N919FD

Part: SKIN — DENTED (ZONE 100) · airframe 78,558 hrs · 29,351 cycles

INCOMING A/C DAMAGE JUST BELOW AND FWD OF THE MAIN CARGO DOOR. DENT MEASURING APPROX 2"X3" AND MAX DEPTH OF 0.0119. LOCATED 2" AFT OF FS460 JUST BELOW STR 18L. FUSELAGE - PLATES AND SKINS - INCOMING DENT DAMAGE FWD OF MAIN CARGO DOOR - DOUBLER REPAIR. ACCOMPLISHED EA F-5330-T0380626 PT1. SRM 53-00-01 REPAIR 29. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 78,558 hrs · 29,351 cycles

MAIN DECK FLOORGOARD PANEL 251MXF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MXF ON VTMAE TRAVELER #T24/1774251 IAW SRZ-25-005 REVISION R DRAWING MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 78,558 hrs · 29,351 cycles

MAIN DECK CARGO COMPT FLOORBOARD PANEL 251 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER T24/1774230 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 78,558 hrs · 29,351 cycles

MAIN DECK CARGO COMPT FLOORBOARD PANEL 252 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MWF ON VTMAE TRAVELER T24/1774253 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.

Part: SUPPORT — DAMAGED (LT FLAP FAIRING) · airframe 78,455 hrs · 29,274 cycles

L/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGED HOLE AND REPLACED BRACKET REF. B757 SRM 57-53-02-2R REPAIR 3. AND INSTALLED FAIRING TO BRACKET REF. B767 51-40- 02 AND BOEING DWG'S 113N2002 AND 113N1752.

Part: WINDOW — CRACKED (COCKPIT) · airframe 78,350 hrs · 29,199 cycles

WHILE IN CRUISE FLIGHT FL360, CAPTAIN SIDE FRONT WINDSCREEN ARCED FOLLOWED BY SHATTERING WITH OUTER PAIN. RAN QRH, ARCING CONTINUED. POSSIBLE DEFORMED WINDOW WITH CONTINUING ARCING THROUGHOUT DESCENT. EMERGENCY DECLARED. REMOVED & REPLACED L1 WINDOW AS PER AMM 56-11-01-4. ALL REQUIRED OP CHECKS CHECK GOOD. ACFT OK FOR SERVICE.

Part: TRANSMISSION — CONTAMINATED (TE FLAPS) · airframe 78,330 hrs · 29,185 cycles

TE FLAP DISAGREE MESSAGE FOLLOWING SELECTION OF FLAPS 1. FLAPS INDICATED UP. COMPLETED QRH. DECLARED EMERGENCY. LANDED FLAPS 20. PERFORMED FIM 27-51 FT 808, NO FAULTS FOUND. NO OVERLOAD INDS WERE TRIPPED ON FLAP XMSNS. FLAP CONTROL LEVER MOVES FREELY WHEN SELECTING EACH FLAP POSITION. ALL FLT DECK INDS NORMAL & FLAPS MOVE SMOOTHLY WITHOUT BINDING OR ABNORMAL NOISE. NO EVIDENCE OF BINDING FOUND ON FLAP CARRIAGES, TORQUE TUBES, TRACKS/ROLLERS, OR BALLSCREWS, GIMBALS. COMPLETED TE FLAP SYS LUBE IAW AMM 12-21-09-3. FOUND WATER IN INBD XMSN OF LT INBD FLAP. FOUND DIRTY OIL IN OTBD XMSN OF RTOTBD FLAP. DRAINED & REFILLED XMSNS IAW 12-13-06-3. SUSPECT WATER IN L/W INBD XMSN FROZE. NO OTHER FAULTS.

Part: BOTTLE — FAILED (R1 DOOR ASSIST) · airframe 78,330 hrs · 29,185 cycles

R1 DOOR SLIDE ASSIST BOTTLE EXTINGUISHED DURING OPENING OF R1 DOOR. REMOVED AND REPLACED R1 DOOR EMERGENCY POWER RESERVOIR CYLINDER. REPLACED R1 DOOR SLIDE IAW B757 AMM 25-66-01-4. A/C OK FOR SERVICE.

Part: CHARGER — FAILED (N/A) · airframe 77,951 hrs · 28,920 cycles

MDIS 919 33-50 5583 13AUG23 SHV FACT U DURING SERVICE CHECK FOUND L1 DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP FACT 14AUG23 20:34 SHV U AMM: 33-51-07-02 REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-07-02. OPS TESTED GOOD.

Part: NONE — NONE (R1 DOOR SLIDE) · airframe 77,423 hrs · 28,571 cycles

DUE TO WRI 25-60/5015 AND A POSSIBLE SAFTEY CONCERN OF THE NORMAL OPERATION OF THE R1 DOOR SLIDE WHEN OPENING FROM THE EXTERIOR. R1 DOOR, TO INCLUDE THE SLIDE, IS TO BE PLACED ON MEL AND HAVE AN INSPECTION PLANNED AT AN APPROPRIATE GROUND TIME IAW AMM 52-11-13-2, AND AMM 52-11-20-5. COMPLIED WITH TSI 52-10/5020, INSPECTED R1 DOOR, IAW AMM 52-11-13-2, STEP 5, & AMM 52-11-20-5, STEP H3. NO DEFECT NOTED AND ALL MESSUREMENTS ARE IN LIMITS.

Part: LIGHT — MALFUNCTIONED (R14 DOOR SLIDE) · airframe 77,416 hrs · 28,566 cycles

R1 SLIDE LIGHT DOES NOT EXTINGUISH WHEN DISARMING DOOR. ACCOMPLISHED GIRT BAR ESCAPE SLIDE ARM & DISARMED OPERATION IAW AMM 25-66-00-10 & 25-66-01-4. ALL INDICATIONS OPS CHECKED NORMAL. ORIG SUB DATE: 11/30/2022

Part: RESERVOIR — FALSE ACTIVATION (R1 DOOR SLIDE) · airframe 77,418 hrs · 28,567 cycles

UPON BLOCK IN PILOTS REQUEST MAINTENANCE TO OPEN R1 DOOR FROM OUTSIDE DUE TO INDICATION MEL. WHEN OPENING DOOR BOTTLE DISCHARGED AND SLIDE FELL OUT OF BUSTLE BUT DID NOT INFLATE. REMOVED R1 DOOR EMERGENCY POWER RESERVOIR AND REPLACED WITH R1 DOOR EMERGENCY POWER RESERVOIR. ORIGINAL SUBMISSION DATE: 11/30/2022

Part: FRAME — CRACKED (BS 1460 S26L) · airframe 77,369 hrs · 28,533 cycles

WHILE PERFORMING HFEC INSP OF FRAME WEB INBD OF STRINGER S-26L AT BODY STATION 1460, FOUND CRACK INDICATON ON INBD HOLE AT 6:O,CLOCK. ACCOMPLISHED REPAIR PER EA TF-5310-T0371176 EA TITLE: FUSELAGE - MAINFRAME - STA1460 FRAME BETWEEN S-26L AND S-27L CRACK REPAIR. THIS EA DEVIATES FROM EO F-5310- E0347443. MAJOR REPAIR

Part: FLOORBOARD — DENTED (MAIN CARGO) · airframe 77,369 hrs · 28,533 cycles

MAIN CARGO FLOOR PANEL 241MMF IS DAMAGE. FABRICATED ZONE 240 FLOORBOARD 241MMF ON VTMAE TRAVELER # T22/1641931 IAW DWG SRZ- 25-005 REVISION R. PART MARK PER GMM 07-0-1000. MAJOR REPAIR.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 77,369 hrs · 28,533 cycles

ZONE 220 FLOORBOARD 221 MBF IS DAMAGED. FABRICATED COURIER AREA FLOORBOARD 221 MBF FROM TRAVELER T22/1641793 IAW DWG SRZ- 25-005. PART MARKED IAW GMM 07-01-1001. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 77,369 hrs · 28,533 cycles

ZONE 220 FLOORBOARD 221 BF IS DELAMINATED. FABRICATED COURIER AREA FLOORBOARD 221BF FROM TRAVELER T22/1640838 IAW DWG SRZ-25- 005. PART MARKED IAW GMM 07-01-1001. MAJOR REPAIR

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 77,256 hrs · 28,476 cycles

AT 300FT ON LANDING, WE EXPERIENCED A L HYD QTY MESSAGE, FOLLOWED BY L HYD SYS PRESS UPON LANDING. HYD QTY SHOWS 0.00. DUE TO L HYD SYS TOTAL LOST OF FLUID, INTERNAL DAMAGE CHECK FOR LEFT ENGINE-DRIVEN PUMP MUST BE PERFORMED. AMM 20-10-10-8 TEMPORARY REPAIR OF FLEXIBLE HYD HOSES INSTALLATION OF A FLEXIBLE HOSE IS NOT CONSIDERED TO BE A PERMANENT REPAIR FOUND NOSE LANDING GEAR FLEXIBLE HOSE BROKEN. PERFORMED TEMPORARY REPAIR AS PER AMM 20-10-10-8 USING ALTERNATE HOSE CPN 3211517 DUE TO ORIGINAL PART NOT AVAILABLE AT STA. APPROVED FOR AN OIL. WORK PERFORMED IAW AMM 29-11-00-2 STEP 1.E TABLE 201 "CONDITION 2. A PUMP FAILURE OR COMPLETE LOSS OF SYSTEM FLUID THAT CAUSES HYDRAULIC FLUID CONTAMINATION.

Part: SKIN — DENTED (CROWN) · airframe 77,071 hrs · 28,374 cycles

CROWN SKIN HAS OUTWARD DENTS LEFT AND RIGHT OF STRINGER 1 JUST FORWARD OF STA 418. REPAIRED DENTED CROWN SKIN PER EA F-5330-T036881

Part: PLUG — LOOSE (FUEL INDICATOR) · airframe 76,260 hrs · 27,831 cycles

AT CRUISE AT FL350 THE RIGHT AND TOTAL QTY INDICATIONS ARE INTERMITTENT. AT OTHER TIMES THE RIGHT QTY INDICATION FLUTUATED - 1,000 POUNDS. DIVERTED TO SIN AND MX APPLIED MEL 28-41-01-01/28-41-07-A FOUND M723 BUSSING PLUG UNIT WAS LOOSEN, RETIGHTENED THE PLUG UNIT. PERFORMED WIRING-CHECK FROM FQPU TO RH WING SPAR HARNESS CONNECTOR PER WDM 28-41-31, ALL GOOD. I.A.W FIM 28-41-00-2-1 AND AMM 28-41-08-4, PERFORMED FUEL QUANTITY BITE TEST, NO FAULT CODE SHOWN, PERFORMED FQPU RESET. MEL CLOSED. OK TO CONTINUE SERVICE.

Part: SPAR — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 76,112 hrs · 27,717 cycles

RIGHT HAND WING LEFT HAND TRAILING EDGE OUTBOARD MAIN FLAP REAR SPAR UPPER CHORD FOUND CORROSION AT AROUND WBL 387 OUTBOARD OF NR 7 FLAP TRACK. EA F-5750-T0357675 COMPLIED WITH. THIS REPAIR CLASSIFIED AS MINOR, AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 76,112 hrs · 27,717 cycles

MAIN DECK, CARGO SEAT TRACK FOUND CORROSION AT STATION 876, RBL 45.5 MAIN DECK STATION 876 RBL 45.5. CARGO SEAT TRACK CORROSION REPAIRED, AS PER B757 SRM 53-00-52-2R REPAIR 1 FIGURE 201. THIS REPAIR CLASSIFIED AS MAJOR, AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1180-1200) · airframe 74,411 hrs · 26,752 cycles

MDCC SEAT TRACK CORRODED B/W STA 1180-STA 1200, LBL 45.5. REPLACED THE CORRODED SEAT TRACK AT MDCC STA1180-STA1240,LBL45.5 PER B757 SRM51-40-02. MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 74,411 hrs · 26,752 cycles

MDCC CROSSBEAM CORRODED B/W STA1640, LBL24.75-LBL45.5. THIS IS A MINOR REPAIR, CLOSE THE SDR.

Part: SEAT TRACK — CORRODED (BS 1620-1640) · airframe 74,411 hrs · 26,752 cycles

MDCC SEAT TRACK CORRODED B/W STA1620-STA1640,LBL45.5. REPLACED THE CORRODED SEAT TRACK AT MDCC STA1540-STA1640,LBL45.5 PER B757 SRM51-40-02. MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: CROSSBEAM — CORRODED (BS 1680) · airframe 74,411 hrs · 26,752 cycles

MDCC CROSSBEAM CORRODED B/W STA1680,RBL0-RBL24.75. REPAIRED THE CORRODED CROSSBEAM AT MDCC STA1680,RBL0-RBL24.75 PER B757 SRM51- 40-02 AND SRM53-60-51 REPAIR 3. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 73,817 hrs · 26,328 cycles

L1 SLIDE WAS DEPLOYED BEFORE DEPARTURE. REMOVED AND REPLACED THE SLIDE IAW MM 25-66-01-4.

Part: MODULE — MALFUNCTIONED (NLG STEERING) · airframe 73,157 hrs · 25,789 cycles

AFTER LANDING, COMING OUT OF TURN ONTO TAXIWAY, NOSE WHEEL STEERING WAS UNRESPONDING FEELS AS THOUGH NWS TILLER WAS BINDING. PERFORMED RIGGING CHECK AND SYSTEM TEST OF NOSE WHEEL STEERING IAW MM 32-51-00-5-3. TEST PASSED 3 TIMES. TILLER MOVES NORMALLY LEFT AND RIGHT. NO HYDRAULIC LEAKS NOTED. INSPECTED ALL CABLES AND LINKS AS PER SAME AMM. NO FINDINGS. AS A PRECAUTION, THE METERING VALVE MODULE REPLACED. SUMMING MECHANISM COVER IS REMOVED AND PLACED IN THE LEADS OFFICE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 73,042 hrs · 25,712 cycles

LEFT ELEVATOR DAMAGED ON UPPER SURFACE. REPAIRED IAW EA F-5520-T0329101 P1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 402, 1.5'' ABOVE 24R REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 370, 1.5'' ABOVE STR 24RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6, SECTION I REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 409, 1.5'' ABOVE STR 24R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 SECTION I REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 535, 2.5'' ABOVE STR 23 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6 ,SECTION I, REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 329, 1.5'' ABOVE STR 24 RT. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201 REPAIR 6 SECTION I REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 692, 1.5'' BELOW STR 21R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01 FIG 201, REPAIR 6, SECTION I REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 282, 29'' BELOW LAPJOINT STR 20R. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01, FIG 201, REPAIR 6, SECTION I, REV 118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,042 hrs · 25,712 cycles

LIGHTNING STRIKE AT BS 468, 0.5" ABOVE STR 23R ON FUSELAGE SKIN. CARRIED OUT REPAIR IAW SRM 53-00-01 FIG 201 REPAIR 15 REV118

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 73,042 hrs · 25,712 cycles

DELAMINATION FOUND IN THE RT OTBD SLAT NR 7 T/E WEDGE UPPER AND LOWER SURFACE AT IB END. REMOVED AND REPLACED IAW AMM 27-81-02 ACCOMPLISHED EA F-5750-T0329030.

Part: STEERING SYS — OUT OF RIG (NLG) · airframe 72,837 hrs · 25,521 cycles

DURING TAKEOFF, AFTER ENGAGING THE THRUST TILE, THE ACFT WOULD NOT HOLD CENTERLINE. REJECTED TAKEOFF 08 L CDG. BOTH THRUST LEVERS WERE ALIGNED, RUDDER & AILERON WERE CENTERED. TROUBLE SHOT IAW FIM 32-51 TASK 802 & FOUND NOSE WHEEL STEERING NOT PROPERLY RIGGED. READJUSTED NOSE WHEEL STEERING IAW AMM 32-51-00-5 & PERFORMED STEERING TEST IAW AMM 32-51-00-5, ALL TESTED OK. PERFORMED BVCU BITE TEST IAW FIM 75-32 TASK 830, PERFORMED EEC BITE TEST IAW FIM 73-21 TASK 802, PERFORMED TPU BITE TEST IAW FIM 75-32 TASK 831, FOUND NO FAULTS. LUBRICATED THE STEERING COLLAR ON THE NLG IAW AMM 12-21-12-3. PERFORMED ON BOTH MLG , A BRAKE BLEEDING PROCEDURE IAW AMM 32-41-00-2. PERFORMED AUTO THROTLE TMC 02, SERVO TEST 10 & GND TEST 30 IAW AMM 22-00-02-2, ALL TESTS PASSED & NO FAULT DETECTED. RAN BOTH ENGS TO EPR=1.7 IAW JRH ALL PARAMETERS WERE NORMAL. FOR INFO EVERY EPR STEP THE THROTTLES WERE ALIGNED, 1.3, 1.5, 1.6 & 1.7.

Part: SWITCH — DIRTY (AUTOTHROTTLE SYS) · airframe 72,647 hrs · 25,356 cycles

ON TAKEOFF, AT APPROX 40 KTS, MASTER CAUTION ILLUMINATED WITH CHIMES, AUTO THROTTLE DISC, DISPLAYED ON EICAS. TAKEOFF WAS REJECTED. FOLLOWED QRH PROCEDURES, ALERT CLEARED. NORMAL TAKEOFF WAS COMPLETED. INSPECTED & CLEANED LT & RT AUTO THROTTLE DISCONNECT SWITCH INSIDE THE THRUST LEVER HANDLE IAW SMP. PERFORMED MCDP TEST 2 TMC, 10 A/T SERVO, 12 A/T DISC SWITCH, 30 CURRENT FAULT & 40 A/L IAW MM 22-00-02-2. ALL TEST PASSED, NO CURRENT FAULT. ACFT READY FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 725 hrs · 25,254 cycles

DURING CRUISE, LT FWD WINDOW ARCING & THEN OUTER PANE CRACKED. R & R NR 1 FLIGHT DECK WINDSHIELD IAW AMM 56-11-01-4. PERFORMED WINDOW HEATING SYS TEST, TEST PASSED. PERFORMED FIRST & SECOND TORQUE OF NR 2 BOLTS. THIRD TORQUE SEQUENCE WILL BE TRANSFERRED TO OIL.

Part: CYLINDER — INOPERATIVE (R1 DOOR) · airframe 724 hrs · 25,209 cycles

RIGHT DOOR OPEN WITH GIRT BAR ACTIVATED, BUT NO ACTIVATION SLIDE, NOT POSSIBLE TO ARM DOOR. R & R R1 DOOR EMER POWER CYLINDER IAW AMM 52-11-30-4-0. REINSTALLED & INSPECTED GIRT BAR IAW AMM 25-66-10-2, NO DAMAGE FOUND. PERFORMED R1 DOOR ESCAPE SYS ADJUSTMENT, TESTED SEVERAL TIMES IAW AMM 25-66-00-5. ALL TEST PASSED. MEL CLOSED & ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 724 hrs · 25,165 cycles

HEAVY BURNING ELEC SMELL IN COCKPIT WHEN ENCOUNTERING HEAVY RAIN & TURBULENCE FL360. ACCOMPLISHED EVIDENCE OF SMELL IAW MM:05-51-56-2, RUN APU WITH PACKS, INSPECTED E & E COMPARTMENT. NO MORE SMELL PRESENT.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 71,737 hrs · 24,623 cycles

RIGHT WING INBD FLAP UPPER SURFACE FOUND TO HAVE SMALL PUNCTURE HOLE. REPAIRED IAW SRM 51-70-17 TRACKING EA F-5750-T0312308.

Part: BRACKET — LOOSE (TE FLAP) · airframe 71,737 hrs · 24,623 cycles

RIGHT WING FAIRING 672HB BRACKET INBD SECURING BRACKET FOUND LOOSE FLAP. REPAIRED IAW EA F-5720-T0312233.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 71,737 hrs · 24,623 cycles

NUMBER 1 SLAT TE WEDGE DISBONDED ON UPPER & LOWER SURFACES. REPAIRED IAW EA F-5750-T0311993.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

BS 215 LIGHTNING STRIKE BETWEEN STRINGER 25 - 26L. REPAIRED IAW EA F-5300-T0312150.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 71,737 hrs · 24,623 cycles

NUMBER 5 SLAT FOUND TO HAVE TE WEDGE DISBONDED ON OTBD LOWER SURFACE. REPAIRED IAW EA F-5750-T0311994.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

THREE LIGHTNING STRIKES FWD OF E & E BAY DOOR. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

SUSPECT DENT LOCATED APPROX BS 213 STRINGER 26 - 27L. ASSESSED & REPAIRED IAW EA F-5300-T0312150.

Part: SKIN — DAMAGED (TE FLAP) · airframe 71,737 hrs · 24,623 cycles

LEFT WING OTBD MAIN FLAP LE BULLNOSE DAMAGED. REPLACED IAW SRM 51-40-02 & DWG 113N3500.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

LIGHTNING STRIKE FOUND AT BS 215 STRINGER 27L. REPAIRED IAW SRM 53-00-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,737 hrs · 24,623 cycles

SURFACE CORROSION ON FWD SHEAR DECK AFT OF 9G BARRIER. REMOVED IAW SRM 51-20-01. REPAIR CARRIED OUT IAW EA F-5300-T0311939A. REPAIR CLASSED AS MINOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

LIGHTNING STRIKE DAMAGE TO CROWN SKIN BS 1335 STRINGER 1. REPAIRED IAW EA 5300-T0312097.

Part: ARM — DAMAGED (RT MLG) · airframe 71,737 hrs · 24,623 cycles

RIGHT WING MLG REAR MOVEABLE FAIRING 671BB ACTUATING ARM FOUND DAMAGED. INVESTIGATE & RECTIFY IAW AMM SRM RT MLG MOVEABLE FAIRING 671BB ACTUATING ARM BLENDED & REPAIRED IAW F-5720-T0311986. REPAIR CLASSED AS MAJOR REPAIR, JPF STAGES SHOW DETAILS OF INITIAL BLEND STAGES.

Part: GATE — CHAFED (R4 DOOR) · airframe 71,737 hrs · 24,623 cycles

NUMBER 4R DOOR LOWER GATE AFT EDGE HAS CHAFING DAMAGE. NR 4R DOOR LOWER GATE ASSEMBLY REPLACED IAW AMM 52-11-38-4.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 71,737 hrs · 24,623 cycles

NUMBER 2R DOOR LOWER GATE EDGE IS CORRODED. NR 2R DOOR LOWER GATE REPLACED IAW AMM 52-11-38-4

Part: SKIN — WORN (TE FLAP) · airframe 71,737 hrs · 24,623 cycles

RIGHT WING OTBD FLAP LE BULLNOSE PAINT WORN AT INBD END RT WING OTBD FLAP LE BULLNOSE WEAR ASSESSED OUT OF LIMITS 2 INCHES X 1.25 INCHES X 0.046 INCHES, BULLNOSE SECTION REPLACED IAW SRM 51-40-02 & DWG 113N3500.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

LIGHTNING STRIKE TO FUSELAGE BS 1460 STRINGER 1R. REPAIR CARRIED OUT IAW SRM 53-00-01 REPAIR 6.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,737 hrs · 24,623 cycles

LIGHTNING STRIKE DAMAGE BS 1220 STRINGER 1 FASTENER. REPAIRED IAW SRM 53-00-01 REPAIR 6.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 71,737 hrs · 24,623 cycles

L1 DOOR LOWER GATE EDGE IS CORRODED. L1 DOOR LOWER GATE REPLACED IAW AMM 52-11-38-4

Part: SKIN — DAMAGED (ZONE 200) · airframe 71,737 hrs · 24,623 cycles

L1 DOOR SNUBBER SPRING CANISTER ASSEMBLY FOUND TO BE FOULING ON FUSELAGE SKIN INBD OF SPRING CANISTER. SKIN PANEL REPLACED IAW SRM 51-40-02, 51-40-05 REF DWG 141N8315.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,185 hrs · 24,181 cycles

DURING SERVICE CHECK, FOUND L1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. CHECKED FOR 28VDC AT LAMP & FOUND NO POWER, CONFIRMED GOOD GROUND. R & R EMERGENCY LIGHTS POWER SUPPLY, & BATTERY CHARGER, IAW AMM 33-51-07-2. PERFORMED OPS CHECK IAW AMM 33-51-06-2-1 & FOUND SATISFACTORY. ACFT OK TO CONTINUE SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 71,024 hrs · 24,046 cycles

PRESSURIZATION SYSTEM 2 WOULD NOT MAINTAIN CABIN ALTITUDE. CABIN ALTITUDE CONTINUOSLY ROSE, DESCENDED TO FL 100. FOUND NR 2 CABIN PRESSURE CONTROLLER AT FAULT. REPLACED CONTROLLER IAW AMM 21-31-02-4.

Part: CYLINDER — LEAKING (EMERGENCY SLIDE) · airframe 70,679 hrs · 23,781 cycles

AFTER BLOCK IN, ARRIVAL PERSONNEL OPENED DOOR WHILE SLIDE WAS ARMED FROM OUTSIDE. SLIDE BOTTLE BLED OUT AND GIRT BAR IS SLIGHTLY AJAR. REMOVED RED EMERGENCY POWER SPRING CYLINDER IAW MM 52-11-33-4. ACFT OK TO CONTINUE.

Part: VALVE — MALFUNCTIONED (MLG) · airframe 70,176 hrs · 23,347 cycles

AFTER EXTENDING THE LANDING GEAR FOR LANDING. LANDING GEAR "DOORS" LIGHT DID NOT EXTEND. R & R DOWNLOCK VALVE PER AMM 32-32-07-4. MAIN GEAR DOWNLOCK, OPERATED DOOR SEQUENCE PERFORMED CHECK OF THE UPLOCK OPERATE SEQUENCE VALVE PER SUBTASK 32-32-09-864-014.TEST SATISFACTORY AND PERFORMED CHECK OF SAFETY VALVE PER AMM 32-35-05-864-018. ALL TEST SATISFACORY NO HYD LEAK DETECTED. ACFT OK FOR SERVICE.

Part: APU — SMOKE · airframe 69,895 hrs · 23,136 cycles

PRIOR TO START CHECKLIST, ACRID SMOKE ENTERED COCKPIT. INTITALLY SMELLED SMOKE, THEN VISIBLE. APU RUNNING, BOTH LT & RT PACKS ON. TURNED OFF PACKS & OPENED WINDOWS TO VENT COCKPIT. SMOKE STOPPED AFTER PACKS TURNED OFF. PRIOR TO DECLARING SMOKE IN COCKPIT, MX WITNESSED APU EXHAUST BACKFIRE WITH SMOKE. SMOKE FOUND TO BE EXITING THROUGH THE AIR CONDITIONING VENTS. INSPECTED AVIONICS COMPARTMENTS TO VERIFY NO ELECTRICAL BURNING ISSUES. NONE FOUND WITH APU SHUTDOWN, VISUALLY INSPECTED AROUND THE COCKPIT INSTRUMENT PANELS FOR EVIDENCE OF MORE SMOKE WITH NONE FOUND. SECOND SMOKE INSP CONDUCTED. RELEASED FOR SERVICE.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 69,359 hrs · 22,821 cycles

RT CREASE BEAM CORRODED AROUND ANCHOR NUT HOLES APPROX BS 1020-1040. CORROSION FOUND TO BE OUT OF LIMITS. REPLACEMENT FABRICATED IAW DWG 144N5140 AND INSTALLED IAW SRM 51-40-02.

Part: FUEL CELL — CORRODED (BS 920) · corrosion level 2 · airframe 69,359 hrs · 22,821 cycles

CENTER TANK UPPER SKIN UPPER SURFACE FOUND CORRODED AT BS 920 , AT AREA JUST UNDER RT STUB BEAM CORROSION. REMOVED AND ASSESSED IAW SRM 57-10-01 MAX BLEND MATERIAL REMOVED 0.013 " MAX LIMIT 0.028" BLEND FOUND TO BE WITHIN LIMITS. DUE TO ACCUMALATIVE BLENDS IN AREA IN VARIOUS LOCATIONS IN CLOSE PROXIMITY IT IS INCORPORATED WITHIN EA F 5710-154331 BLENDED AND TREATED.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 69,359 hrs · 22,821 cycles

LEFT CREASE BEAM INBD CHORD CORROSION FOUND AROUND ANCHOR NUT HOLES APPROX BS 1020-1040, CORROSION FOUND TO BE OUT OF LIMITS. REPLACEMENT CHORD FABRICATED IAW DWG 144N5140 AND INSTALLED IAW SRM 51-40-02.

Part: SKIN — CORRODED (WING) · airframe 69,359 hrs · 22,821 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING SKIN BENEATH STUB BEAM AT BS940, LBL65. REPAIR CARRIED OUT IAW EA F-5710-154331.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 69,359 hrs · 22,821 cycles

LIGHTNING STRIKE AT STA 1160-1180, ST7, REPAIR CARRIED OUT IAW EA F.5300-154337.

Part: SKIN — DAMAGED (ZONE 200) · airframe 69,359 hrs · 22,821 cycles

LIGHTENING STRIKE ON FUSELAGE SKIN, BS 1240 S7-8R. REPAIR CARRIED OUT TO SKIN IAW EA F-5300-154337.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

CORROSION FOUND BENEATH STUB BEAM ON CENTER TANK SKIN AT BS 940 LT AND RT SIDE OF CABIN CORRODED AREAS REPAIRED IAW EA F-5710-154331.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

CTR TANK UPPER SKIN UPPER SURFACE ATTACHED REPAIR PATCH AT BS 960-980 LT STUB BEAM AREA FOUND DISBONDED. CORRODED AREA BLENDED AND REPAIRED IAW EA F-5710-154339.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

WING CENTER TANK, UPPER SURFACE BS 940 STUB BEAM CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-51. NEW STUB BEAM FABRICATED IAW DWG 144N1019 AND FITTED.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 69,359 hrs · 22,821 cycles

EXFOLIATION CORROSION FOUND ON UPPER WING SKIN BENEATH STUB BEAM AT RBL 65 REPAIR CARRIED OUT IAW EA F-5710-154331.

Part: SKIN — DAMAGED (BS 1520) · airframe 69,359 hrs · 22,821 cycles

SKIN HAS A LIGHTENING STRIKE AT BS 1520 S8R. REPAIRED IAW EA F-5300-154337.

Part: SKIN — DAMAGED (BS 1360) · airframe 69,359 hrs · 22,821 cycles

FUSELAGE SKIN HAS A LIGHTNING STRIKE AT BS 1360 S7-8R. REPAIR CARRIED OUT IAW EA F-5300-154337.

Part: BEARING — CORRODED (L1 DOOR) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

L1 DOOR EMERGENCY POWER TRIGGER MECHANISM CABLE ACTUATION BELLCRANK SEIZED DOOR TRIGGER QUADRANT BEARINGS FOUND SEIZED RERIG OF DOOR CARRIED OUT POST BEARING CHANGE IAW 52-1136.

Part: SKIN — DAMAGED (ZONE 200) · airframe 69,359 hrs · 22,821 cycles

LIGHTNING STRIKE AT STA 1460 ST 8-9R LIGHTNING STRIKE REPAIR CARRIED OUT IAW EA F-5360-154332.

Part: FUEL CELL — CORRODED (CENTER TANK) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

CENTER TANK UPPER SKIN SURFACE ATTACHED REPAIR PATCH AT BS 980-1000 RT STUB BEAM AREA FOUND DISBONDED. CORROSION REMOVED FROM AFFECTED AREA REPAIR CARRIED OUT IAW EA F-5710-154339.

Part: BEARING — CORRODED (ZONE 800) · airframe 69,359 hrs · 22,821 cycles

L1 DOOR EMERGENCY POWER TRIGGER MECHANISM CABLE ACTUATOR BELLCRANK SEIZED. TWO OFF BEARINGS IN CABLE ACTUATING BELLCRANK REPLACED.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 3 · airframe 69,359 hrs · 22,821 cycles

EXFOLIATED CORROSION FOUND BENEATH STUB BEAM AT BS940 LT SIDE OF CABIN AT CENTER TANK SKIN. REWORK CARRIED OUT ON NON ROUTINE N00425 AND EA F-5710-154331.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 68,995 hrs · 22,466 cycles

DELAMINATION FOUND ON SLAT1 OTBD UPR T/E FROM OTBD END TO 250MM AND 40MM FROM T/E DIM 250MMX40MM, 15SQIN. REPAIRED IAW SRM 57-70-10CH REPAIR #4, 57-43-02 FIG 1 AND FIG 201REPAIR DOUBLER INSTALLED,

Part: TRANSMITTER — MALFUNCTIONED (EPR) · airframe 68,606 hrs · 22,113 cycles

REJECTED TAKEOFF AT 100KTS. AT 80KT POWER WAS SET TO STANDARD AT APPROX 1.57 EPR. AFTER 80 KTS NR 1 ENG PWR DECREASED ABOUT 10 PERCENT. ADVANCED NR1 THRUST LEVER AND NR1 EPR WOULD NOT RECOVERED. CHECKED EJECTOR FILTER AND FOUND CLEAN. PURGED EPR LINE AND R & R EPR TRANSMITTER REF MM 77-11-01-4. PERFORMED MAX POWER ASSURANCE CHECK IAW AND ALL OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,410 hrs · 21,988 cycles

C-1 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS ROUTE OUT GREATER THAN .001". CUT OUT DAMAGE DIMS 1 1/4" X 1/4" IAW SRM 52-30-1, FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 5 7/8" X 5 3/4" IAW SRM 52-30-1 AND INSTALLED REPAIR DOUBLER IAW SRM 52-30-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,410 hrs · 21,988 cycles

C-2 DOOR LOWER FWD CORNER EXTERNAL SKIN HAS TRIM OUT GREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6.7500" X 6.5" IAW SRM 52-30-1, FIG 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER FWD CORNER EXTERNAL SKIN IAW SRM 52-30-1, FIG 201.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,410 hrs · 21,988 cycles

C-2 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS TRIM OUT FGREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6 3/4" X 6 1/4" IAW SRM 52-30-1 FIGURE 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER AFT CORNER EXTERNAL SKIN IAW SRM 52-30-1 FIGURE 201.

Part: SWITCH — OUT OF POSITION (AIRSPEED ZIPPER) · airframe 67,637 hrs · 21,566 cycles

AFTER TAKEOFF AND PASSING 10,000 FT, AIRSPEED ZIPPER DID NOT INCREASE TO EXPECTED CLIMB AIRSPEED, MAX AIRSPEED 268 KTS AT FL 360, ZIPPER RESTRICTED AIRSPEED TO 238 KIAS. DURING DESCENT, PASSING FL300 ZIPPER INCREASED TO 268. DURING APPROACH ZIPPER INDICATIONS WERE NORMAL WITH FLAP EXTENSIONS. FOUND VMO/MMO SWITCH ON THE P65 PNL TO BE IN THE ALTN POSITION. RETURNED TO NORMAL AND INSTALLED NEW SHEAR WIRE. PERFORMED OPS CHECK IAW MM 34-12-00-5. OPS GOOD.

Part: SKIN — CHAFED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

RT WING O/B MAIN FLAP O/B L/E CORNER HAS 4 INCH CHAFF MARK (FROM LOWER WING PANEL). DEFECT REPAIRED IAW EA F-5750-120571. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BULKHEAD — CRACKED (ZONE 400) · airframe 66,518 hrs · 21,044 cycles

NR 1 STRUT MID BULKHEAD LOWER FLANGES RT FWD FITTING BOLT HOLE CRACKED. REF CARD 5450-7-5005 P1 CARD 15 OF 33. NR 1 NACELLE STRUT MID-BULKHEAD LOWER FLANGE RT FWD FITTING BOLT HOLE REPAIRED IAW FEDEX EO F-5450-7-5005 PT 5. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

RT WING TOP SURFACE REAR SPAR AREA APPROX WS 230-345, 3 SPOTS OF CORROSION ON TOP OF WING. REPAIR CARRIED OUT BY BLENDING OUT IAW B757-200 SRM 57-20-01 TABLE 1 AND EA F- 5730-124309. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LT FUSELAGE PANEL 197EL CENTER SUPPORT FRAME CHANNEL FACE HAS CORROSION. CORROSION FOUND EXCEEDED ALLOWABLE SRM LIMITS. CHANNEL REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LT AFT MAIN TANK BOOST PUMP HEAVY CORROSION ON SPAR. CORROSION REMOVED AND AREA TREATED IAW FEDEX EA NR F-5710-124306. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

MAIN CARGO FLOORBEAM AT BS 377, LBL 22 HAS CORROSION. MINOR CORROSION ON FLOORBEAM REMOVED, TREATED, AND IS WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-51 REV 93, FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STRAP — CORRODED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

AFT CARGO CORROSION ON SKIN STRAP AT BS 1400, RBL 20 BETWEEN S27R AND S28R. MINOR CORROSION ON STRAP REMOVED AND AREA TREATED IAW SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

MAIN CARGO FLOORBEAM HAS CORROSION AT BS 345, LBL 21 TO 34. MINOR CORROSION REMOVED, TREATED AND IS WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-51 REV. 93, FIG. 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DENTED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

TWO DENTS FOUND ON FUSELAGE SKIN AT RT STA 395, WL208.10. REPAIR CARRIED OUT IAW FEDEX EA NR F-5330-111008. REPEAT INSPECTION REQUIRED WHEN AIRFRAME ACCUMULATES 37,500 FC AND THEREAFTER AT 12,000 FC INTERVAL. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SILL — CORRODED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

L1 DOOR SILL FACE HAS LIGHT CORROSION IN SEVERAL AREAS. MINOR CORROSION BLENDED OUT AND AREA TREATED, FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01 REV 93, DETAIL II FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SILL — CORRODED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

R2 DOOR LOWER SILL HAS SEVERAL SPOTS OF SURFACE CORROSION. MINOR SURFACE CORROSION REMOVED IAW SRM 51-10-02 REV 93 AND FOUND WITHIN ALLOWABLE LIMITS. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

CORROSION ON CABIN FLOORBEAM AT BS 324, LBL 20. MINOR SURFACE CORROSION BLENDED OUT AND SURFACE TREATED, FOUND WITHIN ALLOWABLE LIMIT IAW B757-200 SRM 53-00-51 REV. 93 DETAIL III FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

CORROSION ON STRINGER 6R AT BS 686 IN MAIN CABIN. CORROSION FOUND BEYOND SRM LIMITS. REPAIR CARRIED OUT IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

CABIN FLOORBEAM AT BS 350, LBL8, HAS CORROSION. MINOR SURFACE CORROSION BLENDED OUT AND SURFACE TREATED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW B757-200, SRM 53-00-51 REV 93 DETAIL III, FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

MAIN CABIN RT FLOOR SUPPORT ANGLE FROM BS 630 TO BS 640, RBL 64 HAS CORROSION. CORROSION FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B757-200 SRM 51-70-12 DETAIL VI. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LT FUSELAGE BS 780-799, S-30 HAS CORROSION ON FWD SUPPORT FRAME AT SEVERAL PLACES. CORROSION FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-02 REV. 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

AT BS 1630, 63LBL, FLOOR SUPPORT ANGLE HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REPAIR CARRIED OUT IAW B757-200 SRM 51-70-12 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

LT LWR FUSELAGE FROM BS 1460 TO 1480 BETWEEN STR 27L AND 28L HAS EXISTING LIGHTNING STRIKE REPAIR. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT 1. FOUND ACCOMPLISHED IAW B757-200 REM 53-00-01 FIG 201, REPAIR 6 SECT 1, BASED ON EXTERNAL VISUAL EVALUATION OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

LT LWR FUSELAGE FROM BS 1480 TO BS 1500, STR 27L AND 28L HAS EXISTING LIGHTNING STRIKE REPAIR. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 ATTACHMENT B, FOUND ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 6 SECT 1, BASED ON EXTERNAL VISUAL EVALUATION OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

MINOR CORROSION FOUND ON WING LOWER INTERNAL SURFACE ACCESS 531AB WHILE CARRYING OUT TREATMENT. CORROSION REMOVED IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LOWER FUSELAGE LEFT MID SUPPORT FRAME FOR FAIRING 197LL HAS SURFACE CORROSION. REPAIR CARRIED OUT ON WING-TO-BODY FUSELAGE STRUCTURE LOWER CHORD IAW EA NR F-5320-124303. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

BS 1640 RBL 20 TO LBL 20 BULKHEAD FLOOR SUPPORT ANGLE HAS CORROSION. ANGLE ASSY AT BS 1640 BULKHEAD IS REPLACED UNDER EO F-2550-7-5001 PT 1: EQUIPMENT/FURNISHINGS, CARGO COMPARTMENT/LOADING SYSTEMS. REPLACE BS 1640 BULKHEAD, AFT CARGO COMPARTMENT SB 757-25-0157 R1. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

AT BS 650 RBL 8, CORROSION ON FLOOR SUPPORT BEAM. CORROSION FOUND EXCEEDED SRM LIMITS. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FAIRING — CRACKED (ZONE 400) · airframe 66,518 hrs · 21,044 cycles

NR 2 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT HAS ABOUT 1/3 INCH LONG CRACK NEAR PPSTA 276. CRACKED SKIN REMOVED AND REPLACED IAW B757-200 SSRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT AT BS 750 RBL 8 HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FAIRING — CRACKED (ZONE 400) · airframe 66,518 hrs · 21,044 cycles

NR 1 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT FOUND WITH A CRACK ABOUT 1/2 INCHES LONG. CRACKED SKIN REMOVED AND REPLACED IAW B757-200 SRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (BS 810) · airframe 66,518 hrs · 21,044 cycles

LIGHTNING STRIKE AT BS 810, S7L. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW SRM 53-00-01 REV 93, FIG 201 REPAIR 6, SECT II PARA 3. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (BS 860) · airframe 66,518 hrs · 21,044 cycles

AT BS 860, STR 7L. DAMAGE REPAIR CARRIED OUT IAW SRM 53-00-01 REV 93, FIG 201, REPAIR 6, SECT I PARA 3. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541LB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL PANEL ACCESS CUTOUT 541JB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 543BB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV, 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541EB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541GB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL PANEL ACCESS CUTOUT 542CB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541FB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 542AB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541HB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

SURGE TANK ACCESS PANEL CUTOUT 643BB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01, REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541KB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL PANEL ACCESS CUTOUT 542DB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93. REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541MB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541DB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 543AB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 653 TO BS 700, RBL 10, FOUND WITH CORROSION. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN SRM. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 653 TO BS 700, LBL 8, HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REMOVED AND REPLACED STRINGER IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 653 TO BS 700, RBL 16, HAS CORROSION. CORROSION FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (BS 560-645) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

TRANSITION PANEL FROM BS 560 TO BS 645.75 HAS CORROSION. CORROSION FOUND BEYOND ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. PANEL REPLACED IAW B757-200 51-10-02 AND 51-40-02. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

RIGHT TRANSITION PANEL FROM BS 640 TO BS 765 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE SRM LIMITS. PANEL REMOVED AND REPLACED IAW B757-200 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

RIGHT TRANSITION PANEL FROM BS 760 TO BS 845 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE SRM LIMITS. PANEL REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LEFT SIDE TRANSITION PANEL FROM BS 1200 TO BS 1310 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE LIMITS IN SRM. PANEL REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

LIGHTNING STRIKE MARK ON FUSELAGE AT BS 1310 BETWEEN S-18R AND S-19R. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW B757-200 SRM 53-00-01 REV 93, SECT 1, PARA 3 REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (RT WING) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641EB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 642DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641HB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 642CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641GB HAS CORROSION AND BARE METAL. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641MB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641FB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641LB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641JB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS PANEL CUTOUT 641KB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

LIGHTNING STRIKE MARK ON FUSELAGE AT BS 1294, 2 INCHES BELOW S-18R. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW B757-200 SRM 53-00-01 REV 93, SECT 1 PARA 3 REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 642AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 641AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 600) · airframe 66,518 hrs · 21,044 cycles

FUEL TANK ACCESS CUTOUT 642BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,518 hrs · 21,044 cycles

FUEL ACCESS PANEL CUTOUT 541CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

MAIN DECK FLOORBEAM AT BS 365, RBL 62 HAS AN UNFILLED HOLE. DAMAGED PART OF BEAM REPAIRED IAW B757-200 SRM 53-00-51 REV 93 DETAIL 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LOWER FUSELAGE KEEL BEAM AREA, SURFACE CORROSION ON CENTER SUPPORT FRAME AT BS 900. CORROSION FOUND EXCEED ALLOWABLE DAMAGE LIMITS IN B757-200 SRM 53-00-71. CHORD REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORTS FROM BS 1340 TO BS 1445, RBL 3, 6, 11, 16 HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED AND FOUND EXCEED LIMITS IN B757-200 SRM 51-10-02. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 1340 TO BS 1445, LBL 3, 6, 11, 16 HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED. FOUND EXCEEDED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. REMOVED AND REPLACED STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 1200 TO BS 1340, RBL 3, 6, 11, AND 16 HAS CORROSION AROUND NUTPLATE HOLES IN SEVERAL LOCATIONS. CORROSION FOUND EXCEED DAMAGE LIMITS IN B757-200 SRM 53-00-53 FIG 101. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORT FROM BS 1445 TO BS 1640, RBL 3, 6, 11, HAS CORROSION AROUND NUTPLATE HOLES. CORROSION FOUND EXCEEDED DAMAGE LIMITS IN B757 SRM 51-10-02. REMOVED AND REPLACED STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

CORROSION FOUND ON FLOOR STRINGER FROM BS 1445 TO BS 1510, RBL16.21. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200SRM 51-10-02. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

FLOOR SUPPORTS FROM BS 1445 TO BS 1640, LBL 3, 6, 11, HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. STRINGER REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

AFT CARGO DOOR LOWER SILL FROM BS 1380 TO BS 1440 HAS CORROSION IN NUMEROUS AREAS. CORROSION FOUND EXCEED B757-200 SRM 51-10-02 ALLOWABLE LIMITS. REMOVED AND REPLACED LOWER SILL PANEL IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LT FUSELAGE FWD OF BS900 SUPPORT ANGLE HAS SURFACE CORROSION. CHORD REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (BS 1000) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LWR FUSELAGE KEEL BEAM AREA, CORROSION ON CENTER SUPPORT FRAME AT BS1000. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 53-0071 FIG 101 DETAIL VII. REMOVED AND REPLACED TEE CHORD IAW B757-200 SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LWR FUSELAGE KEEL BEAM AREA AT BS 1040 RT SIDE, SUPPORT FRAME HAS SURFACE CORROSION. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757 SRM 51-10-02. REMOVED AND REPLACED TEE SUPPORT IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

BS 1560, STR 22R TO 26R SIDEWALL SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

SIDEWALL SUPPORT ANGLE FROM BS 1600 TO 1640, STR 23R HAS CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE ASSY IAW B757-200 SRM 51-10-02 AND 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SUPPORT — CORRODED (BS 960) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

LWR FUSELAGE KEEL BEAM AREA, CORROSION ON CENTER SUPPORT FRAME AT BS 960. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 53-00-71. REMOVED AND REPLACED TEE SUPPORT IAW B757-200 SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

SIDE WALL SUPPORT ANGLE AT BS 1300, STR 27R TO 30R FOUND CORRODED. CORROSION FOUND EXCEED SRM 53-00-71 LIMITS. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE IAW SRM 51-10-02 AND SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

LIGHTNING STRIKE REPAIR FOUND AT BS 550 BETWEEN S-26L AND S-27L TO EVALUATE REPAIR. EXISTING LIGHTNING STRIKE REPAIR EVALUATED AS PER EO F-5100-7-5001 PT 1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 201, REPAIR 6 SECTION 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

SURFACE CORROSION FOUND ON LT FUSELAGE WING-TO-BODY FAIRING ATTACHMENT HOLES AT BS 820. CORROSION FOUND EXCEED LIMITS IN SRM 53-00-71 FIG 101 DETAIL VIII. REMOVED AND REPLACED LOWER TEE FITTING IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

CORROSION FOUND ON FLOOR SUPPORT AT BS 750, LBL4. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. REMOVED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

CORROSION FOUND ON FLOOR SUPPORT AT BS750, LBL 8. CORROSION FOUND EXCEED ALLOWABLE DAMAGE LIMITS IN SRM 51-10-02. REMOVED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,518 hrs · 21,044 cycles

CORROSION FOUND ON FLOOR SUPPORT AT BS 748, RBL 12. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. REMOVED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

EXISTING PATCH REPAIR FOUND ON AFT PRESSURE PANEL AT BS 1720, LBL24 TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUNT TO BE ACCOMPLISHED IAW B757-200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

PATCH REPAIR FOUND ON PRESSURE PANEL AT BS1720, RBL16 TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757 -200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 66,518 hrs · 21,044 cycles

PATCH REPAIR FOUND ON PRESSURE PANEL AT BS1720, RBL4, TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757-200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 66,518 hrs · 21,044 cycles

UNRECORDED EXISTING REPAIR FOUND ON FLOORBEAM AT BS 1640, BETWEEN LBL 4 AND RBL 4 TO EVALUATE EXISTING REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757-200 SRM 53-00-51 FIG 201, REPAIR 3, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: NONE — NONE (IAW SRM) · airframe 66,518 hrs · 21,044 cycles

UNRECORDED PREVIOUS REPAIR FOUND ON RT APU COWLING LOCATED AT MIDDLE HINGE. REPAIR TO BE EVALUATED. EXISTING REPAIR FOUND TO BE IAW B757-200 SRM 52-40-01 FIG 201, REPAIR 5, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. NOT AN SDR.

Part: NONE — NONE (IAW SRM) · airframe 66,518 hrs · 21,044 cycles

PATCH REPAIR ON OUTBOARD LEADING EDGE OF LH WING OUTBOARD FLAP TO BE EVALUATED. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-53-01 FIG.202. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. NOT AN SDR

Part: SKIN — DENTED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1416 TO BS 1446, BETWEEN S-26R AND S-28R (REAR LOWER CORNER OF AFT CARGO DOOR CUTOUT), TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT 1 ATTACHMENT B, AND FOUND PREVIOUSLY ACCOMPLISHED IAW BOEING TELEX NO: GUE-MAN-03-00089H WITH FAA FORM 8110-3. LFEC INSPECTION REQUIRED AT EVERY 3,000 FC INTERVAL AFTER AIRFRAME ACCUMULATED 50,000 FC. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE AT BS365, S-21R TO BE EVALUATED. EXISTING REPAIR FOUND ACCOMPLISHED IAW SRM 53-00-01 FIG 203, BASED ON EXTERNAL VISUAL EVALUATION OF THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON NR 2 RT DOOR UPPER HINGE CUT-OUT TO BE EVALUATED. REPAIR CARRIED OUT AS PER EA F-5240-118832. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.B

Part: NONE — NONE (IAW SRM) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON AFT CARGO DOOR LOWER CENTER EDGE BEAM TO BE EVALUATED. EXISTING REPAIR FOUND PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 52-30-01 FIG 205. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DENTED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1520 TO BS 1540, BETWEEN S-28L AND S-29L TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-1500-7-5001 PT1 ATTACHMENT B, AND FOUND TO HAVE BEEN ACCOMPLISHED IAW B757 SRM 53-00-01 FIG 204. EXISTING REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NO DAMAGE) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1701 TO BS 1708, BETWEEN S-17L AND S-19L TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED BY ENGINEERING LIMITED REPAIR NO: MON/757/53-252/REP/502 ISSUE B. REPAIR RE-INSPECTED AS PER FEDEX EA: F-5310-120564 AND EA F-5310-120565. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: NONE — NONE (IAW SRM) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE BS 1717, BETWEEN S-20L AND S-21L, TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT.1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED IAW MESSAGE 1-730176994-3, WITH FAA FORM 8110-3. SUPPLEMENTAL INSPECTION REQUIRED NOT LATER THAN 08 JANUARY 2009. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1701 TO BS 1720, BETWEEN S-14L AND S-17L TO BE EVALUATED. EXISTING REPAIR FOUND PREVIOUSLY ACCOMPLISHED IAW BOEING TELEX NR GUE-MAN-03-00062H, WITH FAA FORM 8110-3. LFEC REPEAT INSPECTION AT EVERY 3,000 FC INTERVAL AFTER AIRFRAME ACCUMULATES 31,000FC. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.

Part: SKIN — DENTED (ZONE 100) · airframe 66,518 hrs · 21,044 cycles

EXTERNAL SMALL HOLE FLUSH REPAIR AT FUSELAGE BS740, S-18L, TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 ATTACHMENT B AND FOUND TO BE PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 208. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.