, LBL- 24.75, IAW SRM 53-60-52, PAGE 2, FIG 1 CATEGORY "A", MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · airframe 57,415 hrs · 17,967 cycles

EXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED AT BS 1635-1640, LBL 24.75, WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK BS 1540-1640, LBL 24.75 IAW SRM 51-40-02. REMOVED WEB BS 1620-, 1640, LBL 24.75 IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, 7178-, T6511, IAW SRM 53-60-52. LOCATED/DRILLED NEW SEAT TRACK IAW SRM 51-40-05. TREATED/PRIMED IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK BS 1640-1640, LBL 24.75, PN FX146N5130, IAW SRM 51-40-02. INSTALLED WEB BS 1620-1640, LBL 24.75, P/N 140N2506-1, IAW SRM 51-40-02. MAJOR REPAIR .

Part: SEAT TRACK — DAMAGED (BS 1635-1640) · airframe 57,415 hrs · 17,967 cycles

EXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640 AT RBL 24.75, WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK SECTION AT RBL 24.75, BS 1540-1640. FABRICATED NEW SEAT TRACK SEC, TREATED/PRIMED AND TOP COATED IAW SRM 51-40-02/ 51-20-01/ AMM 51-21-00-377-00-1. INSTALLED NEW SEAT TRACK SECTION AT BS 1540-1640, RBL 24.75, IAW SRM 51-40-02. NEW SEAT TRACK SECTION MADE FROM BAC 1520-792 EXTRUSION, PN 146N5135. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 415-440) · airframe 57,415 hrs · 17,967 cycles

STA 415-440 RBL 45 SEAT TRACK GOUGED. BLENDED AREA. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52,FIG 101, DETAIL 7. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · airframe 57,415 hrs · 17,967 cycles

FLOOR SUPPORT CHANNEL AND ATTACHED FITTING AT BL 0 STA 324-345 IS CORRODED.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

NR1 PYLON AT STA 144-170 SKIN HAS CORROSION. REMOVED CORROSION ON NR 1 PYLON SKIN STA 144-170 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FIG 101 DETAIL III. ORIG MATERIAL .090 EXFOLIATED BEYOND LIMITS. L=12" W=3". REMOVED AND REPLACED SKIN IAW SRM 51-40-02 AND DWG 311N5002 SHEET 13. CLASSIFIED CATEGORY "A" MAJOR REPAIR

Part: CREASE BEAM — CORRODED (BS 430-450 S17R) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM OUTER CHORD AT STA. 430 TO STA. 450 CORRODED. REMOVED CREASE BEAM, CORROSION OUT OF LIMITS IAW SRM 53-30-13, DET III, FIG 101. FABRICATED NEW CREASE BEAM MAT BAC 1515-553, IAW SRM 51-10-02. INSTALLED CREASE BEAM INNER CHORD STA 430-450, S17R, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 450-490 S17R) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM OUTER CHORD AT STA 450 TO STA 490 CORRODED. REMOVED CREASE BEAM, CORROSION OUT OF LIMITS IAW SRM 51-10-02, DET III,PG 101, 53-30-13. FABRICATED NEW CREASE BEAM BAC 1515-553, IAW SRM 51-10-02. INSTALLED CREASE BEAM AT BS-450-665, S17R, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (365) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM UPPER TEE, STA. 365 B.L. 0 TO RBL 59 CORRODED. REMOVED CORROSION ORIGINAL MATERIAL .125, MATERIAL REMOVED .016, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101, DETAIL III. INSTALLED REPAIR AT STA 365, LBL 17- RBL 70, IAW SRM 53-00-51 FIG 201, REPAIR 3, CATEGORY "A", MAJOR REPAIR.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR RT SHEAR WEB, STA 1060-1080 HAS CORROSION.

Part: FRAME — CORRODED (BS 1600) · airframe 57,415 hrs · 17,967 cycles

MAIN CABIN FRAME 1600 OTBD CHORD ANGLE HAS CORROSION AT STR 17R. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 3, P.103. FABRICATED ANGLE AND FAIL-SAFE. LOCATED, DRILLED, TREATED AND PRIMED ALL REPAIR PARTS IAW SRM 51-40-05/ 51-20-01 AND TOP COATED IAW AMM 51-21-00-7. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 305-324) · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM OUTER CHORD STA 305-324 CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-30-13, FIG.101, DETAIL 8, P.105; BEFORE: .070", AFTER: .060", LOSS: .010". REMOVED O/B ANGLE BS 297-365, PER SRM 51-40-02. FABRICATED NEW ANGLE ON TRAVELER T10/839328. LOCATED, DRILLED, TREATED AND PRIMED PER SRM 51-40-05 / 51-21-01. APPLIED TOPCOAT PER AMM 51-21-00-7. INSTALLED NEW O/B CREASE BEAM PER SRM 51-40-02 / DRAWING 141N8422, AT BS 297-365. MAJOR REPAIR.

Part: DOOR FRAME — DENTED (ZONE 100) · airframe 57,415 hrs · 17,967 cycles

NR 2 CARGO DOOR FWD FRAME LOWER CORNER HAS DENT.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM TEE HAS DOUBLE DRILLED HOLE BS 353 LBL 52 MAIN CARGO CAMPARTMENT. REMOVED DAMAGED PART IAW SRM 51-40-02. RECEIVED NEW REPAIR ANGLES TRAV NR T10/836720, AND REPAIR STRAPS TRAV NR T10/836719. INSTALLED NEW REPAIR SPLICE PARTS FLOORBEAM UPPER TEE AT STA 345, LBL- 52, IAW SRM 53-00-51, FIG 201, CATEGORY "A", REPAIR NR 3. MAJOR REPAIR.

Part: FRAME — CORRODED (NR 2 NACELLE) · airframe 57,415 hrs · 17,967 cycles

NR 2 ENG STRUT FAIRING PANEL 443AR FRAME HAS CORROSION. COMPLIED WITH EA F-5450-141157 PART 1, STEPS 1-7. A MINOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 440-644.5) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK SEAT TRACK LBL 45.5 STA 440 TO 644.5 GOUGED IN SEVERAL AREAS. REMOVED GOUGES AND FOUND PART TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DET 1, PG 102. ORIGINAL MATERIAL IS .230, REMAINING MATERIAL .195, A REMOVAL OF .035. FABRICATED SEAT TRACK FROM BAC1520-792, 7178-T6511, BATCH NR 0001864040 IAW DWG 143N5086. LOCATED AND DRILLED IAW SRM 51-30-01. TREATED AND PRIMED IAW SRM 51-10- 02, TOP COAT IAW AMM 51-21-10-7. INSTALLED TRACK IAW SRM 51-40-02. PART MARKED IAW GMM 7-0-1001-1, STA 440- 644.5, LBL 45.5. CATEGORY "A". MAJOR REPAIR.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM BL0 AND STA 324 GOUGED. DAMAGED FLOORBEAM FOUND OUT OF LIMITS WITH ORGINAL MATERIAL .110 LOSS.024 MATERIAL REMAINING .086, L-.050 W-2" AS PER SRM 53-00-51 PG.103 DETAIL 3 & FLOOR SUPPORT ORGINIAL MATERIAL .050 MATERIAL LOSS .009 REMAINING MATERIAL.041 L-10" W-.050" PER SRM 53-00-51 DETAIL 3.

Part: FLOORBEAM — MISINSTALLED (BS 660) · airframe 57,415 hrs · 17,967 cycles

SECTION 43, SEAT TRACK AT RBL 58.22 BETWEEN STA 620, 640 AND 660 UNABLE TO LOCATE SEAT TRACK EXISTING FASTENER HOLES ON THE FLOORBEAM ARE NOT POSITIONED AS DEPICTED IN THE DWG 657N3321, SHEET 12, REV B. ON ACCESSING AREA, FOUND EXISTING GOUGES ON BS 660 FLOORBEAM WEB, RBL 58.22. REMOVED GOUGES IAW SRM 51-10-02; ORIG. MATL, .090", MATERIAL REMOVED: .040", REMAINING: .050", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. R & R BS 660 FLOORBEAM, LBL 64 - RBL 64, IAW SRM 51-40-02. NEW FLOORBEAM WAS FABBED FROM BAC 1518-338, 7075-T6511, IAW DWG 143N5911. DISCREPANT CONDITION NO LONGER EXISTS. MAJOR REPAIR.

Part: SHEAR WEB — CORRODED (BS 1360-1380) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR, RT, SHEAR WEB, BS 1360-1380, LOWER SURFACE HAS CORROSION.

Part: FLOORBEAM — CORRODED (BS 700) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

STA 700, FLOORBEAM, RBL 55 UPPER FLANGE CORRODED.

Part: FLOORBEAM — GOUGED (BS 1600) · airframe 57,415 hrs · 17,967 cycles

STA. 1600 FLOORBEAM SCRATCHED AND GOUGED FROM BL "0" TO RBL 60.

Part: FLOORBEAM — GOUGED (BS 1240) · airframe 57,415 hrs · 17,967 cycles

STA 1240 FLOORBEAM SCRATCHED AND GOUGED FROM RBL 25 TO LBL 60. BLENDED AREA IAW SRM 51-10-02,ORIGINAL MAT =.125 IN AFTER BLEND = 090 IN WHICH IS OUT OF LIMITS IAW SRM 53-00-51. REMOVED AND REPLACED FLOOR BEAM. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-05, PRIMED AND PAINTED IAW SRM 51-20=01. INSTALLED FLOORBEAM IAW SRM 51-40-02

Part: SEAT TRACK — DAMAGED (BS 1635-1640) · airframe 57,415 hrs · 17,967 cycles

EXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED STA 1635-1640 AT LBL 45.50" WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK BS 1540-1640, LBL 45.5, IAW SRM 51-40-02. REMOVED WEB, BS 1620-1640 PET SRM 51-40-02. FABRICATED NEW SEAT TRACK PN BAC 1520-792, MAT.7178-T6, BATCH NR 0001833789, IAW SRM 53-60-52. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED/PRIMED IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK, BS 1540-1640, LBL 45.5, PN FX146N5130 PET SRM 51-40-02. INSTALLED WEB, BS 1620-1640, LBL 45.5, IAW SRM 51-40-02. MAJOR REPAIR

Part: FLOORBEAM — GOUGED (BS 1320) · airframe 57,415 hrs · 17,967 cycles

STA. 1320 FLOORBEAM BL "0" TO LBL 60 GOUGED AND CORRODED. REMOVED GOUGED & CORROSION AREA IAW SRM 51-10-01, ORIG MAT THICKNESS 0.125", AFTER REWORK 0.106", MEASURED AREA L=60.00", X W=2.00", X DEPTH 0.019", FOUND OUT OF LIMITS IAW SRM 53-00-51, PAGE 101, FIG 101, DETAIL III, REMOVED CREASE BEAM, FOR ACCESS, IAW SRM 51-40-02, REMOVED INTERCOSTAL BET STA 1300-1320, RBL 60 FOR ACCESS IAW SRM 51-40-02, R & R FLOORBEAM, PN 1520-338/18 IAW SRM 51-40-02, AND DWG NR 146N5008, REINSTALLED INTERCOSTAL BET STA 1300- 1320, LBL 60 TO RBL 60, REINSTALLED CREASE BEAM ON N/R N01045. CATEGORY "A", MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 740) · airframe 57,415 hrs · 17,967 cycles

STA. 740 FLOORBEAM RBL 46 TO RBL 60 UPPER FLANGE CORRODED.

Part: SEAT TRACK — DAMAGED (BS 1635-1640) · airframe 57,415 hrs · 17,967 cycles

EXISTING SEATTRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640 AT RBL 45.50" WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. REMOVED SEAT TRACK SECTION AT RBL 45.5, BS 1540-1640. FABRICATED NEW SEAT TRACK SECTION, TREATED/PRIMED, APPLIED TOP COAT IAW SRM 51-40-02/ 51-20-02/ AMM 51-21-00-377-00-1. NEW SEAT TRACK MADE FROM BAC 1520-792, PN 146N5135 EXTRUSION. INSTALLED NEW SEAT TRACK SECTION AT BS 1540-1640, RBL 45.5, IAW SRM 51-40-02. MAJOR REPAIR

Part: SUPPORT ANGLE — CORRODED (BS 1080) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR RT SHEAR WEB INBOARD SUPPORT ANGLE JOINT SUPPORT FITTING ON FRAME CORRODED STA 1080. REPLACEMENT OF SUPPORT FITTING ACCOMPLISHED (SECONDARY STRUCTURE).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR LT SHEAR WEB INBD SUPPORT ANGLE HAS CORROSION AROUND FASTENER HOLES STA 1160-1180. REMOVED CORROSION PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-40-13, P.104, DETAIL 7; BEFORE: .071", AFTER: .057", LOSS: .014". FABRICATED I/B SUPPORT ANGLE, USING PN BAC 1515-551, PER DRAWING 2312033, ON BATCH 0001805485. FOUND SPLICE CRACKED OUT OF LIMITS, BS 1080, PER SRM 53-40-13. RECEIVED SPLICE ON TRAVELER T10/842169. REMOVED AND INSTALLED LT I/B SUPPORT ANGLE, SPLICE PER SRM 51-40-02. PART MARKED BOTH SPLICE AND ANGLE PER GMM 7-0-1001. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1600) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

STA 1600 FLOORBEAM SCRATCHES AND GOUGES FROM BL0 TO RBL 60. REMOVED SCRATCHED AND GOUGED AREAS IAW SRM 51-10-02, ORIG MAT .125 AFTER .115", MEASURED AREA L=24:00" X W=2.00", X DEPTH 0.010", FOUND OUT LIMITS IAW SRM 53-00-51, PAGE 103, FIG 101, DETAIL III, REMOVED AND REPLACED FLOORBEAM AT STA 1600, PN BAC 1548-338/18, BATCH 0001671872, IAW SRM 53-30-51, FIG 1, SH 5 OF 6, AND PER DWG 146N5087. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 57,415 hrs · 17,967 cycles

LT CREASE BEAM WEB HAS CORROSION BS 1020 TO 1040 STR 17L.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR LT SHEAR WEB INBD SUPPORT ANGLE, STA 755 HAS CORROSION.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR RT SHEAR WEB OTBD SUPPORT ANGLE HAS CORROSION AROUND FASTENERS AT STA 1600-1620. REMOVED ANGLE SUPPORT OUT OF LIMITS IAW SRM 51-40-02 CHECKED LIMITS ORIG MAT .090 LOSS .025. REMAINING .065 IAW SRM 53-60-13 LOCATED 7 DRILLED NEW ANGLE SUPPORT IAW SRM 51-40-05 INSTALLED NEW ANGLE SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 700) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

STA 700 FLOORBEAM, RBL 55 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIG MATERIAL 0.130 AFTER REWORK 0.107. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. R & R FLOORBEAM AT STA 700, LBL 63 TO RBL 63 IAW SRM 51-40-02 AND DWG 214N5014, SHEET 1. PART MARK IAW GMM 7-0-1001.

Part: FLOOR SUPPORT — CORRODED (BS 1180-1291) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

MAIN DECK FLOOR RT SHEAR WEB INBD SUPPORT ANGLE SRA 1180 TO 1291 HAS CORROSION AND CHAFE MARKS NEAR FASTENER HOLES. REMOVED FASTENERS IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 3, PAGE 103; ORIG. MATL. = .080", REMAINING = .048", LOSS = .032". REMOVED SPLICE IAW SRM 51-40-02. REMOVED INBD ANGLE IAW SRM 51-40-02. FABRICATED INBD ANGLE, PN 1805485/ BAC 1515-553, LOCATED & DRILLED, TREATED & PRIMED IAW SRM 51-40-05 / 51-21-01. NEW INBD ANGLE MADE FROM BAC 1515-553 EXTRUSION. INSTALLED NEW INBD ANGLE, AND SPLICE IAW SRM 51-40-02, AT BS 1180-1290, LBL 64. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

STA 740, FLOORBEAM, RBL 46 TO RBL 60 UPPER FLANGE CORRODED. REMOVED CORROSION, EVALUATED FOUND OUT OF LIMITS, MAT THICKNESS 0.125", MAT BLENDED .018", REMAINING MAT .107", IAW SRM 53-00-51, FIG 101, PG 101, DETAIL III, REMOVED FLOORBEAM IAW SRM 51-40-02, LOCATED & DRILLED NEW FLOORBEAM IAW SRM 51-40-05, PROTECTIVE TREATMENT AND TOP COAT APPLIED IAW SRM 51-20-01, INSTALLED NEW FLOORBEAM IAW SRM 51-40-02. CATEGORY 'A' MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,415 hrs · 17,967 cycles

SEAT TRACK STA 1180-1280, RBL 25 HAS GOUGES, CORROSION, AND WORN PAINT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,415 hrs · 17,967 cycles

FLOORBEAM UPPER CAP CORRODED STA 377, LBL 60 TO RBL 60. REMOVED CORROSION FROM RBL 16-60, ORIGINAL MATERIAL : .125", REMOVED: .008"; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-51,FIG.101,DETAIL 3. REMOVED CORROSION FROM BS 377, RBL 15-LBL 60, ORIGINAL MATERIAL: .125", REMOVED: .028"; FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGE. FABRICATED -1 UPPER CHORD FROM MATERIAL PN BAC 1505-100880, BATCH NR 1787163. RECEIVED -2 AND -3 REPAIR ANGLES IAW TRAVELER T10/836718. RECEIVED -4 AND -5 REPAIR STRAPS IAW TRAVELER T10/836717. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51, FIG.201, REPAIR NR 3. - CAT. "A" MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM INNER CHORD STA 820 TO 900 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 3; BEFORE: .080", AFTER: .061", REMOVED: .019". REMOVED RT CREASE BEAM INNER CHORD, BS 760-900, IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM INNER CHORD, RT, USING BAC 1515-557, 7075-T6, IAW DWG 143N5520. LOCATED/DRILLED IAW SRM 51-40-05. COATED NEW CREASE BEAM RT INNER CHORD IAW SRM 51-24-09-701. INSTALLED NEW RT CREASE BEAM, INNER CHORD, BS 760-900, IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,415 hrs · 17,967 cycles

RT CREASE BEAM OUTER CHORD STA 378 TO 430 CORRODED AT NUTPLATES AND FASTNER HOLES. REMOVED CORROSION IAW SRM 51-10-02, ON CREASE BEAM INBD CHORD, BS 297-430. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL 8; BEFORE: .071", AFTER: .057", LOSS: .014". REMOVED CREASE BEAM IAW SRM 51-40-02. FABBED NEW CREASE BEAM PN BAC 1515-553, BATCH NR 0001827675 AND DWG 141N8422. LOCATED/DRILLED IAW SRM 51-40-05. TREATED/PRIMED IAW SRM 51-21-01. APPLIED TOPCOAT IAW AMM 51-21-00-7. INSTALLED NEW CREASE BEAM, INBD CHORD, AT BS 297-430, RT, IAW SRM 51-40-02. MAJOR REPAIR.