N351AX

BOEING 767 33A No injuries Part 121 — OMNI AIR INTERNATIONAL LLC

Operated by Omni Air International (per NTSB report)

ATA 3600

Part: PRESSURE VALVE — INOPERATIVE · airframe 101,593 hrs · 16,572 cycles

L HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATED

ATA 3416

Part: ALTIMETER — INOPERATIVE (ZONE 200) · airframe 101,436 hrs · 16,539 cycles

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

ATA 5713

Part: LONGERON — CRACKED (ZONE 500) · airframe 99,982 hrs · 16,197 cycles

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.

ATA 2921

Part: RELAY — INOPERATIVE · airframe 96,110 hrs · 15,353 cycles

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.

ATA 2910

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 94,862 hrs · 15,034 cycles

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.

ATA 2565

Part: CYLINDER — EMPTY · airframe 94,297 hrs · 14,895 cycles

L/H OVERWING EXIT SLIDE INFLATION BOTTLE PRESSURE READS ZERO. CORRECTIVE ACTION: L/H OVERWING EXIT SLIDE BOTTLE REPLACE IAW B767-300 AMM 25-65-02-404-010 REV 136.

ATA 5230

Part: PSEU — DEFECTIVE · airframe 94,248 hrs · 14,884 cycles

PRIOR TO CRUISE, IN CLB OUT, ALL CARGO / ENTRY DOORS CAUTION ILLUM. CORRECTIVE ACTION: REPLACED PSEU BOX IAW B767AMM 32-09

ATA 3260

Part: SENSOR — DEFECTIVE · airframe 91,347 hrs · 14,223 cycles

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

ATA 2810

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 87,824 hrs · 13,472 cycles

R ENG FUEL FILT ICAS MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER AMM B767 73-34 LEAK CHECK GOOD MESSAGE CLEARED NO FURTHER DEFECTS NOTED AT THIS TIME. REF FIM 767 73-11 FAULT TREE 803

ATA 2133

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 86,658 hrs · 13,228 cycles

YELLOW CABIN AUTO INOP ICAS MESSAGE. WHITE CABIN ALT AUTO 2 AND AUTO 1 STATUS MESSAGES. MANUAL CONTROL INOP. CORRECTED ACTION: T/S TO OUTFLOW VALVE ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW B763 AMM CH 21-31. OPS CHECK SATISFACTORY.

ATA 2710

Part: PCA — FAILED (LT AILERON) · airframe 85,927 hrs · 13,040 cycles

EXCESSIVE RIGHT RUDDER TRIM (5 UNITS) REQ'D TO MAINTAIN LEVEL YOKE DURING CLIMB OR ON APPROACH WITH FLAPS OUT. ON GROUND DURING INITIAL FLAP EXTENSION, R INBD AILERON WAS NOTED SIGNIFICANTLY LOWER THAN L INBD AILERON, BUT FLT CONTROL CHECK FELT & LOOKED OK. IN FLT ACFT REQ'D A LOT OF LEFT YOKE INPUT TO MAINTAIN HDG. THEN TRIMMED IT OUT WITH 5 UNITS RIGHT RUDDER TRIM IN CRUISE, WITH THROTTLES BACK. 2.5 UNITS RIGHT RUDDER TRIM REQ'D WITH FLAPS OUT NEEDED 4.5 UNITS RIGHT RUDDER TRIM. CORRECTIVE ACTION: REMOVED AND TEMP INSTALLED LEFT INBOARD AILERON OUTBOARD PCA REQUIRES TORQUE AND RIG (BW 14641) CB'S PULLED: (12) 1) L ENG PUMP DEPRESS 2) ELEC CNT 1 3) ELEC CNT 1 4) SYS PRESS L 5) SYS PRESS CTR 6) R ENG PUMP DEPRESS 7) ELEC CTR 2 8) ELEC L 9) SYS PRESS R 10) L ENG PUMP SUPPLY 11) R ENG PUMP SUPPLY 12) AIR PUMP FLY CONTROL VALVE SHUTOFF SWITCHES (OFF) WING ONLY INSTALLED LEFT INBOARD AILERON OUTBOARD PCA IAW AMM 27-11-48. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. PERFORMED AILERON CONTROL CABLE SYSTEM IAW 27-11-00 ALL RIG PINS SLIPPED IN EXCEPT A13 AND A14 PERFORMED RIG CK AND ADJUSTMENT OF RT DROOP ANGLE GEAR BOX PER AMM 27-51-40 CKS NORMAL AT THIS TIME.

ATA 5350

Part: RADOME — DENTED (FUSELAGE) · airframe 66,917 hrs · 9,441 cycles

BIRD STRIKE - AFTER BIRD STRIKE INSP FOUND RADOM DAMAGE INDENTED APPROX 2 FT ROUND SLIGHT LT OF CTR. R & R NOSE RADOME IAW AMM 53-12. LATCHED AND OK FOR SERVICE, RADOME WAS NOT PERFORATED AND RADAR ANTENNA AREA WAS INTACT.