N928FD

Part: GIRT BAR — DAMAGED (ZONE 800) · airframe 101,504 hrs · 33,907 cycles

L1 DOOR WILL NOT OPEN. TROUBLESHOT L1 DOOR AND DISCOVERED FWD END OF GIRT BAR JAMMED IN ARMING SLIDER. REMOVED AND REPLACED L1 DOOR GIRT BAR REMOVED IAW AMM 25-66-10-2 AND PERFORMED L1 DOOR ADJUSTMENT TESTS PER AMM 52-11-25-5. L1 DOOR OPS AND FUNCTIONS NORMAL. REMOVED PLACARD.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 101,155 hrs · 33,640 cycles

FLOOR PANEL #252MWF HAS DAMAGE AND MISSING INSERTS, R/H AFT O/B MAIN CABIN FLOOR PANEL. FABRICATED FLOOR PANEL #252MWF ON VTMAE TRAVELER #T25/1800902 IAW STMAE DWG. #11864182 REV. D, MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 101,155 hrs · 33,640 cycles

FLOOR PANEL #251MXF AFT MAIN CABIN L/H O/B HAS DAMAGE/MISSING INSERTS. FABRICATED FLOOR PANEL #251MXF ON VTMAE TRAVELER #T25/1800901 IAW STMAE DWG. #11864182 REV. D, MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 101,155 hrs · 33,640 cycles

SEAT TRACK AT FS 980 BL 0 HAS DAMAGE. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 879 TO 1065 BL 0 IAW SRM 51-40-02 FROM MATERIAL BAC 1520-2473 BATCH # 0002425804 IAW SRM 53-40-52-01 FIGURE 1 DETAIL II, MAJOR REPAIR.

Part: GUST LOCK — FAILED (ZONE 800) · airframe 101,116 hrs · 33,609 cycles

R1 DOOR GUST LOCK INOP. R&R BROKEN GUST LOCK ON R1 DOOR. OPS CHK GOOD. OK FOR SVC.

Part: FLAP SYSTEM — MALFUNCTIONED (LE FLAPS) · airframe 101,114 hrs · 33,608 cycles

TE FLAP DISAGREE, EMERGENCY DECLARED. ON INITIAL TROUBLESHOOTING NO EICAS MSG NOTED FOR TE FLAP DISAGREE. PUT FLAPS BACK TO NORMAL CONFIG FROM ALT MODE. BITE CHECKED ALL 3 FSEU S AND NO FAULTS NOTED. FLAP SELECTOR LEVER CLEANED AND LUBED AS PRECAUTION. PLACED FLAPS TO 30 DEGREES. ALL THE WAY DOWN TO LAST DETENT WITH NO ISSUES. ALL FLAP SURFACES MOVED FREELY AND IN SEQUENCE. WITH FLAPS DOWN ALL THE WAY, CHECKED ALL 8 FLAP TRANSMISSION UNITS FOR A OVERLOAD INDICATOR TRIPPING AND FOUND NOT TRIPPED. ALL 8 UNITS HAD FLUIDE IN IT TOO. JACK SCREWS WERE SMOOTH TO THE TOUCH AND FREE FROM DIRT OR DEBRIS. CYCLED FLAPS MULTIPLE TIMES AND UNABLE TO DUPLICATE THE FAULT. NO HISTORY FOR PASS 180 DAYS. THEREFORE, TE FLAPS OPS CHECK GOOD. A/C RETURN TO SERVICE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 100,944 hrs · 33,491 cycles

ON SERVICE CHECK FOUND R1 DOOR EMERGENCY RESEVOIR BELOW MINIMUM REQUIRED PRESSURE. AMM: 52-11-30-4 REMOVED AND REPLACED RI DOOR ASSIST BOTTLE PER ABOVE B757 REF.

Part: FERRULE — DAMAGED (EMERGENCY LIGHT) · airframe 100,749 hrs · 33,353 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. AMM: 33-51-06-2-1 RELAMPED, NO HELP. FOUND LIGHT WOULD INTERMITTENTLY COME ON WHEN MANIPULATING LIGHT ASSY. REMOVED BULB AND FOUND LAMP BASE WORN AND PITTED. NEEDS NEW BASE, LIGHT ASSY IS REMOVED AND IN MX OFFICE. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK GOOD A/C OK FOR SERVICE.

Part: ENGINE — INOPERATIVE (NR 1) · airframe 100,501 hrs · 33,196 cycles

PDIS 928 73-22 1096 25JAN24 MEM OPEN U AT CRUISE, FL360, #1 ENG EPR DID NOT INDICATE PROPERLY. THE WHITE EPR NEEDLE WAS FULL POWER ABOVE THE DIAL, THE POWER STRIP WAS ALSO WELL ABOVE THE MAX PORTION, THE N1 WAS SLOWLY DEGRADING AND WE BEGAN TO LOOSE AIRSPEED. THE SEI REFLECTED THE ABNORMALITY. WE DECLARED AN EMERGENCY AND DIVERTED TO KMEM. THE DESCENT, APPROACH AND LANDING WERE NORMAL. EMERGENCY WAS CANCELLED BY THE CREW AFTER LANDING. ***EMERGENCY DECLARED***

Part: CONTROL PANEL — FAILED (EMERGENCY LIGHTS) · airframe 99,768 hrs · 32,680 cycles

OVERHEAD COCKPIT EMERGENCY LIGHTS PANEL WON'T TEST IAW AMM 33-51-08-4. REMOVED AND REPLACED P5 EMEGENCY LIGHTS PANEL IAW AMM 33-51-08-4. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 98,933 hrs · 32,036 cycles

TRAILING EDGE FLAP DISAGREE. HANDLE AT 20. INDICATOR SAID BOTH FLAPS AT 15. RAN QRH. RECONFIGURED FLAPS FROM ALT TO REGULAR AND RAISED FLAPS. OPERATED FLAPS THROUGH ALL DETENTS FOR SEVERAL CYCLES, REF MM 27-51-00-5. NO FAULTS NOTED. PERFORMED BITE CK OF ALL THREE FSEU'S, REF FIM 27-51 FT 805, NO CURRENT FAULTS PRESENT. REF FIM 27-51 FT 808, CHECKED ALL TE FLAP TRANSMISSIONS FOR POPPED OVER-TORQUE INDICATORS AND PROPER SERVICING, ALL CHECKED NORMAL. RAN FLAPS THROUGH ALL DETENTS FOR SEVERAL ADDITIONAL CYCLES, NO FUTHER FAULTS. CHECKED 90 DAY HISTORY, NONE FOUND. AC OK FOR SERVICE.

Part: FAIRING — CRACKED (NR 2 NACELLE) · airframe 98,588 hrs · 31,776 cycles

#2 ENG PYLON O/B LOWER FLEXABLE FAIRING CLOSEOUT PANEL IS CRACKED ABOVE EXHAUST NOZZLE REMOVED AND REPLACED PANEL PER DWG # 311N5137

Part: STOP FITTING — CRACKED (R2 DOOR) · airframe 98,588 hrs · 31,776 cycles

R2 DOOR, 3RD FROM BOTTOM DOOR STOP IS CRACKED REMOVED AND REPLACED R-2 DOOR PER FEDEX B757 AMM 52-11-01-4

Part: WEB — DENTED (BS 500-520) · airframe 98,588 hrs · 31,776 cycles

MCD FWD PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 500 AND 520. REMOVED, FABRICATED AND REPLACED WEB AS REQ IAW BOEING DWG 65-49309 REV "D" AND B757 SRM 51- 40- 02-0G.

Part: WEB — DENTED (BS 580-600) · airframe 98,588 hrs · 31,776 cycles

MCD AFT PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 580 AND 600 REMOVED, FABRICATED AND REPLACED WEB AS REQUIRED IAW BOEING DWG 65-49309 REV "D" AND B757 SRM 51- 40-02-0G

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 98,588 hrs · 31,776 cycles

LMLG WHEEL WELL FWD EDGE WING TO BODY PANEL ATTACH CLIP IS CRACKED 32" OUTBOARD OF KEEL BEAM. REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP PER BAC DWG 149N7550

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 97,637 hrs · 31,177 cycles

UPON DESCENT INTO DESTINATION APPROXMATELY FL 180 IN IMC/RAIN RT ENG FIRE WARNING AND LIGHT CAME ON. RAN PHASE ONES AND QRH FOR RT ENG FIRE. UPON RT ENGINE SHUTDOWN, FIRE LIGHT WENT OUT THEN CAME BACK ON SO FOLLOWED QRH AND FIRED THE FIRE BOTTLE. RED LIGHT AND WARNING THEN WENT OUT AND STAYED OUT. EMERGENCY LANDED, FIRE CREW, THEN MX, DECLARED NO OBSERVABLE FIRE COMPLETED RT ENGINE FIRE AND OVERHEAT DETECTION SYSTEM OPS CHECK REF B 757 AMM 26-11-00-5 CHECKED NORMAL AT THIS TIME. SEE WRI UPDATES FOR ADDTIONAL WORK PREFRORMED AND PARTS CHANGED SEE WRI 2620/8278 FOR #2 ENG FIRE BOTTLE CHANGE. CONF CALL WITH MOCC ALL CONCUR A/C OK FOR SERVICE.

Part: LANYARD — OUT OF POSITION (ENTRY DOOR) · airframe 97,112 hrs · 30,845 cycles

RT CABIN ENTRY DOOR WILL NOT ARM FOUND LANYARD CORD STUCK IN GIRT BAR, PROPERLY STOWED LANYARD CORD . DOOR ARM LIGHT OPS CHECKED NORMAL PER AMM 52-71-00-5

Part: BRACKET — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 96,815 hrs · 30,636 cycles

BS 1410, AFT CARGO DOOR, LOWER FRAME SUPPORT BRACKET HAS EXFOILIATING CORROSION, 1 INCH BY 1 INCH SIZE. BOTH SIDES OF BRACKET ARE CORRODED.

Part: SEAT TRACK — CORRODED (BS 1540) · corrosion level 2 · airframe 96,815 hrs · 30,636 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN STA. 1540 RBL 45.50 PERFORMED SEAT TRACK REPAIR AT RBL 45.50 BETWEEN BS 1500-1540 IAW B757 SRM 53-00-52- 2R FIG 201 REPAIR 1 OPTION1. REMOVED COR ON SEAT TRACK IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILATION FOUND OUT OF LIMITS IAW B757 SRM 53-00-52

Part: CREASE BEAM — CORRODED (BS 860-880) · corrosion level 2 · airframe 96,815 hrs · 30,636 cycles

MAIN CABIN CREASE BEAM STA. 860-880 RBL64.20 HAS CORROSION REMOVED CORR. ON CREASE BEAM STA 860-880 RBL 64.20 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS .020 FOUND OUT OF LLIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. REMOVED, FABRICATED AND INSTALLED NEW CREASE BEAM SECTION IAW B757 SRM 53-00 00-13-2R REP. 1 ALT 1

Part: TUBE — DAMAGED (EPR SYSTEM) · airframe 95,977 hrs · 30,078 cycles

PDIS 928 76-00 6718 24APR18 BNA OPEN U LOGPAGES:2252904 AT CRUISE NOTICED L EPR PEGGED. FUEL FLOW AT 1.5. LOTS OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICAS. L ENG DID NOT RESPOND TO THROTTLE MOVEMENT. PART 24APR18 11:37 MC1 U IDENTIFIED PARTS COLD CURING SILICONE (WT) MPN: SILC0SET152 CPN: 0201664 QTY: 1 PART 24APR18 11:38 MC1 U IDENTIFIED PARTS P1 PROBES MPN: 851JB CPN: 7311062 QTY: 1 P1 PROBE MPN: K7311062K2 CPN: 7311417 QTY: 1 PART 24APR18 11:38 MC1 U IDENTIFIED PARTS TUBE-P1 AIR-PROBE ASSY MPN: LJ35801 CPN: 7311158 QTY: 1 PART 24APR18 11:42 MC1 U ORDER PART MPN: LJ35801 CPN: 7311158 QTY: 1 MSN: 1912048 MPN: 851JB CPN: 7311062 QTY: 1 MSN: 1912049 MPN: K7311062K2 CPN: 7311417 QTY: 1 MSN: 1912050 MPN: SILC0SET152 CPN: 0201664 QTY: 1 MSN: 1912051 FOUND P1 TUBE JUST AFT OF PROBE DAMAGED. R&R'D TUBE.

Part: TUBE — DAMAGED (ENGINE) · airframe 95,977 hrs · 30,078 cycles

DURING CRUISE, NOTICED THE LT EPR PEGGED. FUEL FLOW AT 1.5. A LOT OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICAS. LT ENG DID NOT RESPOND TO THROTTLE MOVEMENT. FOUND THE P1 TUBE JUST AFT OF PROBE DAMAGED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 95,954 hrs · 30,061 cycles

MAIN CABIN STA 580 FLOORBEAM STUB FITTING HAS A CRACK ON AFT FLANGE AT LBL 45. COMPLIED WITH EA F-5310-T0339360 P1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 95,954 hrs · 30,061 cycles

MAIN CABIN SEAT TRACK LBL 45.5, BS 580 CROWN AREA DAMAGED. INSTALLED A NEW SECTION OF SEAT TRACK IAW DWG 143N5090, REV-, SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 51-20-01-0G, AMM 51-21-00-7, AND DWG 143N8750 REV-.

Part: TUBE — LEAKING (LT ENGINE) · airframe 95,801 hrs · 29,966 cycles

DURING CLIMB THROUGH FL 270, THE LEFT ENGINE INDICATED N1 OF 82% VS N1 95%, FOR THE RIGHT ENGINE. LEFT EGT WAS 120DEG. LOWER, N2 WAS 10% LOWER. RUDDER TRIM OF 4 RIGHT REQUIRED. LEVEL AT 270 ALL INDICATIONS THE SAME FOR BOTH ENGINES EPR 1.37, N1 75%, EGT 505, N2 75%. NORMAL OPERATION FROM LEVEL AT FL270 . WHILE INSPECTING P1 PROBE LINES, FOUND LINE IN NOSE COWL CRACKED IN HALF, R & R P1 PROBE LINE IAW AMM 72-00-00-2. PERFORMED EPR P1 SYSTEM TEST IAW AMM 77-11-00-5 . SYS CHECKED GOOD.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 95,364 hrs · 29,676 cycles

RT ENGINE FLAMED OUT ON ARRIVAL AT 15000 FT. AT BLOCK IN, THE RT ENG LP PUMP STATUS MESSAGE INDICATED. REMOVED AND REPLACED THE HIGH PRESSURE FUEL PUMP, ENGINE TRANSIENT PRESSURE UNIT, AND LOW PRESSURE FUEL PUMP IAW AMM 73-11-03-4-4, 73-11-01-4, AND 75-32-15-4. SYSTEMS OP CHECKED NORMAL IAW AMM 75-32-15-5 AND TESTS 1 AND 2 IAW JRH REF 7-5. ACFT OK TO CONTINUE.

Part: GOVERNOR — MALFUNCTIONED (RT ENGINE) · airframe 95,263 hrs · 29,604 cycles

RIGHT ENGINE FAILED AT APPROXIMATELY 7000' MSL DURING DESCENT. INITIALLY NOTED RIGHT GENERATOR OFF, THEN UTILITY BUSSES, AUTOTHROTTLES, AND AUTOPILOT. ENGINE WAS A SLOW SHUTDOWN. RIGHT OIL PRESSURE WAS ZERO. WINDMILLED RIGHT ENGINE FOR 7 - 8 MINUTES. NO VIBRATION OR NOISE WAS NOTED. LANDED UNEVENTFUL. REMOVED THE RT ENGINE FUEL DRAINS, TANK EJECTOR VALVE, FILTER AND INSPECTED. NO DEBRIS NOTED. CLEANED FILTER AND REINSTALLED IAW AMM 71-71-04-2. REMOVED THE RT ENGINE LP FILTER ELEMENT AND INSPECTED. NO DEBRIS NOTED. INSTALLED NEW FILTER ELEMENT IAW MM 73-11-10-4. TROUBLESHOT IAW FIM 71-05 FT 807. REMOVED HP FUEL PUMP VERIFIED SHAFT NOT SHEARED. VERIFIED VOLTAGES AT FFG CONNECTOR. IAW FIM BLOCK 24, REPLACED HP FUEL PUMP IAW MM 73-11-03-4 AND RT ENGINE FUEL FLOW GOVERNOR IAW MM 73-21-01-4. ALL OPS & LEAK CHECKED SATISFACTORY. ACFT OK FOR SERVICE.

Part: TERMINAL — LOOSE (CABIN) · airframe 95,152 hrs · 29,520 cycles

EMERGENCY LIGHTS FAIL TO TEST WITH SWITCH ABOVE L1 DOOR IN COURIER COMPT. FOUND TERMINAL END OF WIRE W3532-0036-20 LOOSE AT GROUND STUD GD1420-DC. TIGHTENED TERMINAL STUD AND VERIFIED GROUND AT SWITCH S10292. REF WDM 33-51-12 AND SWPM. A/C REQUIRES REINSTALLATION OF DOOR FRAME PANEL AND OPS CHECK OF EMERGENCY LIGHTING. REINSALLED PANEL ASSY 411N2331-113B THEN PUSHED IN C/B N35 AND N36 AND PERFORMED A SUCCESSFUL OPS . CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW AMM 33-51-00. A/C OK FOR SERVICE.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 95,139 hrs · 29,512 cycles

DURING REMOVAL OF INBOARD MAIN FLAP OUTBOARD FLAP FAIRING FWD INBOARD ATTACH BRACKET. FOUND THE SKIN MOUNT BOLT HOLES WORN AND ELONGATED. COMPLIED WITH EA 5750-TO332573 P1.

Part: BRACE — CRACKED (NR 1 PYLON) · airframe 95,139 hrs · 29,512 cycles

TWO CRACK INDICATIONS AT THE INSIDE HOLES ON AFT SIDE OF NR 1 PYLON DIAGONAL BRACE FITTING LOWER SURFACE IN ALUMINUM ONLY. COMPLIED WITH EA F-5450-T0332370 B P1.

Part: FITTING — CRACKED (BS 580 FLOORBEAM) · airframe 95,139 hrs · 29,512 cycles

MAIN CABIN FLOORBEAM BS 580, STUB BEAM FITTING AT LBL 44.5 HAS A CRACK IN UPPER RADIUS OF TOP FLANGE. REMOVED AND REPLACED THE STUB BEAM FITTING IAW DWG 657N4311, REV, AND SRM 51-40-02-0G.

Part: COVER — LOOSE (PAX DOOR SLIDE) · airframe 95,032 hrs · 29,418 cycles

CAN NOT ARM LEFT MAIN ENTRY DOOR SLIDE. FOUND LOWER SLIDE COVER LOOSE, REMOVED SLIDE COVER AND FOUND THE HOOK AND LOOP STRAPS LOOSE THAT STOW THE MATERAL TO THE GIRT BAR. TIGHTENED THE HOOK AND LOOP STRAPS AND CLEANED THE GIRT BAR MECHANISM AND SENSORS ON THE DOOR AND THE FLOOR FITTINGS, REINSTALLED SLIDE COVER IAW MM 25-66-01. OPS CHECKED IAW MM 25-66-11-2.

Part: CONTROL CABLE — OUT OF ADJUST (NLG STEERING) · airframe 94,966 hrs · 29,372 cycles

ON EXITING RUNWAY TILLER STUCK HARD AT 45' POSITION DURING 90' LT TURN. UPON GETTING BACK ON CENTER LINE, TILLER REQUIRED .5 TO 1 INSIDE RT TO REMAIN IN POSITSION. IF RELEASED, ACFT TURNED HARD LT. ACFT TURNED HARD LT OF TAXIWAY. PROBLEM DID NOT OCCUR ON TAXI OUT. INSPECTED AND ADJUSTED NOSE WHEEL STEERING A AND B (NWS) CABLES IAW AMM 32-51-00-5-3 .. INSPECTED AND ADJUSTED NOSE GEAR PISTON POSITION A AND B (NGPP) CABLES AND PERFORMED NOSE WHEEL STEERING SYSTEM ADJUSTMENT TEST IAW MM 32-51-00-5-3. TAXIED IAW JRH CH12. PERFORMED FULL RT AND FULL LT TURNS, TILLER MOVEMENT IS SMOOTH AND CENTERS. ACFT STAYS ON LINE WITHOUT TILLER CORRECTIONS. NO VIBRATIONS, NOTCHINESS OR CLUNKING DURING ENTIRE TAXI OPS.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 94,683 hrs · 29,152 cycles

DURING CLIMBOUT, RECEIVED LT HYD SYS LOW QUANTITY MESSAGE. SHORTLY, RECEIVED LT HYD SYS PRESSURE MESSAGE. COMPLIED WITH QRH EXTEND FLAPS ALTERNATELY AND ALTERNATELY EXTEND LANDING GEAR. FOUND LEFT MAIN GEAR DOWN LOCK ACTUATOR PRESSURE LINE LEAKING. REPLACED THE LINE IAW MM 32-32-04-4 AND SMP.

Part: LINE — OUT OF POSITION (OXYGEN MASK) · airframe 93,461 hrs · 28,298 cycles

LEFT COURIER SEAT O2 MASK DOES NOT TEST. AMM SMP UPON INSPECTION OF NR 1 COURIER MASK, FOUND OXYGEN LINES IMPROPERLY STOWED. STOWED MASK & LINES IAW AMM 35-11-00-2-99. SYS OPERATES NORMALLY IAW AMM 35-11-00-5. NO LEAKS OR DEFECTS NOTED AT THIS TIME.

Part: PANEL — NOT SEATED (L1 DOOR) · airframe 93,331 hrs · 28,206 cycles

L1 DOOR SLIDE WOULD NOT ARM PROPERLY BEFORE PUSHBACK. THE POP OUT ARMED PANEL STAYS FLUSH AGAINST THE DOOR WHEN THE EVACUATION SLIDE LEVER IS MOVED TO THE ARMED POSITION. FOUND CTR PANEL OUT OF TRACK, RESEATED CTR DOOR PANEL. GND TESTED NORMAL IAW SMP.

Part: BRACKET — BROKEN (SLIDE COVER) · airframe 93,330 hrs · 28,205 cycles

SLIDE COVER LOOSE & NOT ATTACHED PROPERLY AT THE BOTTOM OF THE L1 DOOR. FOUND TOP LT BRACKET BROKEN ON SLIDE RAFT COVER. INSTALLED SERVICEABLE SLIDE COVER

Part: BOLT — SHEARED (RUDDER) · airframe 92,943 hrs · 27,900 cycles

DURING TAXI OUT, CAPTAIN'S RT RUDDER PEDAL BROKE AS THE PARKING BRAKE WAS BEING SET. RT PEDAL MOVES FREELY WITH NO EFFECT ON FLIGHT CONTROLS. FOUND THE BOLT WHERE THE RT RUDDER PEDAL PUSHROD ATTACHES TO THE RUDDER PEDAL ARM TO BE SHEARED. REF IPC 24-21-02-02 FIG 2 SHEET 3 ITEM 068. R & R CAPTAIN`S RT RUDDER PEDAL ARM TO PUSHROD BOLT. CYCLED RUDDER PEDALS NUMEROUS TIMES WITH NO BINDING & HAD FULL MOTION FROM BOTH CAPTAIN'S & FIRST OFFICER`S SIDE. NO ADJUSTMENT TO PUSHROD NEEDED AS RIG CHECKED GOOD. WORK ACCOMPLISHED IAW AMM 27-21-02-4.

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 92,253 hrs · 27,290 cycles

LEFT ENTRY DOOR SLIDE COVER IS LOOSE. TIGHTENED LOWER STRAP. OPS CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (BS 1300 S20-21L) · airframe 92,086 hrs · 27,171 cycles

AFT CARGO BS 1300 FRAME HAS A CRACKED SHEAR TIE BETWEEN S20-21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW DRAWING 140N2002 AND SRM 51-40-02

Part: SKIN — DENTED (BS 637 S20L) · airframe 92,086 hrs · 27,171 cycles

FUSELAGE SKIN DENTED LEFT SIDE BS 637, STR 20L. CUT OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01 REPAIR 15 AND SRM 53-00-00.

Part: COVER — LOOSE (ESCAPE SLIDE) · airframe 91,518 hrs · 26,826 cycles

L-1 DOOR SLIDE HOUSING IS LOOSE. RETIGHTENED SLIDE COVER IAW 25-66-01-414-101, FIG 402. OK FOR SERVICE.

Part: BRACKET — BACKED OUT (PAX DOOR) · airframe 91,231 hrs · 26,641 cycles

L1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE. LOWER RT SIDE OF DOOR IS NOT ALIGNING PROPERLY AND IT TAKES SEVERAL ATTEMPTS TO CLOSE. REF PRIOR WRITE UPS. QTY 2 FITTING MSN 1267859 DURING GVI FWD UPPER AND LOWER FITTINGS IN DOOR FRAME HAVE LIGHT GOUGES FROM ROLLER MISALIGNMENT. FOUND BOLTS ON GUIDE ARM SUPPORT BRACKET BACKED OUT. RESECURED BOLTS AND ADJUSTED GUIDE ARM BRACKET IAW MM 52-11-04-2. REPLACED UPPER FWD. LATCH CAM AND ADJUSTED REF. MM 52-11-00-5. BURNISHED SCRATCHES OUT OF LOWER LATCH CAMS IAW SRM 52-10-00. REINSTALLED DOOR LINER REF.MM 52-11-02-4. ACFT OK FOR SERVICE.

Part: ACM — FAILED (ZONE 100) · airframe 90,776 hrs · 26,398 cycles

AFTER ENGINES STARTED, AN ACRID ODOR SEEMED TO ORIGINATE FROM THE LT PACK. WE ALSO HEARD A WHINNING NOISE AS THE THRUST LEVERS WERE ADVANCED. BOTH THE SMELL AND THE WHINE DID NOT RECUR WITH THE LT PACK OFF. INWORK. TROUBLESHOT AND FOUND ACM NOT TURNING WHEN PACK IS ON. R & R ACM IN REF TO AMM 21-51-03-4. OPS AND LEAKS CHECK GOOD. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.

Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 90,710 hrs · 26,361 cycles

EICAS RT EMERGENCY DOOR AND OVERHEAD EMERGENCY DOOR LIGHT ON MOST OF FLIGHT. OFF DURING DESCENT. ADJUSTED DOOR PROX SENSOR GAP. OPS CHECKS GOOD.

Part: DUCT — DISCONNECTED (A/C PACK) · airframe 90,660 hrs · 26,332 cycles

ON DEPARTURE WITH LT PACK MEL'D, RECEIVED "RT PACK TRIP". COULD NOT PRESSURIZE ACFT. FOUND DUCT DISCONNECTED FROM TOP OF R/H HEAT EXCHANGER AND FROM THE ACM COMPRESSOR OUTLET, INSTALLED DUCT WITH NEW COUPLER AND PERI SEALS IAW AMM ACM. R & R SECTION. FOUND REMAINING 2 DUCTS COMING FROM ACM TO HAVE THEIR CONNECTING BOLTS VERY LOOSE; TIGHTENED SAME, OPS CHECKED RT PACK IS NORMAL REF AMM 21-51-03-4 SUBTASK 21-51-03-434-033.

Part: SEAT TRACK — DAMAGED (BS 1438) · airframe 90,419 hrs · 26,163 cycles

STA 1438 BL 0 SEAT TRACK SPLICE REPAIR WAS ACCOMPLISHED DURING PTF CONVERSION ON MAE EA 757-5365-16-F3127, 8110-3 DATED JAN 30, 2011. THIS N/R GENERATED FOR TIME TRACKING AT STA 1420-1440, BL0 A REPAIR WAS ACCOMPLISHED ON STAM W/C 118350557EZ2R07 AND STAM EA 757-5365-16-F3127 REV- DATED 01/25/11. CLASSIFIED MAJOR REPAIR.

Part: SKIN — CRACKED (L4 DOOR) · airframe 90,419 hrs · 26,163 cycles

L4 DOOR HAS CRACKED SKIN 2 PLACES ON INSIDE OF DOOR. FWD SIDE WL 251, STA 1652. BLENDED OUT DAMAGE ON L4 DOOR FWD SIDE WL 251 STA 1652 IAW SRM 51-10-02. BLEND OUT OF 1ST CRACK. .200X1.5 BLEND OUT OF 2ND CRACK .400X2.5. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-01 FIG 101 DETAIL V. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13 AND SRM 51-40-02. MAJOR REPAIR

Part: PRESSURE PANEL — MISALIGNED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

2 EA EXISTING CUT OUTS IN AFT PRESSURE WEB AT STA 1710-1720, RBL 15 AND RBL 35 WILL INTERFER WITH INSTALLATION OF MOD REPAIR OF PRESSURE WEB AT STA 1710-1720 RBL 15 AND 35 WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE NR 45256110001 AND MAE EA 757-5365-16-F2985 REV- DATED OCT 22, 2010. REF FORM 8110-3 DATED JAN. 26, 2011. CLASSIFIED MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · airframe 90,419 hrs · 26,163 cycles

CORRSION ON BOTTOM OF FUSELAGE STA 640, BETWEEN S-28L TO S-30L.

Part: FRAME — GOUGED (BS 1380) · airframe 90,419 hrs · 26,163 cycles

AFT CARGO DOOR CUTOUT STA 1380 S-25R TO S27R, FRAME INBD CHORD GOUGED AND BARE METAL AFT CARGO DOOR CUTOUT, STA 1380 S-25R TO S-27R REPAIR COMPLIED WITH EA F-5310-146264. REF FAA FORM 8100-9 DATED MARCH 14, 2011. CLASSIFIED MAJOR REPAIR.

Part: SKIN — DENTED (BS 1500-1520) · airframe 90,419 hrs · 26,163 cycles

EXTERNAL FUSELAGE SKIN STA 1500-1520 BETWEEN S-22R TO S-23R HAS DENT. REPAIRED DENT ON FUSELAGE SKIN STA 1500-1520 BETWEEN S-22R TO S23R IAW SRM 53-00- 01 REPAIR 16 FIG 201. REPAIR INSPECTION REQUIRED IAW SRM 53-00-01 DETAIL II FIG 201 TABLE V. INITIAL INSPECTION AT 16,000 FC INTERVAL/SUBSEQUENT 6,000 FC CATEGORY "B" REPAIR.HFEC METHOD IAW NTM 51-00-01 PT 6

Part: SKIN — MISREPAIRED (BS 798 S15-16L) · airframe 90,419 hrs · 26,163 cycles

REPAIR BS 798 BETWEEN STR 15L-16L, INCORRECT SRM USED FOR INSTALLATION, REPAIRED IAW SRM 53-00-01, REPAIR 16 FIG 201 SHEET 1 THROUGH 6, CATEGORY "B" REPAIR RECURRENT INSPECTION IAW 53-00-01 FIG 201, TABLE V. MAJOR REPAIR.

Part: SKIN — FAILED (BS 765 S16-17L) · airframe 90,419 hrs · 26,163 cycles

REWORK OF SRM N00045 REPAIR ASSESSMENT EXT FUSE SKIN REPAIR BS 765 BETWEEN STR 16L-17L C/W ATTACHMENT "B' OF E.O 7-5001-7-5001 PT 1 INCORRECT SRM USED FOR INSTALLATION COMPLIED WITH FED EX EA F-5330-146395. REF FAA FORM 8110-3 DATED MARCH 12,2011. CLASSIFIED MAJOR REPAIR

Part: FRAME — CRACKED (BS 1280 L25-26R) · airframe 90,419 hrs · 26,163 cycles

AFT CARGO TA 1280 26R-25R FRAME HAS A CRACK. COMPLIED WITH E.A. F-5310-146259,8100-9 DATED MARCH 11, 2011- FIRST STAGE APPROVAL DTA 24 MONTHS. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

WHILE DRILLING P/N 11864182-21 AND -20 BL 0 AT STA 1438.0 SEAT TRACK SPLICES WERE MISDRILLED P/N 146N5178-1 AND 146N5185-U1. REPAIR ACCOMPLISHED IAW EA 757-5365-16-F3127 AND 8110-3 DATED JAN 30, 2011IN STMAE MOD CARD 118350557EZR07 REFERENCE EA F-5310-146387 FOR TRACKING. THIS A MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 1460 BETWEEN STR 2L TO 3L SEVERAL EXISTING TV MONITOR MOUNT AT HOLES DO NOT HAVE PROPER ED. REMOVED FRAME DAMAGE, FABRICATED NEW PARTS AND INSTALLED IAW SRM 53-00-07, FIG. 201. REPAIR NR 3 CAT "B" REPAIR WITH SUPPLEMENTAL INSP INITIAL-36, 163 F/C REPEAT EVERY 12,000 F/C METHOD HFEC NDT MANUAL 51-00-01, APT 6.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 90,419 hrs · 26,163 cycles

REWORK OF SNRM N00090, REPAIR INSTALLED IAW INCORRECT SRM REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXT SKIN DENT AT STA 310 AND STR S23R. REMOVED EXT REPAIR AT STA 310 AND S23R IAW SRM 51-40-02, ACOMPLISHED REPAIR IAW SRM B757-200 SF 53-00-01. REPAIR 15, FIG 201 INSPECTION THRESHOLD REPETATIVE. INSP REQUIRED BEFORE 29,000 F/C REPEAT INSP LFEC INTERVAL 3000 F/C CATEGORY B REPAIR. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 90,419 hrs · 26,163 cycles

REPAIR INSTALLED IAW INCORRECT SRM. REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXTERNAL SKIN STA 520 BETWEEN S-24R TOS-25R. R & R REPAIR IAW SRM 53-00-01, REPAIR 15 B757-SF. OUTER ROW OF FASTNERS MUST BE INSPECTED EVERY 25,000 FC, CATEGORY "B" MAJOR REPAIR.

Part: STRINGER — GOUGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

STA 278-270.5 S-23R HAS A GOUGE. NO ALLOWABLE DAMAGE FOR SPECIAL FREIGHTER EXIST. R & R S-23R AT STA 278-270.5 IAW SRM 51-40-02. FABRICATED STRINGER ON MAE TRAVELER T10/863577. CAT "A" MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1280 S11L) · airframe 90,419 hrs · 26,163 cycles

REWORK OF NR N01479, REWORK REQUIRED ON FRAME STA 1280 AT STRINGER 11L DUE TO REPAIR INSTALLED IAW INCORRECT SRM. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR SRM 53-00-07, FIG 201, DETAIL 1, REPAIR 3.

Part: FRAME — MISREPAIRED (BS 1280 S11-13R) · airframe 90,419 hrs · 26,163 cycles

REWORK OF NR N01483, REWORK REQUIRED ON FRAME, STA 1280 BETWEEN S11R AND S13R DUE TO REPAIR INSTALLED IAW INCORRECT SRM. R & R REPAIR AT STA 1280, BETWEEN S11R AND S13R IAW SRM 53-00-07, FIG 201, DETAIL 1 REPAIR 3. MAJOR REPAIR.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 90,419 hrs · 26,163 cycles

AFT CARGO DOOR, BELOW INTERNAL HANDLE, SKIN GOUGED. ACCOMPLISHED EA F-5230-146219, STEPS 1-8, AFT LOWER CARGO DOOR INNER SKIN GOUGED REPAIR, STA 1400, STR 25R. MAJOR REPAIR.

Part: SKIN — DAMAGED (NR 2 SLAT) · airframe 90,419 hrs · 26,163 cycles

LT WING NR 2 SLAT LOWER SURFACE FSS 635 WEDGE PUNCTURED REPAIRED NR2 SLAT LOWER WEDGE PUNCTURE IAW SRM 51-70-10, REPAIR 2. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 90,419 hrs · 26,163 cycles

RT FUSELAGE EXT SKIN DENTED AT STA 1620 S-18R EVALUATED DENT AT STA 1620 S-18R A=.9 Y=.020 A/Y RATION 45. FOUND OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DAMAGE IAW EA F-5330-146212. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1280 S11L) · airframe 90,419 hrs · 26,163 cycles

STA 1280, S-11L, FRAME REPAIR IS NOT IAW SRM INCOMING CONDITION. R & R FRAME IAW SRM 51-70-11, FIG 1 AND SRM 51-40-02. DTE REPAIR ASSESSMENT ON WO 00049137, N/R 00078. MAJOR REPAIR

Part: FRAME — MISREPAIRED (BS 1280 S11-13R) · airframe 90,419 hrs · 26,163 cycles

FRAME REPAIR AT BS 1280 BETWEEN ST 11-13R NOT IAW SRM REQUIREMENTS. R & R FRAME IAW SRM 51-70-11 FIG 1 AND SRM 51-40-02. MAJOR REPAIR

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 1360, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FROME FROM 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED REPAIR PARTS 1 PORTION OF FRAME T10/860856 2 CHANNEL T10/960858 2 CHANNELS T10/86054 AND CHANNELS T10/863415 IAM SRM 53-00-07 FIG 202 DETAIL I LOCATED AND DRILLED THE REPAIR PART IAW SRM 51/40/05 INSTALLED REPJAIR PARTS IAW SRM 51-40-02

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 1360 STR S-2R, HAS EXISTING MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FRAME FROM STA 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED THE REPAIR PARTS 1. PORTION OF FRAME TRAVLER T10/860856 2 CHANNEL T10/860858 2 CHANNEL T10/860854 AND 2 CHANNELS T10/863415 IAW SRM 51-00-07 FIG 202 LOCATED AND DRILLED THE REPAIR PARTS IAW 51-40-05 INSTALLED PARTS IAW SRM 53-00-07 FIG. 202 REPAIR 1 AND TABLE 203 ZONE 3 12,000 FLIGTH CYLES FROM REPAIR INSTALLATION OR 50,0000 AIRFRAME FLT CYCLES WHICHEVER COMES FIRST, THIS IS A "B" MAJOR REPAIR

Part: SKIN — DENTED (BS 231 S23-24R) · airframe 90,419 hrs · 26,163 cycles

RT FUSELAGE EXT SKIN DENTED AT STA 231 BETWEEN S-23R TO S-24R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG III. REPAIRED DAMAGE AREA IAW EA F-5330-143238 DATED 12/14/10. FAA FORM 8100-9, DATED JAN 10, 2011, CATEGORY "B" MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1330-1360) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CORROSION ON FLOOR MOUNT HOLES STA 1330 TO 1360, RBL62, MAIN CABIN. REMOVED CORROSION CHECK LIMITS ORIG MAT .070",L=2.0", W=0.80",D=.010" FOUND TO BE OUT OF LIMITS.REMOVED I/B CHORD, LOCATED DRILLED AND INSTALLED PART IAW SRM 51-40-02. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CREASE WEG AT STA 1683, RBL 60 CORRODED ON UPPER SURFACE. CORROSION ON WEB AT STA 1683 RBL 60, BLENDED CORROSION AND CHECKED LIMITS IAW SRM 53-60-13, FIG 101,CORROSION FOUND TO BE OUT OF LIMITS. REMOVED WEB IAW SRM 51-40-02, RECEIVED NEW WEB PN 146N8723-2 ON TRAVELER NR T10/861148, LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05, INSTALLED NEW WEB IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — DENTED (BS 310) · airframe 90,419 hrs · 26,163 cycles

RT FUSELAGE EXT SKIN DENT AT B STA 310 AND STRINGER S23R INSTALLED REPAIR DOUBLER AT STA 310, S23R DENT WAS OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. DOUBLER WAS FABBED FROM .071 2024-T3 BATCH NR 1941519. FILLER WAS .063 2024-T3, BATCH NR 1905681 LOCATED AND DRILLED IAW SRM 51-40-05 CATEGORY B, REPAIR HFEC AT 6,000 FLIGHT CYCLES DENT L=.5 W=.75 D=.013 A/Y=57.7 DENT WAS AT STRINGER. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CABIN FLOORBEAM BS 720 TOP SURFACE IS CORRODED ADJACENT TO L-2 DOOR SILL. ACCOMPLISHED STEP 1-7 OF EA -5310-143217 COMPLIANCE WITH FAA FORM 8110-3. MAJOR REPAIR.

Part: GATE — CHAFED (ZONE 100) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

NR4 RT DOOR LOWER GATE SEAL SUPPORT STRUCTURE BOTH ENDS HAS CHAFED. BLENDED AREAIAW SRM 51-10-02 ,CHECKED LIMITS L=1.5,W=1,D=.060, FOUND TO BE OUT LIMITS IAW SRM 52-10-02 DETAIL V FIG 101. REMOVED DOOR GATE IAW SRM 51-40-02, RECEIVED NEW LOWER GATE P/N 146N606U56, LOCATED AND DRILLED IAW SRM 51-40-05 INSTALLED NEW LOWER DOOR GATE IAW SRM 51-40-02, R-4 DOOR LOWER GATE. MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE EDS. REMOVED AND INSTALLED STRINGER CLIP AT S-2L IAW SRM 51-40-02. CUT OUT FRAME FROM STR 1 TO STR 5L, IAW SRM 53-00-07, FOR SPECIAL FREIGHTER AND REPAIRED IAW SRM 53-00-07 FOR SPECIAL FREIGHTER REPAIR 3 RECURRENT INSP REQUIRED IAW SRM 53-00-07, FLAG NOTE "D" 10,000 FLT CYCLES AND HFEC INSPECTION EVERY 12,000 FLT CYCLES INTERVAL. (CATEGORY "B"). MAJOR REPAIR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. R & R STRINGER CLIP S2R IAW SRM 51-40-02. CUT OUT FRAME FROM STR 2R TO STR 5R, IAW SRM 53-00-07 FOR SPECIAL FREIGHTER AND REPAIRED IAW SRM 53-00-07 FOR SPECIAL FREIGHTER. REPAIR 3 RECURRENT INSP REQUIRED IAW SRM 53-00-07, FLAG NOTE "D", 10,000 FLT CYCLES AND HFEC INSP EVERY 12,000 FLT. CYCLES INTERVAL. (CATEGORY "B"). MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 418 S1R) · airframe 90,419 hrs · 26,163 cycles

MAIN CARGO DECK FRAME AT STA 418 BETWEEN STRINGER S-1R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. REPLACED FRAME AT STA 418 FROM RBL 2.5 TO TO LBL 2.5 IAW EA 757-5312-16-F3027. MAJOR REPAIR.

Part: SKIN — DENTED (BS 520 S24-25R) · airframe 90,419 hrs · 26,163 cycles

RT FUSELAGE EXTERNAL SKIN DENT BS 520 BETWEEN STRINGER 24R-25R. FABRICATED, INSTALLED DOUBLER & FILLER 2024-T3 BATCH 0001928869 .063 &2024-T3 .056 BATCH 0001383027 IAW SRM 53-00-01 REPAIR 2 THRESHOLD INSPECTION OF REPAIR DOULBER TO OCCUR ON OR BEFORE 37,500 FLIGHT CYCLES AND INTERVALS OF 6.000 FOR HFEC OR 3,000 FLIGHT CYCLES FOR LFEC THEREAFTER IAW SRM 53-00-01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1080-1180) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

SEAT TRACK CROWN AT RBL 45, STA 1080-1180 HAS SEVERAL AREAS OF CORROSION AND GOUGES FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101, FABRICATED NEW SEAT TRACK P/N BAC 1520-792 IAW SRM 53-40-02, LOCATED AND DRILLED IAW SRM 51-40- 05, INSTALLED NEW SEAT TRACK ON RBL 45 FROM STA 1080-1180 IAW SRM 51-40-02. ORIG MAT .550 REMAINING MAT .530 ALLOWABLE DAMAGE 0.02 FOUND TO BE OUT OF LIMITS IAW SRM 53-0052 DETAIL I FIG 101. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1080-1180) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

SEAT TRACK CROWN AT LBL 45 STA1080-1180 HAS SEVERALAREAS OF CORROSION AND GOUGES. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. ORIGINAL MATERIAL .550 MATERIAL REMOVED .050 MATERIAL REMAINING .500 .FOUND OUT CLEANED AREA IS OUT OF LIMITS REMOVED AND INSTALLED NEW SEAT TRACK BATCH 1904663 IAW SRM 51-40-02 MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1640) · airframe 90,419 hrs · 26,163 cycles

CORROSION ON SEAT TRACK STA 1640 RT SIDE AT END OF TRACK MAIN CABIN. REMOVED CORROSION ON SEAT TRACK STA 1640 RBL 45. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL VII. ORIG MATERIAL .070 AFTER REWORK .025. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: CUSP WEB — CORRODED (BS 1140-1160) · airframe 90,419 hrs · 26,163 cycles

LT SIDE CUSP WEB BETWEEN FR 1140 &FR 1160 HAS CORROSION ON UPPER SURFACE REMOVED CORROSION IAW 51-10-02 SHEAR WEB AND WEB OUT OF LIMITS IAW SRM 53-40-13 FIG-101, DETAIL III. INSTALLED NEW SHEAR WEB AND WEB ON TRAVLERS T10/858934 AND T10/858933. REINSTALLED ANGLE IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 365) · airframe 90,419 hrs · 26,163 cycles

SEAT TRACK AT RBL 24 AHS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL XIK. ORGINAL MAT.080 AFTER REWORK .040 EXCEEDS REMOVE SEAT TRACK SUPPORT IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK SUPPORT ON PN BAC 1505-237/16 BATCH NR 1895840 IAW SRM 51-01-01. INSTALLED SEAT TRACK SUPPORT IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

SEAT TRACK CORRODED AT STA 440 RBL 24.75 ORIGINAL MATERIAL .070 REMOVED .060 REMAINING MATERIAL .010 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG. 101 DETAIL VII PAGE 104 REMOVED AND REPLACED SEAT TRACK IAW SRM 50- 40-02 PN BAC 1520-792 BATCH 0001904663 FROM STA 440 RBL 24.75

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CORROSION ON FLOORBEAM STA 1661, RBL 42, RT SIDE MAIN CABIN. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL II FABRICATED FLOORBEAM 1661 FROM MAT BAC1518-338 BATCH 1915536 LOCATED AND DRILLED IAW SRM 51-40-05. REMOVED AND REPLACED IAW SRM 51-49-02 MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 90,419 hrs · 26,163 cycles

CORROSION ON FLOORBEAM STA 1640, FROM RBL 62 TO LBL 62, MAIN CABIN. REMOVED CORROSION AT FLOORBEAM, STA 1640 FROM RBL 62 TO LBL 62, MAIN CABIN IAW SRM 53-00. ORIGINAL MATERIAL .130, AFTER REWORK .095, AMOUNT OF MATERIAL REMOVED TO BE IN OUT OF LIMITS IAW SRM 53-00-51, DETAIL II, FIG 101. R & R FLOORBEAM AT STA 1640 IAW SRM 51-40-02, TREATED AND PRIMED IAW SRM 51-20-01. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

AT STA 1681, FLOORBEAM HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE OF FLOOR. REMOVED CORROSION IAW SRM 51-10-01 FOUND FLOOR BEAM OUT OF LIMITS ORIG. MAT 0.150 AFTER BLEND OUT THE WORST SPOT 0.091 IAW SRM 53-00-51 DETAIL VI. REMOVED AND REPLACED FLOORBEAM STA. 1681 LBL 62 TO RBL 62 IAW SRM 51-40-05 AND 51-40-02 MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CORROSION ON FLOOR STA 1345, LBL 62, MAIN CABIN. REMOVED CORROSION ON LT SIDE INBD CREASE BEAM CHORD STA 1292-1370 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. ORIG MATERIAL .070 AFTER REWORK .045. R & R CHORD IAW SRM 51-40-02. CLASSIFIED CAT "A" MAJOR REPAIR.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CUSP WEB BETWEEN FR1600 AND FR1620 HAS CORROSION ON UPPER SURFACE LBL 62. REMOVED CORROSION ON WEB IAW SRM 51-10-02, CHECKED LIMITS L=4",W=3", D=.020",MAT ORIG .040 IAW SRM 53-60-13, DET VI, OUT LIMITS IAW SRM 53-60-13, PG 103, DET III, R &R WEB IAW SRM 51-40-02, WEB P/N FX 146N8722-13. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

SEAT TRACK AT RBL 48 HAS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DETAIL VII. ORIGINAL MAT .080" AFTER REWORK .48" EXCEEDS. REMOVED SEAT TRACK SUPPORT IAW SRM 51-40-02. FABRICTED NEW SEAT TRACK SUPPORT P/N BAC 1505- 237/16 BATCH NR 1895840, IAW 51-01-01. INSTALLED SEAT TRACK SUPPORT IAW SRM 51-40-02. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

BS 365, FLOORBEAM HAS CORROSION ON UPPER SURFACE FROM BL 0.0 TO RBL 65.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MAT .125. AFTER REWORK .095 AREA OF DAMAGE L(.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51. REPAIR NR3 FROM LBL13 TO RBL 65, STA 365, CATEGORY "A". MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

BS 345 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT RBL 2.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101. AFTER REWORK .101, AREA OF DAMAGE L(2.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51, REPAIR 3, FROM RBL 35 LBL 50. BS 345. CATEGORY "A" REPAIR. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1280) · airframe 90,419 hrs · 26,163 cycles

FRAME 1280 IS GOUGED JUST BELOW STR S-11L.

Part: CREASE BEAM — CORRODED (BS 1180) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CORROSION STA 1180, LBL 62, W/L 208 CREASE BEAM. REMOVED AND REPLACED NEW CREASE BEAM IAW SRM 51-40-02 AND SRM 51-40-05, FABRICATED ON BATCH 0001879122, MAJOR REPAIR .

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

BS 324 FLOORBEAM HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEEN BL 0 AND RBL 40. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. ORIG MATERIAL .125 AFTER REWORK .085. R & R UPPER CHORD RBL 62 TO LBL 62 IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CABIN FLOOR BS 440 TO BS 640 SEAT TRACK RBL 46 IS WORN/SCRATCH AND CORRODED IN SEVERAL PLACES AS MARK. BLENDED ARE IAW SRM 51-10-02,MAT ORIG ORIG .O70 MAT LOSS L=1.50",W=1",D=.026 OUT OF LIMITS IAW SRM 53-10-52 FIG 101 DETAIL III, REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK FROM MAT BAC 1520-792 BATCH 1904663 IAW SRM 53-00-52, LOCATED AND DEILLED NEW SEAT TRACK IAW SRM 51-40-05 AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,419 hrs · 26,163 cycles

CORROSION BETWEEN STA 1040 AND STA 1020 RBL 62 W/L 208 4EA SPOTS MAIN CABIN. REMOVED CORROSION AT INNER CHORD IAW SRM 51-10-02. ORIG. MAT. .070" IAW DWG BAC1515-551 MAT. LOSS D=.030" L=4.200 W=1.00" MAX. MAT. REMOVE ALLOWABLE IS .007", FOUND OUT LIMITS IAW SRM 53-40-13. REMOVED INNER CHORD BETWEEN STA 900 TO 1040 IAW SRM 51-40-02, RECEIVED NEW PART BATCH1844725 PART BAC1515-551, FABRICATED PART IAW SRM 53-40-13, TRATED & PRIMED IAW SRM 51-20-01, TOP COATED IAW AMM 51-21-00 & INSTALLED INNER CHORD BETWEEN STA 900 TO 1040 IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.