N973FD

Part: SKIN — GOUGED (BS 522 S29L) · airframe 52,658 hrs · 23,875 cycles

FUSELAGE SKIN GOUGED AT STA 520 2", 3" IB OF STR 29L. MARKED WITH TAPE. 1" HOLE IN FUSELAGE REPAIRED PER 757 SRM 53-00-01 REP7.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 52,466 hrs · 23,753 cycles

L1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT PER B757-200 AMM 33-51-06-2-1, OP'S CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 52,466 hrs · 23,753 cycles

L1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT PER B757-200 AMM 33-51-06-2-1, OP'S CHECKS NORMAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,360 hrs · 23,692 cycles

UPON REMOVAL SPLICE STRAP STA 1400 FOUND CORROSION ON INTERCOSTAL BETWEEN STA 1400 - 1420 LBL 19. REMOVED INTERCOSTAL AT AFT CARGO BETWEEN STA 1400 - 1420 LBL 19 IAW B 757 SRM 51- 40-02-OG.UPON EVALUATION FOUND CORROSION 100% MAT LOSS OUT OF LIMITS IAW B 757 SRM SRM 53-00-04-1A FIG 101 DETAIL I.FORMED,TRIMMED,LOCATED,DRILLED AND INSTALLED NEW INTERCOSTAL IAW BOEING DWG # 146N5427 REV : A AND B 757 SRM 51-40-02-OG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

SHEARED / PILLOWED RIVETS STA 1400 BETWEEN STR 26L - 27L. REMOVED 3EA RIVETS AT STA 1400 BETWEEN STR 26L - 27L IAW B 757 SRM 51-40-02-OG. UPON UPON FURTHER EVALUATION FOUND SHEAR TIE AT STA 1400 BETWEEN STR 26L - 27L OUT OF LIMITS LIMITS DUE TO CORROSION WITH EXFOLIATION PRESENT IAW B 757 SRM 53-00-07-1A FIG 101 DETAIL II. FORMED,TRIMMED,LOCATED,DRILLED AND INSTALLED NEW SHEAR TIE IAW BOEING DWG # 146N1011 REV : E , INSTALLED 3EA RIVETS IAW B 757 SRM 51-40-02-OG.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN FLOOR SUPPORT ANGLE HAS AREAS OF CORROSION ON UPPER SURFACE BS 700 TO BS 720 LBL 62.5 EVALUATED CORROSION AT MAIN CABIN FLOOR SUPPORT ANGLE BS 700 TO BS 720 LBL 62.5 FOUND 100% MAT LOSS IAW B 757 SRM 51-10-02-OG. REMOVED,LOCATED,DRILLED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW B 757 SRM 51-40-02-OG AND 51-40-05-OG.

Part: SPLICE — CORRODED (FUELAGE) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

UPON REMOVAL OF SHEAR TIE STA 1400 BETWEEN S26L - S27L,FOUND CORROSION ON INTERNAL FUSELAGE SPLICE STRAP. REMOVED INTERNAL FUSELAGE SPLICE STRAP AT AFT CARGO STA 1400 BETWEEN STR 26L TO TO 27R IAW B 757 SRM 51-40-02-OG,UPON EVALUATION FOUND CORROSION 100% MAT LOSS OUT OUT OF LIMITS IAW B 757 SRM 53-00-01-1A FIG 101 DETAIL I. FABRICATED,LOCATED,DRILLED AND AND INSTALLED NEW SPLICE STRAP IAW BOEING DWG # 143N3400 REV : B,146N3810 REV : H,C AND AND B 757 SRM 51-40-02-OG.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN FLOOR PANEL SUPPORT ANGLE UPPER SURFACE HAS AREAS OF CORROSION AT BB BB BS 1020 BETWEEN BL0 AND LBL 24. ACCOMPLISH WITH FEDEX E.A.#:F-5310-T0359922 P1. TITLE: FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1020 CORRODED,NEW PART FABRICATION - TEMPER A ALTERATION.

Part: ANGLE — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN L/H FLOOR MOP SILL /CREASE WEB ANGLE HAS AREAS CORROSION ON UPPER SURFACE BETWEEN BS 795 AND BS 880. REMOVED CORROSION AT MAIN CABIN L/H CREASE WEB ANGLE "MOP SILL" ON UPPER SURFACE BETWEEN BS 795 - 880 IAW B 757 SRM 51-10-02-OG,EVALUATED AREA ORIGINAL MAT .070",MAT LOSS MORE THAN 50% FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-30-13-01 FIG 1 DETAIL III AND 53-30-13-1A FIG 101 DETAIL III.REMOVED,FABRICATED AND INSTALLED NEW CREASE WEB ANGLE,MOP SILL IAW B 757 SRM 51-40-02-OG AND BOEING DWG # 143N5520 REV: BM & E. FROM STA 750 TO 900.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN FLOOR PANEL SUPPORT ANGLE UPPER SURFACE HAS AREAS OF CORROSION AT BS 1055 BETWEEN BL0 AND LBL 24. ACCOMPLISH WITH FEDEX E.A.#:F-5310-T0359923 P1. TITLE: FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1055 CORRODED,NEW PART FABRICATION - TEMPER ALTERATION.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN L/H FLOOR MOP SILL / CREASE WEB ANGLE UPPER SURFACE HAS AREAS OF CORROSION AT BS 685 AND BS 735. REMOVED CORROSION AT MAIN CABIN L/H CREASE WEB ANGLE "MOP SILL" BETWEEN BS 685 - BS 735 IAW B 757 SRM 51-10-02-OG.EVALUATED AREA LOWEST REM .025" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-30-15-01 FIG 1 DETAIL II AND 53-30-15-1A FIG 101 DETAIL IV. REMOVED,LOCATED,DRILLED AND INSTALLED NEW CREASE WEB ANGLE "MOP SILL" BETWEEN BS 670 - BS 750 IAW B 757 SRM 51-40-02-OG & 51-40-05-OG AND B DWG # 143N8322 REV: K & REV : BG.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN BS 1200 FLOOR BEAM HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BL0 AND LBL 24. REMOVED CORROSION AT MAIN CABIN BS 1200 FLOOR BEAM ON UPPER SURFACE BETWEEN BL0 AND LBL 24 IAW B 757 SRM 51-10-02-OG.EVALUATED AREAS ORIG MAT .125" LOWEST READING .035" FOUND OUT OF LIMITS IAW B 757 SRM 53-00-51-1A FIG 101 DETAIL IV. CUT OUT DAMAGED FLOOR BEAM UPPER CHORD AT BS 1200 BETWEEN LBL 70" - RBL 10.5" DIM 81.5/8" FABRICATED AND INSTALLED NEW FLOOR BEAM UPPER TEE CHORD REPAIR. DIM 88" LONG AND REPAIR SPLICE IAW B 757 SRM 53-00-51-2R REPAIR 8 FIG 201 DETAIL II .

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN RBL 24.75 SEAT TRACK HAS AREAS OF CORROSION ON UPPER SURFACE AT BS 1320. COMPLIED WITH FEDEX EA.# :F-5310-T039848 P1. TITLE : FUSELAGE - MAINFRAME - RBL 24 SEAT TRACK REPAIR BETWEEN STA 1320 - 1340 - SRM REPAIR DEVIATION FOR ALTERNATE FINISH. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B757 SRM 51-10-02-0G AND 53- 00-52-1A FIG 101 DETAIL VII. REMOVED DAMAGE SEAT TRACK, FABRICATED, AND INSTALLED REPAIR SECTION AND SPLICE IAW B757 SRM 53-00-52-2R REP 3 - OPTION 2.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN R/H FLOOR MOP SILL / CREASE WEB ANGLE HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 1320 AND BS 1360. REMOVED CORROSION AT MAIN CABIN R/H CREASE WEB ANGLE "CHORD" ON UPPER SURFACE BETWEEN BS 1320 - 1360 IAW B 757 SRM 51-10-02-OG.EVALUATED AREA ORIGINAL MAT .100" LOWEST REM .087" MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-60-15-01 FIG 1 DETAIL II & 53-60-15-1A FIG 101 DETAIL VI. REMOVED AND REPLACED CREASE WEB ANGLE "CHORD" BETWEEN STA 1290 - 1370 P/N 146N8326U2 P.O # FS2101734 IAW B757 SRM 51-40-02-OG AND BOEING DWG 146N8326 REV : C.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 52,360 hrs · 23,692 cycles

MAIN CABIN RBL 24.75 SEAT TRACK UPPER CROWN BROKEN OFF AT BS 820. REMOVED SEAT TRACK SECTION,MAIN CABIN BETWEEN STA 780 TO 880 RBL 24.75,FOUND AREA OUT OF LIMITS IAW B 757 SRM 51-40-02-OG AND 53-00-52-1A FIG 101,FABRICATED NEW SEAT TRACK IAW BOEING DWG 143N5080 REV A,INSTALLED NEW SEAT TRACK SECTION STA 780 TO 880 RBL 24.75 IAW BOEING DWG 143N5080 REV A AND VENTURA AEROSPACE DWG # 3458 REV L.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 52,111 hrs · 23,532 cycles

EMERGENCY LIGHTS AT L1 DOOR EXIT, L1 SLIDE LIGHT AND COCKPIT EMERGENCY LIGHT INOPERABLE DURING TESTING. REPLACED AND TESTED BATTERY PACK, IAW AMM: 33-51-07-2, TEST OK.

Part: PRESSURE DECK — WORN (BS 1684-1690) · airframe 50,814 hrs · 22,625 cycles

MAIN CABIN AFT PRESSURE DECK HAS 4 EA BLEND OUTS THAT ARE OUT OF LIMITS AT APPROX. LBL.50 APPROX. STA.1684 TO STA. 1690. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK PLATE AT STA. 1684 TO STA. 1690 LBL. 50 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.

Part: PRESSURE DECK — CHAFED (BS 1708) · airframe 50,814 hrs · 22,625 cycles

MAIN CABIN AFT PRESSURE DECK HAS 1 EA BLEND OUT, OUT OF LIMITS AT STA 1708 LBL 25. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK STA.1708 LBL.25, IAW B757 SRM 53-60 60-51-2R REPAIR 2 ALTERNATIVE I.

Part: PRESSURE DECK — CHAFED (BS 1702) · airframe 50,814 hrs · 22,625 cycles

AFT PRESSURE DECK HAS BLENDS OUT AT STA 1702 RBL 25 TO RBL 33. INSTALLED DOUBLER REPAIR ON AFT DECK IN MAIN CABIN STA. 1702 RBL.25 TO RBL 33 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.

Part: PRESSURE DECK — CHAFED (BS 1689-1706) · airframe 50,814 hrs · 22,625 cycles

MAIN CABIN AFT PRESSURE DECK HAS 3 EA BLEND OUTS, OUT OF LIMITS AT APPROX STA 1689 TO STA 1706, RBL 23 TO RBL 35. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK AT STA.1689 TO STA. 1706, RBL 23 TO RBL 35 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.

Part: INLET — FAILED (N/A) · airframe 50,695 hrs · 22,551 cycles

82081 APROX 1200 FT AGL EXPERIENCED WHAT WE THOUGHT WAS A LEFT ENG COMPRESSOR STALL. HEARD A LOUD BANG SURGE IN EGT. INSTRUMENTS RETURED TO NORMAL IN A SECOND. DECLARED AN EMERGENCY AND RETURNED TO MEM REMOVED AND REPLACED LEFT ENGINE PER 7180260-01-01,5410600-00-01, 7180260-01-02, AND 2400400-01-01 . ALL REQUIRED RUNS, OPS AND LEAK CHECKS SATISFACTORY. A/C OK FOR SERVICE. COMPLETED LEFT ENGINE INLET COWL INSTALLATION REF AMM 71-11-01-4. OPS AND LEAK CHECKS GOOD. A/C OK FOR SERVICE.

Part: COVER — DAMAGED (L1 DOOR) · airframe 50,642 hrs · 22,521 cycles

MDIS 973 52-10 4805 09NOV18 AFW OPEN U RAMP REPORTED THAT L1 ENTRY DOOR HAD RUBBER FLAP HANGING DOWN WHEN DOOR OPEN. MEL 09NOV18 06:24 AFW U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 12NOV18 "MEL 52-11-01-A: L1 DOOR SL IDE - INOP." L1 DOOR SLIDE COVER LOWER RUBBER DUST AND DEBRIE SEAL RETAINER HAS PULLED ALL THE BLIND FASTNERS FROM FIBERGLASS DOOR COVER. TAPED SEAL INTO PLACE, BUT SLIDE IS INOP. WILL NEED TIME TO GLUE BLIND FASTNERS BACK INTO DOOR COVER. ITEM REMAINS ON MEL. OKAY TO CONT. END. C/7162371 PART 09NOV18 12:04 MC1 U IDENTIFIED PARTS SLIDE COVER MPN: 416N2100-723SP CPN: 2526346 QTY: 1 REMOVED AND REPLACED L1 ESCAPE SLIDE COVER PER M.M. 25-66-01-4

Part: TRANSMISSION — MALFUNCTIONED (TE FLAPS) · airframe 49,945 hrs · 22,079 cycles

ARRIVED AT 210 KIAS, FLAPS SELECTED TO 1, FLAPS DID NOT MOVE, RECIEVED TRAILING EDGE ANNUNCIATORS. USED ALTERNATE FLAPS IAW QRH. REMOVED AND REPLACED THE NR 5 FLAP TRANSMISSION. OPS TESTED GOOD IAW MM 27-51-06-4. FLAPS OPERATE NORMAL. OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 49,889 hrs · 22,050 cycles

WHEN FLAPS SELECTED TO 1, TE EDGE FLAP DISAGREE LIGHT CAME ON & FLAPS INDICATED UP. RAN QRH AND LANDED WITH FLAPS 20 PERFORMED BFIM 27-51 FT 808 FLAPS AND SLATS NOW OPERATE AND INDICATE NORMAL ALL SELECTED POSITIONS. A/C OK FOR SERVICE.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 48,938 hrs · 21,404 cycles

L1 DOOR WOULD NOT OPEN, AFTER BLOCK IN. SUSPECT DOOR WAS CLOSED IMPROPERLY WHICH WILL PREVENT DOOR OPENING FROM OUTSIDE. FOUND DEBRIS IN THE GIRT BAR FLOOR FITTINGS. CLEANED AND LUBRICATED THE FLOOR FITTINGS AND GIRT BAR IAW MM 12-21-18-3. OPENED AND CLOSED DOOR FROM INSIDE AND OUTSIDE NUMEROUS TIMES WITH NO ISSUES IAW MM 52-11-00-2. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,580 hrs · 21,170 cycles

INTERIOR R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. POWER SUPPLY, PN BPS7-3, BATTERY, PN 2013-1A, MEL 07JUN16. RELEASED FOR SERVICE IAW MEL: 33-51-01-01, CATEGORY: D EXPIRATION : 04OCT16, MEL 33-51-01-01: INTERIOR EMERGENCY LIGHTS INOPERATIVE. NEW BATTERY, NO HELP. SUSPECT POWER SUPPLY, REINSTALLED ORIGINAL BATTERY. POWER SUPPLY REF: MM 33-51-07-2. R & R POWER SUPPLY IAW AMM-33-51-07-2, LIGHT COMES ON, BUT WILL NOT STAY ON THE 15 MINUTES TO PASS OPS CHECK, IAW THE AMM THE POWER SUPPLY MUST RECHARGE FOR 16 HRS TO PASS TEST, WRI -33-50-2902 FOR TAG INFORMATION. SYSTEM OPS CHECKS NORMAL, REF AMM 33-51-07-2, OK TO CONTINUE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,580 hrs · 21,170 cycles

RIGHT EXTERIOR EMERGENCY BATTERY POWERED LIGHT INOPERATIVE. POWER SUPPLY, PN BPS7-3, BATTERY, PN 2013-1A, MEL. RELEASED FOR SERVICE IAW MEL: 33-51-02-02. MEL 33-51-02-02: EXTERIOR EMERGENCY LIGHTING SYSTEM, INOPERATIVE. BATTERY NO HELP, SUSPECT POWER SUPPLY. REF NR FOR ASSOCIATED INTERIOR INOPERATIVE LIGHT. IDENTIFIED PARTS, MPN: BPS7-3, CPN: 3312001, QTY: 1. T/S TO FAULTY POWER SUPPLY, REF: MM 3-51-07-2. DELETED PARTS, MPN: BPS7-3, CPN: 3312001, QTY: 1. IDENTIFIED PARTS MPN: 2012-1, CPN: 3311913, QTY: 1 PART. IDENTIFIED PARTS, MPN: 2013-1, CPN: 3301128, QTY: 1.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 48,476 hrs · 21,098 cycles

EXTERNAL & INTERNAL R1 DOOR EMER LIGHT INOPERATIVE. APPLIED POWER, ALLOWED POWER SUPPLY TO CHARGE IAW AMM 33-51-00-0. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-5.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 48,476 hrs · 21,098 cycles

RAMP REPORTS BROKEN LOCK IN CTR, BETWEEN POSITION 7L & 7R. ENSURE NO LOCK IS INSTALLED IN THIS POSITION. R & R BROKEN SEAT TRACK BL 0, STATION 900 TO 1080 IAW SRM 51-40-02-06. R & R BROKEN CARGO LOCK ASSEMBLY IAW SRM 51-40-02--06.

Part: GIRT BAR — OUT OF ALIGNMENT (ZONE 800) · airframe 48,398 hrs · 21,039 cycles

R1 SLIDE ARMED LIGHT DOES NOT ILLUMINATE. NO JUMP SEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. DEFERRED UNDER MEL 52-11-01-B. COULD NOT USE PREVIOUS DEFERRAL REFERENCE DUE TO STEP 3 OF THE MX ACTION FAILED.

Part: LIGHT — INTERMITTENT (ENTRY DOOR) · airframe 48,330 hrs · 20,990 cycles

THE LEFT ENTRY DOOR WILL NOT ARM. TROUBLE SHOT IAW FIM 25-66 FT 802. FOUND SLIDE LIGHT BULBS, L404 TO BE INTERMITTENTLY INOPERATIVE. R & R L404, TWO 387 BULBS IAW WDM 25-66-11 & SMP. GND TESTED GOOD MULTIPLE TIMES IAW AMM 25-66-00-0 PAR 5A. OK FOR SERVICE.

Part: SKIN — DENTED (BS 1691) · airframe 47,503 hrs · 20,403 cycles

FUSELAGE HAS A DENT AT BS 1691 JUST BELOW STRINGER 20L LAP SEAM. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND TRIPLER AND INSTALLED THE REPAIR IAW EA F-5330-T0314693 PT1.

Part: SKIN — DENTED (BS 645) · airframe 47,503 hrs · 20,403 cycles

FUSELAGE SKIN DENTED AT BS 645 JUST BELOW STRINGER 26L. REPAIRED IAW EA F-5330-T0314549 POS P1.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 46,898 hrs · 19,981 cycles

SERVICE CHECK FOUND R1 EMERGENCY LIGHT INOPERATIVE. REPLACED BULB, NO HELP. REPLACED EMERGENCY POWER SUPPLY, OPERATIONS CHECKED GOOD IAW MM 33-51-07-2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,576 hrs · 19,741 cycles

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

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,381 hrs · 19,572 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY.(M731). OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 46,336 hrs · 19,537 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-06-2-1. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 46,173 hrs · 19,430 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. FOUND 6VDC AT FLT DECK EMERGENCY LIGHT ASSY M10549, CHECKED FOR GROUND ON TERMINAL 1 NR GROUND. SUSPECT 10 OHM RESISTOR TO BE AT FAULT. R & R DOME LIGHT HOUSING.

Part: FRAME — CRACKED (ZONE 200) · airframe 46,151 hrs · 19,408 cycles

STA 377.7 BETWEEN S-8R TO S-9R FRAME IS CRACKED AROUND RIVET HOLE IN WEB OF FRAME. NON-ROUTINE FOR TRACKING PURPOSES ONLY A FRAME REPAIR WAS ACCOMPLISHED AT STA 377.7 BETWEEN S-8R TO S-9R ON STAM NR 49016710001 AND STAM EA 757-5312-16-F4012. THIS N/R IS FOR TRACKING PURPOSES ONLY. REF EA F-5310-163721. MAJOR REPAIR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 46,151 hrs · 19,408 cycles

RIGHT INBD FLAP HAS A DENT ON TOP SIDE, OTBD SIDE ABOVE FAIRING. REPAIRED IAW SRM 57-53-01 AND SRM 51-70-10 REPAIR 4. PERMENANT REPAIR ACCOMPLISHED PER EA F-5750-T0300135. MAJOR REPAIR

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 46,151 hrs · 19,408 cycles

LT ELEVATOR L/E WRAP AROUND FAIRING ON THE OTBD SIDE OF THE OTBD ELEVATOR PCU IS DAMAGED. REPAIRED LT ELEVATOR LEADING EDGE WRAP AROUND FAIRING ON THE O/B SIDE OF THE O/B PCA IAW SRM 51-70-04. DAMAGE MEASUREMENT WAS 1.00" DIAM. LOCATED BETWEEN EVEV STA 160.525 AND 172.521. ACCOMPLISHED PERMENANT REPAIR WITHOUT ANY DEVIATIONS PER EA F-5520-T0300137A. MAJOR REPAIR

Part: SKIN — DENTED (ZONE 200) · airframe 46,151 hrs · 19,408 cycles

FUSELAGE SKIN DENTED BS 418-426 BETWEEN S-8-9L. REPAIRED IAW EA 757-5311-16-F4032, REV. CAT "B" MAJOR REPAIR.

Part: SKIN — FAILED (ZONE 100) · airframe 46,151 hrs · 19,408 cycles

SKIN BS 740-760 BETWEEN S18-19L MISREPAIRED. ACCOMPLISHED EA 757-5331-16-F4077. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 46,151 hrs · 19,408 cycles

EXTERNAL FUSELAGE SKIN BS 1661-1681 BETWEEN S28L TO 28R HAS APPROX. 6 INCH CREASE. A SKIN REPAIR WAS ACCOMPLISHED IAW EA 757-5361-16-F4074, REV -. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 46,151 hrs · 19,408 cycles

EXTERNAL FUSELAGE SKIN DENTED, BS 640 BETWEEN S19 TO 20R. ACCOMPLISHED SKIN REPAIR IAW EA 757-5331-16-F4029. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 46,151 hrs · 19,408 cycles

FOUND SCRIBE LINE AT S26L LAP JOINT BS 656.687 TO BS 660.812. ACCOMPLISHED REPAIR IAW EA 757-5331-16 F3973 AND 49016670001. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 46,151 hrs · 19,408 cycles

EXTERNAL SKIN MISREPAIRED BS 535.5 BETWEEN S22 AND 23R ACCOMPLISHED EA F-5330-165118. CAT "B" MAJOR REPAIR.

Part: FRAME — DENTED (BS 800) · airframe 46,151 hrs · 19,408 cycles

DENTS ON FRAME AT BS 800 BETWEEN STR 23 & 24R. COMPLIED WITH EA F-5310-165116. MAJOR REPAIR.

Part: SKIN — DENTED (BS 365-385) · airframe 46,151 hrs · 19,408 cycles

FUSELAGE SKIN DENTED BS 365-385 BETWEEN S-17 TO 18R. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, FIG 201 REPAIR 16. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 46,151 hrs · 19,408 cycles

MAIN DECK CARGO SEAT TRACK AT BS 1640-1540 LBL 25 HAS AREAS WITH NICKS, SCRATCHES, AND CORROSION. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL III, FIG 101 SH 2. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5120. MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (BS 1040-1180) · airframe 46,151 hrs · 19,408 cycles

CREASE BEAM AT BS 1040 -1180, RBL 60 HAS EXISTING HOLES WITH SHORT EDGE DISTANCE. R & R CREASE BEAM INNER CHORD BS 1040-1180, RBL 63 IAW DWG 144N5214 AND SRM 51-40-02. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 46,151 hrs · 19,408 cycles

MAIN DECK CARGO TRACK AT BS 1540-1640, LBL 45, HAS SEVERAL AREAS WITH NICKS, SCRATCHES AND CORROSION. REMOVED CORROSION IAW-SRM-51-10-02, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-52, FIG 101 DETAIL I SHEET 2. R & R SEAT TRACK IAW-SRM-51-40-02 AND DWG 146N5130 CAT "A" MAJOR REPAIR.

Part: SKIN — DENTED (BS 1500-1520) · airframe 46,151 hrs · 19,408 cycles

FUSELAGE SKIN DENTED BS 1500 -1520 BETWEEN S24 TO 25R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01 FIG 201 REPAIR NR 7. MAJOR REPAIR.

Part: FLOORBEAM — MISREPAIRED (BS 324) · airframe 46,151 hrs · 19,408 cycles

FLOORBEAM AT BS 324 APPROX RBL 12 MISREPAIRED. REPAIRED IAW-SRM- 51-40-02 AND SRM-53-10-08, REPAIR 1. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1640) · airframe 46,151 hrs · 19,408 cycles

FLOORBEAM UPPER TEE AT BS 1640 HAS SEVERAL NICKS, SCRATCHES AND CORROSION. R & R FLOORBEAM IAW-SRM-51-40-02 AND DWG 146N5089, CAT."A" MAJOR REPAIR.

Part: RIB — CORRODED (RT WING) · airframe 46,151 hrs · 19,408 cycles

RT WING T/E AT 812, RIB WITH ATTACHED BONDING JUMPER SHOWS EVIDENCE OF CORROSION BETWEEN MATING SURFACES. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57- 51-09, FIG.101, DETAIL VI, A1. FABRICATED NEW RIB. R & R RIB IAW-SRM-51-40-02, CAT."A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 46,151 hrs · 19,408 cycles

UPPER DECK FLOORBEAM AT STA 1680 UPPER FLANGE LOWER SURFACE NUT PLATE STRIPS AT RBL 38, 46, AND 50 ARE CORRODED AND MISSING NUT PLATES. BLENDED OUT CORROSION ON FLOORBEAM UPPER FLANGE LOWER SURFACE STA 1681 RBL 38, 46, AND 50 IAW SRM 51-10-02. ORIGINAL THICKNESS ON STA 1681 FLOORBEAM UPPER FLANGE AREA .156 AFTER REWORK .038 MATERIAL LOSS .118 FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REMOVED AND REPLACED FLOORBEAM AT STA 1681 IAW DRAWING 146N5091 AND SRM 51-40-02. INSTALLED NUTPLATES ON UPPER FLANGE IAW SRM 51-40-02. MAJOR REPAIR

Part: CREASE BEAM — DAMAGED (BS 1290-1370) · airframe 46,151 hrs · 19,408 cycles

LT INBD CREASE BEAM AT BS 1370-1290 HAS NICKS, SCRATCHES AND CORROSIONS, TOP & BOTTOM SURFACES INCLUDED. R & R CREASE BEAM BS 1290-1370 IAW SRM-51-40-02 AND REF DWG 146N5590, CAT "A" MAJOR REPAIR.