N358UP

Part: PANEL — CRACKED (COMBUST SECTION) · airframe 29,579 hrs · 10,661 cycles

NUMBER 2 ENG BETWEEN 9 & 8 O CLOCK 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 9/8 O'CLOCK POSITION ON THE COMBUSTION OUTER LINER. ITEM DEFERRED WRT B767 MM 72-00-00-206-361-H00 TABLE 684.

Part: PANEL — CRACKED (COMBUST CASE) · airframe 29,579 hrs · 10,661 cycles

NUMBER 2 ENGINE BETWEEN 4 & 5 O`CLOCK, PANELS CRACKED OUTTER PANEL BY LWD IGNITER PLUG. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 4/5 O'CLOCK POSITION ON THE COMBUSTION OUTER LINER. ITEM DEFERRED WRT B767 MM 72-00-00-206-361-H00 TABLE 684.

Part: PANEL — CRACKED (COMBUST SECTION) · airframe 29,579 hrs · 10,661 cycles

NUMBER 2 ENG BETWEEN 5 & 6 O CLOCK POS 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 5/6 O'CLOCK POSITION ON THE COMBUSTION OUTER LINER. ITEM DEFERRED WRT B767 MM 72-00-00-206-361-H00 TABLE 684.

Part: PANEL — CRACKED (COMBUST SECTION) · airframe 29,579 hrs · 10,661 cycles

NUMBER 2 ENG BETWEEN 2 & 4 O CLOCK 2 PANEL CRACK OUTTER PANEL ABOVE IGNITER PLUG. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 2/4 O'CLOCK POSITION ON THE COMBUSTION OUTER LINER. ITEM DEFERRED WRT B767 MM 72-00-00-206-361-H00 TABLE 684.

Part: PANEL — CRACKED (COMBUST SECTION) · airframe 29,579 hrs · 10,661 cycles

NUMBER 2 ENG BETWEEN 12 & 1 O CLOCK 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACK(S) ON PANELS 1 AND 2 AT THE 12/1 O'CLOCK POSITION ON THE COMBUSTION OUTER LINER. ITEM DEFERRED WRT B767 MM 72-00-00-206-361-H00 TABLE 684.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

DENT - PANEL, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NO. 241ZFF BETWEEN STA 977 AND STA 1114, LBL 54.75 ~ LBL 77.5, P/N : 145T5876-77 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-000-801 REV.144 REMOVE MAIN DECK CARGO FLOOR PANEL SEALANT AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

DENT - PANEL, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NO. 242UFF BETWEEN STA 977 AND STA 1114, RBL 54.75 ~ RBL 77.5, P/N : 145T5876-76. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. MAJOR REPAIR ACCOMPLISHED PER SREO-9693-REQ001.

Part: SEAL — BROKEN (ZONE 800) · airframe 28,455 hrs · 10,286 cycles

AERODYNAMIC SEAL BROKEN , FWD LH ENTRY DOOR. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.141T6121 SH 13 REV: B. I.A.W AMM 52-12-01-404-024 REV. 144 INSTALL FWD LH ENTRY DOOR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-136 PANEL NO: 252WFF. (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-404-016, AMM 25-57-07-404-017, AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,326 hrs · 10,239 cycles

FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 RBL 74 OUTBD SIDE. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T5650 SH 5 REV: C.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-19 PANEL NO: 251QFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-57-07-404-017, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-27 PANEL NO: 251VFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-57-07-404-017, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,326 hrs · 10,239 cycles

FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 LBL 74 INBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T5650 SH 5 REV: C. I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANELS AT STA 1578 LEFT SIDE 2EA AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-109 PANEL NO: 232GFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-404-016, AMM 25-57-03-404-005, AMM 25-58-01-404-018 AND AMM 25-58-05-404-062 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR REPAIR PER SREO-9693-REQ001.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,326 hrs · 10,239 cycles

FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 LBL 74 OUTBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO:146T5650 SHEET 5 REV. C.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,326 hrs · 10,239 cycles

FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 RBL 74 INBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T5650 SH 5 REV: C. I.A.W AMM 25-59-01-004-001 REV.144 REMOVE MAIN DECK CARGO DADO PANELS AT STA 1578 RIGHT SIDE 2EA AND PERFORM G.V.I CHECK RESULT WAS NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-58 PANEL NO : 231RFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: SEAL — BROKEN (ZONE 800) · airframe 28,326 hrs · 10,239 cycles

AERODYNAMIC SEAL BROKEN , FWD LH ENTRY DOOR. (REPLACE) 1.REMOVED ENTRY DOOR LINER I.A.W AMM 52-12-01-004-001 REV.144 AND G.V.I CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-135 PANEL NO : 251XFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-404-016, AMM 25-57-07-404-017, AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-63 PANEL NO : 231EFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.231EFF , P/N:143T5876-63 AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 145T5876-59 PANEL NO : 242EFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.242EFF , P/N:145T5876-59 AND CONDITION CHECK NORMAL.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 28,326 hrs · 10,239 cycles

FAULT - CRACK, CENTER WING FRONT SPAR STIFFENR AT STA 785.9 LBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV.91 AND EGAT WORK SHEET NO. 50137, UPS SREO-58151-REQ001 REV1, BOEING DWG NO. 111T5200 SH 2 REV: B, 140T0520 SH 23 REV: -, 111T2000 SH 20 REV: F, SH 21 REV: J AND SH 22 REV: G. PAPER FINAL CHECK COMPLETED.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-110 PANEL NO : 251TFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.251TFF , P/N:146T5869-110 AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,326 hrs · 10,239 cycles

FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-134 PANEL NO : 252UFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.252UFF , P/N:146T5869-134 AND CONDITION CHECK NORMAL.

Part: A/C PACK — ODOR (ZONE 100) · airframe 27,407 hrs · 9,886 cycles

STRONG OIL FUME SMELLS WHEN RUNNING LEFT PACK. DISCONTINUED USING LEFT PACK ++ PERFORMED PACK OPS CHECK IAW AMM 21-32-00 NO DEFECT WAS NOTED. RUN LEFT PACK FOR OVER 1 HOUR IN DIF TEMP SETTINGS. NO OIL OR UNUSUAL SMELL WAS NOTED. OPS CHECKED GOOD. SUSPECT BAD GROUND AIR CART AT DEPARTURE GATEWAY

Part: SEAL — LEAKING (PAX DOOR) · airframe 23,223 hrs · 8,320 cycles

ENTRY DOOR SEAL LEAKING AIR PRESSUREFOUND APPROX 10 INCHES OF SEAL PULLED OUT ON BOTTOM ENTRY DOOR. RE-SEATED SEAL IN REF TO AMM 52-09-01-424-019.

Part: NONE — NONE (COCKPIT) · airframe 22,875 hrs · 8,170 cycles

INSPECTION TYPE:N/A**SDR FILED OPEN**ACRID "ELECTRICAL BURNING SMELL" IN OVERHEAD CB PANEL. ACCOMPLISHED SMOKE AND FUMES CONDITIONAL INSPECTION IAW AMM 05-51-56-202-001. FOUBD TO BE FUME SMELL FROM APU BLEED. DEFERRED APU BLEED IAW MEL 49-11-1-1. C/W DMP 49-11-1-1. M790065 ASSIGNED

Part: ENGINE — SURGES (LEFT) · airframe 21,412 hrs · 7,623 cycles

INSPECTION TYPE:N/A**IFSD**DIVERSION**EMERG DECL'D* REQ'D RADAR VECTORS*SUPPLEMENTAL SDR** A/C LANDED W/OUT INCIDENT**A/C OOS**ABNORMAL ENGINE INDICATIONS DURING CLIMB OUT OF EWR. EGT AND N1 ABNORMAL SURGE. PER QRH ENGINE SURGE CHECKLIST. LEFT ENG SHUTDOWN. DIVERT A/C INTO PHL.REMOVED AND REPLACED #1 ENGINE IAW B767 T/C'S 6001 AND 6002. OPS AND LEAK CHECKS GOOD. SN ON 707134 SN OFF 707254.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 19,752 hrs · 7,029 cycles

INSPECTION TYPE:C4CRACK ON LEADING EDGE SKIN OF NO.6 SLAT NEAR ISS 300.REPAIR I.A.W. BOEING SR:3-5034298589 AND UPS EO B767-5750-80466-A

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 18,610 hrs · 6,631 cycles

INSPECTION TYPE: N/A P5 OVERHEAD EMERGENCY SIGN ARM SWITCH INTERMITTENT. R & R EMERGENCY LIGHTS PANEL AND OPERATIONS CHECK OK, IAW AMM 33-51-08 ESR: IPC 31-12-11-66A-010.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,421 hrs · 5,847 cycles

INSPECTION TYPE:N/A**DIVERSION** DURING APPROACH TO MMX UPON SELECTING FLAPS 25, EICAS ALERT "LEADING EDGE SLAT ASYMETRY" DISPLAYED.FSEU: T/S IAW FIM 27-51-00-815-809 REV 129.00. FOUND LAST LEG FAULT 27-810343 LE INBD SLAT (REF BLOCK 73), NEXT STEP GO TO FIM 27-81-00/101 FIG 106 FOUND NO SENSOR FAULTS. PSEU BITE PROC IAW FIM 32-09-00-815-803-001 REV 129.00 PERF. NO FAULTS FOUND. T/S IAW FIM 27-81-00-815-809 REV 129.00 PERFORMED.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 14,839 hrs · 5,311 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHTS PANEL INTEGRAL LIGHTS INOPC/W E/O B767-3310-72533A

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 14,025 hrs · 4,997 cycles

MAIN CARGO COMP FLOOR PANEL REPAIR POSITION 11L/12L. FABRICATED FLOOR PANEL IAW EO B767-5320-9696-I ** SUPPLEMENTAL SDR**REPAIR COMPLETED ON NON ROUTINE 591343. THIS CLEARS M629696

Part: WINDOW — INOPERATIVE (L1) · airframe 13,721 hrs · 4,890 cycles

LEFT SIDE WINDOW HEAT INOPERATIVE DURING FLIGHT. QRH PROCEDURE DID NOT RESOLVE THE PROBLEM. REPLACED THE L2 WINDOW ASSY IAW AMM 56-11-02-401.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,591 hrs · 4,848 cycles

EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW M/M 33-51-16-962-001, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,591 hrs · 4,848 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM 33-51-16-962-001, OPS NORMAL.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI-SKID SYSTEM) · airframe 13,119 hrs · 4,682 cycles

ANTI-SKID EICAS ENROUTE FOR 1-2 MINUTES, THEN CLEARED ITSELF. EMERGENCY DECLARED. ON TOUCHDOWN, DID NOT GET SPOILER DEPLOYMENT. MANUALLY DEPLOYED SPOILERS. R & R THE ANTI-SKID, AUTOBRAKE CONTROL UNIT IAW AMM 32-42-01-004-001. OPS CHECKED GOOD.

Part: PROBE — FAULTY (TAT) · airframe 12,399 hrs · 4,426 cycles

ATB - CLIMBING ABOVE 12,000 FT TAT PROBE ECIAS MESSAGE WITH AN OVERHEAD TAT LIGHT ILLUMINATED AIRSPEED BUG FAILED ALONG WITH AUTOPILOT WE ALSO LOSS LNAV & VNAV AND AUTO THROTTLES ACCOMPLISHED AUTOFLIGHT BITE PER AMM 22 00 02 FOUND SYSTEM CODES 311661, 210401 AND 220401 ALL CODES DEFINE TAT FAILURE REMOVED & REPLACED TAT PROBE IAW MM 34 12 02/401 ACCOMPLISHED NECESSARY GROUND TESTS PER AMM 22 00 02 ALL TETS GOOD A/C OK FOR SERVICE EFF SOURCE REF 34 12 02 01A 005

Part: WARNING LIGHT — ILLUMINATED (CAPTAIN'S EVAS)

CAPTAIN'S EVAS INOPERATIVE. R & R EVAS BOX IAW AMM 25-69-00-4, REV 112.01. OPS CHECKED OK. T