N651GT
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING TAXI, RT ENGINE HOT START-563 DEGREES FOR 6 SECONDS. RETURNED TO THE GATE (BTB). PER ABX AMM 71-00-00 & FIM 71-08 FAULT TREE 816 . MOTORED RT ENG FOR 30 SECONDS. STARTED ENGINE WITH A MAX EGT OF 381. AIRCRAFT OK FOR SERVICE.
DURING TAXI, FWD CARGO DOOR EICAS CARGO DOORS DISCRETE ILLUMINATED. RETURNED TO THE GATE (BTB). MTC DEFERRED FWD CARGO DOOR INDICATION SYSTEM PER MEL 52-71-1-1. PLACARDS INSTALLED. VERIFIED DOOR CLOSED AND LOCKED. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH DEPARTURE. ACFT RETURNED TO SERVICE.
DURING MTC/INSP, WHEEL WELL AFOLTS TEST INOP. PUT STBY POWER SWITCH IN AUTO. WHEEL WELL FIRE DETECTION SYSTEM CHECKS GOOD PER AMM 26-17-00. ACFT RETURNED TO SERVICE.
VERY HEAVY VIBRATION FROM LEFT ENGINE DURING ENGINE START UP & TAXI. DID ENGINE RUN UP & IT GOT WORSE. NO BAD ENGINE INDICATIONS ON EICAS. A/C RETURNED TO BLOCKS (BTB). AIRCRAFT FREIGHT LOAD IS LIGHT AT 15,500. PERFORMED ENGINE IDLE RUN AND BREAK AWAY POWER RUN UP OF BOTH ENGINES IAW AMM 71-00-00, WITH EEC'S ON AND OFF. ALL INDICATIONS NORMAL, NO VIBRATIONS NOTED. PERFORMED GVI INSP WITH NO DEFECTS NOTED. A/C OK FOR SVC. A/C REMAINS NO ETOPS.
DURING TAXI AFTER ENG START "RIGHT BLEED OFF" LIGHT ILLUMINATED W/ "R BLEED OFF" EICAS MESSAGE. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. FOUND RT HPSOV LOCKOUT PLUG RETAINER CABLE IN BETWEEN PLUG AND HOLE, ALLOWING AIR TO BYPASS. REMOVED OLD, THEN INSTALLED NEW RT HPSOV PER AMM 36-11-07. LEAK CHECK OK. OPS CHECK UNABLE; HOLE IN ECS TUBE. SEE L/P 39434-42/2. REMOVED AND REPLACED HPSOV TUBE AS REQUIRED IAW AMM 36-11-07. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE: PWA, JT9D7R4D
DURING TAKE-OFF, RECEIVED R ENG BLEED VALVE CAUTION MESSAGE DURING FIRST 60 KTS OF T/O ROLL. AIRCRAFT ABORTED TAKE-OFF (ATO). MAINTENANCE DEFERRED RT ENG HPSOV IAW MEL 36-11-2-1. MX PREOCEDURES C/W. PLACARDS INSTALLED. MBCB 03/30/2026. AIRCRAFT RETURNED TO SERVICE.
R ENGINE BLEED VALVE CAUTION MSG ON THE CLIMB THROUGH 8000 FT .WE RAN THE QRH AND CONTINUED CRUISING AT FL380 SINCE THERE WAS NO LIMITING FACTOR TO THE FLIGHT. JUST AS WE STARTED DESCENDING TO FL240 WE GOT A CABIN ALTITUDE WARNING MESSAGE WHICH FORCED US TO EXECUTE AN EMERGENCY DESCENT TO 10.000 FT.THEN LANDED .MTX GROUNDED A/C, INSPECTED AND FOUND TERMINALS 1 AND 2 BROKEN ON HPSOV. RE-TERMINATED TERMINALS 1 AND 2 ON R ENG HPSOV IAW SWPM 20-30-11 AND WDM 36-11-62. OPS CHECK OF HPSOV GOOD IAW AMM 36-11-07. PERFORMED ENGINE RUN ON R ENG IAW AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME.AND RETURNED A/C TO SERVICE .
STATUS MSG AFT CARGO DET 2, WHILE PERFORMING MAINTENANCE, MTX REMOVED AND REPLACED SMOKE DETECTOR M327 'AFT DET 2 . IAW AMM 26-16-01. OPS CHECK GOOD . MSG.CLEARED REF LOG PAGE 39342-63/3. AC RETURNED TO SERVICE.
DURING PREFLIGHT CHECK, FOUND MAIN CARGO LOOP A2 INOP. MAINTENANCE DEFERRED ITEM MBCB 03-15-26 IAW MEL 26-16-2-1. REMOVED AND REPLACED SMOKE DETECTOR 2A IAW B767 AMM 26-14-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE.
DURING TAXI OUT, AND AFTER ENGINE START, ENG EEC PROBE AND MACH PROBE LIGHT AFTER START STILL ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE T/S IAW ABX FIM 30-34 FAULT TREE 803. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.
ON TAXI OUT, STAB TRIM EICAS MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED SYSTEM IAW ABX-27-41-2. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI OUT PILOT VERBAL RH T/R REV. ISLN VALVE EICAS MEASAGE .APPEARED.A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX DEFERRED RH T/R FOR DEARTURE IAW MEL 78-31-1 MX PROCEDURES ACCOMPLISHED PLACARDS INSTALLED MBCB 01/13/26.AND RETURNED A/C TO SERVICE.
DURING TAXI OUT, R DUCT LEAK LP 1 STATUS MSG. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX THEN DEFERRED LP 1 DUCT LEAK DETECTION IAW MEL 26-18-1-1-1, MX PROCEDURES C/W, MBCB 01/08/26, PLACARDS INSTALLED.AND RETURNED A/C TO SERVICE
RIGHT BLEED AIR VALVE MESSAGE CAME ON TAKE-OFF ROLL, ABORTED AT 40 KNOTS. (ATO) TAXIED BACK TO GATE. (BTB) DEFERRED R ENG HPSOV PER MEL 36-11-2-1, MX PROCEDURES ACCOMPLISHED PER MPM 36-11-2, PLACARDS INSTALLED, MBCB 01-03-26 , AUTH# 2025-046. AIRCRAFT RETURNED TO SERVICE.
AFT CARGO FIRE INDICATION AFTER ENGINE SHUT OFF IN BLOCK, RAN QRH CHECKLIST AND DISCHARGED FIRE BOTTLE. CALLED TOWER AS EMERGENCY AIRCRAFT AND ASKED FOR FIRE TRUCKS. FIRE CHIEF FOUND NO ISSUE, NO SMOKE OR FIRE. MAINTENANCE REMOVED & REPLACED #1 AFT CARGO FIRE BOTTLE IAW BAC AMM 767 26-23-02; OPS CHECK GOOD C/W RII FORM 26-04-01. AIRCRAFT RETURNED TO SERVICE.
A/C TAXIED OUT WITH OPEN L/B WRITE UP. MAINTENCE PREVIOUSLY PULLED CVR C/B P11/H34 TO FOM. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE RESET P11 H34 CIRCUIT BREAKER I.A.W B767 AMM 20-60-01. AIRCRAFT RETURNED TO SERVICE.
WHILE FLYING FLIGHT ABX520 FROM HOUSTON TO SAN ANTONIO, GOT A LE SLAT DISAGREE CAUTION MSG ON DEPARTURE FROM KIAH. ACCOMLISHED QRH AND GOT LIGHT AND MSG TO EXTINGUISH. QRH DIRECTS TO LAND AT FLAPS 20, WHICH IS A NON-STANDARD LANDING CONFIG. EMERGENCY DECLARED TO BE ON SAFE SIDE. FOUND FSEU FAULT "LVR1 NOT IN DETENT" DUTRING BITE TEST IAW FIM 27-51 FT 809 PERFORMED LEVER SENSOR BITE PROCEDURE IAW FIM 27-51 FT 842 FOUND VOLTAGE OUT OF LIMITS AT MULTIPLE POSITIONS ADJUSTED SENSOR M604 TO BE BACK WITHIN LIMITS IAW B767 FIM 27-51-00/101 FIG 104A. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, RT ENG FIRE LOOP 2 STATUS MESSAGE ILLUMINATED. ITEM PLACED ON MEL ABX 26-11-1-1. PLACARD INSTALLED MBCM DATE 12/11/2025. AIRCRAFT RETURNED TO SERVICE.
ON PUSHBACK, ENG EEC PROBE LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS. (BTB). ACCOMPLISHED SYS OPS CK IAW AMM 30-34-00, ALL CKS NORMAL. VERIFIED WITH ENG IDLE RUN ON BOTH ENGINES. AIRCRAFT RETURNED TO SERVICE.
RT ENG ABORTED ENG START DURING TAXI OUT,BECAUSE OF HOT START. EXCEEDED LIMITS FOR 1 SEC. UP TO 539 DEGREES.A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX PERFORMED A SECOND TIME R ENG START. EGT READING 279 REF FIM 71-08 TASK 816. NO FURTHER MX ACTION NEEDED. AMENDED ALSO WHILE IN GATE A FLAP / SLAT ELEC.MEASSAGE APPEARED.MTX PERFORMED FIM TASK FLAP SLAT ELEC UNIT REF FIM 27-51 TASK 836 OPS CK OK MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.AND DEPARTED
RIGHT ENG ABORTED ENG START DURING TAXI OUT,BECAUSE OF HOT START. EXCEEDED LIMITS FOR 1 SEC. UP TO 539 DEGREES.A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX PERFORMED A SECOND TIME R ENG START. EGT READING 279 REF FIM 71-08 TASK 816. NO FURTHER MX ACTION NEEDED. AIRCRAFT RETURNED TO SERVICE.
DURING CRUISE, NOTICED R1 WINDOW ELECTRICAL ARC FOLLOWED BY R FWD WINDOW CAUTION MSG FOLLOWED BY SPIDER WEB CRACKING IN R1 WINDOW. EMERGENCY DECLARED. AIR TURN BACK TO CVG. REMOVED AND REPLACED R1 WINDOW ITEM CONTROLLER IAW B767 AMM 30-41-01. OPS CK GOOD. AND REPLACED R1 WINDOW IAW AMM 56-11-01. OPS CK GOOD. AIRCRAFT RETURNED TO SERVICE.
LE SLAT DISAGREE EICAS DISPLAYED AFTER TAKEOFF. OUT OF PHX ACCOMPLISHED QRH, AND CLEARED MSG, CONTIUNED TO LAX AND LANDED WITH FLAPS 20. AND DECLARED EMERGENCY BECAUSE OF FLAP CONFIGURATION NOT NORMAL.PER QRH, LANDED WITH NO OTHER COMPLICATIONS AND TAXIED TO GATE ,MTX GROUNDD A/C AND PERFORMED FSEU BITE TEST IAW FIM 27-51 FAULT TREE 809, FOUND M483 INBD SLAT POSITION 1 OUT OF RIG ACCORDING TO TABLE 405/27-81-11-993-810. ADJUSTED POSITION RET AND LDG OF SLAT PDU BVDT (M483), RIG WITHIN LIMITS REF 27-81-11 A/C RETURNED TO SERVICE.
RIGHT BLOWOUT PANEL 611KB WAS MISSING UPON AIRCRAFT ARRIVAL INTO LAX. RT BLEED DUCT LEAK CAUTION MESSAGE IN CLIMB OUT AND DUCT LEAK DESCRETE LIGHT . INSPECTED AND FOUND LEADING EDGE TAI DUCT BLOWN. REMOVED AND REPLACED DUCT SECTION OF RH WING LE IAW AMM 36-11-01. PERFORMED INSPECTION CHECKS FOR LEAKS IAW AMM 36-11-01 NO LEAKS NOTED. OPS GOOD. INSTALLED SERVICABLE RT PRESSURE RELIEF WING LE PANEL (611KB) IAW AMM 57-91-57. A/C OK FOR SERVICE.
DURING TAXI OUT ANTI-STALL CIRCUIT BREAKER POPPED WHEN RIGHT ENGINE START SELECTOR WAS PUT IN GND . ACFT RETURNED TO THE GATE (BTB). AND MTX GROUNDED AC . MTX DEFERRED RH T/R PER MEL 78-31-1. MX PROCEDURES 78-31-1 C/W. PLACARDS INSTALLED .MBCB 10-20-25. AIRCRAFT DOWNGRADED TO CAT 3 A .MTX RETURNED AC TO SERVICE.
ON LANDING, EMERGENCY ESCAPE IN SUPERNUMERARY SELF DEPLOYED ON LANDING. MAINTENANCE REMOVED AND REPLACED 4 EACH DECENT DEVICES IN SUPERNUMERARY IAW B767 AMM 25-61-03. THIS CLEARS DI 68427, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. ALL 4 P/N'S REMOVED: 379103D-29. S/N'S REMOVED: POS: 2SUP S/N: 12297, POS: 4SUP S/N: 20801, POS: 5SUP S/N: 20995, POS: 6SUP S/N: 24103.
AFTER ENGINE START, UNUSUAL AIRFRAME VIBRATION. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED FLT CONTROL CHECK IAW AMM 27-00-00, NO DEFECTS FOUND. ADDED MORE FUEL TO AIRCRAFT AND PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS GOOD, NO VIBRATION NOTED. AFTER MORE WEIGHT ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE.
DURING SERVICE CHECK FOUND PILOT SEAT LIFE VEST DUE INSP WITHIN 30 DAYS REMOVED OLD LIFE VEST REPLACED WITH SERVICABLE UNIT IAW B767 AMM 25-62-00 RETURNED TO SERVICE
(4) INERTIAL ESCAPE REELS DROPPED AFTER LANDING. DEFERRED IAW MEL C ABX-25-61-1-1. REMOVED AND REPLACED 4 DESCENT DEVICES IAW AMM 25-61-03. PLACARDS REMOVED. THIS CLEARS DI 65509. NO FURTHER MAINTENANCE ACTION REQUIRED. LP 39229-54/1. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI, AT THE "AFTER START" THE LEFT PACK OFF REMAINED ILLUNMINATED. ACCOMPLISH QRH 2-31. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED LT PACK PER MEL 21-51-1-1. MPM 21-51-2 COMPLIED WITH. PLACARDS INSTALLED. MBCB 08-29-25. LP 39197-90/1. AIRCRAFT RETURNED TO SERVICE.
DURING PRE-FLIGHT INSPECTION, INERTIAL ESCAPE REELS #4 AND #6 FELL OUT OF THE HOUSING. DEFERRED IAW MEL C ABX-25-61-1-1. INSTALLED INERTIAL ESCAPE REELS DESCENT DEVICES AT THE #4 AND #6 SPOT IAW AMM 25-61-03. DI 65048 CLOSED. REF LP 39197-68/1. #4 - PN: 379103D-29, SN 21776. #6 - PN: 379103D-29, SN 11220. AIRCRAFT RETURNED TO SERVICE.
ON #2 ENG START WHILE TAXING EGT EXCEEDANCE TO 562Â AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC. MTX PERFORMED #2 ENG. START ,EGT FOUND TO BE IN LIMITS. IAW FIM TASK 71-08 FAULT TREE 816. AND MTX RETURNED AC TO SERVICE.
"DURING THE ACCOMPLISHMENT OF APU REPLACEMENT AT CVG/FEAM, CORROSION WAS DISCOVERED IN THE APU COMPARTMENT. ONE OF THE AFFECTED COMPONENTS IS SKIN PANEL PIN I 48T3280-2. THE CORROSION ON THIS ITEM WENT OUT OF I IM ITS. THE SKIN PANEL IS A BONDED UNIT MADE OF 2EA. 0.0 I 6"" 2024-T3 CLAD PLIES. ABXAIR CONTACTED AMES ENGINEERING REQUESTING TO FABRICATE THE PANEL FROM A SINGLE SHEET OF0.032'"" 2024-T3 SHEET PER QQ-A- 250/5. THE REPAIR/REPLACEMENT SKIN PANEL WAS MANUFACTURED FROM 2024-T3 X 0.032"" ALUMINUM CLAD SHEET (QQ-A-250/5) IN LIEU OF2 PLIES OF2024-T3 X 0.016"" ALUMINUM CLAD SHEET (QQ-A-250/5) BONDED TOGETHER PER BMS5-69, TYPE I, CLASS_3, GRADE B. BY OBSERVATION THE REPLACEMENT SKIN PANEL RETAINS THE SAME CROSS SECTION AREA BY DESIGN AND MECHANICAL PROPERTIES PER MMPDS-04. THIS PART WAS REVIEWED PER 767-200 SRM 51-00-04 AND DETERMINED TO BE SECONDARY STRUCTURE, NON-PSE, NON-ALI, AND NON-FCBS WITH NO APPLICABLE OEM SERVICE DOCUMENTATION OR AIRWORTHINESS DIRECTIVES.REPAIRED FRAMES AND REPLACED SKIN PANEL, 2 CLIPS, AND 2 INTERCOSTALS IAW B767-200 SRM 53-80-01, 53-80-07, 51-40-02, B767 AMM 51-21-10,AND ABX-REA-5300-65805-00."
DURING TAXI, HOT START #2 ENG WITH EGT EXCEEDANCE AT 543 C. A/C RETURNED TO BLOCKS. (BTB). MAINTENANCE MOTORED #2 ENGINE AND LET IT COOL PER AMM 71-00-00 AND FIM 71-08 FT 816. RESTARTED #2 ENGINE. MAX EGT DURING ENGINE START WAS 355 DEGREES AUTH NUMBER 2025-019. AIRCRAFT RELEASED FOR SERVICE.
DURING TAXI OUT, L PACK EICAS MESSAGE DISPLAYED AFTER ENGINE START. A/C RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED L PACK IAW MEL ABX-21-51-1-1. A/C RETURNED TO SERVICE.
DURING TAXI OUT LT PACK INOP MSG CAME ON, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED LH PACK FOR DEPARTURE IAW MEL ABX-21-51-1-1. AND RETURNED A/C TO SERVICE .
DURING TAXI, R GEN DR EICAS MESSAGE APPEARED AFTER START, R GEN OFF EICAS MESSAGE AFTER START. AICRAFT RETURNED TO GATE. (BTB) DEFERRED RH GEN IAW MEL ABX-24-00-1-3. MTX RETURNED A/C TO SERVICE.
DURING TAXI, FWD CABIN TEMP AND AFT CABIN TEMP EICAS OCCURED. MAINTENANCE GROUNDED A/C. TROUBLESHOT AND REMOVED AND REPLACED ZONE TEMP CONTROLLER REF B767 AMM 21-61-03. OPS CK NORMAL. MTX RETURNED A/C TO SERVICE.
DURING C CHECK AIRBORNE MAINTENANCE REPORTED AN EXISTING FLUSH SKIN REPAIR INSTALLED AT STA 440-460 BETWEEN STRINGERS 33R AND 35R. THE REPAIR WAS ACCOMPLISHED BY THE PREVIOUS OPERATOR IN 2008 AND IT WAS DOCUMENTED AS ACCOMPLISHED PER 767-200 SRM 53-00??0L REPAIR 003. A NEW CRACK WAS NOTED IN THE FUSELAGE SKIN FWD OF THE REPAIR CUTOUT(FLUSH FILLER). AIRBORNE FOUND THE REPAIR NOT TO BE PER SRM GUIDELINES DUE TO MULTIPLE REASONS. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. REPAIRE ACCOMPLISHED IAW ABX-REA-5335-65592-00.
RIGHT ENGINE SURGED DURING CLIMB, AC DECLARED EMERGENCY AND PERFORMED (ATB) AC RETURNED TO GATE AND MTX GROUNDED AC .AC IS CURENTLY BEING WORKED IN LAX , AMENDED REORT WILL BE SENT WHEN WORK IS COMPLETED. REMOVED AND REPLACED EEC PT2/TT2 PROBE IAW AMM 73-21-04. OPS CHECK GOOD.AC WAS RETURNED TO SERVICE.
THIS REPORT IS AMENDED AC IS RECORDED 650GT AND ACTUALLY IS 651GT . DURING FLIGHT FROM CVG TO ELP WX RADAR FAILED AND AIRCRAFT DECIDED TO RETURN TO CVG .AC LANDED AND MTX GROUNDED AC . MTX TROUBLESHOT AND REPLACED WEATHER RADAR TRANSCEIVER IAW B767 AMM 34-43-01 OPS CHECK GOOD . MTX RETURNED AC TO SERVICE
DURING FLIGHT FROM BOS TO CVG Â TO FL380 AT LEVEL OFF R ENG PAC STALLED AND SURGED THE RIGHT ENG ROLLED BACK TO IDLES AS THIS BEGAN THE EGT STARTED INCREASING WE SECURED R ENG @ 680 EGT.CREW DECARED EMERGENCY, SHUT DOWN RH ENGINE AND DIVERTED TO JFK AIRPORT AND LANDED SAFELY. BLOCKED INTO GATE. MTX GROUNDED AC AND AC IS CURRENTLY IN WORK IN JFK. REMOVED AND REPLACED RH ENG FUEL PUMP ASSY AND MEC IAW AMM 73-11-01 AND 73-21-01. ACCOMPLISHED ENGINE TESTS #3 IAW AMM 71-00-00.CONDUCTED TEST 9 ON RH ENGINE PER AMM 71-01-00/501. ALL NAMED TRIM ITEMS WITHIN PARAMETERS LP 38898-84/1 AC RETURNED TO SERVICE.
DURING TAXI Â FIRST OFFICER WINDSHIELD WIPER IS INOP AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC MTX CYCLED CONTROL SWITCH AND POWER, F/O'S WINDSHIELD WIPER SYSTEM OPS CHECK GOOD IAW B767 AMM 30-42-00 AC WAS RETURNED TO SERVICE AND DEPARTED
WHILE STARTING #2 ENGINE DURING TAXI ,START TEMP RAPIDLY INCREASED AND EXCEEDED EGT START LIMITS(551 MAX) AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC MAINTENANCE PERFORMED FIM 71-08 FAULT TREE 816 CHART AREA F. PERFORMED SECOND ENG START, ENG START WAS SATISFACTORY PEAK EGT 365'C (06/17/2024) A/C OK TO CONTINUE SERVICE.
AFTER CLIME STARTED TO LEVEL OFF AND LEFT ENGINE COMPRESSOR STALL NOTED 4 TIME 39-34 LEFT EPR DROPPED BELOW 1.0 R EPR 1.0 LEFT THEN SURGED TO BACK TO 1.0 . AC PERFORMED AIR TURN BACK AND LANDED NO ENGINE SHUT DOWN. MAINTENANCE GROUNDED AC AND PERFORMED ACCOMPLISHED SURGE (STALL) INSPECTION IAW B767 AMM 72-00-00 .ACCOMPLISHED FRONT TO BACK BORESCOPE INSPECTION IAW B767 AMM 72-00-00/601. NO DEFECTS NTOED FOUND EXCESSIVE HYDRAULIC BUILDUP IN LEFT ENGINE 7TH STAGE UNISON RING.CLEANED IAW B767 FIM 71-07 FT 827. LEFT ENGINE THRUST REVERSER FLOW AND METERING VALVE LEAKING .REMOVED AND REPLACED LH TR FLOW CONTROL VALVE MANIFOLD IAW B767 AMM 78-34-02 LEAK CHECK OPS CHECK GOOD PERFORMED HIGH POWER RUNS CHECKED GOOD AND PERFORMED MX TEST FLIGHT AND WAS TEST FLIGHT SATISFACTORY.AC RETURNED TO SERVICE.
DURING TAXI WHILE STARTING #2 ENGINE RIGHT ENGINE HAD SIGNIFICANT VIBRATION AFTER ENGINE START ,ENGINE INSTERMENTS WERE NORMAL. AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC .PERFORMED VISUAL INSPECTION OF FAN BLADES, CORE COMPONENTS VBV/VSV, GEARBOX, ALL LOOK NORMAL NO DEFECTS. PERFORMED MULTIPLE ENGINE RUNS AT IDLE AND PART POWER NO EXCESSIVE VIBRATION FELT ON RH ENG AND COMPARED TO LEFT ENG, OK FOR SRVC AMM 71-00-00 ALL ENG PARAMETERS AND INDICATION NORMAL-VIB .1 @ IDLE AND .2 @ PART POWER. CYCLED EEC'S OFF/ON NO CHANGE. ALL RUNS WERE GOOD IAW AMM 71-00-00. AC RETURNED TO SERVICE .
DURING TAXI OUT CENTER HYD SYS FAILED. CENTER HYD SYS & PRESS & QTY LIGHTS ILLUMINATED WITH "C HYD SYS PRESS" EICAS MSG. CENTER HYD QTY READS .09 RF ON STATUS PAGE AND RESERVE BKS AND STRG SWITCH "VALVE" LIGHT REMAINS ILLUMINATED WHEN DEPRESSED TO ON POSITION,AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC .TROUBLE SHOT AND FOUND RAT CHECKOUT MODULE LEAKING, REMOVED AND REPLACED RAT CHECKOUT MODULE. SERVICED CENTER HYD. SYSTEM TO 1.02. CYCLED FLIGHT CONTROLS + MLG DOORS TO PURGE AIR FROM SYSTEM. RAT CHECKOUT MODULE LEAK CHECK GOOD. WORK DONE IAW B767 AMM 29-21-11, 12-12-01. AFTER SERVICE RESERVE BRAKE AND STEERING SYSTEM OPS CHECK GOOD IAW B767 AMM 32-41-00 AC RETURNED TO SERVICE
CENTER HYD SYSTEM HYD LEAK. REPLACED C1 PUMP IAW B767 AMM 29-11-02. OPS AND LEAK CHECK GOOD.AC RETURNED TO SERVICE.
RIGHT ENGINE START VALVE BAD. REMOVED AND REPLACED RIGHT ENGINE STARTER CONTROL VALVE ASSY. IAW ABX B767 AMM 80-11-02 SERVICEABLE UNIT INSTALLED OP CK OK. DI 50365 IS CLEARED PLACARD REMOVED NO MX DI PROCEDURE ACCOMPLISHED.
ATTEMPTED X BLEED START ON RT ENG INITIALLY N2 ROSE TO 20% THEN START VALVE DISCRETE LIGHT CAME ON AGAIN AND N2 DROPPED AS LOW AS 8% ABORTED START. DEFERRED PER ABX-80-00-2-1, PERFORMED MANUAL START. REMOVED AND REPLACED RIGHT ENGINE STARTER CONTROL VALVE ASSY. IAW ABX B767 AMM 80-11-02 SERVICEABLE UNIT INSTALLED OP CK OK. DI 50365 IS CLEARED PLACARD REMOVED NO MX DI PROCEDURE ACCOMPLISHED.
DURING TAXI STARTING RH ENGINE #1 INGNITOR LACKET TO START THE ENGINE AC RETURNED TO GATE AND MAINTENACE GROUNDED AC AND DEFERRED THE #1 IGNITION IAW MEL 74-00-1B. AC WAS RETURED TO SERVICE AND DEPARTED .
DURING TAXI RH ENG EGT OVERTEMP ON START EGT 562 AC RETURED TO GATE AND GROUNDED BY MAINTENANCE PERFORMED FIM 71-08 FAULT TREE 816 SECOND ENGINE START ATTEMPT CARRIED OUT AND WITHIN LIMITS. NO IMMEDIATE MTC ACTION REQUIRED. AUGH #2024-0020 MAINTENANCE REURNED AC TO SERVICE AC DEPARTED .
DURING TAXI FWD CABIN TEMP EICAS PLUS FWD CABIN INOP LIGHT ,A/C RETURNED TO GATE AND MAINTENANCE GROUNDED A/C.DEFERRED SYSTEM FOR DEPARTURE IAW MEL ABX-21-61-1-2 TROUBLE SHOT AT NEXT BASE AND REMOVED AND REPLACED FWD CABIN TRIM AIR MODULATING VALVE IAW B AMM21-61-07,AND REMOVED AND REPLACED TEMP CONTROL PANEL IAW B AMM 21-51-13 THIS CLEARES DMI 48261
LEFT ENGINE MACH PROBE DISCRETE / LT ENGINE EEC PROBE DISCRETE & LT ENGINE ANOLOG N2 EICAS MESSAGE AC RETUREN TO GATE & MAINT GROUNDED ACFT. DEFERRED IAW MEL 73-21-1-1A. FOR DEPARTURE .CONDUCTED TS PER FIM 71-01 FT 804. LT ENG P2 LEAK & LABEL 353 BIT 24 DISPLAYED. CHECKED SENSE LINES TO LT ENG PT2 PROBE. UNION LOOSE. TIGHTENED UNION. RANG OUT PROBE HEAT FOR PT2 WIRING, NO FINDINGS. SWAPPED LT & RT EEC DISCRETE CARDS PER AMM 73-21-12 THEN RAN BOTH ENGINES. FAULTS DID NOT FOLLOW TO RT ENG. NEW FAULT, LENG EEC PROBE HEAT DISPLAYED DURING EEC BIT, FIM 71-01 FT 804. RETURNED LT & RT EEC DISCRETE CARDS TO ORIGINAL POSITIONS. DURING LT ENG RUNS, N2 INDICATION NOT ACTIVE DURING START UNTIL 15% N2. ALL ITEMS SUSPECT TO FAULTY LT ENG N2 TACHOMETER REF SSM 77-00-01, 73-21-05. DI REMAINS OPEN. SYS REACTIVATED PER MEL 73-21-1-1A. AC VERIFIED NO ETOPS. R & R LT N2 TACH GENERATOR IAW AMM 77-12-02. ACCOMP ENG RUN LT EEC MESSAGE STALL PRESENT. BIT EEC MONITOR, LT ENG P2 LEAK & LABLE 353 BIT 24 STILL PRESENT. NO EICAS INDICATION OF EPR. FURTHER TROUBLESHOOTING REQUIRED. DI REMAINS OPEN. FOUND PREVIOUSLY INSTALLED N2 TACH XMITER BAD FROM STOCK REINSTALLED ORIGINAL N2 TACH XMITER. ALSO REPLACED L ENG CURRENT SENSE MACH PROBE 1 K751. SYSTEM CHECKS GOOD PER 77-12-00 MEL AND PLACARD REMOVED NO MX PROCEDURES APPLIED. 38069-95/1.
RT ENGINE HOT START DURING PUSH BACK MAX EGT 539. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED HOT START INSPECTIN PER B767 FIM 71-08 FT 816 PARA F. NO DEFECTS NOTED. OPS CHECKED GOOD. STABLE EGT WAS 394 DEGREES CELSIUS. PEAK EGT WAS 415 DEGREES CELSIUS. AIRCRAFT RETURNED TO SERVICE.
AFTER PUSH BACK & PRIOR TO TAXI C HYD PRIM ONE ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE SWAPPED C1 & C2 ELCU IAW AMM 29-11-14 C1 PUMP OPS CHK GOOD. C2 HYDRAULIC PUMP DEFERRED IAW MEL 29-11-2. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.
R ENGINE EGT 541, ABORTED ENGINE START FOLLOWED BY QRH. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RAN ENGINE IAW FIM 71-08 FT 816 PARAGRAPH F. OPS CHECK GOOD. STABLE EGT WAS 408. AIRCRAFT RETURNED TO SERVICE
N1'S FLUCTUATING AT IDLE BOTH ENGINES 23.3-26.5 ACCOMPANIED BY INTERMITTENT VIBRATION IN COCKPIT THAT DOES NOT APPEAR ON VIBRATION GAUGES. ALL OTHER EICAS GAUGES WITHIN LIMITS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LH N1 TACH. TRANSMITTER IAW B767 AMM 77-12-01. ACCOMPLISHED N2 INDICATION OPS CHECK ON BOTH ENGINES IAW B767 AMM 77-12-00 OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
ON CLIMB: RIGHT ENGINE EPR AND N1, EGT FLUCTUATING. ON LEVEL OFF THE FLUCTUATIONS STOPPED AIRCRAFT LANDED AT CVG WITHOUT FURTHER INCIDENCE. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE REPLACED RIGHT ENGINE PT2/TT2 PROBE PER B767 AMM 73-21-04. REPLACED PT2/TT2 PROBE PLUG D78 PER BOEING SWPM 20-61-11. AIRCRAFT RETURNED TO SERVICE.
R ENG UNCONTROLABLE THRUST (EPR) ON CLIMB.AIRCRAFT LANDED AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RT. EPR PER MEL 77-11-1-1, PLACARD INSTALLED. MX PROCEDURES C/W. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI N1 FLUCUATES BETWEEN 24.4-26.7 BOTH ENGINES AT IDLE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RAN ENGINES TO T/O PWR IAW B767 AMM 71-00-00 N 1 FLUCTUATIONS WITHIN LIMITS WITH EEC'S INOP NO SURGE NOTED. AIRCRAFT RETURNED TO SERVICE.
AFTER ENGINE START WE GOT AN FLT DECK TEMP EICAS RAN THROGH ABNORMAL AND COULD NOT CONTROL HEAT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED & REPLACED ZONE TRIM AIR VALVE (V!) IAW AMM 21-61-07 AND ZONE TEMP CONTROLLER IAW AMM 21-61-03. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED & REPLACED ZONE TRIM AIR VALVE (V!) IAW AMM 21-61-07. AIRCRAFT RETURNED TO SERVICE.
DURING C CHECK FOUND DENT AT FWD CARGO DOOR CUTOUT EDGE OF EXTERNAL FUSELAGE SKIN P/N 143T3520 AS SHOWN IN FIGURE 1. 767-200 SRM 53-00-15 HAS NO REPAIR FOR THIS AREA. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED.REFERENCE ABX -REA-5335-64901-00
DURING C CHECK FOUND WEB STRINGER L-16 CORRODED AND LOCATED AT STA 314.3. 767-200 SRM 57-00-03 DENIES MAINTENANCE TO REPAIR IT AT THIS LOCATION DUE TO THIS REPAIR CANNOT BE COMBINED WITH OR BE INSTALLED WITHIN 10 INCHES (254 MM) OF SKIN AND/OR STRINGER REPAIRS. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED.REFERENCE ABX-REA-5720-64907-00
DURING C CHECK FOUND KEEL BEAM WEB P/N 145T8612 HAS PROTRUDING DENT WITH CRACK AT STA 1045 AND BL 0. 767-200 SRM 53-50-12 ALLOWABLE DAMAGE HAS A REPAIR FOR .250â HOLE, BUT THE CRACK FOUND IS .3â OF LENGTH EXCEEDING LIMITS. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED WITH REPAIR PROPOSAL, AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. REFERENCE ABX-REA-5720-64907-00
DURING C CHECK AMES TAMPA REPORTED CORROSION ON THE LEFT WING LOWER SKIN PANEL NO. 4 TOP SURFACE AT WING STATION 314.4 AND STRINGER 16L. CORROSION WAS ALSO NOTED AT TOP SURFACE OF TANK ACCESS PANEL FLANGE. THE DAMAGE WAS REMOVED IAW 767-200 SRM 51-10-02 AND UT INSPECTION WAS PERFORMED TO DETERMINE THE REMAINING THICKNESS, AND FOUND TO BE OUT OFF LIMITS IAW 767-200 SRM 57-20-01. BOEING WAS CONTACTED VIA SR#4-5742615444, AND PERMANENT REPAIR INSTRUCTIONS WERE PROVIDED. REPAIRED PER ABX-REA-5725-64905-01. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY AN FAA AUDIT OF THE VENDOR
L1 WINDOW HEAT EICAS MESSAGE. AIRCRAFT DIVERTED TO CVG AND GROUNDED BY MAINTENANCE. MAINTENANCE C/W FIM 30-41 FT 803 NO DEFECTS NOTED PERFORMED RESISTANCE CHECK ON L1 WINDOW. NO DEFECTS FOUND. RANG OUT WIRING FROM L1 WINDOW TO WHCU. IAW FIM 30-41- FT 801. MAINTENANCE REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-01. AIRCRAFT RETURNED TO SERVICE.
CREW ABORTED TAKEOFF AND REPORTED NO STEERING REACTION TO LEFT RUDDER PEDAL INPUTS. TILLER WORKS NORMAL BUT IS SLUGGISH. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED FIM 32-11 FT 809 AND 811 NO DEFECTS NOTED. FOUND NOSE GEAR COLLAR VERY DRY, LUBRICATED IAW B767 AMM 12-21-13. PERFOMRED RUN UP AND TAXI IAW B767-10A, RUDDER PEDAL STERRING OPS CHECKS NORMAL AND TILLER SHOWED NO SLUGGISH MOVEMENT. AIRCRAFT RETURNED TO SERVICE.
R HYD QTY INDICATES RF DURING TAXI. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE SERVICED RH HYDRAULIC SYSTEM IAW B767 AMM 12-12-01. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE
AFTER PUSH LH GENERATOR DISCONNECTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET LEFT HAND GENERATOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
ON TAXI OUT THE FWD EQIP VAL EICAS MSG CAME ON, AFTER GOING TO STANDBY THE MSG REMAINED ON. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CLEANED CANNON PLUG OF INTERCON VLVE IAW SWPM 20-60-1AND AMM 21-58-01. MSG CLEAR PER FIM SUPPLEMENT 21-58-00. PERFORMED ENG RUN AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING RIGHT ENGINE START - WHEN TO GND, RIGHT ENGINE SHOWED EGT EXCEEDANCE. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE CLEARED MX MESSAGES ON EICAS BIT EEC MONITOR, NO FAULTS NOTED. ACCOMPLISHED MES OF #2 ENGINE IAW 71-00-00, ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE.
DURING PUSH BACK LOAD NOISE COMING FROM OVER HEAD SPEAKER. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT , OPS CHECK AND TESTED SYSTEM OPS CHECK GOOD IAW AMM 23-51-00.AIRCRAFT RETURNED TO SERVICE.
AILERON LOCKOUT EICAS MSG AFTER PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT IAW MEL 27-11-2. AICRAFT RETURNRD TO SERVICE.
DURING TAXI AILERON LOCK OUT MESSAGE AND SELECTED FLAPS 5 AND TE DISAGREE EICAS AND FLAPS DID NOT EXTEND PAST FLAPS 5. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF AILERON LOCKOUT SYSTEM IAW B767 AMM 27-11-44. OPS CHECK GOOD, MESSAGE REMAINED CLEARED. RESET FSEU, NO FIX PERFORMED BITE OF FSEU. NO DEFECTS NOTED. INSPECTED FLAPS BYPASS VALVE. FOUND STUCK IN BYPASS CLEANED CANNON PLUG IAW B767 20-30-02 SOPM. LUBRICATED TE FLAP BYPASS VALVE AND ADJUSTED TILL SMOOTH. OPS CHECK OF FLAPS GOOD. FOR 2 FULL CYCLES IAW B767 AMM 27-11-44. NO FAULTS ON FSEU IAW FIM 27-51. AIRCRAFT RETURNED TO SERVICE.
AILERON LOCKOUT LIGHT AND EICAS MSG ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED FIM 27-11 FAULT TREE 804 AND NO DISCREPANCIES NOTED AT THIS TIME PER 27-11-44. DMI 29728 CLEARED. PLACARD REMOVED. OUTBOARD AILERON LOCK OUT MECHANISM OPS CHECK NORMAL PER AMM 27-11-44. AIRCRAFT RETURNED TO SERVICE.
LEFT FWD BOOST PUMP INOP AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED LEFT FWD FUEL BOOST PUMP PER MEL 28-22-1. AIRCRAFT RETURNED TO SERVICE.
EICAS: FWD EQPT VAL. MESSAGE ILLUMINATED AFTER DEICE OPERATIONS, AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED SYSTEM TEST IAW AMM 21-58. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.
EICAS MSG "R ENG EEC" DURING CLMB. CREW DECIDE TO PERFORM AN AIR TURNBACK, AIRCRAFT LANDED UNEVENTFULLY. AIRCRAFT GROUNDED BY MAINTENANCE.BITE SHOWN R-J2 UNPLUD'D. INSPECT EEC J2 PLUG, D4224P, D4246J. IT WAS TIGHTENED & NO DEFECTS NOTED. REMOVED AND REPLACED M591 AND R EEC, EEC GROUND TESTS GOOD IAW B767MM 73-21-04 AND WITH ENGINE RUN, NO DEFECTS NOTED.
TWO HUNG STARTS ON LEFT ENGINE, AIRCRAFT BACK TO BLOCK. MAINTENANCE BOARDED AIRCRAFT AND GROUNDED AIRCRAFT. MAINTENANCE OBSERVED CREW START PROCEDURE . START WAS SUCCESSFUL AND AIRCRAFT WAS RELEASED FOR FLIGHT
EMERGENCY ESCAPE DEVICE DROPPED AFTER LANDING. REF L/P 1260506 REF DMI# 147887(<P>TRANSFER TO DMI# 147887 PER MEL25-61-01-01 CAT C. DUE DATE 11JUN21. BA 1445Z. INSTALLED DESCENT DEVICE IN #2 POSITION&NBSP; IAW AMM 25-61-03. NO DEFECTS NOTED . THIS CLEARS DMI# 147887. MCC NOTIFIED PLACARDS REMOVED&NBSP;&NBSP;</P>)
AFTER BLOCK OUT AND EACH ENGINE START EICAS "TAT PROBE" AND OVERHEAD LIGHT CAME ON FOR ABOUT A MINUTE . 3-4 TIMES AND SUBSEQUENTLY STAYED OFF PRIOR TO TAKE OFF.(<P>PERFORMED FIM 30-33 FT 804 AND FOUND SYS O. 1 AIR/GROUND RELAY BAD (K514) IAW SWPM 20-81-13 PERFORMED OPS CHECK IAW AMM 30-30-00 OF TAT SYSTEM. NO DEFECTS NOTED AT THIS TIME.</P>)
FAN CASE DAMAGED AND BLADE ON LH ENGINE (REMOVED AND REPLACED #1 ENG 2EA ACOUSTIC PANELS PER AMM 72-33-05 & REPLACED BLADES 39 & 19 PER AMM 72-31-02. SEE LOG PAGE 1329001 FOR OPS CHECK. TEST NO.11 VIBRATION SURVEY ACCOMPLISHED PER AMM 71-00-00. NIL DEFECTS NOTED. MAX VIB 6. AIRCRAFT OK FOR SERVICE.)
AFT CARGO DOOR LOWER INNER SKIN WEB HAS CORROSION THROUGHOUT. UPON EVALUATION OF THE AFT CARGO DOOR LOWER SKIN, FOUND TO BE 100% MAT. AND OUT OF LIMITS, IAW B767 SRM 52-30-01-1A-1. REMOVED AND REPLACED AFT CARGO DOOR LOWER INNER SKIN, IAW BOEING DWG 140T2640, B767 SRM 51-40-02-0G-0.
AFT CARGO DOOR AT CARGO SERVICE LIGHT SHROUD LOWER FRAME CORRODED. UPON EVALUATION OF AFT CARGO DOOR TEE CHORD, FOUND OUT OF LIMITS, IAW B767 SRM52-30-02-1A-1. REMOVED AND REPLACED TEE CHORD, IAW B767 BOEING DWG 140T2606, B767 SRM 51-40-02-0G-0.
AFT CARGO DOOR INNER FRAME HAS 2 SQ IN EXFOLIATED CORROSION AT CARGO SERVICE LIGHT SHROUD. UPON EVALUATION OF INNER TEE-CHORD AT AFT CARGO DOOR LIGHT SHROUD, FOUND OUT OF LIMITS, IAW B767 SRM 52-30-02-1A-1. REMOVED AND REPLACED AFT CARGO DOOR INNER TEE-CHORD AT LIGHT SHROUD, IAW BOEING DWG 140T2606, B767 SRM 51-40-02-0G-0.
FWD CARGO PIT BENEATH FLOOR STA 485 STRINGER 33R HAS 3SQ IN OF CORROSION. UPON EVALUATION OF STR 33R AT STA 485, FOUND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR. 33R STA 485, IAW B767 SRM 53-00-03-2R-2.
RH ENG BOTTLE #2 DISCHARGE LIGHT AND ADVISORY MSG ON REMOVED, SERVICED AND REINSTALLED FIRE BOTTLE IAW AMM 26-21-03
RT ENG OIL QTY WENT TO 0 FOR 20 MINUTES. REMOVED AND REPLACED OIL QTY TRANSMITTER IAW AMM 79-31-01. OPS CHECKS GOOD BUT NO FIX, FURTHER TROUBLESHOOTING NEEDED. LP 1092409 - M3: REMOVED AND REPLACED TUBE ASSY #4 BRG SCAVENGE ON #2 ENG PER REQUEST IAW AMM 79-21-00. OFF PART (P/N: 5008098-01, S/N: NSN) LP 1092410 - M6: REMOVED AND REPLACED #4 OIL SCAVENGE LINE. PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00. NO FURTHER DEFECTS OR LEAKS NOTED AT THIS TIME. RT OIL LEVEL MAINTAINED AT AN ACCEPTABLE LEVEL WITH NO OIL CONSUMPTION.
LE FLAP DISAGREE. REF QRH, RETURNED TO DEPARTURE. OCCURRED ON RETRACTION FROM FLAP 5 TO FLAP 1. T/S IAW B767 FIM 27-81 FAULT TREE 808. NO CURRENT FAULTS FOUND. PERFORMED A BITE TEST ON THE PSEU FOUND "LVR NOT IN DENT" FAULT IN THE LAST FLIGHT LEG. PERFORMED LE BITE AND FLAP/SLAT CONTROL CABLES TENSION CHECK IAW AMM 27-51-00. TENSIONS FOUND TO BE WITHIN LIMITS. PERFORMED FLAP CONTROL LEVER LOAD TEST IAW AMM 27-51-00 735-233. LEVER LOAD TEST FOUND TO BE WITHIN LIMITS.
BULK CARGO RT FLOOR PNL HAS MULTIPLE REPAIRS, DENTS AND 1 PUNCTURE. (<P>FABRICATED NEW BULK CARGO FLOOR PNL RT IAW SRM 53-60-53. FLOOR PNL REMOVED AND WILL BE RE-INSTALLED ON TASK NR-00004.<BR /></P>)
#2 ENG STRUT FAIRING I/B SIDE PERMANENT REPAIR IS DELAMINATED ON INTERIOR SURFACE, VIEWED THRU ACCESS DOOR #447BL AREAS MARKED.(<P>REPAIRED #2 ENGINE STRUT FAIRING I/B SIDE, P.N. 313T3381-1 IAW SRM 51-70-10-2R-0.<BR /></P>)
KEEL BEAM AREA FWD MLG ACCESS PNL SUPPORT ANGLE CORRODED. (<P>UPON FURTHER EVALUATION, FOUND SUPPORT ANGLE WITH 100% MATERIAL LOSS IAW SRM 53-50-12. REMOVED AND REPLACED SUPPORT ANGLE ON KEEL BEAM AREA FWD MLG IAW SRM 51-40-02.<BR /></P>)
BULK CARGO COMP. LT FLOOR PNL HAS AREAS OF CORROSION ON UPPER SURFACE BS 1461-1540. (<P>REMOVED, FABRICATED, AND INSTALLED NEW BULK CARGO LT FLOOR PNL IAW SRM 53-60-53.<BR /></P>)
DURING HFEC INSPECTION, FOUND FLOOR POST TO FRAME CRACKED ON MIDDLE FASTENER, LOWER FASTENER AND UPPER O/B RADIUS ON AFT SIDE OF FLOOR POST STATION 1395 STR 33R. (<P>REMOVED AND REPLACED STA 1395 STR 33R CLIP IAW SRM 51-40-02 AND DWG 146T1516 REV C.<BR /></P>)
MAIN ENTRY DESCENT DEVICE (P/N: 379103D-29, S/N: 21244) IS NOT IN GOOD CONDITION.(<P>REMOVED AND REPLACED MAIN ENTRY DESCENT DEVICE IAW AMM 25-61-00.<BR DATA-MCE-BOGUS="1" /></P>)
EICAS, LEADING EDGE SLAT DISAGREE QRH FOLLOWED. EICAS WENT AWAY BEFORE PROCEDURE COMPLETE. NO YAW OR VIBRATION. REMOVED AND REPLACED FSEU IAW AMM 27-51-01. TEST GOOD PER AMM 27-51-01. FOUND SENSOR M549 OUT OF LIMITS, ADJUSTED RVDT IAW AMM 27-81-11. OK FOR SERVICE.
ONE INERTIAL REEL INOP. INSTALLED DESCENT DEVICE IAW AMM IAI 25-61-03. INSTALLATION CHECK GOOD.
EMERGENCY ESCAPE DEVICE DEPLOYED. MAINTENANCE PROCEDURES C/W SIX SERVICEABLE REMAIN CAT C EXPIRES 23JUL18.
HALF OF THE GALLEY EMERGENCY LIGHTS INOPERATIVE. SWAPPED THE BATTERY PACKS IAW AMM 33-51-07. OPS CHECKED GOOD.
CHAFING ON A DOUBLER JUST FWD OF PANEL 432AL ON THE NR 1 STRUT OTBD SIDE. COMPLIED WITH EA 180054, REV 1R.
A CRACK INDICATION NOTED DURING OPEN HOLE INSPECTION OF THE RT FAILSAFE STRAP. REPAIR THE FAILSAFE IAW S/B 767-53A0100, REV 3, FIG 3 & REINSTALLED IAW SRM 51-40-02.
A CRACK INDICATION NOTED DURING OPEN HOLE INSPECTION OF THE LT FAILSAFE. REPAIRED THE FAILSAFE IAW S/B 767-53A0100, REV 3 FIG 3 & REINSTALLED IAW SRM 51-10-00.
RIGHT INBD AFT PYLON AT PANEL 4470B WHERE SUPPORT ANGLE BRACKET ATTACHES TO WING, THE BRACKET IS CRACKED. REPAIRED IAW EA 180048, REV 1R.
MAIN CARGO DECK INTERIOR UNDER ONL 221K FLOORBEAM HAS MULTIPLE SIGNS OF CORROSION. REPAIRED IAW EA 180039.
MAIN CARGO INTERIOR RT SIDE BS 479 UNDER PBL 232G TAP SECTION BETWEEN SEAT TRACKS HAS CORROSION. REMOVED AND REPLACED THE DAMAGED SHEAR WEB IAW SRM 51-40-02.
NR 2 PYLON PANEL LANDING HAS A CRACKED. REPAIRED IAW EA 180055, REV 1R.
ENTRYWAY EMERGENGY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. OPS CHECKED GOOD IAW AMM 33-51-07-002-006, AND 33-51-07-402-010.
ENTRYWAY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. OPS CHECK GOOD IAW AMM 33-51-07-002-006 & 33-51-07-402-010.
L BLEED DUCT LEAK CAUTION MSG AND LEFT DUCT LEAK LIGHT DISPLAYED AT CRUISE POWER. RETURN TO SFO(<P>PER FIM 26-18-FT804. AT A/C ARRIVAL FOUND P61 PANEL LOOP SW SELECTED TO #1 POSITIONED TO LOOP #2 RAN ENG&NBSP; AT HIGH POWER WITH NO FAULTS. MDDR 86884 REMAINS OPEN.REF ITEM 3 - PER AMM 36-11-00-795-148 VISUALLY INSPECTED LH DUCT LEADING EDGE & #1 ENG STRUT FOR LEAKEAGE. NO DISCREPENCYS FOUND. OK FOR SERVICE</P>)
THE LEFT FWD WINDSHIELD OUTER PANE SHATTERED. REPLACED THE L1 WINDSHIELD IAW AMM 56-11-01.
DURING TAKE OFF ROLL, AN EICAS ALERT MESSAGE FOR BODY DUCT LEAK, FOLLOWED BY CABIN AUTO INOPERATIVE. PERFORMED REJECTED TAKEOFF PROCEDURES FOLLOWED BY QRH PROCEDURES AND RETURNED TO GATE. INSTALLED DUCT ASSY IN AFT CARGO AT VERTICAL DUCT CONNECTION TO ADP, ANGLE DUCT. LEAK CK GOOD EXTERNAL A/C PANEL REINSTALLED IAW AMM 36-11-01.
CABIN CARGO MAIN DECK FLOOR BOARD SKIN HAS SEVERE PUNCTURE DAMAGE AT BS 1220 - 1225, RBL 35. REPAIRED IAW SRM 53-00-50 REPAIR 6.
REJECTED T/O, CAPTAIN`S AIRSPEED INDICATOR ZERO-EFIS NORMAL, STDBY NORMAL. OK TO CONTINUE IAW DDPG 34-13-01-03, CAT-C, DMI: 70096 ASSIGNED DISPATCHER UP 03:59Z, DUE DATE 20, SEP 16.
NR 2 ROTARY ACTUATOR AND REACTION RING HAS CORROSION. REMOVED AND REPLACED THE NR 2 ROTARY ACTUATOR AND REACTION RING IAW AMM 27-51-22 AND SB 767-27A0229.
TWO EMERGENCY DEVICES BROKEN, EMERGENCY DECENT DEVICES REPLACED IAW AMM 25-61-03.
NR 7 ROTARY ACTUATOR AND REACTION RING IS CORRODED. REMOVED AND REPLACED THE ROTARY ACTUATOR AND REACTION RING IAW AMM 27-51-22 AND SB 767-27A0229 FIG 2.
NR 9 SLAT AFT SIDE OF UPPER EDGE CHAFED ALONG LENGTH OF SLAT. REPAIRED THE SLAT IAW SRM 51-70-16-22-0.
NDT OF STRUCTURE AT BS 859.5 HAS A 0.25" CRACK INDICATION ON THE TRASITION RADIUS, LT SIDE OF ACFT. COMPLETED REPAIR IAW SRM 51-10-02, 51-40-02, AMM 25-59-05, 12-21-13, AND 51-24-09, AND SB 767-53A0209 FIG 7.
RIGHT OUTBRD FLAP L/E HAS DELAMINATION ON INBD END. REPAIRED IAW SRM 51-70-17 PARA 4.C.
TWO EACH DESCENT DEVICES INOPERATIVE AT L1 DOOR. R & R TWO EACH EMER DESCENT DEVICES IAW AMM 25-61-03. THIS CLEARS MDDR 67065, PLACARD REMOVED.
LOW SPEED ABORT FOR RT ENG GEN DRIVE, CAUTION MSG COMPLIED WITH QRH. TRANSFERRED TO MEL 24-00-01-03 MDDR 65929 CAT B.
AFTER TAKEOFF AT 9,500 THE MAIN CARGO DOOR LIGHT ILLUMINATED. DID THE QRH & RETURNED TO DEPARTURE. DUPLICATED DEFECT BY PRESSURIZING ACFT. FOUND MAIN DOOR HOOK LATCH INDICATOR SWITCH OUT OF ADJUSTMENT. CORRECTED INDICATOR SWITCH ADJUSTMENT IAW MM 52-71-09. OPS CHECKED GOOD.
EO 6753A156 ISSUED FOR FUSELAGE SKIN REPAIR FOR DENTS AT 1439 BETWEEN STRINGER 34L & 39L. MULTIPLE MODIFICATIONS TO ORIGINAL STATED REPAIR REQUIRED, REPAIR AREA EXPANDED TO INCLUDE EXISTING REPAIR BETWEEN STATION 1470 - 1439 & STRINGER 34L - 35L & STRINGER 37L & 39L. SPLICE REPAIRS, STRAP REPAIR, STRINGER CLIP & SHEAR TIE REPLACEMENTS.
MAIN CARGO DOOR MSG ON AT 12000 FT, OUT AT 7000 FT & IN DESCENT. ACCOMPLISHED FIM 52-7 FT 809, VERIFIED SWITCH S9023 OUT OF ADJUSTMENT, ADJUSTED CARGO DOOR LOCK INDICATOR SWITCH S9023. ACCOMPLISHED MAIN CARGO WARNING SYS TEST IAW AMM 52-71-09. ACFT PRESSURIZED ON GND WITH APU SOURCE, AMM 21-31-00, MAIN CARGO DOOR WARNING LIGHT NOT DISPLAYED AT THIS TIME, CHECKED NORMAL, DID NOT DUPLICATE. MDDR REMAINS OPEN, FLIGHT CREW EVALUATION REQUIRED.
MASTER WARNING IN FLIGHT, MAIN CARGO DOOR, LIGHT ILLUMINATED ON CLIMB OUT, PASSING FL180. LIGHT EXTINGUISHED ON DESCENT PASSING 7000'. OPERATED & INSPECTED MAIN CARGO DOOR, NO DEFECTS AT THIS TIME, PRESSURIZED ACFT, ALL CHECKED GOOD. OK FOR CONTINUED SERVICE IAW AMM 52-71-00, 52-32-00 & 5-51-24.
LEFT AC BUSS OFF- COMPLIED WITH QRH AND RETURNED TO DEPARTURE. (R & R RELAY K863) (LEFT TRANSFER BUSS RELAY), AND "A" PHASE CIRCUIT BREAKER UNIT C313, BOTH OPS CHECKED GOOD, ENGINE RUN ALSO OPS CHECKED GOOD. FAULT CLEARED, IAW AMM 24-25-00, AND 24-51-11, 24-22-00).