N351AX
Registered owner: CARGO AIRCRAFT MANAGEMENT INC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| OMNI AIR INTERNATIONAL LLC (CNMA) | Operator | 2017-02-28 – 2017-02-28 | Operator named in NTSB report |
| Omni Air International | Operator | 2017-02-28 – 2017-02-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATED
CA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.
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.
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.
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.
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.
PRIOR TO CRUISE, IN CLB OUT, ALL CARGO / ENTRY DOORS CAUTION ILLUM. CORRECTIVE ACTION: REPLACED PSEU BOX IAW B767AMM 32-09
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
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
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.
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.
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.