N915FD

Part: SEAT TRACK — CORRODED (BS 1480-1500) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 1480-1500 RBL 45 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG.201, TYPICAL TRACK REPAIR OPTION 1. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1100-1120) · airframe 59,032 hrs · 28,658 cycles

FOUND CORROSION ON SEAT TRACK AT STA 1100-1120 RBL 58 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5320-T0371663- SEAT TRACK AT RBL 58.22, CORROSION FOUND, PERMANENT REPAIR. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 520-540 RBL45) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 520-540-RBL 45 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG.201, TYPICAL SEAT TRACK REPAIR OPTION I. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (N/A) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK AT STA 860-780 LBL 25 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0371831- SEAT TRACK HORIZONTAL INBOARD FLANGE STA 700-760 LBL 24.75, CORROSION, PERMANENT REPAIR MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 350-377 LBL7) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 350-377 LBL 7 DAMAGED SEAT TRACK REMOVED AND REPLACED WITH NEW FAB. SEAT TRACK PER FEDEX E.A # F-5310-T0371591 P1 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1580-1640) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK AT STA 1580-1640 RBL 45 DAMAGED PART REMOVED AND NEW PART P/N FX-146N5130-5 INSTALLED PER SRM 51-40-02 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1580-1640) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 1580-1640 RBL 25 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG.201, OPTION I MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 540-600 LBL25) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 540-STA 600 LBL 25 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG.201 TYPICAL SEAT TRACK REPAIR OPTION I

Part: SEAT TRACK — CORRODED (BS 1400-1500) · airframe 59,032 hrs · 28,658 cycles

CORRODED SEAT TRACK LOCATED AT STA 1400-1500 LBL 58 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG 201, TYPICAL SEAT TRACK REPAIR OPTION I MAJOR REPAIR

Part: FLOORBEAM — CORRODED (N/A) · airframe 59,032 hrs · 28,658 cycles

CORRODED FLOOR BEAM LOCATED AT STA 720 RBL 62 PERFORMED FLOOR BEAM REPAIR PER SRM 53-00-51-2R FIG. 201, REPAIR 8 DAMAGE ON THE FLOOR BEAM UPPER CHORD AT THE SIDE OF THE BODY MAJOR REPAIR

Part: FLOORBEAM — CORRODED (N/A) · airframe 59,032 hrs · 28,658 cycles

CORRODED FLOOR BEAM LOCATED AT STA 720 LBL 45-LBL 64 PERFORMED FLOOR BEAM REPAIR PER SRM 53-00-51-2R , FIG. 201, REPAIR 8 DAMAGE ON THE FLOOR BEAM UPPER CHORD AT THE SIDE OF THE BODY MAJOR REPAIR

Part: CREASE BEAM — CORRODED (N/A) · airframe 59,032 hrs · 28,658 cycles

CORRODED I/B CREASE BEAM LOCATED AT STA 1340-1360 LBL 64 DAMAGED PART REMOVED AND NEW PART P/N FX146N8326-1 (CHORD) INSTALLED PER SRM 51-40-02. MAJOR REPAIR

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 11861182-15 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/17/2022.

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 11861182-2 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. P/N:FX11861182-2 222MDF, W.O.:20471352. MAJOR REPAIR. ORIG SUBMISSION DATE: 11/17/2022.

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 141N5370-40 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/17/2022

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL FOUND WORN AT SEC. 41 ON FWD AREA. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/18/2022

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 141N5370-10 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/17/2022

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 11861182-14 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. P/N: 11861182-14 222MBF. W.O.:20471432. MAJOR REPAIR. ORIG SUB DATE: 11/17/2022

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 11861182-16 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER DWG SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/18/2022

Part: FLOOR PANEL — WORN (CABIN) · airframe 59,032 hrs · 28,658 cycles

FLOOR PANEL P/N 141N5370-31 FOUND WORN AT SEC. 41 ON FWD AREA FABRICATED FLOOR PANEL PER SRZ-25-005. MAJOR REPAIR. ORIG SUB DATE: 11/18/2022

Part: SKIN — DENTED (RT NR 7 SLAT) · airframe 59,032 hrs · 28,658 cycles

SLAT 7 R/H WING HAS DENT 2" FROM EDGE A=2.3' Y=0.023' A/Y= 100 PERFORMED HOT BOND REPAIR PER SRM 51-70-10, REF SRM 57-43-02-2R,FIG. 201,DETAIL II,NOTE D. REP. DIM.:DIA. 5.5".REP. LOC.: 46" FROM I/B EDGE AND 0.5" FROM T/E OF SLAT #7. REV.137.0 MAJOR RAPAIR.

Part: STRINGER — CORRODED (N/A) · airframe 59,032 hrs · 28,658 cycles

CORRODED STRINGER IN FWD CARGO COMP. LOCATED AT STA 740-760 STR 20R WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0371690, STR 20R, STA 740-760, HEAVY CORROSION PERMANENT REPAIR. MAJOR REPAIR

Part: DECK PLATE — CORRODED (BS 1680 RBL2-28) · airframe 59,032 hrs · 28,658 cycles

FOUND CORROISON ON EXISTING REPAIR DOUBLER ON DECK PLATE LOCATED AT STA 1680 RBL 2-RBL 28 REPLACED DAMAGED REPAIR WITH NEW PER SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE I, FIG 201

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 58,817 hrs · 28,543 cycles

MDIS 915 33-50 4663 05AUG22 HAJ FACT U RH SIDE EMERGENCY LIGHTS INOP R/I 05AUG22 05:26 HAJ U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1ASMI POS: 1 SRL: 4711 ON MPN: 2013-1A SRL: 50292 TAG NBR: 797G35 FACT 05AUG22 05:26 HAJ U EATF-3350-T0338301 BATTERY PACK REPLACED IAW AMM 33-51-07-902-001, TEST SATIS.

Part: SPEED BRAKE — FAULTY (N/A) · airframe 58,578 hrs · 28,417 cycles

WHEN SPEED BRAKES PLACED IN ARMED POSITION IN FLIGHT, IT FEELS LIKE SPOILERS ARE DEPLOYING. WHEN SPEEDBRAKE LEVER IS PUT IN ARM POSITION, NOTICED SLIGHT DEFLECTION OF ALL SPOILERS. ALL SPEEDBRAKE LVDT ADJUSTED PER AMM 27-61-00-05. SPEEDBRAKE TEST PASSED PER 27-61-00-05, NO MORE SPOILERS DEFLECTION WHEN SPEEDBRAKE LEVERS IS ON ARM POSITION.

Part: CONTROL PANEL — FAILED (MODE) · airframe 58,027 hrs · 27,902 cycles

ON CLIMB OUT THE MCP ALT WINDOW FROZE AT 5000. TRIED SPINNING THE KNOB PUSHING THE KNOB WITH NO RESULT. DISCONNECTED THE A/P MANUALLY FLEW THE AIRPLANE TO FL230. SHORTLY AFTER LEVEL OFF THE ALT WINDOW BEGAN WORKING. THIS ALT WINDOW SITUATION IS A SAFETY OF FLIGHT ISSUE.THE AIRPLANE CANNOT FLY AGAIN UNTIL FIXED. PERFORMED T/S IAW FIM 22-12-77-00 TASK 22-02 - 801 AFTER SEVERAL TEST OFF MCP PANEL FOUND ALT SWICH FAULT REPLACED MODE CONTROL PANEL I.A.W. AMM 22-11-02-2, ALL OPS CHECK SATIS. COMPLIED WITH LLM M-3574 AND RVSM M-3586. A/C OK FOR CONTINUE IN SERVICE PANEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,998 hrs · 27,874 cycles

MDIS 915 33-50 3264 16APR21 MUC FACT U R1 EMERGENCY LT NOT FULLY ILLUMINATED LAMPS REPLACED ACC AMM 33-51-01-2 REV 127.8. FUNCTION CHECK OK

Part: LINE — LEAKING (RT FSCM) · airframe 57,968 hrs · 27,838 cycles

MDIS 915 71-00 3183 22MAR21 BSL FACT U LOGPAGES:3301523 ON ARRIVAL FUEL DRIPPING FROM RH ENGINE COWLS FACT 22MAR21 22:14 BSL U LEAK TRACED TO FSCM RETURN LINE WHICH WAS LOOSE. RE-TORQUED IAW AMM 70-51-00-2-0-R REV 127.3. LEAK CHECKED SATIS.

Part: SENSOR — LOOSE (PILOT VALVE) · airframe 57,947 hrs · 27,817 cycles

L ENG HI STAGE EICAS @ APROXYMATLY 80 KNOTS, REJECTED TAKEOFF. COMPLIED W/QRH. RETURN TO GATE. FOUND CONTROL PRESSURE SENSE ON HIGH STAGE PILOT VALVE SLIGHTLY LOOSE,TIGHTENED SAME ,FOUND MANUALLY RESET BOTTON POPPED,RESET SAME.RAN L/H ENGINE PER JRK AND CHKD HI STAGE PILOT VALVE PER MM 36-11/08/4-1. NO LEAKS AT THIS TIME AND ALL PARAMETERS NORMAL

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 57,936 hrs · 27,806 cycles

L REV ISLN VAL STATUS MSG IN FLIGHT. FIM PROC 78-36-FT 804 FIG 105 BLK 1,1A,2,3,4,5,25,44 NO DEFECTS EVIDENT-T/R FUNCTIONED SEVERAL TIMES WITHOUT FAULT- ALL INDICATIONS NORMAL-AMBER REV EXTINGUISHED AND ACTUATOR LOCKS AND SYNC LOCKS FULLY LOCKED- L/H SYSTEM FULLY SERVICEABLE. AMM:78-36-00-FIM PROC 78-36-FT 804 FIG 105 BLK 1,1A,2,3,4,5,25,44 NIL DEFECTS EVIDENT-T/R FUNCTIONED SEVERAL TIMES WITHOUT FAULT- ALL INDICATIONS NORMAL-AMBER REV EXTINGUISHED AND ACTUATOR LOCKS AND SYNC LOCKS FULLY LOCKED- L/H SYSTEM FULLY SERVICEABLE

Part: HOUSING — CONTAMINATED (NR 1 FUEL FILTER) · airframe 57,898 hrs · 27,768 cycles

UPON REMOVAL OF ENG#1 LP FUEL FILTER, FOUND FILTER AND HOUSING TO BE CONTAMINATED REPLACED ENG#1 LP FUEL FILTER AND HOUSING IAW AMM 73-11-10

Part: FRAME — CRACKED (ZONE 100) · airframe 57,898 hrs · 27,768 cycles

CRACK INDICATION FOUND AT BSTA 1681 IN FUSELAGE FRAME AT RH SIDE BELOW CABIN FLOOR LEVEL AT UPPER FASTENER ROW MOST IB FASTENER COMMON TO FLOOR BEAM REPAIRED R/H FRAME AT BSTA 1681 BELOW WL 208 IAW FEDEX EA F-5310-T0359258 TITLE: FUSELAGE - MAINFRAME - BS 1681 R/H FRAME CRACK FINDING. THIS IS A MAJOR CATAGORY B REPAIR WITH REPEAT INSPECTIONS.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,898 hrs · 27,768 cycles

DENT AT BSTA 669 2.5" BELOW STR 26 LT EVALUATED DENT AT BSTA 669, 2.5" BELOW STR 26 LT, IAW SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIG 101 AND FOUND OUT OF LIMITS DUE TO DISTANCE FROM LAP JOINT. REPAIRED DENT, IAW SRM 53-00-01-2R REPAIR 6 FIG 201. THIS IS A CATAGORY A MAJOR REPAIR.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,898 hrs · 27,768 cycles

STUB BEAM FOUND CRACKED BSTA 580 LBL 45.5 REPAIRED STUB BEAM AT BSTA 580 LBL 45.50, IAW EA F-5310-T0359108. CATEGORY B REPAIR.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 57,898 hrs · 27,768 cycles

CORROSION FOUND ON SEAT TRACK AT BSTA 565 RBL 45.5. EVALUATED CORROSION FOUND ON SEAT TRACK AT BSTA 565 RBL 45.5, IAW SRM 53-00-52-1A AND FOUND OUTSIDE LIMITS. LIMIT 0.02" CLEAN UP 0.05". REPAIRED SEAT TRACK AT BSTA 565 RBL 45.5, IAW SRM 53-00-52-2R REPAIR 1 FIG 201. THIS IS A CATAGORY A MAJOR REPAIR. SEE ATTACHED JPF FOR DETAILS OF NDT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,856 hrs · 27,716 cycles

MDIS 915 33-50 2939 21NOV20 LGG FACT U. DURING SERVICE CHECK FOUND EMERGENCY LIGHT AT DOOR L1 INOPERABLE. REPLACED BULB, IAW AMM 33-51-01, TESTED ALL SATISFACTORY.

Part: DOOR — DELAMINATED (LT MLG) · airframe 57,446 hrs · 27,281 cycles

DAMAGE FOUND ON LH MLG DOOR DEPTH = 3.14, L= 27.77 W= 41.37 SEQ NO 000206 WRI 52801178 WO 00076120 PERFORMED REPAIR OF LH MLG DOOR FIBERGLASS PLYS IAW FEDEX REPAIR DRAWING SR 57- 52-01 REV A (SHEETS 1-3) SRM 51-70-00 SRM 52-80-02 AND 51-40-02 MATERIAL USED GLASS FABRIC BMS9-3/TH-3C7S7781 BN = 21263467SE ADHESIVE EA 9396 BN = 25315517MH SEALER EPIBOND 156 BN = 0191879419 SEALANT PS870 B1/2 BN = 28939709

Part: DOOR — UNKNOWN (L1) · airframe 57,423 hrs · 27,263 cycles

L1 DOOR DIFFICULT TO CLOSE AND LATCH. PERFORMED IAW AMM 52-11-00-2 OPS CHECK OF THE L1 DOOR SEVERAL TIMES ,FOUND GOOD SEQUENCE TO CLOSE AND LATCH FROM INSIDE AND OUTSIDE .A/C OK FOR SERVICE.

Part: COVER — MISINSTALLED (L1 DOOR) · airframe 57,415 hrs · 27,258 cycles

PDIS 915 52-10 1848 05DEC19 CDG FACT U LOGPAGES:2805999 DOOR L1 IS DIFFICULT TO ARM. FOUND COVER NOT PROPERLY INSTALLED, REINSTALLED DOOR SLIDE RAFT COVER AS PER AMM 25-66-01-4, SELECT LEVER MOVE TO ARM POSITION EASILY. A/C OK FOR SERVICE.

Part: ARMING LEVER — BINDING (L1 DOOR) · airframe 57,382 hrs · 27,229 cycles

PDIS 915 52-10 1789 13NOV19 CDG OPEN U LEFT FOWARD ENTRY DOOR IS VERY DIFFICULT TO ARM. NEED TO OPEN/CLOSE DOOR MULTIPLE TIMES TO ARM THE DOOR. REPEAT WRITE-UP. "MEL 52-11-01-A: L1 SLIDE INOP. INSPECTED 1L SLIDE AND GIRT BAR MECHANISME PER MM : 52-11-25-5 , ALL OK . PRECAUTIONNARY , CLEANED AND LUBRICATED GIRT BAR . MEL CLOSED , A/C READY FOR SERVICE .

Part: HANDLE — UNSECURE (R1 DOOR ARMING) · airframe 57,423 hrs · 27,263 cycles

DOOR 1R DIFFICULT TO ARM AND DISARM. DOOR 1R SLIDE AND GIRT BAR INSPECTED IAW AMM 25-66-01-6. FOUND GIRT RELEASE HANDLE PARTLY HANGING OUT. WHEN DOOR ARMED RELEASE HANDEL IS IS GOING BETWEEN FLOOR AND GIRT BAR. RELEASE HANDLE PUT CORRECT POSITION. DORR 1R ARMING CHECKED OK.

Part: HANDLE — UNDERSERVICED (LT FIRE) · airframe 57,347 hrs · 27,200 cycles

PDIS 915 76-15 1679 17OCT19 CDG OPEN U LOGPAGES:2941127 AT THE GATE , LEFT ENGINE WOULD NOT SHUTDOWN USING THE FUEL CONTROL SWITCH. THE SPAR VALVE WAS MOVING BUT THE ENG VALVE LGT WOULD ILLUMINATE WHEN THE F/C SW WAS PLACED OFF. FINALLY PULLED FIRE HANDLE. CHECKED LH ENG FIRE SW S37 AND FOUND 139 OHMS BETWEEN PIN 7 AND 19. REMOVED AND REPLACED LEFT ENGINE FIRE HANDLE AS PER AMM 26-21-02-4.PERFORMED LEFT ENGINE FIRE SWITCH INSPECTION CHECK IAW AMM 26-21-03-6, ALL CHECK SATISFACTORY.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 57,269 hrs · 27,122 cycles

SLIDE LIGHT ABOVE R1 DOOR DOES NOT ILLUMINATE WITH SLIDE ARMED. R1 DOOR ESCAPE SLIDE FLOOR RETAINER CLEANED AND TESTED IAW AMM 25-66-01 .OK.

Part: PAN — DAMAGED (FUSELAGE) · airframe 57,204 hrs · 27,061 cycles

MAIN CARGO DOOR JAMB LOWER SILL ACTUATOR PAN PUNCTURED REPLACED MAIN CARGO DOOR JAMB LOWER SILL ACTUATOR PAN IAW EA #F-5320-T0348051B AND SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (FLAP/SLAT SYSTEM) · airframe 57,163 hrs · 27,027 cycles

DURING PREFLIGHT, DISCOVERED TWO C/B'S PULLED AND FLAG WITH A WHITE "DANGER DO NOT OPERATE THIS UNIT" PLACARD. C/B'S "SLAT ALTERNATE POWER AND FLAP ALTERNATE POWER". RESETED CB'S "ALT FLAP PWR" & "ALT SLAT PWR" AND PERFORMED OPERATIONNAL TEST OF FLAP/SLAT ALTERNATE-(ELECTRIC) DRIVE SYSTEM IAW AMM 27-51-00-5. TEST OK. A/C OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 57,088 hrs · 26,973 cycles

PDIS 915 29-02 1209 02MAY19 BUD OPEN LOGPAGES:2826538 ON SHORT FINAL PASSING 800' EXPIERENCE L HYD SYS PRESS/L HYD QTY RUDDER RATIO/ CONTINUED TO LANDING RWY 31L STOPPING ABEAM CHARLY DUE TO LOSS OF ACFT STEERING. TB LEFT HYD QTY LOST TO ZERO FOUND LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR HOSE LEAKING IPC 32-32-51-16. ITEM 345. P/N INSTALLED AS115-06K0232 WAS PRE EO F-2920-7-5001. P/N MUST BE 271N6119-1 POST EO F-2920-7-5001. TEMPORARY FLEX LINE INSTALLED PER AMM 20-10-10-8. LINE P/N 271N6119-1 FOR POST EO F-2920-7-5001 INSTALLED FOR TERMINATING ACTION.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

CORROSION ON 2L LOWER DOOR GATE FOUND OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02- 1A, FIG 101, SHEET 7 , REV.125 REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.

Part: CLEAT — DENTED (L3 DOOR) · airframe 56,891 hrs · 26,770 cycles

DOOR 3L CLEATS BENT ON CENTER STRINGER, REPLACE. FABRICATED NEW CLEATS FOR DOOR 3L CTR STRINGER IAW DRAWING 146N6346 REV INITIAL AND GMM 7-0-1001 REV 153. INSTALLED NEW CLEATS IAW DRAWING 146N6313 REV K AND SRM 51-40-02 REV 125.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

LOWER CANTED BEAM UNDER WING TO BODY FAIRING 197AL B/S 1040-1060 CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71-1A ALLOWABLE DAMAGE 1, FIG 101, DETAIL IV AND VII, REV 125. INSTALLED NEW BEAM IAW SRM 51-40-02 REV 125 AND DRAWING 149N7553 REV C.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

WTB. CHORD CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101 DETAIL IV AND VII REV 125 REPAIRED CHORD IAW EA F-5340-T0344282 P1.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 56,891 hrs · 26,770 cycles

BS 231.21 BL0 FRAME DAMAGED AT FWD ACCESS DOOR LATCH FITTING. REPAIRED FRAME AT BS 231.21 B/L0 IAW SRM 53-00-07 REPAIR 7 REV 125.

Part: MOUNT — DAMAGED (FUSELAGE) · airframe 56,891 hrs · 26,770 cycles

FWD LAV UPPER I/B FWD MOUNT IS DAMAGED ON FRAME B/S 297 BETWEEN S2L AND S3L, REPLACEMENT REQD. FABRICATED AND INSTALLED NEW MOUNT P/N 232N2003-4 IAW SRM 51-40-02 REV 125 AND DRAWING 232N2003 REV A.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 56,891 hrs · 26,770 cycles

CREASE BEAM WEB DAMAGED BS 1016 RBL 64 REPLACEMENT REQD. REPLACED CREASE BEAM WEB IAW SRM 53-40-13-1A REV 125 AND DRAWING.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

KEEL BEAM WEB TEE CORRODED OUT OF LIMITS IAW SRM 53-00-71-1A FIG 101 DETAIL III AND DETAIL VII REPLACE AS REQD. KEEL BEAM TEE REPLACED IAW SRM 51-40-02 REV 125 AND DRAWING 144N8140 REV E.

Part: GATE — WORN (L4 DOOR) · airframe 56,891 hrs · 26,770 cycles

WEAR MARK ON DOOR 4L LOWER GATE AFT O/B. EDGE OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.

Part: GATE — DAMAGED (R4 DOOR) · airframe 56,891 hrs · 26,770 cycles

WEAR MARK ON DOOR 4R LOWER GATE OUTSIDE OF ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 56,891 hrs · 26,770 cycles

DENT FOUND ON FLOOR PANEL BSTA 560-680 LBL 25-45. FLOOR PANEL REPAIRED AT BSTA 560-680 LBL 25-45 IAW SRM 53-00-50-2R FIG 201 REV 125.

Part: GATE — CORRODED (R2 DOOR) · airframe 56,891 hrs · 26,770 cycles

LOWER DOOR GATE 2R HAS CORROSION OUTSIDE ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACED DOOR GATE IAW AMM 52-11-38-4 REV 122.7.

Part: SEAT TRACK — CORRODED (BS 1204-1210) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

EVIDENCE OF CORROSION ON SEAT TRK BSTA 1204-1210 RBL 58.22 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABLE CLEANUP = 0.017" , MAX DEPTH OF CLEAN UP = 0.060" SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 3 REV 125 AND EA.#:F-5310- T0344017 P1

Part: ANGLE — CORRODED (LE SLAT) · airframe 56,891 hrs · 26,770 cycles

LT WING, RIVETS DAMAGED ON OT/BD TRAILING EDGE WEDGE OF NR 5 LE SLAT REPLACED CORRODED CLOSURE ANGLE TO SLAT NR 5 T/E WEDGE O/B END IAW EA T F-5750-T0344281 A P1 "WING -FLIGHT SURFACES-OUTBD CLOSURE ANGLE - SLAT NR 5 - CORROSION. THIS REPAIR IS CLASSIFIED AS MAJOR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

FITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 CORRODED. EVA AND RECTIFY FITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 REPLACED IAW SRM 51-40-02 REV 125.

Part: SEAT TRACK — CORRODED (BS 1188-1200) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

SUSPECT CORROSION AT B/S 1180-1200 LBL 24.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABLE CLEANUP = 0.017" , MAX DEPTH OF CLEAN UP = 0.021" SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 3 REV 125 AND EA.#:F-5310- T0344052 P1

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING, CORROSION ON UPPER SURFACE, ABOVE FRONT SPAR, WS 642 TO WS 654 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING, CORROSION ON UPPER SURFACE, 22" AFT OF FRONT SPAR AT WS 204.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING, CORROSION ON UPPER SURFACE, AS OF REAR SPAR WS 289-293 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING CORROSION ON UPPR SURFACE AFT OF REAR SPAR, WS312 TO WS316 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW FEDEX EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (ZONE 500) · airframe 56,891 hrs · 26,770 cycles

LT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 300 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOUND TO BE OUTSIDE OF LIMITS DUE TO LOCATION OF DAMAGE. REPAIR CARRIED OUT IAW EA # F-5730-T0344299 P1.

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 269 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (RT WING) · airframe 56,891 hrs · 26,770 cycles

RT WING, CORROSION ON UPPR SURFACE, ABOVE REAR SPAR AT WS 361 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW EA # F-5730-T0344253. P1

Part: SKIN — CORRODED (LT WING) · airframe 56,891 hrs · 26,770 cycles

LT WING UPPER TE, EVIDENCE OF CORROSION ADJACENT TO FASTENER HEADS AT AREA 5 INCHES AFT OF REAR SPAR AND 67 INCHES OUTBOARD OF WING ROOT FAIRING 195AL REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOUND TO BE OUTSIDE OF LIMITS DUE TO LOCATION OF DAMAGE. REPAIR CARRIED OUT IAW EA # F-5730-T0344299 P1.

Part: SKIN — CORRODED (LT WING) · airframe 56,891 hrs · 26,770 cycles

LT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 215 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOUND TO BE OUTSIDE OF LIMITS DUE TO LOCATION OF DAMAGE. REPAIR CARRIED OUT IAW EA # F-5730-T0344299 P1.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

LT WING, UPPER SURFACE RSS 170 TO RSS 200 AT WING SKIN AND TRAILING EDGE PANEL JOING SUSPECT CORROSION. COROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1 REV 125. REPAIR CARRIED OUT IAW EA #F-5730-T0344090 P1.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 56,891 hrs · 26,770 cycles

FLOOR PANEL 251 MXF CRACKED REPAIRED FLOOR PANEL 251 MXF I.A.W. 53-00-50-2R FIG 201 REV125

Part: SEAT TRACK — CORRODED (BS 1180-1230) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

EVIDENCE OF CORROSION ON SEAT TRK BS1180-1200 RBL 47 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABLE CLEANUP = 0.017" , MAX DEPTH OF CLEAN UP = 0.028" SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 3 REV 125 AND EA.#:F-5310- T0344054 P1

Part: SKIN — CORRODED (LT WING) · airframe 56,891 hrs · 26,770 cycles

PLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS.748 TO WS761, 2 INCHES FWD OF REAR SPAR AND TRILING EDGE PANEL JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOUND TO BE OUTSIDE OF LIMITS DUE TO LOCATION OF DAMAGE. REPAIR CARRIED OUT IAW EA # F-5730-T0344299 P1.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 56,891 hrs · 26,770 cycles

FLOOR PANEL CRACKED 252MUF FLOOR PANEL REPAIRED IAW SRM 53-00-50 FIG 201 RPR # 00001. SHEET 001.

Part: SKIN — CORRODED (LT WING) · airframe 56,891 hrs · 26,770 cycles

PLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125 EVALUATED BLEND OUT AND FOUND AREA TO BE OUT OF LIMITS IAW DUE TO LOCATION OF DAMAGE IAW SRM.

Part: BOLT — SHEARED (CRGO DOOR ACT) · airframe 56,891 hrs · 26,770 cycles

MAIN CARGO DOOR FWD HOOK LATCH ACTUATOR BELLCRANK WAS FOUND TO HAVE A SHEARED BOLT. REPLACED MAIN CARGO DOOR FWD HOOK AND ATTACHING BELLCRANK IAW CMM 52-32-03 REPLACED FWD HOOK ATTACH BOLTS IAW SRM 51-40-02 PRFORMED ADJUSTMENT CHECK OF MAIN CARGO DOOR FWD HOOK AND BELL CRANK IAW AMM 53-32-00-5 PERFORMED OPERATIONAL CHECK OF MAIN CARGO DOOR IAW AMM 52-32-00-0.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

EVIDENCE OF CORROSION ON CREASE BEAM BSTA 1052-1180 RBL 64 CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 1052 AND BS 1145 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWING 144N5214 DRAWING 144N5200 AND EA F-5310-T0344019 PART 1 (P1).

Part: SKIN — CORRODED (LT WING) · airframe 56,891 hrs · 26,770 cycles

PLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101 TABLE III, FLAG NOTE H, REV 125. AND FOUND TO BE OUTSIDE LIMITS DUE TO LOCATION OF DAMAGE. REPAIR CARRIED OUT IAW EA # F-5730-T0344299 A P1.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

EVIDENCE OF CORROSION ON CREASE BEAM BS907-936 RBL64. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 936 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWING 144N5152 DRAWING 144N5140 AND EA F-5310--T0344018 PART 1 (P1).

Part: SEAT TRACK — CORRODED (BS 1188-1200) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

EVIDENCE OF CORROSION ON SEAT TRK BS1188-1200 LBL 45 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABLE CLEANUP = 0.017" , MAX DEPTH OF CLEAN UP = 0.027" SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 3 REV 125 AND EA.#:F-5310- T0344053 P1

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

RT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. ALLOWABLE MINIMUN REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.148 REPAIR CARRIED OUT IAW EA F-5730-T0343998 AND SRM 57-20-01-2R REPAIR 7 REV 125.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 56,891 hrs · 26,770 cycles

LT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. REV 125 ALLOWABLE MINIMUM REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.145" REPAIR CARRIED OUT IAW EA F-5730-T0343997 P1 AND SRM 57-20-01-2R REPAIR 7 REV 125.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,717 hrs · 26,600 cycles

DURING A DAILY CHECK, FOUND THE L1 DOOR INTERIOR EMERGENCY LIGHT WAS NOT WORKING WITH THE COCKPIT SWITCH OR TEST PB. REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2. OPS CHECKED THE EMERGENCY LIGHTS, NORMAL.

Part: CAM — DEFORMED (CARGO DOOR) · airframe 56,224 hrs · 26,286 cycles

FOUND THE MAIN DECK CARGO DOOR CAM LATCH NR 7 LIP DEFORMED. REMOVED AND REPLACED THE CAM LATCH IAW MM 52-32-00-0-0. ADJUSTED AND TEST PERFORMED IAW MM 52-32-00-05. TESTED OK.

Part: LIGHT — INOPERATIVE (RT DOOR SLIDE) · airframe 55,965 hrs · 26,105 cycles

RIGHT DOOR SLIDE ARM LIGHT NOT ILLUMINATED WHEN FIRST OFFICER WENT TO DISARM THE DOOR. RT DOOR SLIDE ARM LIGHT FILLARMENTS REPLACED IAW AMM 33-20-00. OPS TESTED GOOD.

Part: GIRT BAR — CONTAMINATED (ZONE 800) · airframe 55,950 hrs · 26,085 cycles

LEFT DOOR ARMING HANDLE IS STIFF TO MOVE TO THE ARM POSITION AMM 25-66-10-2. GIRT BAR FLOOR FITTINGS FOUND CONTAMINATED WITH DEBRIS. FITTINGS CLEANED AND DEBRIS REMOVED. DOOR ARMING NOW SATISFACTORY TO CREW.

Part: FMC — MALFUNCTIONED (RIGHT) · airframe 55,863 hrs · 26,012 cycles

ON TWO OCCASIONS DURING FLIGHT, RT FMC GAVE INCORRECT PITCH COMMANDS TO AUTOPILOT. R & R THE RT FMC IAW AMM 34-61-01-4-2.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 55,815 hrs · 25,968 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL AT POSITION 6R IS DAMAGED. REPAIRED MAIN CARGO FLOOR PANEL AT POSITION 6R IAW SRM 53-00-50, REV 121.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 55,815 hrs · 25,968 cycles

MAIN CARO BAY FLOOR PANEL 6R IS DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50, REV 121.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 55,793 hrs · 25,949 cycles

CABIN ALTITUDE EICAS WARNING AT FL380. COMPLIED WITH QRH, DESCENDED TO FINAL ALTITUDE FL250. RECOVERED CABIN PRESSURE IN AUTO 2 AT CABIN ALTITUDE 7500. NORMAL DESCENT AND PRESSURE UNTIL LFPG. REPLACED THE NR 1 CPC IAW MM 21-31-02-4, TESTED OK. COMPLYED WITH CABIN PRESSURE DECAY CHECK IAW MM 05-51-24-2, TEST PASSED.

Part: SEAL — DAMAGED (FLAP MODULE) · airframe 55,573 hrs · 25,774 cycles

LOST ALL LT HYD FLUID AT LEVEL OFF FL 380. FOUND LT WHEEL WELL, FLAP/SLAT DEPRESS MODULE LEAKING FROM A CAP. FOUND SEAL DAMAGED, REPLACED THE SEAL IAW SMP. LEAK CHECK PERFORMED IAW AMM 29-00-00-6, NO LEAKS FOUND.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 55,563 hrs · 25,768 cycles

R1 DOOR WON'T ARM. RIGHT DOOR GIRT BAR ADJUSTED AS PER AMM 25-66-10-2. OPS CHECK OK. DOOR CAN ARM NORMALLY.

Part: PROXIMITY SENSOR — MALFUNCTIONED (R1 DOOR) · airframe 55,452 hrs · 25,687 cycles

VERBAL REPORT FROM FLIGHT CREW. RT DOOR 1 SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED. TROUBLESHOT AND FOUND PROXIMITYSENSOR M10116 BAD, REPLACED THE SENSOR IAW MM 25-66-11-2, CHECKED OK. ACFT OK FOR SERVICE.

Part: SKIN — CORRODED (RT WING) · airframe 55,447 hrs · 25,682 cycles

RIGHT WING LOWER SKIN HAS CORROSION. REPAIRED IAW EA F-5730-T0329901.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 55,447 hrs · 25,682 cycles

LEFT ELEVATOR FOUND DEBONDED ON UPPER AND LWR SKIN AT PREVIOUS REPAIR AREA. REPLACED THE LEFT ELEVATOR IAW AMM 27-31-01.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 55,447 hrs · 25,682 cycles

THE RT INBOARD MAIN FLAP DENTED 20 INCHES FROM OUTBOARD EDGE OF FLAP AND 23 INCHES FROM AFT EDGE OF FLAP. REPAIRED IAW SRM 57-53-01, 57-53-01 AND SRM 51-70-10.

Part: HINGE — DAMAGED (NR 1 NACELLE) · airframe 55,447 hrs · 25,682 cycles

FOUND NR 1 ENGINE INBD AFT HINGE BOLT HOLE DAMAGED. REPAIRED IAW EA TF-5450-T0328068P2.

Part: GATE — CORRODED (L1 DOOR) · airframe 55,447 hrs · 25,682 cycles

L1 DOOR CORROSION FOUND ON LOWER GATE, CORROSION BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. THE GATE WAS REPLACED IAW CMM 52-11-05 REV.120, AND AMM 52-11-38-4 REV.117

Part: GATE — CORRODED (R1 DOOR) · airframe 55,447 hrs · 25,682 cycles

CORROSION ON R1 DOOR LOWER GATE, BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 ALLOWABLE DAMAGE 1 REV119. THE GATE WAS REPLACED IAW CMM 52-11-05 REV.120

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 55,447 hrs · 25,682 cycles

RT INBD SLAT NR 6 T/E WEDGE DELAMINATION FOUND. REPLACED THE SLAT IAW AMM 27-81-01

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTING STRIKE ON SKIN PANEL BS 648, 3" BELOW STR 27R. REPAIRED LIGHTNING STRIKE IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTING STRIKE ON FASTENER BS 247, 15" BELOW STR 29R. REPAIR LIGHTNING STRIKE IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTNING STRIKE ON SKIN PANEL BS 701, 3" BELOW STR 23R. REPAIRED LIGHTNING STRIKE IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTNING STRIKE COVERED BY PAINT FOUND AT BS 244 16" BELOW STRINGER 20R. REPAIRED LIGHTNING STRIKE IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 55,447 hrs · 25,682 cycles

CUSTOMER REQUEST SLAT 8 T/E WEDGE TO BE MAPPED FOR DAMAGE AND REPAIRED. SLAT REPAIRED IAW EA F-5750-T0329709

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTNING STRIKE ON FASTENER BS 297, 2" ABOVE STR 23R. REPAIRED LIGHTNING STRIKE IAW SRM.

Part: SKIN — BURNED (BS 520) · airframe 55,447 hrs · 25,682 cycles

LIGHTENING STRIKE COVERED BY PAINT FOUND @ BS 520 2" BELOW STRINGER 22 R/H. REPAIRED LIGHTNING STRIKE IAW SRM 53-00 -01 FIG 201 REPAIR 6 REV 119 .

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,447 hrs · 25,682 cycles

LIGHTNING STRIKE ON SKIN PANEL B/S 431-5, 2" BELOW STR 21R. REPAIRED LIGHTNING STRIKE IAW SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,442 hrs · 25,678 cycles

DURING SERVICE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-51-06-2-1 REV 117. TESTED GOOD.

Part: HINGE — DAMAGED (THRUST REVERSER) · airframe 55,373 hrs · 25,604 cycles

NR1 ENGINE, INBD THRUST REVERSER AFT HINGE HAS A SHEARED BOLT. REPLACE THE HINGE FITTING IAW EA F-540-T0328068

Part: CONTROL UNIT — LACK OF LUBE (AILERONS) · airframe 54,982 hrs · 25,320 cycles

STIFFNESS ON ROLL AXIS ON BOTH CAPTAIN & COPILOT CONTROLS. TROUBLE SHOT FOLLOWING TECH TIPS NR 15-0019 & FIM 27-11. INSPECTED & CLEANED ROD COMING TO LATERAL OVERRIDE QUADRANT & FEEL CENTERING & TRIM MECHANISM, NO DEFECTS FOUND. THEN INSPECTED LT, RT PCUS & LT. RT BREAKOUT QUADRANT. FOUND RT & LT PCUS DRY, PCUS NEEDED A LOT OF GREASE SERVICING. SERVICED ALL PCUS IAW AMM 12-21-07-03. NO MORE DEFECT FOUND. PERFORMED LT & RT AILERONS CHECK IAW AMM 27-11-00-5. OPERATIONS & CHECK OK. ACFT OK FOR SERVICE.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 54,744 hrs · 25,182 cycles

DURING SERVICE CHECK, FOUND THE EXTERIOR EMERGENCY LIGHT ON FWD RT DOOR INOPERATIVE. BULB REPLACED BUT LIGHT STILL INOPERATIVE. CLEANED LAMP SUPPORT & TIGHTENED THE SOCKET. PERFORMED ADJUSTMENT TEST IAW AMM 33-51-00-5, FOUND SATISFACTORY.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 544 hrs · 24,870 cycles

EICAS DISPLAY LIT UP WITH ORAL TONE AND RT ENGINE FIRE, LT ENGINE FIRE, FLAP WARNINGS, CABIN ALTITUDE, SEL CALL, UTILITY BUSS OFF, MAIN CARGO DOOR AND SEVERAL OTHERS. DURING LANDING INDICATIONS WERE NORMAL. ON S/DOWN HAD EQPT CLOGGED FAN AND HYD GEN ON, ON STATUS PAGE. NEVER HAD A MASTER CAUTION LIGHT, JUST EICAS & TONE. BOTH REV. INDICATIONS WERE SHOWN FLASHING AND TAI INDICATOR ON ENG NR 2 WAS DISPLAYED. IF EICAS COMP SWITCH SELECTOR IS TURNED RT COMP, "EQPT CLG FAN" AND "HYD GEN ON" WILL NOT TRANSFER (DISPLAYED ON EICAS SCRN), WHEN TURNED BACK TO AUTO/LFT, BOTH MSG APPEAR AGAIN. ACCMPLSHD EICAS COMP TEST PER AMM 31-41-00/501. LT AND RT TEST SHOW NO INTRFC FAULTS, NO INT FAULTS. PICS . T/O CONF TEST, LDG CONF TEST, GND PROX TEST, EQUIP COOL TEST, YAW DAMP L R TEST, DUCK LEAK TEST, FUEL QTY TEST, WINDOW/PRBE HEAT TEST, AIR DATA COMP. L R TEST AND STALL L R TEST. ALL OF THIS TEST GOOD. REGARDING THE "HYD GEN ON" EICAS MESSAGE WORKED IAWFIM 24-25 FLT TREE 803 AND ERSD MSG. ALSO ERSD "EQPT CLG FAN" MSG IAW FIM 31-41-00/101 FAULT TREE 819.AT NEXT WORKED IAW FIM 31-41 FAULT TREE 811 (EICAS BITE PROCEDURE) AND NO FAULTS NOTED ON LEFT NOR RIGHT EICAS COMPUTERS. PRECAUTIONARY REMOVED AND REPLACED LEFT EICAS COMPUTER IAW AMM 31-41-02/401 AND PERFORMED AGAIN AN EICAS BITE PROC WITH NO FAULTS. PERFORMED ENGINE RUN FOR BOTH ENGINES IAW RUN-UP HANDBOOK WITH NO FAULTS. ACFT OK FOR SVC.

Part: TRANSMISSION — LOW (TE FLAP) · airframe 543 hrs · 24,809 cycles

WHEN PUTTING FLAPS FROM 20 TO 25, TE FLAP DISAGREE EICAS WARNING CAME ON. FLAPS STAYED AT 20. WENT AROUND & FOLLOWED QRH. RETURNED TO AIRPORT FOR UNEVENTFUL 20 FLAP LANDING. TROUBLE SHOT SYS IAW FIM 27-51 FT 808. FOUND NO FLAP OVERLOAD INDICATORS TRIPPED. INSPECTED ALL FLAP TRANSMISSIONS FLUID LEVELS & FOUND LT INBD FLAP TRANSMISSION FLUID LEVEL LOW. SERVICED LT INBD FLAP TRANSMISSION IAW AMM 12-13-06-3. ALSO LUBRICATED ALL FLAP SYS IAW AMM 12-21-09-3. CARRIED OUT FLAP SYS OPERATIONAL CHECK IAW AMM 27-51-00-5. ALL OPERATIONS SATISFACTORY. OK FOR SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

SURFACE CORROSION ON SKIN. CORROSION REMOVED IAW SRM 53-00-01 & FOUND TO BE WITH IN SRM LIMITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

PREVIOUS LIGHTNING STRIKE OBSERVED ON THE LT FUSE SKIN & STILL SHOWS SIGNS OF BURNING. LOCATED 4 INCHES BELOW STRINGER 23 BS 666. PREVIOUS LIGHTNING STRIKE OBSERVED ON THE LT FUSE SKIN LOCATED ON THE LT FUSE SKIN LOCATED 4 INCHES BELOW STRINGER 23 BS 666. DAMAGE REMOVED & REPAIRED IAW SRM 53-00-01 REPAIR 6 SECTION I ARE NDT INSPECTED & FOUND DEFECT FREE. CLASSED AS MAJOR REPAIR CAT A.

Part: SKIN — DAMAGED (BS 560) · airframe 54,027 hrs · 24,581 cycles

PREVIOUS LIGHTNING STRIKE BLEND OBSERVED ON THE LT FUSE SKIN & STILL SHOWS SIGNS OF BURNING. LOCATED BS 560 BETWEEN STRINGERS 24 - 25. REPAIRED IAW SRM 53-00-01 REPAIR 6. CLASSED AS MAJOR CAT A REPAIR.

Part: SKIN — DAMAGED (BS 360) · airframe 54,027 hrs · 24,581 cycles

EXTERIOR SKIN PANEL, BELOW AFT CORNER OF R1 DOOR CUT OUT, BS 360 STRINGER 17R. REPAIRED IAW SRM 51-40-02 AND EA F-5330-T0313464.

Part: SKIN — GOUGED (BS 340) · airframe 54,027 hrs · 24,581 cycles

EXTERIOR SKIN PANEL, BELOW FWD CORNER OF DOOR 1 RT CUT OUT APPROX BS 340 STRINGER 17R. REPAIRED IAW EA F-5330-T0313464

Part: FLOORBEAM — DAMAGED (BS 680) · airframe 54,027 hrs · 24,581 cycles

BS 680 FLOORBEAM TOP CAP DOUBLER DAMAGED. REPLACED IAW F-5310-T0313468. REPAIRED AND DOUBLER REPLACED IAW EX F-5310-T0313468.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

DOOR 1 RT, FUSELAGE EXTERIOR SKIN BELOW LOWER SILL, STRINGER 17R, APPROX STATION 345, FASTENER HEAD FOUND PARTIALLY DRILLED.

Part: FLOORBEAM — DAMAGED (BS 760) · airframe 54,027 hrs · 24,581 cycles

BS 760 FLOORBEAM DOUBLER DAMAGED. FLOORBEAM DOUBLER REPLACED & TOP CAP REPAIRED IAW EA F-5310-T0313469.

Part: FASTENER — WRONG PART (LE SLAT) · airframe 54,027 hrs · 24,581 cycles

PREVIOUS REPAIR FOUND WITH INCORRECT FASTENERS INSTALLED ON NR 9 SLAT FASTENERS. REPLACED IAW EA F-2780-123876C.

Part: FASTENER — WRONG PART (LE SLAT) · airframe 54,027 hrs · 24,581 cycles

PREVIOUS REPAIR FOUND WITH INCORRECT FASTENERS INSTALLED ON NR 9 SLAT FASTENERS. INSTALLED IAW EA F-2780-123876C.

Part: SKIN — BURNED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE, AT 1360 - 1380 STRINGER 21 - 22, IN POCKET REPAIR IAW SRM 53-00-01. REPAIR 6 IS RESTRICTED BY RVSM REQUIREMENTS 51.10.01 FIG 7 & 53-00-01 FIG 201.

Part: SKIN — BURNED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

SUSPECT LIGHTNING STRIKE TO 5 FASTENERS AT STATION 500 STRINGER 26LT. LIGHTNING STRIKE DAMAGE AT 5 FASTENERS REPAIRED IAW EA F-5330-T0313473.

Part: SKIN — DENTED (TE FLAP) · airframe 54,027 hrs · 24,581 cycles

LEFT INBD FLAP UPPER SURFACE DENTED & POSSIBLY CRACKED. COMPOSITE REPAIR CARRIED OUT IAW 57-53-01 FOR TRACKING OF REPAIR, SEE EA F-5750-T0313689.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 54,027 hrs · 24,581 cycles

SLAT NR 4 HAS DELAMINATION APPROX 2 INCHES X 3 INCHES ON INBD EDGE LOWER SURFACE AT EXTERNAL DOUBLER SLAT. REMOVED, REPAIRED & REFITTED IAW AMM 27-81-02 & EA F-5750-TO312973.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

UPON REMOVAL OF UPPER FUSELAGE VHF ANTENNA LIGHT CORROSION FOUND ON SKIN. CORROSION REMOVED, SKIN REMAINING THICKNESS CHECKED TO PRODUCTION DWG. NDT HFEC CHECKS CARRIED OUT. REMOVED MATERIAL WITHIN SRM LIMITS MAXIMUM 0.003" 6"X1".

Part: SUPPORT — MISSING (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

DOOR 1L LOWER SILL, GUTTER SUPPORT STRUCTURE MISSING FROM STATION 365.25 TO 377.0. NEW SUPPORT STRUCTURE INSTALLED IAW DWGS 141N5170 & 141N8322.

Part: SKIN — DAMAGED (BS 700) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE BS 700 STRINGER 23L. REPAIRED IAW SRM 53.00.01 REPAIR 6.

Part: FASTENER — WRONG PART (NR 2 PYLON) · airframe 54,027 hrs · 24,581 cycles

NUMBER 2 PYLON UPPER DRAG LINK ATTACHMENT FITTING ON PYLON UPPER SURFACE HAS 3 LOOSE LOCK FASTENERS VERTICALLY THROUGH FITTING BELOW DRAG LINK ATTACHMENT FUSE PIN. FASTENERS REMOVED, FOUND TO BE INCORRECT DASH LENGTH FITTED WITH INCORRECT QTY OF WASHERS. DIMENSION OF HOLES INSPECTED, NDT INSPECTION OF HOLES CARRIED OUT, CORRECT LOCK FASTENERS & WASHER COMBINATION REFITTED SRM 54-50-90.

Part: SKIN — DAMAGED (BS 680) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE BS 680 BELOW STRINGER 23L. REPAIRED IAW EA F-5330-T0313342.

Part: SKIN — DAMAGED (ZONE 100) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE BS 740 BELOW STRINGER 23L. REPAIRED IAW IAW SRM 53.00.01 REPAIR 6 AND 53.00.01 FIG 101.

Part: SKIN — DAMAGED (BS 231) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE ON FWD LT FUSELAGE SKIN AT BS 231.25 STRINGER 25 - 26L.. REPAIRED IAW SRM 53.00.01 REPAIR 6.

Part: SKIN — DAMAGED (BS 223) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE ON FWD LOWER LT FUSELAGE SKIN TWO INCHES AFT OF BS 223 STRINGER 25 - 26L. REPAIRED IAW IAW SRM 53-00-01 REPAIR 6.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

SUSPECT LIGHTNING STRIKE FUSE SKIN BS 1360 - 1380 LT APPROX 10 INCHES FROM STATIC PORT. LIGHTNING STRIKE DAMAGE REPAIRED WITH FASTENER INSTALLATION IAW SRM 53-00-01 REPAIR 6 & SRM 51-10-01 FIG 1.

Part: SKIN — DAMAGED (BS 215) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE ON SKIN BS 215 STRINGER 25 - 26L. REPAIRED IAW SRM 53-00-01 REPAIR 6.

Part: SKIN — GOUGED (BS 220-223) · airframe 54,027 hrs · 24,581 cycles

GOUGE FOUND ON FUSELAGE SKIN AT BS 220 - 223 STRINGERS 25 - 26L. REPAIRED IAW EA F-5330-T0313528A.

Part: SKIN — DAMAGED (BS 215) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE ON SKIN TWO INCHES FWD OF BS 215 AT STRINGER 25 - 26L. REPAIRED IAW IAW SRM 53-00-01 REPAIR 6 AND SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE FOUND BS 700 STRINGER 23L.

Part: SKIN — DAMAGED (FDEA201411043483) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE BS 231.25 LBL 20 ON FASTENER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE FOUND BS 680 BELOW STRINGER 23L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE FOUND BS 740 BELOW STRINGER 23L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE FOUND BS 215 LBL 20 ON FASTENER HEAD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,027 hrs · 24,581 cycles

LIGHTNING STRIKE FOUND BS 225 LBL 20 ON FASTENER HEAD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 53,099 hrs · 23,745 cycles

DURING SERVICE CHECK FOUND RT SLIDE LIGHT FWD EMERGENCY BURNED. REPLACED LAMPS IAW AMM 33-51-06-2-1. TESTED AND WORKS PROPERLLY. RIGHT SLIDE LIGHT FWD EMERGENCY OK TO CONTINUE.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 53,098 hrs · 23,744 cycles

CREW REPORTED R1 DOOR SLIDE PARTIALLY DROPPED. REPOSITIONED SLIDE IAW MM:25-66-01-4. ALSO FOUND EMERGENCY RESERVOIR EMPTY. R & R SAME IAW MM:52-11-30-4. ALL CHECKED OK. ACFT OK TO CONTINUE.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 52,646 hrs · 23,350 cycles

L1 DOOR SLIDE PARTIALLY DEPLOYED ON OPENING. R & R L1 SLIDE PER MM 25-66-01-4. CHECKED OK, ACFT OK FOR SERVICE.

Part: SKIN — GOUGED (DOOR) · airframe 52,062 hrs · 22,824 cycles

MEC BAY DOOR 119BL EXTERNAL SKIN HAS DAMAGE AROUND EXTERIOR HANDLE CUTOUT MEC DOOR HANDLE AND EXTERIOR SKIN REPLACED.

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 52,062 hrs · 22,824 cycles

SURFACE CORROSION TO INTERNAL SKIN OF ACCESS PANEL 623HR. REPAIR CARRIED OUT IAW SRM AND EA F-5743-154347.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,062 hrs · 22,824 cycles

RBL 14, BS 345-377 SEAT TRACK FOUND CORRODED. SEAT TRACK REPLACED IAW SRM 51-40-02 AND 53-10-52.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 52,062 hrs · 22,824 cycles

RIGHT WING AFT FLAP, CRACK FOUND IN FITTING, FITTING REPLACED.

Part: RETAINER — CRACKED (ZONE 500) · airframe 52,062 hrs · 22,824 cycles

RETAINER FOUND CRACKED, RETAINER REPLACED.

Part: SKIN — DAMAGED (BS 1460) · airframe 52,018 hrs · 22,777 cycles

LIGHTNING STRIKE ON SKIN AT BS 1460 REPAIRED IAW SRM 53-00-01 AND EA F-5360-154332.

Part: PROBE — MALFUNCTIONED (TAT) · airframe 52,010 hrs · 22,768 cycles

ON ROTATION , RECEIVED "TAT PROBE" EICAS MESSAGE, AUTO-THROTTLES STAY DISCONNECTED, AUTOPILOTS WOULD NOT ENGAGE, MCP VNAV AND LNAV INPUTS WERE LOCKED UP AND FLIGHT DIRECTOR GUIDANCE NOT AVAILABLE. REPLACED K410 TAT PROBE CURRENT SENSING RELAY AS PER STANDARD MAINTENANCE PRACTICES. REPLACED TOTAL AIR TEMPERATURE PROBE AS PER B757 AMM 34-12-02-4. PERFORMED OPERATIONAL CHECK OF TAT PROBE AS PER AMM 30-33-00-5. OPERATIONAL CHECK FOUND OK. REMOVED AND REPLACED RELAY K10264 IAW AMM 20-60-00. TAT PROBE HEAT OPS CHECKED OK.

Part: RESERVOIR — EMPTY (DOOR ASSIST) · airframe 51,805 hrs · 22,640 cycles

DURING SERVICE CHECK, FOUND CREW DOOR ENTRY L1 EMERGENCY POWER RESERVOIR PRESSURE GAGE AT ZERO PSI. L1 DOOR POWER ASSIST BOTTLE REPLACED IAW AMM52-11-30-4.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 51,795 hrs · 22,629 cycles

LEFT CREW ENTRY DOOR SLIDE CAME OUT OF CONTAINER BUT DID NOT DEPLOY, AS F/O AND MX ATTEMPTED TO CLOSE DOOR. SLIDE REMOVED IAW 25-66-01-004-154. INSTALLED ESCAPE SLIDE ON L1 DOOR IAW AMM 25-66-01-4-0. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (ZONE 100) · airframe 50,679 hrs · 21,834 cycles

DENT STA 1700 STR 16L. DENT IS ON A PREVIOUS REPAIR AND DENT GOES ACROSS SEVERAL FASTENER HEADS. REMOVED PREVIOUS REPAIR IAW SRM 51-40-01, REWORKED AREA TO ORIGINAL CONTOUR IAW SRM 51-70-01, FABRICATED NEW DOUBLER USING 2024T-3 .050 DIMS 14.5" X 9", FILLER USING 2024T-3 .040 DIMS 4.6250" X 1.7500", 3 SHIMS USING 2024T-3 .040 DIMS 5.7500" X 5.8750", 5.8750" X 1.7500" AND 5" X 3", TAPER SHIMS 2 EACH USING 2024T-3 .050 DIMS 5.2500" X 1.3750" IAW SRM 53-00-01 AND INSTALLED IAW SRM 53-00-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,679 hrs · 21,834 cycles

DENT ON RT FUSELAGE AT FS 524 STR 25R CUT-OUT DAMAGED AREA DIMS 3" X 3", FABRICATED DOUBLER USING 2024T-3 .071 DIMS 12.5" X 10", FILLER USING 2024T-3 .063 DIMS 3" X 3", SHIMS USING 2024T-3 .016 DIMS 8.75" X 5", 14.25" X 5.75", AND 3.5" X 3.5", 2 EACH TAPER SHIMS USING 2024T-3 .071 DIMS 5" X 1" EACH, STRINGER SHIM USING 2024T-3 .016 DIMS 5" X 1" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-00-01.

Part: SEAT TRACK — DAMAGED (BS 582) · airframe 50,679 hrs · 21,834 cycles

SEAT TRACK DAMAGED AT STA 582, LBL 45.5. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION USING BAC1520-792, 7178T6511, DIMS 241" LONG AND INSTALLED IAW EA F-5320-139586 "FUSELAGE - SEAT TRACK - INTERIM REPAIR OF SEAT TRACK LUG DAMAGE AT STA 582 LBL 45.5".

Part: SEAT TRACK — DAMAGED (BS 582) · airframe 50,679 hrs · 21,834 cycles

SEAT TRACK DAMAGED AT STA 582 LBL 45.5.

Part: OIL SYSTEM — LEAKING (LEFT ENGINE) · airframe 50,475 hrs · 21,728 cycles

APPROX 80K ON TAKEOFF MASTER WARNINGS LIGHTS ILLUMINATED. CARGO FIRE HORN SOUNDED. MAIN CARGO FIRE ECIAS. LIGHT HAZY SMOKE IN COCKPIT. T/O REJECTED. MAIN CARGO FIRE CHECKLIST ACCOMPLISHED. FIRE DEPT SCANNED ACFT FOR HEAT. NONE PRESENT. PERFORMED AN OPS CHECK OF MAIN DECK SMOKE DETECTORS REF AMM SUP 26-16-30. NO DEFECTS NOTED. DRAINED 2 QTS FROM RT ENG, QTY SHOWS 19 QTS WITH CREW ON BOARD RAN BOTH ENGINE TO TAKEOFF PWR. BOTH PACKS ON WITH LT AND RT BLEEDS OPEN. AT TAKEOFF PWR WE HAD HAZY SMOKE IN ACFT. BROUGHT ENGINE TO IDLE AND SHUTOFF RT BLEED. WITH CROSSFEED OPEN AND BOTH PACKS ON, LT ENG BLEED OPEN, BROUGHT BOTH ENGINES TO TAKEOFF AND NO SMOKE OR HAZE IN SYS. SYS OPS CHECKS GOOD. INSPECTED RT ENGINE INTAKE. NOTICED OIL JUST AFT ON C1 BLADES AT 6 0CLOCK POS. REMOVE ENGINE P/N RB211-535E S/N 30942 AS PER WORK CARD 71T0002-RR. INSTALLED NEW ENGINE P/N RB211-535E4, S/N 30891. COMPLETED WORK 24T1302 NR 2 ENGINE IDG DISCONNECT, OPS CHECK. ENGINE MOUNT FITTINGS-INSP.

Part: GIRT BAR — MALFUNCTIONED (ESCAPE SLIDE) · airframe 49,908 hrs · 21,414 cycles

R-1 DOOR WAS OPENED WITH SLIDE ARMED. DOOR ASSIST BOTTLE DISCHARGED BUT SLIDE COVER CAUGHT ON DOOR FRAME AND SLIDE DID NOT DEPLOY. RELEASED FOR SERVICE IAW MEL: 52-11-01-B CATEGORY: B EXPIRATION: "MEL 52-11-01-B: R-1__ (IDENTIFY L1 AND/OR R1) DOOR SLIDES - INOP, NO JUMP SEATERS/ACM S ARE TO OCCUPY COURIER AREA IN FLIGHT. " UNABLE TO MAKE SLIDE ARM/DISARM CONSISTANTLY. AFT GIRT BAR ATTACH POINT HANGS UP. NO TIME TO T/S FURTHER. REMOVED R-1 SLIDE AND STOWED IN GALLEY COMPARTMENT. R-1 DOOR OPERATION NORMAL. WILL ALSO NEED DOOR ASSIST BOTTLE RECHARGED OR REPLACED.

Part: DOOR FRAME — CORRODED (L1 DOOR) · airframe 48,896 hrs · 20,919 cycles

L-1 DOOR, AFT -SIDE, FRAME EXFOLIATED BELOW DOOR ASSIST HANDLE. REPAIRED DAMAGED FRAME, L-1 DOOR, AFT-SIDE, BELOW DOOR ASSIST HANDLE, IAW SRM 51- 70-11. ALL PARTS REMOVED FOR ACCESS WERE RE-INSTALLED IAW SRM 51-40-02. ALL REPAIR PARTS INSTALLED IAW SRM 51-70-11. THIS IS A CAT "A" MAJOR REPAIR, WITH NO FOLLOW UP TRACKING.

Part: SKIN — DAMAGED (ZONE 400) · airframe 48,896 hrs · 20,919 cycles

WHILE DRILLING THE NR 1 PYLON INBD FWD 311N5193-2 SKIN PANEL NUMEROUS FASTENER HOLES WERE OVERSIZED AND ELONGATED. THE NUMEROUS FASTENER HOLES THAT WERE OVERSIZED AND ELONGATED WERE REPAIRED AND A NEW 311N5193-2 SKIN PANEL INSTALLED PER MAE EA NR 757-5452-16-A1808 REV A. COMPLIED WITH FEDEX EA NR F-5450-124028 REV A ON NR 1 PYLON INBOARD SKIN.

Part: WEB — CORRODED (BS 1681) · airframe 48,896 hrs · 20,919 cycles

DECK PLATE WEB AT STA 1681, RBL 13 CORRODED. REPAIRED CORRODED DECK PLATE WEB AT STA 1681 RBL 13 IAW SRM 53-60-51 REPAIR NR 2 "A" MAJOR REPAIR NO FOLOW-UP INSP REQUIRED (TRANSFERED FROM N00582 ).

Part: STRINGER — GOUGED (BS 750-770 S5L) · airframe 48,896 hrs · 20,919 cycles

INTERNAL STRUCTURE , STR 5L HAVE SEVERAL SCRATCHES BS 750-BS770. REPAIRED IAW SRM 53-00-03, REPAIR NR 1, ENTIRE STR SECTION REPLACED BS 730-780 AT S-5L CAT "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 48,896 hrs · 20,919 cycles

FLOORBEAM CORRODED AT STA 1681 RBL 13. REPAIRED CORRODED FLOORBEAM AT STA 1681 RBL 13 IAW SRM 53-00-51. REPAIR NR 2, "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED .

Part: STRINGER — DAMAGED (BS 730-780 S5L) · airframe 48,896 hrs · 20,919 cycles

INTERNAL STRUCTURE, STRINGER 5L HAVE SEVERAL SCRATCHES BS 750-BS 770. REPAIRED IAW SRM 53-00-03, REPAIR NR 1, ENTIRE STRINGER SECTION REPLACED BS 730-780 AT S-5L CAT "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.

Part: STRINGER — GOUGED (BS 1000-1020) · airframe 48,896 hrs · 20,919 cycles

INTERNAL STRUCTURE S 8L BS 1000-1020 STR HAVE SEVERAL NICKS. REPAIRED STR 8 L BS-1000-1020 IAW SRM 53-00-03 REPAIR NR 1 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: WEB — CORRODED (BS 1681) · airframe 48,896 hrs · 20,919 cycles

DECK PLATE WEB AT STA 1681 RBL 13 CORRODED. REPAIRED CORRODED DECK PLATE WEB AT STA 1681 RBL 13 IAW SRM 53-60-51 REPAIR NR 2 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED (TRANSFERED FROM N00582 ).

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 48,896 hrs · 20,919 cycles

FLOORBEAM CORRODED AT STA 1681 RBL 13. REPAIRED CORRODED FLOORBEAM AT STA 1681, RBL 13 IAW SRM 53-00-51 REPAIR NR 2 , "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED ( TRANSFERRED FRON N00582 )

Part: STRINGER — DAMAGED (BS 1000-1020) · airframe 48,896 hrs · 20,919 cycles

INTERNAL STRUCTURE S 8L BS 1000-1020 STRINGER HAS SEVERAL NICKS. REPAIRED STRINGER 8 L BS-1000-1020 IAW SRM 53-00-03 REPAIR NR 1 "A" MAJOR REPAIR, NO FOLLOW-UP INSP REQUIRED.

Part: FRAME — GOUGED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN AT STA 1620 STR 5L HAS TOOLMARK. REPAIRED FRAME BS 1620 S5L IAW SRM 53-00-07 REPAIR NR 1. REMOVED AND REINSTALLED SHEAR TIES FOR ACCESS. CATEGORY A REPAIR, NO FOLLOW-UP REQUIRED.

Part: FRAME — GOUGED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN AT STA. 1600 BETWEEN STR2-5L HAS TOOLMARKS. REPAIRED FRAME BS 1600 S2-5L IAW SRM 53-00-07 REPAIR NR 1.THIS IS CATEGORY A REPAIR WITH NO FOLLOW-UP.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FLOOR STA 640 RBL 45 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR NR 1. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FLOOR BS 640 RBL 45 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR NR 1. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN STA 345 LBL14 FLOOR SUPPORT HAS AREA OF CORROSION AROUND FASTENER HOLES. REMOVED THE DAMAGED AND FABRICATED PARTS ON MAE TRAVELERS NR T8/755777, T8/755776, T8/748077, T8/748078. INSTALLED REPAIR PARTS AND UPPER T-CHORD ON STA 345 LBL 52 TO RBL18 IAW SRM 53-00-51 FIGURE 20 REPAIR 3. THIS IS CATEGORY A REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. FOUND SKIN ASSY CORRODED OUT OF LIMITS IAW SRM 54-50-01 (L= 1.5 INCH, W= 2.0 INCH, D= .028 INCH). ROUTED SKIN PANEL ASSY FOR REPAIR ON AMII WORK ORDER NR 7434, DATED 07/14/08 AGAINST W/C T F-5450-122806 AND EA F-5450-122806, REV "A", DATED 07/17/08. INSTALLED NR1 PYLON INBD REPAIRED SKIN PANEL ASSY IAW DRAWING 311N5002. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — GOUGED (BS 1280) · airframe 48,896 hrs · 20,919 cycles

FLOORBEAM BS 1280 UPPER SURFACE LBL 60 TO RBL 60 HAS GOUGES. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED DAMAGED AREA OF FLOORBEAM UPPER CHORD, FABRICATED NEW CHORD, LOCATED AND DRILLED ANGLES AND STRAPS IAW SRM 53-00-51, FIG 201. TREATED AND PRIMED NEW CHORD AND INSTALLED CHORD, ANGLES AND STRAPS IAW SRM 51-20-01. THIS IS A CATREGORY "A" REPAIR "MAJOR REPAIR".

Part: FLOORBEAM — GOUGED (BS 1280) · airframe 48,896 hrs · 20,919 cycles

FLOORBEAM STA 1280 UPPER SURFACE LBL 60 TO RBL 60 HAS GOUGES. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. REMOVED DAMAGED AREA OF FLOORBEAM UPPER CHORD, FABRICATED NEW CHORD, LOCATED AND DRILLED ANGLES AND STRAPS IAW SRM 53-00-51, FIG 201. TREATED AND PRIMED NEW CHORD AND INSTALLED CHORD, ANGLES AND STRAPS IAW SRM 51-20-01. THIS IS A CATEGORY "A" REPAIR "MAJOR REPAIR"

Part: SKIN PANEL — CORRODED (NR 1 NACELLE) · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON LT SKIN, INNERWALL IS CORRODED JUST FWD OF PRE-COOLER. REMOVED AND REPLACED LT SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002 AND EA F-5450-121408. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIRED.

Part: SKIN PANEL — CORRODED (NR 2 NACELLE) · airframe 48,896 hrs · 20,919 cycles

NR 2 PYLON I/B FWD SKIN PANEL ASSY, HAS CORROSION ON INNER AND OUTER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B FWD SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

NR 2 PYLON O/B FWD. 311N5193-3 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED HINGE TO GAIN ACCESS TO REMOVED SKIN PER SRM 51-40-02, INSTALLED AFT T/R HINGE PER SRM 51-401-02. REMOVED FWD SKIN P/N 311N5193-2 PER SRM 51-40-02, REMOVED CORROSION PER SRM 54-50-01. OUT OF LIMITS IAW SRM 54-50-0. FWD LOWER DOOR CORNER CUTOUT BS 106- 110 ORIG. MAT. .205 REMAINING MAT .0031. RECEIVED NEW SKIN P/N 311N5193-2. LOCATED AND DRILLED NEW SKIN PER SRM 81-40-05 AND INSTALLED NEW SKIN P/N 311N5193-2 PER DRAWING 311N5002 AND SRM 51-40-02. THIS IS A CATEGORY " A" REPAIR MAJOR REPAIR.

Part: SKIN PANEL — CORRODED (NR 2 NACELLE) · airframe 48,896 hrs · 20,919 cycles

NR 2 PYLON I/B AFT SKIN PANEL, 311N5046-33, HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B AFT SKIN PANEL IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIRED.

Part: BULKHEAD — DAMAGED (NR 1 PYLON) · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON MID BULKHEAD LT SIDE HAS 1 NUT PLATE WITH DOUBLE DRILLED FASTENER HOLES. REPAIR COMPLIED WITH EA F 5452- 110907 AND MAE EA 757- 54521-16-A1802, REV, MAJOR REPAIR.

Part: BULKHEAD — DAMAGED (NR 1 NACELLE) · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON MID BULKHEAD LT SIDE HAS 1EA NUT PLATE WITH DOUBLE DRILLED FASTENER HOLES. REPAIR COMPLIED WITH EA F 5452-110907 AND MAE EA 757- 54521-16-A1802, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 48,896 hrs · 20,919 cycles

EXISTING RT FUSELAGE SKIN EXTERNAL DOUBLER REPAIR AT BS 670, S-20R-S-21R, COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. DURING EVALUATION OF ABOVE NOTED REPAIR PER ATTACHMENT "B" OF EO F-5100-7-5001, PART 1, IT WAS DISCOVERED THAT PREVIOUS REPAIR WAS NOT PER ANY APPROVED DATA. REMOVED EXISTING REPAIR AND INSTALLED A NEW DOUBLER REPAIR PER SRM 53-00-01, FIGURE 201, REPAIR NR 16. NEWLY INSTALLED DOUBLER REPAIR AT BS 670, S-20R - S-21R, EXTERNAL, IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING REPETITIVE INSPECTION: INSPECTION THRESHOLD; 25,000 FC; REPEAT INTERVALS OF 3,000 FC (LFEC).

Part: CREASE BEAM — CORRODED (BS 1360-1340) · airframe 48,896 hrs · 20,919 cycles

AFT PIT, CREASE BEAM WEB, LOWER SURFACE BS 1360 BS 1340 RBL 67 INCH HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. FABRICATED NEW WEB ON TRAVELER T8/753327. INSTALLED NEW WEB IAW SRM 51-40-02 AND REINSTALLED CREASE BEAM IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: CREASE BEAM — CORRODED (BS 1360) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

AFT PIT, CREASE BEAM WEB, LWR SURFACE BS 1360 BS 1340 RBL 67 INCHES HAS CORROSION REMOVED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FABED NEW WEB ON TRAVELER T8/753327, INSTALLED NEW WEB IAW SRM 51-40-02 AND REINSTALLED CREASE BEAM IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON OTBD FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PAANEL IAW SRM 51-40-02, AND DWG 311N5002, 311N5108. (CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED)

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

NR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON OTBD SKIN PANEL PN 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .

Part: SKIN PANEL — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

NR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON O/B SKIN PANEL P/N 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .

Part: SKIN PANEL — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

NR 1 PYLON O/B FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40-02,AND DWG. 311N5002, 311N5108, CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

SEAT TRACK LBL 45.50 HAS CORROSION ON AFT SIDE OF BS 1120 FLOORBEAM. REMOVED CORROSION FROM SEAT TRACK IAW SRM 53-00-52. ORIGINAL MATERIAL THICKNESS WAS .084 INCH, AFTER REWORK .044 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REMOVED SEAT TRACK, FABRICATED REPLACEMENT SEAT TRACK PER MAE TRAVELER NRT8/748466 AND SRM 51-40-02. INSTALLED REPLACEMENT SEAT TRACK PER SRM 53-00-52 AND 51-40-02. THIS IS CLASSIFIED AS A MAJOR REPAIR, CATEGORY A REPAIR. NO FOLLOW UP TRACKING IS REQUIRED.

Part: SKIN — CORRODED (ZONE 500) · airframe 48,896 hrs · 20,919 cycles

LT WING REAR SPAR UPPER FITTING, UPPER SKIN LOWER SURFACE, ALONG THE AFT EDGE WHERE SKIN OVERLAPS THE REAR SPAR'S UPPER CAP, IS CORRODED JUST ABOVE LT DEFUEL VALVE. REPAIRED WING PANEL IAW FEDEX EA F-5730-110881, REV -, DATED 06/19/2008 AND SB 757-57- 0036, REV 1, DATED 06/04/92.

Part: CREASE BEAM — CORRODED (BS 395-418) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCHES, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DRILLED HOLES IAW SRM 51-40-05 TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7, INSTALLED CREASE BEAM IAW SRM 51-40-02, STA 324-395. (CREASE BEAM FROM BS 395-418 DELETED BY P TO F MOD, MAJOR REPAIR.

Part: WEB — CORRODED (BS 1681-1720) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG FIG. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED REPAIR DOUBLERS IAW SRM 53-60-51 REPAIR 2 ALT 1, MAJOR REPAIR.

Part: CREASE BEAM — CORRODED · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DRILLED HOLES IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7. INSTALLED CREASE BEAM IAW SRM 51-40-02, STA 324-395, CREASE BEAM FROM BS 395-418. DELETED BY P TO F MOD, MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 324-395) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREASE BEAM IAW SRM 51-40- 02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DRILLED HOLES IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7. INSTALLED CREASE BEAM IAW SRM 51-40-02, STA 324-395, (CREASE BEAM FROM BS 395-418 DELETED BY P TO F MOD, MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51 FRON 2024-T3 .063 BATCH NR 0001466849. INSTALLED REPAIR DOUBLERS IAW SRM 53-60-51 REPAIR 2 ALT 1 , MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 324-395) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCH, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DRILLED HOLES IAW SRM 51-40-05 TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7, INSTALLED CREASE BEAM IAW SRM 51-40-02, STA 324-395. (CREASE BEAM FROM BS 395-418. DELETED BY P TO F MOD, MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 680-740) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN CREASE BEAM CHORD BS 680 -740, RBL 66 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CREASE BEAM, RECEIVED NEW PART NR 143N8328U54 IAW SRM 53-30-13. INSTALLED NEW CREASE BEAM PART IAW SRM 51-40-02, AND 51-10-02, FS 680-740, RBL 66.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

STA 1046, LBL 47, LUG SCALLOP IS MISSING ON SEAT TRACK. REMOVED SEAT TRACK SECTION IAW SRM 53-00-52. FABRICATED NEW ON MAE TRAV NR T8/750424. INSTALLED NEW SEAT TRACK REPAIR PARTS IAW SRM 51-40-02, AND 53-00-52.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FLOOR STA 365 RBL 58 FLOORBEAM CORROSION. REMOVED DAMAGE, FABRICATED ANGLES MAE TRAV T8/748437. FABRICATED T-CHORDS MAE TRAV T8/748430, IAW SRM 53-00-51. INSTALLED REPAIR PARTS STA 365 RBL 34-70 IAW SRM 53-00-51 FIG 201. REPAIR 3. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN BS 418, BL0 TO LBL 15, FLOORBEAM HAS AREAS OF CORROSION AROUND FASTENER HOLES. CLEANED AREA AND CHECKED LIMITS IAW SRM 51-10-3 AND 53-00-51, DETAIL 3. FLOORBEAM OUT OF LIMITS PER SRM 53-00-51, DETAIL 3; ORIGINAL MATERIAL THICKNESS .125 INCH, AFTER REWORK .094 INCH. CUT OUT DAMAGED AREA PER SRM 53-00-51, FIG 201, REPAIR NR 5. FABRICATED REPAIR PARTS, ON TRAVELER NR T8/745527, AND INSTALLED PER SRM 53-00-51, REPAIR NR 5. THIS REPAIR IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

STA 377.7, BL0 TO LBL 45 HAS CORROSION AROUND NUT PLATE HOLES. REMOVED DAMAGED AREA, LBL 13 TO LBL 70, BS 377.7 IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRICATED T-CHORD AND SHIM IAW SRM 53-00-51, REPAIR NR 3. FABRICATED STRAP NR 4 AND NR 5 ON TRAVELER NR T8/744935. FABRICATED ANGLE NR 2 AND NR 3 ON TRAVELER NR T8/744935. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51, FIG 201, REPAIR NR 3. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,896 hrs · 20,919 cycles

MAIN CABIN FLOORBEAM STA 1640 RBL 47-51 HAS CORROSION BLENDED AREA IAW SRM 51-10-02, ORIG MAT. .125 AFTER 0.90 FOUND OUT LIMITS, IAW SRM 53-00-51 PAGE 103, CUT OUT DAMAGED AREA STA 1640 BET RBL36.5 TO RBL 68.5, IAW SRM 53-00-51 PAGE 201. RECEIVED REPAIR PARTS NR 1 TEE CHORD, NR 2 ANGLE FAB`D. ON TRAV NR T8/746064 PART NR 3 REPAIR ANGLE FAB`D. ON TRAV NR T8/746065, AND STRAP NR 4 AND 5 FAB`D IAW SRM 53-00-51 PAGE 203 FIG 201. LOCATED AND DRILLED FASTENERS HOLES REPAIR PARTS DEBURRED, TRIMED AND TREATED AND PRIMED IAW SRM 51-20-01 AND SRM 51-40-05. INSTALLED REPAIR PARTS IAW SRM 53-00-51 IAW SRM 51-40-02. CATEGORY A REPAIR NO FOLLOW UP TRACKING REQUIRED.

Part: SKIN — DENTED (ZONE 800) · airframe 48,896 hrs · 20,919 cycles

R1 DOOR SKIN DENTED. REMOVED DAMAGE AND INSTALLED A DOUBLER REPAIR ON R1 DOOR SKIN IAW SRM 52-10-01 REPAIR NR 2, FIGURE 202. THIS REPAIR IS CLASSIFIED AS A "MAJOR" REPAIR, CATEGORY A, WITH NO FOLLOW UP TRACKING REQUIRED.