N342UP

Part: FLAP — DAMAGED (ZONE 600) · airframe 34,472 hrs · 12,840 cycles

BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. REMOVED PANEL 666AT AND ROUTED TO SHEET METAL SHOP FOR REPAIR.

Part: FLAP — DAMAGED (ZONE 600 LE FLAP) · airframe 34,475 hrs · 12,842 cycles

BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLETED REPAIR TO LEADING EDGE PANEL PER SRM 51-70-05-0G-0 ALL STEPS OF REPAIR COMPLETE. REPAIR PLIES INSTALLED AND CURED. REAPPLIED PROTECTIVE COATINGS AND PERFORM POST REPAIR REQUIREMENTS. INSTALLED REPAIRED PANEL 666AT PER AMM 06-44-00-992-006 AND AMM 20-11-00-910-802

Part: FMC — FAULTED (ZONE 200) · airframe 33,566 hrs · 12,524 cycles

ATB FMC LOCKED UP WITH STBY ONE MSG PRESENT (FULL WRITEUP IN FAULT DESCRIPTION). + PERFORMED TROUBLE SHOOTING REF B767 FIM 34-61 FAULT TREE 854,NO FAULTS FOUND.REMOVED AND REPLACED L/H FMC REFB767AMM 34-61-01 9 (PRECAUTIONARY) OPS CHECK GOOD ATT.

Part: NONE — NONE (NONE) · airframe 32,562 hrs · 12,187 cycles

ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIEWED.

Part: SKIN — DEBONDED (NR 8 SLAT) · airframe 32,562 hrs · 12,187 cycles

DISBOND PNL, RT WING NR 8 L/E SLAT INBD, SIDE INNER UPPER WEDGE. INST THE EXT DBLR WITH FILM ADHESIVE & CURE IAW SRM 51-70-10-2R-0 PARA 18 & 20. PERFORMED NDT/UT FOR REWORKED AREA & 8" FROM WHERE EDGES OF HEAT BLANKET, IAW NDT MANUAL PT1 51-01-01 & 51-04-00 REV:139. NO DEFECT FOUND. CLEAN, SEAL & FINISH REP AREA IAW SRM 51-70-10-2R-0 PARA 22 REV.91. IAW AMM27-81-02-424-099 REV.144 STEP 3.A TO 3.H(16) INST RT WING NR 8 SLAT IAW AMM 27-81-02-424-099 REV.144 STEP 3.H(17) TO 3.I(13) ADJUST & TEST NR 8 SLAT RT WING RESULT CONDITION CK SATIS IAW AMM 30-11-06-404-009 REV 144 INST DUCT. CONDITION CK IAW AMM 30-11-00-790-801 REV 144, LEAK CK, TEST OF 8-9 ANTI-ICE DUCT, SATIS & NO LEAK FOUND.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 32,562 hrs · 12,187 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF STA 1197+22~STA 1197+110 LBL 55~LBL 77. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: ANGLE — CRACKED (ZONE 100) · airframe 32,562 hrs · 12,187 cycles

FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91 INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.251CGF AND CONDITION CHECK NORMAL. I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANEL AT STA 1578 LEFT SIDE TOTAL:2EA. AND CONDITION CHECK NORMAL.

Part: ANGLE — CRACKED (ZONE 100) · airframe 32,562 hrs · 12,187 cycles

FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 32,562 hrs · 12,187 cycles

FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.252YFF AND CONDITION CHECK NORMAL. I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANEL AT STA 1578 RIGHT SIDE TOTAL:2EA AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 32,562 hrs · 12,187 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF STA 1440~STA 1540 LBL 77.5~LBL 54.75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015, AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 32,562 hrs · 12,187 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 145T5876-68 PANEL NO: 241AFF STA 731~STA 834 LBL 11~RBL 11. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 32,562 hrs · 12,187 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-9 PANEL NO: 241KFF STA 1197+22~STA 1197+110 LBL 77~LBL 88. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015 AND AMM 25-58-01-404-005 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: PITOT HEAD — DAMAGED (ZONE 200) · airframe 11,425 hrs

LUZ DE CAPT PITOT ENCENDIDA DESPUES DEL ARRANQUE DE MOTORES, PROBETA DE TUBO PITOT DEL CAPITAN DAÑADA CAPT PITOT LIGHT ON AFTER STARTING, PITOT TUBE DAMAGED.

Part: FLOORBEAM — DAMAGED (BS 246 LBL53) · airframe 28,265 hrs · 10,488 cycles

INSPECTION TYPE:C6, DAMAGE ON M/D CARGO FLOORBEAM, BS 246, LBL 53. FABRICATED A REPLACEMENT IAW DWG 141T5146 SH 15 REV B, PL REV F AND PSDL REV-. REPLACED IAW SRM 51-40-02-0G-0 REV. 85.01.

Part: SEAL — DETACHED (L1 DOOR) · airframe 28,031 hrs · 10,391 cycles

INSPECTION TYPE:N/ACREW ENTRY DOOR SEAL MAKES VERY LOUD HISSING NOISE IN FLIGHT.PRESSURISATION OKAYFOUND CREW ENTRY DOOR BOTTOM SEAL DETACHED SECURED AND CLEANED DOOR SEAL PER AMM 52-09-01-424-019 FOUND SATIS

Part: APU — FAULTED (EMPENNAGE) · airframe 25,795 hrs · 9,599 cycles

INSPECTION TYPE:N/ASUPPLEMENTAL SDR**DIVERSION**EMERG DECLARED**A/C LANDED W/OUT INCIDENT**APU FAULT AT FL 390 DIVERTED TO STL. DEFERRED PER MEL 49-11-1A ASSIGNED M766577REPLACED APU COOLING FAN AMM 49-51-03-401 AND APU OIL COOLER AMM 49-27-09-404-011. OPS & LEAK CKS GOOD. THIS CLEARS M766577, PLACARD REMOVED. EFF SOURCE REF: IPC 49-51-00-01-046K AND 49-27-00-01-265.

Part: TIRE — DAMAGED (LANDING GEAR) · airframe 21,935 hrs · 8,142 cycles

INSPECTION TYPE:N/A** EMERGENCY DECLARED ** THE FIRE TRUCKS FOLOWED THE A/C TO THE RAMP & THE FIRE CHIEF DETERMINED IT WAS SAFE TO TAXI TO THE GATE & FOLLOWED THE AIRCRAFT TO THE GATE ** # 7 MLG TIRE HEATSHIELD DAMAGED.R & R'D # 7 MAIN WHEEL ASSY IAW MM 32-45-01-401, SPACER & WASHER VERIFIED INSTALLED. IPC 32-45-01-01B ITM. 051T.

Part: CONTROL MODULE — INOPERATIVE (RUDDER TRIM) · airframe 21,906 hrs · 8,130 cycles

INSPECTION TYPE:N/AHYDRAULIC POWER CAME ON PRIOR TO ENGINE START ON PUSHBACK, BOTH YOKES WENT 3/4 FULL LEFT TURN FOR NO REASON. A/P OFF.R/R AILERON RUDDER TRIM AILERON CONTROL MODULE PER AMM 27-21-23-022-001 & 27-21-23-422-007 OPS TEST AILERON & AILERON TRIM CONTROL SYS PER AMM 27-11-00-715-417 & OPS TEST RUDDER TRIM CONTROL SYS PER AMM 27-21-00-715-001-002.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,276 hrs · 7,526 cycles

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATT PACK PER AMM 33-51-07 OPS CHK GOOD. ESR: IPC 33-51-07-32.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,209 hrs · 7,123 cycles

EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-16-962-001 OPS CKS OK

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 18,653 hrs · 6,940 cycles

INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834-STA 930, LBL 11 - RBL 11, PNL NR 241FFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: SKIN PANEL — BROKEN (RT WING) · airframe 18,653 hrs · 6,940 cycles

INSPECTION TYPE:C4 BROKEN ON LOWER SKIN PANEL OF RT WING INBD AFT FLAP NEAR IFS 119.75. REPAIR IAW SRM 57-53-01 REPAIR 1, SRM 51-70-10 REPAIR 2, SRM 51-70-10 GENERAL, SRM 51-70-03 GENERAL, REV.73.01

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,389 hrs · 6,843 cycles

INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP W/ REF TO AMM. 33-51-16. LIGHT OPERATES NORMAL P/N ON/OFF 767.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 12,601 hrs · 4,668 cycles

MCD FLOOR PANEL PUNCTURED POSITION 2R, FABRICATED NEW PANEL IAW EO B767-5320-9693-I.

Part: FIRE LOOP — MALFUNCTIONED (RT NACELLE) · airframe 11,482 hrs · 4,160 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED THE RT FWD LOWER FIRE LOOP DETECTOR IAW AMM 26-11-02 AND TESTED NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 9,716 hrs · 3,550 cycles

DURING MAJOR MAINTENANCE VISIT NR 6749, FOUND DENT ON SKIN, BULK CARGO DOOR OUTER SURFACE, STA 1447, BETWEEN S-23L AND S-24 L/E, EVALUATED DAMAGE IAW SRM 52-30-01-1A-1, FIG 101, REF: TAIL VI, REV 61.00 INFORMATION SUBMITTED FOR ADM, DENT WITHIN ALLOWABLE DAMAGE, REF LOG PAGE 694809.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.

Part: LATCH — BROKEN (ESCAPE ROPE)

CAPTAIN'S OVERHEAD ESCAPE ROPE DOOR LATCH INOPERATIVE. OVERHEAD PANEL ASSY R & R IAW AMM TASK 25-1 4-02. ROPE INSTALLED IAW AMM TASK 25-61-02-682-001, REV 110, 02.

Part: FLOOR PANEL — DAMAGED

FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: SKIN — DENTED (LT NR 3 SLAT) · airframe 4,700 hrs · 1,702 cycles

A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 0.78" (LENGTH) X 0.55" (WIDTH) X 0.012" (DEPTH) AT OSS 801.5. REPAIR IAW 767-300F SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.

Part: SKIN — DENTED (LT WING SLAT) · airframe 4,700 hrs · 1,702 cycles

INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.88" (LENGTH) X 0.62"(WIDTH) X 0.025" (DEPTH) AT OS S 804.5 REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.

Part: WEDGE — DENTED (NR 3 SLAT) · airframe 4,700 hrs · 1,702 cycles

INSPECTION TYPE:C01, LT WING NR 3 SLAT T/E WEDGE ASSY UPPER SKIN DENTED AT OSS 819. DAMAGE SIZE IS MEASURED AS 1.0" (LENGTH) X 0.66"(WIDTH) X 0.013"(DEPTH) AND THE CUT OUT IS MEASURED AS 1" DIAMETER. REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4 FIG 201, REV 55.

Part: SKIN — DENTED (LT WING SLAT) · airframe 4,700 hrs · 1,702 cycles

INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 1.75"(LENGTH) X 1.5"(WIDTH) X 0.031"(DEPTH) AT OSS 807. REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.

Part: SKIN — DENTED (LT WING SLAT) · airframe 4,700 hrs · 1,702 cycles

INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.62" (LENGTH) X 0.55" (WIDTH) X 0.012"(DEPTH) AT OSS 805.5 REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.

Part: FLOOR PANEL — DENTED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL POS NR 12L OTBD HAS DENT CENTER OF PANEL. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A .5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693H, FABRICATED A REPL PANEL FROM A402H ACCOMPLISHED PARA B STEP 5&6 REF EO B767-5320-9695-H. INSTALLED INSERTS.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693 H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320-9695-H. INSTALLED INSERTS.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320--9693-H.