N59053
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| United Air Lines | Operator | 2015-02-15 – 2015-02-15 | Operator named in NTSB report |
| UNITED AIRLINES INC | Operator | 2015-02-15 – 2015-02-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
49F EMERGENCY LIGHT IS HANGING BY WIRE, ITEM DEFERRED IAW MEL EMERGENCY LT AT SEAT 49F INOP. ITEM DEFERRED TOMC APPROVED INSTALL 49F EMERGENCY LIGHT SEAT ASSEMBLY.OPS CK GOOD.MEL REMOVED.OK TO CONTINUE.
PRIXIMITY LIGHT POSITION 34F HAS NO LENS. REMOVED AND REPLACED ESCAPE PATH LIGHT SEAT MOUNTED LIGHT ASSEMBLY REF. AMM TASK 33-51-10-962-104 REV-. GOOD FOR SERVICE.
DURING SAFA INSPECTION CEILING EMER LIGHT AT ROW 7A INOP CEILING EMER LIGHT AT ROW 7A INOP IAW MEL 3351A INTERIOR EMERGENCY LIGHT SYSTEM HAS INOPERATIVE LIGHT CEILING EMER LIGHT AT ROW 7A INOP IAW MEL 3351A RELAMPED LIGHT NO HELP NEEDS FURTHER T/S. REMOVED AMD REPLACED EMERGANCY EXIT LIGHT BULB AT ROW 7A IAW AMM REF. 33-51-01/201. USED ONE BULB ALL OPS CHECK PASSED SAT.
IT WILL BE NECESSARY TO REPAIR THE OTBD LT AILERON. COMPLETED REPAIR IAW SRM 57-60-02-2R-1, & SRM 51-70-05-0G-0.
ON CLIMBOUT AND CRUISE INTERMITTANT ANTISKID EICAS. AS PER FLIGHT CREW, MESSAGE APPEARED ON CLIMB OUT THEN DISAPPERED UNTIL DESCENT AROUND FL300 AROUND 300 KTS THEN STAYED ON REMAINING OF THE FLIGHT. FOUND ANTISKID/AUTOBRAKE DISPLAYED MAINTENANCE MESSAGE. PERFORMED FIM TASK 32-42 FAULT TREE 823, BITE TEST PASSED AND FAULT NO LONGER ACTIVE.
C HYD QTY EICAS MSG DURING CRUISE FLIGHT, QTY WAS SHOWING .48 DURING RECOVERY OF AIRCRAFT. NOTICED LARGE AREA OF HYD LEAKAGE UNDER LT WING. FURTHER EVALUATION REQUIRED. AIRCRAFT REPOSITIONED AT THE HANGAR WITH 28% ON CENTER HYD SYSTEM. AFTER INSPECTION OF LT WING FOR LEAKS, FOUND NR 4 SPOILER ACTUATOR LEAKING FROM FILTER CAP DUE TO DAMAGED O-RING. REFER TO IPC 27-61-02-51 ( ITEM 425). REMOVED AND REPLACED FILTER CAP O-RING IAW AMM 27-61-02. OPS AND LEAK CHECKED GOOD, NO DEFECT NOTED. OK TO CONTINUE.
LEFT GEN DRIVE EICAS C THE LT GEN DRIVE HAS LOW OIL PRESSURE OR HIGH OIL TEMPER ATURE WHILE THE ENGINE IS IN OPERATION. LT ENG. C-DUCT OPENING AS AMM 78-31-00 THE FOLLOWING DAMAG ES HAS BEEN OBSERVED AS X GENERAL OVERVIEW: IDG ASSY ALL IDG OI L HOSES APPEARING STRETCHED ALL IDG CONNECTORS APPEARING SEPARATED FROM ITS WIRING IDG GONE PART LOOKS LIKE TOUCHING METAL PIPES NEXT TO AIR STARTER AND ONE IS DAMAGED.AFT FIREWALL STRUCK BY IDG LOOKS LIKE DEEPLY BENT AND TOUCHING PNEUMATIC DUCT BEHIND IT. LT ENGINE IDG REPLACED AS PER AMM 24-11-01-004-001-002 AND 24-11-01-404-012-002. POST INSTALLATION OP CHECKS AND LEAK CHECKS TO BE CARRIED OUT. IDT INSPECTION RAISED FOR CONNECTION OF LT ENGINE IDG TERMINAL FEEDER CABLES INSTALLATION. LH ENGINE IDG TERMINAL FEEDER PHASE CABLES INSTALLED AS PER AMM 24-11-01-404-012-002, STEP 3. I. (5). LT ENGINE IDG OP-CHECK AND LEAK CHECK CARRIED OUT AS PER AMM 24-11-00-715-004-001. ALL OPERATIONS AND INDICATIONS ARE CORRECT AT TIME OF TEST WITH NO LEAKS APPARENT.
DOOR 2R SLIDE COVER NOT SEATED FLUSH WITH DOOR. DOOR ARMS AND IN DICATES LOCKED INSTALLED BUSTLE REF AMM SUBTASK 25-66-01-414-066. ITEM OKAY
INTERMITTENT RIGHT ENGINE FUEL FILTER BYPASS. REMOVED, INSPECTED AND REPLACED RIGHT ENGINE FUEL FILTER REF AMM 73-11-02. INSPECTION OF FILTER SHOWED CLEAN NO DEBRIS NOTED. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REF AMM 73-34-01. LEAK CHECK REQUIRED FOR INSTALL ON BOTH SWITCH, FUEL PR OFF 64-7334-9-9001 5693 ON 64-7334-9-9001 5206 COMPONETS. PERFORMED ENGINE IDLE RUN AS A PRECAUTION PER POWERPLANT REFERENCE TABLE 71-00-00, NO LEAKS NOTED MESSAGE DID NOT REAPPEAR, OKAY FOR SERVICE
CONTROL EICAS MESSAGE (01=L, 02=R) GEN OFF DISPLAYED. GEN OFF LI GHT ON. GENERATOR RESET DID NOT CORRECT CONDITION 02 CRUISING AT FL320 GOT EICAS MESS RT GEN OFF RT GEN FILED OFF LIGHT IS ON ALSO. SFOMM PLZ CHK BPCU FOR ANY FAULTS PER FIM... BPCU BITE SHOWS ON RT CHANNEL: 24-35002. PICS INCL. REF MSG 24-35002, AND R GEN OFF EICAS MSG, R IDG SWITCH DRIVE LIGHT ILLUMINATED, PER FIM 24-20 TASK 844 WILL REQUIRE RIGHT IDG REPLACEMENT. REPLACED #2 IDG, TORQUED PHASE LEADS REF MM 24-11-01-404-012-002, ACPD IDT OF #2 ENG IDG FEEDER CABLE INSTALLATION. ACOD R IDG OPS CHK REF MM 24-11-00-715-016-001 AND MM 24-11-01-404-012-002, OPS CHK AND LEAK CHK GOOD, VOLTS AND FREQS WITHIN LIMITS, ACPD BPCU BITE CHK REF MM 24-11-00-745-001-001, NO FAULTS
FOUND DOOR 2R EMERGENCY EXTERIOR LIGHT INOP. RE-LAMPED OPS CHECK GOOD REF AMM 33-51-06
EXTERIOR LIGHT OPERATIONAL CHECK {B767-33-3-0008} - DOOR 3R EXTERIOR EMERGENCY LIGHT INOP. RELAMP REQUIRED. OPS CHECK FOR DOOR 3R EMERGENCY LIGHT IS GOOD. FOUND DOOR 4R EMERGENCY LIGHT IS OUT. RELAMPED DOOR 4R EMERGENCY LIGHT REF AMM 33-51-06. TEST IS GOOD.PARTS USED: 99-3351-3-0014, QTY :1
AIRCRAFT AIR RETURN FOR FIRE BELL ON CONTINUOUSLY WITH NO OTHER LIGHTS OR FAULTS. CREW UNABLE TO SILENCE. AUPON ARRIVAL AC. PULLED CB J34 WARRNING ELEX CB WARRNING SOUND STOP RESET CB AND BELL REMAIN OFF . TS PER SSM 31-51-07-11 SUSPECT FAILUER OF M1000 BELL SHIME CONTROL CARD . REMOVED AND REPLACED M1000 BELL/CHIME MODULE IAW TASK 31-51-04-004-133 & TASK 31-51-04-404-014. PERFORMED BELL/CHIME AURAL WARNING CARD MODULE TEST IAW TASK 31-51-04-724-154 STEP 4. G. OP CHECK GOOD. REFER TO LP 3663439 FOR FINAL OP CHECK. FIRE WARNING BELL AT TAKE OFF WITH NO OTHER INDICATIONS NOTED. AIRCRAFT RETURNED TO FIELD. FLIGHT 2143 CONTINUED ON ANOTHER AIRCRAFT. PER SUPERVISOR THAT DEBRIEFED CREW: THE INBOUND CAPTAIN THAT EXPERIENCED THIS EVENT STATED: BELL STARTED SOUNDING JUST BEFORE ROTAION.
30D SEAT COACH POSITION EMERGENCY LIGHTS FLOOR PROXIMITY DO NOT WORK. R/R FLOOR PROXIMITY LIGHT 30D SEAT POSITION. REF AMM 33-51-10. OPERATIONAL TEST. GOOD FOR SERVICE.PARTS USED: 76-2525-3-0269, QTY :1
GEAR DOORS EICAS OPERATED GEAR DOORS MANUALLY WITH BELLY SWITCHES AND DOORS EXTEND AND RETRACT AS REQUIRED. PERFORMED FIM TASK 32-61 FAULT TREE 827 UPON ARRIVAL ON A/C FOUND NO MSG. PERFORMED PSEU BITE PROCEDURE AND FOUND NO FAULT MSGS. PERFORMED MAIN GEAR EXTENSION AND RETRACTION OPS CHECK REF AMM 32-32-00-705-001-001. RH DOOR WOULD NOT GO UP. RESET SAFETY VALVE AND ALL SUBSEQUENT EXTENSION AND RETRACTIONS WORKED PROPERLY. 5 EXTENSIOIN AND RETRACTIONS PERFORMED. REMOVED AND REPLACED MAIN LANDING GEAR DOOR SAFETY VALVE PRECAUTIONARY REF AMM 32-35-10-004-001-001. PERFORMED 6 MORE EXTENSION AND RETRACTIONS OPS CHECK GOOD ABOVE MAINTENANCE PERFORMED.
EMERGENCY LIGHTS DO NOT WORK FROM SEAT ROW 30 TO SEAT ROW 35 FOUND PLUG LOOSE UNDER SEAT 36FED , RE-TIGHT PLUG IN REF WDM 33-51-19-902 AND PERFORMED OPERATIONAL TEST IN REF AM. TASK 33-51-00-715-001 ITEM OK FOR FLIGHT .
PDA 2 FOUND DOOR NACELLE ASSY. ON E2 SIDE ALSO MISSING. REF. L/P 9904036 ON LOCATION 436/446. REQUESTING CDL DEFERRAL PER CDL 54C. DEFERRED PER CDL 54C. COMPLIED WITH DDP. INSTALLED PLACARD.
L ENG BLEED OFF EICAS W/ ASSOC L ENG BLEED LIGHT OCCURED MULTIP LE TIMES IN FLT. THEY NOTICED THIS FLUCTUATION AT LEAST 6 TIMES. UPON DEBRIEFING FLT CREW MAINT WAS NOTIFIED THAT THE LEFT BLEED ALSO THE LEFT PACK WOULD INDICATE OFF DUE TO NOT HAVING ENOUGH INDICATION WAS FLUCTUATING CONSTANTLY AFTER TAKEOFF AND AFTER PSI FROM THE LEFT BLEED. EVENTUALLY THEY SHUT OFF THE LEFT BLEED REDUCTION IN ENGINE POWER. FLT CREW NOTICED THAT THE LEFT BLEED VALVE ALONG WITH THE LEFT PACK. RIGHT BLEED MAINTAINED PROPER WOULD GO DOWN TO AS LOW AS 10 PSI AND THEN INCREASE BACK UP. PRESSURE, NO FLUCTUATIONS NOTED. VALVES ARE FUNCTIONING AND OR A HEALTH CHECK. DID BITE TEST ASCTU AND RECEIVED MESSAGE 36-10720:L PRV FAIL CL. ASCTU BITE IAW FIM 36-00 FAULT TREE 801. FAULT 36-10720 PRV RAN L ENG, OPS CHK FAILED, NO DUCT PRESS. NEED FURTHER T/S PERFORMED MANUAL CHECK OF HPSOV, PRSOV AND PRV. ALL VALVES MOVE PERFORMED BITE TEST OF ASCTU AND FOUND NO MSGS RELATED TO ANY OF FOLLOWED FIM 36-10 TASK 804. PRVC RECENTLY R+R. SUSPECT FAULTY L FAILED DISPLAYED. REMOVED AND REPLACE PRV IAW AMM 36-11-18 ON TO SMOOTHLY WITHOUT ANY BINDING. ALSO PERFORMED LEAK CHECK OF PRV THE VALVES. PERFORMED HPSOV ACTUATOR LEAKAGE (THUMB) TEST. TEST PRV. STEP F IN THE INSTALLATION.PARTS USED: 64-3611-9-0007,QTY PRESSURIZATION UPSTREAM OF THE PRSOV AS PER PASSED. SUGGEST PERFORMING AN ENGINE IDLE RUN WHILE MONITORING :1 36-11-09-782-001-003. NO LEAKS NOTED. ATA36 IN THE MX PGS TO VERIFY MOVEMENT OF HPSOV AS THE ISOLATION.
L BLEED PRV ON ICAS AHM: ADDING CHIME DATA PERFORMED FIM TASK 36-10 TASK 804. GROUND TEST PASSES. PERFORMED ASCTU BITE TEST; FOUND FAULT CODE 86-10720 AS PER FIM 36-00 FAULT TREE 801 & 36-00-00/301. THAN AS PER FAULT CODE AS PER FIM 36-10 TASK 804; R/R PRV CONTROLLER AS PER AMM REF 36-11-19/401. OPS CHECK GOOD. NO LEAKS NOTED NOR FAULTS AT THIS ADD EMP:U379161 TIME.PARTS USED: 00-0593-3-1982,QTY :1 40-0596-3-5426,QTY :1 64-7611-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1376678 SN OFF 0091 CONTROLLER, PRV OFF 64-7611-9-0002 0091 ON 64-7611-9-0002 0049
PDA 2 FOUND PANEL 436AR ON #1 ENGINE INBOARD PYLON MISSING ON AIRCRAFT ARRIVAL INSTALLED SERVICEABLE PART REMOVED FROM AC 0061, PANEL 436AR REFERENCE AMM 54-53-01-404-007.
CAPT REPORTED LANDING GEAR DISAGREE MSG WHEN RETRACTING GEAR. PLANE ARRIVED IN EWR WITH LEFT GEAR DOOR DOWN. T/S PER SSM 32-30-01-101, VERIFIED THAT SYSTEM OPERATES ON GROUN D WITHOUT ANY NOTED ELETRICAL DEFECTS. OPENED AND CLOSED MLG DOO RS SEVERAL TIMES WITHOUT ANY C/B''S TRIPPING. SUSPECT PREVIOUSLY INSTALLED L MLG SAFETY VALVE BAD FROM STOCK. SAFETY VALVE AND PACKING IN FWD GALLEY. REMOVED AND REPLACED V649 LH MLG SAFETY VALVE REF AMM 32-35-10 OPS CHECKED MLG DOORS NO DEFECTS NOTED AT THIS TIME
FOUND TAIL SKID STRUT YELLOW INDICATOR EXTENDED DURING CONDITIONAL INSPECTIONS PICTURE UPLOAD DURING CLOSER INSPECTIN ORANGE AND YELLOW INDICATOR HOUSING FELL ACTUATOR CRUSHABLE CATRIDGE REMOVED IN REFERENCE WITH BOEING AMM OUT OF TAIL SKID STRUT ABSORBER. REQUIRES REPLACEMENT PICS 32-71-08. ADDED. INSTALLED TAIL SKID CARTIDGE IN REF AMM 32-71-08. PARTS USED: 64-3271-3-0009,QTY :1
LOST DATALINK. AFTER CMU AC L RESET PER FOM 5.50.5, LOST ACARS PRINTER AND UNABLE TO MAKE SATCOM CALLS. ABLE TO RECEIVE SATCOM CALLS ONLY. CB RESETS PER FLIGHT MANUAL FAILED TO REGAIN LOST COMM SYSTEMS. SBB FAILED LIGHT ILLUMINATED ON MMUII PANEL, REMOVED AND REPLACED SBU TRANSCEIVER REF AMM 23-15-01-000-801-C1, DURING OP CHECK, CALL WAS UNABLE TO COMPLETE. AN AUTOMATED MESSAGE WOULD PLAY "CALL HAS BEEN REGISTERED AS SPAM". UNABLE TO COMPLETE OP TRANSCEIVER, AV OFF 64-2315-9-0002 6916 ON 64-2315-9-0002 0222 TRANSCEIVER, AV OFF 64-2315-9-0002 6916 ON 0000 CHECK REQUIRES SERVICE PROVIDER REGISTRATION. PARTS USED: 64-2315-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1501907 SN OFF 6916 PERFORMED AMM FANS (CPDLC/ADS-C) OPS TEST AND PASSED. PRINTER WORKED PROPERLY. ABLE TO MAKE A CALL FROM THE PLANE TO MY PHONE WITH NO ISSUES. AFTER TALKING TO UNITED ENGINEER THEY FEEL THE ISSUE IS IN THE UNITED NETWORK AND NOT WITH THE AIRCRAFT. TRIED CALLING ON ANOTHER 767 AND FAILED CALLING WITH THE PRELOADED NUMBERS. REF AMM23-22-00-710-801-C1.
DURING CLIMBOUT FWD CARGO DOOR FWD ACCESS DOOR R CTR PERFORMED PSEU BITE TEST AND FOUND CODE 006 AND 010. SEE FOR INFO, SEE ATTACHED PICTURE, MESSAGE TAKEN BY FLIGHT CREW IN ATTACHED PICTURES. FLIGHT. BITE CODES 006 AND 010 INDICATED FAILED LEFT CARD WITH CARD USED: 76-3260-9-0005,QTY :1 LIGHT. VERIFIED S214 AND S200 PROX. SENSORS AND FOUND TO BE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1605634 SN OFF 0634 OK.REMOVED AND REPLACED M162 PROXIMITY SWITCH ELECTRONICS UNIT. FER AMM 32-09-04 AND SSM 52-70-01. GROUND OPS CHECK OK. PARTS ADD FAULT:52900644, 52900144 UNIT, ASSY, PRO OFF 76-3260-9-0005 0634 ON 76-3260-9-0005 0996
LAV 3F-1LC AND 3F-1RC EMERGENCY LIGHT SUDDENLY LIGHT UP REFER HAECO NON-ROUTINE NO.9460067 - ORIGINATED BY EMP V903178 SPEC NO .MULT-33-3-0004 PERFORMED BY EMP V903178 REPLACED M7236 EMERGENCY LT POWER SUPPL Y CHARGER AND M7236 POWER SUPPLY CHARGER TESTED,THE RESULT FOUND ''SATIS'' IAW AMM 33-51-07-002-014-001 REV 139, AMM 33-51-07-402-0 18-001 REV 139,IDT BY EMP V903214
EY SEAT ROW 33F,37F,39F,44F,46F,47F,48F,49F EMERGENCY LIGHT FOUN D CRACKED REF HAECO NON-ROUTINE NO.9456048. REPLACED EY SEAT ROW 33F,37F,39F,44F,46 F,47F,48F,49F EMERGENCY LIGHT AND LAMPS TESTED,THE RESULT FOUND SATIS IAW AMM 33-51-10-962-104 REV 139.
AFT ZONE EY SEAT FRONT ROW L/H SIDE EMERGENCY LIGHT FOUND DIM,PO S:38D REF HAECO NON-ROUTINE NO.9454713 - SPEC NO.B767-33-3-7000. REPLACED AFT ZONE EY SEAT POS:38D EMERG ENCY LIGHT AND LAMPS TESTED,THE RESULT FOUND ''SATIS'' IAW AMM 33- 51-10-962-104 REV 139,
FOUND THE R4 FWD CUTOUT PANEL LOWER EXIT IDENTIFIER CRACKED(P/N: 702409-1001), REPLACED THE R4 FWD CUTOUT PANEL LOWER EXIT IDENTIFIER AND INSTALLATION TEST "PASSED",IAW AMM 33-51-09- 422-042 REV 139 & AMM 33-51-09-022-041 REV 139.
LAV J AND K WALL MOUNTED EMERGENCY LIGHT BASE FOUND CRACKED.(TTL :4EA), REPLACED THE LAV J AND LAV K WALL MOUNT ED EMERGENCY LT EACH FOR TWO FORM FWD SIDE,PERFORMED THE LAV J A ND LAV K WALL MOUNTED EMERGENCY LT LAMPS TEST,THE RESULT FOUND " NORMAL".IAW AMM 33-51-10-962-173 REV 139,
R4 DOOR CUTOUT AREA BIG EXIT SIGN BASE FOUND CRACKED, REF TO HAECO NON ROUTINE NO.9454710,SPEC NO.B767- 33-3-7000. REPLACED R4 DOOR CUTOUT AREA BIG EXIT S IGN AND PERFORMED EXIT SIGN INSTALLATION TEST,THE RESULT FOUND " NORMAL".IAW AMM 33-51-01-402-030 REV 139 & AMM 33-51-01-022-029 REV 139,
G5 WALL L/H FWD 1EA EMERGENCY LIGHT BASE FOUND CRACKED,ORIGINATE D BY EMP V903178,REF TO HAECO NON ROUTINE NO.9455397,SPEC NO.B76 7-33-3-7000. PERFORMED BY EMP V903178,REPLACED G5 WALL L/H FWD 1EA EMERGENCY LIGHT AND LAMPS TESTED.THE RESULT FOUND "NORMAL",IAW AMM 33-51-1 0-962-173 REV 139,IDT BY TA688.
EY SEAT ROW 36D,47D EMERGENCY LIGHT FOUND CRACKED,ORIGINATED BY EMP V903178,REF TO HAECO NON ROUTINE NO.9456047,SPEC NO.B767-33- 3-7000. PERFORMED BY EMP V903178,REPLACED EY SEAT ROW 36D & 47D EMERGENC Y LIGHT AND LAMPS TESTED,THE RESULT FOUND "SEAT",IAW AMM 33-51-1 0-962-104 REV 139,IDT BY TA688.
L1 DOOR AREA LOWER CEILING PANEL EMERGENCY LIGHT ASSY L611 FOUND DAMAGED,ORIGINATED BY EMP V903178,REF TO HAECO NON ROUTINE NO.9 455163,SPEC NO.B767-33-3-7000. PERFORMED BY EMP V903178,REPLACED L1 DOOR AREA LOWER CEILING PAN EL EMERGENCY LIGHT ASSY L611 AND LAMPS TEST PERFORMED.THE RESULT WAS "NORMAL",IAW AMM 33-51-04-002-017 REV 139 & AMM 33-51-04-40 2-051 REV 139,IDT BY TA 688.
EXTERNAL EMERGENCY LIGHT OF L2 DOOR FWD AREA FOUND DIM(P/N:767), REPLACED L2 DOOR FWD AREA EXTERNAL EMER GENCY LIGHT AND OPS CHECKED,THE RESULT FOUND "SATIS",IAW AMM 33- 51-06-902-082 REV 139,
PER CREW: AT CRUISE W/GEAR HNDL UP, GEAR DISAGREE MSG W/NOSE GEAR UP/L GEAR DN/R GEAR IN TRANSIT. REMOVED AND REPLACED PSEU. PARTS USED: 76-3260-9-0005,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1605339 SN OFF 1028 UNIT, ASSY, PRO OFF 76-3260-9-0005 1028 ON 76-3260-9-0005 0634 PERFORMED 5 FULL GEAR SWINGS REF AMM 32-32-00-735-057-001. ALL INDICATIONS NORMAL IN EXTENDED AND RETRACTED CONFIGURATIONS DURING ALL SWINGS.
FWD IFE COOLING EICAS S "FORWARD COOLING SYSTEM FAN FAILURE, ACTUAL SMOKE DETECTED, IFE CARD FAILURE, OR INBOARD SHUTOFF VALVE FAILED CLOSED." FWD IFE COOLING STATUS MESSAGE R/R IFE EQUIPMENT COOLING SYSTEM CIRCUIT CARD IAW AMM 21-58-67. NO FAULTS ARISED , OPS CHECK GOOD AT THIS TIME. PARTS USED: 64-2158-3-0012,QTY :1
HAD TE FLAP DISAGREE LOCKED UNLOCKED FOR UPDATE FSEU BITE FAULT ON FLIGHT LEG 0: ''ALT UP DISAGREE'', MSG NO. ACCOMPLISHED FSEU BITE TEST PROCEDURE PER FIM 27-51 TASK 809. 27-51043, FDE: DISAGREE, INTRMTNT INACTIVE, ALT SYS A/S <90. ALL TEST PASSED. STARTED FIM TASK 810 STEP 22. PERFORMED FIM TREE 27-51 TASK 810. TE FLAP DISAGREE. REPLACED RELAY K351 IN P36 PANEL. PERFORMED PRIMARY AND ALTERNATE TEST OF FLAPS AND SLATS PER AMM TASK 27-58-00-715-001-003. OPS CHK OK.
COCKPIT PORTABLE EMERGENCY EXIT SIGN INOP REPLACED COCKPIT PORTABLE EMERGENCY EXIT SIGN LIGHT BATTERY AND INSTALLATION TEST NORMAL AS PER AMM 33-51-01 R137
UA 200-0164 B767-53-3-0175 CABIN FWD WET AREA FLOORBEAM STRUCTU RE FND CORROSION AT STA303 LBL36 CARRIED OUT REPAIR AT FLOOR BEAM STA303 LBL36 AS PER B767-400ER SRM 53-00-51-2R-1 REV67, DETAIL STEPS REF TO UAL 44-0008 FORM. WORK PERFORMED BY BSH PVG BY V914247
UA 200-0143 B767-53-3-0175 FWD WET AREA FLOORBEAM STRUCTURE FND CORROSION AT ATA325,LBL54.75 CARRIED OUT REPAIR AT FLOOR BEAM STA325 LBL54.75 AS PER 767-400E R SRM 53-00-51-2R-1 REV67. DETAIL STEPS REF TO UAL 44-0008 FORM. WORK PERFORMED BY BSH PVG BY V914247
L ENGINE BLEED OFF LIGHT DURING TAKEOFF ROLL. REJECTED TAKEOFF. HPSOV FAIL OPEN FAULT ON AIR SUPPLY UNIT. VERIFIED LEFT HPSOV NOT IN THE FULL CLOSED POSITION. REMOVED AND REPLACED LEFT ENGINE HPSOV. GROUND OPS AND LEAK CHECKS GOOD.
B767-06-3-0052 FUSELAGE EXTERNAL SKIN SURFACE 1EA FASTENER HOLE FOUND CRACK AT STA 1654.5 BTN S3R-S4R (AS MARK) REF NR LP 9130095 FUSELAGE EXTERNAL SKIN REPLACED AS PER EC/RA 5380-01290 REV - JUST AT STA 1654.5 BETWEEN STR-3R AND STR-8R THIS EC/RA PROVIDES AND INSTRUCTION TO ACCOMPLISH A CATEGORY A REPAIR FORM 44.0008 ITEM 1-29 ACCOMPLISHED ADD EMP:V926514 RII APPROVED BY HX 146606
MULT-33-3-0004 FOUND SEATS 43-44 EMER LT DIM TRANSFER REF. BATT CHARGER / POWER SUPPLY REPLACED & TESTED NORMAL IAW AMM 33-51-07.
GEAR DISAGREE AND NLG WILL NOT RETRACT. TOMC CONTACT TOMC TO CLEAR UNLOCKING T/S PER FIM 32-34-00-715-001. R&R NLG SEL BYPASS VLV. LEAK CK''D OK REF AMM 32-31-04. NLG EEXTENSION & RETRACTION PERFORMED IAW AMM 32-34-00715-001. OPS CK''D GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1760686 SN OFF 0361 IPC REFERENCE # VERIFIED P/N FOR CONFIGURATION AND FUNCTIONAL/OPS CK AND INSTALLATION AND SECURITY CK OK. VALVE, NLG, SEL OFF 25-3231-9-0004 0361 ON 27-3221-9-0012 0434
GEAR DISAGREE ON TAKEOFF PERFORMED FIM TASK 32-61-00-815 -827-001 FOR DISPLAYED STATUS MS G LDG GEAR MONITOR, FROM SHEET 1 (BLOCK 1) TO SHEET 2 (BLOCK 2), RECORDED FAULT CODES 260 AND 264. ADD FAULT: 32-90-24-00 PERFORMED CHECKS OF SYS 2 LATCH LOCK S260,S264 SENSOR VALUES FRO M REAR PSEU CONNECTOR D2166E AND COMPARED TO SYS 1 LATCH LOCK SE NSOR VALUES ARE GOOD. T/S USED WDM 32-61-11 AND SSM 32-61-01. CALL TOMC PRIOR TO SIGNING OFF THIS LOG PAGE. OKAY TO UNLOCK PERFORMED GEAR SWING AND FOUND NO FAULTS. REPLACED MAIN GEAR BY PASS /CONTROL VALVE V652 SEE L/P 3498413, CHECKED NOSE GEAR STEE RING CHECK VALVE AND RESTRICTOR SEE L/P 3499930. SINCE PSEU SHO WED CARD FAILURE 1,5,6, & 7. REMOVED AND REPLACED PSEU SEE L/P 3496924.CHECKED GOOD ON GEAR SWING AFTER ALL L/P WERE COMPLETED.
AFT BAY CTR FUEL TANK STIFFNER BRACKET PNL BETWEEN AFT BULKHEAD & CENTER BAY WALL APPROX 40"LBL AFT UPPER CORNER IS CRACKED ALL WORK ACP REF AVO 07394, ECRA 5711-01154 AND WORK ACP ON DOCK NON-ROUTINE 6496967.
AFTER TAKEOFF MSGS LT MLG GEAR DISAGREE GEAR DOORS EICAS CPT REPORTED THAT THE NOSE AND R/MLG SHOWED UP AND LOCK. THE LEFT DID NOT SHOW UP AND LOCK. AC TAXI IN WITH LEFT MLG DOOR DOWN ONLY, RED UNSAFE LT ILLUMINATED. INITIAL INSPECTION FOUND THE LDG GR DOOR CLOSE C/B ON THE P34 TRIPPED EVERY TIME AND MLG DOORS WOULD NOT CLOSE. TROUBLESHOT PER WDM 32-35-11 AND FOUND THE LEFT MLG DOOR SAFETY VALVE AT FAULT. R&R LT MLG DOOR SAFETY VALVE PER AMM 32-35-10, OPS AND PANEL OPEN. CLOSED C/B AND JACKED A/C TO PERFORM GEAR SWING. C/B ROTABLE PARTS CHANGE WAS INDICATED - TT 1365204 SN OFF 0039 VALVE, MLG, SAF OFF 64-3235-9-9002 0039 ON 64-3235-9-9002 0049 LEAK CK GOOD. PERFORMED MULTIPLE GEAR SWINGS, ALL CKS GOOD.
EMERGENCY LIGHTS IN PAX CABIN FLICKERED ON TAKEOFF ROTATION. PERFORMED AN EMERGENCY LIGHT SYSTEM TEST SEVERAL TIMES ON THE GROUND FOUND OK IAW 33-51-00-501.
LEFT ENGINE OIL QUANTITY LOW. AIRCRAFT DIVERTED TO KSFO WHEN READING 5 QTS. DURING ENGINE MOTORING, FOUND OIL TUBING LEAKING AT LOWER CASE. BORESCOPE FOUND EXCESSIVE OIL LEAKAGE UPPER QUADRANT WITH DAMAGE TO OIL LINE. ENGINE CHANGE UNDER WAY.
EXT EMER SLIDE LIGHT DOOR L3 INOP, RELAMP NO HELP. CLEANED SOCKET AND RELAMPED L3 DOOR SLIDE LIGHT IAW AMM 33-51-06 . OPS CHK GOOD.
EXT EMER SLIDE LIGHT DOOR R3 INOP, RELAMP NO HELP. CLEANED SOCKET AND RELAMPED R3 DOOR SLIDE LIGHT IAW AMM 33-51-06 . OPS CHK GOOD.
R3 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-06. OPS CHECHED GOOD.
BS 325, RBL 33 - 55 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.
BS 303, LBL 11 TO 53, FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND FOUND OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.
BS 347 RBL 24-48 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.
BS 325 LBL 22 TO 54 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.
CREW REPORTED APU DOOR STATUS MESSAGE IN FLIGHT WITH NOTICEABLE VIBRATION & BUFFETING. APU WOULD NOT START. REMOVED APU INLET DOOR ACTUATOR IAW AMM 49-15-06. INSTALLED APU INLET DOOR ACTUATOR IAW AMM 49-15-06 UP TO STEP G(1)(J).
FOR SDR REPORTING R4 & L4 EMER LIGHTS IN OPERATION. R & R EMER LIGHT BATTERY PACK AT 4R DOOR FLIGHT ATTENDANT SEAT. OPERATIONS TESTED GOOD IAW AMM 33-51-07. PN INSTALLED AD-D717-01-100, SN 155504, 29-3351-3-001 3.
ON TAKEOFF ROLL, LT ENG BLEED OFF, EICAS MSG. AFTER DEPARTURE RAN QRH V LIST, LIGHT REMAINED ILLUMINATED. NOTICED RESIDUAL BLEED AIR OF 15 PSI ON LT SIDE WITH LT ENG BLEED OFF. ALSO LT BLEED HPSOV STATUS MSG. ACCOMPLISHED ASCTU BITE PROCEDURE IAW MM 36-23-00-501. LT HPSOV FAILED TO OPEN. REPLACED NR 1 ENG HPSOV IAW MM 36-11-07. ACCOMPLISHED ASCTU GND TEST, ALL NORMAL. STATUS MSG EXTINGUISHED. ACCOMPLISHED GND RUN IAW MM 71-00-00. ALL BLEED INDICATIONS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED TT 1706868 SN OFF 04268 FAULT DATA, FAULT CODE 1 36-10240 FAULT CODE 2 1140, FAULT COMMENTS LT HPSOV BUTTERFLY SEAL FOUND DAMAGED AFTER REMOVAL. VLV ASSEMBLY HI OFF 64-3611-9-0007 4266 ON 64-3611-9-0007 5050.
ON CLIMB OUT HAD LIGHTNING STRIKE ON NOSE WITH STRONG ELEC SMELL. PREFORMED LIGHTNING INSPECTION IAW 05-51-19-212-001.
RIGHT ENG BLEED LIGHT CAME ON DURING TAKEOFF ALONG WITH RT REVERSER ISOLATION VLV. IAW NR 4712443 FOR R & R OF HPSOV, PERFORMED AIR SUPPLY DISTRIBUTION SYS TEST IAW 36-11-00-715-029-0-01, SYS CHECKED NORMAL AT THIS TIME, NO DEFECTS NOTED.
IAW B767-33-3-0006 CABIN SEAT 1D FWD POSITION EMERGENCY LIGHT DIM. SEAT 1D FWD POSITION EMERGENCY LIGHT LAMP REPLACED & LAMP TEST NORMAL IAW AMM 33-51-10.
B767-33-3-0006 CABIN FWD ZONE SEAT PROXIMITY EMERGENCY LIGHT FOUND NOT ILLUMINATED. EMERGENCY LIGHT BATTERY REPLACED & OPERATION TESTED NORMAL IAW AMM 33-51-07.
EMERGENCY LIGHT BATTERY CHARGER M1210, STA 1545 DR, 4R SELF TEST FUNCTION INOPERATIVE. R & R BATTERY CHARGER, OPS CHECKED NORMAL.
AFTER ACFT DEPARTURE, THE AIRPORT AUTHORITY FOUND SEVERAL BRAKE DEBRIS ON THE INNER TAXIWAY NEAR THE POSITION 17. THE DEBRIS HAVE BEEN GIVEN TO OUR LINE MX PERSONNEL, AND HAVE MX STORE. FOLLOWING THIS QUICK INVESTIGATION, IT APPEARS THAT THE BRAKE DISK AND PISTON DEBRIS FOUND ON THE TAXIWAY ARE VERY SIMILAR TO THE DISK INSPECTED ON THE SPARE BRAKE. FURTHER TO THIS RESULT, MX HAS BEEN INFORMED AND PICTURES OF THE DEBRIS SENT TO THEM FOR DEEPER INVESTIGATION. THE ACFT HAD BEEN INSPECTED BEFORE FLIGHT AND ETOPS PRE-DEPARTURE CHECK PERFORMED. DURING THE INSP/CK NO REMARKS OR DISCREPANCIES HAD BEEN REPORTED. AFTER ACFT ARRIVAL, MX CONFIRMED THAT THE AFT INNER BRAKE (NR 7) WAS DAMAGED AND THAT THE DEBRIS FOUND WERE COMING FROM THAT BRAKE.
CABIN STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORRODED. STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORROSION BLEND OUT D:0.019" (ORG.063") OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND SPLICE PLATE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WORKING DETAIL REFER NRC 200-11025306784) AT STA 325 RBL 37 TO LBL 63.
CABIN: STA 303 LBL 30 TO 40 FLOORBEAM DOUBLER CORROSION FOUND. CABIN: STA 303 LBL 30 TO LBL 40 FLOORBEAM DOUBLER COR BLEND OUT D 0.020"(ORG 0.063") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM UPPER CHORD AND DOUBLER REPAIRED AS PER SRM 53-00-51 REPAIR FIG 201 AND FORM 44.0008 ATTACHED ITEM 1-18 ACCOMPLISHED AT BS 303 LBL 6 TO LBL 63.
CABIN: STA 325 LBL 48 TO 53 FLOORBEAM CORROSION FOUND. CABIN STA 325 LBL 48 TO 53 FLOORBEAM CORRODED BLEND OUT D0.037" (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE, FIG 101 LIMIT AND COR FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND FORM 44.0008 ATTACHED ITEM 1-18 ACCOMPLISHED AT STA 325 RBL 37 AND LBL 63.
CABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION FOUND. CABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION BLEND OUT D:0.018 (ORG 0.063) OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND DOUBLER REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WORKING DETAIL REFER NRC 200-1102 (5306784) AT STA 325 RBL 37 TO LBL 63.
CABIN STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION FOUND. STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION BLEND OUT D:0.036 (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DMG FIG 101 LIMIT AND FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WORKING DETAIL REFER NRC 200-0964 (5306762) AT STA 303 LBL 6 TO LBL 63.
CABIN STA 301 TO 304 LBL 84 FLOOR SUPPORT CORROSION FOUND. CABIN FLOOR SUPPORT CORROSION BLEND OUT D:0.047" (ORG.0063") OUT OF SRM 53-00-15 ALLOWABLE DMG FIG 101 LIMIT AND CORRODED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ATTACHED ITEM 1-15 ACCOMPLISHED AT STA 246 TO STA 368 LBL 89.
CABIN RBL 88 STA 1386 TO 1390 SEAT TRACK CORROSION FOUND. CABIN RBL 88 STA 1386 TO 1390 SEAT TRACK CORROSION BLEND OUT D :0.035 OUT OF SRM 53-00-52 ALLOWABLE DMG 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPAIRED AS PER ECRA 5320-02010 AT STA 1219 TO STA 1417 RBL 88 AND FORM 44.0008 ATTACHED ITEM 1-16 ACCOMPLISHED.
CABIN STA 1222-1351 RBL 88.5 SEAT TRACK CORROSION FOUND. CABIN STA 1222-1351 RBL 88.5 SEAT TRACK CORROSION BLEND OUT D:0. 038" W:0.8" L:2.5" OUT OF SRM 53-00-52 ALLOWABLE DAMAGE FIG 101 LIMIT AND SEAT TRACK REPAIRED AS PER ECRA 5320-02010 AT STA 1219 TO STA 1417 WORKING DETAIL REFER NRC 200-0357 (5303981).
CABIN: BS 1480 LBL 55 SEAT TRACK BASE CORRODED. CABIN BS 1480 LBL 55 SEAT TRACK BASE CORROSION BLEND OUT D:0.036" OUT OF SRM 53-00-52 ALLOWABLE DMG 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02 AT BS 1362.45 TO 1480 LBL 55 AND FORM 44.0008 ATTACHED ITEM 1-9 ACCOMPLISHED.
SUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 I/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 I/B STIFFENER REPLACED AND INSTALLED AS PER FCD5420-01488 STEP 6 AND BOEING DWG 311T2400.
SUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 O/B STIFFENER REPLACED AS PER FCD5420- 01488 STEP 6 AND BOEING DWG 311T2400, AND INSTALLED AS PER FCD 5420-01488 STEP 6 AND BOEING DWG 311T2400.
SUPPORT TASK FCD5420-01487 NR 1 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED NR 1 PYLON NAC STA 285 O/B STIFFENER. REPLACED AND INSTALLED AS PER FCD5420-01487 STEP 6 AND BOEING DWG 311T2400.
R-3 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON R-3 DOOR EXT EMERGENCY LIGHT CONTACTS. CLEANED LIGHT ASSY CONTACTS PER 33-51-06.
L-4 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON EMERGENCY LIGHT CONTACTS AT L-4 DOOR. CLEANED CONTACTS PER PER 33-51-06.
R-4 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON R-4 DOOR EMERGENCY LIGHT CONTACTS. CLEANED CONTACTS PER 33-51-06.
L-3 DOOR EXTERIOR EMERGENCY LIGHTS ARE NOT WORKING. L-3 DOOR EMERGENCY LIGHT ASSY FOUND WITH CORROSION ON LIGHT CONTACTS. CLEANED CONTACTS PER 33-51-06.
STA 325 LBL 22 TO 50 FLOOR SUPPORT FOUND CORROSION. REPAIRED PER SRM 53-00-51.
FX FLOORBEAM STIFFENER FOUND CRACKED AT BS 246 LBL 40 FWD SIDE. FX FLOORBEAM BS 246 LBL 40 FWD SIDE STIFFENER REPAIRED AS PER ECRA5310-04723 AND HFEC , NO CRACK FOUND.
CABIN STA 303 LBL 20 TO 40 FLOOR SUPPORT FOUND CORROSION. REPAIR PER SRM 53-00-51.
THE EMERGENCY PATH LIGHT AT SEATS 5, 6 AND 7 WOULD NOT ILLUMINATE. THE EMERGENCY POWER SUPPLY D21296 WAS REMOVED AND REPLACED IAW AMM 33-51-07.
THE R-4 DOOR FWD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED.
INSPECTION FOUND A 0.025 INCH CRACK IN RT WING IB AILERON IB HINGE RIB SUPPORT AT AFT HI-LOK AREA, WS 467.8. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5740-02094.
INSPECTION FOUND FLOORBEAM CORRODED AT STA 303-325, LBL 22-34. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.
INSPECTION FOUND FLOORBEAM CORRODED AT STA 325, LBL 48 - RBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201.
THE LANDING GEAR DISAGREE AND GEAR DOOR DISAGREE EICAS MESSAGES CAME ON AFTER TAKEOFF FROM GRU. THE GEAR WAS CYCLED TWICE WITH NO CORRECTION. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GRU WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING PER MM 32-32-00 FOUND THE RIGHT MLG DRAG BRACE ACTUATOR BROKEN AT THE ROD END. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-02-401. OPERATIONAL AND LEAK CHECKS WERE GOOD.
AT 90 KNOTS LOST ALL OIL PRESSURE ON LEFT ENGINE. REJECTED TAKEOFF. REPLACED RT DATA CONCENTRATOR UNIT PER MM 31-63-06, PG 401. LOADED SOFTWARE IAW MM 31-63-06, PG 201.
RIGHT GENERATOR CONTROL OFF LIGHT CAME ON IN FLIGHT. STARTED APU BUT APU GENERATOR OFF LIGHT CAME ON. REPLACED RIGHT GENERATOR CONTROL UNIT.