N306UP

Part: PAWL — FAULTED (ZONE 800) · airframe 74,493 hrs · 24,901 cycles

MAIN CABIN DOOR WON`T CLOSE. R & R ENTRY/SERVICE DOOR INTERLOCK PAWL PER AMM 52-11-26/401. OPS CHECK GOOD REF AMM 52-11-26-710-801.

Part: SKIN — DENTED (ZONE 100) · airframe 74,071 hrs · 24,720 cycles

MAJOR REPAIR, FOUND DENT AT STA 570 A/C LEFT 13.5" BELOW SKIN LAP JOINT REPAIRED DAMAGE IAW EO-92838-REQ2

Part: TEE FITTING — CRACKED (ZONE 500) · airframe 73,142 hrs · 24,371 cycles

CRACK , SUPPORT STRUT AT L/H WING FAIRING PANEL 195CL. (REPLACE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92500-REQ1 REV. 1. INSTALLED REPAIR PARTS I.A.W SRM 51-40-02-0G REV. 91. AND BOEING DWG NO. 149T7500 SH. 3 REV. C AND 149T7500 SH. 2 REV. K. JOB COMPLETED. ATTACHEMENTS ARE UPLOADED.

Part: NONE — NONE (NONE) · airframe 73,142 hrs · 24,371 cycles

ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.

Part: PANEL — CRACKED (ZONE 100) · airframe 73,142 hrs · 24,371 cycles

FAULT - FOUND THE BALL MAT FLOOR STRUCTURE CRACK AT AFT CARGO STA 1336 BL 0 (REPLACE). FABRICATE PARTS (P/N:451T2603-65) PER BOEING DWG NO: 451T2603 DWG SH 11 REV."-"; PL REV."AP"; AND PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV.9 REQUIREMENT AND EGAT WORK SHEET NO. 50010. INSTALL FABRICATED PART I.A.W SRM 51-40-02-0G REV. 91 AND BOEING DWG 451T2612 SHEET 2 REV.B. JOB COMPLETED. REVIEW COMPLETE

Part: ANGLE — CRACKED (ZONE 100) · airframe 73,142 hrs · 24,371 cycles

FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT OUTBOARD AREA STA 1578 LBL 60. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED 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 DADO PANEL. JOB COMPLETED. ATTACHEMENTS ARE UPLOADED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 73,142 hrs · 24,371 cycles

FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT OUTBOARD AREA STA 1578 RBL 60. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED 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 DADO PANEL. JOB COMPLETED. ATTACHEMENTS ARE UPLOADED.

Part: CYLINDER — CORRODED (RT MLG) · airframe 73,142 hrs · 24,371 cycles

FOUND OUTER CYLINDER INNER SURFACE CORROSION OF RIGHT MAIN GEAR. (EVALUATE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92452-REQ1 REV. 1. JOB COMPLETED.

Part: RIB — CRACKED (ZONE 500) · airframe 73,142 hrs · 24,371 cycles

FAULT - CRACK - CHORD, L/H WING OUTBD L/E UPPER RIB LOWER CHORD, OSS 531.71. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 91. AND BOEING DWG NO. 114T2206 SH. 1 REV. B. JOB COMPLETED. REVIEW COMPLETE.

Part: SKIN — DEBONDED (ZONE 300) · airframe 73,142 hrs · 24,371 cycles

DISBOND FOUND RUDDER R/H SPAR AND ADJACENT STRUCTURE BETWEEN RUDDER STATION 106 AND STATION 181. (REPAIR). REPAIR DELAMINTION ON RH RUDDER SKIN PANEL AT RUD STA 140.108 I.A.W. UPS EO-92480-REQ1 REV1. CONDITION CHECK IS SATISFACTORY.

Part: LATCH — CORRODED (ZONE 100) · airframe 73,142 hrs · 24,371 cycles

CORROSION - LATCH, KEEL BEAM AFT SECTION PANEL 149BL AFT SIDE. (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.145T8629 SH 3 REV: C. JOB COMPLETED.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 73,142 hrs · 24,371 cycles

FOUND MAIN DECK FLOOR PANEL DENT, P/N:146T5869-9 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV 144 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 73,142 hrs · 24,371 cycles

FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-68 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV 144 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 73,142 hrs · 24,371 cycles

FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-19 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV 144 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 73,142 hrs · 24,371 cycles

FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-82 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-58-01-404-018 AND AMM 25-58-05-404-026 AND AMM 25-58-05-404-052 REV 144 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — DENTED (ZONE 100) · airframe 73,142 hrs · 24,371 cycles

*SDR FILED OPEN* REF BARCODE T3F18E005AYYG DENT ON TAIL OF FUSELAGE, TO THE LEFT OF TAIL SKID. APPROXIMATELY 6" FORWARD OF STRINGER AT ST 1702.0. RE-OPENED DUE TO REVISED RECURRING INSPECTION ADJUSTMENT. REPAIR IAW: SRM 53-00-01-2R-10 REPAIR MATERIAL: -1 DOUBLER 0.063IN 2024-T3 CLAD -2 BACR15FV()KE RIVETS THIS IS A CATEGORY A REPAIR. THE INSPECTION GIVEN IN THE MAINTENANCE PLANNING DATA (MPD) ARE SUFFICIENT TO MAINTAIN THE DAMAGE TOLERANCE OF THE INITIAL STRUCTURE WITH THIS REPAIR INSTALLED.

Part: SEAL — LOOSE (CREW DOOR) · airframe 72,154 hrs · 24,004 cycles

CREW ENTRY DOOR SEAL LOOSE ON THE UPPER FORWARD PORTION OF THE DOOR WHEN DOOR IS CLOSED. FOUND DECORATICE AND PROTECTIVE RUBBER SEAL INSIDE OF DOOR MOVED OUT OF RETAINER. AFFECTED SEAL IS NOT RESPONSIBLE FOR SEALING OF CABIN PRESSURIZATION. RUBBER SEAL REFITTED IAW AMM: 52-12-00, REV: 142, OPS TEST SATIS.<BR><BR>CRN97068215 / ULLMER / Q9DY421Y

Part: LANDING GEAR — MALFUNCTIONED (RT & LT) · airframe 71,836 hrs · 23,862 cycles

LOWERED LANDING GEAR TO DOWN NOSE TURNED GREEN BUT LT & RT DID NOT.EICAS GEAR DISAGREE AND GEAR DOORS MESSAGE APPEARED. ITEM DEF PER MEL32-30-1. C/W DMP. PLACARD INSTALLED. LAND GEAR ACTUATION SYSTEM INOP. OPEN

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 71,850 hrs · 23,867 cycles

LOWERED LANDING GEAR TO DOWN. NOSE TURNED GREEN BUT LEFT&RIGHT DID NOT.EICAS GEAR DISAGREE AND GEAR DOORS MESSAGE APPEARED. VISUALLY INSPECTED BOTH MAIN LANDING GEAR, GEAR DOORS AND LAND GEAR SENSORS, NO DAMAGE NOTED. C/W LANDING GEAR POSITION INDICATORS AND WARNING SYSTEM TEST PER AMM 31-61-00-501, NO FAULT FOUND IN PSEU BITE.

Part: LEVER — INOPERATIVE (DOOR) · airframe 71,016 hrs · 23,544 cycles

ENTRY/SERVICE DOOR CAPTURE LEVER WILL NOT LATCH FROM THE INSIDE. ++ FOUND BOTH ARMS OF SECONDARY LOCK PAWL BROKEN/MISSING. R&R'D SAME IAW CMM 52-11-12-81205. OPS GOOD, OK TO CONTINUE

Part: BRACKET — NONE (BULK CARGO FLOOR) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14CRACK ON BRACKET (P/N:146T1261-25) OF BULK CARGO FLOOR BEAM AT STA 1418, LBL22.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01, BOEING DWG NO. 146T1216SH 5 REV"A", AND BOEING DWG NO.1 146T5002 SH 1 REV"E"

Part: BRACKET — NONE (L/H HST) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14CRACK ON BRACKET (P/N:148T7312-43) OF L/H HORIZONTAL STABILIZER SEAL FAIRING NEAR STA 1767.25INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO. 148T9220 SH 3 REV ''A'' , BOEING DWG NO. 148T7320 SH 2 REV ''E'' AND BOEING DWG NO.148T7320 SH 1 , REV''G''

Part: NONE — NONE (AFT CGO) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-38) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, RBL26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO. 140T0130 SH 10 REV"G"

Part: SKIN — CRACKED (NO.4 SLAT SKIN) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4104-3) OF NO.4 SLAT AT OSS 572.549.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01.

Part: SKIN — CRACKED (NO.2 SLAT SKIN) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4102-3) OF NO.2 SLAT AT OSS 946.828.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01.

Part: NONE — NONE (AFT CARGO) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-39) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, LBL 26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO.140T0130 SH 10 REV ''G''.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N:111T2011-5 ON STA 785.9, LBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.85.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A

Part: STIFFENER — CRACKED (CENTER WING) · airframe 68,964 hrs · 22,850 cycles

INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N:11T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.85.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A.

Part: WARNING MESSAGE — ILLUMINATED (OVERHEAT) · airframe 66,522 hrs · 21,939 cycles

EICAS MSG FIRE/ OVERHEAT SYS ON FINAL APPROACH. RAN CHECKLIST, MESSAGE CLEARED. NOTED MSG CLEARED WITH CHECKLIST, PERFORMED FIRE DETECTION TEST REF AMM 26-11-00-715-001. RT ENG OH LPI ALREADY ON DEFERRAL ITEM M768813. (OPEN)

Part: LENS — DETACHED (EMERGENCY SIGN) · airframe 64,393 hrs · 21,180 cycles

INSPECTION TYPE:NADOOR EXIT SIGN COVER FELL OFF.INSTALLED DOOR EXIT SIGN PER AMM 33-51-01-402-030. TESTED OK.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 745, RBL 77.5. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 554 , RBL 77.5. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 654 PLUS 110, LBL 75. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 676, RBL 84. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 652, LBL 11 - LBL 13. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE: C13 CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5, S-13AR. REPAIR IAW SRID: 3-4978953707 AND UPS EO B767-5330-79406-A.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 64,339 hrs · 21,162 cycles

INSPECTION TYPE:C13CORROSION ON M/D SEAT TRACK (P/N:143T5243-10) BETWEEN STA 434 AND STA654 PLUS 11 AT RBL 88.50.PART REPLACEMENT I.A.W. BOEING DRAWING 143T5226 SH 1 REV '' C '',143T5226SH 2 REV '' D '' ,143T5226 SH 3 REV '' D '' , 143T0050 SH 14 REV '' B '',143T0050 SH 15 REV'' B '' AND 767-300F SRM 51-40-02,REV79.01.

Part: HOLDER — MISSING (EXIT SIGN) · airframe 60,810 hrs · 19,868 cycles

INSPECTION TYPE:N/A FLIGHT DECK FWD ENTRY DOOR EMERGENCY EXIT GIN FLOOR ILLUMINATION LAMPS INOP. REMOVED ENTRY DOOR EMERGENCY SIGN LENS FOUND FLOOR ILLUMINATION LAMP HOLDER ASSEMBLY MISSING. R&R'ED EXIT SIGN REF AMM 33 51 01 OPS CKS NORMAL PER SAME.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N : 111T2005-7) UPPER SIDE AT STA 785.9 , LBL 11REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.73.01 AND UPS EO B767-5740-58151-A

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , LBL 11 - LBL 33 , PNL NO . 231GFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , RBL 55 - RBL 77 , PNL NO. 232HFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , LBL 33 - LBL 55 , PNL NO. 231HFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I

Part: STIFFENER — CRACKED (BS 785.9) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N : 111T2008-11) UPPER SIDE AT STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.73.01 AND UPS EO B767-5740-58151-A

Part: FITTING — MISSING (LE SLAT) · airframe 59,573 hrs · 19,404 cycles

INSPECTION TYPE:C12 DURING C12 CHECK OF DATUM AIRCRAFT M FITTING WAS MISSING (P/N : 114T4302-4) ON NR 9 SLAT. REPAIR IAW SRID 4-4361059322 AND EO B767-5750-71763-A.

Part: COVER — BROKEN (L1 DOOR) · airframe 58,603 hrs · 19,066 cycles

DOOR LOCK COVER PLATE WAS BROKEN OFF. REPLACED THE HINGE AND COVER.

Part: WINDOW — FAULTY (COCKPIT) · airframe 57,905 hrs · 18,808 cycles

"L SIDE WINDOW" EICAS MSG DURING CRUISE. AFTER RESET IAW QRH PROC, "L SIDE WINDOW' EICAS AND ASSOC INOP LITE OUT. R&R L2 SIDE WINDOW PER MM 56-11-02-004-001/404-026. WIRING INSTALLATION PER WDM 30-41-12.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 57,902 hrs · 18,807 cycles

LEFT SIDE WINDOW EICAS MSG.C/O TECH RECOMMENDATION ALERT H182251, LEFT SIDE WINDOW EICAS MSG, NO PHYSICAL BURNS NOR DAMAGE NOTED ON L2 AND L3 WINDOW. PERFORMED OPS CHECK PER AMM 30-41-00-715-001, NO ABNORMALITIES FOUND. AS PER PRE-CAUTIONARY R&R WHCU PER MM 30-41-01-004-001/404-007. PN ON/OFF: 624066-5 SN ON: 022C-2212 OFF:

Part: UNKNOWN — NONE (CARGO BAY) · airframe 56,489 hrs · 18,318 cycles

INSPECTION TYPE:N/ADIV - DECENDING THROUGH 20000 FT INTO UIO HEARD A LOUD BANG. LEVELED OFF AT 18000 FT TO COMENCE APPROACH SELECTED FLAPS ONE AND HEARD ANOTHER BANG. DISCONECTED AUTOPILOT SUSPECTING A CARGO SHIFT. DIVERTED GYE AND LANDS A WITH 13 UNITS OF TRIM.INSPECTION ACCOMPLISHED IAW GMM 04-01.01.02 INSPECTED FLOOR AREA AT POS 4 AND 3, EXERCISED ALL CARGO LOCKS AT POS 4AND3 AND THEY ALL WORKED PROPERLY. NO DAMAGE FOUND, AIRCRAFT OK FOR SERVICE.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 54,835 hrs · 17,743 cycles

INSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN AT IFS 145.25. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 54,835 hrs · 17,743 cycles

INSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 3 & 4, AND SRM 51-70-10, REPAIR GENERAL, REV.67.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 54,835 hrs · 17,743 cycles

INSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN AT IFS 194.75. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.

Part: SEAL DEPRESSOR — DENTED (MAIN CARGO DOOR) · airframe 54,765 hrs · 17,725 cycles

MAIN CARGO DOOR SILL AFT SEAL DEPRESSOR DENTED. ABOUT 12 INCHES AFT, UPPER CORNER. DAMAGED AREA REPAIRED IAW EO B767-5230-08088-1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 54,765 hrs · 17,725 cycles

INSPECTION TYPE: C11, DENTS ON RT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 53,357 hrs · 17,193 cycles

ATB - RUDDER RATION EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. AILERON LOCKOUT EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. R & R C FCC IAW MM 22-11-1. OPS NORMAL. R & R L ADC IAW MM 34-12-01. OPS NORMAL.

Part: CASE — CRACKED (PBE) · airframe 53,283 hrs · 17,162 cycles

PBE CASE CRACKED. REPLACED THE PBE.

Part: PRESSURE SWITCH — INOPERATIVE (HYD SYSTEM) · airframe 51,149 hrs · 16,390 cycles

"C HYD SYS PRESSURE" ALERT AND ASSOCIATED"SYS PRESSURE" LIGHT ILLUMUNATED ON CLIMBOUT AFTER SELECTING ADP PUMP OFF IAW MEL TURNED ADP BACK TO "ON" POSITION IAW QRH PROCEDURE. EICAS MSG AND PRESSURE LIGHT REMAINED. R & R CENTER SYSTEM PRESSURE TRANSMITTER IAW MM REF 29.31.01.004.014 AS PRECAUTIONARY. OPS & LEAK CHECKS NORMAL. R & R CENTER SYSTEM PRESSURE SWITCH IAW MM 29.11.09.024.001. OPS & LEAK CHECKS NORMAL SYSTEM NOW OPERATES NORMAL.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 51,130 hrs · 16,383 cycles

MCD FLOOR PANEL POS 11-L DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320=9693-H.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,338 hrs · 16,082 cycles

INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT STA 785.9, RBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 61, SRID: 4-2866088213 AND EO: B767-5710-57147-A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 50,338 hrs · 16,082 cycles

INSPECTION TYPE:C10, FOUND CRACK ON M/D CARGO FLOOR PANEL, 241MFF, AT STA 955, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.

Part: FIRE DETECTOR — DAMAGED (LT NACELLE)

INSPECTION E, PERFORMED AN AIR TURN BACK DUE TO LT ENGINE FIRE INDICATION. REPLACED UPPER AND LOWER EGT THERMAL COUPLE CABLE ASSY. R & R DAMAGED 7TH STAGE COOLING AIR TEE. REPLACED DAMAGED FIRE LOOP WIRES AND PERFORMED NR 2 ENGINE FIRE DETECTION LOOP TEST. TESTS GOOD. R & R FIRE DETECTOR ASSY. NO FAULTS NOTED IAW MM 26-11-02-024-001 & MM 26-11-02-424-033.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — CUT (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL CENTER HAS A ONE INCH CUT UNDER NR 3 LATERAL CAN GUIDE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MCD FLOOR PANEL BS 412 HAS DAMAGE. REPAIRED IAW SRM 53-00-50-2R.

Part: SEAT TRACK — CORRODED (BS 522-566) · airframe 45,898 hrs · 14,370 cycles

INSPECTION TYPE:C09 FOUND CORROSION ON RBL 88 SEAT TRACK AT BS 522 AND 566. REPAIRED IAW EO NR B767-5310-50212-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN FLOOR PANEL POS 9L FWD SECOND FLOOR PANEL FROM OTBD OF MAIN CARGO DECK. FABRICATED NEW FLOOR PANEL REF EO B767-5320-9693-H.

Part: FLOOR PANEL — TORN (MAIN CARGO)

TWO SMALL UPPER SURFACE TEARS ON FLOOR PANEL, POS 8 FWD JUST AFT OF CENTERLINE FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H. T

Part: FSEU — INOPERATIVE (TE FLAPS)

FLAP T/E DISAGREE LIGHT AT FLAPS 5 POSITION WHEN RETRACTING AFTER TAKE OFF. HAD TO USE ALTERNAT FLAP SWITCH LAND FLAPS 20. R & R FSEU IN REF TO MM 27-51-01-4. PERFORMED BITE CK IN REF TO FIM 27-51-00. SYS CKS GOOD. FSEU ALSO TESTS GOOD IAW MM 27-51-01-4. OK FOR CONTINUED SERVICE.

Part: FLOOR PANEL — PUNCTURED (CABIN)

DAMAGED FLOOR PANEL POS 4L OTBD. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — PUNCTURED

DAMAGED FLOOR PANEL AT POS 2L OTBD. REPAIRED IAW SRM 53-00-50-2R, PARA 4C.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL HAS TWO HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

TWO HOLES IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

FLOOR PANEL POS 6R HAS HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

TWO HOLES FLOOR PANEL. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

DAMAGE IN FLOOR PANEL 145T5876-73 FWD CTR PANEL 6" LEFT OF CTR, FABRICATED PANEL REF EO B767-5020-9693-H.

Part: FLOOR PANEL — DAMAGED (CABIN)

HOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW B767-5320-9693-H.

Part: SKIN — DENTED (RT WING TE FLAP)

RT WING OTBD FLAP T/E WEDGE DENTED. REPAIRED IAW EO B767-5750-44843-B.

Part: ADI — FAILED (COCKPIT)

AT FLT LEVEL 340, CAPTAINS ADI CRT CB POPPED. SCREEN WENT BLANK FOLLOWED BY AN ELECTRICAL BURNING ODOR. CHECKED EADI CONNECTOR FOR BURN, FOUND OK. REPLACED EADI LT SIDE IAW 34-22-03-4, OPS CHECK COMPLETE.

Part: FLOOR PANEL — DENTED (BS 930-975) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FLOOR PANEL FOUND SEVERAL DENTS AND PUNCTURES AT STA 930 TO 975 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (BS 654-690) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FLOOR PANEL FOUND SEVERAL DENTS AND PUNCTURES AT STA 654+22 TO STA 690 LBL 11 TO RBL 11. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: STRAP — CRACKED (BS 955) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955, REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT FAIL SAFE STRAP ON 4 O/C AND 10 O/C POSITION APPROX .1875" AND THROUGH THICKNESS FUS BS 955 RT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-H, APPENDIX D, ORG MAT'L IS 2024T351-0.750" MACHINED STRAP, CRACK AT 4 O/C & 10 O/C POSITION APPROX .1875" & THROUGH THICKNESS, FINAL CUTOUT SIZE IS 7.75" X 2" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE: C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA CORROSION CRACK FOUND AT FAILSAFE STRAP FROM 5 O/C TO 7 O/C POSITION APPROX .1250" IN DEPTH FUS BS 955 LT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIR IAW EO B767-5350-17922-H APPENDIX 'C' ORIGINAL MATERIAL 2024T351-0750" MACHINED STRAP, CRACK IS AT 5 O/C TO 7 O/C POSITION APPROX .1250" IN DEPTH, FINAL CUTOUT SIZE IS 7.75" X 2" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT T-FITTING INBD LAYER APPROX 0.040" IN LENGTH. FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA T-FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H APPENDIX 'C' ORIGINAL MATERIAL IS 7075-T73 DIE FORGING, CRACKED AT INBD LAYER APPROX 0.040" IN LENGTH, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR

Part: FITTING — CORRODED · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA CORROSION CRACK FOUND ON 6 O/C POSITION AT TEE FITTING OUTBOARD LAYER APPROX .1250" IN DEPTH. FUSELAGE RT BS 955 REAR SPAR BULKHEAD AREA TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H, APPENDIX "D", ORIGINAL MATERIAL IS 7075-T73 DIE FORGING, CORROSION CRACK ON 6 O/C POSITION AT OTBD LAYER APPROX .1250" IN DEPTH, THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: STRAP — CRACKED (BS 955) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACK SUSPECT FOUND, PLS REMOVE BOLT FOR NDT CRACK CONFIRMATION. FUS RT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP ATT MOST LOWER BOLT REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPENDIX 'D', FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FAIL SAFE STRAP CRACK SUSPECT FOUND, REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPENDIX 'C' FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: STIFFENER — CRACKED (BS 246) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246 LBL40 FLOORBEAM VERTICAL STIFFENER FOUND CRACKED. FX MEC STA246 LBL40 FLOORBEAM VERT STIFFENER REPAIRED IAW SRM 53-10-51-2R4, REPAIR 4 FIG 201. CRACKED LENGTH 0.75" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. REPEAT INSP AT 3000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER OCCURS FIRST IS REQUIRED IAW SRM 53-10-51-2R4 REPAIR 4 FIG 201. REPAIR LENGTH IS 14.6"

Part: FLOOR PANEL — DENTED (BS 1340) · airframe 41,576 hrs · 12,859 cycles

INSPECTION TYPE:C, DMI NR D442907 MAIN CARGO DECK POSITION 11R FLOOR PANEL INTERIM REPAIR DUE TO DENT AT STA 1340. MCD FLOOR PANEL AT STA 1263 TO 1370, RBL 88 FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (BS 1490)

MCD POS 14L STATION 1490 FLOOR PANEL HAS 3 HOLES. FAB NEW FLOOR PANEL REF EO B767-5300-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO DECK FLOOR PANEL POS 7R THIRD FLOOR PANEL FROM OTBD. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:C MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE CRACKED. CRACKED 0.75 INCH LENGTH. MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP CRACKED. MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: STIFFENER — CRACKED (AFT CARGO BAY) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C AFT CARGO COMPT STA 1087 LBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:C EMP VERTICAL STAB RT LWR FWD EXTERNAL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 43, 51-70-10 REPAIR 4 FIG 201, DOUBLER MATERIAL 7075T6BARE0025IN, REPAIR DOUBLER SIZE: 16.125 X 13 INCHES.

Part: STIFFENER — CRACKED (AFT CARGO BAY) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C AFT CARGO COMPT STA 1087 RBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 RBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C LT WING - NR 4 SLAT EXT SKIN FOUND CRACK AT O/B STRINGER FASTENER AREA. LT WING NR 4 SLAT OSS641-74 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6.071" AND 7075T6.063" AS REPAIR DOUBLERS AND REPAIR PLATE WITH 5.5" X 10.125" REPAIR SIZE FOR DOUBLERS AND 7.125" X 8.875" FOR REPAIR PLATE RESPECTIVELY.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C LT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05, PAR 5A (1), FIG 5, REV 43.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG FOUND CRACKED 1.5 INCH LENGTH AT I/B FLANGE AND 0.9 INCH LENGTH AT O/B FLANGE. LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 43.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C RT WING - NR 9 SLAT O/B UPPER AREA FOUND CRACKED. RT WING NR 9 SLAT OSS641.74 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6.071 AND 7075T6.063 AS REPAIR DOUBLERS AND REPAIR PLATE WITH 5.625 X 10.375 INCHES REPAIR SIZE FOR DOUBLER AND 7.375 X 9.375 INCHES FOR REPAIR PLATE RESPECTIVELY.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET FOUND CRACKED. RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-02, FX BS 388-400 BETWEEN STR 29L AND 30L, THE SKIN REPAIR CANNOT BE CORRELATED TO SRM. FX REPAIRED AS PER SRM 53-00-01-2R1 FIG 201 REV 43 JUST AT STA 385 - 415 BETWEEN STR 28L AND 31L. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH DOUBLER MATERIAL 2024T3-0071IN & FILLER MATERIAL 2024T3-0063IN, REPAIR SIZE IS 15.5"X17.75". SUBSEQUENT INSP REQUIRE AS PER SRM 53-00-01-2R1 FIG 201 REV 43. UPS MPI P20642 ISSUED.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C M/D STA 1241 - 1263 STR 16R FOUND DEEP CHAFING MARK. MAIN DECK BS 1233 TO 1271 STR 16R STRINGER REPAIR AS PER SRM 53-00-03-2R1 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A CATEGORY 'A' REPAIR WITH MATERIAL BAC1498-208 7075T62 AND BAC1498-203 7075T62 AS STRINGER, HAT SECTION 38 INCHES IN LENGTH AND STRINGER SPLICES 12.375 INCHES IN LENGTH RESPECTIVELY.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 654+3, RBL 74 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R, REV 43, FIG 201.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 1576 LBL 11 FOUND PUNCTURE ABOUT 1 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT CRACKED. NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT REPAIRED AS PER HX RS R-54-51-36328 REV A. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AMS4911-00901IN AND AIS1-301-00161INFH, REPAIR SIZE 11.5 X 10.25 INCH AND UPS EO B767-5430-33634-A.

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:C RT WING I/B AFT FLAP LOWER O/B EXISTING REPAIR FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 REV 43. REPAIR DOUBLER MATERIAL 2024T3-0040IN AND ADHESIVE FILM AF163-2K0010IN REPAIR DOUBLER SIZE: 9 X 9 INCHES.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C RT WING - NR 9 SLAT I/B UPPER AREA FOUND CRACKED. RT WING - NR 9 SLAT OSS573 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201, REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0063IN AND 7075-0-0071IN. REPAIR DOUBLER AND REPAIR PLATE WITH 5.375 X 10.25 INCHES (2 EA) REPAIR SIZE FOR DOUBLER IS 7.25 X 9 INCHES FOR REPAIR PLATE RESPECTIVELY.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 326, LBL 6 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43, FIG 201.

Part: CYLINDER — CORRODED (LT MLG) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SIDE AND O/B SIDE NUMEROUS LOCATIONS FOUND RUSTY ABOVE TORSION LINK UPPER FTG UP TO 56 INCHES TOP AREA HAND BLEND AREA 50" X 14" REWORK DEPTH 0.001". LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SIDE AND O/B SIDE RUSTY REMOVED AND NDT INSPECTED AND SURFACE FINISHED AS PER RS-R-3200-36333-A AND UPS EO B767-3210-33595-A.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C FWD CARGO COMPT STA 786, WL 196, RBL 33 WING CENTER SECTION FRONT SPAR ATT STIFFENER FOUND CRACKED. FWD CARGO COMPT BS 786 RBL 33 CENTER TANK FRONT SPAR STIFFENER REPAIR AS PER HX RS R57-11-36330 REV A WITH MATERIAL 2024T351.0250 AND 2024T351.100 AS REPAIR STRAPS 12.5 X 15 INCHES AND 11-25 INCHES IN LENGTH RESPECTIVELY. THIS REPAIR CLASSIFIED AS A CATEGORY A PERMANENT REPAIR AND REF UPS EO B767-5710-33635-A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 36,735 hrs · 11,250 cycles

INSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-05 FUSELAGE BS 1241 - 1263 STR 15R - 17R DOUBLER AND TRIPLER FOUND IDENTIFY REQUIRE. SKIN REPAIR AS PER SRM 53-00-01-2R1 FIG 201 REV 43. SUBSEQUENT INSP ARE NECESSARY AS PER SRM 53-00-01-2R1 FIG 201 SHT 9 TABLE V. THIS REPAIR CLASSIFIED AS A CATEGORY B. REPAIR WITH MATERIAL 2024R3.100 & 2024T3.160 AS DOUBLER & FILLER RESP. DOUBLER SIZE 27 X 20 & 24.5 X 17.125 INCHES, FILLER SIZE13.5 X 12.5 INCHES. UPS MPI P20647 ISSUED FOR SUBSEQ INSP.

Part: SHUNT — INOPERATIVE (EGT)

INSPECTION TYPE:ETOP ATB - LT ENG PRI AND STBY EGT INOP. EPER FIM 77-21-00 PIMU BITE SHOWS 352 16A EGT SENSOR AND 352 16B EGT SEN PER PIMU MESS INDEX. REMOVED AND REPLACED SHUNT JUNCTION BOX IAW 77-21-53-4 UP TO OPS CK. SHUNT BOX CKS J131 PIN B TO J3 PIN E OPEN. J131 PIN A TO J4 PIN E OPEN. J131 PIN A & B TO GROUND OPEN ALL OTHER RESIS OK PER FIM PIMU MSG INDEX. COMPLY WITH OPS CHECK GOOD.

Part: BRACKET — CRACKED (R2 WINDOW)

INSPECTION TYPE:N/A R2 WINDOW CARRIAGE ASSEMBLY BRACKET CRACKED. REMOVED AND REPLACED BALL SCREW ASSEMBLY AND CARRIAGE ASSEMBLY PER MM 56-11-04-4.

Part: INDICATOR — MALFUNCTIONED (LE FLAPS)

ATB - RECEIVED MESSAGE AND FLAP INDICATOR SHOWED LE FLAPS NOT UP. RAN CHECKLISTS. REMOVED AND REPLACED IAW 27-58-02-4 FLAP POSITION INDICATOR OPERATION CHECKED SATISFACTORY IAW 27-58-00-5.

Part: PSEU — FAULTED (LE FLAP)

2ND ATB - LE FLAP ASSYMETRY. REF FIM 27-81-00 FIG 107 PSEU FAULTED S280. INSPECTED TARGET AND AFFECTED SLAT. NO DAMAGE FOUND. CLEARANCE WITHIN LIMITS AT .111 INCH. TESTED INDUCTANCE IAW FIM 32-09-03 FIG 108. FOUND S280 OUT OF LIMITS READING 5.8 MILLIHENRYS. REPLACED S280 IAW MM 27-88-01-2. PSEU BITE NORMAL IAW FRIM 32-09-03.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:ETOP BTB - RIGHT PRV MSG ON START. PERFORMED ENGINE START AND EICAS MESSAGE WENT AWAY. OK FOR AIRCRAFT TO CONTINUE PER FIM 36-10-00.

Part: CONNECTOR — DIRTY (RT SHUTOFF VALVE)

INSPECTION TYPE:ETOP RT ENG PRV EICAS MSG WITH STATUS MSG AND BLEED LIGHT ON RIGHT SIDE. REMOVED AND CLEANED CONNECTOR ON RT PRSOV. CYCLED VALVE MANUALLY. RAN ENGINE, NO MSG OR BLEED LIGHT. OPERATES NORMAL PER MM 36-11-00.

Part: SEAT TRACK — CORRODED (BS 1439) · airframe 31,042 hrs · 9,580 cycles

INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,042 hrs · 9,580 cycles

INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.

Part: SEAT TRACK — CORRODED (BS1373-1390) · airframe 31,042 hrs · 9,580 cycles

INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.

Part: SKIN — CRACKED (BS 687) · airframe 31,042 hrs · 9,580 cycles

INSPECTION TYPE:2C CRACKS IN SKIN AT UPPER GPS ANTENNA DOUBLER. REPAIRED IAW EO B767-5330-26944-A, ER 07-2324. CUT OUT DAMAGED AND INSTALLED DOUBLER.

Part: CASE — CORRODED (NR 1 ENGINE) · airframe 31,042 hrs · 9,580 cycles

INSPECTION TYPE:C2 NR 1 ENGINE CORROSION ON AFT FAN CASE AT 5-6:30 POS AT NUT PLATES 8 INCHES FROM AFT END OF CASE. REPAIRED PER UPS ENGINEERING FILE NUMBER 80C2-72-20000.

Part: SERVO — MALFUNCTIONED (YAW DAMPER)

UNCOMMANDED RUDDER YAW TWICE IN FLIGHT. R & R LT & RT YAW DAMPER SERVO IAW MM 22-21-02-4. LEAK CHECK RIGHT & LEFT YAW DAMPER SERVO PER TECH SERVICES. R&R RIGHT YAW DAMPER MODULE ASSY IAW MM 22-21-04-2. ALSO R&R LEFT YAW DAMPER MODULE ASSY AS PRECAUTIONARY. PERFORMED MCDP BITE TEST 09,30,40,69 PER MM 22-00-02-2 & FIM 22-21-00 YAW DAMPER SYSTEM BITE. NO FAULTS NOTED

Part: VALVE — MALFUNCTIONED (BLEED AIR)

INSPECTION TYPE:ETOP LEFT DUCT PRESSURE FLUCTUATES W/ENGINE RUNNING AND BLEED SWITCH ON. AFTER TAKEOFF PRESSURE DROPPED BELOW 20 PSI & ROSE ABOVE 60 PSI. TURNED LEFT PACK OFF AND LEFT ENG BLEED SWITCH OFF. DEF LEFT ENG PRSOV PER MEL 36-11-1-1. C/W DMP 36-11-1. PER FIM 36-10-00 FIG 109 FAN AIR MODULATING VALVE DEF. R&R FAV PER 36-11-16. PERFORMED AIR SUPPLY BITE CHECK & NO FAULTS. OK FOR SERVICE.