N993FD

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 64,111 hrs · 25,000 cycles

ZONE 220 FLOORBOARD 221MBF IS DAMAGED. FABRICATED NEW BOARD 11861182-16, 221MBF FROM TRAVELER T22/1651611 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIR

Part: GIRT BAR — OBSTRUCTED (L1 DOOR SLIDE) · airframe 62,867 hrs · 24,088 cycles

L1 DOOR GIRT BAR ENGAGEMENT "SLIDE" LIGHT INOP. GIRT BAR OPERATION NORMAL. REMOVED DEBRIS FROM L1 GRIT BAR AREA AND TESTED THE ARM AND DISARM SLIDE LIGHT INDICATIONS I/A/W AMM 25-66-11-2 PAR. 5, SUB PAR. 11. GND TESTED MULTIPLE TIMES. NO DISCREPANCIES NOTED. OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOBRAKE SYS) · airframe 62,760 hrs · 24,018 cycles

BRAKE SOURCE LIGHT ILLUMINATED WHILE ARRIVING IN MEMPHIS ... PASSING 10,000 FT. RAN QRH , DECLARED EMERGENCY , LANDED ... DID NOT TAXI . THE BRAKE SOURCE LIGHT REMAINED ON AFTER SELECTING RESERVE BRAKES. NOTE: PILOT DEBRIEF - ALL HYD. PRESSURES WERE NORMAL, ALSO GOT A ANTI-SKID ECIAS MESSAGE. VERIFIED BRAKE ACCUMULATOR PRESSURES WERE WITHIN LIMITS REF 757 AMM 12-15-04-3. VERIFIED INTEGRITY S415 ALTN VALVE SELECT PRESSURE SWITCH REF 757 SSM 32-41-01. REMOVED REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT IAW 757MM 32-42-04-1. ALL OPS CHECKS ARE GOOD.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 62,698 hrs · 23,976 cycles

WHEN EXTENDING FLAPS TO 1 LEADING EDGE SLAT DISAGREE DISPLAYED ON THE EICAS AND FLAP POSITION WAS STUCK BETWEEN UP AND 1. FOLLOWED QRH PROCEDURE AND USED ALTERNATE FLAP EXTENSION TO EXTEND FLAPS TO 20 FOR LANDING. FOUND HYDRAULIC LINE P/N 271N6445-1255 IN LH WHEEL WELL FOR THE HMG SYSTEM BROKEN. REMOVED AND REPLACED LINE ON WRI 29-02-8281. PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IAW AMM 27-51-00-5.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 62,698 hrs · 23,976 cycles

DEPARTING FROM BFM LANDING GEAR DISAGREE AND GEAR DOOR ON EICAS. ALSO DOORS LIGHT AND NOSE GEAR LIGHT STAYED ON WITH MAIN LEFT AND RIGH GEAR LIGHTS OUT. AFTER ABOUT TWO MINUTES NOSE GEAR LIGHT AND DOORS LIGHT WENT OUT AND LANDING GEAR DISAGREE MESSAGE WENT OUT ON EICAS. NORMAL GEAR EXTENSION. FOUND HYDRAULIC LINE P/N 271N6445-1255 IN LH WHEEL WELL FOR THE HMG SYSTEM BROKEN. REMOVED AND REPLACED LINE ON WRI 29-02-8281. PERFORMED OPERATIONAL TEST OF LANDING GEAR SYSYTEM IAW AMM 32-32-00-5 FOUND TO BE WITHIN LIMITS. GEAR EXTEND 18 SEC'S AND RETRACTED IN 25 SEC'S PSEU REMOVED AND REPLACED IAW AMM 32-09-04-4 TEST GOOD IAW AMM 32-09-04-4 STEP 3(E)

Part: FRAME — CRACKED (ZONE 200) · airframe 62,698 hrs · 23,975 cycles

BODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14 AT LH. CRACK INDICATION NOTED FOR BOTTOM INBOARD HOLE COMPLIED WITH EA# F-5310-T0359452 P1. FUSELAGE-MAINFRAME-CRACK INDICATION AT STA 1640 FUSELAGE FRAME WEB, S-14L AT LOWER INBOARD HOLE LOCTION- TEMPORARY FREEZE PLUG REPAIR. CAT "C" MAJOR REPAIR

Part: SWITCH — DAMAGED (SLAT SYSTEM) · airframe 62,657 hrs · 23,951 cycles

AT CRUISE WE RECEIVED AN EICAS MESSAGE LEADING EDGE SLAT ASYM EMERGENCY DECLARED. PER FIM/27-81 F/T 804 FOUND AND WDM 27-81-31. RANG OUT SLAT LOSS SENSING SWITCHES FROM FSEU TEST RECEPTICLE D1251 AND FOUND ALL SWITCHES READING OPEN. FSEU 1 FAULTED SLAT LOSS 317 R & R FSEU NR 1, REF/AMM 27-51-01-2. FAULTS CLEARED AND FLAPS/SLATS OPERATE FLAPS/SLATS OPERATE NORMAL AT THIS TIME. OPERATIONAL TEST ON FSEU NOT COMPLETE. MOCC REQUEST INSPECTION OF SLAT LOSS SWITCHES AND WIRING. REMOVED FSEU 1 & 2, FOUND HI RESISTANCE SHORT TO GROUND AT PIN G9 IN THE D3258A CONNECTOR WITH MEGGER AT FSEU 2. REMOVED CONNECTOR D41381 AND MEGGED PIN G9 IN D3312A CONNECTOR, NO FAULTS NOTED. ISOLATED PROBLEM TOI RIGHT WING SWITCHES. DISCONNECTED CONNECTOR D41396P AND MEGGED PIN 11 IN THE J SIDE OF THE CONNECTOR, NO DEFECTS NOTED. RECONNECTED CONNECTOR D41396P. VERIFIED FAULT BETWEEN FSEU 2 AND CONNECT D41396. SUSPECT RT INBOARD SWITCH S10588. REMOVED AND REPLACED RT INBOARD SLAT LOSS SENSING SWITCH (S10588) AND LEVER ARM, IAW AMM 27-81-41-4. OPERATIONS CHECK NORMAL, PER AMM 27-81-41-4. A/C OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,591 hrs · 23,247 cycles

ON PREFLIGHT FOUND LT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LT BATTERY PACK PER AMM 33-51-07-2. OP'S CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 61,281 hrs · 23,029 cycles

ON FINAL GOT A SLAT DISAGREE LIGHT. RAN QRH, LANDED UNEVENTFULLY USING ALTERNATE FLAP SYSTEM. SLAT DISAGREE LIGHT EXTINGUISHED DURING QRH PROCEDURES. INSPECTED FLAPS AND SLAT AREAS, NO IMMEDIATE DEFECTS NOTICED AT THIS TIME. RESET ALTERNATE FLAP SWITCHES TO NORMAL. OPERATED FLAP/SLAT SYSTEMS REF MM 27-80-00-2. ALL INDICATIONS CK NORMAL AT THIS TIME WITH NO FAULTS PRESENT. A/C OK FOR SERVICE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

CORROSION FOUND @ AFT CARGO COMPT INTERCOSTAL STA 1400-1420 STR 29R-30 FOUND CORR ON INTERCOSTAL IN AFT CARGO STA 1400-1420 STR 29R-30 TO BE OUT OF LIMITS IAW SRM 53-00-04-1A. REMOVED INTERCOSTAL IAW SRM 51-40-02. FABRICATED AND INTALLED NEW INTERCOSTAL IAW DWG 146N5425 REV F AND 146N5399 REV B.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT. CARGO COMPT. UPON REMOVAL OF TRANSITION PANEL SECTION FOR REPAIR. FOUND AT BS. 1440, AND STR.27R. CARGO TIEDOWN, MOUNT STRUCTURE FOR TIEDOWN WITH EXFOLIATED CORROSION. FOUND AFT CARGO TIEDOWN MOUNT STRUCTURE CORR. TO BE 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-53-1A FIG 101 DET I. REMOVED TIEDOWN MOUNT STRUCTURE IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW TIEDOWN MOUNT STRUCTURE IAW DWG 146N5420 REV B.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

UPON REMOVAL OF AFT CARGO COMPT CLIP P/N 146N5422-4 STA 1440 STR 27R FOUND OUT OF LIMITS. FABRICATED LOCATED, DRILLED AND TRIMMED TO FINAL SIZE AFT CARGO COMPT. CLIP STA 1440 STR 27R AS PER DWG 146N5422 REV B & D AND SRM 51-40-05-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT CARGO COMPT. BETWEEN BS.1320 AND BS.1340,AND STR 28L.INTERCOSTAL WEB HAS CORROSION. EVALUATED CORROSION AT AFT CARGO COMPT. BETWEEN BS 1320-1340 AND STR 28L INTERCOSTAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A FIG 101 REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G, DWG 146N5398 REV. A AND 146N5425 REV F.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT CARGO COMPARTMENT WEB LOCATED BETWEEN BS 1360 AND 1380 STRINGER 27R HAS CORROSION. AFT CARGO COMPARTMENT WEB STA 1360-1380 - STR 27R HAS COROSION. FOUND CORROSION 100% OUT OF LIMITS IAW SRM 53-60-04-1A AND 53-00-04-1A FIG 1 DETAIL II, FABRICATED, LOCATED AND DRILLED NEW INTERCOSTAL WEB DIM 191\4" X 41\2 IAW DRWG # 146N8522 REV E TREATED AND PRIMED, TOP COATED SRM 51-20-01-0G AND MM 51-21-00-07 PART MARKED WEB P\N FX 146N8522-14 PER GMM 07-0-1001.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE AT STA 1380 STR 27R ELONGATED HOLES. FORMED NEW SUPPORT ANGLE (CHANNEL), TRIMMED, LOCATED AND DRILLED IAW DRWG 146N8522 REV E, TREATED AND PRIMED, TOP COAT IAW SRM 51-20-01-0G AND AMM 51-21-10-07.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT CARGO COMPT. INTERCOSTAL HAS CORROSION, BETWEEN BS. 1440 AND BS. 1460 AND BETWEEN STR 27R AND STR 26R. REMOVED CORR ON INTERCOSTAL & ANGLE STA 1440 & 1460 STR 26R - 27R IAW SRM 51-10-02. FOUND 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-04-1A. REMOVED INTERCOSTAL AND ANGLE IAW SRM 51-40-02 FABRICATED AND INSTALLED NEW INTERCOSTAL & ANGLE IAW SRM 51-40-02 AND DWG 146N5413 REV A AND 146N5215 REV -.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

AFT CARGO COMPT. AT BS.1380,AND STR .28R. SHEARTIE HAS EXFOLIATED CORROSION. DOT 24/042 ACCOMPLISHED WITH E.A F-5310-T0344528 P1 TITLE: FUSELAGE-MAINFRAME-STA 1380 FRAME OUTER CHORD PARTIAL REPLACEMENT AND SPLICE REPAIR BETWEEN S-26R AND S29R.

Part: SKIN — GOUGED (TE FLAP) · airframe 61,259 hrs · 23,010 cycles

LT. WING T/E AFT FLAP 36" FROM O/B END LOWER SURF. IS GOUGED REPAIRED LT. WING GOUGE AT T/E AFT FLAP 36" FROM O/B END LOWER SURFACE IAW SRM 51-70-04-0G (PARA 5.B) & 51-70-17-0G (PARA 3.G) AND EA T F-5750-T0344477 P1 WING- FLIGHT SURFACES- LT OUTBOARD AFT FLAP LOWER SURFACE REPAIR-RSC TRACKING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

SUPERNUMERARY SEAT TRACK SHOWS EVIDENCE OF CORROSION FWD OF THE 9G BULKHEAD IN THE VESTUBLUE RBL 12 REMOVED CORROSION ON SEAT TRACK AT STA 345 TO 377, RBL 12 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA,ORIG. MAT=.070",REM MAT=.055",MAT LOSS=.015" FOUND TO BE OUT LIMITS IAW SRM 53-00-52-1A, FIG 101, DETAIL VII. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G AND V.A DWG 3470 REV:G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,259 hrs · 23,010 cycles

SUPERNUMERARY SEAT TRACK SHOWS EVIDENCE OF CORROSION FWD OF THE 9G BULKHEAD IN THE VESTUBULE LBL 05. REMOVED CORROSION ON SEAT TRACK AT STA 345 TO 377, LBL 5 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA, ORIG. MAT=.070", REM MAT=.046", MAT LOSS=.024" FOUND TO BE OUT LIMITS IAW SRM 53-00-52-1A, FIG 101, DETAIL VII. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02-0G AND V.A DWG 3470 REV : G.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,259 hrs · 23,010 cycles

CABIN BS 1620 LBL 55 SIDE ANGLE HAS A LARGE SPOT OF CORROSION. REMOVED CORROSION ON MAIN CABIN, ANGLE (CREASE BEAM) BS 1620 LBL 65 IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-13-1A FIG 101 DETAL VIII. REMOVED DAMAGED CREASE BEAM, FABRICATED AND INSTALLED REPAIR AT CREASE BEAM, IAW SRM 53-00-13-2R FIG 201 REP 1.

Part: FSEU — MALFUNCTIONED (NR 2) · airframe 60,205 hrs · 22,298 cycles

25 MINUTES AFTER TAKE OFF AT FL 370, CAUTION EICAS FOR LE SLAT ASYM, NO VIBRATION, NO CHANGE ON FLAP GAUGE, FOLLOWED QRH . NO ROLL OR VIBRATION DURING CONFIGURATION. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE NR 2 FSEU IAW AMM 27-51-01-2, OK FOR SERVICE.

Part: STRUT — DAMAGED (LT NACELLE) · airframe 59,540 hrs · 21,859 cycles

LEFT PYLON ABOVE FWD ENGINE MOUNT INSIDE FWD ACCESS PANEL HAS SEVERAL OPEN HOLES ON BOTH SIDES. COMPLIED WITH EA # F-5430-TO330415 P1, DRILLED & INSTALLED FASTENERS. MAJOR REPAIR.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 59,540 hrs · 21,859 cycles

R-2 DOOR UPPER HINGE CUTOUT INNER CHORD OF THE DOOR FRAME CRACKED. REPAIRED IAW SRM 52-10-02-2R DETAIL III FIG.201.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 58,939 hrs · 21,447 cycles

RIGHT CREW DOOR SLIDE WILL NOT ARM. RE-STOWED R1 DOOR SLIDE CORDS IAW AMM 52-11-00-5-0. SYS OPERATIONS CHECKED GOOD.

Part: OXYGEN BOX — LEAKING (CAPTAIN'S) · airframe 583 hrs · 21,016 cycles

CAPTAIN`S OXYGEN PRESS TO TEST DOOR BROKEN. COURIER OXYGEN MASK INOPERATIVE. SWAPPED NR 3 COURIER POSITION OXYGEN STOWAGE BOX TO CAPTAIN`S POSITION TO MAKE CAPTAINS POSITION SERVICEABLE IAW AMM 35-11-51-4-99. REMOVED AND REPLACED THE COURIER NR 3 OXYGEN MASK STOWAGE BOX IAW AMM 35-11-51-4-99. LEAK AND OPS CHECKED OK.

Part: LATCH — DAMAGED (ESCAPE ROPE) · airframe 580 hrs · 20,837 cycles

CAPTAIN ESCAPE ROPE DOOR WILL NOT STAY SHUT. LATCH APPEARS TO BE BROKEN. LATCH BASE IS BROKEN ON INSIDE OF SIDEWALL PANEL. THE UPPER EAR FOR THE MOUNTING OF THE BUTTON LATCH IS MISSING & BROKEN OFF. REMOVED TWO RIVETS AND OLD LATCH "STRIKER" BASE. INSTALLED TWO BACR15BA4A RIVETS WITH NEW LATCH ASSY. REF. IPC 25-61-52-02 AND B757 AMM 25-61-00-4. DOOR OPS NORMAL.

Part: CLOSEOUT PANEL — DENTED (CARGO DOOR) · airframe 57,963 hrs · 20,736 cycles

MAIN CARGO DOOR, FWD PRESSURE RELIEF DOOR CLOSEOUT PANEL IS GOUGED. REMOVED DAMAGED CLOSEOUT PANEL, FABRICATED NEW CLOSEOUT PANEL, AND INSTALLED IAW SRM 51-40-02, SRM 52-30-02 FIG 101, DRAWING 65-49309 REV A, SRM 51-40-05, SRM 51-20-01, AND SRM 51-40-02 .

Part: SKIN — DENTED (BS 761) · airframe 57,963 hrs · 20,736 cycles

FUSELAGE DENTED AT BS 761 JUST BELOW STRINGER 17L. REPAIRED IAW SRM 53-00-01 REPAIR 16. MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 10 SLAT TE WEDGE UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 10 SLAT ASSEMBLY IAW AMM 27-81-02. ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.

Part: SKIN — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT WING INBD FLAP UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R RT INBD MAIN FLAP IAW AMM 27-51-02 401. ADJUSTED RT INBD TE FLAP IAW AMM 27-51-12-5. PERFORMED POST INSTALLATION TEST IAW AMM 27-51-02-5, CHECKED GOOD.

Part: SKIN — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

LEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R LT INBD MAIN FLAP IAW AMM 27-51-02 401. ADJUSTED LT INBD TE FLAP IAW AMM 27-51-02-5. PERFORMED POST INSTALLATION TEST IAW AMM 27-51-020-5 CHECKED GOOD.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 36 INCHES FROM INBD END, 7 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 77 INCHES FROM OTBD END, 2 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-01 & SRM 51-70-04.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 53 INCHES FROM INBD END, 91/2 INCHES FROM AFT EDGE. BONDED & REPAIRED, RT OTBD AFT FLAP IAW SRM-57-53-01 & 51-70-04, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 6 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 6 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD, IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 2 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 2 SLAT ASSEMBLY IAW-AMM-27-81-02 ADJUSTMENT TEST GOOD IAW AMM- 27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 1 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 1 SLAT ASSEMBLY IAW-AMM-27-81-02, ADJUSTMENT TEST GOOD IAW-AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 5 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 5 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT & TEST GOOD, IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 7 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 7 SLAT IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 57,562 hrs · 20,456 cycles

RIGHT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 342BR, 342CR & 342DR. SANDED, CLEANED & APPLIED CONVERSION COATING IAW EA F5510-T0308665 & SRM 51-70-01.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 22 INCHES FROM INBD END, 111/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 113 INCHES FROM OTBD END 2 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW-SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 18 INCHES FROM INBD END, 8 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 59 INCHES FROM OTBD END, 71/2 FROM AFT EDGE. REPAIRED RT AFT FLAP WEDGE UPPER SURFACE IAW SRM 757 51-70-04.

Part: SKIN — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

LEFT WING OTBD FLAP AFT FLAP UPPER SURFACES HAS SEVERAL AREAS WITH HAIL STRIKES. BONDED & REPAIRED LT WING OTBD FLAP, AFT FLAP, IAW SRM-57-53-01 & SRM-51-70- 04, APPROX .5 INCHES IN DIAMETER. REMOVED 4 INCHES. REPAIRED THREE AREAS, 1ST LOCATED AT 13.5 INCHES FROM INBD END & 6.5 INCHES FROM TE, 2ND LOCATED AT 18 INCHES FROM INBD END & 3 INCHES FROM TE. 3RD LOCATED AT 19 INCHES FROM INBD END & 12.7 INCHES FROM TE. CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 9 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 9 SLAT IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 66 INCHES FROM INBD END 10 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM- 51-70-04, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 6 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 6 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 4 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 4 SLAT ASSEMBLY IAW-AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE PUNCTURED 67 INCHES FROM INBD END 4 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04 CAT A MAJOR REPAIR.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATED DENT 57 INCHES FROM INBD END, 5 1/2 INCHES FROM AFT EDGE. BONDED & REPAIRED RT OTBD AFT FLAP IAW SRM-57-53-01 & SRM-51-70-04, CAT A MAJOR REPAIR.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 3 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 3 SLAT ASSEMBLY IAW AMM-27-81-02, ADJUSTMENT TEST GOOD IAW AMM-27-81-02-4, CAT A MAJOR REPAIR.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 57,562 hrs · 20,456 cycles

LEFT HORIZONTAL STAB FWD UPPER SKIN HAS NUMEROUS HAIL DAMAGE ADJACENT TO PNLS 332BL, 332CL & 332DL. REPAIRED DENTS BY FILLING & FAIRING IAW EA F5510-T0308665.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 57,562 hrs · 20,456 cycles

RIGHT OTBD AFT FLAP WEDGE UPPER SURFACE HAS DELAMINATION DENT 32 INCHES FROM OTBD END, 5 INCHES FROM AFT EDGE. REPAIRED RT OTBD AFT FLAP WEDGE UPPER SURFACE IAW SRM 57-53-91 & SRM 51-70-04.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 57,562 hrs · 20,456 cycles

NUMBER 8 SLAT TE WEDGE UPPER SURFACES HAS SEVERAL AREAS WITH MULTIPLE HAIL STRIKES. R & R NR 8 SLAT ASSEMBLY IAW AMM 27-81-02 ADJUSTMENT TEST GOOD IAW AMM 27-81-02-4.

Part: LIGHT — CORRODED (CABIN) · airframe 56,635 hrs · 19,839 cycles

THE L1 ENTRY DOOR ESCAPE SLIDE LIGHT INOP. T/S ESCAPE SLIDE LITE,TESTED BATTERY PACK IAW MM 33-51-07-2-2, BATTERY PACK OP'S NORMAL, REMOVED LAMP AND REMOVED CORROSION FROM RECEPTICLE, RE INSTALLED LAMP, TESTED EMERGENCY LIGHTS IAW MM 33-51-06-2-1. ESCAPE LIGHT OP'S NORMAL, ACFT OK FOR SERVICE.

Part: WIRE — UNKNOWN (EMERGENCY LIGHT) · airframe 56,611 hrs · 19,821 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. FOUND NO WIRE IN PIN 12 OF D68 ON M731, WIRE W3532-0160-22 IS CAPPED AND STOWED AT D68 AND IS THE WIRE CALLED OUT IN WDM 33-51-12. WIRING LIST FOR D68 SHOWS WIRE 0502- 22 CONNECTED TO PIN 12 FOR THIS AIRCRAFT. APPEARS THAT WIRE W3532-0160-22 WAS SIMPLY DEPINNED FROM SOCKET 12 AND HEAT SHRINK APPLIED OVER THE PIN & WIRE TO PREVENT SHORT AND SECURED BACK ONTO BUNDLE. PERFORMED ERS 13-02538 IAW WDM 33-51-12. OPS CHECKED NORMAL OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED SYSTEM) · airframe 56,535 hrs · 19,768 cycles

DURING CRUISE FL400, LT ENGINE BEGAN TO SURGE WITH EPR, N1, EGT, N2, FOLLOWING. QRH PROCEDURES STARTED. TRIED TO RETURN THRUST LEVER TO NEAR NORMAL. SURGING BEGAN AGAIN. REDUCED THRUST TO IDLE. TURNED BLEED OFF. ENGINE RESPONDED. TURNED ENGINE BLEED ON AS LAST STEP. DIVERTED WITH LT THROTTLE NEAR IDLE. LT BLEED WAS 45 PSI, RT WAS 25 PSI. PERFORMED ENGINE RUN IAW JRH , CYCLED BLEED ON AND OFF AT 85 PERCENT N2 WITH NO ENGINE SURGES ON EITHER ENGINE, ALL PARAMETERS REMAINED STABLE N1, N2, EGT, FUEL FLOW. IAW FIM 36-10, CHECKED ALL SENSE LINES TO RFCC, HS PILOT AND VALVE, PRSOV PILOT AND VALVE AND TO 450 TEMP SENSOR ALL INTACT AND IN GOOD CONDITION. REPLACED HIGH STAGE PILOT IAW AMM 36-11-08-4. PERFORMED PNEUMATIC SYS TEST IAW AMM 36-11-00-5 AND PRSOV TEST IAW AMM 36-11-09-5. ALL RESULTS NORMAL. RAN ENG TO VARIOUS HIGH POWER SETTINGS IAW ALL INDICATIONS NORMAL, STABLE AND WITHIN LIMTS. ACFT OK FOR SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (FIRE DETECTION) · airframe 56,452 hrs · 19,714 cycles

ON ROLLOUT RECEIVED "MAIN CARGO FIRE" WARNING LASTED MAYBE 2-4 SEC, THEN WENT OUT. PASSENGER OXYGEN WENT ON. REPLACED MAIN DECK SMOKE CONROL PANEL IAW AMM P TO F26-16-30. MAIN DECK CARGO DETECTION. OPS CHECKS NORMAL IAW P TO F AMM 26-16-30, P 501. ACFT RELEASED FOR SERVICE.

Part: SHEAR TIE — CRACKED (BS 1300) · airframe 56,342 hrs · 19,634 cycles

AFT CARGO BS 1300 FRAME HAS CRACKED SHEAR TIE BETWEEN STR 20L AND STR 21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW AND INSTALLED IAW SRM 51-40-02, 51-40-05, 51-70-11 AND DWG 140N2002 REV EU.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 56,342 hrs · 19,634 cycles

NR 2 PYLON, STA 102.1 INBD SIDE ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-40-02 AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 311N3510 REV C.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LE SLATS) · airframe 56,003 hrs · 19,401 cycles

ON APPROACH, RECEIVED A L/E SLAT ASYM ALERT. ACFT DID NOT HAVE CONTROL PROBLEMS. UNABLE TO EXTEND FLAPS BEYOND 0 DEGREE AND 1 DEGREE, HYDRAULICALLY. USED ALTERNATE FLAPS FOR LANDING. R & R LOSS SENSING SWITCH FOR INBOARD LE SLATS IAW AMM 27-81-41-4, THRU STEP 4.C.(7).

Part: RING — DISLODGED (L1 DOOR SLIDE) · airframe 55,117 hrs · 18,824 cycles

L1 DOOR HAS STRAP AND D-RING HANGING DOWN OUT OF DOOR PACKAGE. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 29JUN11 "MEL 52-11-01-A: L1 DOOR SLIDE- INOP (IDENTIFY INOP OR MISSING)." FOUND D-RING TO INTERFEAR WITH ARMING GIRT BAR, REPOSTION D-RING. ACFT OK FOR SERVICE.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 55,044 hrs · 18,771 cycles

L1 CREW ENTRY DOOR SLIDE LIGHT WAS DIFFICULT TO ARM. OPS CHECKED L1 DOOR SLIDE ESCAPE SYSTEM REF MM 25-66-00-5-0. OPS CHECK GOOD, ACFT OK FOR SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

CORROSION ON S-26L BETWEEN STA 760-780 INSIDE FWD CARGO COMPARTMENT REQUIRES REWORK DUE TO INCORRECT SRM REF USED. REWORKED REPAIR SPICE AT STA 760-780 ON S-26L. RECEIVED NEW FILLER AND SPLICES ON T11/867864 AND T11/868216. INSTALLED NEW FILLER AND SPLICES IAW SRM 53-00-03, REPAIR 2 CAT "A" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 54,902 hrs · 18,656 cycles

PREVIOUS OPERATOR INSTALLED REPAIR EVALUATED IAW INCORRECT SRM REF. COMPLIED WITH EA F-5330-146251. FUSELAGE PLATES AND SKINS EO F-5100-7-5001 PART 1-EXISTING REPAIR TRACKING (DTA REQUIRED). MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 770 S27L) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

REWORK OF NR N00451: FWD CARGO PIT STA 770, S-27L, WL 138 CORRODED REQUIRES REWORK DUE TO INCORRECT SRM REF USED REWORKED REPAIR SPLICE AT STA 770 S-27L . INSTALLED SPLICES IAW SRM 53-00-03 REPAIR 3 CAT "A" MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 54,902 hrs · 18,656 cycles

DENT ON FUSELAGE SKIN STA 580-600 BETWEEN S-27L TO S-28L. DENT AT STA 580-600 BETWEEN S-27L TO S28L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, PG 201, FIG 201, REPAIR 16. CATEGORY "B" ZONE A REPAIR WITH SUPPLEMENTAL INSP AT 25,000 FC INITIAL AND EVERY 3,000 FC INTERVAL . LFEC METHOD IAW NDT 53-00-06 PT6. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

REWORK OF NR N00182: EXTERNAL FUSELAGE SKIN FOUND DENT AT STA 1120-1139, S-8R DENT AT STA 1120-1139, S-8R FOUND OUT OF LIMITS DUE TO PROXIMITY TO STRINGER IAW SRM 53-00-01, FIG 101 DETAIL II. REPAIRED AREA IAW SRM 53-00-01, FIG 201, PG 204, TABLE 1 REPAIR 15. CATEGORY "B" ZONE B REPAIR WITH SUPPLEMENTAL INSP INITAIL THRESHOLD OF 25,000 FC AND EVERY 6,000 FC THEREAFTER. HFEC METHOD IAW NDT 53-00-06 PT6. MAJOR REPAIR.

Part: SKIN — DENTED (BS 333.45 S21-22) · airframe 54,902 hrs · 18,656 cycles

DENT ON FUSELAGE SKIN, STA 333.45 BETWEEN S-21L TO S-22L REQUIRES REWORK DUE TO INCORRECT SRM REF USED. DENT ON FUSELAGE SKIN STA 333.45 BETWEEN S-21L TO S-22L FOUND OUT OF LIMITS DUE TO PROXIMITY TO FRAME IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, PG 203, FIG 201, TABLE I REPAIR 15. CATEGORY "B" ZONE A REPAIR WITH SUPPLEMENTAL INSP THRESHOLD 25,000 FC INITIAL AND EVERY 3,000 FC INTERVAL. LFEC METHOD IAW NDT 53-00-06, PT6.

Part: BULKHEAD — GOUGED (ZONE 400) · airframe 54,902 hrs · 18,656 cycles

NR 2 PYLON AFT BULKHEAD GOUGED INBD AND OTBD LOWER CORNER. COMPLIED WITH EA F-5450-141204- NACELLES/ PYLONS -(AD 2003-18-05), ENGINE STRUT AFT BULK HEAD LOWER CORNERS CHAFED USING REPAIR PARTS FABRICATED ON TRAVLERS. T10/852810, T10/852831, T10/852832. THIS IS A MAJOR REPAIR. SIGNED 8100-9 DATED 10/01/10. (PYLON STA 203.5 TO 203.5)

Part: SPAR — GOUGED (VERTICAL STAB) · airframe 54,902 hrs · 18,656 cycles

BETWEEN AFT SPAR AND RUDDER RIB STA 97.354 LT SIDE HAS 2 GOUGES. REPAIRED DAMAGE IAW EA F-5530-143212. STABILIZER-VERTICAL-ELONGATED HOLES IN TRAILING RIB. MAJOR REPAIR.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 54,902 hrs · 18,656 cycles

RT WING INBD MAIN FLAP OTBD END AREA T/E LOWER SIDE HAS CHAFED AREA. REMOVED GOUGE ON RT WING I/B MAIN FLAP O/B END AND FOUND OUT OF LIMITS IAW SRM 57- 53-01 FIG 101 DETAIL V. REPAIRED FLAP IAW SRM 57-53-01 REPAIR 2. EA F-5750-146241. MAJOR REPAIR

Part: SKIN — DAMAGED (ZONE 100) · airframe 54,902 hrs · 18,656 cycles

SCRIBE LINE FOUND AT STA 664.438-668.813 S26L. DURING LAP SEAM INSP, REPAIRED DAMAGE TO SKIN STA 664-668 S-26L PER EA F-5330-142243 FUSELAGE -PLATES AND SKIN - AD2007-19-07/EO F-5330-7-5000-SCRIBE LINE FINDINGS. MAJOR REPAIR

Part: SKIN — GOUGED (BS 686 S7R) · airframe 54,902 hrs · 18,656 cycles

GOUGE ON RT FUSELAGE SKIN NEAR R-2 DOOR UPPER FWD CORNER, STA 686,STR 7R. REPAIR ACCOMPLISHED IAW EA 757-5331-16-F2978 REF FAA FORM 8110-3, DATED NOV 22, 2010. (FIRST STAGE APPROVAL DTA PENDING) REF EA F-5330-1432220. THIS NR IS FOR TRACKING PURPOSES ONLY. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION BS 324 TO BS 350, RBL 40 TOP SIDE. REMOVED CORROSION IAW SRM 51-40-02. ORIG MAT THICKNESS .100 MAT LOSS .031 MAT REMAINING .069 FOUND AREA OUT OF LIMITS IAW SRM 53-00-51, PAG 103, DETAIL III, FIG 101. R & R FLOOR SUPPORT- (CHANNEL) PN 141N5161-40 BATCH NR 0001950763 IAW SRM 51-40-02 AND 51-20-05. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1120-1139) · airframe 54,902 hrs · 18,656 cycles

EXTERNAL FUSELAGE SKIN, FOUND DENTED AT BS 1120-1139.819, STRINGER 8R. FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101, DETAIL. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FIG 201, REPAIR 2. CLASSIFIED CATEGORY "B" MAJOR REPAIR WITH SUPPLEMENTAL INSPECTION DUE INITIAL 25,000 F/C THEREAFTER REINSPECT EVERY 6,000 F/C USING HFEC METHOD PER NDT MANUAL 51-00-01 PT6.

Part: GATE — CORRODED (L4 DOOR) · airframe 54,902 hrs · 18,656 cycles

L-4 DOOR UPPER GATE HAS CORROSION. R & R L-4 PASSENGER ENTRY DOOR UPPER GATE IAW MM 52-11-38-4 AND SRM 51-10-02, FIG 101. PERFORMED ADJUSTMENT CHECK IAW MM 52-11-00-5. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 54,902 hrs · 18,656 cycles

DENTS ON FUSELAGE SKIN STA 580-600 BETWEEN STR 27L-28L EVLAUATED DENT AT STA 580-600 BETWEEN S-27L TO S28L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III, DUE TO DENT BEING LESS THAN .5 FROM FRAME. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FIG 201, REPAIR 3. CLASSIFIED CAT "B" MAJOR REPAIR WITH SUPPLEMENTAL INSP REQUIREMENT OF INITIAL INSP AT 25,000F/C'S WITH REPEAT INSP EVERY 6,000 F/C'S USING HFEC PROCEDURE.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT SEAT TRACK TOP HAS DOUBLE HOLES. BS 740 TO 760 RBL 45.50. FOUND DOUBLE HOLES AT FLANGE OUT OF LIMITS IAW SRM 53-00-52, DETAIL "G", FIG 101 PG 101. R & R SEAT TRACK IAW SRM 51-40-02 AND 51-20-05 AT BS 640- 780, RBL 45.50. MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MCD UPPER LOBE- FRAME AT STA 1520, S3L CRACKED. REMOVED DAMAGED AREA IAW SRM 51-10-02. FABRICATED NEW FRAME SECTION ON TRAV T10/854913, CHANNEL NR1 (2EA) TRAV T10/854912 & CHANNEL NR2 (2EA) TRAV T10/854911. LOC & DRILLED IAW SRM 53-00-07. TREATED & PRIMED IAW SRM 51-20-01. COLD WORKED FASTENER HOLES IAW SRM 51-40-09, INSTALLED FRAME, NR1 & NR2 CHANNELS IAW SRM 53-00-07, FIG 201, DETAIL I, CAT "B" REPAIR. 12,000 FLIGHT CYCLES FROM INST- OR 50, 000 AIRFRAME CYCLES. WHICH EVER OCCURS IST. DVI INSP. REPAIR NR1. MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MCD UPPER FRAME AT STA 1560 CRACKED AT STR 2R. REMOVED DAMAGED FRAME SECTION IAW SRM 53-00-07, REPAIR 1 FABRICATED NEW FRAME SECTION AND REPAIR PARTS ON TRAVELERS T10/854916, T10/854914 AND T10/854915. LOCATED AND DRILLED IAW SRM 53-0007 COLD WORK HOLES IAW SRM 51-40-09 AND INSTALLED REPAIR. THIS IS MAJOR CLASS "B" REPAIR TO BE INSPECTED 37,000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST(REPAIR INSP DETAIL VISUAL AT INTERVAL OF 12,000 FLIGHT CYCLES).

Part: SKIN — DAMAGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

ACFT SKIN STA, 686 DAMAGED AT STRINGER 7R AT STA 686 STR 7R A MAJOR REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F MOD ON STAM W/O 11850045JUPR07 AND STAM EA 757-5331-16-2978, REV NEW DATED NOV 3, 2010. THIS NR IS FOR TRACKING PUPOSES ONLY AND CLASSIFED AS A MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPT. SEAT TRACK HAS CHAFFED MARKS, GOUGES, AND NICKS STA 640-780 RBL 24.75 REMOVED DAMAGE ON SEAT TRACK STA 640-780 RBL 24.75 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. ORIG MATERAIL .265 REMOVED .025. MAX MATERIAL LOSS ALLOWED .020. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. CLASSIFED CATEGORY "A" MAJOR REPAIR

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARMENT CREASE BEAM HAS CORROSION RBL 62, BS 1260-1290. BLENDED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .070 MAT. REMAINING .059 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PG 105, FIG 101, DET. VIII, R & R CREASE BEAM FROM STA 1180 TO 1290 RBL 62 IAW SRM 51-40-02. FABED NEW BAC 1515-553 IAW DWG 146N5590-59. MAJOR REPAIR.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 54,902 hrs · 18,656 cycles

NR1 PYLON LT SIDE SKIN 1 EA AND RT SIDE SKIN HAS 2 EA ELONGATED HOLES AT AFT BULKHEAD. COMPLIED WITH STAM EA 757-5450-16 F2907 REV - ELONGATED FASTENER HOLE FOUND IN THE RT AND LT SKIN OF NR1 PYLON COMMON TO BULKHEAD AT PP STA 201.5. EA F-5450-14227 NACELLES/PYLON-(AD2003-18-05)-EO F-5450-7-5010, NR 1 ENGINE PYLON SIDE SKIN DAMAGE HOLES ISSUED TO TRACK REPAIR IN SYS FAA FORM 8100-9 DATE 10-05/10 ATTACHED.PYLON PN 311N3000-25, SN 000440. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

L-2 DOOR INNER CHORD HAS SURFACE CORROSION BET BSTA 700-720 LBL 64. BLENDED AREA & REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS, MATERIAL THICKNESS .080", MAT LOST .010" MATERIAL REMAINING .070" WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, PAG 106, DETAIL IV. REMOVED CHORD ( BS 695 TO BS 755, LBL 64) IAW SRM 51-40-02. RECEIVED NEW CHORD PN 143N8328-53, INSTALLED NEW CHORD IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — DENTED (BS 310) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT FLOORBEAM HAS DENT BS 310.5. DENTS ON FLOOR BEAM STA 310.5 NOT PERMITTED IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02. CLASSIFIED CAT "A" MAJOR REPAIR

Part: STRUCTURE — DAMAGED (NR 1 NACELLE) · airframe 54,902 hrs · 18,656 cycles

NR1 PYLON 1EA CODE L HOLE INCOMING DIA. .312, EO F-5450-7-5010 P5 CALLS FOR .2651-.2661 COMPLIED WITH EA F-5450-141205. NACELLES/PYLON-NR 1-INCOMING OVERSIZED HOLES. CLASSIFED CATEGORY "A" MAJOR REPAIR.

Part: BULKHEAD — GOUGED (ZONE 400) · airframe 54,902 hrs · 18,656 cycles

NR 2 PYLON AFT BULKHEAD GOUGED INBD AND OTBD LOWER CORNERS. MACHINED DAMAGED AREAS, FABRICATED & INSTALLED REPAIR FILLERS AND GUSSETS IAW EA F-5450-141204 AND TRAVLERS T10/852810, T10/852831, T10/852832. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 54,902 hrs · 18,656 cycles

DENT ON FUSELAGE SKIN STA 33.45 BETWEEN S-21L TO S-22L. FOUND OUT TO BE OUT OF LIMIT IAW SRM 53-00-01, PG 101. DETAIL IV HFEC ON CUT- OUT & INITIAL FUSELAGE HOLES IAW NTM 51-00-19PT 6, NO CRACK NOTED. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 PG 201, TABLE I. INSTALLED DOUBLER & FILLER IAW SRM 51-40-02 AND SRM 53-00-01 PG 201, FIG 201, REPAIR 2, CAT B REPAIR ZONE A, THRESHOLD INSP 37,500 FLIGHT CYCLE, INTERVAL 6,000 FLIGHT CYCLE, HFEC, NDT PT6 51-00-01. MAJOR REPAIR.

Part: BULKHEAD — CHAFED (ZONE 400) · airframe 54,902 hrs · 18,656 cycles

NR 1 PYLON AFT BULKHEAD RT BOTTOM CORNER SIDE HAS CHAFED MARK NAC STA 201.02. MACHINED DAMAGED AREA, FABRICATED & INSTALLED REPAIR FILLER IAW EA F-5450-142253 AND TRAVLERS T10/852836 & T10/852837. MAJOR REPAIR.

Part: BULKHEAD — CHAFED (ZONE 400) · airframe 54,902 hrs · 18,656 cycles

NR 1 PYLON AFT BULKHEAD LT BOTTOM CORNER SIDE AND EDGE HAS CHAFED MARK, NAC STA 201.02. MACHINED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER IAW EA F5450-142253, AND TRAVLERS T10/852834, T10/852833. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

SEAT TRACK CORRODED STA 1640, RBL45. REMOVED CORROSION ON STA RBL 45.5 IAW SRM 51-10-02 ORIG MAT=.100" AFTER REWORKED 0.050" FOUND OUT OF LIMIT IAW SRM 53-00-52, FIG 101, SH3 T0 6 DETAIL V L=6" W=2" D=0.050", R & R SEAT TRACK FROM STA 1540-1640 RBL 45.5 FABRICATED FROM MAT PN BAC 1520-792 STRUSION BATCH NR 1891618 IAW SRM 51-40-02 & SRM 53-60-52, FIG I, PAGE 2. MAJOR REPAIR

Part: SKIN — DAMAGED (BS 1140-1360) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

EXTERNAL SKIN BS 1140 TO 1360 16R/28R HAS SCRATCHES, CORROSION(COMMON TO WTB FAIRINGS). REMOVED CORROSION FROM SKIN STA 1140-1360 S-16R TO S-28R AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II. ORIG MAT .055 AFTER REWORK .023. REPAIRED SKIN IAW SRM 53-00-01 REPAIR 5. CLASSIFIED CATEGORY "B" REPAIR WITH SUPPLEMENTAL INSP ACCOMPLISHED AT THRESHOLD 3,000F/C WITH REPETITIVE INSP AT 12,000 F/C.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS CHAFFED MARK AND GOUGES.BS 418 TO 440, RBL 45.50. REMOVED CORROSION FROM CROWN, REMOVED .031 MAT (NO THICKNES), FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52 FIG 101 DET I. FABRICATED NEW SEAT TRACK OF PN BAC1520-792, BATCH 0001891618 IAW SRM 53-10-52,FIG 101, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. CATEGORY "A". MAJOR REPAIR.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

FWD CARGO PIT, STA 770, S27L, WL 138 CORRODED. REMOVED DAMAGED AREA OF STR IAW SRM 53-00-03, FABRICATED FILLER AND SPLICE ON TRAV NR T10/856553 AND T10/856554 BATCH NR 0001611893, 7075-0.090C LOCATED , DRILLED, AND INSTALLED SPLICE AND FILLER IAW SRM 53-00-03, ZONE 1 37,500 AIRFRAME FLIGHT CYCLES GENERAL VISUAL INSP. CATEGORY "A" , MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 760-780 S26L) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

CORROSION ON STRINGER 26L BS 760-780 INSIDE FWD CGO COMPARTMENT. REMOVED DAMAGE IAW SRM 51-10-02 CHECKED LIMITS ON STA 760 S-26L SKIN ATTACHMENT (STRINGER) FOUND TO BE EXFOLIATED AROUND HOLES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 101 SHEET 1 PG 105 IAW SRM 53-00-53, REPAIR STRINGER FROM 760-775 S-26L PER SRM 53-00-03. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK SEAT TRACK GOUGE IN SEVERAL AREAS FROM STA 1540 TO 1640, LBL 45.5. REMOVED GOUGE AREA IAW SRM 51-10-02, ORG MAT THINESS .180" AFTER REWORKED FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, FIG 101, SH2 PAGE 102 L=6" W=1" D=0.050" R & R SEAT TRACK FROM STA 1540,1640,LBL 45.5 FABRICATED FROM MAT P/N BAC 1520-792 STRUSION BATCH NR1891618 IAW SRM 53-60-52, FIG 1, PAGE 2 AND SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

STA 418, RBL-45 AFT SEAT TRACK FITTING IS MISLOCATED (INCOMING). REMOVED FITTING AT RBL 45, STA 418, SEAT TRACK SPLICE IAW SRM 51-40-02, RECEIVED NEW FITTING PN 14N2504-1 BATCH 1923858, INSTALLED FITTING AT RBL 45 STA 418 SEAT TRACK SPLICE IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

MAIN DECK FLOOR SUPPORT ANGLE CORRODED AT STA 374, LBL 58. REMOVED COPRROSION ON CHANNEL IAW SRM 51-10-03 CHECKED LIMITS ORIGINAL MAT .050. REMAINING .042 LOSS .008 FOUND OUT OF LIMITS DETAIL FIG 101 PG 103 W=2.00 L=3.00 DEPTH .008 IAW SRM 53-00-51 R & R IAW DWG 141N5170-48, MINOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1540-1640) · airframe 54,902 hrs · 18,656 cycles

SEAT TRACK GOUGE IN SEVERAL AREA FROM STA 1540 TO 1640 LBL 24. GOUGES ON SEAT TRACK STA 1540-1640 LBL 24 MEASURED OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS CHAFFED MARK AND GOUGES BS 418 TO 440 RBL 25.75. REMOVED .023 MATERIAL FROM SEAT TRACK CROWN AT STA 418-440,RBL 25.75,OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DET I REMOVED SEAT TRACK FABRICATED NEW SEAT TRACK FROM MATERIAL P/N BAC 1520-792, BATCH 1891618 IAW SRM 53-00-52 DET I INSTALLED NEW SEAT TRACK AT RBL 25.75 ,STA 418-440 IAW SRM 51-40-02. MAJOR REPAIR

Part: FRAME — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MCD FRAME WITH 3EA GOUGES STA 1280 STR 10L,11L AND 13L. EMOVED GOUGES STA 1280 BETWEEN S-10L TO S-13L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. ORIG MATERIAL .071 AFTER REWORK .062. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 1.

Part: FRAME — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

RH CABIN FRAME AT B STA 1280 BETWEEN S-10R THRU S-12R HAS AREAS GOUGED AND SCRATCHED. REMOVED GOUGES STA 1280 BETWEEN S-10R TO S-12R AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. ORIG MATERIAL .071 AFTER REWORK .058. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 1.

Part: SHEAR WEB — CORRODED (BS 1680-1720) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT FLOOR SHEAR WEB HEAVY CORRROSION BS 1680 TO BS 1720 LBL 51.5 TO RBL 51.5. REMOVED CORROSION AT STA 1681-1720, LBL 51.5 TO RBL 51.5 ON SHEAR WEB 5 EA PLACES. NR 1 ORIG MAT .071 MAT. LOSS .019, REMAINING .052, NR 2. ORIG MAT .071, MAT LOSS .009 REMAINING .062 NR 3. ORIG MAT .071 MAT LOSS .015. REMAINING .056, NR 4 ORIG, MAT 071, MAT LOSS .011 REMAINING .060 NR 5, ORIG MAT .071 MAT LOSS .008 REMAINING .063, ALL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 DET, IV FIG 101, PG 103, FABRICATED NEW WEB IAW DWG 145N5318. R & R WEB IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1420) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

RH MAIN DECK CREASE INNER CHORD AT STA 1420 BOTTOM SURFACE NEAR SCREW HOLES CORRODED. RT SIDE CREASE BEAM IB CHORD STA 1420 MEASURED OUT OF LIMITS IAW SRM 53-60-15 FIG 101 DETAIL III. REMOVED AND REPLACED CHORD IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR

Part: SUPPORT — CRACKED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

SEAT TRACK SUPPORT STA 365-418 RBL 24 CRACKED. REMOVED SEAT TRACK SUPPORT, FABRICATED NEW SEAT SUPPORT IAW SRM 53-10-52 PG3,DETAIL II INSTALLED NEW SEAT TRACK SUPPORT AT RBL 24 STA 365-418 IAW SRM 51-40-02. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

STA 365-418, RBL 45, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION, ORIGIN MAT .070, MAT REMOVED .028, MAT REMAINING .042 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52 FIG 101 DET VII. REMOVED DAMAGED SEAT TRACK SUPPORT IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK SUPPORT IAW SRM 53-10-52, INSTALLED NEW SEAT TRACK SUPPORT IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.

Part: FAILSAFE — CORRODED (BS 700-720) · airframe 54,902 hrs · 18,656 cycles

FAIL SAFE CHORD HAS SURFACE CORROSION BET BSTA 700-BSTA 720 RBL 64 (NEAR R-2 DOOR). REMOVED CORROSION FROM CHORD STA 600-720 ORIGINAL MAT .080 REMOVED .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15 DET III, PAG 106. R & R CHORD, PN 143N8328U54, MAJOR REPAIR .

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

SEAT TRACK LBL 45.50 FROM BS 1075 TO 1180 HAS GOUGES, CHAFE MARKS AND WORN SCALLOPS. BLENDED DAMAGED AREA IAW SRM 51-10-02 ORIGINAL THICKNESS .230 MAX CLEAN UP DEPTH ON TOP SURFACE .020 MATERIAL REMOVED .03 FOUND TO BE OUT OF LIMITS IAW 53-00-52 FIG 101 DETAIL I, PAGE 102. FABRICATED NEW SEAT TRACK BATCH NR 1869949 FROM BAC1520-792 IAW SRM 53-40-52 LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-02. MAJOR REPAIR

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT UNDER SEAT TRACK WEB HAS GOUGE BS 780 TO 879 RBL 45.50. REMOVED GOUGE UNDER SEAT TRACK WEB BS 780 TO 879 RBL 45.50 IAW SRM 51-10-50 CHECKED LIMITS MATERIAL THICKNESS .145" MATERIAL LOST .015" MATERIAL REMAINING .130" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I. REMOVED SEAT TRACK FROM BS 780 TO 879 RBL 45.50 IAW SRM 51-40-02 RECEIVED NEW MATERIAL BAC 1520-792 BATCH NUMBER 0001869949. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-05 TREATED PRIMED IAW SRM 51-20-01 INSTALLED SEAT TRACK BS 780 TO BS 879 RBL45.50. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 377.5) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

MAIN DECK SEAT SUPPORT CORRODED AT STA 377.5, LBL24. REMOVED .024" FROM .070" ORIGINAL MATERIAL,OUT OF LIMITS IAW SRM 53-0052 FIG 101 DET VII REMOVED SEAT TRACK SUPPORT, FABRICATED NEW SEAT TRACK SUPPORT IAW SRM 53-10-52 DET III INSTALLED NEW SEAT TRACK AT 377.5-418, LBL 24 IAW SRM 51-40-02. MAJOR REPAIR

Part: SEAT TRACK — GOUGED (BS 1075-1180) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AND CHAFED MARKS BS 1075 TO 1180 RBL 45.50. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 NOTE "G". R & R ON SEAT TRACK IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 54,902 hrs · 18,656 cycles

INSIDE CABIN STA 1640 LBL 58" FLOORBEAM HAS CORROSION AT FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS FOUND REMAINING MAT 0.095", OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DET VI. REMOVED FLOORBEAM AT STA 1640 IAW SRM 51-40-02, RECEIVED NEW FLOORBEAM PN BAC 1518-338/18A, BATCH 1847767, TRIMED BOTH END AND DRILLED FASTENER HOLES IAW SRM 51-40-02, INSTALLED NEW FLOORBEAM AT STA 1640 BETWEEN LBL70 TO RBL 70 IAW SRM 53-60-51, PAGE 5, FIG 1 AND SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK SEAT TRACK GOUGES AT STA. 418 LBL24. REMOVED 0.032" GOUGED MATERIAL FROM SEAT TRACK CROWN. OUT OF LIMITS IAW SRM 53-00- 52 DET.I AND SRM 51-10-02. MAJOR REPAIR

Part: SEAT TRACK — GOUGED (BS 418) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK SEAT TRACK GOUGED AT STA 418 LBL 45. REMOVED 0.025" GOUGED MATERIAL FROM SEAT TRACK CROWN. OUT OF LIMITS IAW SRM 53-00-52 DET.I AND SRM 51-10-02. REMOVED SEAT TRACK . FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 DET I INSTALLED NEW SEAT TRACK AT LBL 45 STA 418-440 IAW SRM 51-40-02. MAJOR REPAIR

Part: STRINGER — CORRODED (BS 600 S26L) · airframe 54,902 hrs · 18,656 cycles

FWD PIT STRINGER CORRODED 26L AT FRAME STA 600. REMOVED CORROSION ON STRINGER STA 600 S-26L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL II. R & R STRINGER IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

FLOORBEAM UPPER TEE SURFACE HAS CORROSION BS 1661 LBL 55 NEAR DOOR TRESHOLD. REMOVED CORROSION IAW SRM 51-10-02, ORIG MAT THICKNESS 0.125" MEASUREMENT. FOUND OUT LIMITS IAW 53-00-51,PG 101,FIG 101, DETAIL VII. REMOVED & REPLACED FLOORBEAM IAW SRM 53-00-51, PG 5 AND FIG 1. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 878-900) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT SEAT TRACK HAS SEVERALS GOUGES AND CHAFFED MARKS BS 878 TO 900 RBL 45.50. DAMAGE TO SEAT TRACK MEASURED OUT OF LIMITS IAW SRM 53-00-52 PG102 FIG 101 DET I. REPLACED SEAT TRACK IAW SRM 51-40-02 PG 1 PAR A REPAIR CATEGORY A. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT FLOORBEAM, STA 1320 HAS CORROSION ON TOP SIDE. REMOVED CORROSION ON FLOORBEAM, STA 1320 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. ORIG MATERIAL .125 AFTER REWORK .106. R & R FLOORBEAM IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK SEAT TRACK GOUGE AT STA 839 TO 879, LBL 24. DAMAGE TO SEAT TRACK MEASURED OUT OF LIMITS IAW SRM 53-00-52, PG 102, FIG 101, DET I. REPLACED SEAT TRACK IAW SRM 51-40-02, PG 1, PAR A REPAIR CATERGORY A. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK FLOORBEAM UPPER TEE CORRODED FROM BL 0 TO LBL 24.5 STA 345. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL THICKNESS .125" AFTER REMOVED .106" FOUND OUT OF LIMITS IAW 53-00-51, FIG 101, DET III REMOVED FLOORBEAM AT STA 345 BET, LBL 70 RBL 70 AND ASSY PARTS FOR ACCESS IAW SRM 51-40-02 RECEIVED NEW FLOORBEAM PN BAC 1518-338, BATCH 1898860, TRIMED BOTH END PICKED UP EXISTING FASTENER HOLES IAW DWG 141N5111 AND SRM 53-10-51 PAG 4 FIG 1. INSTALLED NEW FLOORBEAMAND ASSY PARTS IAW SRM 51-40-02 AND DWG 141N5111. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 600) · airframe 54,902 hrs · 18,656 cycles

MAIN CARGO COMPARTMENT FLOORBEAM HAS CORROSION AND ELONGATED HOLES TOP SIDE AT STA 365. REMOVED CORROSION ON FLOORBEAM, STA 365, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MATERIAL .125 AFTER REWORK .023. R & R FLOORBEAM IAW SRM 51-40-02. CLASSIFIED CATEGORY "A", MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 54,902 hrs · 18,656 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT STA 377.5, LBL 38.5-45.5. REMOVED CORROSION FROM FLOORBEAM UPPER CHORD AT STA 377 BETWEEN LBL 20 AND LBL 58 IAW SRM 51-10-02. REMOVED .017 FROM .125 ORIGINAL THICKNESS. MATERIAL FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REMOVED FLOORBEAM AND FABRICATED NEW WITH PN BAC 1518-338, BATCH 1898860 IAW DWG 141N5113 AND INSTALLED IAW DWG 141N5113 AND SRM 53-10-51. MAJOR REPAIR.