N463UP

Part: UNKNOWN — FUMES (ZONE 200) · airframe 38,823 hrs · 20,586 cycles

AT CRUISE LEVEL 300 SMELLED FUMES IN THE COCKPIT PERFORMED CHECKLIST CLEARED EMERGENCY AND LANDED IN IND. ACCCOMPLISHED CONDITIONAL INSPECTION PER MM 05-51-56-202. PERFORMED TROUBLESHOOTING PER FIM 21-00-01/801. INITIALLY FOUND OIL SMELL IN COCKPIT WHEN LEFT ENGINE WAS STARTED AND LEFT PACK OPERATED , SMELL DECCIPITATED AFTER A FEW SECONDS . CONTINUE TROUBLESHOOTING PROCEDURE PER FIM 21-00-01/301 RAN ENGINE AT TAKEOFF POWER PER AMM71-00-00 TEST 13. NO FUMES NOTED IN COCKPIT DURING ENGINE RUN. REVERSED DMP PERFORMED AMM 21-00-01-201 NO ODOR FOUND. PLACARD REMOVED

Part: UNKNOWN — ODOR (CABIN) · airframe 38,818 hrs · 20,584 cycles

EMERGENCY DECLARED. AT CRUISE LEVEL 300 SMELLED FUMES IN THE COCKPIT PERFORMED CHECKLIST CLEARED EMERGENCY AND LANDED IN IND.

Part: STRUT — GOUGED (ZONE 400) · airframe 38,295 hrs · 20,311 cycles

NR 2 ENGINE INBOARD PYLON GOUGED. ACCOMPLISHED REPAIR PER VT-SAA EA 757-5451-01-B0289 I/R AND EO-91693-REQ1, PRIOR TO FURTHER FLIGHT.

Part: THRUST REVERSER — DAMAGED (NR 1) · airframe 38,295 hrs · 20,311 cycles

UPON REMOVING AFT DAMAGED PANDOWN AT #1 ENG. O/B T/R, INNER BARREL, FOUND 3 EA DOUBLE DRILLED HOLES TO MATTING STRUCTURE. ATA 78-31. ACCOMPLISHED PERMANENT REPAIR PER VT-SAA EA 757-7830-01-B0287 IR AND EO-91497-REQ1, PRIOR TO FURTHER FLIGHT. ACCOMPLISHED EA 757-7830-01-B0287 P1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

CORROSION ON SEAT TRACK AT LBL 62 STA 1078-1184. INSTALLED NEW SEAT TRACK P/N 144N5016-3 IAW B757-200 SRM 51-40-02-0G-0. REINSTALLED DATTO PANEL AT MAIN CARGO LBL-62 STA-1060 TO STA 1180 IAW B757-200 SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

CORROSION ON FLOOR BEAM AT STA 1200 LBL 62 TO RBL 62. ACCOMPLISHED REPAIR PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAIR 6 FIGURE 201 REV 121.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

MAIN CABIN. SEAT TRACK HAS CORROSION LOCATED AT BL0 BETWEEN STA1160 AND STA1200. (015-43) ATA53. ACCOMPLISHED REPAIR PER 757-S00PF SRM REV 121 53-00-52-2R-7 REPAIR 7.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

MAIN CABIN. SEAT TRACK HAS CORROSION LOCATED AT LBL62 BETWEEN STA1140 AND STA1200. (015-45) ATA53. ACCOMPLISHED VT-SAA EA 757-5310-01-B0282 I/R AND EO-91510-REQ1, PRIOR TO FURTHER FLIGHT.

Part: THRUST REVERSER — DAMAGED (RIGHT) · airframe 38,295 hrs · 20,311 cycles

ENG#1 RH T/R TORQUE RING INNER FAIRING V BLADE NICK DAMAGE ABOUT 1 0' CLOCK POSITION (CT-10B) ATA 78 SKILL STR. ACCOMPLISHED REPAIR PER VT-SAA EA 757-7830-01-B0284 IR AND EO-91509-REQ1, PRIOR TO FURTHER FLIGHT.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

MAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1140 - 1200 LBL 48", INSTALLED SEAT TRACK SECTION BTW STA 1075.5 TO 1180 LBL 45.5 IAW B757PF SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

MAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1018 LBL 46. ACCOMPLISHED EA 757-5340-01-B0280 IR AND EO-91447-REQ1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,295 hrs · 20,311 cycles

MAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1140 - 1200 LBL 26" - LBL 40", 4-018 , ATA 53 SKILL STR. PERFORMED FPI PER SOPM 20-20-02 IAW 757 SRM 51-10-02-OG-0. NO DEFECTS NOTED AT SEAT TRACK FLANGE LBL 40 STA=1140 TO STA=1200. REVIEW COMPLETE

Part: BRACKET — CORRODED (APU FIREWALL) · airframe 38,295 hrs · 20,311 cycles

FWD FIRE WALL OF APU COMPARTMENT LWR BRACKET HAS CORROSION ATA 49. INSTALLED BRACKET FWD WALL APU COMPARTMENT, P/N 284N1489-6SAAU IAW B757-200 SRM 51-40-02-0G-0. INSTALLED PLACARD SERVICE INTERPHONE APU COMPARTMENT, P/N: BAC27NEX1404SAAU, PER BAC27NEX1404. INSTALLED FABRICATED STIFFENER AT FWD FIRE WALL OF APU COMPARTMENT. IAW B757-200 SRM 51-40-02-0G-0.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 37,722 hrs · 19,985 cycles

**ATB - EMERGENCY DECLARED**LOST CAPT AIRSPEED ON TAKEOFF, PERFORMED UNRELIABLE AIRSPEED V LIST, EICAS SHOWED RUDDER RATIO AND MACH IAS.ON CLIMB OUT F/O'S AIRSPEED DROPPED SIGNIFICANTLY, GOT F/O'S STICK SHAKER. AIR TURN BACK NOTE: RUDDER RATIO EICAS MSG ADDRESSED ON LINE ITEM #4. CW CAPT'S AND F/O'S ADC BITE TEST PER FIM 34-12 FAULT TREE 813, FIG 109. NO DEFECTS FOUND, PURGED LINES FROM CAPT'S AND F/O'S ADC PER AMM 34-11-01-167-004 TO PITOT TUBES, REMOVED ALL DEBRIS BLOCKING BOTH PITOT TUBES. CW PITOT PROBE TEST OF CAPT AND FO'S PITOTS. POS CK NORMAL PER AMM 34-11-01-755-033.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,285 hrs · 19,745 cycles

**SDR FILED OPEN**EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN ON POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07-902-001. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 36,062 hrs · 19,031 cycles

INSPECTION TYPE:CLEFT HOR. STAB. LWR SKIN HAS A NEW DENT 41 IN. FROM INBD EDGE AND 14 IN. FROM L/E.REPAIRED PANEL IAW B757 SRM 51-70-10-2R -4 PER SRM 55-10-01-1A.

Part: SKIN — CORRODED (NR 2 NACELLE) · airframe 36,062 hrs · 19,031 cycles

INSPECTION TYPE:SEG1#2 ENGINE OUTBD PYLON FWD OF PRECOOLER (INTERNAL) BETWEEN NAC STA 105.66 - 169.8 HAS CORROSION.WORK PER UPS EO B757-5430-84529-A, UPS RCD 279930 AND VT MAE EA 757-5450-27-A3002 REV-

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 36,062 hrs · 19,031 cycles

INSPECTION TYPE:SEG1#1 ENGINE PYLON OUTBD INNER SKIN FWD OF VENT PANEL $443CL HAS CORROSIONWORK PER UPS EO B757-5430-84530-A, UPS RCD 279965 AND VT MAE EA 757-5450-27-A3003 REV-

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 36,062 hrs · 19,031 cycles

INSPECTION TYPE:SEG1#1 ENGINE INBD PYLON INNER SKIN FWD OF PRECOOLER HAS CORROSION OUT OF LIMITSWORK PER UPS EO B757-5430-84537-A, UPS RCD 279961 AND VT MAE EA 757-5450-27-A3005 REV-

Part: FRAME — DENTED (BS 1460 S26L) · airframe 36,062 hrs · 19,031 cycles

INSPECTION TYPE:SEG1FRAME STA 1460 AT S-26L IS DENTED ON TOP OF FRAME FLANGE IN THE RADIUSACCOMPLISHED REPAIR IAW SRM 53-00-07-2R-5 DETAIL 1 AND RCD 279873

Part: STRAP — CORRODED (BS 620) · airframe 36,051 hrs · 19,027 cycles

INSPECTION TYPE:C13MAIN CARGO DOOR CUTOUT LOWER STRAP REPAIR AT STA 620, BETWEEN STR 24L AND STR 26L.WORKED, PER UPS EO B 757-5330-84558-A, UPS RCD 279834, AND VT MAE EA 757-5330-27-A3007 REV- FAA 8100-9

Part: FAN — NONE (CABIN) · airframe 35,442 hrs · 18,701 cycles

INSPECTION TYPE:NAAFT EQ EXHAUST FAN 2 STATUS MSGAFT EQUIPMENT EXHAUST FAN 2 OPS CHECKS GOOD. REF B757 FIM 21 20 00 815 802

Part: FAN — NONE (CABIN) · airframe 35,442 hrs · 18,701 cycles

INSPECTION TYPE:NAAFT EQ EXHAUT FAN STATUS MSGAFT EQUIPMENT EXHAUST FAN 1 OPS CHECKS GOOD REF B757 FIM 21-20-00-815-805

Part: NONE — NONE (LANDING GEAR) · airframe 34,824 hrs · 18,356 cycles

INSPECTION TYPE:N/A** ATB*SUPPLEMENTAL SDR*NO EMERG DEC'D* A/C LANDED WITHOUT INCIDENT**PILOT REPORTED GEAR DOOR NOT CLOSED. AFTER DEPARTURE FLIGHT CREW RECEIVED A GEAR DISAGREE & GEAR DOOR EICAS MSG. THEY DID NOT HAVE SUFFICIENT FUEL TO OPERATE TO SDF WITH GEAR DOWN.FOUND GEAR PINS INSTALLED LH MLG AND NLG. REMOVED IAW 757 AMM 32-00-20.

Part: FRAME — DENTED (BS 640) · airframe 33,223 hrs · 17,441 cycles

INSPECTION TYPE: SEG FWD CARGO RIGHT SIDE FRAME BENT AT STA 460 BETWEEN S-23R-S-24R. REPAIRED IAW UPS EO NO B757-5310-77954-A.

Part: SKIN — GOUGED (BS 1862-1870) · airframe 33,223 hrs · 17,441 cycles

INSPECTION TYPE: SE GLH FUSELAGE HAS WEAR GOUGE UNDER HORIZONTAL STAB AT STA AT 1862-1870. REPAIRED IAW B757-200PF SRM 53-80-01-2R-2 FIG 201 DETAIL II.

Part: SKIN — DAMAGED (BS 1862-1870) · airframe 33,223 hrs · 17,441 cycles

INSPECTION TYPE: SEG GROOVE WORN UNDER RT HORIZONTAL STAB ON SKIN AT STA 1862-1870. REPLACED IAW B757-200 SRM 53-80-01-2R-2 FIG 201 DETAIL II.

Part: FRAME — DENTED (FUSELAGE) · airframe 33,223 hrs · 17,441 cycles

INSPECTION TYPE: SEG DENT FOUND ON RT LOWER RIB AT STA 680 BETWEEN S-23R AND S-25R. REPAIRED IAW SRM 53-00-07-2R-5 DETAIL III, PER SRM 53-00-07-2R, IAW BOEING MESSAGE REF MOE-UPS-20-0045-02B.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 32,801 hrs · 17,201 cycles

INSPECTION TYPE:N/A EMERGENCY LIGHT EGRESS INOP. R&R LAMP IAW AMM 3351-06-962-001-003. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT MLG TRUCK) · airframe 32,554 hrs · 17,059 cycles

INSPECTION TYPE:N/AATB - RAISED GEAR HANDLE ON T/O GOT DISAGREE LIGHT & HANDLE WOULD NOT RAISE ABOVE OFF.REPLACED LEFT MAIN LANDING GEAR TRUCK POSITION ACTUATOR REF AMM 32 32 15 401 OP AND LEAK CHECKED GOOD EFF SOURCE REF 32 32 51 15 OP AND LEAK CHECK GOOD.Ï¿½Ï¿½IPC: 32-31-51-15

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,960 hrs · 16,150 cycles

INSPECTION TYPE:N/A L1 EMERGENCY EGRESS LIGHT INOP. RELAMPED L1 EMERGENCY EGRESS LIGHT REF MM CH 33 51 06 OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,497 hrs · 15,876 cycles

EMERGENCY LIGHT HAD FOUR INOPERATIVE BULBS. R & R THE BULBS IN THE EMERGENCY LIGHT IAW AMM 33-51-01-2.

Part: SKIN — DAMAGED (TE FLAP) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, RT IB MAIN FLAP LOWER SURFACE DAMAGE APPROX 1 FOOT OB OF FLAP CANOE FAIRING. REPAIRED LWR SURFACE PANRL PN 113N2402 IAW SRM 51-70-10-2R.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 242 XBF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 242 XMF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251XAF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XHF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XGF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PNAEL 251 XNF HAS CORRODED INSERTS AND DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XKF HAS DAMAGE INSERTS. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MIAN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 231 XDF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XDF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL 242 XFF IS DELAMINATED. FABRIBRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMP FLOOR PANEL 241 XGF IS DAMAGED. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMP FLOOR PANEL 252 XDF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252 XLF IS CRACKED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 221 XAF IS DELAMINATED. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL 251 XJF IS DELAMINATED. FABRICATED NEW PANEL.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252 XJF HAS CORRODED INSERTS. FABRICATED NEW FLOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252XKF HAS CORRODED INSERTS AND DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XPF HAS CORRODED INSERTS AND DAMAGE. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 XGF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232 XFF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252XEF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMP FLOOR PANEL 252 XCF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL 252 XAF HAS CORODED INSERTS. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252 XPF HAS CORODED INSERTS AND DAMAGE. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231 XUF IS DELAMINATED. FABRICATED NEW PANEL.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 251 XBF HAS CORRODED INSERTS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO, FLOOR PANEL 251 XCF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMP FLOOR PANEL 241 XFF IS DAMAGED. FABRICATED NEW FLOR PANEL.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPT FLOOR PANEL 252 XSF HAS CORRODED INSERTS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 CCF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR 221 XCF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232 XRF HAS CORRODED INSERTS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232 XTF HAS CORRODED INSERTS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 221 XBF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232 XEF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232 XDF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232XDF IS DELAMINATED. FABRICATED NEW PANEL.

Part: FLOOR PANEL — CORRODED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL 231 XLF HAS CORRODED INSERTS. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PNEL 231XEF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232 XAF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 222 XCF IS DELAMINATED. FABRICATED NEW FOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, FLOOR PANEL 212 XAF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231XEF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 XBF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 XAF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 XFF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 232 XGF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 231 XHF IS DELAMINATED. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL J41XEF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR 222 XAF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN DECK FLOOR PANEL 222 XBF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, FLOOR PANEL 232 XHF IS DELAMINATED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:C/CK, MAIN CARGO FLOOR PANEL 232 XVF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLOOR PANEL 252XNF HAS CORRODED INSERTS AND DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLOOR PANEL 251XLF HAS CORRODED INSERTS AND DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLOOR PANEL 251XRF HAS BROKEN INSERTS AND DAMAGE. FABRICATED NEW PANEL.

Part: FLOOR PANEL — NOT REPORTED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLOOR PANEL 252XRF. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN DECK FLOOR PANEL 251XQF DELAMINATED. FABBED PNL 251XQF AND CUT PER SREO B757-5320-9692-K

Part: INSERT — BROKEN (FLOOR PANEL) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLORR PANEL 252XUF HAS BROKEN AND CORRODED INSERTS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN CARGO COMPT FLOOR PANEL 251XEF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, FLOOR PANEL 211XAF DELAMINATED. FABBED PANEL 211XAF AND CUT PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN DECK PNL 231XJF DELAMINATED. FABBED PNL 231XJF AND STEP CUT PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG3, MAIN DECK FLOOR PANEL 232XJF IS DELAMINATED. FABBED PNL 232XJF AND STEP OUT PER SREO B57-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 30,487 hrs · 15,868 cycles

INSPECTION TYPE:SEG, MAIN DECK FLOOR PANEL 232XCF IS DELAMINATED. FABBED PNL 232XCF PER SREO B757-5320-9692-K.

Part: SCREW — MISSING (EXIT LIGHT) · airframe 30,358 hrs · 15,790 cycles

EXT EMERG EGRESS LIGHT ASSY MISSING 3 SCREWS. INSTALLED 3 EA MISSING SCREWS IAW MM 33-51-06-201-3.

Part: STRUCTURE — CORRODED (RAT DOOR) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2C, LOWER STRUCTURE AT RAT ACCESS DOOR CORRODED. FABRICATED NEW STRUCTURE IAW SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (BS 1180) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2, RT WING TO BODY FAIRING CORRODED. FABRICATED SUPPORT IAW SRM 71-70-12-0G.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2, MCD FLOOR PANEL 231XFF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2, FLOOR PANEL 231XJF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW EO 757-5320-9692-H.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2, MAIN CARGO DECK FLOORBOARD 242XJF DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 28,309 hrs · 14,549 cycles

INSPECTION TYPE: SEG2, FLOOR PANEL 242XCF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO 757-5320-9692-H.

Part: PITOT TUBE — OBSTRUCTED · airframe 28,088 hrs · 14,412 cycles

ON TAKEOFF AIRSPEED BECAME UNRELIABLE EICAS MESSAGE RATIO RATIO MACH SPEED TRIM A\S UNRELIABLE MESSAGES SHORT FINAL. WINDSHEAR WARNING F/O AIRSPEED BECAME UNRELIABLE ON SHORT FINAL. FOUND DEBRI ON CAPTAINS F/O AND AUX PITOT TUBES FLUSH THE PITOT STATIC SYS IAW MM 34-11-00-173-009, CLEAR MESSAGE IAW FIM 31-41-00-815-811.

Part: SLEEVE — CORRODED (THRUST REVERSER) · airframe 26,817 hrs · 16,623 cycles

INSPECTION C9, NR 2 ENGINE INBD THRUST REVERSER UPPER AFT OUTER SKIN CORRODED. REPLACED THRUST REVERSER SLEEVE IAW AMM 78-31-23.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 26,817 hrs · 13,623 cycles

INSPECTION C9, MAIN CABIN FLOORBOARD 242XCF EDGE IS BROKEN. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 26,817 hrs · 13,623 cycles

INSPECTION C9, MAIN CABIN FLOORBOARD 242XGF EDGE IS BROKEN. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS)

PS-1 INSPECTION, EMERGENCY LIGHTS "UNARMED" OVERHEAD LIGHT IS HALF-LIT. R & R EMERGENCY LIGHTS PANEL IAW AMM 31-51-08-004-001. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (BS 213)

FUSELAGE SKIN DAMAGE, BS 213. REPAIRED IAW EO B757-5330-39184-B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MCD FLOOR PANEL 221XCF HAS EDGE DAMAGE. DOT 11-71, FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MCD FLOORBOARD 222XCF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO 757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, CABIN FLOOR PANEL 231XFF IS DELAMINATED ON THE EDGES. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MCD FLOOR PANEL 232XHF UPPER SKIN RIPPED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MAIN CARGO DECK FLOOR PANEL 231XMF BROKEN. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN CARGO DECK FLOOR PANEL 232XRF UPPER SKIN RIPPED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MCD FLOOR PANEL 232XUF UPPER SKIN RIPPED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MAIN CARGO FLOOR PANEL 232XMF UPPER SKIN RIPPED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MAIN CARGO FLOOR PANEL 232XJF HAS A HOLE DRILLED WHERE NO FASTENER IS LOCATED AND EDGES ARE WORN. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (BS 440) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 232XAF FWD EDGE BS 440, DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS440-480) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, MAIN DECK FLOOR PANEL 231XAF BS 440-480 DAMAGED ON ALL FOUR SIDES. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 232XFF SCREW INSERT MISSING. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — BROKEN (BS 879) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL, 231XWF, BS 879 HAS FOUR SCREW INSERTS MISSING NR 53-93. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 820-900) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 231XTF, BS 820-900, DAMAGED ON ALL FOUR EDGES AND MISSING A SCREW INSERT. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN CARGO FLOOR PANEL 241XMF IS MISSING INSERTS AND HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 440) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: C8, MAIN DECK FLOOR PANEL 232XBF FWD EDGE BS 440, DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN CARGO FLOOR PANEL 232XSF HAS MISSING INSERTS AND EDGE DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — WORN (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE :S4C8, MAIN CARGO COMPARTMENT FLOOR PANEL 251XCF HAS WORN EDGES. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 440) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 222XAF AFT EDGE BS440 DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 879) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL, 232XYF, BS 879 HAS A SCREW INSERT MISSING. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 440) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 221XAF AFT EDGE BS 440 DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN CARGO FLOOR PANEL 241XDF HAS BROKEN INSERTS AND EDGE DAMAGE. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (BS 440) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, MAIN DECK FLOOR PANEL 231XBF, BS 440 DAMAGED AT INBD EDGE FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, FLOOR PANEL 251XRF AT BS 1680-1720, BL-0 TO LBL-45 IS DELAMINATED ON FWD CORNER AND HAS BROKEN AND MISSING INSERTS. FABRICATED NEW FLOOR PANEL IAW EO B757-53 20-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, COURIOR COMPARTMENT FLOOR PANEL 211XAF HAS DAMAGED EDGES AND LOOSE INSERTS. FABRICATED NEW FLOOR PANEL IAW EO B757-53 20-9692-H.

Part: FLOOR PANEL — DAMAGED (BS 560-620) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, FLOOR PANEL 231XJF BS 560-620 HAS SPOT OF DELAMINATION AND DAMAGED ON ON EDGE. FABRICATED NEW FLOOR PANEL.

Part: FRAME — CORRODED (BS 1825 S3R) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE:S4C8, APU INLET DOOR HSG CUT-OUT FWD FRAME CORRODED. REMOVED AIR INTAKE HSG IAW 49-15-08-004-001, EMP: 05948. UPON REMOVAL OF AIR INTAKE HSG FOUND MORE CORROSION ON THE MATING SURFACES OF THE UPPER LOWER AND AFT SUPPORT FLANGES. REMOVED 9EA NUT PLATES FOR ACCESS, REMOVED CORROSION IAW SRM 51-40-02-06. ON UPPER SUPPORT FLANGES, REMOVED CORROSION IAW SRM 51-10-02 ORG MAT .063", DIME.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,652 hrs · 12,838 cycles

INSPECTION TYPE: S4C8, DENT ON LOWER SKIN OF LT INBD MAIN FLAP AT MF STA 130.0. DENT 1.25" X .75" X .035 DEEP WITH A SMALL PUNCTURE DRILLED .0625 DIAM HOLE TO CLEAN UP PUNCTURE, FABRICATED REPAIR PARTS IAW 51-70-10-2R-REP NR 2.

Part: FRAME — DENTED (BS 1300) · airframe 23,259 hrs · 11,878 cycles

INSPECTION TYPE:C3, AFT PIT STA 1300, RBL 26", FRAME DENTED REPAIRED IAW EA 110056 AND EO B757-5310-41366.

Part: FRAME — DENTED (BS 1280) · airframe 23,260 hrs · 11,878 cycles

INSPECTION TYPE:C, AFT PIT FRAME STA 1280 LBL 27" DENTED. REPAIRED IAW EA110055 AND EO B757-5310-41382.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 23,260 hrs · 11,878 cycles

INSPECTION TYPE:C, RT WING OTBD AFT FLAP BOTTOM SURFACE DELAMINATED 24" OTBD FROM INBD EN END AND 4" FWD. FROM T/E REPAIRED IAW SRM-57-53-01-2R1 AND 51-70-04-G.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 23,260 hrs · 11,878 cycles

INSP TYPE:C, LT WING INBD T/E FLAP DAMAGE. REPAIR EA 110065 AND EOB757-5750-41387.

Part: SKIN — PUNCTURED (BS 213 S23L)

0.80 HOLE PUNCTURED THROUGH ACFT SKIN BY AIRSTAIR AT APPROX STA 213, S STR 23L CUTOUT DAMAGE IAW SRM 53-00-00-01, THIS REPAIR IS CLASSIFIED AS A MAJO R REPAIR IAW GMM 03.43.01.04. TRANSFERRED TO NRC 34 6743

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

EXTERIOR EMERGENCY EGRESS LIGHT INOP. RELAMPED PER AMM 33-51-06-2. OPS CKS NORMAL.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS)

INSPECTION TYPE:N/A NO AIRSPEED IND ON CAPT'S SIDE. RUDDER RATIO LIGHT AND MACH SPEED TRIM LIGHT CAME ON. CAPT'S AIRSPEED START TO INCREASE AND GOT IAS DISAGREE MSG. UNABLE TO USE CENTER A/P. AUTOTHROTTLES WENT FWD MAX THRUST (DISCONNECTED THEM. A/P DISCONNECT HORN GOING OFF AFTER CLICKING OFF TWICE. FINALLY TURNED OFF. FLUSHED CAPT'S PITOT AUX-1 SY. FOUND CONTAMINATION. CLEARED PITOT LINE PER MM 34-11-00/401. TEST PITOT SYS PER MM 34-11-00-501. CAPT AUX-1 SYS OPS CHECK GOOD.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN IS DENTED AND GOUGED 15 INCHES FROM SPAR AND 80 INCHES FROM FUSELAGE. REPAIRED SKIN PER SRM 51-70-10-2R-2 PAR 4D CONTROL 09-1327.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO DOOR CUTOUT UPPER SILL UPPER SURFACE AT WIRE STANDOFF BS 587 RBL 62 WL 201. REMOVED CORROSION, HFEC, INSTALLED REPAIR DOUBLER IAW SRM 51-70-13-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 765-840 LBL 21 WL158. REPAIRED PER EO B757-5330-32143A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 500-645 LBL 21 WL 158. REPAIRED PER ATS ENGINEERING REPAIR 09-1290 DATED 2-3-09.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT 645-765 LBL 21 WL 158. REPAIRED PER ATS ENGINEERING NR 09-1290 DATED 2-3-09.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 645-765 RBL 21 WL 158. REPAIRED PER ATS ENGINEERING NR 09-1291 DATED 4FEB2009.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 620-645 RBL 21 WL 158. REPAIRED PER ATS ENGINEERING REPAIR NR 09-1291 4FEB2009.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 765-840 RBL 21 WL 158. REPAIRED PER ATS ENGINEERING REPAIR NR 09-1291 DATED 04FEB2009.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 645-765 RBL 21, WL 158. REPAIRED PER ATS ENGINEERING REPAIR 09-1291 REV A DATED 2-6-09.

Part: BRACKET — BROKEN (NR 1 ENGINE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 UPPER TURBINE CASE DRAIN TUBE BRACKET BROKEN NR 1 ENGINE. REMOVED, FABRICATED, INSTALLED BRACKET PER M/M 78-11-04-8.

Part: MOUNT BRACKET — CRACKED (LT MLG) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 LEFT MAIN LANDING GEAR WHEEL WELL, LEFT SYSTEM HYDRAULIC MODULE MOUNTING BRACKET IS CRACKED. REPLACED BRACKET PER SRM 51-40-02-0G.

Part: SKIN — DAMAGED (TE FLAP) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 RT WING I/B FWD FLAP T/E UPPER SURFACE I/B OF AFT FLAP HAS A LIGHTNING STRIKE. REPAIRED PER SRM 51-70-10-2R2 REV 73 SEP 2008.

Part: SKIN — DAMAGED (RT AILERON) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 RT AILERON HAS LIGHTNING STRIKE DAMAGE ON UPPER T/E SURFACE 8 INCHES I/B OF THE O/B END. REMOVED AND REPLACED CONDUCTIVE FRAME PER SRM 51-40-02-0G, AMM51-21-10-7 SRM 51-60-01-0G.

Part: FRAME — GOUGED (FUSELAGE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR LWR FRAME ANGLE BS 488 STR 14-15L IS GOUGED IN 3 PLACES. REPAIRED PER SRM 51-40-02, SRM 51-40-05 AND DRAWING 65-25327.

Part: STRAP — BROKEN (LE SLAT) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 NR 9 SLAT L/E ACCESS PANEL (TAI ACCESS) LWR SUPPORT STRAP IS BROKEN. REPLACED WITH NEW STRAP.

Part: PANEL — CORRODED (RT WING) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 RT WING FUELING PANEL (AROUND GAUGES) HAS SURFACE CORROSION. REMOVED RT WING CORRODED FUELING PANEL AND INSTALLED NEW RT WING FUELING PANEL IAW AMM28-21-08-4.

Part: SKIN — DENTED (TE FLAP) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 LT WING O/B AFT FLAP LWR SURFACE T/E HAS DISBONDED DENT 27.5 INCHES I/B OF O/B END, AND 8.5 INCHES FWD OF T/E. REPAIR PER SRM 57-53-2R-1, SRM 51-70-04 FIG 5.

Part: RETAINER — CRACKED (RT ENGINE) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 RT ENGINE I/B C-DUCT AFT LWR SEAL RETAINER IS CRACKED. REMOVED AND REPLACED PER SRM 51-40-02-0G.

Part: SKIN — DENTED (TE FLAP) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 LT WING O/B AFT FLAP LWR SURFACE T/E HAS DISBONDED DENT 13.5 INCHES O/B OF I/B END, AND 12 INCHES FWD OF AFT EDGE. REPAIR PER SRM 57-53-2R-1, SRM 51-70-04 FIG 5.

Part: CAM — GOUGED (CREW ENTRY DOOR) · airframe 20,707 hrs · 10,391 cycles

INSPECTION TYPE:C2 CREW ENTRY DOOR UPPER LATCH CAM IS GOUGED. ALL WORK ACCOMPLISHED PER SRM ADDENDUM B757-5210-14721 AND AMM 51-12-00-5.

Part: SKIN — PUNCTURED (BS 213 S23L)

.80 DIA HOLE PUNCTURED THROUGH ACFT SKIN BY AIRSTAIRS DURING STORM AT APPROX STA 213, STR 23L. CUT DAMAGE AREA IAW SRM 53-00-01-2R. HFEC AREA IAW 757 NDT PART 6, 51-00-19-DD. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 03-43-01-4. TRANSFERRED TO NRC 346743.

Part: ENGINE — DAMAGED (LEFT)

LEFT ENGINE SHUT DOWN PER QRH. EMERGENCY DECLARED DUE TO LARGE BIRD ST STRIKE ON FIRST OFFICER'S NR 1 WINDOW. EICAS MSGS APPEARED. OIL PRESSURE FOR LEFT ENGINE WAS AT 0 AND THE EGT AT 165. [SUP 05-07-07] R & R LEFT ENGINE PER T/C 5001/5002RR AND ALL APPLICABLE MM REFERENCES. CHECKS GOOD.