N406UP

Part: VALVE — FAULTED (ZONE 400) · airframe 38,882 hrs · 26,175 cycles

ATB, CLIMB OUT PASSING 24000€™ L OIL TEMP WAS IN THE AMBER RANGE (165°) QRH COMPLETED ACCOMPLISHED AIR TURNBACK. REMOVED AND REPLACED L/H ENG AIR/OIL HEAT EXCHANGER VALVE IAW AMM 79-21-08. OPS AND LEAK CHECKS PERFORMED IAW AMM 71-00-00 NO LEAKS NOTED AND OPS CHECK GOOD. FAULT NO LONGER PRESENT ON ECPS.

Part: TAIL CONE — DAMAGED (ZONE 300) · airframe 38,866 hrs · 26,163 cycles

MAJOR REPAIR, DAMAGE ON TOP OF TAILCONE AREA BELOW RUDDER ALL STEPS OF EO-94785-REQ2 COMPLETED. THIS DEFERRAL IS NOW CLOSED.

Part: ANGLE — FAULTED (ZONE 100) · airframe 38,255 hrs · 25,799 cycles

FAULT: REFERANCE FRAME REPAIR T3F18E005ERCC, CORRECTIVE ACTION 6 & 7 SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1500 IN AFT PIT REQUIRES RII AUTHERIZATION. ACCOMPLISH REPAIR PER EA 757-5360-27-A3758, REV- PRIOR TO FURTHER FLIGHT. VERIFIED RECEIVING OF FINAL EA #757-5360-27-A3758 REV - WORKED STEPS 1 - 12 WITHOUT DEVIATIONS. RECEIVED EO-92445-REQ1 ACCOMPLISHED STEP 1 WITHOUT DEVIATIONS. REVIEWED

Part: FRAME — DAMAGED (ZONE 100) · airframe 38,255 hrs · 25,799 cycles

FAULT: Z100 STR OPEN UP FLOOR PANELS, MBA SYSTEM, SIDEWALLS, AND TRANSITION PANEL TO F.O.M FS 1500 FRAME REPAIR AT STR 26R. INSTALLED SIDEWALL PANELS 162BW, 154JW IAW B757-200 SRM 51-40-02 AND INSTALLED LOWER AFT MBA SYSTEM AFT/AFT #8 AND #9, IAW B757-200 AMM 25-57-01-404-007-001. REVIEWED

Part: FRAME — NOT REPORTED · airframe 38,254 hrs · 25,798 cycles

*SDR FILED OPEN* REF FRAME REPAIR T3F18E005ERBT, CORRECTIVE ACTION 7. - SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1460 RH SIDE IN AFT PIT REQUIRES RII AUTHORIZATION ACCOMPLISH REPAIR PER EA 757-5360-27-A3756, REV- PRIOR TO FURTHER FLIGHT.

Part: TEE ANGLE — CORRODED (ZONE 100) · airframe 38,196 hrs · 25,759 cycles

STA 1680 HAS CORROSION ON UPPER AND LOWER SURFACE OF UPPER T-CHORD

Part: TEE ANGLE — DAMAGED (ZONE 100) · airframe 38,196 hrs · 25,759 cycles

WTB LOWER STRUCTURE, T-CHORD STA 1142, LBL 60 WITH CORROSION. INSTALLED T CHORD AT STA 1142, LBL 60 IAW SRM 51-40-02. REVIEWED

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,196 hrs · 25,759 cycles

MAIN DECK FLOOR SUPPORT STRUCTURE, STA 1195 RBL 24 SEAT TRACK CORRODED. DOT 28-100 REVIEWED

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 38,194 hrs · 25,758 cycles

FLOOR PANEL 252XBF BROKEN STA 1200. FABRICATED FLOOR PANEL 252XBF USING MATERIAL P/N:5024N400001SS-G BATCH#:0000096292 I.A.W. SREO-B757-5320-9692-K.

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 38,196 hrs · 25,759 cycles

LEFT INBOARD FLAP UPPER OUTBOARD SURFACE IS DELAMINATED IN TWO AREAS. DOT AA014. REVIEWED

Part: FRAME — DENTED (ZONE 100) · airframe 38,196 hrs · 25,759 cycles

FRAME 1500 RIGHT SIDE IN AFT PIT IS DENTED. DOT AA007. REQUIRED SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF, REV 121, 53-00-07-2R-5, TABLE #3 FOR ZONE #1.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,252 hrs · 25,797 cycles

FAULT-STR-100-AGING ACFT INSP.- FLOOR BEAM AT STA 1200, FORWARD SIDE, HAS EXFLOIATION CORROSIN AROUND NUT PLATE.. DOT AA10. ACCOMPLISHED REPAIR PER VT-MAE EA 757-5360-27-A3717, REV- AND EO-91891-REQ1. REVIEWED

Part: FRAME — DENTED (ZONE 100) · airframe 38,196 hrs · 25,759 cycles

FRAME 1460 RIGHT SIDE BETWEEN S-25R AND S-27R, IN AFT PIT IS DENTED. DOT AA006. CORRECTION TO LAST STATEMENT REPAIR PER DETAIL #1

Part: SKIN — DELAMINATED (MLG DOOR) · airframe 38,196 hrs · 25,759 cycles

LEFT MLG STRUT MOUNTED DOOR LOWER AFT TRAILING EDGE IS DELAMINATED. DOT AA002. REVIEWED

Part: UNKNOWN — MISSING (EVAS) · airframe 37,895 hrs · 25,584 cycles

FO'S EVAS TEST TOOL MISSING. INSTALLED FO'S EVAS TEST TOOL AS REQUIRED

Part: LANDING GEAR — WARNING MESSAGE · airframe 37,773 hrs · 25,526 cycles

GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY FOUND LEFT SYSTEM RETURN CHECK VALVE P/N BACV10CD13 FOR THE NLG EXTENSION & RETRACTION BYPASSING. R&R BOTH LEFT SYSTEM RETURN CHECK VALVES FOR THE NLG EXTENSION & RETRACTION IAW AMM 20-11-00. PERFORMED NLG SWING PER AMM 32-34-00, OPS AND LEAK CHECK GOOD. REMOVED NLG JACK FROM A/C PER AMM 07-11-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 37,771 hrs · 25,525 cycles

**SDR FILED OPEN** GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY VERIFIED VALVE INPUT ARM ON LANDING GEAR SELECTOR VALVE INSTALLED PROPERLY PER AMM 32-31-02. <BR>CAPPED MAIN CARGO DOOR SHUTOFF VALVE, PSI REMAINED AT 1900. RETURNED TO NORMAL CONFIGURATION PER AMM 52-32-09.<BR>DISCONNECTED AND CAPPED LANDING GEAR SELECTOR VALVE LEFT HYD GEAR DOWN LINE, HYD PRESSURE READING 2900PSI WITH GEAR LEVEL IN THE DOWN POSTION. RECONNECTED LINE PER AMM 32-31-02. FURTHER TROUBLESHOOTING REQUIRED.

Part: DOOR — WARNING MESSAGE (DOORS) · airframe 36,764 hrs · 24,910 cycles

INSPECTION TYPE:N/AON LANDING WE RECIEVED A LEFT FORWARD ENTRY DOOR MESSAGEINSPECTED CREW ENTRY DOOR INDICATION PROXIMITY SWITCH AND FOUND LOWER PORTION OF SHIM TO NOT BE PROPERLY ATTACHED. RE-ATTACHED LOWER PORTION OF SHIM IAW AMM 52-71-00-420-017. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,418 hrs · 24,693 cycles

FLT DECK INTERIOR EMERGENCY LIGHTS OVER ENTRY DOOR INOP. R & R EMERGENCY EXIT LIGHT BATTERY ENTRY DOOR. OPS CK GOOD IAW AMM 33-51-01-012-002, 33-51-01-402-003. OPS CK GOOD. THIS CLEARS M793866

Part: FRAME — DENTED (BS 1360 S26L) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1360 STRINGER 26L NEEDS AN ALTERNATIVE METHOD TO INSPECT EXISTNG REPAIR PER EO# B757-5310-73926-A APPENDIX A STEP #4FOLLOWED INSPECTION METHOD PER VT MAE EA# 757-5360-27-A3047 REV- UPS EO NO: B757-5310-28011-B

Part: SKIN — DENTED (BS 436 S25L) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1FUSELAGE SKIN AT STA 434 BETWEEN S23L AND 25L HAS 2 DENTS DENT 1 IS L-1.0" W=1.030" DEPTH=.046" AND DENT 2 L=.632" W=.621" AND DEPTH=.048" MAKING THE SKIN OUT OF LIMITS PER SRM 53-00-01-1A-1 DET 3.REPAIRED SKIN PER EA# B757-5310-27-A3062 PRELIM 2

Part: FRAME — DENTED (BS 1480 S26R) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1480 AT STRINGERS 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 1

Part: FRAME — DENTED (BS 1560 S25-26R) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1560 BETWEEN STRINGERS S25R AND S26R HAS TWO DENTS ON THE UPPER FLANGE OF FRAME 1560 NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1560 PER SRM 53-00-07-2R-5 DETAIL 1

Part: FRAME — DENTED (BS 1460 S25-26L) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1460 BETWEEN STRINGERS S25L AND S26L THERE IS A .420" LONG BY .032" DEEP DENT ON THE UPPER FLANGE NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3

Part: FRAME — DENTED (BS 1300 S23-26L) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1INCOMING REPAIR ACCOMPLISHED ON FS 1300 BETWEEN STRINGERS S23L AND S26L WAS DONE PER SRM 51-70-11. CUSTOMER REQUEST TO REMOVE REPAIR AND INSTALL REPAIR PER SRM 53-00-07-2R-5 DETAIL 3REPAIRED FRAME 1300 LH PER SRM 53-00-07-2R-5 DETAIL 3 AND EA 757-5360-27-A3055

Part: FRAME — DENTED (BS 1540 S26R) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1540 1.2" O/B OF STRINGER S26R HAS A .70" LONG BY .45" WIDE BY .50" DEEP GOUGE ON THE UPPER PART OF WEB INTO THE FRAME FLANGEREPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 2

Part: FRAME — DENTED (BS 1520 S23-26R) · airframe 36,400 hrs · 24,685 cycles

INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1520 BETWEEN STRINGERS 23R AND 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 36,318 hrs · 24,632 cycles

INSPECTION TYPE:N/ARIGHT ELEVATOR LOWER SKIN PUNCTUREDREPAIRED DAMAGED SKIN IAW EO B757-5520-84504-A

Part: NONE — BROKEN (CABIN) · airframe 35,946 hrs · 24,397 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHT SWITCH GUARD IS BROKENREPLACED SWITCH GROUND. OPS TEST GOOD IAW AMM CH 33-51-08

Part: RADOME — DAMAGED (NOSE) · airframe 34,901 hrs · 23,708 cycles

EMERG DECLARED-NO EQUIP USED - LANDING UNEVENTFUL. DURING DESCENT THROUGH APPROX 15000 FT LOUD NOISE AND MULTIPLE EICAS MSG DISPLAYED DUE TO RADOME DAMAGE IAS DISAGREED AND LEFT SIDE AIR DATA SW ENGAGEDREMOVED NOSE RADOME PER MM 53 12 01 902 008 TAF 0558016 6-4-21/ INSTALLED NEW RADOME PER MM 53 12 01 902 0058 AND TESTED AIR DATA SYSTEM PER MM 34 12 00 0501 RETURNED CAPT AIR DATA SWITCH TO NORMAL. EFF SOURCE REF IPC 53 12 01 01.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 34,583 hrs · 23,518 cycles

INSPECTION TYPE:SEG4AFT CARGO STRINGER 30 STA 1200 HAS CORROSIONREPAIRED IAW 53-00-03-2R-1 REMOVED DAMAGED SECTION SPLICED IN NEW SECTION

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 34,583 hrs · 23,518 cycles

INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT, FLOOR PANEL 242XDF DAMAGEDFABBED PANEL 242XDF FROM 5024M400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 34,583 hrs · 23,518 cycles

INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XGF DAMAGEDFABBED PANEL 242XGF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 34,583 hrs · 23,518 cycles

INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XCF DAMAGEDFABBED PANEL 242XCF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K

Part: FRAME — BENT (BS 200 BULKHEAD) · airframe 33,420 hrs · 22,783 cycles

INSPECTION TYPE:SPVCHORD ON RIGHT SIDE PRESSURE BULKHEAD HAS SLIGHT BENT AT STA200 RBL37 WL200REMOVED DAMAGED AREA AND INSTALLED NEW SECTION AND REPAIRED SPLICE

Part: BULKHEAD WEB — DENTED (BS 199) · airframe 33,420 hrs · 22,783 cycles

INSPECTION TYPE:SPVFWD PRESSURE BULKHEAD WEB PART #141N2800-164 DENTED BLKHD STA199 RBL30 WL200REMOVED DAMAGE, INSTALLED FILLER AND REPAIR DOUBLER

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 32,583 hrs · 22,280 cycles

EMERGENCY LIGHT GUARD HAD A BLACK PIECE BREAK OFF. R&R THE SWITCH GUARD IAW SWPM 20-83-11, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (LT ENGINE BLEED) · airframe 32,569 hrs · 22,270 cycles

DIVERSION - L ENG BLEED OFF ILLUMINATED AFTER EAI WAS SELECTED ON DURING FLIGHT AT CRUISE FL 300. L ENG WAS FOLLOWED BY R ENG. L AND R PACK OFF. ACCOMPLISHED CHECKLIST AND DESCENDED TO 10,000 AFTER LOSS OF PRESSURE.REPLACED LT ENG HI PRESS SHUTOFF VALVE REF 36-11-07 AND LT FAN AIR TEMP SENSOR REF 36-11-17-004 AND LT FAN AIR MOD VALVE REF 36-11-16-024. LEAK AND OPS NORMAL.

Part: SKIN — DENTED (BS 520) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, DENT STA 520 S-22L DOT18-13FOUND TO BE OUT OF LIMITS DUE TO LOCATION, DENT MUST BE MORE THAN 0.5" REPAIRED PER EA #B757-5330-27-A2331

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1MCD FLOOR PANEL 231XFF DELAMINATEDFABRICATED NEW FLOOR PANEL 231XFF FROM 5024N400001SS-G BATCH# 3350636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1MCD FLOOR PNL 221XBF DELAMINATEDFABRICATED NEW PNL FROM 5024N400001SS-G, BATCH#33550626 PER SREO B757-5320-9692 K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1MCD FLOOR PNL 232 XJF DELAMINATEDFABRICATED NEW PNL 232XJF FROM 502N400001SS-G BATCH#0002379150 & 0003418355

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1MCD FLOOR PANEL 231XFJ DELAMINATEDFABRICATED NEW FLOOR PANEL 231XJF FROM 5024N400001SS-G, BATCH #3350636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1MCD FLOOR PNL 252 XTF DELAMINATEDFABBED PNL 252 XTF FROM 5024N400001SS-G, BATCH # 0003384848 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, PANEL 252XSF REQUIRES FAB. FABBED PANEL 252XSF FROM 5024N40000-G BATCH 33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, FLIGHT DECK, FLOOR PANEL 211XAF IS DAMAGED. FABBED PANEL 211XAF FROM 5024N40000-G BATCH 33550636 AND STEP CUT PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, PANEL 252XEF REQUIRES FAB. FABBED PANEL 252XEF FORM 5024N40000-G BATCH 33550636 AND STEP CUT PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, PANEL 231XCF REQUIRES FAB. FABBED PANEL 231XCF FROM 5024N40000-G BATCH 33550636 AND STEP CUT PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, PANEL 232XCF REQUIRES FAB. FABBED PANEL 232XCF FROM 5024N40000-G BATCH# 33550636 AND STEP CUT PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, MAIN CABIN FLOOR PANEL 211XAF REQUIRES FAB. FABBED PANEL 211XAF FROM 5024N40000-SS-G BATCH 33550636 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, PNL 252XUF REQUIRES FAB. FABBED PANEL 252XUF FROM 5024N40000-G BATCH 33550636 AND STEP STEP SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1, MAIN CABIN PANEL 252XDF REQUIRES FAB. FABBED PNL 252XEF FROM 5024N400001SS-G, BATCH 33550636 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XHF REQUIRES FABFABBED PNL 232XHF FROM 5024N400001SS-G, BATCH #33550636 PER SERO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3, MAIN CABIN FLOOR PANEL 222XAF REQUIRES FAB. FABBED PNL 222XAF FROM 5024N400001SS-G, BATCH 33550636 PER SERO B757-5320-6962-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3PNL 231XHF REQUIRES FABFABRICATED PNL 231XHF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 231XGF REQUIRES FABFABBED PNL 231XGF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 211XAF REQUIRES FABFABBED PNL 211XAF FROM 5024N400001SS-G, BATCH #33550636 PER SERO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XAF REQUIRES FABFABBED PNL 232XAF FROM 5024N400001SS-G, BATCH #33550636 PER SERO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3, MAIN CARGO FLOOR PANEL 222XBF REQUIRES FAB. FABBED PNL 222XBF FROM 5024N400001SS-G, BATCH 33550626 PER SERO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 231XBF REQUIRES FABFABBED PNL 231XBF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CARGO FLOOR PANEL 232XEF REQUIRES FABFABBED PNL 232XEF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PNL 231XAF REQUIRES FABFABBED PNL 231XAF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XFF REQUIRES FABFABBED PNL 232XFF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3, MAIN CABIN FLOOR PANEL 211XCF REQUIRES FAB. FABBED PNL 211XCF FROM 5024N400001SS-G, BATCH 33550636 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XDF REQUIRES FABFABBED PNL 232XDF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 231XEF REQUIRES FABFABBED PNL 231XEF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MANI CABIN FLOOR PANEL 232XBF REQUIRES FABFABBED PNL 232XBF FROM 5024N400001SS-G, BATCH #33550636 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 231XDF REQUIRES FABFABBED PNL 231XDF FROM 5024N400001SS-G, BATCH #33550636 PER SERO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3, MAIN CABIN FLOOR PANEL 222XCF REQUIRES FAB. FABBED PNL 222XCF FROM 5024N400001SS-G, BATCH 33550636 PER SERO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XGF REQUIRES FABFABBED PNL 232XGF FROM 5024N400001SS-G, BATCH #33550636 PER SERO B757-5320-9692-K

Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 32,468 hrs · 22,201 cycles

INSPECTION TYPE:C1REP. DI# D614352 R/H I.B. MAIN FLAP COVE PANEL HAS 1/2" PUNCTURE IN COVE PANEL 4.25" FLOOD OF AFT EDGE 30" I.B. OF O.B. EDGEREPAIRED IAW RCD SECTION 2

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,429 hrs · 22,179 cycles

INSPECTION TYPE:N/A EMERGENCY LIGHT HAS FIVE INOP BULBS. RELAMPED FIVE BULBS IN EMERGENCY LIGHT PER AMM 33-51-01-2.

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 32,118 hrs · 21,990 cycles

AT FL 320 WITH LEFT PACK OFF RECEIVED CABIN ALT WARNING, WE PUT ON MASKS AND TURNED ON LEFT PACK. WE RAN QRH PROCEDURE CABIN CAME BACK BUT RIGHT DUCT PRESSURE WAS LOW 5-10 PSI. WE WERE IN ICING SO ENG HEAT WAS ON. WHEN WE CAME OUT OF REMOVED AND REPLACED RT ENG. PRECOOLER FAN VALVE AND FAN AIR TEMP SENSOR AS PER MM 36-11-16-004/36-11-17-004. OP'S CK'S GOOD. ACFT OK FOR CONTINUED SERVICE. IPC 36-11-01-08/36-11-16-05.

Part: SKIN — CORRODED (BS 1465) · airframe 32,050 hrs · 21,936 cycles

FUSELAGE SKIN REPAIR HAS MISSING RIVET HEAD AND SIGNS OF CORROSION IN FASTENER HOLES, REPAIRED IAW EO B757-5310-69873-A.

Part: STRINGER — CORRODED (BS 1465) · airframe 32,050 hrs · 21,936 cycles

STRINGER 29R CORRODED JUST AFT OF BS 1460. REPAIRED THE STRINGER IAW B757-5310-69873-A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,050 hrs · 21,936 cycles

CORRODED AND CRACKED SHEAR TIE STA 1460, STRINGER 29L. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SHIM — CORRODED (FUSELAGE) · airframe 32,050 hrs · 21,936 cycles

FUS SKIN FASTNERS DAMAGE REPAIR STA 1455-1464 STR 29L. REMOVED PRODUCTION STRING SPLICE AND FOUND CORROSION TO UNDER LYING SHIM STOCK IAW SRM 51-40-02. FAB NEW SHIM IAW DWG 146N3400 REINSTALLED SHIM AND STRINGER SPLICE CHANNEL IAW SRM 51.40.02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,918 hrs · 21,841 cycles

UPON LANDING EICAS L FWD ENTRY DOOR, DURING TAXI IN EICAS EXTINGUISHED. PERFORMED SYSTEM FUNCTIONAL CHECK IAW AMM TASK 52-71-00-735-053. OPS CHECK NORMAL

Part: ALTIMETER — ABNORMAL (FIRST OFFICER'S) · airframe 31,408 hrs · 21,503 cycles

FIRST OFFICER`S ALTIMETER IN ERROR. IT READS 33840. CAPTAIN`S ALTIMETER READS 34000. STBY ALTIMETER READS 339000. FIRST OFFICER`S ALTIMETER NORMAL WITH ALTERNATE AIR DATA SELECTED. TROUBLESHOT IAW FIM 34-12-00-815-802, FIG 103, PERFORMED FULL RANGE PITOT STATIC SYS TEST IAW MM 34-11-00-735-176, NO LEAKS NOTED . R & R THE FIRST OFFICER`S ALTIMETER & RT ADC IAW MM 34-13-01-404-004, & 34-12-01-424-006, OPS CHECKED GOOD.

Part: PITOT TUBE — OBSTRUCTED (FIRST OFFICER'S) · airframe 31,099 hrs · 21,320 cycles

IAS DISAGREE, FIRST OFFICER`S AIRSPEED INDICATED 10KTS SLOWER THAN THE CAPTAIN`S STANBY IAS. FOUND OBSTRUCTION IN FIRST OFFICER`S PITOT TUBE. REMOVED DEBRIS IAW AMM 34-11-01-226-012, FOLLOWED BY A PITOT SYSTEM FLUSH IAW AMM 34-11-00-173-009. LOW RANGE, HIGH RANGE AND PITOT STATIC LEAK CHECKED IAW AMM 34-11-00-501.

Part: SMOKE GOGGLES — DAMAGED (SAFETY EQUIPMENT) · airframe 30,633 hrs · 20,976 cycles

ONE PAIR OF SMOKE GOGGLES DAMAGED. INSTALLED NEW GOGGLES ONBOARD A/C

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, RT WING INBD FLAP UPPER SURFACE, OTBD SIDE DELAMINATED. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, 51-70-10-2R-4, REPAIR 4, 51-70-10-2R.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 241XKF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREP B757-5320-9692.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOORBOARD 242XJK DAMAGED, FABRICATED A NEW FLOORBOARD 242XJF IAW SREO 757-5320-9692-J.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, RT WING INBD FLAPS UPPER SURFACE, OTBD SIDE PREVIOUS REPAIR DELAMINATED. REMOVED PREVIOUS REPAIR, PERFORMED WATER CYCLE, REMOVED PANEL AND PERFORMED REPAIR IAW SRM 57-53-01-2R-1, AND 51-70-10-2R 250.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 231XJF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-J.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 241XEF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-J.

Part: FLOORBOARD — DELAMINATED (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOORBOARD 231XFF DELAMINATED. FABRICATED A NEW FLOORBOARD IAW SREO 757-5320-9692-J.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 30,571 hrs · 20,929 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOORBOARD 241XHF DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-J.

Part: CONTAINER — TORN (LIFE VEST) · airframe 29,585 hrs · 20,231 cycles

OBSERVER BENCH SEAT BOTH LIFE VESTS BAG TORN. R & R BOTH LIFE VESTS FOR OBSERVER BENCH SEAT REF MM 25-60-00 EFF SOURCE, REF 25-64-51-01 033K.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 29,311 hrs · 20,046 cycles

RT ENGINE OVERTEMP ON DEPARTURE. THE EGT REACHED 655 DEGREES C. REDUCED THRUST LEVER TO NORMAL RANGE. DECLARED EMERGENCY. RETURNED. ACCOMPLISHED OVERTEMP VISUAL INSPECTION ON RT ENGINE MAX TEMP 654, DEGREES C. DURATION 9 SEC STEADY STATE. EPCS MSG EGT RED S 14 BLEED/EEC P 14 BLEED/EEC NO FAULTS FOUND. IAW AMM 72-00-00-216-519-P00, FIG 609, AREA A.

Part: WARNING LIGHT — FALSE ACTIVATION (L1 DOOR) · airframe 29,276 hrs · 20,020 cycles

EICAS MESSAGE, LT FWD ENTRY DOOR DISPLAYED STEADY AND ENTRY DOOR OPEN LIGHT ON STEADY WITH DOOR CLOSED WHILE TAXI IN TO PARK, CYCLED L1 FWD ENTRY DOOR SEVERAL TIMES INSPECTED DOOR SWITCH COULD NOT DUPLICATE REPORT. DOOR WARNING INDICATIONS NORMAL.

Part: SHEAR WEB — CORRODED (BS 236) · airframe 29,186 hrs · 19,948 cycles

INSPECTION TYPE:C17, COCKPIT, FLOOR PANEL CORROSION BS 236, LBL 11-LBL 23 OUT OF LIMITS. ACCOMPLISHED REPAIR IAW EO B757-5310-56937-A AND REO-G18794, REV A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-01/201. TESTED OK.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 28,191 hrs · 19,196 cycles

INSPECTION TYPE:C-10, RT WING INBD MAIN FLAP LOWER SURFACE DELAMINATED. PERFORMED 250 DEGREE, PREPREG REPAIR IAW SRM 51-70-07, PARA 5D, FIG 6.

Part: FLOORBOARD — DEBONDED (MAIN CABIN) · airframe 28,191 hrs · 19,196 cycles

INSPECTION TYPE:C16, MAIN CABIN FLOORBOARD 242XMF AFT CORNER IS DISBONDED. FABRICATED FLOORBOARD IAW SREO B757-5320-9692-H8.

Part: EEC — INOPERATIVE (LT ENGINE)

CREW SHUTDOWN LT ENGINE DUE TO LOW OIL PRESSURE. DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT. R & R LEFT ENG EEC IAW AMM 73-21-04-4. C/W POWERPLANT ADJ TEST 7 IAW AMM 71-00-00-5. TESTS GOOD.

Part: SENSOR — INOPERATIVE (RT ENG OVRTEMP)

ATB - EMERGENCY DECLARED. THE LT PACK WAS PREVIOUSLY DEFERRED AND CREW REPORTED LOSS OF RT PACK AND LT ENG ANTI ICE. RETURNED TO MSP WITHOUT INCIDENT. R & R RT ENG OVERTEMP SENSOR W/REF TO MM 36-11-13-4. OPS CK NORMAL DURING ENGINE RUN. OK FOR SERVICE.

Part: FRAME — DENTED (BS 540 S16-17R) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FRAME IS DENTED. INBD FLANGE, STA 540, WL 213, BETWEEN STR 16-17R. REPAIRED IAW ER 11-02733, DATED 27MAY2011.

Part: FLOOR SKIN — CORRODED (BS 270-275) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR UPPER SURFACE AT 4 NUTPLATE LOCATIONS, BS 270-275, LBL 25.5 TO 27.5, WL 200. REPAIRED IAW ER 11-02718.

Part: FLOOR SKIN — CORRODED (BS 275) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR UPPER SURFACE, BS 275, LBL 39, WL 200. REPAIRED IAW ER 11-02718 25MAY2011.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO COMPARTMENT FLOOR PANEL AT BS 560-620, RBL 25-45, IS DAMAGED ALONG THE TOP INBD AFT SURFACE. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, WHILE WORKING CCN M-3450-39526B FOUND E 3-3 RACK FWD, RT ATTACH POINT CRACKED. R & R CRACKED ANGLE IAW SRM 51-30-01-0G; SRM 51-40-05-0G; SRM 51-40-08-0G, SRM 51-40-02-0G; DWG 284N1013.

Part: FRAME SPLICE — GOUGED (BS 620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C, SCREW STRIKE ON THE BS 620 FRAME SPLICE DOUBLER, INBD FLANGE, BETWEEN STR 8-9L. R & R FRAME SPLICE DOUBLER IAW SRM 51-40-02-0G.

Part: FLOOR PANEL — DAMAGED (BS 820-880) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 820-880, RBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 820-880) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 820-880, RBL 0-25. FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 0-25. REPLACED FLOOR PANEL IAW EO B757-5320-G, SRM 53-00-50-1A1, AMM 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (BS 440-480) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 440-480, LBL 0-25. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, BL0-RBL25. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1320) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOORBOARD AT STA 1320, LBL45 TO 62 HAS MECHANICAL DAMAGE. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 333-440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCB FLOORBOARD BS 333-440, WL 208, LBL 45-LBL 62 IS PUNCTURED AND HAS DAMAGES ON UPPER SURFACE. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 333-440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCB FLOOR PANEL BS 333-440, BL 0-RBL 25, WL 208, FLOORBOARD HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 45-65. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-820) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-820, LBL 0-25. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 879-900, RBL 0-25. FABRICATED REPLACEMENT FLOOR PANEL EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-780) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-780, RBL 45-65. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, BL 0 - RBL 25 FLOOR PANEL REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-820) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-820, LBL 0-25. FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, BL 0-LBL 25. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FRAME — DAMAGED (BS 440 S13R) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, SCREW STRIKE ON INNER FLANGE OF FRAME, STA 440, STR 13R. REPAIRED BS 440 FRAME BETWEEN STR 10R AND 11R TO STR 14R IAW SRM 53-30-07-0I 1, SRM 53-00-07-1A 1, SRM 53-00-07-2R 1, SRM 51-20-01-0G, SRM 51-40-09-0G, SRM 51-40-02-0G, SRM 51-40-05-0G.

Part: FLOOR PANEL — DAMAGED (BS 820-879) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE AND INSERT MISSING, STA 820-879, LBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SEAT TRACK — CORRODED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION AROUND NUTPLATE HOLES ON SEAT TRACK, STA 879-900 LBL 45, WL 208. REPLACED SEAT TRACK IAW SRM 53-30-52-0I1, SRM 51-40-02-0G, DWG 143N5405 REV, SRM 51-40-08-0G, SRM 51-40-05-0G, SRM 51-20-01-0G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 0-25. REPLACED FLOOR PANEL IAW EO B757-5320-G, SRM 53-00-50-1A1, AMM 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (BS 820-880) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3 FLOOR PANEL HAS EDGE DAMAGE, STA 820-880, RBL 0-25. REPLACED FLOOR PANEL IAW EO B75705320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 333-440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCB FLOOR PANEL BS 333-440, BL 0-LBL 25, WL 208, HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SEAT TRACK — CORRODED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION AROUND NUTPLATE HOLES ON SEAT TRACK, STA 879-900 LBL 45, WL 208. REPLACED SEAT TRACK IAW SRM 53-30-52-0I 1, SRM 51-40-02-0G, DWG 143N5405 REV-, SRM 51-40-08-0G, SRM 51-40-05-0G, & SRM 51-20-01-0G.

Part: FLOORBEAM — CORRODED (BS 879) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION AROUND NUTPLATE HOLES ON FLOORBEAM, STA 879, LBL 45-54, WL 208. REPAIR IAW EO B757-5310-42979-A AND ATS ER 11-02744.

Part: FLOOR PANEL — DAMAGED (BS 1600-1681) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL AT STA 1600 TO 1681, LBL 45 TO 65 AFT OTBD CORNER DAMAGED. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO NR B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, LBL 45-65, FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 440-480) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA. 440-480, LBL 0-25 FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, RBL 0-25. FABRICATED REPLACEMENT FLOOR PANEL IAW EO NR B757-5320-9692-G.

Part: SHEAR WEB — CORRODED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON SHEAR WEB, AT STA 560-620, LBL 45-65, SEVERAL AREAS. (MARKED) REPAIRED IAW ER 11-02760.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 480-560, LBL 0-25. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, LBL 25-45. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, RBL 45-65 FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SHEAR WEB — CORRODED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON SHEAR WEB, AT STATION 480-560, LBL 45-65, SEVERAL AREAS. (MARKED) REPAIRED IAW ER 11-02760.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DECK: FLOOR PANEL FROM BS 480-560, BL 0-RBL 25, FWD OTBD CORNER IS DELAMINATED. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 440-480) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 440-480, LBL 25-LBL 45. REPLACED IAW EO B757-5320-9692-G.

Part: FRAME — DENTED (BS 580 S16-17R) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FRAME IS DENTED, INBD FLANGE, STA 580, WL 213, BETWEEN STR 16-17R. REPLACED BS 580, RT FRAME SECTION IAW DWG 143N1008, 143N1024, ER 11-02814 DATED 05-17-11, SRM 51-40-02-0G, AND SRM 51-40-05-0G.

Part: SUPPORT FITTING — CRACKED (BS 330) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, INTERIOR, STR 5L TO 9G, SUPPORT CLIP IS CRACKED AT BS 330. REPLACED CLIP IAW DWG 141N8226, 141N8206, AND SRM 51-40-02-0G.

Part: FLOOR PANEL — DAMAGED (BS 440-480) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 440-480, LBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-820) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-820, LBL 25-45 FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, BL 0 - LBL 25, FLOOR PANEL REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-820) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 820-720, RBL 0-25. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL AT STA 879-900, LBL 45-65, IS MISSING INSERT, AND HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G; SRM 53-00-50-1A1, AMM 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3 FLOOR PANEL HAS DAMAGE, STA 480-560, LBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 25-45. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-780) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-780, RBL 25-45. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3 FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 45-65. FABRICATED REPLACEMENT FLOOR PANEL IAW EO NR B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 480-560, LBL 25-LBL 45. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL AT STA 1236, LBL 45 FWD EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSP TYPE:C3, MAIN CARGO DECK; FLOOR PANEL FROM BS 560-620, BL 0 - RBL 25, HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 440-480) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE AND 1 EA INSERT MISSING, STA 440-480, LBL 45-65. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 480-560, LBL 0-25. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 333-440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCB BS 333-440, RBL 45-62, WL 208, FLOORBOARD HAS EDGE DAMAGE. REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, RBL 45-65. REPLACED FLOOR PANEL IAW EO B75705320-9692-G.

Part: SEAT TRACK — CORRODED (BS 440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DECK: CORROSION ON SEAT TRACK AT BS 440, RBL 46, WL 208. R & R CORRODED SEAT TRACK SECTION IAW SRM 51-40-02-08, SRM 51-10-02-0G, SRM 53-00-52-1A, SRM 53-10-52-2R DWG PL143N5273, DWG PL1435276.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 879-900, LBL 25-45 FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1680-1720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1680-1720, RBL 0-65, WL 208 FLOORBOARD MISSING INSERT. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, LBL 45-65. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720-820) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720-820, RBL 0-25. REPLACED FLOOR PANEL IAW EO B75705320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1300) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOORBOARD AT STA 1300, RBL 45 TO 62 IS DAMAGED. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 720, LBL 25-45. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 820-880) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3 FLOOR PANEL HAS EDGE DAMAGE, STA 820-880. LBL 0-25. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 480-560, LBL 45-65. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SHEAR WEB — CORRODED (BS 440-460) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON SHEAR WEB AT STATION 440-460, LBL 45-65, 3 AREAS. (MARKED) REPAIRED IAW ER 11-02760.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, RBL 25-45. REPLACED IAW EO B75705320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 333-440) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCB BS 333-440, BL 0 - RBL 25, WL 208, FLOORBOARD HAS EDGE DAMAGE REPLACED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL AT STA 879-900, LBL 45-65, IS MISSING INSERT, AND HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW EOB757-5320-9692-G; SRM 53-00-50-1A1, AMM 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 560-620, LBL 25-45 FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA. 560-620, LBL 0-25. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DELAMINATED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DECK; FLOOR PANEL FROM BS 480-560, BL 0 - RBL 25, FWD OTBD CORNER IS DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 879-900, RBL 25-45. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G; SRM 53-00-50-1A1; AMM 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (BS 1680-1720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1680-1720, LBL 0-65, WL 208, FLOOR PANEL MISSING INSERT. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SEAT TRACK — DAMAGED (BS 780-880) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, SEAT TRACK IS DAMAGED AT STA 872, LBL 25. REPLACED SEAT TRACK BS 780 TO BS 880, LBL 25, IAW SRM 53-00-52-1A1, SRM 51-40-02-0G, SRM 51-40-08-0G, SRM 51-40-05-0G, SOPM 20-41-02, DWG 143N5274 REV.

Part: FLOOR PANEL — DAMAGED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 480-560, LBL 45-65. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DELAMINATED (BS 480-560) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DECK; FLOOR PANEL FROM BS 480-560, BL 0 - RBL 25, FWD OTBD CORNER IS DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 879-900) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 879-900, RBL 45-25. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G; SRM 53-00-50-1A1; AMM 53-01-01-4.

Part: FLOORBOARD — DAMAGED (A230/Z200) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOORBOARD PANEL HAS EDGE DAMAGE, BS 820-879, LBL 45-65. FABRICATED FLOORBOARD PANEL BS 820-879, LBL 45-65 IAW SRM 53-00-50-1A1.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, LBL 45-65. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 620-720) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, FLOOR PANEL HAS EDGE DAMAGE, STA 620-720, RBL 25-45. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1060-1080) · airframe 27,025 hrs · 18,368 cycles

INSPEB757-5320-96G.CTION TYPE:C3, BS 1060-1080, LBL 46-64, WL 208, FLOORBOARD HAS EDGE DAMAGE AND MISSING INSERT. FABRICATED REPLACEMENT PANEL IAW EB757-5320-96G.O

Part: FLOOR PANEL — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, RBL 25-45 WL 208, FLOORBOARD HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-520-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1020-1060) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1020-1060, RBL 45-64, WL 208, FLOORBOARD DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1060-1080) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1060-1080, LBL-46-64, WL-208, FLOORBOARD HAS EDGE DAMAGE AND MISSING INSERT. REPLACED FLOORBOARD IAW EO B75705320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, RBL 45-65, WL 208, FLOORBOARD BROKEN AND EDGE DAMAGE. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, LBL 0-25, WL-208, FLOORBOARD HAS EDGE DAMAGE. REPLACED FLOORBOARD IAW EO B75705320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1020-1060) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS-1020-1060, RBL-0-24, WL-208, FLOORBOARD DAMAGED. FABRICATED REPLACEMENT FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020. LBL 24-44, WL 208, FLOORBOARD HAS EDGE DAMAGE. FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1020-1060) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS-1020-1060, LBL 0-25, WL 208, FLOORBOARD HAS EDGE DAMAGE. FABRICATED REPLACEMENT PANEL IAW EO NR B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1020-1060) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS-1020-1060, RBL-24-44, WL-208, FLOORBOARD DAMAGED. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1056) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1056, RBL 45-65, WL 208, FLOORBOARD HAS EDGE DAMGE AND A MISSING INSERT. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1056) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1056, RBL-45-65, WL-208, FLOORBOARD HAS DAMAGE AND A MISSING INSERT. REPLACED FLOORBOARD IAW EO B75705320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 1056) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS-1056, RBL 25-45, WL 208, FLOORBOARD HAS EDGE DAMAGE. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: SUPPORT — CORRODED (BS 797-801) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3 FWD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT UPPER SURFACE HAS CORROSION AT BS 797 TO BS 801, RBL 21 TO RBL 24. R & R PER SRM 51-70-13-0G.

Part: FLOOR PANEL — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, LBL 44-65, WL 208, FLOORBOARD HAS MISSING INSERT AND EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — BROKEN (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, RBL 45-65, WL 208, FLOORBOARD BROKEN AND EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, LBL 44-65, WL 208 FLOORBOARD HAS MISSING INSERT AND EDGE DAMAGE. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, LBL 0-25, WL 208, FLOORBOARD HAS EDGE DAMAGE FABRICATED REPLACEMENT FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020, RBL 01-25, WL208, FLOORBOARD HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1100-1200) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1100-1200, LBL 25-45, WL 208, FLOORBOARD IS DAMAGED AND MISSING INSERT. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 900-1020 LBL 24-44 WL 208 FLOORBOARD HAS EDGE DAMAGE REPLACED FLOORBOARD IAW EO B75705320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 1100-1200) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, BS 1100-1200, LBL 0-24, WL 208, FLOORBOARD DAMAGED. FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.

Part: FRAME — CHAFED (BS 377) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CHAFE IN FRAME FLANGE AT BS 377, BETWEEN STR 22R AND 23R REPAIRED IAW ATS ER 11-02743.

Part: FLOOR SUPPORT — CORRODED (BS 312-322) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON 4 EA NUTPLATES ON LWR SURFACE OF FLOOR SUPPORT RBL 13.5, BS 312-322, WL 207.5. REPLACED IAW SRM 51-10-02-0G.

Part: FRAME — GOUGED (CARGO DOOR) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DOOR-INTERIOR STRUCTURE-GOUGED IN FRAME-STA 540-5 INCHES UP FROM BOTTOM. REPAIRED IAW ENGINEERING REPAIR NR 11-02746.

Part: FRAME — GOUGED (CARGO DOOR) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN CARGO DOOR-INTERIOR STRUCTURE-GOUGED IN FRAME-STA 560-5 INCHES UP FROM BOTTOM. REPAIRED IAW ENGINEERING REPAIR 11-02732

Part: FRAME — GOUGED (CARGO DOOR) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MAIN DECK CARGO DOOR-4 EA GOUGES IN FRAME-STA 487-3, 4, 5.5 AND 8.5 INCHES UP FROM BOTTOM. R & R FRAME DOUBLER IAW SRM 51-40-02.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C, MAIN DECK CARGO DOOR - INTERIOR STRUCTURE - GOUGE IN FRAME - STA 612 - 4" UP FROM BOTTOM. REPLACED FRAME ANGLE IAW SRM 51-40-02 AND DWG 69-24182.

Part: FLOORBOARD — GOUGED (CARGO BAY) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, MCD INTERIOR STRUCTURE, WEB HAS GOUGE 5" UP FROM BOTTOM EDGE. FABRICATED NEW FLOORBOARD IAW DWG 65-49309 AND SRM 50-10-02-0G, 51-40-02-0G, 51-40-05-0G.

Part: SHEAR WEB — CORRODED (BS 324-333) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON UPPER SURFACE OF SHEAR WEB AT 9PLACES, BS 324-333, LBL 47.5 TO LBL 61.5, WL 208. REPAIR IAW EO B757-5310-42904-A DATED 01-JUN-2011 AND ATS ER 11-02729 DATED 31-MAY-2011.

Part: SILL — GOUGED (FUSELAGE) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CREW ENTRY DOOR LWR SILL UPPER SURFACE HAS SEVERAL GOUGES, BS 298-323, WL 215, LBL 64. R & R IAW SRM 51-40-02-0G; SRM 53-10-15-1A1; SRM 53-10-15-OI 1 SRM 51-40-05-0G; DWG 141N8326; SRM 51-20-01-0G; SRM 51-20-05-0G.

Part: FLOOR SUPPORT — CORRODED (BS 297-310) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BS 297-310, LBL 59.5, WL 208. REPLACED PART IAW SRM 51-40-2.

Part: FLOOR PANEL — DELAMINATED (BS 297-333) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, COCKPIT FLOOR PANEL BS 297-333, RBL 10 TO RBL 60 HAS DELAMINATION ON LOWER SURFACE AT POTTED INSERT. REPLACED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SUPPORT ANGLE — GOUGED (BS 298-323) · airframe 27,025 hrs · 18,368 cycles

INSP TYPE:C3, CREW ENTRY DOOR LWR SILL SUPPORT ANGLE HORIZ FLANGE UPPER SURFACE HAS 2 GOUGES, BS 298 AND BS 323 WL 215 LBL 63 (MARKED). REPLACED INNER CHORD ANGLE BS 298-323, WL 215, LBL 63, IAW SRM 53-10-15-1A 1, SRM 53-10-15-0I-1, SRM 51-40-02-0G, SRM 51-40-05-0G, AMM 51-00-58-2.

Part: FLOOR SUPPORT — CORRODED (BS 312-322) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BS 312-322, LBL 59.5, WL 208. REPLACED PART IAW SRM 51-40-02.

Part: STRAP — CORRODED (COCKPIT) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR STRAP. FABRICATED AND REPLACED COCKPIT FLOOR STRAP IAW SRM.

Part: STRAP — CORRODED (COCKPIT) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR STRAP. FABRICATED AND REPLACED COCKPIT FLOOR STRAP IAW SRM.

Part: FLOOR SKIN — CORRODED (COCKPIT) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR UPPER SURFACE AT CAPT'S INBD AFT SEAT TRACK AT 2 PLACES, BS 254-27. (MARKED) REPAIR DOUBLER IAW ATS ER11-02718, AND EO B757-5310-42849-A.

Part: STRAP — CORRODED (BS 293) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR STRAP UPPER SURFACE BS 293, RBL 2, WL 200. R & R STRAP IAW SRM 51-40-02.

Part: FLOOR SKIN — CORRODED (COCKPIT) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, CORROSION ON COCKPIT FLOOR UPPER SURFACE AT CAPT'S INBD FWD SEAT TRACK AT 3 PLACES, BS244-257. (MARKED) REPAIR DOUBLER IAW ER 11-02718, AND EO B757-5310-42849-A.

Part: SKIN — GOUGED (A210/Z200) · airframe 27,025 hrs · 18,368 cycles

INSPECTION TYPE:C3, SKIN GOUGED A PERMANENT REPAIR OF EXTERNAL REPAIR BETWEEN STRINGERS 21-22, STA 279-289 INSTALLED WITH BLIND RIVETS: REF ATA 5300, D114426. PERMANENT REPAIR IAW EO B757-5330-42858-A, ER 11-02754.

Part: SHEAR WEB — CORRODED (BS 356) · airframe 26,419 hrs · 17,955 cycles

INSPECTION TYPE:SPV, WHILE EVALUATING SHEAR WEBS, FOUND PREVIOUS BLEND AT BS 356, LBL 43, WL 208, TO BE OUT OF LIMITS IAW EO B757-5310-38276. REPAIRED IAW ATS ER NR 10-3477, DATED 10JUL10.

Part: PLUNGER — DIRTY (COCKPIT WINDOW)

INSPECTION TYPE:N/A ON PREFLIGHT, NOTED THAT FIRST OFFICER EXTERIOR EMERGENCY EGRESS LATCH UNDER WINDOW WAS OPEN APPROX ONE INCH. CREW CYCLED WINDOW AND RE-SECURED LATCH. AFTER LANDING CREW NOTED LATCH ON EXTERIOR OPEN AGAIN. TRIED TO RESET EMERGENCY EGRESS HANDLE. FOUND PLUNGER BALL DIRTY ON EXTERNAL HANDLE. CLEANED & LUBED. OPERATES NORMAL PER AMM 56-11-02-5. OK FOR SERVICE.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 FWD CARGO BAY NR 3 FLOOR PANEL IS CORRODED ON THE TOP. FABRICATED FWD CARGO BAY NR 3 FLOOR PANEL AND INSTALLED IAW SRM 51-40-02-0G, SRM 53-30-53-0I.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE-C2 MAIN CARGO DECK BS 1060-1100 BL 0 LBL 25 FLOOR PANEL HAS BROKEN/ MISSING INSERTS. REPLACED PANEL IAW SRM ADDENDUM B757-5320-9692-G2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 FLOORBEAM BS 1016 BL 0 CORRODED ON UPPER FLANGE. REPAIRED PER ATS ER 09-3033.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1100-1200, RBL 45-60, FLOOR PANEL HAS BROKEN/MISSING INSERTS. FABRICATED NEW FLOOR PANEL IAW ER B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1100-1200, RBL 25-45 FLOOR PANEL HAS BROKEN/MISSING INSERTS. FABRICATED NEW FLOOR PANEL IAW ER B757-5320-9692-G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 BS 1040-1080 BL 0 LONGITUDINAL FLOORBEAM HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED BS 1040-1080 BL 0 FLOORBEAM IAW SRM 51-40-05-0G, SRM 51-40-08-0G AND SRM 51-40-02-0G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1100-1200 BL 0 - RBL 25, FLOOR PANEL HAS BROKEN/MISSING INSERTS. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR SUPPORT — PUNCTURED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 BS 1020 BL 0-LBL 25 FLOOR PANEL SUPPORTS PUNCTURED. FABRICATED NEW PANEL SUPPORT IAW SRM 51-40-05-OG, 51-40-02-0G, 51-40-01-0B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 BS 1055 LBL 25-45 FLOOR PANEL HAS CORROSION. FABRICATED PANEL SUPPORT IAW SRM 51-40-05-0G, 51-40-02-0G, 51-20-01- 0G.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE-C2 MAIN CARGO DECK BS 900-10200 LBL 45-60 FLOOR PANEL HAS BROKEN / MISSING INSERTS. REPLACED PANEL IAW SRM ADDENDUM B757-5320-9692-G2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1029 RBL 45 LONGITUDINAL FLOORBEAM HAS CORROSION O/B FLANGE. REPAIRED PER ER 09-3034 DATED 06/12/09.

Part: COWLING — WORN (NR 2 ENGINE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 NR 2 ENGINE I/B CORE COWL JUST AFT OF THE AFT HINGE WORN THROUGH. REMOVED AND REPLACED PER SRM 51-40-02.

Part: PLATE — CRACKED (SPOILER) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE-C2 RT WING NR 8 SPOILER AREA, WIGGLE PLATE, IB AND FWD OF PCU, CRACKED IN USUAL PLACE REPLACED PLATE IAW SRM 51-40-02-0G.

Part: WEB — GOUGED (E&E BAY) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 GOUGE IN E&E BAY WEB AT BS 468 RBL 6 WL 147 TO 143. REMOVED, FABRICATED AND INSTALLED NEW IAW SRM 51-40-08, SRM 51-40-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 EXTERNAL FUSELAGE SKIN SECTION 48 LEFT, HAS A CREASED DENT MARKED AT BS 1949 BL 6L. REPAIRED PER SRM 51-70-10-2R-01-3.

Part: DOUBLER — ERODED (LE SLAT) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE-C2 WIND ERROSION/DELAMINATION OF PREVIOUS REPAIR ON NR 7 SLAT UPPER SURFACE, 30 INCHES INBD FROM OTBD EDGE 10 INCHES FWD FROM AFT EDGE. REPAIRED IAW SRM 57-43-02-2R 1.

Part: SUPPORT ANGLE — CORRODED (APU INLET) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 APU INLET SUPPORT STRUCTURE ON RIGHT SIDE IS CORRODED ALONG NUT PLATES FROM BS 1787-1824. REPAIRED PER ER 09-3024 DATED 12JUN09.

Part: GUIDE — GOUGED (COCKPIT WINDOW) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 CAPTAINS NR 2 WINDOW GUIDE HAS A DEEP GOUGE. REPAIRED PER ATS ENGINEERING 09-3020.

Part: GUIDE — GOUGED (COCKPIT WINDOW) · airframe 36,623 hrs · 17,381 cycles

INSPECTION TYPE:C2 F/O'S NR 2 WINDOW GUIDE HAS A DEEP GOUGE. REPAIRED PER AP\TS ENGINEERING 09-3020.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A LT SIDE FUSELAGE HAS LIGHTNING STRIKE LOCATED 1.5 INCH FROM FWD RADIO ALT ANTENNA. REPAIR ACCOMPLISHED PER EO B757-5330-32920-A.

Part: SKIN — DELAMINATED (RT AILERON)

RIGHT AILERON HAS DELAMINATION. R & R RIGHT AILERON ASSY PER MM 27-11-21-4. CHECKS NORMAL.

Part: LENS — BROKEN (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT LENS ASSY BROKEN. REMOVED AND REPLACED LIGHT LENS ASSY.

Part: SKIN — DENTED (CARGO DOOR) · airframe 24,078 hrs · 16,379 cycles

INSPECTION TYPE:C REPAIR DENT IN LOWER EXTERNAL SKIN SURFACE OF AFT CARGO DOOR. REPAIRED DENT IN LOWER EXTERNAL SKIN AFT CARGO DOOR IAW SRM 52-30-01- 2R4. THIS IS A CATEGORY B REPAIR PER SRM 52-30-01-2R4. REINSPECTION PER SRM 52-30-01-2R4 TABLE IV FIGURE 201 PAGE 1 SHEET 4.

Part: BULKHEAD — CHAFED (NR 1 NACELLE) · airframe 24,078 hrs · 16,379 cycles

INSPECTION TYPE:C NR 1 PYLON AFT ENG MOUNT BULKHEAD LWR O/B CORNER OUTER SURFACE IS CHAFED. COMPLIED WITH FINAL EA 757-5453-27-A1757 AND EO B757-5410- 27988-A.

Part: FRAME — DENTED (BS 1340 S25-26R) · airframe 24,078 hrs · 16,379 cycles

INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1340 APPROX BETWEEN S25R AND S26R. REPAIR ACCOMPL PER SRM 53-00-07 REPAIR S DETAIL III FIG 201 SHEET 8 OF 15. THIS IS A CATEGORY B REPAIR PER SRM 53-00-07. REINSPECTION PER SRM 53-00-07 DETAIL V FIG 201 SHEET 12 OF 15 ZONE 1 TABLE II FIG 201 SHEET 10 OF 15.

Part: A/C PACK — ODOR (LEFT)

LEFT PACK HAS FOUL ODOR. OPERATED LEFT PACK FOR EXTENDED PERIOD OF TIME. NO ODOR NOTED. THIS CLEARS M349455.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ARMED, LIGHT HAS LEFT BULB INOP. LAMPED EMERGENCY EXIT LIGHT (ARMED). OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (SECT 46) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED AT STA 1318, LBL 24. REPAIRED PER ER 05-4597.

Part: SEAT TRACK — CORRODED (SECT. 46) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED STA 1542 RBL 47 REPAIRED PER ER 05-4597.

Part: STRUCTURE — CORRODED (MAIN CARGO BAY) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 CORROSION ON TOP OF SEAT TRACK AT BS 1184 RBL 1. REMOVED AND REPLACED SEAT TRACK BS 1180 TO BS 1209 IAW UPS ER 05-4598.

Part: FITTING — CORRODED (BULK CARGO BAY) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 BULK CARGO RT MBA TIE DOWN FITTING HAS CORROSION STA 1580,1600, AND 1620. REMOVED CORROSION FROM FITTINGS AT BS 1580, FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FITTING AT BS 1580 IAW SRM 53-00-53-1A AND SRM 51-40-02. REMOVED CORROSION FROM FITTINGS AT BS 1600 AND 1620 FOUND IN LIMITS ARE RESTORED FINISH IAW SRM 53-00-53-1A.

Part: SEAT TRACK — CORRODED (MAIN CARGO BAY) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED AT STA 1173, LBL 44.5. REMOVED AND REPLACED SEAT TRACK BS 1070 TO BS 1180 IAW SRM 53-00-52 AND SRM 51-40-02.

Part: BEAM — CORRODED (MAIN CARGO BAY) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO LONITUDINAL BEAM HAS CORROSION AT STA 1058, RBL 44. CORROSION FOUND OUT OF LIMITS, REMOVED AND REPLACED LONGITUDINAL BEAM BS 1040 TO BS 1080, RBL 44, WL 208 IAW SRM 53-00-57-1A, SRM 51-40-02

Part: FLOORBEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 CORROSION ON TOP OF FLOORBEAM FWD FLANGE AROUND FASTENER HOLES AT SEVERAL LOCATIONS AT BS 1200 BETWEEN BL-O AND LBL 65 REPAIRED PER ER 05-4596.

Part: BEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C-4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION AT STA 974 LBL 24. REPAIRED PER ER 05-4559.

Part: FLOOR SUPPORT — CORRODED (SECT. 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO FLOOR SUPPORT CORRODED AT STA 1056 RBL 5-23. REMOVED AND REPLACED PER SRM 51-40-02 AND SRM 51-30-01

Part: BEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION STA 997, RBL 44. REPAIRED PER ER 05-4558.

Part: BEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 LONGITUDINAL BEAM CORRODED AT STA 1063 LBL 26, LONGITUDINAL BEAM IS BEING REPLACED FROM BS 1040-BS1080, LBL26 WL 208 0N CUST CARD#561467.

Part: SEAT TRACK — CORRODED (SECT 46) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE: C4- SEAT TRACK CORRODED BETWEEN BS 1180 AND 1200 RBL 46 TO BE REPAIRED ON CUST CARD NR 561511. BLENDED CORROSION ON SEAT TRACK FLANGE AT BS 1190 RBL 46 REMOVED .20" ON A 1X 1.2" AREA ORIGINAL THICKNESS OF .085 WHICH IS OUT OF LIMITS PER SRM 53-00-52-1A1 FIG 101. DETAIL VII. SEAT TRACK WILL BE REPAIRED ON CUST CARD 561511 (INTERIOR 05138).

Part: BEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION STA 1007 RBL44. REPAIRED PER ER 05-4558.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION AT STA 1084. REPLACED SEAT TRACK IAW 51-40-02.

Part: BEAM — CORRODED (SECT 44) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 CORRISION OUT OF LIMITS ON LONGITUDINAL BEAM AT BS 1040 TO BS 1080 LBL 25 WL 208. REPLACED LONGITUDINAL BEAM.

Part: FLOOR PANEL — CORRODED (SECT 41) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C4 CONTROL CABIN FLOOR SURFACE CORRODED BS282 LBL 28 WL 200. REPAIRED PER SRM 51-70-13-00.

Part: ANCHOR — CORRODED (BULK CARGO) · airframe 22,061 hrs · 15,018 cycles

INSPECTION TYPE:C-4 BULK CARGO RT MBA TIE DOWN FITTING HAS CORROSION, STA 1460 AND STA 1480. REPLACED FITTING PER SRM 51-40-05-OG.

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

INSPECTION TYPE:N/A SMOKE GOGGLES AT AFT COURIER SEAT ARE CRACKED. REPLACED SMOKE GOGGLES.

Part: BRACKET — LOOSE (L1 DOOR)

INSPECTION TYPE:N/A ATB-UNABLE TO PRESSURIZE. MX SECURED L1 DOOR SWITCH BRACKET. REPLACED PROX SWITCH MOUNTING BRACKET IAW 757 SRM 51-40-02.

Part: BEAM — CORRODED (BS1200LBL47-62) · airframe 18,287 hrs · 12,377 cycles

INSPECTION TYPE:MOD UPON REMOVAL OF FLOOR PANELS FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM AT BS 1200 LBL 47 TO LBL 62 WL 208 CORROSION TO BE OUT OF LIMITS FABRICATE REPAIR ANGLE AND ACCOMPLISH ERO 02-0295

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,287 hrs · 12,377 cycles

INSPECTION TYPE:MOD UPON REMOVAL OF BALLMAT, FOUND CORROSION IN SEAT TRACK AT BS 614, LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 440 TO 680, LBL 45 PER SRM 51-40-02 AND SRM 53-00-52.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

INSPECTION TYPE:N/A PIREP-LEFT HYD QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE LIGHT ILLUMINATED (SHUT OFF ENG AND ELECTRICAL PUMPS WHEN PRESSURE LIGHTS ED). FOUND RT MLG DOWNLOCK ACTUATOR FLEX LINE WORN (LEAKING). REMOVED AND REPLACED LINE P/N -115-04K0232, HYDRAULIC SYS REPLENISHMENT PER MM 29-18 LT ENG DRIVEN HYD PUMP INSPECTED PER MM 29-11-05, NO CONTAMINATION NOTED SYSTEM TESTED SERVICEABLE.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

INSPECTION TYPE:N/A ATB-LOSS OF HYD FLUID. *S/D* INSTALLED TEMP FLEX LINE HOSE ON LT MLG SIDE STRUT ACTUATOR LEAK CHECKS OK. REMOVED AND REPLACED HYD PUMP AND FILTERS IAW MM 29-11-05, OPS AND LEAKS CHECK GOOD.

Part: BRACKET — CRACKED (CABIN)

INSPECTION TYPE:N/A OXY BOTTLE BRACKET CRACKED REPAIRED OXY BOTTLE BRACKET

Part: SENSOR — FAILED (NLG)

INSPECTION TYPE-N/A, EICAS MSG NOS A/G DISAGREE IN FLIGHT. REPEAT DISCREPANCY, S10067 FAILS NEAR TARGET TEST WITH NORMAL TARGET GAP VERIFIED. REPLACED FAULTY NOSE GEAR NOT COMPRESSED SENSOR, S10067 PER MM 32-09-08 EXCEPT FOR PERMANENT ELECTRICAL CONNECTION.

Part: SEAT TRACK — CORRODED (BS 1180)

INSPECTION TYPE-C, CORROSION ON SEAT TRACK AT BS 1180 LBL 45 WL 208 AROUND NUT PLATES. REMOVED CORRODED SEAT TRACK FROM BS 1180 TO 1320 AND INSTALLED NEW SEAT TRACK FROM BS 1180 TO 1320. ALL WORK DONE IAW SRM 51-40-02.

Part: BEAM — CORRODED (BS 900-1040)

INSPECTION TYPE-C, CORROSION ON LONGITUDINAL BEAM BS 900 TO 1040 AROUND NUT PLATES, LBL 45, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LMITS PER SRM 53-00-51. REMOVED AND REPLACED LONGITUDINAL BEAM PER SRM 51-40-02, EO 757-53-0048.

Part: BEAM — CORRODED (BS 1040-1076)

INSPECTION TYPE-C, CORROSION ON LONGITUDINAL BEAM BS 1040 TO 1076 LBL 45, WL 208 AROUND NUT PLATES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51. REMOVED AND REPLACED LONGITUDINAL BEAM IAW SRM 51-40-02.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER LIGHTS EICAS MSG SWITCH ARMED, NO UNARMED LIGHT ILLUMINATED. EMERGENCY EXIT LIGHT BATTERY PACK REMOVED AND REPLACED AS PER MM 33-51-07, AND OPS CHECKS GOOD.

Part: ENGINE — FAILED (NR 1)

INSPECTION TYPE-N/A, AIR TURNBACK DUE TO SMOKE IN COCKPIT AND MAIN CARGO FIRE WARNING. LEFT ENGINE LOST 8 QTS IN 16 MIN OF FLIGHT AND 45 MIN OF BLOCK TIME. CLIMBING THROUGH 12,000 FT MAIN CARGO FIRE WARNING CAME ON AND SMOKE ENTERED COCKPIT. ACCOMPLISHED CHECKLIST. REPLACED LT ENGINE PER TASK CARD 5001. RAN ENGINE PER TASK CARD 500 2, ENGINE RAN IN PARAMETERS.

Part: WEDGE — DELAMINATED (NR 3 LE SLAT)

DURING C-CHECK, MAINTENANCE FOUND NR 3 SLAT T/E WEDGE IS DELAMINATED AND EXCEEDS ALLOWABLE LIMITS. REPLACED SLAT PER MM 27-81-02.