OMNI AIR INTERNATIONAL LLC

Operated by Omni Air International (per NTSB report)

Operated by Omni Air International (per NTSB report)

Operated by Omni Air International (per NTSB report)

Operated by Omni Air International (per NTSB report)

Operated by Omni Air International (per NTSB report)

Operated by Omni Air International (per NTSB report)

Operated by OMNI AIR INTERNATIONAL INC (per NTSB report)

Operated by Omni Air International (per NTSB report)

DURING CLIMB FUEL IMBALANCE CK LIST CAME UP. EVENTUALLY RT SIDE SHOWED 8K LEFT SIDE SHOWED 35K DURING DESCENT IT WENT BACK TO NORMAL

L HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATED

R ENG HPSOV EICAS MESSAGE. COMPLIED WITH QRH PROCEDURE

FAINT ELECTRICAL SMELL BEGAN, ACCOMPANIED BY LIGHT VIBRATION FWD EQ EXH FAN STATUS MESSAGE DISPLAYED, FOLLOWED BY DISAPPEARANCE OF VIBRATION AND ELECTRICAL SMELL.

FLIGHT CONTROL SYS STS MSG DURING CLIMB

CA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.

AFTER PASSING 10,000 FT., INFORMED FROM CABIN OF SLIGHT FUEL LEAK IN OVERWING FUEL CAP. RT WING LEAK INCREASED AT 310. DECLARED EMERGENCY, DUMPED 24.5K FUEL, RETURN TO PGUA.

R HPSOV EICAS AND STATUS MESSAGE IN FLIGHT

AT CRUISE AUTOTHROTTLE AND AUTOPILOT DISCONNECTED. AUTO THROTTLE WOULD NOT RE-ENGAGE. AUTOPILOT L AND C INOP. R AUTOPILOT WORKED. LEFT AND FO FLIGHT DIRECTORS INOP. CAPT HEADING BUG INOP. CAPT SPEED BUG INOP. CAPT ALTITUDE SEL INOP.

PILOTS REPORTED MAIN BAT CHARGER HAD A STRONG BURNING SMELL.

AFTER TAKEOFF AT APROX 100' AGL HEARD A LOUD BANG AND AN ASSOC LEFT MOMENTARY YAW.

ON CLIMB AT 5000 FEET R RECIRC FAN EICAS. AT 6500 FEET LOUD BAND AND YAW AND R RECIRC FAN EICAS EXTINGUISHED. WE HAD A BURNING SMELL, ENGINE INDICATIONS NORMAL. VIBRATION ON DECENT BUT ENGINE INDICATIONS NORMAL. OIL SMELL BACK OF CABIN AFTER SHUTDOWN

REASSESS DENT 20 RH FUSELAGE STATION 368+6INCHES STRINGER 26+4INCHES. FOUND TO BE OUTSIDE OF ALLOWABLE DAMAGE LIMITS IAW B767-300 SRM 53-00-01-1A-1 REV 128.

GOUGES ON LH H-STAB LOWER INSPAR SKIN AT S-2 AND STA 226.605 (RIB 12 CENTERLINE).

DISBOND AROUND HOIST POINT ATTACH POINT L/H WING UPPER SURFACE.

DENT #13, REPAIRED ON STRINGER 19L BETWEEN STATION 368-388 IAW B767-300 SRM 53-00-03-2R-1 REV128.

DURING C CHECK, CORROSION WAS FOUND ON THE NR 2 ENGINE FWD AND AFT CASE AROUND THE EXTERIOR AND INTERIOR SKIN. IT WAS FOUND TO BE OUT OF REPAIRABLE LIMITS FOR THE FWD FAN CASE PER AMM 72-32-00 AND OUT OF FLYABLE LIMITS PER AMM 72-00-00. THE ENGINE WAS REMOVED AND SENT FOR REPAIR. WHILE AT GA TELESIS IT WAS FOUND BY THE ENGINE SHOP THAT THE AFT FAN CASE WAS ALSO BEYOND REPAIR. THE FWD AND AFT FAN CASE WERE CHANGED AT GA TELESIS ON WO#1155. AFTER REPAIR THE ENGINE WAS SENT BACK AND INSTALLED BACK ON N36NE AT THE #2 POSITION.

DENT NR 12 LT FUSELAGE STATION 368 +8 INCHES, STRINGER 17L +4 INCHES. DURING SCHEDULED MAINTENANCE, TWO DENT DAMAGES WERE FOUND COMMON TO THE LOWER FUSELAGE SKIN BETWEEN STA 368 - STA 390 AND STGR 17L - STGR 19L..

DURING C-CHECK AT YHM, THE RH HORIZONTAL STABILIZER AUXILIARY SPAR WEB NEAR OUTBOARD CLOSURE RIB AT HSBL 357.442 WAS FOUND TO HAVE TOOLING MARKS, AFTER BLENDING OUT OF THE DAMAGED AREAS, TWO CRACKS OF 0.300" AND 0.250" LONG WERE FOUND.

DURING ACCOMPLISHMENT OF INSPECTION 76AD2012-15-12-G, A CRACK WAS FOUND IN THE LH UNDERWING LONGERON. PER SB 767-57A0126 INSTRUCTIONS, THIS REQUIRES FURTHER INSPECTION OF THE STRUCTURE AND AT MINIMUM REPLACEMENT OF THE UNDERWING LONGERON.

AT 10,000 MSL, CREW O2 QTY DROPPED TO 70 PSI

BULK CARGO TEMP 8 DEGREES CELSIUS AT FL280, 2 HOURS AT CRUISE

R ENG FUEL FILT EICAS MESSAGE ON MOMENTARILLY DURING CLIMB. STATUS MESSAGE R ENG FUEL FILT DISPLAYED.

PASSING THROUGH FL240 DURING CLIMB, LEFT CENTER FUEL PUMP FAILED.

DURING CLIMB, RIGHT HYDRAULIC DEMAND PUMP FAILED

CORROSION FOUND ON GROUNDING BRACKETS INTERNAL NOSE RADOME @ 2 & 4 O'CLOCK POSITION.

CORROSION FOUND ON FUSELAGE SKIN AND STRINGER 36R BETWEEN STA 1175 - 1197+22 AFT CARGO

PANEL 611 FB REMOVED FROM A/C DUE TO BIRDSTRIKE

EICAS R AC BUS OFF. STATUS: WXR SYS / R ICE DETECTOR / HI FLOW INHIBIT

CABIN ALTITUDE WARNING - EICAS MESSAGE @ 10650'. CABIN WOULD NOT PRESSURIZE.

ON APPROACH FLIGHT CONTROLS FELT AS THOUGH THEY WERE BINDING. FLIGHT CONTROLS ASYMETRY IS INDICATED ON INDICATOR.

DURING CRUISE FLIGHT AT FL370 LEFT ENGINE N1 ROLLED BACK WITH CORRESPONDING VIBRATIONS

RIGHT ENGINE OIL PRESSURE IN CAUTION RANGE AT TOP OF CLIMB. RIGHT ENGINE OIL QUANTITY ZERO. SHUT DOWN ENGINE AT OIL PRESSURE IN THE RED.

L CDU FAILURE, L FMC FAILURE: DURING FLIGHT CREW REPORT THE L FMC FAILED. DISCUSSIONS WITH MOC AND DO. ALL PARTIES AGREED TO CONTINUE. CREW CALLED BACK 1 HOUR LATER AND STATED THE L CDU FAILED AND WENT BLANK. FIGHT DIVERTING TO ANC DUE TO ETOPS AND FUEL RESTRICTIONS.

EICAS MESSAGE "HEAT PITOT R"

BOTH WX RADARS FAILED IN FLIGHT - REMOVED AND REPLACED WX RADAR ANTENNA AND R WX (?) IAW B763 AMM CHP 34-43 OPS CHECKS GOOD

RAT DID NOT DEPLOY DURING AUTO DEPLOYMENT TEST ~ RAT DEPLOY RELAY K235 REPLACED RAT AUTO DEPLOY TESTED SERVICEABLE IAW B767-300 AMM 29-21-00-735-048 REV 139.

ODOR OF SMOKE DETECTED AFTER TAKE OFF SHORTLY THEREAFTER THE FLIGHT DECK LOCK CIRCUIT BREAKER WAS DISCOVERED TO HAVE POPPED. CORRECTIVE ACTION: REMOVED AND REPLACED FLIGHT DECK DOOR ELECTRIC STRIKE PER B767 AMM 52-51

R HYD QTY EICAS DURING CRUISE. QUANITY INDICATOR INDICATED HYDROLIC LEAK. CORRECTIVE ACTION: REMOVED AND REPLACED O-RING ON #11 SPOILER ACTUATOR IAW B767 AMM CHP 20-10. LEAK CHECKS GOOD.

CORROSION TOP OF STABILIZER BOX ASSESSMENT FRONT RIGHT SPLICE. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED DAMAGE ON H-STAB BOX UPPER SKIN FROM FRONT SPAR TO S-11 AT RBL 13.833 IAW STS EA 79-2022-141 REV IR AND OMNI AIR INTERNATIONAL EO B7655-10 INITIAL ISSUE REFERENCE Q1 AVIATION W/O 139617-2, 139617-3 AND 139617-16 FOR ALL NDT HFEC, RHEC AND UT REQUIREMENTS NIL FINDINGS THIS IS A CAT B REPAIR WITH FIRST STAGE APPROVAL WHICH APPROVES THE STATIC STRENGTH DATA AND WHICH PROVIDES THE SCHEDULE FOR SUBMITTAL OF THE DT DATA WHICH MUST BE SUBMITTED NO LATER THAN 24 MONTHS FROM THE DATE OF THIS FORM.

LE SLAT DISAGREE CAUTION MESSAGE AT 35,000 FT ~ REMOVED AND REPLACED CENTER HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-31. OPS CHECK NORMAL.

RT ENGINE BLEED OVERHEAT RT ENGINE BLEED OFF R1 PACK AFT EICAS OCCURED AT HIGH & LOW TRUST SETTING ~ R&R FAMV PER B767-300 FIM 36-10 FT 835 SHT 3 BLK 4+47 & AMM 36-11 P.CASAS 13013 R&R "R" ENG BLEED AIR CONT CARD PER FIM 36-10 FT 835 SHT 3 BLK 44 & AMM 36-11 P.CASAS 13013 R&R THE PRSOV PER AMM 36-11 & FIM 36-10 FT 835 SHT 3 BLK 3 D.F. 14232 PERFORMED ENGINE RUN IAW AMM 71-00 OPS CHECKED PRSOV & FAMV BOTH FOUND GOOD

L2 LAV USED ALL THE WATER, WON'T STOP FILLING. MANUALLY SHUT OFF WATER VALVE ~ INSPECTED MS-13 LAV TOILET ASSY. FOUND RINSE VALVE CONSTATNLY ON & POPPET VALVE LEAKING REMOVED & REPLACED RINSE VALVE ASSY & POPPET VALVE PACKING OPERATIONAL CHECKS NORMAL NO LEAKS IAW AMM 38-32.

R ENG BLEED OVERHEAT (EICAS MSG) EARLY ON CLIMB OUT ~ REMOVED AND ATTACHED WIRES IAW WDM 36-11 AND UNLOCKED FAMV FOR OPS CHECK IAW AMM 36-10. OPS CHECK OKAY.

R WINDSHIELD SHATTERED. CORRECTIVE ACTION: REMOVED AND REPLACED R #1 WINSHIELD PER B767 AMM 561101 THRU STEP 21.B.

LE SLAT DISAGREE EICAS ON DEPARTURE CLIMB AND ENROUTE. CORRECTIVE ACTION: PERFORMED BITE PROCEDURE AND GAVE MESSAGE 2781045 WHICH LEADS TO B762 FIM 278100 101 FIG 106 PSEU BITE TARGET PROCEDURE LEADS TO S305 ON #7 INBD SLAT FIM 3209 00 101 FIG 104 S305 SENSOR FOUND WITH PAINT ON IT SANDED AND WITHIN LIMITS OPS CHECKED GOOD NO FURTHER MESSAGES PREVIOUS FSEU BITE PROCEDURE DONE IAW B762 FIM 2751 FAULT TREEE 809

AIR GROUND DISAGREE STATUS MESSAGE CORRECTIVE ACTION: R&R SENSOR S10598 PER SB76727A0160 AND ADJUSTED. OPS CK GOOD. TS IAW B767 FIM 3209 FAULT TREE 810 REPLACE RELAYS K199 & K293 IAW SB 76727 A0160

RIGHT WING SINGLE POINT FUEL CAP LEAKING. CORRECTIVE ACTION: REMOVED AND REPLACED SPR FUEL CAP IAW 767 AMM 28-11.

DURING CRUISE FLIGHT, AUTOTHROTTLES DISCONNECTED FOLLOWED BY ALL AUTOPILOTS DISENGAGED AND LEFT FLIGHT DIRECTOR FAILED. REPLACED THE CAPTAIN'S ASA IAW AMM 22-14 AND LEFT TPM IAW AMM 24-32. AUTOPILOTS & AUTOTHROTTLE CHECKED IAW MCDP, GROUND TESTED, NO FAULTS AT THIS TIME ALSO REPLACED CB.

STATUS - APU OIL QTY. CORRECTIVE ACTION:UPON VISUAL INSPECTION FOUND APU OIL SIGHT GAUGE READING LOW OIL QUANTITY. RAN THE APU AND OIL QUANTITY RETURNED TO CORRECT LEVELS IAW B767 AMM 49-11. NO LEAKS NOTED