N788FD

Part: SKIN — DENTED (ZONE 300) · airframe 77,004 hrs · 30,523 cycles

RH HORIZONTAL STAB FRONT SPAR UPPER SURFACE HAS A DENT (STA 86.600) FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 86.600, OUT OF LIMITS DIM A=1.500", Y=0.069", A/Y=21.73 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4

Part: SKIN — DENTED (ZONE 300) · airframe 77,004 hrs · 30,523 cycles

RH HORIZONTAL STAB FRONT SPAR UPPER SURFACE DENT STA 159.248 APPROX FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 159.248 OUT OF LIMITS DIM A= 1.500" Y=0.054" A/Y=27.77 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I, NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4

Part: SKIN — CORRODED (ZONE 100) · airframe 77,004 hrs · 30,523 cycles

AFT POTABLE WATER SERVICE DOOR PAN POSSIBLE CORROSION STA 1681 TO STA1701 BTW STRINGERS 26R TO STR 29R COMPLIED WITH FEDEX EA F-5330-T0385436 P1 TITLE: FUSELAGE-PLATES AND SKINS-AFT LAV PAN CUT OUT SKIN CORROSION REPAIR. MAJOR REPAIR.

Part: RESERVOIR — EMPTY (ZONE 800) · airframe 76,698 hrs · 30,295 cycles

L1 DOOR EMERGENCY POWER ASSIST RESERVOIR GAUGE SHOWS EMPTY. REMOVED AND REPLACE DTHE L1 DOOR EMERGENCY POWER RESERVOIR IN REF TO AMM 52-11-30-4. A/C OK FOR SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

CRACK FOUND AT FRAME 1640 RIGHT HAND SIDE COMPLIED WITH ALL STEPS 1-16 OF E.A. TF-5310-T0377033 P1 AND COMPLETED "FUSELAGE- MAINFRAME-STA 1640 FRAME, SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20R-EO F-5310- E0367020 A CRACK INDICATION REPAIR-PARTIAL FRAME REPLACEMENT, MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 FLOORBOARD 221AF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221AF ON VTMAE TRAVELER # T23/1718653 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221MBF ON VTMAE TRAVELER # T23/1718650 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 COURIER FLOORBOARD 222AF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222AF ON VTMAE TRAVELER # T23/1718647 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 COURIER FLOORBOARD 222BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222BF ON VTMAE TRAVELER # T23/1718643 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 FLOORBOARD 222MAF ON VTMAE TRAVELER # T23/1718633 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 75,979 hrs · 29,765 cycles

ZONE 220 COURIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221BF ON VTMAE TRAVELER #T23/1718651 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 75,977 hrs · 29,764 cycles

L/H SLIDE LIGHT DOES NOT TURN ON. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR L/H SLIDE LIGHT, REF. AMM 33-51-07-2. L/H SLIDE LIGHT OPS CHECK NORMAL, REF. SAME. OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,975 hrs · 29,762 cycles

PDIS 788 26-12 6589 03NOV23 BHM FACT U DESCENDING THROUGH 12000 MSL RECEIVED MAIN CARGO FIRE EICAS MESSAGE AND INDICATIONS. INDICATIONS WENT AWAY WHILE RUNNING QRH. AFTER LANDING RECEIVED EQUIPT OVERHEAT. EMERGENCY DECLARED. ***EMERGENCY DECLARED*** FACT 03NOV23 14:36 BHM U AMM: 26-16-30-5 UPON ARRIVAL CONFIRMED NO EVIDENCE OF SMOKE OR FIRE. PERFORMED SEVERAL TEST WITH NO FAULTS IAW 757 A.M.M. 26-16-30-5 SYSTEM CK'S GOOD. THE A/C WAS CARRING ALMOST 1000 LBS OF DRY ICE IN POS 4 WHICH IS BELIEVED TO SET OFF THE ALARM. OK TO CONTUNE SERVICE AT THIS TIME .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,954 hrs · 29,029 cycles

RT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND BATTERY CHARGER PER AMM 33-51-07-2. SYSTEM OPS NORM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,954 hrs · 29,029 cycles

RT DOOR SLIDE EMERGENCY LIGHT INOP. FACT 04JUN22 18:56 GJT REF WRI 25-60/5466. REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND BATTERY CHARGER PER AMM 33-51-07-2. SYTEM OPS NORM.

Part: NONE — NONE (N/A) · airframe 74,570 hrs · 28,768 cycles

STRINGER SPLICE AT STA 1464 , STR29L , REQUIRES REPLACEMENT ACCOMPLISHED FEDEX EA# F-5310-T0365675-P1 ;FUSELAGE -,MAIN FRAME - STRINGER ,STA 1430-1460 , S29L,SPLICE REPAIR AND STA1460 - STA1489 STRINGER AND STRINGER SPLICE REPAIR IAW B757-200 SRM 53-00-03-2R FIGURE 201 SHEET 6 AND BAC DWG 146N3400 REV. E

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,570 hrs · 28,768 cycles

AFT CARGO LOWER FRAME CORRODED AT STA 1460 BL0 TO RBL 4.5 ACCOMPLISHED FEDEX EA # F-5310-T0365644-P1 , FUSELAGE MAIN FRAME , S28L TO S28R SPLICE REPAIR

Part: BRACKET — CRACKED (N/A) · airframe 74,570 hrs · 28,768 cycles

EMPENNAGE INTERIOR ABOVE CENTER SECTIONAPU INLET DUCT LOWER SUPPORT BRACKET CRACKED AT BS1864 REMOVED BRACKET , INSTALLED SERVICEABLE BRACKET IAW B757 SRM 51-40-02-0G

Part: BRACKET — CRACKED (N/A) · airframe 74,570 hrs · 28,768 cycles

SUPPORT BRACKET AT STA 1864 FOR APU INLET DUCT ,CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 353N1043 REV A AND BOEING DWG # 353N1001 REV F

Part: FITTING — DAMAGED (N/A) · airframe 74,570 hrs · 28,768 cycles

R/H ELEVATOR TIP FITTING HAS ELONGATED HOLES UNDER STATIC WICK BASE REPAIRED PER FEDEX EA #F-5520-T0365567-P1

Part: PANEL — DELAMINATED (N/A) · airframe 74,570 hrs · 28,768 cycles

R/W I/B L/E PANEL 611KT HAS COMPOSITE DAMAGE ON THE INNER SURFACE@ CORNER REPAIRED PER FEDEX EA # F-5730-T0365459-P1

Part: SLAT — DELAMINATED (N/A) · airframe 74,570 hrs · 28,768 cycles

#6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED SLAT PER B757 AMM 27-81-01-4

Part: DOOR — UNKNOWN (ZONE 800) · airframe 74,570 hrs · 28,768 cycles

R2 DOOR UPPER HINGE CUT OUT REPAIR HAS INCORRECT AND MISSING FASTENERS INSTALLED IAW B757 SRM 52-10-02-2R REMOVED AND REPLACED FASTENERS FOR R2 DOOR UPPER HINGE CUT OUT REPAIR IAW B757-200 SRM 52- 10-02-2R, FIG 201, REPAIR 1, DETAIL III

Part: NONE — NONE (ZONE 500) · airframe 74,570 hrs · 28,768 cycles

#4 SLAT SHOWS SKIN TO CORE DISBONDING REMOVED AND REPLACED #4 SLAT AND OPS TEST PER B757 AMM 27-81-02-4

Part: NONE — NONE (N/A) · airframe 74,570 hrs · 28,768 cycles

#8 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #8 SLAT AND OPS TEST IAWB757 AMM 27-81-02-4

Part: NONE — NONE (N/A) · airframe 74,570 hrs · 28,768 cycles

#7 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #7 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOOD.

Part: FRAME — GOUGED (N/A) · airframe 74,570 hrs · 28,768 cycles

EMPENNAGE INTERIOR BELOW CENTER SECTION BILGE AREA FRAME HAS A GOUGE AT BS 1844 RBL 5 REPAIRED PER B757 SRM 51-70-11-OG

Part: NONE — CORRODED (N/A) · airframe 74,570 hrs · 28,768 cycles

R/H ELEVATOR TIP UPPER AND LOWER PLATES ARE CORRODED FABRICATED NEW PLATES PER BOEING DWG # 183N2007 REV A

Part: NONE — CRACKED (N/A) · airframe 74,570 hrs · 28,768 cycles

#1 ENG I/B SIDE CORE COWL SPRING SEAL IS CRACKED APPROX 12"AFT OF THE FWD EDGE REMOVED AND REPLACED PER BOEING DWG # 311N3570 REV Y

Part: DEFLECTOR — CRACKED (N/A) · airframe 74,570 hrs · 28,768 cycles

#1 ENG I/B CORE COWL LOWER LONGERON FWD EDGE SUBSTRUCTURE IS CRACKED REMOVED AND REPLACED DEFLECTOR PER BAC DWG # 314N3210 REV H AND B757 SRM 51-40-02-0G

Part: NONE — NONE (N/A) · corrosion level 2 · airframe 74,570 hrs · 28,768 cycles

MAIN CABIN RH SIDE AT THE R4 DOOR ENTRANCE STA 1660 UPPER SURFACE OF THE DOOR SILL WEB IS CORRODED REMOVED DAMAGE FROM UPPER SURFACE OF DOOR SILL WEB, STA 1660 RBL 52, ORIGINAL MATERIAL .071, MAT REMOVED .O07", MATERIAL REMAINING .064" , FOUND TO BE WITHIN LIMITS PER B757-2 SRAM 53-60-15-1A FIG 101 DET VIII, REMOVED AND REINSTALLED FASTENERS PER B757-2 SRM 51-40-02 AND VTMAE DWG 11864170 REV B RESTORED FINISH PER B 757 SRM 51-20- 01-0G

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,126 hrs · 27,758 cycles

L1 DOOR EXTERIOR EMER EXIT LIGHT INOP RELAMPED L1 DOOR EXT EMER EXIT LIGHT (SLIDE LIGHT) USING LAMP P/N 767 LIGHT CHECKS GOOD. REF B757 AMM 33-51-06-2-1. OK FOR SERVICE

Part: STRAP — DENTED (BS 480) · airframe 72,994 hrs · 27,674 cycles

MAIN EQUIPMENT CENTER CEILING AREA,, MAIN FLOOR STRUCTURE ATTACH STABILIZER STRAP HAS A CRACK AT FASTENER HOLE ABOUT 1.5" LONG, BS.480 RBL. 24.75 CUT DAMAGED AT STABILIZER STRAP IAW B757 SRM 51-10-02-0G AND SRM 53-00-51-2R FIG 201 DETAILV REP 12, FABRICATED REPAIR PARTS FILLER AND STRAP IAW B757 SRM 53-00-51-2R REP 12 INSTALLED REPAIR PARTS AT BS 480 RBL 24.75 FLOOR BEAM ATTACH STABILIZER STRAP IAW B757 SRM 53-00-51-2R REPAIR 12 FIG 201 DETAIL V

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,994 hrs · 27,674 cycles

LOWER FUSELAGE SKIN BULGE AT BS 1464 STR29L APPROX. SUSPECT OF CORROSION EVALUATED AREA AT LWR FUSE SKIN FOUND STR SPLICE CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SPLICE AS PER SRM 51-40-02-0G, 51-10-02-0G AND DWG 146N3820 REV C.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,994 hrs · 27,674 cycles

UPON REMOVAL OF APU INTAKE DUCT FOUND ANGLE CORRODED APPROX STA 1787 TO 1800 RBL6. FOUND ANGLE AT APU INTAKE DUCT TO BE 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-15. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 148N3152 REV -.

Part: SOLENOID VALVE — LEAKING (HYD SYSTEM) · airframe 72,857 hrs · 27,578 cycles

RIGHT HYD QTY EICAS MESSAGE INFLIGHT. COMPLIED WITH QRH. FOUND LEAK AT RT SYSTEM APCS ELECTROHYDRAULIC SOLENOID VALVE WHERE IT MATES TO THE SOLENOID. REMOVED AND REPLACED METAL GASKET ON SOLENOID VALVE IAW MM 22-12-02-2. PERFORMED OPS AND LEAK CHECKS. OPS CHECK GOOD AND NO LEAKS NOTED AT THIS TIME.

Part: LINER — OUT OF ADJUST (R1 DOOR) · airframe 72,196 hrs · 27,125 cycles

PDIS 788 25-60 2763 20DEC18 MEM FACT U LOGPAGES:2992755 R FWD DOOR ARMED PANEL DOSN'T EXTEND FACT 20DEC18 06:30 MEM U ADJUSTED R-1 DOOR LINING- DOOR ARMED PANEL(KNUCKLE KNOCKER) OPS CHKS GOOD- REF: B757 M/M 52-11-02-4

Part: SOCKET — SHORTED (EMERGENCY LIGHT) · airframe 71,629 hrs · 26,728 cycles

RIGHT EXTERIOR EMERGENCY LIGHT FOR R1 DOOR INOPERATIVE. REMOVED LIGHT SOCKET AND REFLECTOR FROM OUTSIDE OF AIRCRAFT AS PER SB 33-0012 IAW AMM 33-51-06-2-1. TROUBLESHOT IAW WDM 33-51-12, PG 902. FOUND GOOD POWER AND GROUND AT LIGHT ASSY L30. FOUND THAT THE LIGHT WOULD ILLUMINATE BY WIGGLING THE LIGHT ASSY SOCKET POWER TERMINAL BUT WOULD NOT STAY ON. INSTALLED THE LIGHT SOCKET AND REFLECTOR IAW AMM 33-51-06-2-1.

Part: POWER SUPPLY — BENT (EMERGENCY LIGHTS) · airframe 71,024 hrs · 26,325 cycles

RIGHT EXTERNAL EMERGENCY SLIDE LIGHT FAILED AN OPS TEST. REPLACED THE POWER SUPPLY IAW MM 33-51-07-2, OPS CHECKED OK.

Part: TORQUE TUBE — LOOSE (TE FLAPS) · airframe 69,918 hrs · 25,553 cycles

AFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 1 TO FLAPS 0, HAD EICAS MESSAGE, LE FLAP ASYM, & AMBER LIGHT LE. RETURNED TO LAND IAW QRH FAULT CODE FRM 27 90 24 00. INSTALLED TORQUE TUBE COUPLER AND OPS CHECKED LEADING EDGE SLAT SYSTEM IN REF 27-81-00-5 AND OPS RIG CHECKED GOOD.

Part: SKIN — CHAFED (RT WING) · airframe 69,849 hrs · 25,496 cycles

PANEL 655AR EXTERNAL SKIN HAS CHAFED. REPAIRED IAW EA F5750-T0320958. MAJOR REPAIR.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 698 hrs · 25,496 cycles

REWORK OF NR N00207, VERTICAL STAB LT SIDE AUXILIARY PANEL HAS DENT, 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM, DUE TO PER NOTED SRM. A VISUAL & NDT INSPECTION OF DAMAGED AREA FOR DISBONDS, DELAMINATION, IS REQUIRED PRIOR TO APPLYING REPAIR. THIS WAS NOT DOCUMENTED ACCOMPLISHED REWORK OF NR N00207. REPAIRED VERTICAL STAB LT SIDE AUXILIARY PANEL, PN 175N2001, DENT LOCATED AT FSS 170.259 IAW SRM 51-70-10-2R. REPAIR NR 2, DAMAGE IS NOT DENT, .25" DIAMETER HOLE. MAJOR REPAIR.

Part: FLAP — CRACKED (LT WING) · airframe 698 hrs · 25,496 cycles

DURING SURVEILLANCE CHECK, A CRACK WAS NOTED, APPROX 1/2", ON LT WING INBD MAIN FLAP, MID TE. REPAIRED CRACK ON LT WING INBD MAIN FLAP, MID TE, LOCATED AT TE, 111.5" OTBD OF MF STATION 74.0. PN 113N2003-47H, SN 000539, FINAL REPAIR 7.5" X 3.25". COMPLIED WITH EA F-5750-T0321427 PT 1. REPAIR PERFORMED IAW SRM 51-70-07. MAJOR REPAIR.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 698 hrs · 25,496 cycles

VERTICAL STAB RT SIDE, AUXILIARY PANEL HAS DELAMINATION, 26" FROM AUXILIARY SPAR & 120" FROM BOTTOM. REMOVED DAMAGED PANEL ASSEMBLY & INSTALLED NEW PANEL ASSEMBLY PN 175N2001-4, IAW SRM 51-40-02 & WG 175N2001, SHEET 1 AT RT SIDE VERTICAL STAB. MAJOR REPAIR.

Part: SKIN — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 69,849 hrs · 25,496 cycles

AFTER PREPARING THE REPAIR AREA ON THE VERTICAL STAB AUXILIARY PANEL DENT, FOUND A DISBONDED AREA OF APPROX 13" X 13" DUE TO CORROSION ON THE INNER SKIN. THIS DISBONDED AREA IS APPROX 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM. REPAIRED LT VERTICAL STAB AUXILIARY PANEL INNER SKIN IAW SRM 51-70-10-2R REPAIR 4. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

FUSELAGE EXTERIOR SKIN HAS DENT WITH ASSOCIATED SCRATCH, BELOW STRINGER 24R & FWD OF BS 1768. NOTED DURING EVALUATION OF NR N00049, ACCOMPLISHED EA F-5330-T0320261. FUSELAGE SKIN CREASE, GOUGE & DEEP SCRATCH DAMAGES, BETWEEN BS 1763 & BS 1773, STRINGER 24R TO STRINGER 25R. THIS IS A CAT A REPAIR, MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

FUSELAGE EXT SKIN DENT BETWEEN STATION 1380 - 1400, JUST BELOW AFT CARGO DOOR CUT OUT. ACCOMPLISHED EA F-5330-T0320147. FUSELAGE SKIN REPAIR BETWEEN BS 1380 - 1400 & NR 2 CARGO DOORWAY LOWER MAIN SILL & STRINGER 29R. THIS IS A CAT B REPAIR, MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

PITTING CORROSION RUNNING UP UNDER LAP SEAM AT STRINGER 19L, BS 753 - 780. ACCOMPLISHED EA F-5330-T0320609. CATEGORY B REPAIR, MAJOR REPAIR.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 698 hrs · 25,496 cycles

LEFT WING INBD FLAP EXTERNAL UPPER SKIN HAS PUNCTURE AT 3 LOCATIONS. REPAIRED LT WING AT 3 LOCATIONS IAW SRM 51-70-06-0G. REF EA F-5750-T0320431 ISSUED FOR TRACKING. CATEGORY A REPAIR MAJOR REPAIR.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 698 hrs · 25,496 cycles

LEFT WING INBD FLAP AFT FLAP EXTERNAL SKIN BOTTOM AREA HAS PUNCTURE ADJACENT TO CTR TRACK. REPAIRED ONE EACH PUNCTURE IAW SRM 51-70-17 IAW EA F-5750-T0320393 ISSUED FOR TRACKING. CATEGORY A REPAIR MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

FUSELAGE EXTERIOR SKIN HAS AN OUTWARD DENT, BETWEEN BS 1420 - 1440, STRINGER 24L & 25L. NOTED DURING DENT EVALUATION OF NR NOOO48, EVALUATED DENT FOUND A & Y=28.18 OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET III. REPAIRED DENT STATION 1420 - 1440, STRINGER 24L - 25L IAW SRM 53-00-01-2R R16. THIS IS A CAT B REPAIR. MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 698 hrs · 25,496 cycles

AFT PIT LT SIDE FRAME IS CORRODED AT STATION 1420, BETWEEN STRINGER 19L & 20L. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL . 063, REMAINING .052, OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET II. R & R FRAME STATION 1420, STRINGER 14L - 24L IAW SRM 51-40-02 & DWG 146N1012. MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

FUSELAGE EXT SKIN DENTS, COMBINATION INWARD & OUTWARD, BETWEEN STRINGER 27L & 28L, STATION 1580. DENTS AFTER EVALUATED FOUND OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101 DET III. REPAIRED AREA IAW SRM 53-00-01-2R REPAIR 16. CATEGORY B REPAIR, MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 698 hrs · 25,496 cycles

AFT PIT SIDEWALL LT SIDE FRAME, INNER CHORD CORRODED AT STATION 1420 BETWEEN STRINGER 19L & 18L. R & R FRAME, INNER CHORD AT STATION 1420, STRINGER 18L - 22L IAW SRM 51-40-02 & DWG 146N1012. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-02, SRM 53-00-07-1A FIG 101 DET II. CATEGORY A REPAIR, MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

AFT PIT SIDEWALL LT SIDE FRAME, INNER CHORD CORRODED AT STATION 1420, BETWEEN STRINGER 19L & 18L. R & R FRAME INNER CHORD IAW SRM 51-40-02 & DWG 146N1012. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-02, SRM 53-00-07-1A FIG 101 DET II. CATEGORY A REPAIR, MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

AFT CARGO RT FRAME AT STATION 1200, INNER CHORD, TOP SURFACES HAS CORROSIONS, FROM STRINGER 28R - 26R. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS IS 0.080", AFTER BLEND OUT, NO MATERIAL REMAINING. OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET II. R & R FRAME STATION 1200, BETWEEN STRINGER 24L & 24R IAW SRM 51-40-02 & DWG 146N1001. CATEGORY A REPAIR, MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 698 hrs · 25,496 cycles

FLOORBEAM BS 1681 IS CORRODED ON THE UPPER SURFACE . REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL VI , REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5000 . MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 698 hrs · 25,496 cycles

MAIN DECK FLOORBEAM AT BS 1661 RBL 56, HAS CORROSION AROUND FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5090. MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,845 hrs · 25,495 cycles

AFT CARGO CIRCUMFERENTIAL STRAP & FUSELAGE SKIN CORRODED BS 1400, STRINGER 27L - 28L. REMOVED PREVIOUSLY INSTALLED DOUBLER & CIRCUMFERENTIAL STRAP SPLICE SECTION. FABRICATED & INSTALLED 6 STRAIGHT SHANK FREEZE PLUGS, REPAIR DOUBLER, 146N3810-8200 SKIN SPLICE, 2 FILLERS, 4 STRAPS & SHIM FOR SHEAR TIE IAW REO G13562 REV B & UAL EVA 80616 085625PER UAL EVA 80616. THE REPAIR AT BS 1385 - 1416 FUSELAGE SKIN HAS RECEIVED FIRST & SECOND STAGE APPROVAL, STATIC STRENGTH & INSPECTION THRESHOLD. A NEW FORM 8100-9 MUST BE ISSUED PRIOR TO THE INSPECTION THRESHOLD OF 72200C TOTAL AIRFRAME CYCLES. AIRPLANE SOLD AS IS ON 13 JUN 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.