N941FD

Part: NONE — NONE (N/A) · corrosion level 2 · airframe 76,914 hrs · 32,527 cycles

#2 PYLON UNDER PANEL #443HL CORROSION ON INNER SURFACE LOWER CORNER AROUND FASTENER ACCOMPLISHED FEDEX EA# F-5450-T0366121 P1, NACELLES / PYLON - WING PYLON/STRUT - #2 PYLON, INB SIDE, SKIN, INNER SURFACE PP STA 144, CORROSION

Part: NONE — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#8 SLAT I/B TRACK I/B SIDE COVE PANEL CRACKED REMOVED AND REPLACED COVE PANEL PER BAC DWG #114N4004 REV F

Part: STRAP — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#2 ENG I/B T/R FWD STRAP CRACKED REMOVED AND REPLACED STRAP PER B757 AMM 78-31-20-8

Part: NONE — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#2 PYLON UNDER ACCESS PANEL 611KT FWD OUTBOARD END U-CHANNEL CRACKED. REMOVED AND REPLACED U-CHANNEL ON #2 PYLON UNDER ACCESS PANEL 611KT IAW BAC DWG 313N5004 REV D

Part: NONE — WORN (N/A) · airframe 76,914 hrs · 32,527 cycles

#1 ENGINE OTBD T/R UPPER AFT INNER THERMAL SHIELD METAL PLATE IS WORN THRU. ENGINE EXHAUST - TR STRUCTURE/SLEEVE - #1 LH TR INNER DUCT REAR INNER PANDOWN WELD REPAIR PER FEDEX EA F-7833-T0366003

Part: NONE — NONE (N/A) · airframe 76,914 hrs · 32,527 cycles

FUSELAGE EXTERNAL SKIN, STA 460 STR28R, HAS 2EA DEEP GOUGES ACCOMPLISHED FEDEX EA# F-5330-T0365972-P1: FUSELAGE - PLATES AND SKIN - STA 456, S- 27R - S-28R, GOUGES, DOUBLER REPAIR.

Part: STRAP — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#2 ENG I/B T/R FWD CROSSBRACE SUPPORT BRACKET IS CRACKED REMOVED AND REPLACED BRACKET PER B757 AMM 78-30-20-8

Part: BRACKET — LOOSE (N/A) · airframe 76,914 hrs · 32,527 cycles

L/W I/B FLAP O/B TRACK UNDER FAIRING SUPPORT BRACKET IS LOOSE REMOVED AND REINSTALLED L-WING FLAP UPPER PANEL IAW BAC DWG 113N2003 REV A AND B757 SRM 51-40-04 - T# E110392G. ACCOMPLISHED INBOARD MAIN FLAP FASTENER HOLE REPAIR AT THE AFT FAIRING SUPPORT FITTING LOCATION IAW B757 SRM 57-53-02-2R REPAIR 3

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,914 hrs · 32,527 cycles

@2 PYLON LANDING FOR ACCESS PANEL #443GL HAS CORROSION FWD LOWER CORNER NACELLES/PYLONS - SKIN/PLATES/PANELS - #2 PYLON INBD SKIN PANEL, PP STA 114, INNER SURFACE, CORROSION REPAIR PER FEDEX EA F-5430-T0366016

Part: NONE — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#1 ENGINE EXHAUST DUCT LOWER FORWARD EDGE HAS A CRACKED BRACKET REMOVED AND REPLACED BRACKET PER RR EM 78-11-04-300-008-801

Part: NONE — NONE (N/A) · airframe 76,914 hrs · 32,527 cycles

NO.2 ENGINE INBD COWL EXTERIOR SURFACE HAS A DENT REPAIRED NO 2 ENGINE COWL ENG INBD EXTERIOR SURFACE IAW B757 SRM 54-20-01-1A, SRM 54-20-01-2R,

Part: BRACKET — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

#2 ENGINE AFT DRAIN LINE BRACKET CRACKED LOWER AFT HOT SECTION REMOVED AND REPLACED BRACKET PER RR EM 78-11-04-300-010

Part: PANEL — DELAMINATED (N/A) · airframe 76,914 hrs · 32,527 cycles

WING TO BODY PANEL 195EL IS DELAMINATED ON THE EDGE REPAIRED PER B757 SRM 53-00-70-2R-1 AND 53-60-70-2R

Part: FRAME — DAMAGED (N/A) · airframe 76,914 hrs · 32,527 cycles

REPLACEMENT OF THE CAT C REPAIR INSTALLED ON FRAME BOTTOM ASSEMBLY AT STATION 1640, S26R - S27R REQUIRED ACCOMPLISHED PERMANENT REPAIR IAW FEDEX EA F--5310-T0352854-P2 (A), RELEASED JAN 03, 2022, TITLED "FUSELAGE - MAINFRAME - FRAME, STA 1640, S-26R - S-27R, GOUGE ANGLE REPAIR".

Part: FRAME — CRACKED (N/A) · airframe 76,914 hrs · 32,527 cycles

STA 1640 FRAME, RHS, HAS CRACK INDICATION @ LOWER, INBD HOLE @ S14R ACCOMPLISHED FEDEX EA# F-5310-T0365884: FUSELAGE - MAINFRAME - FRAME, STA 1640, S14R CRACK INDICATION *THIS EA DEVIATES FROM EO F-5310-E0344602

Part: CIRCUIT CARD — MALFUNCTIONED (WARNING SYSTEM) · airframe 76,361 hrs · 32,191 cycles

AURAL WARNING SOUNDED CONTINUOUSLY INFLIGHT NO LAND 3. PERFORMED MCDP TEST 30/40 WITH NO FAULTS FOUND. LAST FLIGHT FAULT WAS "RUD SRVO/FCC C" DIAGNOSTIC CODE 131361. REMOVED AND REPLACED LEFT AND RIGHT SIREN/OWL CARD MODULE (M999 & M619) IAW 757 AMM 31-51-04- 4. TESTS NORMAL. OK FOR SERVICE. TSI 31-50/8687. 2>DUE TO DELAY IN SJO CAUSED BY AURAL WARNING ISSUES PLEASE TROUBLESHOOT PER 757 FIM 31-51 FT 814 AND REPAIR ALL FAULTS FOUND. COMPLETE 3>DUE A PREVIOUS FAULT ON THE CENTER FCC PLEASE REPLACE UNIT AS A PRECAUTION PER AMM 22-11-01. . COMPLETE 4>PLEASE INSPECT THE THE P51 CARD FILE AND SURROUNDING AREA FOR ANY SIGN OF WATER ACCUMULATION . COMPLETE

Part: THROTTLE — FAULTED (RT ENGINE) · airframe 75,938 hrs · 31,947 cycles

RIGHT THRUST LEVER FROZEN AT 12 O'CLOCK POSITION. RT ENGINE SHUT DOWN IN FLIGHT. DISCONNECTED THROTTLE CABLE OF RH ENGINE BETWEEN UPPER GEARBOX AND INTERMEDIATE GEARBOX AT ARROWHEAD DISCONNECT. THROTTLE FREE IN COCKPIT. DISCONNECTED LOWER GEARBOX FROM FFG. FFG NOT BINDING. FOUND INNER LINER DISBONDED ON HARD LINE ON LOWER GEARBOX. INNER LINER WAS BINDING CABLE OF LOWER GEARBOX. REMOVED AND PARTIALLY INSTALLED LOWER GEARBOX ASSY IAW AMM 76-11-10-4-0. RIG PINS REMAIN INSTALLED. UPPER GEARBOX, INTERMEDIATE GEARBOX, AND LOWER GEARBOX.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 75,274 hrs · 31,562 cycles

LT FWD ENT DOOR SLIDE DEPLOY IN MEM. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHK GOOD. REMOVED FROM MEL. A/C OK FOR SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE STATION 1640 STRINGER 26 RIGHT, FRAME HAS A GOUGE AND SUPPORT ANGLE HAS AN ELONGATED HOLE. ACCOMPLISHED EA # F-5310-T0352854 P1 FUSELAGE - MAINFRAME - FRAME, STA 1640, S26R-S27R, GOUGE, ANGLE REPAIR

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR BEAM LWR SURFACE IS DAMAGED AT STA 1560 APPROX LBL 53 (STREAMER ATTACHED) ALL WORK ACOMPLISHED IAW FEDEX EA# F-5321-T0352761 P1, FUSELAGE- CARGO COMP FLOORS- STA 1560 1560 LBL 53 FLOOR BEAM LWR FWD FLANGE

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE EXT SKIN STA 1280 TO 1400 AND FROM S26L TO S26R HAS SEVERAL PREVIOUS BLENDS REPAIRED AREA PER EA# F-5310-T0352664-P1

Part: FRAME — BENT (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

AFT CARGO PIT LH STA 1580 FRAME BENT ALL WORK ACOMPLISHED IAW FED EX EA# F-5310-T0352536-P1

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE EXT BETWEEN STA 1540 AND STA 1560 AND BETWEEN S20L AND S22L PREVIOUS REPAIR HAS SEVERAL TOOLING MARKS REMOVED REPAIR AND REPAIRED AREA IAW FEDEX EA # F-5330-T0352692-P1

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

BROKEN SHEAR TIE AT STA 1600 BETWEEN STR 27L AND 28L REMOVED BROKEN SHEAR TIE IAW B757-200 SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW FED EA F-5310-T0352992-P1 AND BOEING DWG 146N1021 REV A. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 AND DWG 146N1021 REV A. (TITLE FUSELAGE - MAINFRAME - AFT CARGO COMPARTMENT SHEAR TIE, STA 1600 BETWEEN STR 27L AND 28L, ALTERNATE FINISH.) PART MARKED IAW FED EX GMM 07-0-1000.

Part: FRAME — BENT (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

AFT CARGOPIT LH STA 1600 FRAME BENT ALL WORK ACOMPLISHED IAW FEDEX EA# F-5310-T0352546-P1

Part: SKIN — DENTED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S27R TO S29R HAS 4EA DENTS. REPAIRED AREA PER EA# F-5310-T0352664-P1

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S30 TO S26L HAS SEVERAL PREVIOUS BLENDS AREA REPAIRED PER EA # F-5310-T0352664 P1

Part: FRAME — BENT (BS 1600) · airframe 75,087 hrs · 31,452 cycles

AFT CARGO LT BS 1600 FRAME BENT. ALL WORK ACOMPLISHED IAW EA F-5310-T0352546-P1.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

AFT PIT RBL 16.21 WL 160.0 INTERCOSTAL HAS MULTIPLE ELONGATED AND DOUBLE DRILLED HOLES REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 146N5443 REV J AND DWG 146N5451 REV C

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

AFT PIT LBL 16.21 WL 160.0 INTERCOSTAL HAS MULTIPLE ELONGATED AND DOUBLE DRILLED HOLES REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 146N5443 REV J AND DWG 146N5451 REV C

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN AFT DECK PLATE VIEWED FROM BELOW STA 1715 RBL 12 SUPPORT ANGLE CORRODED REMOVED AND REPLACED CORRODED ANGLE IAW BOEING DWG 146N5221 REV B

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

SURFACE CORROSION AT BODY STATION 118 (UNDERNEATH MAIN CARGO DECK FLOORBOARD) FLOOR SUPPORT BEAM, SECOND BEAM FROM LEFT, AROUND AND BELOW SEAT TRACK, AROUND HYLOCKS ON SEAT TRACK STANDOFF BRACKET, AND AROUND AND ON STANDOFF FOR SEAT TRACK. DOT AND STREAMER ATTACHED. REPAIRED IAW FEDEX EA# F-5321-T0352826-P1 FUSELAGE-CARGO COMP FLOORS-SEAT TRACK-STA 1080 TO 1180, LBL 45.50,REPLACEMENT EXTRUSION PROFILE, AND FEDEX EA# F-5321-T0352783-P1 FUSELAGE-CARGO COMP FLOORS-SEAT TRACK SPLICE FITTING, STA 1180, LBL 45.5, EDGE DAMAGE, BLEND REPAIR AND IAW BOEING DWG 144N5002

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT, STRUCTURAL SHEAR WEB IS CORRODED AT APPROX STA 1691 APPROX LBL10 REPAIRED IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1686 APPROX LBL10 ALL WORK ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1701 APPROX LBL7 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: NUT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 23 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 22 SHEAR WEB IS CORRODED REPAIR ACCOMPLISHED ON N/R N00334 IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: SHEAR WEB — DAMAGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX 1683 RBL 31 ACCOMPLISHED FEDEX EA # F-5321-T0352653, FUSELAGE - CARGO COMP FLOORS - FLOOR SUPPORT, STA 1681 - 1701, RBL 20 AND 23, EDGE DAMAGE, BLEND REPAIR. ACCOMPLISHED DOUBLER REPAIR ON N/R N00334 IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1706 APPROX LBL7 ALL WORK ACCOMPLISHED ON NR N00342 IAW B757-2 SRM 53-60-51-2R REPAIR 2

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 40 FLOOR BOARD NUTPLATE STRIP IS CORRODED ACCOMPLISHED FEDEX EA # F-5321-T0352606 FUSELAGE- CARGO COMP FLOORS - STA 1681, RBL 40, DOUBLE DRILLED HOLE, FREEZE PLUG REPAIR. ACCOMPLISHED DOUBLER REPAIR IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1683 APPROX LBL 12.5 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2

Part: NUT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 32 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 75,087 hrs · 31,452 cycles

R-2 DOOR SKIN UPPER HINGE CUT OUT IS CRACKED. REPAIR OF FWD FRAME OF NUMBER 2 RIGHT SIDE PASSENGER DOOR COMPLIED WITH IAW B757-200 SRM 52-10- 02 02-2R REPAIR 1. HFEC INSPECTION REQUIRED AT 50,000 TOTAL DOOR FLIGHT CYCLES OR 5,800 FLIGHT CYCLES AFTER REPAIR INSTALLATION IF THE DOOR FLIGHT CYCLES ARE NOT KNOWN AND EVERY 5,800 DOOR FLIGHT CYCLES AFTER IAW B757-200 SRM 52-10-02-2R REPAIR 1 PARA. 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

CABIN SEAT TRACK CORRODED ABS1071- BS 1075, BL LBL 24 REPAIRED SEAT TRACK IAW B757-2 SRM 53-00-52-2R REPAIR #4

Part: SLAT — DELAMINATED (LT WING) · airframe 75,087 hrs · 31,452 cycles

#3 SLAT REQUIRES REPLACEMENT REMOVED AND REPLACED AND PERFORMED OPS TEST ON #3 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOOD

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN RH SIDE SEAT TRACK IS GOUGED BS 619, RBL 00 REPAIRED SEAT TRACK IAW FEDEX EA# F-5320-T0352523-P1 FUSELAGE AUXILIARY STRUCTURE - CABIN SEAT TYRACK STA 619 BL 0 GOUGE SPLICE REPAIR

Part: RUB STRIP — CRACKED (TE FLAP) · airframe 75,087 hrs · 31,452 cycles

RIGHT WING INBD FLAP SUPPORT BRACKET HAS CRACKED RUB STRIP AT AFT TRUNNION FAIRING REMOVED ABD REPLACED RUB STRIP AT R/W I/B FLAP SUPPORT AT AFT TRUNNION FAIRING IAW BAC DWG 113N1831 REV-SRM 51-40-02

Part: BALANCE WEIGHT — CORRODED (LT AILERON) · airframe 75,087 hrs · 31,452 cycles

LEFT WING,OUTBOARD AILERON,INBOARD COUNTER BALANCES,SEVERAL HAVE CORROSION AND OR FLAKING PAINT REMOVED AND REPLACED 1 CORRODED L/W O/B AILERON I/B COUNTER BALANCE IAW B757 SRM 51-60-01-OG AND 51-40-02.RESTORED FINISH ON REMAINING COUNTER BALANCES IAW B757 AMM 51-20-01.{NO MOMENT CHANGE.NO REBALANCE REQ}

Part: SKIN — DENTED (BS 1360-1380) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE EXT SKIN BETWEEN ST 1360 AND 1380 ST S20L HAS DENT REPAIRED DENT IAW FEDEX E.A.# F-5330-T0352390 TITLE: FUSELAGE - PLATES AND SKINS - FUSELAGE SKIN, STA 1360 - 1380, S20L, DENT REPAIR

Part: PLATE — CORRODED (BS 676) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN RH SIDE METAL PLATE IS CORRODED UNDER THE SEAT TRACK BS 676, RBL 58 REMOVED AND REPLACED METAL PLATE UNDER THE SEAT TRACK AT BS676RBL 58 IAW VENTURA AEROSPACE DWG : 3458 REV L, B757 SRM 51-40-02-0G, B757 SRM 51-20-01-0G

Part: SKIN — DENTED (FUSELAGE) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE SKIN REPAIR AT APPROX. STA 1600 STR 26L-29L REQ ENLARGING TO INCORPORATE OTHER DAMAGES PER EA F-5330-T0346172B ALL WORK ACCOMPLISHED IAW FEDEX EA # F5330-T0348842-P1, FUSELAGE-PLATES AND SKIN-REPAIR OF FUSELAGE SKIN DAMAGE- STA 1553 TO STA 1625, S24L TO S29R

Part: SKIN — DENTED (BS 284) · airframe 75,087 hrs · 31,452 cycles

L/H SIDE EXTERIOR FUSELAGE SKIN IS DENTED APPROX 7" AFT OF THE PILOTS SIDE SLIDING WINDOW APPROX 20" UP FROM THE FLOOR LEVEL MEASURED DENT; MINOR AXIS .500", DEPTH .010" A/Y = 50, FOUND TO BE STRUCTURALLY ACCEPTEBLE PER FEDEX E.A. # F-5330-T0352423 P1: FUSELAGE - PLATES AND SKIN - -FUSELAGE SKIN DENT AT STA 283 JUST AFT / BELOW THE L-3 WINDOW ( NEAR WL= 230.00)

Part: CLOSEOUT PANEL — CRACKED (BS 418) · airframe 75,087 hrs · 31,452 cycles

PARTS RACK - P51 PANEL LOWER CLOSEOUT CONNECTOR PANEL IS CRACKED MULTIPLE LOCATIONS REMOVED, FABRICATED, AND INSTALLED NEW LOWER CLOSEOUT CONNECTOR PANEL IAW PARSONS DWG# 13481207 REV A AND B757 SRM 51-40-02

Part: WEB — DENTED (CARGO DOOR) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE MAIN CARGO DOOR INTERIOR SKIN FWD LOWER WEB HAS A PROTUDING DENT. REMOVED AND REPLACED MAIN CARGO DOOR INTERIOR FWD LOWER WEB IAW B757 SRM 51-4 40-02, BOEING DWG 65-49309 REV D, B757 SRM 51-20-01

Part: WEB — DENTED (BS 1377) · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR BOARD SUPPORT WEB UNDER RH SEAT TRACK AT STA. 1337 RBL 25 WEB AND ATTACH ANGLE DENTED AT ATTACHING FASTENER. REMOVED, FABRICATED IAW B757-200 SRM 53-60-51-01 AND REPLACED ATTACH ANGLE IN MAIN CABIN FLOOR BOARD SUPPORT WEB UNDER R/H SEAT TRACK AT STA 1337 RBL 25 IAW B757 SRM 51-40-02. DENT IN WEB FOUND WITHIN ACCEPTABLE LIMITS IAW 53-60-51

Part: WEB — DENTED (CARGO DOOR) · airframe 75,087 hrs · 31,452 cycles

FUSELAGE MAIN CARGO DOOR INTERIOR SKIN AFT LOWER WEB HAS PROTUDING DENT. REMOVED AND REPLACED MAIN CARGO DOOR INTERIOR AFT LOWER WEB IAW B757 SRM 51-4 40 40-02, BOEING DWG 65-49309 REV D, AND B757 SRM 51-20-01

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,087 hrs · 31,452 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1701 APPROX LBL 31 REPAIRED MAIN CABIN FLOOR SUPPORT SHEAR WEB (DECK PLATE) AT STA 1701, LBL 31 IAW B757 SRM 53-60-51-2R REPAIR 2, B757 SRM 51-20-01-0G AND B757 AMM 51-21-00-7

Part: SKIN — CRACKED (RT WING) · airframe 75,087 hrs · 31,452 cycles

RIGHT WING TRAILING EDGE LOWER PANEL BETWEEN #8 AND #9 SPOILERS CRACKED. REPAIRED PANEL PER B757 SRM 57-51-01-2R.

Part: BALANCE WEIGHT — CORRODED (LT AILERON) · airframe 75,087 hrs · 31,452 cycles

LEFT WING, OUTBOARD AILERON ,2EA COUNTER BALANCES HAVE FLAKING PAINT AND/OR CORROSION REMOVED AND REPLACED 2 CORRODED LEFT WING O/B AILERON COUNTER BALANCES IAW B757 SRM 51-60-01-OG AND 51-40-02.RESTORED FINISH ON OTHER 2 COUNTER BALANCES IAW B757 AMM 51-20-00.(NO MOMENT CHANGE NO REBALANCE REQUIRED )

Part: CHANNEL — GOUGED (LT MLG WW) · airframe 75,087 hrs · 31,452 cycles

L/H MLG WHEEL WELL PANEL 197DL I/B ATTACH ANGLE GOUGED AT AFT END REPAIRED AREA PER B757 SRM 53-40-71-2R AND 51-70-11-OG

Part: SUPPORT — CRACKED (APU BAY) · airframe 75,087 hrs · 31,452 cycles

APU FIRE BOTTLE ACCESS PANEL LH LOCK BRACKET INBD SUPPORT CRACKED REMOVED AND REPLACED LH LOCK BRACKET INBD SUPPORT PN:148N661449 AT APU FIRE BOTTLE ACCESS PANEL IAW B757 SRM 51-40-09

Part: FLAP SYSTEM — CONTAMINATED (WING) · airframe 75,052 hrs · 31,433 cycles

DURING APPROACH WHEN GOING FROM FLAPS 20 TO FLAPS 25 GOT TE FLAP DISAGREE. RAN QRH. LANDED FLAPS 20, LUBRICATED THE TRAILING EDGE FLAP SYSTEM AMM 12-21-09-3. ALL GEARBOXES WERE SERVICED PROPERLY. NOTED THERE WAS WATER PRESENT IN SOME AREAS AND PUSHED OUT AS GREASE WAS APPLIED. OPERATED FLAPS 3X WITH NO ISSUES. ALSO REFER TO WRI 27-50-7564.

Part: SKIN PANEL — DELAMINATED (RT HORIZ STAB) · airframe 75,006 hrs · 31,404 cycles

RIGHT HAND HORIZONTAL STABILIZER HAS A PANEL ON THE BOTTOM SIDE WITH A DELAMINATED AREA OF APPROXIMATELY 2' X 3'. AREA IS LOCATED JUST AFT OF THE LEADING EDGE AND 5' OUTBOARD OF THE FUSELAGE. REMOVED & INSTALLED NEW SKIN PANEL RT LOWER HORZ STAB IAW SRM 51-40-02-0G.

Part: SKIN — DENTED (RT WING SLAT) · airframe 74,825 hrs · 31,272 cycles

RH WING ON #7 SLAT UPPER SURFACE IB SIDE HAS A DENT. REPAIRED R/H WING #7 SLAT UPPER SURFACE I/B SIDE IAW B757 SRM 57-43-02-2R, REPAIR 1 AND AND B757 SRM 51-70-10-2R, IAW FEDEX E.A. T F-5750-T0348918 P1 WING - FLIGHT SURFACES - #7 SLAT TRAILING EDGE WEDGE UPPER SURFACE REPAIR - RSC TRACKING

Part: DOOR SEAL — OUT OF POSITION (L1 DOOR) · airframe 74,310 hrs · 30,949 cycles

REPEAT WRITE-UP, VERY LOUD SQUEAL FROM L1 ENTRY DOOR. INSPECTED L1 DOOR INSIDE SEAL REF AMM 52-09-01. FOUND SOME LOCATIONS OUT OFF TRACK, RESECURED AND PERFORMED OPS CHECK, OPS CHECK GOOD, SEAL AND DOOR IN NORMAL CONDITION. ACFT OK FOR SERVICE,

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 74,051 hrs · 30,796 cycles

ON APPROACH TO RUNWAY 27 KMEM, WHEN LANDING GEAR SELECTED DOWN, THE LEFT GEAR DOWN GREEN LIGHT DID NOT ILLUMINATE. DECLARED AN EMERGENCY WITH KMEM ATC, MADE LOW PASS TO ALLOW TOWER TO VISUALLY VERIFY ALL GEAR NORMAL. NORMAL LANDING AFTER VERIFYING GEAR DOWN WITH TOWER. UPON CREW DEBRIEF FOUND THAT THE LT GEAR DOWN SWITCH LIGHT WAS BURNED OUT AND WOULD NOT TEST. RELAMPED LT GEAR DOWN LOCKED LIGHT IAW AMM 33-13-00-2. LIGHT ILLUMINATED AND OPS CHECKED GOOD. AS PRECAUTION VISUALLY INSPECTED DOWN LOCK SENSORS ON MAIN AND NOSE GEAR, ALSO PERFORMED BITE TEST OF PSEU AND FOUND NO DISCREPANCIES IAW FIM 32-09 FT804 FIG 103. A/C HAS NO 30 DAY HISTORY AND IS OK TO CONTINUE SERVICE AT THIS TIME.

Part: SENSOR — DIRTY (PAX DOOR) · airframe 73,514 hrs · 30,438 cycles

DURING DESCENT THRU FL 280, RECIEVED A LEFT DOOR EICAS. NO HISTORY NOTED, PERFORMED AN ADJUSTMENT TEST OF THE DOOR, CLEANED THE SENSOR. DOOR WARNING & INDICATION CHECKED GOOD.

Part: FRAME — GOUGED (FUSELAGE) · airframe 73,418 hrs · 30,379 cycles

PUNCTURE AT FRAME STA 1440 AT STR 25L AFT CARGO. ALL WORK ACCOMPLISHED ON EA F-5310-T0338309 P1. FRAME INBOARD CHORD REPAIR BETWEEN STRINGERS S-23L AND S-26L.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,760 hrs · 29,979 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE DURING TEST. REPLACED THE LAMPS AND OPS CHECKED NORMAL IAW MM 33-51-09-3. ACFT OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 72,698 hrs · 29,945 cycles

FOUND R1 DOOR NOT ARMING SMOOTHLY. DURING MX INSPECTION, FOUND THE GIRT BAR SLIDE LEATHER BLOCKING THE R1 DOOR ARMING ROD FROM MOVING. REMOVED THE GIRT BAR CENTER ALIGNMENT PLATE AND REPOSITIONED LEATHER THEN REINSTALLED CENTER ALIGNMENT PLATE ON R1 DOOR. PERFORMED OPERATIONAL CHECKS OF THE R1 DOOR SLIDE. NO MORE DEFECTS NOTED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 72,687 hrs · 29,938 cycles

FOUND L1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW AMM 25-66-01-4. OPS CHECKED GOOD.

Part: RESERVOIR — LOW PRESSURE (L1 DOOR) · airframe 72,239 hrs · 29,683 cycles

WHILE CHANGING L1 DOOR SLIDE FOR SCHEDULED TIME CHANGE. FOUND L1 DOOR EMERGENCY POWER RESERVOIR PRESSURE OUT OF LIMITS LOW. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WINDOW HEAT) · airframe 71,767 hrs · 29,380 cycles

ON DESCENT, L1 WINDOW FOGGED ON THE INSIDE OF THE COCKPIT. UPON LANDING, OUTSIDE OF L1 FOGGED. USED WIPES TO CLEAN WINDOW ENOUGH TO TAXI AND PARK. WRI 30-40-4231, L1 WINDOW HEAT CORRECTED, WINDOW FOG FREE. ACT OK FOR SERVICE.

Part: NOT REPORTED — UNKNOWN (WARNING SYSTEM) · airframe 71,704 hrs · 29,335 cycles

DESCENDING THROUGH FL 280 GEAR NOT DOWN, EICAS WARNING ACCOMPANIED BY AURAL WARNING. THIS CONDITION CONTINUED THROUGHOUT DESCENT ANYTIME THROTTLES RETIRED TO IDLE. TROUBLESHOOTING IAW 31-51 FAULT TREE 817, FOUND PIN 3 OF THE LANDING CONFIGURATION WARNING MODULE CONNECTOR D595 TO HAVE RESISTANCE AT ALL TIME. REMOVED NR 1 FSEU & STILL HAD RESISTANCE AT PIN 3.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 71,514 hrs · 29,228 cycles

RIGHT INBD AFT FLAP UPPER SURFACE, APPROX 2 FT FROM INBD EDGE HAS AREA OF DELAMINATION. REPAIRED IAW SRM 57-53-01- 2R REP 1 FIG 201 TABLE II AND SRM 51-70-17-0G PAR 4B.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,514 hrs · 29,228 cycles

RIGHT INBD AFT FLAP MOST INBD AREA, UPPER SKIN DELAMINATED. APPLIED PERMANENT REPAIR TO RT IB AFT FLAP UPPER SKIN SURFACE IAW SRM 57-53-01- 2R REP 1 FIG 201 TABLE II AND SRM 51-70-04-0G PAR 5A2 AND SRM 51-70-17-0G PAR 4A2.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 711 hrs · 28,967 cycles

DURING CLIMB OUT, ACFT EXPERIENCED A VERY LOUD VIOLENT LIGHTNING STRIKE IN THE NOSE RADOME AREA. COCKPIT IMMEDIATELY FILLED WITH THE SMELL OF ELEC FUMES & DID NOT CEASE UNTIL AFTER LANDING, WHEN ACFT DOOR OPENED. ACCOMPLISHED LIGHTNING STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-11-2 & SMOKE OR FUMES INSPECTION IN THE CABIN & FWD MIDDLE E & E COMPARTMENTS IAW AMM 05-51-56-2. FOUND NO EVIDENCE OF ANY ELEC WIRING DAMAGE.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 711 hrs · 28,953 cycles

AT FL 360 LI WINDOW BEGAN TO ARC. COMPLIED WITH QRH. NO OVERWEIGHT LANDING. R & R NR 1 WINDSHIELD IAW MM 56-11-01-4. OPERATIONS CHECKED GOOD.

Part: WINDOW — ARCED (COCKPIT) · airframe 711 hrs · 28,953 cycles

AT FL 360 L1 WINDOW BEGAN TO ARC. COMPLIED WITH QRH. R & R NR 1 WINDSHIELD IAW MM 56-11-01-4. OPS CHECKED GOOD.

Part: WIRE — BROKEN · airframe 708 hrs · 28,819 cycles

AT 500 FT ON DEPARTURE, EICAS MSG, TAT PROBE APPEARED WITH A/T DISCONNECT. L TAT ANNOUNCED ON OVERHEAD PANEL. BOTH TAT PROBE & LAT AT MSG, DISAPPEARED AFTER LANDING. INSPECTED WIRING IAW WIRING DIAGRAM 30-33-11 PAGE 2 FOUND K203 RELAY WITH ONE WIRING BROKEN BEHIND OF K203 BASE RELAY. SMT S SYS IAW WIRING DIAGRAM 30-33-11PAGE 2. FOUND ONE WIRE BROKEN AT SYS 2 AIR & GND RELAY K203, WIRE B3, REPAIRED WIRE, RAN TEST IAW AM 30-33-00-5-0 ALL TESTS PASSED. ACFT BACK TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,180 hrs · 28,361 cycles

FOUND EMER LIGHT INOPERATIVE DURING SERVICE CHECK AFT OF R1 DOOR. R & R RT EMER BATTERY PACK POWER SUPPLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,738 hrs · 28,082 cycles

BOTH FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RE-LAMPED EXTERIOR SLIDE LIGHTS IAW MM 33-51-06-2-1. BOTH OPERATIONS TESTED GOOD.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 69,738 hrs · 28,082 cycles

EMERGENCY LIGHT WILL NOT TEST WHEN FLIGHT ATTENDANT STATION TEST SWITCH IS PRESSED. REPLACED SWITCH ASSEMBLY IAW SWPM. SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-00-5, ACFT OK FOR SERVICE.

Part: FRAME — CRACKED (BS 235) · airframe 69,709 hrs · 28,061 cycles

FORWARD E & E BAY FRAME CRACKED AT BS 235 BL 0. REMOVED DAMAGE. FABRICATED REPAIR ANGLE & INSTALLED IAW EA F-5310 T0 305612 P1.

Part: PANEL — MISSING (THRUST REVERSER) · airframe 69,676 hrs · 28,035 cycles

LEFT ENGINE OTBD THRUST REVERSER HAS SURFACE SKIN PANEL MISSING FROM TOP TO BOTTOM NEAR THE REVERSER TRAILING EDGE. OUT OF LIMITS IAW AMM 78-31-23-6. R & R LT ENGINE LT OTBD TRANSLATING SLEEVE IAW AMM ATA 78-31-23-4. ADJUSTED & OPS CHECKED GOOD IAW AMM ATA 78-31-00-5-1.

Part: FLEX LINE — LEAKING (BRAKE SYSTEM) · airframe 69,101 hrs · 27,662 cycles

DURING ACFT BLOCK IN, FOUND NR 4 BRAKE SMOKING AND LEAKING HYD ON THE GROUND. FURTHER TROUBLESHOOTING FOUND NR 4 BRAKE FLEX LINE LEAKING. NO RESTRICTION. INSTALLED NEW BRAKE LINE AS REQUIRED. LEAK CHECKED GOOD. IAW MM 20-10-10-4.

Part: LAMP — INOPERATIVE (ESCAPE SLIDE) · airframe 68,864 hrs · 27,504 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP AT R1 DOOR SLIDE IAW MM 33-16-02-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,563 hrs · 27,269 cycles

DURING POST FLIGHT INSPECTION, FOUND RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. LAMPED RT EXTERIOR EMERGENCY LIGHT. OPS CHECKED NORMAL REF AMM 33-50-06 33-51-06, 201 AND 33-50-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,563 hrs · 27,269 cycles

DURING POST FLIGHT INSPECTION, FOUND RT EXTERIOR EMERGENCY LIGHT INOPERTIVE. LAMPED RT EXTERIOR EMERGENCY LIGHT. OPS CHECKED NORMAL REF AMM 33-50-06 33-51-06, 201 AND 33-50-00, 33-51-00, 501.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,521 hrs · 27,246 cycles

ON WALK AROUND, FOUND R1 DOOR SLIDE LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT POWER SUPPLY M370 HAD NO OUTPUT TO R1 DOOR SLIDE LIGHT. CLEANED CORROSION FROM R1 DOOR SLIDE LIGHT ASSY CONTACTS AND REPLACED POWER SUPPLY BATTERY CHARGER. OPS CHECKED NORMAL, WORK ACCOMPLISHED REF MM 33-51-06-2-1 AND 33-51-07-2.

Part: BEARING — MALFUNCTIONED (L1 DOOR) · airframe 68,504 hrs · 27,236 cycles

L1 DOOR UNABLE TO OPEN FROM OUTSIDE. REPLACED BEARING & BUSHING ON L1 OUTER DOOR ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,504 hrs · 27,236 cycles

R1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: SUPPORT BRACKET — LOOSE (L1 DOOR) · airframe 68,393 hrs · 27,167 cycles

L1 DOOR WILL NOT CLOSE. APPEARS TO BE OUT OF RIG. FOUND BOLTS ON LOWER SUPPORT BRACKET FOR THE GUIDE ARM LOOSE ON THE L-1 DOOR. ADJUSTED BRACKET AND RETORQUED BOLTS REF AMM 52-11-04-02 AND 52-11-00-5. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: ROD — MALFUNCTIONED (PAX DOOR HANDLE) · airframe 68,346 hrs · 27,139 cycles

RT ENTRY DOOR SLIDE PLACARD IS PROTRUDING WHEN IN DISARM POSITION. ALL OTHER INDICATIONS SHOW SLIDE DISARMED. REMOVED LOWER AND MID INTERIOR CORES AND DOOR HANDLE REPLACED ROD ASSY AND TESTED PER MM 52-11-00-216-025. OPS CHECKED GOOD, NO RIGGING OR ADJUSTMENTS INVOLVED REINSTALLED INTERIOR COVERS AND DOOR HANDLE. OK FOR SERVICE.

Part: ELBOW — LEAKING (PITOT TUBE) · airframe 68,340 hrs · 27,135 cycles

ON TAKEOFF DISCREPANCY BETWEEN CAPTAIN`S AIRSPEED AN F/O AIRSPEED OF 40KIAS. REJECTED T/O AT 100KIAS BASED ON F/O AIRSPEED INDICATOR. CLEARED RWY & PERFORMED RTO CHECKLIST. BRAKE COOLING TIME OF 51 MIN. FOUND CAPT'S PITOT TUBE CLOGGED WITH ORGANIC MATTER. R & R CAPTAIN'S PITOT TUBE AND OPS TESTED BAD DUE TO LEAKS. FOUND LEAK AT 1ST ELBOW DOWN STREAM FROM CAPTAIN'S PITOT TUBE. R & R ELBOW AND ALL OPS TESTS GOOD. CAPT'S AND F/O'S AIRSPEED INDICATIONS ARE GOOD. ALSO FLUSHED CAPT'S PITOT LINE--NO OTHER DEBRIS FOUND. AMM 34-11-01-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: CONTROL VALVE — INOPERATIVE (RT A/C PACK) · airframe 68,188 hrs · 27,035 cycles

RT PACK TRIPPED OFF ON DECENT LEAVING FL 350 (LT PACK IS STILL MEL'D) FOLLOWED QRH, EMERG DECENT TO 10,000", RT PACK CYCLED ON AND OFF REST OF FLIGHT. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL AND SHUTOFF VALVE IAW MM 21-51-01-2 AND REMOVED AND REPLACED RIGHT FLOW CONTROL CARD ASSEMBLY IAW MM 21-51-09-4. PERFORMED COOLING PACK SYSTEM- ADJUSTMENT/TEST IAW MM 21-51-00-5. COOLING PACK SYSTEMS OPS CHECKS GOOD, OK FOR SERVICE.

Part: FRAME — DAMAGED (ZONE 200) · airframe 68,155 hrs · 27,008 cycles

RIGHT UPPER LOBE FUSELAGE BS 1140 HAS FOUR ELONGATED HOLES AT BS 1140, STR 16R, STRINGER REPAIR WAS ACCOMPLISHED, ON STAM NR 47327410001 AND STAM EA 757-5341-16-F3583, REV -, DATED FEB 11, 2012. "MAJOR REPAIR."

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,155 hrs · 27,008 cycles

FOUND SCRIBE LINE AT S26L FROM BS 661.156 TO BS 662.312 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, FUSELAGE-PLATES AND SKINS-AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,155 hrs · 27,008 cycles

FOUND SCRIBE LINE AT S-26L FROM BS 659.812 TO BB 661 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, "FUSELAGE PLATES AND SKINS- AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"

Part: STRINGER CLIP — DAMAGED (ZONE 200) · airframe 68,155 hrs · 27,008 cycles

STRINGER CLIP AT STA 1640,STR 26R HAS A OVERSIZED FASTENER HOLE. REPAIRED IAW EA NR 757-5361-16-F3621 REV AND STAM NR 47327520001 REF 8110-3.

Part: SKIN — DENTED (BS 1715 S16L) · airframe 68,155 hrs · 27,008 cycles

FUSELAGE SKIN BS 1715, S 16L IS DENTED.

Part: SKIN — DENTED (BS 1715) · airframe 68,155 hrs · 27,008 cycles

FUSELAGE SKIN BS 1715, S 15L IS DENTED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 68,155 hrs · 27,008 cycles

PANEL RACK NR 2 PYLON BULL NOSE PANEL CRACKED AT AFT END, BY RUB SEAL. REMOVED SKIN IAW SRM 51-40-02. FABRICATED NEW SKIN IAW EA F-5710-156984. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 114N1802. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (L2 DOOR) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

L2 DOOR CUTOUT LOWER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL 3, PAGE 106. R & R CHORD ASSY IAW SRM 51-40-02, AND DWG 143N8328. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 418-440) · airframe 68,155 hrs · 27,008 cycles

CREASE BEAM AT S-17R BET BS 418 TO BS 440 INNER CHORD HAS CORROSION. REMOVED CORROSION BY BLENDING IAW SRM 51-10-02. CHECKED LIMITS ORIG MATERIAL WAS .071 AFTER REWORK = .049, FOUND OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 425-430) · airframe 68,155 hrs · 27,008 cycles

FUSELAGE SKIN AT BS 425-430, STR -24L MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, AT BS 425-430, S24L. CAT "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 395) · airframe 68,155 hrs · 27,008 cycles

SKIN AT BS 395, S17R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 316, CAT "B" MAJOR REPAIR.

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

LEFT NACELLE STRUT PANEL 433GR CUT OUT INTERNAL SURFACE CORRODED. REMOVED CORROSION IAW SRM 54-50-01; BEFORE: .130", AFTER: .070", LOSS: .060", FOUND OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL 3. R & R SKIN IAW DWG 311N5193, AND SRM 51-40-02. MAJOR REPAIR.

Part: BUTT JOINT — GOUGED (BS 1621) · airframe 68,155 hrs · 27,008 cycles

UPON REMOVAL OF SEALANT FROM BUTT JOINT, FOUND VERTICAL SCRIBE LINE ON BUTT JOINT STRAP SURFACE AT BS 1621 FROM APPROX S-10 L THROUGH S-14L. REMOVED SPLICE PLATE AT STA 1621 BETWEEN S-10L TO S-14L IAW SRM 51-40-02. FABRICATED NEW SPLICE PLATE AT STA 1621 BETWEEN S-10L TO S-14L FROM 2024-T3 .090 MATERIAL BATCH NR 0002044224 AND IAW DWG 146N3810. INSTALLED NEW SPLICE AT STA 1621 BETWEEN S-10L TO S-14L IAW SRM 51-40-02 AND DWG 146N3810. MAJOR REPAIR

Part: FRAME — MISREPAIRED (BS 1480) · airframe 68,155 hrs · 27,008 cycles

FRAME MISREPAIRED REPAIR AT BS 1480 S24-26L. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1030. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1621) · airframe 68,155 hrs · 27,008 cycles

UPON REMOVAL OF SEALANT FROM BUTTJOINT FOUND VERTICAL SCRIBE LINE ON BUTT JOINT STRAP SURFACE AT BS 1621 FROM APPROX S-14L, THROUGH S-16L. HFEC INSPECTION OF SCRIBE LINE IAW NDTM53-30-09, NO CRACKS NOTE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 5, FIG 101, SHEET 6. REMOVED BUTT SPLICE IAW SRM 51-40-02. FABRICATED NEW BUTT SPLICE IAW DWG 146N3700. INSTALLED NEW BUTT SPLICE, IAW SRM 51-40-02, AND DWG 146N3700. MAJOR REPAIR (CAT. "A")

Part: FRAME — MISREPAIRED (BS 1340) · airframe 68,155 hrs · 27,008 cycles

EXISTING FRAME REPAIR AT BS 1340, STR 22R-26R MISREPAIRED. REMOVED AND REPLACED FRAME AND SPLICE BS 1340 IAW SRM 51-40-02 AND DRAWING146N1028. MAJOR REPAIR.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 68,155 hrs · 27,008 cycles

LEFT WING INBD FLAP UPPER SURFACE AT MAIN FLAP STA 200 HAS AN AREA WITH SIGNS OF DELAMINATION. REPAIRED IAW SRM 51-70-10, REPAIR NR 4. REF EA F-5750-147773. MAJOR REPAIR.

Part: BEAM — CHAFED (CARGO DOOR) · airframe 68,155 hrs · 27,008 cycles

FWD CARGO DOOR LOWER AFT CORNER EDGE BEAM HAS CHAFING AND GOUGE. REMOVED CHAFING IAW SRM 52-30-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 52-30-02, FIG. 101, DETAIL 1 & 2; BEFORE: .050", AFTER: .037", LOSS: .017". REMOVED LOWER AFT CORNER IAW SRM 51-40-02. RECEIVED NEW CORNER ON BATCH NR 0002125683. INSTALLED NEW LOWER CORNER EDGE BEAM IAW SRM 51-40-02, AND DWG 654N0244, AT FWD CARGO DOOR LOWER AFT CORNER. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK, BS 1540-1640, LBL 45.5 GOUGED AND CORRODED. BLENDED SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 1, PAGE 102, AND FOUND TO BE OUT OF LIMITS, ORIG: .145", AFTER: .117", LOSS: .028". REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 53-60-52. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1628-1685) · airframe 68,155 hrs · 27,008 cycles

FOUND GOUGES, SCRIBE LINES, CORROSION ON SKIN AT BS 1625 TO 1685, S17-18R. UNDER SCUFF PLATE.

Part: INTERCOSTAL — CORRODED (BS 1540-1560) · airframe 68,155 hrs · 27,008 cycles

UPON REMOVAL OF AFT PIT FRAME FOUND INTERCOSTAL CORRODED STA 1540-1560, BETWEEN S26L AND S26R.

Part: FILL PORT — CORRODED (FUEL CELL) · airframe 68,155 hrs · 27,008 cycles

LT WING TANK OVERWING FILL PORT FAILED FUNCTIONAL BONDING CHECK.

Part: FRAME — MISREPAIRED (BS 1420 S24-26L) · airframe 68,155 hrs · 27,008 cycles

FRAME BS 1420 S24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028.

Part: SKIN — DENTED (BS 1390-1410) · airframe 68,155 hrs · 27,008 cycles

FUSELAGE SKIN CREASED BS 1390-1410 S15-16L.

Part: FRAME — MISREPAIRED (BS 1400) · airframe 68,155 hrs · 27,008 cycles

FRAME AT BS 1400, STR 24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028. MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (BS 900-1040) · airframe 68,155 hrs · 27,008 cycles

MAIN DECK CREASE BEAM BS 900-1040 RT HAS AN ELONGATED HOLE. REMOVED EXISTING CREASEBEAM IAW SRM 51-40-02. . LOCATED, DRILLED AND INSTALLED NEW CREASEBEAM IAW SRM 51-10-02. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT PER AMM 51-00-07. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1397-1401) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

MAIN CABIN SEAT TRACK, BS 1397-1404, RBL 45.50 UPPER SURFACE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-02, FIG.101, SHEET 2 OF 6. REMOVED SEAT TRACK IAW SRM 51-40-02. INSTALLED NEW SEAT TRACK, BS 1320-1540, RBL 45.50, PER SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 68,155 hrs · 27,008 cycles

FUSELAGE SKIN JUST AFT OF BS 660 TO 675 S20-23L HAS WRINKLING/BUCKLING. REPAIRED IAW SRM 51-40-02 & 53-00-01, REPAIR 16. MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED · airframe 68,155 hrs · 27,008 cycles

MAIN CABIN DECK PLATE STA 1681.8 TO STA 1720 BL-0 TO RBL-58 HAS SEVERAL AREAS OF CORROSION. R & R MAIN CABIN DECK PLATE, BS 1681-1720, RBL 58 - LBL 58, IAW SRM 51-40-02.

Part: FRAME — MISREPAIRED (BS 1500) · airframe 68,155 hrs · 27,008 cycles

FRAME BS 1500, STR 24-26L MISREPAIRED. REMOVED FRAME IAW SRM 51-40-02. INSTALLED NEW FRAME IAW SRM 51-40-02, AND DWG 146N1030.

Part: SEAT TRACK — CORRODED (BS 1180-1280) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

MAIN CABIN SEAT TRACK, BS 1180 TO 1280, RBL 45.50 HAS SEVERAL AREAS OF BARE METAL AND CORROSION. BLENDED CORRODED AREAS PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK PER SRM 51-40-02, AND DWG 146N5133. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-680) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK AT STA 440-530, LBL 45 NICKED, GOUGED & HAS SURFACE CORROSION. BLENDED AREAS IAW SRM 51-10-02. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, FIG 101, PAGE 102. R & R SEAT TRACK AT LBL 45.50, BS 440-680, IAW SRM 51-40-02, 53-30-52, DETAIL 3, FIG.1, AND DWG 143N5090. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1220) · airframe 68,155 hrs · 27,008 cycles

MAIN CABIN SEAT TRACK BS 1220, RBL 24.75 UPPER LOBES GOUGED. GOUGE BLENDED IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I, PG 102. ORIGINAL MATERIAL 0.145 LOSS 0.024 REMAINING 0.021. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW SRM 53-60-52, FIG 1, PAGE 2. LOCATED AND DRILLED IAW SRM 51-40-05 & 51-10-02. INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 68,155 hrs · 27,008 cycles

MAIN CABIN FLOORBEAM STA 1661 BL 0 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. R & R FLOORBEAM IAW SRM 53-60-51, AND DWG 146N5180. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 68,155 hrs · 27,008 cycles

FRAME AT BS 1320 STR 22L- 26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1028.

Part: FRAME — MISREPAIRED (BS 1440) · airframe 68,155 hrs · 27,008 cycles

FRAME MISREPAIRED REPAIR AT BS 1440, S24-26L. R & R FRAME IAW SRM 51-40-02, AND DWG 146N1028. MAJOR REPAIR.

Part: FLOORBEAM — BENT (BS 879) · airframe 68,155 hrs · 27,008 cycles

FLOORBEAM, STA 879 BL 0, BENT. FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, PAGE 101. REMOVED AND REPLACED FLOORBEAM PER SRM 51-40-02 AND DWG 143N5072.

Part: FRAME — MISREPAIRED (BS 1540) · airframe 68,155 hrs · 27,008 cycles

FRAME AT BS 1540, STR 24L-26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1030.

Part: SEAT TRACK — DAMAGED (BS 365-418) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK AT BS 365-440, RBL 45.50 HAS NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK. ORIGINAL: .080", REMAINING: .062", FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7, PAGE 104. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02 AND DWG 141N5131. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (BS 365-440) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

MDC SEAT TRACK AT BS 365-440 RBL 24.75 HAS SEVERAL NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK, ORIGINAL MATERIAL .080", MATERIAL REMOVED .021", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101, DETAIL VII, PAGE 104. REMOVED AND REPLACED SEAT TRACK IAW DWG 141N5131, & SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1681.8) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

FLOORBEAM UPPER TEE IS CORRODED BS 1681.8, LBL 25. CORROSION OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-60-51 AND DWG 146N5091. INSTALLED IAW SRM 51-40-02 AND DWG 146N5091. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (BS 879-900) · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK BS 879-900 LBL 24 NICKED & GOUGED. BLENDED DAMAGE IAW SRM 51-10-02 AND FOUND OUT OF LIMITS PER SRM 53- 00-52 FIG.101, DETAIL 1, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02, AND DWG 143N5481. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 440-680) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK BS 440-570 LBL 24.75 NICKED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 & 53-00-52. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

FLOORBEAM BS 1640, BL15L-R CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-60-51, AND DRAWING 146N5180. FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3, PAGE 103. MAJOR REPAIR.

Part: GATE — GOUGED (L4 DOOR) · airframe 68,155 hrs · 27,008 cycles

L4 DOOR LOWER GATE OTBD FWD AND AFT CORNERS GOUGED. REMOVED DAMAGE AND CHECKED LIMITS OF DAMAGE IAW SRM 52-10-02, SRM 51-10-02. OUT OF LIMITS FOR DAMAGE IAW SRM 52-10-02, FIG 101, DETAIL V. R & R L4 DOOR LOWER GATE AND OPS CHECKED IAW AMM 52-11-38, AMM 52-11-01, AMM 52-11-00. OPS CHECKED/ADJUSTED GOOD. ORIG MATERIAL .160 AFTER REWORK .108 DEPTH .052. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1320-1540) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEAT TRACK, BS 1320-1540, LBL 45.50 GOUGED AND CORRODED. BLENDED SEAT TRACK IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1300-1320) · airframe 68,155 hrs · 27,008 cycles

CREASEBEAM BS 1300-1320 LBL 58.22 CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 8, P 105. R & R CREASEBEAM IAW SRM 51-40-02, AND DWG 146N8322. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1180-1240) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

SEC 41 SEAT TRACK BS 1180-1240, LBL 24.75 GOUGED AND CORRODED. BLENDED AREA ON SEAT TRACK PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1, PAGE 102. ORIGINAL MATERIAL: .145", LOSS: .058:, REMAINING: .087". REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK PER SRM 53-00-52, FIG. 1, PAGE 2. INSTALLED NEW SEAT TRACK PER SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 377-440) · airframe 68,155 hrs · 27,008 cycles

MCD STA 377-440 AT LBL 45.50 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. R & R SEAT TRACK IAW-SRM-51-40-02. REMOVED CORR0SION FROM SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS ORIG MATERIAL WAS .070, AFTER REWORK .052, TOTAL MATERIAL LOSS WAS .028, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-52, FIG 101, DETAIL VII. MAJOR REPAIR CAT A REPAIR.

Part: SEAT TRACK — CORRODED (BS 377-440) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

MDC AT STA 377-440 LBL 24.45 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7; BEFORE: .050", AFTER: .030", LOSS: .020". MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,155 hrs · 27,008 cycles

FLOORBEAM AT STA 365, RBL25 UPPER TEE CORRODED. REMOVED CORROSION ORIG MAT .125, AFTER BLEND .108, TOTAL MAT REMOVED .017, MAT. FOUND TO BE OUT OF LIMITS IAW SRM-53-00-51, FIG 101, DET III, REPAIRED FLOORBEAM IAW-SRM-53-00-51, FIG 201 REPAIR B NR 3. MAJOR REPAIR.