N768NA
Registered owner: HYLIO INC, TX (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 | 2014-06-20 – 2014-06-20 | Operator named in NTSB report |
| Omni Air International | Operator | 2014-06-20 – 2014-06-20 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WHILE PERFORMING MINI EVAC DEMONSTRATION, SLIDE DEPLOYED AS REQUIRED PASSING THE MINI EVAC DEMONSTRATION. HOWEVER, THE SLIDE LIGHT SYSTEM FAILED TO ILLUMINATE DUE TO LANYARD NOT ACTIVATING THE LIGHT BATTERY PACK. REPLACED SLIDE ASSY.
WHILE PERFORMING MINI EVAC DEMONSTRATION, SLIDE DEPLOYED AS REQUIRED PASSING THE MINI EVAC DEMONSTRATION. THE SLIDE LIGHT SYSTEM FAILED TO ILLUMINATE DUE TO LANYARD NOT ACTIVATING THE LIGHT BATTERY PACK. REPLACED SLIDE ASSY.
FLT DECK EMERGENCY LIGHT DID NOT ILLUMINATE. R & R LIGHT ASSY IAW MM 33-51-01. OPS CHECKED NORMAL.
F/A EMERGENCY FLASHLIGHT AT LT OVER WING EXIT NOT BLINKING. R & R BATTERY PACK IAW AMM 25-64-00. OPS CHECKED NORMAL.
GASPER FAN OFF LIGHT ILLUMINATED. SWITCH IN ON POSITION. FAINT SMELL IN CABIN REPORTED. UPON INSPECTION FOUND GASPER FAN BURNED OUT. REMOVED & REPLACED GASPER FAN IAW AMM 21-24-01, CHECKS NORMAL. NO SMELL NOTED IN CABIN.
LEFT AFT SIDE EMERGENCY OVERHEAD LIGHT AND EXIT SIGNS INOP. REPLACED BATTERY PACK AT M739 POSITION AS PER MM 33-51-07, OPS CHECK OK.
WHILE TESTING THE WEPPS, ALL 15 EMERGENCY BATTERIES REQUIRED PBT'S (PERIODIC BATTERY TEST). FOUND 3 BATTERIES FAILING THE LOW VOTLS TEST, REPLACED THE M734, M1208 AND M1395 BATTERIES PER B767 SMM, OPS CHECK OK.
GROUND CREW REPORTED SMOKE FROM LEFT MAIN LANDING GEAR ON BLOCK IN WHILE INSTALLING CHOCKS. INSPECTED LEFT MAIN LANDING GEAR. NO EVIDENCE OF FIRE. JACKED AXLES AND CHECKED FOR FREE TIRE ROTATION LT MLG BRAKES CHECKED GOOD PER AMM 32-41-08.
EMERGENCY LIGHT INOP AT DOOR 2R STA. 654+36, WL 245. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-00, OPS CHECK GOOD PER WEPPS STG-SMM B767.
EMERGENCY LIGHT INOP AT STA 1192, LBL 96 WL 245. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-00 OPS CHECK GOOD PER WEPPS STG-SMM B767.
WEPPS FAILS SYSTEM DAILY TEST. FOUND LEAD BATTERY MODULE M735 WAS DE-REGISTERED PERFORMED RE-REGISTER PER STG SMM 767, OPS CHECK OK.
PURSER REPORTED ELECTRICAL SMELL IN THE AREA OF ROW 5 RIGHT SIDE OF AIRCRAFT DURING FLIGHT. COCKPIT CREW REPORTS NO SMELL IN AREA. CHECKED SEAT SEB'S READING LIGHTS AND OVERHEAD MONITORS IN AREA, NO SMELL NOTED.
EMERGENCY EXIT LIGHT INOP AT DOOR 2R. REMOVED AND REPLACED BATTERY PACK AS PER SSM/CMM B767 (STG).
EMERGENCY EXIT LIGHT INOP AT DOOR 2R. REMOVED AND REPLACED BATTERY PACK AS PER SSM/CMM B767 (STG).
L4 DOOR INTERIOR HANDLE HAS EXCESSIVE PLAY. T/S CONDITION, FOUND EXCESS PLAY DUE TO INNER HANDLE OUT OF RIG. FURTHER INVESTIGATION REVEALED MISSING BUSHING AT AFT SIDE OF SNUBBER MOUNT. INSTALLED BUSHING PER IPC 52-11-25-08A RIGGED INNER HANDLE MECHANISM AS PER MM 52-11-28-822-024 HANDLE RIG DOOR LOCK & INDICATION & EMERGENCY LIGHT OPS CHECK GOOD.
A/C HAD AN AIR TURNBACK TO KWI DUE TO LEFT BLEED DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. ACCOMPLISHED INSPECTION OF WING/BODY LEAK DECTION LOOPS REPLACED DAMAGED HARDWARE AND DECTOR ELEMENTS AS PER MM 26-18-01 REPLACED DECTOR CARDS PER MM 26-10-01 ACCOMPLISHED OPS CHECK OF SYSTEM CHECK GOOD. (ITEM CLOSED)
FOUND EXCESSIVE PLAY IN DOOR L4 HANDLE WHEN DOOR IS CLOSED AND LATCHED. FOUND BUSHING MISSING AT AFT SIDE OF SNUBBER MOUNT REPLACED BUSHING AND RIGGED HANDLE AS PER MM 52-11-28 CLEARED ON SDR NOCA09711.
A/C HAD AN AIR TURNBACK TO BAH DUE TO LEFT DUCT LEAK LIGHT ILLUM EICAS MSG LEFT BLEED DUCT LEAK DISPLAYED LIGHT EXTIN AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. FOUND LEFT ISOLATION BYPASS CHECK VALVE FLOATING SLEEVE LEAKING. REMOVED AND REPLACED 2 EACH SEALS AS PER MM 36-11-05, OPS CHECK GOOD.
NR 2 PLYON, ANGLE CRACKED INSIDE ROUND ACCESS HOLE BELOW I/B MID SPAR FITTING. REMOVED ANGLE LOCATED AND DRILLED REPLACMENT ANGLE PER SRM 51-10-02, INSTALLED NEW ANGLE PER SRM 51-10-02.
NR 2 PLYON, ANGLE CRACKED INSIDE ROUND ACCESS HOLE BELOW I/B MID SPAR FITTING. REMOVED ANGLE LOCATED AND DRILLED REPLACMENT ANGLE PER SRM 51-10-02. INSTALLED NEW ANGLE PER SRM 51-10-02.
SEAT TRACK CORROSION LBL 54.57 STA 654+44 TO 654+88. REMOVED CORROSION AS PER SRM 51-10-02 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE SEAT TRACK AS PER SRM 53-00-52. FABRICATED TRACK, PRIMED AND PAINTED, INSTALLED SEAT TRACK AS PER SRM 53-00-52.
SEAT TRACK CORROSION RBL 88 STA 1329. REMOVED CORROSION AS PER SRM 53-00-52. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REMOVED DAMAGED SEAT TRACK AS PER SRM 53-00-52. FABRICATED SEAT TRACK, PRIMED AND PAINTED, INSTALLED SEAT TRACK AS PER SRM 53-00-52.
SEAT TRACK CORROSION RBL 54.75 FROM STA 654+44 TO 654+88. REMOVED CORROSION PER SRM 51-10-02 FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK DAMAGED SECTION AS PER SRM 53-00-52. FABRACTED REPAIR PARTS PER SRM 53-00-52. TREATED AND PAINTED SEAT TRACK, INSTALLED SEAT TRACK AS PER SRM 53-00-52.
SEAT TRACK CORROSION RBL 55 STA 348. REMOVED CORROSION AS PER SRM 51-10-02 FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK, FABRICATED SEAT TRACK, PRIMED AND PAINTED SEAT, INSTALLED SEAT TRACK AS PER SRM 53-00-52.
RIGHT ENGINE LOOP NR 2 EICAS STATUS MSG. REMOVED AND REPLACED RT ENG NR 2 FIRE LOOP DETECTOR AMM 26-11-02-424-038-001, OPS NORMAL.
DAMAGE FOUND ON NR 2 ENGINE THRUST REVERSER LATCH AREA. AS PER SRM 54-52-90/101 SHEETS 3 AND 5 FIGURE 3, STA 188.42 HAS A DAMAGED FITTING. WIDTH 1.75 INCHES, WITH DAMAGED AREA AT .125 WHICH IS LESS THAN 10 PERCENT AS PER SRM DETAIL V AND DEPTH .125 WHICH IS AT 50 PERCENT OF THICKNESS AND IS OUT OF TOLERANCE AS PER SRM SECTION A-A OF DETAIL V. 10 PERCENT OF FLANGE WIDTH IS OK, FLANGE THICKNESS IS OUT OF TOLERANCE. REPLACED FAN COWL BEAM AS PER SRM 54-52-90 AND DRAWING 311U2510.
FLAP/SLAT ELEC STATUS MESSAGE. RETRACTED SLATS AT 260 KNOTS TRANSIT FOR 20 SECONDS. ACFT DIVERTED. FLAP/SLAT OVERSPEED PICKED UP BY AFIRS. ACCOMPLISHED PHASE 1 AND PHASE 2 INSPECTION OF L/E SLAT LEFT AND RIGHT PER MM 05-51-08, NO DISCREPANCIES FOUND. INSPECTED LEFT AND RIGHT WING TRACK ROLLERS AND SUPPORT BOLTS PER MM 12-21-08, NO DISCREPANCIES FOUND. LUBRICATED LEFT AND RIGHT WING SLAT TRACK ROLLERS AND SUPPORT BOLTS PER MM 12-21-05 AND -08 SYSTEM OPS CHECKED GOOD, NO DEFECTS NOTED.
RIGHT ENG FIRE LP NR 1 STATUS. REMOVED & REPLACED PRINTED CIRCUIT BOARD M689 RIGHT ENGINE LOOP 1 PER AMM 26-10-01, OPS CHECK GOOD, CLEARED CI 26-11 W/MCC.
EMERGENCY LIGHTS FROM 1GF TO MID GALLEY INOP. REPLACED BATTERY PACK AND CHARGER AS PER MM 33-51-07, OPS CHECK GOOD.
EMERGENCY LIGHTS FROM SEATS 1AB TO MID GALLEY INOP. REPLACED BATTERY PACK AS PER MM 33-51-07, OPS CHECK GOOD.
FROM CABIN LOG OVEN NR 1 IN THE FWD GALLEY IS INOP AND SPARKING. IN SEA OPENED CI 25-56 PER MEL 25-20-1 NEF 25-30-H. THE OVEN C/B WAS PULLED AND COLLARED AND OVEN IS NOT TO BE USED. REMOVED AND REPLACED NR 1 MID GALLEY OVEN OPS CHECKS NORMAL.
EICAS MESSAGE RT GEN OFF DISPLAYED, RT GEN OFF LIGHT ILLUMINATED, GENERATOR SWITCH RESET DID NOT CORRECT CONDITION. REMOVED AND REPLACED THE RT ENGINE IDG AS PER MM 24-11-01. IDG OPS CHECKS AND LEAK CHECK OK.
L-1 AND R-4 LAV SMOKE DETECTORS GOING OFF IN FLIGHT. PERFORMED T/S AND SYSTEM OPS CHECK AS PER FIM 26-13-00 FIG 103 AND AMM 26-13-00. L-1 LAV SMOKE DETECTOR SYSTEM OPS CHECKS NORMAL. TRANSFERRED R-4 LAV SMOKE DETECTOR SYSTEM INOP ITEM TO L/P 73139 ITEM 3M FOR DEFERRAL. OPENED CI-26-01 MEL 26-26-3 1-23-10 DISCREPANCY - R-4 LAV SMOKE DETECTOR SYSTEM INOP. LAV SECURED / LOCKED CLOSED PLACARDED INOP - DO NOT ENTER, LAV WASTE RECEPTACLE CONFIRMED EMPTY (DUE TO DETECTOR GOING OFF CONNECTOR DISCONNECTED AND STOWED). DATE:1/25/10 REF CI 26-01, R-4 LAV SMOKE DETECTOR INOP. REPLACED R-4 LAV SMOKE DETECTOR PER AMM 26-13-01, OPS OK.
L1 AND R4 LAV SMOKE DETECTORS SOUNDED, NO SMOKE OR FIRE WAS FOUND UPON INSPECTION. ACCOMPLISHED PROCEDURES IAW FIM 26-13-00 FIG 103 STEPS 1 THRU 6 SYSTEM TESTED SATISFACTORY.
ON T/O ROLL BETWEEN 85-95 KNTS RECEIVED MASTER WARRING AND EICAS MSG OF FLAPS, REJECTED T/O. ON TAXI BACK TO GATE WITH FLAPS AT 5 DEG RECEIVED MASTER / CAUTION EICAS MSG OF LEADING EDGE SLAT ASYM AND LEADING EDGE SLAT DISAGREE. IN BGR PSEU AND SENSOR S294 FOR NR 12 SLAT WAS REPLACED, ALSO CONDUCTED TASK 05-51-14-212-089 HI ENERGY STOP INSP T/S PER FIM 32-61-00 FIG 014 AND 105A PSEU FLT FAULTS CARD 010, AND TARGETS 234, 235, 236, 237 ALL TARGETS OK NORMAL. REMOVED AND REPLACED PSEU IAM AMM 32-09-04. OPS CHECKED OK. P/N OFF 8-497-04 S/N OFF C999. EN ROUTE TO NKT RECEIVED PHONE CALL AT APPROX 80 TO 100KNOTS T/O ROLL EICAS CAUTION RT AUX PITOT, CAPT PITOT, GEAR DISAGREE, LEFT SIDE BRACE & FORWARD CARGO HEAT MSGS. MSGS EXTINGUISHED & DID NOT RE-APPEAR. PER MX SENIOR MANAGER ELECTED TO DIVERT INTO ATL FOR MX WITH DELTA SUPPORT. N768NA ATL ON DEPARTURE AFTER ENGINE START LT AUX PITOT & F/O PITOT LIGHT REMAINED ILLUMINATED WITH PROBE HEAT & SPEED FLAG EICAS MSG, MX REP WITH DELTA MX PERFORMED BITE CHECK ON S236 SENSOR SHOWS NO FAULTS, A/C IS IN ATL HGR GETTING READY TO BE JACKED IN NEXT HOUR TO PERFORM GEAR SWING & OPS CHECK, A PSEU RACK CONNECTOR WAS FOUND TO HAVE A BAD PIN, AND WAS CHANGED, FERRY FLIGHT ATL--DFW. FLIGHT COMPLETED WITH NO MX ISSUES - NO RE-OCCURRENCE OF MX PROBLEM - ALL IS WELL - NO INBD MX ITEMS -A/C N768NA LANDED IN KWI WITH NO ISSUES AND THE A/C SAT FOR 20 MINUTES AT THE GATE. WHILE MX WERE ACCOMPLISHING THE DAILY CHECK, THE CREW INFORMED MX OF THE ISSUE. (EICAS MSGS; CAPT PITOT, LT AUX PITOT, LT AOA, TAT, EQUIPMENT COOLING. ALSO HEARD A LOT OF RELAYS CLICKING IN THE E/E AND ALL INTERIOR LIGHTS GOING BRIGHT TO DIM AND SO ON. WHILE THIS WAS HAPPENING MX WHEN TO BITE THE PSEU AND WERE UNABLE PERFORM THE BITE AND DID NOT STARTED THE TEST. SO MX KILLED POWER TO THE A/C AND REMOVED THE PSEU FOR A VISUAL AND DID NOT SEE ANYTHING WRONG WITH THE CONNECTOR OR THE BOX. THE BAX WAS INSTALLED AND POWER RESTORED THEN THE BITE WAS ENABLE. SEVERAL FAULTS NOTED INCLUDING AN INTERNAL PSEU FAULT. ALL MSG AND PSEU FAULT DISAPPEARED AND ALL WAS BACK TO NORMAL. MINUTE LATER ALL FAULT CAME BACK. RIGHT NOW MX IS LOOKING AT THE AIR/GROUND SYSTEM. ENGINEER IS IN THE LOOP. ALL T/S IS BEING DOCUMENTED IN THE LOG BOOK. A/C N768NA HAS A MX ISSUE RELATED TO THE PREVIOUS ISSUE THIS A/C HAD BACK IN ATL WITH THE PSEU. MX REP IS CURRENTLY T/S PER THE FIM. DUE TO FINDINGS BY MX & ENGINEERING OF IFE SYSTEM SEAT 22CDEF HARNESS SHORTED & CAUSING NUMEROUS PSEU MSGS & SL 767-SL-23-038 REFERENCE SEB MOD, DEACTIVATED SEAT 22CDEF WITH NO FURTHER ISSUES. AS PER CONVERSATION WITH DOM & ENGINEERING SEAT 22CDEF IS DEACTIVATED REF:CI 23-02 & AS PRECAUTION IFE SYSTEM PLACED ON CI 23-03 AS INOP. AS PER ENGINEER E-MAIL LISTED BELOW WITH THE IFE TURNED OFF AS PER FIM 27-80-00 FIG 7 STEP1, NO MESSAGES OR L/E ASSY LIGHT ON. FURTHERMORE, ALL OVERHEAD ENUNCIATOR LIGHTS ALSO OPERATE NORMAL WITH IFE SWITCH TURNED OFF. A BITE OF THE PSEU ALL NORMAL, NO FAULTS. DUPLICATED THE ISSUE SEVERAL TIMES WITH THE IFE TURNED ON AND HARNESS AT 22CDEF CONNECTED. ITEM CORRECTED OPS CHECKS GOOD.
RT ENG FIRE LP 1 STATUS MSG - FIRE LOOP 1 CORRECTION REPLACED TERM. LUG ON TS 683A1 OPS CK NML IAW MM 26-11-02.
EMERGENCY PATH LIGHTS INOP JUST FWD OF R4 DOOR. REPLACED EMERGENCY PATH LIGHT ASSY AS PER MM 33-51-10.
LOW SPEED ABORTED TAKEOFF AT 60 KNOTS DUE TO LEFT PRV EICAS MESSAGE. FLIGHT CREW ACCOMPLISHED AN ENGINE HIGH POWER RUN AND NO RETURNING EICAS MESSAGE.
LEFT MAIN LANDING GEAR SIDE BRACE UPPER SWIVEL FITTING O/B BORE HAS CORROSION ON BUSHING BORE. BLENDED TO REMOVE CORROSION FOR ENGINEERING EVALUATION, REPAIRED PER PRI 475336-14 REV 1 DATED JUNE 2009, RECEIVED FINAL ERA 475336-14 REV ORIGINAL DATED JUNE 10 2009- DEVIATIONS FROM PRI.
AFT CENTER LAV, SMOKE DETECTOR ON. RESET SMOKE DETECTOR AND TEST AS PER MM 26-13-00, OPS CHECK OK.
LT SIDE FLOOR EMERGENCY LIGHTS IN ROW 24 TO EMERGENCY EXIT BEHIND WING IS INOP. REMOVED AND REPLACED 2 EMERGENCY LIGHTS, NO HELP. REMOVED AND REPLACED BATTERY ASSY LT ROW 19-24. OPS CHECK NORMAL IAW 33-51-10 AND 33-51-07.
EMERGENCY PATH FLOOR LIGHTING SYSTEM FROM ROW 20 TO ROW 24 INOP. REPLACED BATTERY CHARGER FUSE F3 AS PER WDM 33-51-17, OPS CHECK OK.
OVERHEAD EMERGENCY EXIT AISLE ILLUMINATION LIGHTS INOP AT FWD GALLEY LT, 1B, 14B, 29G,12G, 37F, AND AFT GALLEY RT SIDE. RELAMPED AS REQUIRED, OPS CK'D NORMAL PER M/M 33-51-05.
SMOKE DETECTOR IN R4 LAV SOUNDING. RESET SMOKE DETECTOR, PERFORMED ADJ/TEST PER M/M 26-13-00 OPS CK'D NORMAL. P/N OFF AND ON - N/A.
APU FIRE EXTINGUISHING SYSTEM INOP. DISCHARGED THE BOTTLE INADVERTENTLY BY THE GROUND CREW FROM THE NOSE GEAR POSITION. ITEM REMAINS OPEN.
SMOKE ALARM KEEPS GOING OFF IN LAV R4. REMOVED AND REPLACED LAV SMOKE DETECTOR AS PER MM 26-13-01, OPS CHECK OK.
EMERGENCY LIGHTS AT ROW 12D THRU 20D INOPERATIVE. SPLICED MADE REPAIRED WIRING IAW SWPM CH 20. ALL OPS CHECKED GOOD. NO DEFECTIVE PART. (K)
F/O AIR DATA INSTRUMENTS PROCESSED RAPIDLY AND ADC FLAGS CAME INTO VIEW ALONG WITH L/R EEC WENT TO ALTERNATE MODE AILERON LOCKOUT AND RUDDER RATIO EICAS MESSAGES. REMOVED AND REPLACED NR 2 DADC, CHECKED NR 2 DADC IAW MM CHAPTER 34-12-01 ALL EICAS MESSAGE CLEARED OBSERVED PROPER AILERON RESPONSE, AND RVSM GEN GMM 3.33.63, 34-11-00 AS REQUIRED.
EMERGENCY PATH LIGHT AT 8B AND 16G INOP. RELAMPED PER MM 33-51-10.
E-PATH LIGHTS FROM L2 DOOR TO ROW 19 INOP. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-7, OPS CHECKED OK.
AUTOTHROTTLE DISCONNECTED ON LANDING. ACCOMPLISHED MCDP TEST 02 & 10 PER FIM TASK 22-00-02 FIG 104 & FOUND TMC AT FAULT. ACCOMPLISHED BY AA E58D-3 9326553. REMOVED AND REPLACED TMC PER MM 22-31-01, OPS CHECK OK. NO FAULTS NOTED.
DURING CLIMBOUT HAD EXCESSIVE AIRFRAME VIBRATION, NO EICAS MSG. REDUCED THRUST VIBRATION WENT AWAY. RETURNED TO BAH. ENGINE LIMITS AND ENGINE INDICATIONS WAS NORMAL. AN EXTERIOR INSPECTION WAS ACCOMPLISHED PER M/M 05-51-38 TASK 201, NO FAULTS WERE FOUND. INSPECTED ENGINE PANELS AND DOORS ALL NORMAL. CARGO BINS ALSO INSPECTED ALL FOUND TO BE NORMAL. ACCOMPLISHED ENGINE HIGH POWER RUN (VIBRATION SURVEY TEST 6) PER M/M 71-00-00-735-320-H00, ALL PARAMETERS WERE NORMAL WITH ENG NR 1 VIB .9 AND ENG NR 2 VIB 1.2 THE HIGHEST READING AT HIGH POWER. BOEING HAS DECODED THE DFDR DATA PROVIDED FOR BOTH THE BAHRAIN ATB ON 18-JAN-08 AND THE FLIGHT FROM NGU TO JFK ON 19-JAN-08. OUR REVIEW OF THE DATA SUPPORTS THE REF /F/ RECOMMENDATION TO REPLACE THE RIGHT ENGINE HMU AND EEC. REPLACED HMU P/N 442274, S/N BECK3868 PER MM 73-21-14 & AND RHT ENGINE FUEL PUMP AS PRECAUTIONARY REF E58 9326550, EEC PER 73-21-15.
DURING CLIMBOUT HAD EXCESSIVE AIRFRAME VIBRATION, NO EICAS MSG. REDUCED THRUST, VIBRATION WENT AWAY. RETURNED TO BAH. NO DOOR LIGHT INDICATIONS, ENGINE LIMITS AND ENGINE INDICATIONS WAS NORMAL. AN EXTERIOR INSPECTION WAS ACCOMPLISHED PER M/M 05-51-38 TASK 201 TO INCLUDE THE FUSELAGE ALL WING SURFACES AND WING TIPS, VERTICAL FIN AND RUDDER WITH THE FLAPS EXTENDED AND AGAIN WITH THE FLAPS RETRACTED NO FAULTS WERE FOUND. INSPECTED ENGINE PANELS AND DOORS ALL NORMAL. CARGO BINS ALSO INSPECTED ALL FOUND TO BE NORMAL. ACCOMPLISHED ENGINE HIGH POWER RUN (VIBRATION SURVEY TEST 6) PER M/M 71-00-00-735-320-H00, ALL PARAMETERS WERE NORMAL WITH ENG NR 1 VIB .9 AND ENG NR 2 VIB 1.2 THE HIGHEST READING AT HIGH POWER. LOG BOOK ITEM CLEARED, A/C DEPARTED BAH WITHOUT ANY ISSUES. BOEING HAS DECODED THE DFDR DATA PROVIDED FOR BOTH THE BAHRAIN ATB ON 18-JAN-08 AND THE FLIGHT FROM NGU TO JFK ON 19-JAN-08. OUR REVIEW OF THE DATA SUPPORTS THE REF /F/ RECOMMENDATION TO REPLACE THE RIGHT ENGINE HMU AND EEC.REPLACED HMU P/N 442274, S/N BECK3868 PER MM 73-21-14 & AND RHT ENGINE FUEL PUMP AS PRECAUTIONARY REF E58 9326550,EEC PER 73-21-15.
RIGHT ENG HPSOV EICAS MESSAGE. CREW FOLLOWED QRH AND TURNED OFF BLEED SWITCH. CREW STATED THAT THE RIGHT PACK WAS INOP AFTER TURNING BLEED SWITCH OFF. WITH BLEED ISSUE AND INOP PACK THE A/C CANNOT CONTINUE ETOPS A/C DIVERTING TO GANDER. SDR REMAINS OPEN.
REMOVE AND REPLACE SLIDE POS EMERGENCY RIGHT P/N 60174-104, S/N 0359. REMOVED AND REPLACED SLIDE POS EMERGENCY RIGHT SIDE PER MM 25-66-10. OK FOR SERVICES.
MID GALLEY LEFT SIDE FLOOR EMERGENCY LIGHT INOP. LIGHT ASSY NOT SECURED. REMOVED AND REPLACED MID GALLEY EMERGENCY LIGHT ASSY PER 33-51-16 WDM. OPS CHECK OK PER MM 33-51-10.
FWD GALLEY RIGHT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED FWD GALLEY RIGHT EMERGENCY LIGHT STRIP, WDM 33-51-16. OPS CHECK OK.
EMERGENCY LIGHTS INOP AT ROW 20-24. REMOVED AND REPLACED POWER SUPPLY AS PER MM 33-51-07.
WHEN RETRACTING THE LANDING GEAR AFTER T/O, THE RT GEAR LIGHT CAME ON WHEN BRINGING THE LEVER TO OFF POS, LANDING GEAR DISAGREE EICAS CAME ON ALSO. REPLACED DOOR LATCH ACTUATOR AND SEQUENCE VALVE ITEM IS STILL OPEN.
LANDING GEAR DOORS EICAS ILLUMINATED AFTER LANDING GEAR SELECTED DOWN. PERFORMED BITE ON PSEU PER FIM 32-09-03 AND 32-30-00, REPLACED S264 RIGHT LATCH SWITCH NR 2 SYS PER MM 32-61-02, OPS CHECK OK.
RIGHT HAND FIRST CLASS EMERGENCY FLOOR LIGHTS DIM THEN EXTINGUISH. REPLACED FWD BATTERY CHARGER, OPS CHECK OK.
APU FIRE BOTTLE ACCIDENTALLY DISCHARGED IN LEJ. REMOVED AND REPLACED APU FIRE BOTTLE IAW AMM 26-22-02. SYSTEM CHECKS NORMAL.
LEFT MLG BOGIE PIVOT PIN CRACKED. REPLACED MLG BOGIE PIVOT PIN AS PER EO 767-32-007.
E-PATH LIGHT INSIDE R4 DOOR JAMB AREA INOP. REPLACED LIGHT AND RECONNECTED WIRE AS PER MM 33-51-00.
RED E-PATH LIGHT INOP 26AB - 26GH. REPINNED BROKEN WIRE AS PER MM 33-51-00.
E-PATH LIGHT BY LEFT LAV INOP. REPLACED LIGHT AS PER MM 33-51-00.
E-PATH LIGHTING ABOVE 14AB INOP. REPLACED LIGHT AS PER MM 33-51-00.
RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED TERMINAL END AT LOWER FWD LOOP 1 DETECTOR PER 26-11-21 WDM. OPS CHECKS OK.
DURING PUSHBACK AND AFTER RT ENGINE START, RECEIVED R GEN OFF AND R GEN DRIVE LIGHT ON UPPER EICAS AND OVHD. REMOVED AND REPLACED NR 2 IDG PER MM 24-11-01. OPS CHECKS OK.
E-PATH LIGHT INOP AT SEAT 8A AND R2 DOOR CEILING INOP. REMOVED AND REPLACED EMERGENCY LIGHTS AT SEAT 8A AND R2 DOOR CEILING PER AMM 33-51-00. OPS CHECKS OK.
FWD GALLEY RT SIDE ELECTRO LUMINESCENT E-PATH LIGHT STRIP INOP. REPLACED LUMINESCENT E-PATH STRIP PER AMM 33-00-00.
LANDING GEAR MONITOR EICAS MESSAGE. REMOVED AND REPLACED NOSE GEAR DOOR SENSORS S234,S235 ADJUSTED NOSE GEAR DOOR AS PER AMM 32-22-02. ACCOMPLISHED GEAR SWING NO EICAS MSG, FAULTS BITE CHECK PROX DET UNIT SHOWS NO FAULTS.
FOUND EXTERIOR EMERGENY LIGHT AT L3 DOOR INOP. CLEANED CONTACTS AND RELAMPED PER AMM 33-51-00. OPS CHECKS OK.
MID GALLEY LT SIDE E-PATH LIGHT STRIP ONLY HALF IS ILLUMINATED. REMOVED AND REPLACED E-PATH LIGHT STRIP AS PER AMM 33-51-00. OPS CHECKS OK.
FOUND RIGHT SIDE EXTERIOR LIGHTS INOP. REPLACED EMERGENCY BATTERY POWER SUPPLY, OPS NML AS PER MM 33-51-07.
STATUS MSG FWD DET FAN DISPLAYED ON EICAS CORRECTIVE ACTION T/S FWD DET FAN MSG PER FIM 26-16-00. REPLACED FWD CARGO SMOKE DETECTOR PRESS SWITCH PER MM 26-16-03.
TCAS FAIL LANDING GEAR INDICATING DOWN. PERFORMED FIM 32-09-03 PSEU AT FAULT, REMOVED AND REPLACED PSEU PER MM 32-09-04, OPS OK. PERFORMED SYS TEST PER 32-09-04, TEST OK.
TAIL SKID LIGHT ON. REMOVED AND REPLACED PSEU PERFORMED FIM TASK 32-71-00, LIGHT AND MESSAGE OPERATE NORMAL.
FOUND AFT RIGHT DOOR AND OVERWING DOOR EMERGENCY LIGHT INOP. RELAMPED AFT RIGHT DOOR AND RIGHT OVERWING DOOR EMERGENCY LIGHTS PER MM 33-51-16. OPS CHECKS OKAY.
LANDING GEAR MONITOR STATUS MESSAGE. ACP BITE TEST ON PSEU CODE 235R NOSE DOOR CLOSE SYSTEM 1 FAULT VERIFIES SYSTEM 2 OPS NORMAL. ITEM DEFERRED PER MEL 32-61-02-01 CI 32-41 VERIFY SYSTEM 2 OPS NORMAL PRIOR TO EACH FLIGHT. 12/22/06 T/S PER FIM 32-61-00 FOUND S235 BAD. REMOVED AND REPLACED S235 (NOSE GEAR DOOR SWITCH) PER MM 32-61-03. ALL OPS CHECKS OK.
FORWARD FUEL CROSS FEED VALVE ION WITH MICAS MSG. ON ARRIVAL NO MICAS MUG NOTED. PERFORMED ENG CROSS FEED VALVE TEST PER MM 28-22-00, OPS TEST OK. NO FAULTS NOTED.
RIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE. PERFORMED SYSTEM T/S AND BITE CHECK AS PER FIM 26-11-00 FIGURE 101. MESSAGE CLEARED. NO FUALTS NOTED. SYSTEM OPS CHECKS NORMAL. A/C OK FOR SERVICE.
"LE SLAT ASYM" MSG DISPLAYED AND LIGHT ILLUMINATED AND CENTER HYD SYS WHITE "ISLN" LIGHT ON P61 PANEL ILLUMINATED. PERFORMED T/S PER FIM 32-09-03 AND INSPECTED L/E PER AMM 27-51-01. REMOVED AND REPLACED ADP AND CENTER ISOLATION VALVE AND CENTER NR 1 PUMP CASE DRAIN FILTER AND ADP PRESS REG SHUTOFF VALVE. OPS AND LEAK CHECK OK PER AMM 29-11-03, 29-11-08, 29-11-19, 29-11-30, 27-58-00. " LE SLAT ASYM" MSG DISPLAYED AND L\E LIGHT ILLUMINATED WHEN FLAPS/SLATS EXTENDED ON TAXI OUT. THEN L\E WOULD NOT RETRACT, T\E FLAPS CAME UP (BLOCK TURN BACK). FOUND NR 3 L\E SLAT POSITION TARGET LOOSE ON INBOARD SENSOR. SECURED TARGET, PERFORMED OPS CHECK PER AMM 27-88-01. REMOVED AND REPLACED PSEU PER AMM 27-1-01. PERFORM
DURING TAKEOFF ROLL AT 60 KNOTS MASTER WARNING AND EICAS (MESSAGE FLAPS). ABORTED TAKEOFF AND PERFORMED LOW ENERGY STOP. PERFORMED T/O WARNING SYSTEM TEST IAW FIM 31-51-00 FIG 107, OPS CHECK. TE FLAPS IAW AMM 27-58-00 PERFORMED PSEU BITE PROCEDURE IAW FIM 32-09-03 FIG 103. CLEARED FAULTS AND NO DEFECTS FOUND. 9/25/06 FOUND NR 303 TARGET NR 9 L/E SLAT MISSING TARGET PLATE FROM AUX TRACK AT IB T\S IAW FIM 27-81-00 FIGURE 107, INSTALLED NR 9 L/E SLAT PLATE IAW MM 27-88-01 / 401 SYSTEM TEST OK.
BIRD STIRKE ON TAKE OFF FROM BJL RT ENGINE, FAN VIB 4.1 RECORDED. LANDED SAFELY AT BJL AFTER FUEL DUMPED. REPLACED 4 FAN BALDES, OPS NORMAL.
EMERGENCY FLASHLIGHT AT R4 INOP. REMOVED AND REPLACED FLASHLIGHT.
EXTERIOR EMERGENCY LIGHTS INOP AT 4L AND 3R. RELAMPED LIGHT AT 4L AND 3R, OPS NORMAL.
ELECTRIC FLAP MOTOR NOT WORKING WHEN SELECTED TO NR 1 DEGREE DETENT. REPLACED SWITCH, OPS NORMAL.
RED EMERGENCY LIGHT INOP AT SEAT 26G. RELAMPED, OPS NORMAL.
LEFT AUTO PILOT DOES NOT ENGAGE IN APPROACH MODE. REPLACED LT ELEVATOR AUTO PILOT SERVO, OPS NORMAL.
LEFT AUTOPILOT WOULD NOT ENGAGE IN APPROACH MODE. REMOVED AND REPLACED LEFT FCC.
LT AUTOPILOT WOULD NOT ENGAGE IN APPROACH MODE. ITEM PLACED ON MEL 22-10-1.
EMERGENCY PATH LIGHT INOP 1GH. REPLACED LIGHT BULB, OPS NORMAL.
O/H EMERGENCY LIGHT INOP BY SEAT 34B
EMERGENCY LIGHT STRIP AT R4 DOOR INOP.
STANDBY ATT INDICATOR SHOWS 3 DEGRESS TO THE RIGHT IN LEVEL FLIGHT.
EXTERIOR EMERGENCY EXIT LIGHT OUT AT RIGHT EMERGENCY EXIT DOOR.
EMERGENCY EXIT LIGHT FLOOR BULB OUT JUST FORWARD OF GALLEY RIGHT SIDE.
THREE EMERGENCY EXIT LIGHTS OUT FORWARD OF RIGHT AFT LAV.
EMERGENCY LIGHTS FROM 26AB TO 36AB INTERMITTENT.
R-3 EMERGENCY DOOR EXTERIOR LIGHT INOP.
R-3 EMERGENCY DOOR EXTERIOR LIGHT INOP.
LT RECIRCULATION FAN WRITTEN UP FOR HAVING AN ELECTRICAL BURNING SMELL, FAN WAS DEFERRED IAW MEL 21-25-01.
FOUND L4 GIRT BAR DEPLOYMENT CABLES DISCONNECTED. REPLACED SLIDE ASSEMBLY. STATEMENT PROVIDED BY MECHANIC INDICATES CABLES WERE BROKEN AT THE GIRT BAR ATTACH POINT. THIS WAS DISCOVERED DURING A FLEET CAMPAIGN DIRECTIVE DUE TO OTHER PROBLEMS ON 767 FLEET EMERGENCY ESCAPE SLIDES.
EMERGENCY FLOOR PATH LIGHTING INOPERATIVE IN FRONT OF 2L LAVATORY. RESEATED CONNECTOR AT 2L LAVATORY OPS CHECK NORMAL. EMERGENCY EXIT MARKER AT 2L DOOR INOPERATIVE. REPLACED CONTACT AND QUICK DISCONNECT AT 2L DOOR EMERGENCY EXIT MARKER OPS CHECKED NORMAL.
DURING CABIN CHECK, FWD GALLEY MEGAPHONE FOUND NOT WORKING. REPLACED BATTERIES FOR MEGAPHONE IN ACCORDANCE WITH AMM-25-63-02. MEGAPHONE OPERATES NORMALLY.