N649UA
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 AIRLINES INC | Operator | 2022-12-08 – 2022-12-08 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2022-12-08 – 2022-12-08 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
BULK CARGO COMPARTMENT: CORROSION FOUND AT S34L & BS 1562. PERFORMED STRINGER REPAIR IAW SRM 53-00-03-2R-2 REPAIR 2, DETAIL IV & EC/RA 5360-02139. PERFORMED INSPECTION OF THE STRINGER REPAIR IAW SRM 53-00-03-2R-2 REPAIR 2, DETAIL IV & EC/RA 5360-02139. PERFORMED INSPECTION OF STRINGER REPAIR IAW SRM 53-00-03-2R REPAIR, DETAIL IV & EC/RA 5360-02139 IN A PREVIOUS UPDATE. IT WAS PERFORMED STRINGER REPAIR IAW SRM 53-00-03-2R-2 AND EC/RA 5360-02139. PERFORMED INSPECTION OF THE STRINGER REPAIR IAW SRM 53-00-03-2R-2 REPAIR 2, DETAIL IV AND EC/RA 5360-02139 ,
DURING REMOVAL OF FASTENERS BETWEEN BS 955 AND 977 RBL 54.75 ON THE ZEE CHORD CRACKS WERE FOUND IN TWO FASTENERS. . THE STEPS OF REPAIR HAVE BEEN PERFORMED ON NON ROUTINE 3389289. FOR THIS REPAIR WAS ISSUED ECRA 5350-02639. NO MORE MAINTENANCE IS REQUIRED. ALL STEPS FROM ECRA 5350-02639 WAS ACCOMPLISHED.
PERFORMING THERMOGRAFIC INSPECTION ON THE RH WING OUTBOARD AILERON IT WAS NOTICED MOISTURE INGRESSION INDICATION AT THE INBOARD END OF THE AILERON. PERFORMED UPDATE OF THE ATTRIBUTES TO MAJOR REPAIR AND IT WAS CREATED THE SFR, IT`S NECESSARY THE QC REVIEW THE INFORMATION AND APPROVAL THE SFR NUMBER. THE SFR NUMBER 3587 HAS BEEN REVIEWED AND APPROVED. THE SFR NUMBER 3587 HAS BEEN REVIEWED AND APPROVED PREVIOUSLY BY QC INSPECTOR U395678 ALL STEPS OF THE ECRA: 5760-01145 RH OUTBOARD AILERON, P/N: 767-3650-42A2, S/N: 000932 WERE ACCOMPLISHED WITHOUT DEVIATION. IT WAS REVIWED ALL STEPS OF THE ECRA 5760-01145 RH OUTBOARD AILERON, WERE ACCOMPLISHED WITHOUT DEVIATION AND THE SFR NUMBER 3587 HAS BEEN REVIEWED AND APPROVED.
PERFORMING THERMOGRAFIC INSPECTION ON THE LH WING OTBD AILERON IT WAS NOTICED MOISTURE INGRESSION INDICATION IN TWO POINTS OF THE AILERON, ONE AT THE INBD END OF THE AILERON AND ANOTHER ABOUT 15 INCHES FROM OF THE OTBD END. ALL THE STEPS WERE ACCOMPLISHED WITHOUT DEVIATION FOLLOWING THE EC/RA 5760-01144
IN CLIMB WITH CLIMB POWER SET EXCESSIVE VIBRATION LEFT ENGINE. 5 .0 VIB WITH FEEL/SOUND.AFTER LANDING IT WAS FOUND AT THE ENGINE NR 1 SIGNALS OF BIRD STRIKE, WITH BLOOD AND STRONG SMELL OF BIRD. AFTER INSPECTION OF BIRD STRIKE REFER AMM 05-51-18-212-001, REMOVED THE INLET CONE REFER AMM 72-31-01-024-001-N00, RECORDED THE BLADES SEQUENCE AND IT WAS FOUND BLADES AT POSITIONS 18, 19, 20, 21, 22, 23, 34, 35 AND 36 DAMAGED, ONE OUTLET GUIDE VANE AT 1 O'CLOCK POSITION WITH MISSING MATERIAL AND PANEL NR 1 OF THE FAN EXIT LINER SEGMENT OUTTER PANEL WITH HOLE. FOR FURTHER EVALUATE IT'S IS NECESSARY TO REMOVE SPINNER FRONT CONE, SPINNER REAR CONE AND FAN BLADES DAMAGED FOR REFERENCE SEE AMM 72-31-02/401. IT WAS REMOVED SPINNER FRONT CONE, SPINNER REAR CONE IAW AMM 72-31-01-024-001-N00. IT WAS REMOVED ENGINE NR 1 FAN BLADES FULL SET AS PER AMM 72-31-02-004-012-N00. INITIATED BIRD STRIKE INSPECTION BY EC/RA 7200-07362, PERFORMED SHEET 1 BLOCKS 1 AND 10. FOUND SEVERAL DAMAGES AT ENGINE FAN BLADES NUMBER 18, 19, 20, 21, 22, 23, 34, 35 AND 36. NECESSARY TO CONTINUE BLOCK 11 BOROSCOPE INSPECTION. NECESSARY BOROSCOPE INSPECTION BY EC/RA 7200-07362 SHEET 1 BLOCK 11. IT WAS ACCOMPLISHED BORESCOPE INSPECTION AS PER EC/RA 7200-07362 SHEET 1 - BLOCK 11, NO ABNORMAL CONDITION FOUPERFORMED TASK 71-00-00-725-008-N00 TEST 8 VIBRATION SURVEY VIBRATION VALUES WITHIN LIMITS DETERMINED PER TASK ABOVE
DOOR 1R YELLOW. EMERG EXIT. FLAG POPS UP BEHIND VICE IN FRONT OF RED. PULL. HANDLE ADJUSTED DOOR 1R YELLOW EMERGENCY FLAG SO THE FLAG GOES INTO ITS PROPPER POSITION ADD EMP: U376824
OPERATIONAL TEST - EMERGENCY ESCAPE PATH LIGHTING (EEL) SYSTEM PERFORM OPERATIONAL CHECK - PATH LIGHT 6D DOESN'T WORK. REMOVED AND REPLACED LAMP ASSY REF 33-51-10-962-105, GOOD FOR SERVICE.
AFTER TO ALL FWD GALLEY OVENS AND CHILLERS INOP. AFT R COFFEPOT INOP OPERATED GALLEY OVENS/CHILLERS FOR APPROX 25 MIN AT HIGH PWR UNABLE TO DUP. PLEASE CHECK KVA SETTING OF FWD ELCU PER NAT DRAWING N0542-D73 WD 25-31-11, PINS 11 & 14 ARE JUMPERED. IF NO DEFECT CONT.. INSPECT GALLEY DISC D9066 FOR SECURITY AND INSPECT PINS FOR DAMAGE. ALSO INSPECT D378 OF FWD ELCU M225 AND MAIN FEEDER CABLES A1,A2,B1,B2,C1,C2, IF NO FAULTS REPLACE THE FWD ELCU M225 AND BPCU AS A PRECAUTION VERIFIED CORRECT KVA SETTING WITH PINS 11 AND 14 JUMPER OF D378, CONTINUITY CHECKED GOOD. REF NAT DRAWING N0542-D73. PERFORMED GVI OF D378 AND FEEDER CABLES A1,A2,B1,B2,C1,C2 AT M225 ELCU, NO ISSUES FOUND. REF AMM 25-31-03-404-009, NAT DRAWING N0542-D73. R & R BPCU REF AMM 24-41-03-404-008, OPS CHECKED OK. R & R ELC REF AMM 25-31-03-404-009 , OPS CHECKED OK. DURING ENGINE RUNS VERIFIED GALLEY POWER DID NOT SHED POWER WITH LOAD SUPPLIED. GALLEY POWER CHECKED GOOD.
EMERGENCY LIGHTS OPERATIONAL CHECK, EMERGENCY LIGHT ON SEATS 35F AND 48F ARE BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ON SEATS 35F AND 48F REF CMM 25-21-53. GOOD FOR SERVICE.
30R EXIT ROW PLASTIC NOT SECURED BRACKET FOR LENS COVER IS DAMAGED. INSTALLED TAPE TO SECURE IN PLACES WAITING ON ECRA FOR SIGN OFF. PICTURES ADDED COMPLIED WITH ECRA 3351-01489 PART 1 AND 2 INITIATED DIP TO COMPLY WITH PART 3 IN 3 FLIGHT CYCLES OK TO CARRY FOR PERMANENT REPAIR WITHIN 3 FLT CYCLES PER ECRA 3351-01489, WILL REQUIRE REPETITIVE INSPECTION PRIOR TO EACH DEPT. QC REVIEWED RECORDS REMOVED AND REPLACED EXIT SIGN AT ROW 30 RH SIDE REF AMM 33-51-01 OPS TEST GOOD.
REJECTED T/O ENG SRG D2 PSBL BIRD INGEST RT ENG SPEED 160 HIGHE ST BTMS 9+ CREW DEBRIEF: 160 KTS, APPROACHING T/O SPEEDS, SAW BIRD FLY IN F RONT OF ACFT, HEARD A BANG ON E2, OBSERVED MOMENTARY DROP AND RE COVERY OF EPR. CAPT SIMULTANEOUSLY THROTTLED DOWN FOR RTO. TOWER REPORTED A FLASH AT E2 ALSO. INSP INLET/EXHAUST- NO EVIDENCE OF BIRD STRIKE. SMELL OF BURNT BIRD NOT PRESENT EITHER. SUSPECT CO MPRESSOR STALL. ALL BRAKE TEMPS WERE NORMAL WHEN ACFT BLOCKED IN , FUSE PLUGS ALL INTACT. LOCKED FOR FINDINGS REF AMM 05-51-14 FOR REQUIRED INSP PERFORMED HIGH ENERGY STOP INSPECTION REF AMM-TASK 05-51-14-212-089. FOUND NO DAMAGE, FUSE PLUGS NORMAL. F.I.M 71-08 FAULT TREE 804 HAS US CHECK THE PS3 AIR FILTER ELEMENT AND THE PNEUMATIC RELAY VALVE ON THE 2.9 BLEED VALVE. FOUND ELEMENT RESTRICTED( DIRTY) UNLOCKED FOR SIGN OFF F.I.M 71-05 TREE 803 FINISHED . SOME WORK DONE ON LOGPAGES 3590303, 3586644 AND 3590561. PROBLEM WAS CLOGGED PS3 FILTER ELEMENTS ON 2.8 BLEED VALVE. REMOVED AND REPLACED BOTH PS3 AIR FILTERS AND 1 PS3 AIR FILTER ASSEMBLY ON 2.8 BLEED VALVE I.A.W ADD EMP:U242424,U365605 A.M.M 75-33-05 . COMPLETED F.I.M 71-08 TREE 804 OPS CHECK GOOD. VALVE AND SOLENOID WORK AS DESIGNED
STAB TRIM EICAS CAME ON ON INIT CLIMBOUT PERFORMED TROUBLESHOOTING PROCEDURE FOR STAB TRIM REF FIM 27-48 TASK 809, FAULTING LEFT HYDRAULIC BRAKE PRESSURE SWITCH STAB TRIM MESSAGE NO LONGER ACTIVE REFERENCE LOG PAGE 8475892 FOR ACTION TAKEN. LEFT HYDRAULIC BRAKE PRESSURE SWITCH FAULTED ON STAB TRIM BOX DURING TROUBLESHOOTING. SETTED LEFT AND CENTER STAB TRIM SHUTOFF VALVE SWITCHES TO CUTOFF. REF B767 AMM 27-41-07 STEP 2E(3) REMOVED AND REPLACED LEFT HYDRAULIC BRAKE PRESSURE SWITCH REF AMM 27-41-07. OPS CK GOOD, LEAK CK GOOD. NO DEFECTS NOTED. NO MESSAGES SHOWING PARTS USED: 75-2741-3-0088,QTY :1
CABIN LIGHTING OPERATIONAL CHECK {B767-33-3-7008} - DIRECT CELING LIGHT AT POSITION 10A, 10D, 10D INOPERATIVE REPLACED THE LAMP REF AMM TASK 33-22-00-962-036 NO HELP.MEL DIRECT CELING LIGHT AT POS ITION 10A, 10D, 10L(CORRECTION) 3321A NEED MORE TIME TO FURTHER TROUBLESHOOTING. PLACED ON MEL 3321A DDP C/W. APPROVED UNPLAGED AND REPLUGED BALLIST. LIGHTS OPERAT NORMALY NOW
PASSENGER AT SEAT 9L LOST LAPTOP DOWN THE SIDEWALL. LAPTOP WAS POWERED UP AT THE TIME IT WAS LOST LAPTOP WAS FOUND AND RETURNED TO PAX AT. 9L.
ELETRICAL BURNING ODOR FROM FWD GALLEY/FWD PORTION OF FIRST CLASS 10 MINUTES INTO FLIGHT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-940-801-C1. FOUND SIDEWALL LIGHT BALLAST AT SEAT 1A TO BE SOURCE OF ELEC ODOR. NEEDS BALLAST 76-3321-3-0013. R+R BALLAST M745, NO HELP. T/S FURTHER, FOUND PIN 7 AT CONNECTOR D5110P BURNED, SUSPECT RELAY K365 FAILURE, RESULTING IN BURNED PIN, REF WDM 33-21-31 SHEET 2B. R+R RELAY S365. ALSO FOUND HIGH RESISTANCE ACROSS TERMINALS OF SWITCH S9102. RETERMINATED WIRES, LIGHTS NOW OPS CHECK GOOD. STILL NEED CONNECTOR D5110P. UPDATING FOR ''SDR'' RPL CONNECTOR D5110P, NO DEFECTS FOUND ON PINS. REF WD 33-21-32-1A, 33-21-31 AND SWPM 20-61-11. FIRST CLASS LIGHTS OP NORMAL AND 1A SIDEWALL LIGHT OVERHEAD TOGGLE SWITCH OPS NORMAL. NO ABMORMAL SMELLS ABOVE FIRST CLASS CEILING AREA. CLOSED CEILING PANELS.
RAT DID NOT PRESSURIZE CENTER HYDRAULIC SYSTEM. RAM AIR TURB MODULE PRESSURE SWITCH REPLACED AND TEST RESULT NORMAL AS PER AMM 29-21-11 AMD 29-21-00. WORK ACCOMP BY MECH V924756 INSP BY V924743. ADD EMP:V924743
B767-28-3-0067, RHW FUEL TANK OVERWING FILL PORT ATTACH UPPER SKIN FOUND CORROSION REF HX NR WO.1865480, ORIG BY V897897 RHW FUEL TANK OVERWING FILL PORT UPPER SKIN PANEL CORROSION REPAIRED AS PER ECRA 5725-01126 REV.- ATTACHED MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 37 ACCOMPLISHED ACCOMPLISHED BY MECH V897537, INSP V897897 RII INSPECTED BY HX147141. ADD EMP:V897897
SUPPORT TASK - EA5315-01152 OP 002 1EA FASTENER HOLE FOUND CRACK AT 2O''CLOCK AND 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER- TRNAFER REFER NON-ROUTINE WO.1843964 AND ORIGINATED BY V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKIN DOOR 1R CUTOUT AFT CORNER REPAIRED AS PER ECRA 5515-01200 REV - PART 1 ITEM A INTERIM REPAIR ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 44 ACCOMPLISHED BY MECH V897473 AND INSPECTED BY V896919 ADD EMP:V896919 SFR 1032882. RII INSPECTED BY HX310582 ADD EMP:V896895
SUPPORT TASK - EA3515-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK AT 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER TRANSFER REFER NON-ROUTINE WO.1843962 AND ORIGINATED BY EMP V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKIN DOOR 1L CUTOUT AFT CORNER REMOVED AS PER ECRA 5315-01199 REV - PART 1 ITEM A INTERIM REPAIR ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 44 ACCOMPLISHED BY MECH V897473 AND INSPECTED BY V896919 ADD EMP:V896919 SFR 1032881 INSPCTED OKAY BY V896895 ADD EMP:V896895
B767-53-3-7025 - FWD CARGO COMPT STA595 RH PDU LH AND RH MOUNT NUTS SUPPORT BEAMS FOUND CORROSION TRANSFER REF HXWO 1858999 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA588-610 RBL33 SUPPORT BEAM (143T0019-11) (MINOR REPAIR) ATTACH MAINTENANCE WORK SHEET FORM 44-0008 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER ITEM 1 TO ITEM 30 ACCOMPLISHED SRM51-40-02 (PSE REPLACED) AND STA588 TO STA600 RBL33 WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 SUPPORT BEAM (143T5019-2) REPAIRED AS PER ECRA 5330-07097 REV- RII INSPECTED BY HX156019 ADD EMP:V897897
B767-53-3-7025 FWD CGO BTW STA 527 - STA 544 UNDER GR PDU INTERNAL 2EA WEB SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858981 AND ORIGINATED BY EMP V896375 FWD CARGO STA524-541 RBL33.08 FLOOR SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 18 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500, RBL 33" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION CRACK TRANSFER REF HXWO 1883016 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA470 TO STA498 RBL30" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SUPPORT REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 14 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7025 FWD CGO COMPT STA 583 RH PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858982 AND ORIGINATED BY EMP V896810 FWD CARGO COMPT STA583 RBL30-RBL40 SUPPORT BEAM REPLACED WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V896375 AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 13 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7025 FWD CGO BTW STA 500 - 522 R/H TORQUE BOX WEB FOUND CORROSION TRANSFER REF HXWO 1858980 AND ORIGINATED BY EMP V896375 FWD CARGO STA497 TO STA541 RBL25 TO RBL40 TORQUE BOX WEB WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V898550 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX185167 ADD EMP:V897008
B767-53-3-7025 - FWD CARGO FLOOR STA512 RBL30-34 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877229 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA512 RBL30-40 SUPPORT BEAM REPLACED AS WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
SUPPORT TASK FWD CARGO COMPT DOOR EXTERIOR FASTENER HAS LIGHTNING STRIKE 65" FROM AFT & 46" FROM LOWER EDGE TRANSFER REF HXWO 1857673 AND ORIGINATED BY EMP V896888 FWD CARGO COMPT DOOR EXTERIOR SKIN STA552 INTERIM REPAIRED AS PER ECRA 5232-01174 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 26 WORK ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V920531 INSPECTED BY V896375 RII INSPECTED BY HX169509 ADD EMP:V898550
B767-06-3-7050, FWD CGO COMPT STA 592 "9R" PDU BELOW MOUNTING SUPPORT BRACKET SHEAR WEB AREA FOUND CORROSION TRANSFER REF HXWO 1878888 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA541-STA600 RBL25 TO RBL40 FLOOR BEAM WEB WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 8 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-06-3-7083 - FUSELAGE SKIN HAS LIGHTNING STRIKE AT BS654+44-BS654+66 BTW S22R / S23R TRANSFER REF HXWO 1839295 AND ORIGINATED BY EMP V896888 FUSELAGE SKIN AT STA654+44 TO STA654+66 BETWEEN STR22R-23R WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SKIN REPAIRED AS PER SRM53-00-01-2R-6 REPAIR 6 FIG.201 (CATEGORY A REPAIR) ATTACH MANITENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 22 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7023, FWD CGO COMPT- STA 498 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883060 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA498 RBL30 TO RBL40 LATERAL TORQUE BOX WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PANEL SUPPORT CHORD REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 , ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY V898550 ADD EMP:V898550
B767-53-3-7023, FWD CGO COMPT- STA 478 TO 500 RBL 39" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION AS MARK TRANSFER REF HXWO 1883040 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA478 TO 497 RBL39" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 SUPPORT REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7025 - FWD CARGO FLOOR STA502-512 RBL36.88 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877224 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA502 TO STA512 RBL36.88 FLOOR SUPPORT BEAM WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 REPLACED AS PER SRM51-10-02 AND FASTENR INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7023, FWD CGO COMPT STA 502 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883048 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA502 RBL30 TO RBL40 LATERAL TORQUE BOX PANEL SUPPORT CHORD REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 9 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550 WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 ADD EMP:V896375
B767-53-3-7025 FWD CGO COMPT STA 550 TR PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858966 AND ORIGINATED BY EMP V896510 FWD CARGO COMPT STA544-566 RBL25 AND RBL33.08 SUPPORT WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 BEAM REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 14 ACCOMPLISHED RII INSPECTED BY HX169509 ADD EMP:V898550
B767-53-3-7058 AFT OF BULK CGO BILGE STA1540 TO STA1562 S39L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856237 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 TO STA1562 STRINGER 39L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO 28 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549
B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S39 POS INNER SKIN FOUND CORROSION TRANSFER REF HXWO 1856087 AND ORIGINATED BY EMP V896810 FUSELAGE STA1540-STA1562 BETWEEN STR39L AND STR39R SKIN INTERIM REPAIRED AS PER ECRA5361-01114 REV - PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 35 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549
B767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S38L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856266 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 STRINGER 38L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTCH FORM 44-0008 ITEM 1 TO ITEM 28 ACCOMPLISHED , WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896375 RII INSPECTED BY HX169517 ADD EMP:V898549
B767-06-3-7011 FWD CARGO : FWD CARGO DOOR AT STA 542 FRAME LOWER PORTION FOUND CRACKED TRANSFER REF HXWO 1851416 AND ORIGINATED BY EMP V898555 FWD CARGO DOOR STA542.4 FRAME INNER CHORD REPAIRED AS PER ECRA5234-01095 REV - ATTACH FORM 44.0008 ITEM 1 TO ITEM 19 ACCOMPLISHED , WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896888 RII INSPECTED BY HX169509 ADD EMP:V898550
CABIN STA 303 LBL 40"-55" FLR SUPPORT CORRDED TRANSFER REF. NON-ROUTINE HX NRC WO.1843972 AND ORIGINATED BY EMP NO. V927576 CABIN STA 303 FLOOR BEAM LBL 40" - LBL 55" UPPER CHORD REPAIRED AS PER SRM 53-00-51-2R-1 REPAIR 1 FIG 201. ATTACHED FORM 44-0008 ITEM 1-31 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V896919 RII INSPECT IS OKAY. APPROVED BY HX 341008.
PDA 3 VERBAL LAV SERVICE REPORT -- NIPPLE MISSING FOR LAV SERVICE -- SEE PHOTO PHOTO ADDED INSTALLED NEW LAV SERVICE NIPPLE. OK FOR SERVICE. CALLED LAV SERVICE TRUCK. REFERENCE 38-32-03-50.
RT ENG HIGH EGT ON TAKE OFF. MAX EGT 737 SECONDS DURATION. DUE TO PREVIOUS HISTORY OF EGT FAULTS A POSITIVE FIX IS UNLOCKED FOR UPDATE. REQUIRED. PER CREW WHEN THROTTLES WERE PULLED BACK RIGHT ENGINE EGT DEBRIEF CREW, CAPTAIN STATED THAT ONCE THROTTLES BACK TO IDLE, INDICATION WENT BLANK ON EICAS AND STAND BY DISPLAYS. THE #2 ENGINE EGT INDICATION ON BOTH THE UPPER EICAS DISPLAY TOMC-MEREDITH AND STBY ENGINE INDICATION WERE BLANK. INSPECTED INLET AND EXHAUST NO OBVIOUS DEFECTS NOTED. REPLACED W6 HARNESS AND 4 EGT PROBES AT ENGINE #2. RAN ENGINES, TOOK #2 ENGINE TO 90% N1 WITH EGT 528 TWICE WITH NO FAULTS NOTED WITH EGT INDICATION.
AUTO THROTTLES FAILED TO ENGAGE ON TAKEOFF THRUST MANAGEMENT SYS (INCLUDING A/T SYS) PLACED ON MEL. MEL STICKER AND C/B COLLARED F16 ON THE P11. DOWNGRADED A/C TO "AUTOLAND LIMIT-LAND 2". DISPATCH DESK: 82 NAME: JERRY DATE: 02-JAN-22- NOC DESK: 76 NAME: DOUG DATE: 02-JAN-22- OK TO DEFER AUTOTHROTTLE SERVO INOP T/S REF. B767-3 FIM 22-03-00 MCDP AUTO FLIGHT BITE. NO FLT. IAW AMM 22-03-00-818, ALL TESTS PASSED. ACFT. UPGRADED TO FULL FAULTS DISPLAYED. PERFORMED MCDP TESTS 02, 10, & 12 IAW FIM CAT CAPABILITY. " AUTO LAND CAT II" PLACARD REMOVED FROM FLIGHT 22-03-00-803, 810, & 812. AUTO THROTTLE SERVOS & DISCONNECT OPS DECK. CHECK NORMAL. UNABLE TO DUPLICATE FAULT. ACCOMP. MCDP TEST 30 ADD EMP:U107527
AUTO THOTTLES WILL NOT ENGAGE. CREW DEBRIEFED, STATED NO FMA ON EADI. TRIED IN MULTIPLE MODES LOCKED FOR T/S. PER LP 7341532 R IDG STATUS MESSAGE. FURTHER DETAILS AWAITED
ON APP ICAS LE SLAT ASSY MESSAGE ON ICAS COMPLIED WITH QRH AND L ANDED BIT THE FSEU AND FOUND THE FOLLOWING FAULT: LE OUTBD ASYM MSG NO. 27-81021. FDE LE ASYM LATCHED. PRIMARY A/S <90 A-A02 FR PSEU, IB SLAT +1.21V, OB SLAT +5.54V, LRV POS -2.33V. INTERROGATED PSEU AND GOT 302 FAULT, (R SLAT #10 INBD). RETRACTED FLAPS ELECTRICALLY AND HAVE SAME FAULT ON FSEU. AND MESSAGE WENT AWAY. LOWERED FLAPS AND MESSAGE CAME BACK. LE WILL NOT RETRACT HYDRAULICALLY. RETRACTED LE ELECTRICALLY REMOVED AND REPACED #10 SLAT INBOARD S302 SENSOR, ADJUSTED SCENSOR SWITCH AND RETRACT TARGET PER AMM 27-88-01-902-001.
DURING CHECK NO 2 SERVICE HMG BLOCK 8 OPRATIONAL CHECK FOUND HYDRAULIC LEAK THRU BODY OF HMG. PERFORMED INTERIM REPAIR PER ECRA 2420-01623 PART 1. HYD LINES PLUGGED ,UNIONS REMOVED NO LEAKS NOTED FROM HYDRAULIC LINES PRESSURIZED.INITIATE A DIP TO PERFORM PERMANENT REPAIR AS PER ADD EMP:U288719,U235671 ECRA PART 3. HMG WILL BE DEFFERED LOG PAGE 6259714. OK TO DIP HMG DEACTIVATED WITH LINES REMOVED AND CAPPED AND REPAIR HMG WITHIN TWO FLIGHT CYCLES PER ECRA 2420-01623 TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED SDR FLAGGED. RECORDS UPDATE - AP QC REVIEWED T/A : 2 FC.......AP/U366012 REPLACED HMG AS PER AMM 24-25-01. OPS CHECK NORMAL AND NO LEAK NOTED. ADD EMP:U288719 TOMCQC REV PERFORMED ROTABLE PARTS UPDATE ADD EMP:U288719 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1119064 SN OFF 1444 IPC REFERENCE # IPC 24-25-01-01
IN REFERENCE LOG PAGE 625880 HMG INOP. IN REFERENCE LOG PAGE 6258880 HMG INOP DEFERRED PER MEL 2425A. ADD EMP:U288719,U235671 DISPATCH DESK: 76 HMG CAPPED DUE TO HYD LEAK PER ECRA 2420-01623 LOG PAGE 6258880 . NO LEAKS WITH LINES AND HMG CAPPED 64-2425-9-0001. HMG INOP DEFERRED PER MEL 2425A. NO PARTS AT GIG. M&E
B767-53-3-7093 FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BL, 322AL , 323AL, 324AL, IS CHAFFED FROM THE PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. REF AMES NR 0446 AND UAL JOB CARD 63-5330-1-2602 ADD EMP:V929553
REF AMES NR 0448 AND UAL JOB CARD 63-5330-1-2602. B767-53-3-7093 AFT FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BR, 322AR, 323AR, 3 24AR IS CHAGGED FROM PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. ADD EMP:V929553
FWD GALLEY COMPT #216 LOWER PATH LIGHT LENS MISSING. INSTALLED FWD GALLEY COMPT #216 LOWER PATH LIGHT LENS PER AMM 33-51-10, OPS CHECK GOOD.
PREVIOUS REPAIR DOUBLER ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS 420 TO 440 HAS DENT ABOVE STRINGER 34L. REF. AAR N/R: 9463825. REMOVED AND FABRICATED NEW REPAIR DOUBLER AND INSTALLED ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS420 TO 440 IAW B767-300 SRM 53-00-01 AND SRM 51-40-08 AND PERM RES-WI 2015143-11 P-1 AND IR AND EC/RA#5310-06002. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT :AAR N/R 9463825. WORK ACCOMPLISHED BY MECHANIC, INSPECTED BY Q.C., RII INSPECTION ACCOMPLISHED BY AAR MIAMI INSPECTOR.
EMERG LIGHT INOP. SEAT 18F SECURED CONNECTOR, OPS CHKS NORMAL.
AT FL360 STANDBY ALTIMETER WAS 500 FEET HIGH AT 36500 FEET. FOUND VIBRATOR INOP. REPLACED STBY ALT INDICATOR. OPS CHECKS GOOD. REF AMM 34-13-06.
M/D STA 256 RBL 59 FLOOR SUPPORT FOUND OVAL SCREW HOLE. M/D STA 256 RBL 59 FLOOR SUPPORT SCREW HOLE OVAL AREA REPAIRED A S PER RI-53-00-12222 REV A AND REF ECRA 5310-07300 REV.
MAIN DECK BS 1241 - 1373, RBL 90 - 94 AFT CARGO DOOR UPPER AREA WEB FOUND CORRODED. THE WEB WAS REPLACED IAW SRM 51-10-02.
MAIN DECK, BS 368, RBL 54 FLOORBEAM CORRODED. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-07288, REV -.
BS 852 RBL 55 FLOOR SUPPORT UPPER SURFACE CORRODED. FLOOR SUPPORT BS 784 TO 883 REPAIRED IAW 53- 00-51, REPAIR 3, FIG 201.
TAIL COMPARTMENT BS 1809, RT FORWARD OUTER STRUCTURE FOUND CRACKED. REPAIRED IAW EA 53-00-01-600, REV A, OP 005.
BS 325, LBL 12 - 16 FLOORBEAM UPPER SURFACE FOUND CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.
FLOORBEAM CORRODED BS 303, RBL 12 TO 46. THE FLOORBEAM REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.
FLOORBEAM CORRODED BS 287, RBL 11 TO 34. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.
RT EMERGENCY EXIT SLIDE PATH AFT LIGHT IS INOP. RELAMPED, OPERATIONAL CHECK GOOD REF AMM 33-51-06
EMERGENCY PATH LIGHT AT LT MID LAV AND CROSS AISLE IS INOP. FOUND CONNECTION AT LEFT MID LAV AT SIDE WALL DISCONNECTED, SECURED, OPS TEST GOOD REF AMM 33-99-99.
DENT ON FUSELAGE AT STRINGER 37 RT & BS 654+44, JUST AFT OF FWD CARGO DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01 FIG 201 REPAIR 12.
CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT, STATION 1131, LBL 36. T CAP IN AFT CARGO HAD 100% MATERIAL LOSS. R & R IAW SRM 51-40-02.
CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT, STATION 1197+88 & RBL 36. UPON EVALUATION FOUND T CAP TO HAVE 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-00-07 FIG 101. R & R T CAP 146T1060-01 IAW SRM 51-40-05 & 51-40-02.
CORROSION ON LOWER SURFACE OF T CAP IN AFT CARGO PIT STATION 1219, LBL 36. R & R AFT CARGO COMPARTMENT, T CAP AT STATION 1219 IAW SRM 51-40-02 & DWG 146T0250.
TRAILING EDGE FLAPS WILL NOT MOVE ELEC OR WITH HYD. FOUND PIN MIGRATING OUT OF VLV INDICATOR LEVER PROHIBITING FULL VLV MOVEMENT. REPLACED FLAP PDU BYPASS VLV & ROTARY ACTUATOR.
DOOR 1L SLIDE WAS DEPLOYED ON ARRIVAL. SLIDE ASSEMBLY MR25708-739 DETACHED FROM ACFT & IS LOCATED IN BAY 1 OF THE SERVICE CTR IAW AMM 25-66-00. COMPLETED MM 25-66-00 FROM PG 203 STEP 18 TO END. REPLACED 1L SLIDE ASSEMBLY IAW MM 25-66-01. CONTINUE WITH PROCEDURE FOR RE ACTIVATION OF ENTRY DOOR AMM 25-66-00 PG 203 STEP 18.
EEL BETWEEN DOOR 1L & 1R INOPERATIVE. CLEANED & REMOVED MOISTURE FROM POWER STRIP CRIMPS & EEL CONTACTS.
EEL BETWEEN DOOR 1L & SEAT 1A INOPERATIVE. CLEANED & REMOVED MOISTURE FROM POWER STRIP CRIMPS & CONNECTIONS. ACCOMPLISHED EMER OPERATIONS CHECKED OK.
EMERGENCY EXIT LIGHT FWD LOWER BY DOOR 1 LT INOPERATIVE. REPLACED LOWER EMER EXIT LIGHT ASSEMBLY OPERATIONS TEST PASS IAW MM 33-51-00.
OVEN 41 RUBBER SEAL MISSING, BUS GALLEY. REQUIRES DOOR SEAL OR OVEN REPLACEMENT AT POS R41. REPLACED OVEN, OPERATIONS CHECKED OK.
EXTERNAL POWER ACCESS DOOR FOUND MISSING ON ARRIVAL.
DENT IN FUSELAGE SKIN AT APPROXIMATELY BS 409 BETWEEN STRINGER 33L & 34L. FOUND DENT TO BE A PREVIOUS OUT OF LIMITS BLEND. REPAIRED.
LT FUSELAGE SKIN DENTED AT APPROXIMATELY BS 396 BETWEEN STRINGER. 33L & 34L. FOUND DENT TO BE PREVIOUS OUT OF LIMITS BLEND REPAIR.
CORROSION FOUND ON FWD CARGO COMPARTMENT DOOR SILL INTERNAL RIB. LOWER SURFACE BS 576 STRINGER 45R - STRINGER 48R.
FWD CARGO COMPARTMENT BILGE FRAME TIE CLIP AT AFT SIDE CORRODED BS 742, RBL 8. LOCATED, DRILLED, PAINTED & INSTALLED NEW SHEAR TIE IAW B767-300 SRM51-40-02 & DRAWING 143T1214 REV E.
MAIN CABIN FLOOR STRUCTURE FOUND CORRODED BEYOND LIMITS BS 790, LBL 32. REMOVED DAMAGE & REPAIRED FLOOR BEAM LOCATED BETWEEN STATION 808 - 788, LBL 32 IAW SRM53-00-51 REPAIR 3 FIG 201 IAW TIMCO NR24938.
SUSPECT HYD LEAK AFT TAIL CONE AREA. FOUND SEVERAL B NUTS LEAKING AT THE ELEVATOR AP ACTUATORS. TIGHTENED, NO LEAKS NOTED.
LIFE VEST MISSING SEAT 35A. INSTALLED LIFE VEST AT SEAT 35A, OK TO CONTINUE.
VERY VERY LOUD SQUEAL IN OVERHEAD MID COACH CABIN. PLACED CEILING LIGHT AT ROW 30-31L ON MEL. BALLAST CONNECTOR D11218 DISCONNECTED & STOWED. BALLAST WAS THE CAUSE OF LOUD HUMMING NOISE, WILL REQUIRE BALLAST PCN 563-0055 & 05814-16 BALLAST.
HYD FLUID STREAM IS VISIBLE COMING FROM APU ACCESS DOOR. FOUND B NUT LOOSE ON RT ELEVATOR PCA. TIGHTENED B NUT, OPERATED ELEVATOR NUMEROUS TIMES WITH NO LEAKS. CLEANED AREA. HYD QTY GOOD.
AFTER TAKEOFF, RT REVERSER ISOLATION VLV STATUS MESSAGE DISPLAYED. ALSO, REVERSER ISOLATION LIGHT IS ON. NO EICAS MESSAGE DISPLAYED.
LT PYLON AFT WEB 313T3355-233 CRACKED AT OTBD AFT FASTENER HOLE. INSTALLED NEW WEB IAW DRAWING 313T3355.
FUEL LEAK LT ENGINE BOTTOM CORE. FOUND FUEL OIL COOLER OUTLET LINE LEAKING & BULGING IAW IPC 73-11- 06-20 PAGE 18 ITEM 68 K P/N 280-4427. REMOVED FM11 TUBE & HOSE ASSEMBLY NEED TO COMPLETE FROM STEP 3 PAGE 402 TO END. REPLACED FM11 FUEL TUBE IAW AMM 73-11-99.
APU SHUTDOWN ON PUSH BACK.
LOWER EICAS MESSAGE FWD & AFT DET FAN. TROUBLESHOT EICAS MESSAGE IAW FIM 26-16 -00 PG 109. SWAPPED CONNECTOR AT FWD BLOWER & MESSAGE CLEARED. SUSPECT FWD & AFT NR 1 BLOWERS IAW WD 26-16-21. REPLACED FWD & AFT NR 1 SMOKE DETECTOR BLOWERS IAW AMM. OPS CHECKED OK, NO MESSAGES.
AMSITM 6449 2086025 MAINT ITEM DISPLAY-STATUS MESSAGE "AFT CARGO DET 2" BY- 118014. REPLACED SMOKE DETECTOR NR 2 AFT IAW MM26-16-01. OPERATIONS CHECKED NORMAL.
ON TAXI OUT RT BLEED DUCT LEAK EICAS MESSAGE. ALSO HAVE "DUCT LEAK" LIGHT ON OVERHEAD PANEL. LIGHT & EICAS MESSAGE OUT APPROXIMATELY FIVE MINUTES AFTER SHUTTING OFF RIGHT BLEED & ISOLATING RIGHT SYSTEM. REPLACED GARLOCK SEALS ON RT BLEED DUCT, IAW IPC 36-11-04 ITEM R. OPERATIONS CHECKED WITH APU, ENGINE NR 2 RUN. NO LEAKS OR MESSAGES.
AFT CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. VERY WEAK AIRFLOW IN AFT CABIN, COULD NOT COOL UNTIL 2 HOURS INTO FLT. FOUND RT PACK VALVE INOPERATIVE. AMS FOUND FCV STUCK IN ALMOST FULL CLOSED POSITION. VALVE MR21290, PCN 643-9118. FOUND PACK CPRSR OUT TEMP AT FAULT R & R REF MM.
AFT CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. VERY WEAK AIRFLOW IN AFT CABIN, COULD NOT COOL UNTIL 2 HRS INTO FLT. FOUND RT PACK VALVE INOPERATIVE. REPLACE THE VALVE. FOUND FCV STUCK IN ALMOST FULL CLOSED POSITION. VALVE MR21290, PCN 643-9118, REF AMM 21-51-01-401 FOR R & I.
RT ENG PIMU FAULT MESSAGES EEC CHANNEL A FAULT CAT 2, EEC CHANNEL A TCC FD-BK FAIL, EEC CHANNEL B FAULT CAT 2 AND EEC CHANNEL B TCC FD-BK FAIL FOUND. REPLACED NR 2 ENG TURBINE CASE COOLING AIR VALVE ACTUATOR IAW AMM. PERFORMED PARTIAL RIG.
WEATHER RADAR ANTENNA FAILED, RETURNED TO FIELD.
C SYS HYD PRESSURE INDICATES 20 BUT NO SYS PRESSURE LIGHT AND NO EICAS EITHER LIGHTS CHECKED OK. R & R CENTER HYD SYS PRESSURE SWITCH IAW AMM. OPS AND LEAK CHECKED GOOD.
EVIDENCE OF HYD FLUID ON RT OTBD AILERON. FOUND LOOSE B-NUT ON PRESSURE LINE TO RT OTBD AILERON. TIGHTENED AND LEAK CHECKED. OPS CHECKED GOOD, NO LEAKS NOTED.
NR 2 AUDIO SELECTOR PANEL VOLUME CONTROL DEFECTIVE. REMOVED AND REPLACED FIRST OBSERVER`S AUDIO SELECTOR PANEL.
EMERGENCY LIGHT INOPERATIVE AT AFT RT INBD LAVATORY. REPLACED EMERGENCY LIGHT. SYS OK.
EMERGENCY LIGHT INOPERATIVE AT R1 DOOR. REPLACED LAMP, OPS NORMAL.
EMERGENCY LIGHTS INOPERATIVE SEAT ROWS 24 LT THRU 33 LT. REPLACED BATTERY AND CHARGER M99082 IAW MM, SEATS OPS CHECKED NORMAL.
FWD EQUIP EXHAUST FAN STATUS MESSAGE. REPLACED FORWARD EXHAUST FAN.
DURING CRUISE, NO RT INBD AILERON INDICATION MOVEMENT. DISCONNECTED AUTOPILOT AND ACCOMPLISHED SERIES OF TURNS. CONFIRMED RT INBD AILERON WOULD NOT MOVE DOWN DURING TURNS. AILERON ALSO NOT FAIRED IN NEUTRAL POSITION AND REQUIRED LT AILERON TRIM TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. REPLACED BOTH RIGHT INBOARD AILERON PCA'S PER AMM.
EMERGENCY LIGHTS INOPERATIVE AT SEATS 1AB TO 9AB. REPLACED EMERGENCY LIGHT CHARGER PER AMM.
R2 DOOR EMERGENCY LIGHT BATTERY INOPERATIVE. BATTERY REPLACED AND OPS TESTED NORMAL IAW MM.
EMERGENCY LIGHTS ARE INOP ON SEATS FROM 24 AB TO 33AB. BATTERY LOCATED BEHIND DADO PANEL AT SEAT 29A. REPLACED BATTERY CHARGER UNIT AND BATTERY AND TEST PER MM, CHECKS NORMAL.
EMERGENCY LIGHTS ARE INOPERATIVE ON SEATS FROM 1ST CLASS THROUGH BUSINESS CLASS ON LEFT SIDE. REPLACED BATTERY. EMERGENCY LIGHT CHECKED OKAY.
EMERGENCY LIGHTS ARE INOP ON SEATS FROM 24 AB TO 33AB.
EMERGENCY LIGHT AT SEAT 19JK IS INOP. SECURED CONNECTOR FOR EMERGENCY SEAT LAMP, OPS CHECK NORMAL.
UNABLE TO TRANSMIT OUT ON LT HF RADIO. NO RECEPTION FROM LT HF EITHER. ESTABLISHED HF COMMUNICATION AND SELCALL CHEC. OPS NORMAL.
CENTER BLEED ISOLATION WILL NOT OPEN. CLEANED CONNECTOR ON CENTER ISOLATION VALVE, OPS CHECKED OKAY.
EMERGENCY LIGHTS INOPERATIVE ON SEATS 1A TO 2A AND 6AB THRU 14AB. EMERGENCY LIGHT BECAME VERY DIM. REPLACED BATTERY AT ROW 8A.
NR 4 FWD MAIN WHEEL HAS 1 EA TIE BOLT NUT CRACKED AND BOLT IS LOOSE IN WHEEL HALVES. REPLACED NR 4 FWD WHEEL TIRE ASSY PER MM.
FLAP O-SPEED WARNING AT CRUISE AT 320 370 AND CLIMBING THRU 32.7.5 TIMES. M545 FAULT REPLACED FSCU PER AMM.
MID RIGHT LAV SINK WATER WON'T SHUTOFF. WATER SHUTOFF VALVE FAILED. REPLACED WATER SHUTOFF VALVE TO ENABLE DEFFERAL. REQUIRES NEW FAUCET VALVE OR TIMER, NO TIME TO TROUBLESHOOT. PER MEL DEACTIVATED WATER HEATER AND BOARDED HAND SANITIZER. ADJUSTED HYDRAULIC TIMER PER MM 38-11-06 TASK 824-804. FAUCET OPERATES NORMALLY, CYCLED NUMEROUS TIMES.
LOW GAIN ON SATCOM WITH BITE FAIL & T-P BSU FAULT. CANNOT PLACE CALL BUT SAT WORKS FOR ACARS. REPLACED PORT BEAM STEERING UNIT PER MM 23-25-17 PER MM 23-25-17 AND ACCOMPLISHED INSTALLATION TEST PER MM 23-25-00, OPS CHECKS GOOD.
APU INOP ELECTRICAL. UNABLE TO LOAD GENERATOR. REFER TO MM. APU FIELD OFF LIGHT. DEFERRED PER TOMC AND SEE CF831 FOR PARTS INFO. REPLACED APU GEN FEEDER HARNESS, REFER TO CF0831.
FOUND APU FEEDER CABLE T1 BURNT ON APU GENERATOR NEED TO REPLACE APU GENERATOR DUE TO BURNT FEEDER HARNESS LEADS. REPLACED APU GENERATOR IN ACCORDANCE WITH MM.
LEFT HYD SYS PRESSURE EICAS, RTFL. FOUND NR 6 SPOILER ACTUATOR HOUSING BROKEN. REPLACED ACTUATOR AND LT CASE RET FILTERS. SERVICED LT HYD FLUID. OPERATIONAL CHECKED OK.
DELAMINATED WINDSHIELD 1R IN UPPER RIGHT CORNER. REPLACED 1R WINDSHIELD PER AMM.
DELAMINATED WINDSHIELD 1L IN UPPER RIGHT CORNER. REPLACED WINDSHIELD PER AMM.
OXYGEN PANEL IN ECONOMY NEEDS TO BE RESTOWED. REPACKED O2 MASK PER AMM. ALL OPS CHECK GOOD.
LEFT PACK INOP WILL NOT RESET. REPLACED LEFT FLOW CONTROL CARD IN P50 CARDFILE PER MM, ALSO LEFT FLOW CONTROL VALVE PER MM, PACK OPS NORMAL.
'LT PACK INOPERATIVE' ILLUMINATED ON EICAS. OPERATED NORMAL AFTER 'STANDBY' SELECTED. REPLACED LOW LIMIT VALVE.
FOUND LT PACK FLOW CONTROL VALVE STUCK CLOSED. REPLACED LEFT FLOW CONTROL VALVE, OPS CHECKED GOOD ON GROUND.
EMERGENCY LIGHT IN COCKPIT IS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW AMM 33-51-01. OPS CHECKED GOOD.
EMERGENCY EXIT LIGHT ABOVE SEAT 36AB IS INOPERATIVE. REPLACED LAMP AT SEAT 36AB. OPS CHECKED GOOD.
RUDDER TRIM INTERMITTENT, FLIGHT DIVERTED. REPLACED RUDDER TRIM ACTUATOR PER MM. REPLACED RUDDER TRIM CONTROL MODULE PER MM. OPS CHECKS GOOD.
RT HYD SYSTEM QTY IS 0.02; R HYD QTY EICAS MSG DISPLAYED. SAMC TEXT: WITH RT QTY LOW LIGHT ALSO. TOMC MAINT TEXT: PER CREW, PUMP LOW PRESS LIGHTS DID NOT ILLUMINATE PRESSURE NORMAL. NO SIGNS OF EXTERNAL LEAKAGE. REPLACED HYD QTY MONITOR UNIT PER MM, QTY SYS CKS NORMAL.
RT HF TRANSMISSIONS ARE INOP, WEAK, GARBLED, INTERMITTENT AT (1=CAPT,2=F-O,3=F-OB) STATION. OTHER STATIONS NORMAL. TRIED NEW TRANSCEIVER, NO HELP. REPLACED O/B AUDIO SEL PNL. OP CKS OK.
DUE TO REPORT OF EXTERNAL POWER CONTACTOR NOT OPENING AFTER EXTERNAL POWER WAS DE-SELECTED AND EXTERNAL POWER WAS REMOVED REPLACED EXTERNAL POWER CONTACTOR K114 PER MM. RPL'D EXTERNAL PWR CONTACTOR, CKS OKAY PER MM TEST. RAN ENGINES TO DUPLICATE DF680, PWR WOULD NOT TRANSFER TO ENG GEN'S & UTILITY BUSSES WOULD NOT COME ON. BPCU SHOWS SIGNS ON BOTH LINES, RESET PWR, BPCU DEAD. RPL'D BUSS PWR CONTROL UNIT REF MM, CKS OK PER MM. ** NEED TO RUN ENGINES TO CONFIRM REF SMC4.
HF TRANSMISSION & RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC. AT ALL CREW STNS. (1 = L HF, 2 = R HF) CREW COMMENTS: UNABLE TO XMIT. CAN RECEIVE OK. LONG SIDE TONE WHEN TUNING. COMPLIED WITH MEL. REMOVED AND REPLACED RIGHT HF TRANSCEIVER.
CENTER HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED WITH EICAS AND ADP LOW PRESSURE LIGHT. REPLACED CENTER HYD SYSTEM LOW PRESSURE SWITCH PER MM, OPS NORMAL.
HYD LEAK ON NR 2 ENG FOUND DURING PREDEPARTURE WALKAROUND, FOUND LEAK FROM LT TOP THRUST REVERSER ACTUATOR. SECURED FITTING FOR INTERCONNECT CABLE HOUSING FOR LEFT TOP THRUST REVERSER ACTUATOR. NO LEAKS NOTED.
NR 2 ENGINE PYLON STRUT PLENUM SUPPORT RODS ARE WORN OUT. REPLACED RODS.
RIGHT WING OUTBD DUCT GOING TO ANTI-ICE VALVE ABOVE NR 2 PYLON IS SPLITTING OUTBD OF CLAMP (MKD WITH TAPE). REMOVED DUCT AND SENT TO WELDING SHOP. REPLACED DUCT.
NR 2 PYLON, EVIDENCE OF HYDRAULIC LEAK, INBD SIDE. FOUND HYD PRESS LINE ABOVE NR 2 PYLON AT BULKHEAD FITTING LEAKING MARKED WITH TAPE. SECURED LOOSE 'B' NUT ON HYDRAULIC LINE. RAN HYDRAULICS AND MOTORED ENGINE, NO LEAKS FOUND.
NR 1 ENG HAS HEAVY COAKING AT 12'O'CLOCK. REMOVED 2 EA DRAIN LINES FROM PYLON AND HYD LINE CLUSTER NO BLOCKAGE NOTED. REMOVED PYLON ACCESS PNL 416BR & FOUND NO EVIDENCE OF LEAKAGE. REINSTALLED PNL. REMOVED NR 1 ENG PYLON JUNCTION BOX INSULATION AND COVER FOR ACCESS TO HYDRAULIC 'B' NUTS. FOUND EVIDENCE OF LEAKAGE FROM CASE DRAIN FITTING. CLEANED AREA,TIGHTENED FITTING. MOTORED ENGINE 114813, NO LEAKS NOTED. RE-INSTALLED J-BOX PNL AND INSULATION BLANKETS.
LEFT OVERWING SLIDE EMERGENCY LIGHT AFT OF FLAPS (2ND TO LAST) INOPERATIVE. RELAMPED PER MM, OP CHECKS NORMAL.
EEL LIGHT AT SEATS 35KJ INOPERATIVE. RELAMPED, OP CHECKS NORMAL PER MM.
WHILE ACCOMPLISHING PIMU BITE CHECK FOUND NR 2 ENG EEC CH A FAULT CAT 2 MESSAGE EEC CH A TCA SOL W-A FAIL. TROUBLESHOT REF FIM 71 PIMU MESSAGE INDEX PG64K,PG64L, MESSAGE 354-22 & REF WDM 71-51-14. COMPLETED TO ITEM G INDICATES NEED EEC. REF PTT # 6562008 FOR T-S (VERIFIED 62 OHMS AT TVBCA SOL), REPLACED R ENG EEC AND MADE W-U FOR R ENG EEC IDLE TEST NR 6.
MISSING WINDSHIELD HEAT TERMINAL CAP F/O WINDSCREEN. REPLACED CAP.
LEFT ENG BLEED OFF EICAS. FOUND FAULTED NR 1 ENG PRVC. REPLACE PRVC. RAN ENG PER JRH. ALL BLEED INDICATIONS NORMAL.
WX RADAR FAILURE, RTFL. MESSAGE DISPLAYED. FOLLOWED PROCEDURE IN FM, NO HELP. ATTEMPTED CB RESET, FAIL MESSAGE RETURNED. ACP'D SYSTEM CHECK OF THE WX RADAR, NO SCAN SWEEP AND FAILURE MESSAGE FAULTED THE ANTENNA. REPLACED THE DRIVE ASSY & ANTENNA PER MM. ALSO DUE TO INTERMITTENT INPUT REPLACED THE CONTROL PANEL PER MM. SYSTEM CHECKED OK REF FAULT ISOLATION CHECK. DRIVE ASSY MR43183, CONTROL PANEL MR43155 ANTENNA.
SEAT 6B EEPL LIGHT INOP ACCOUNT WIRING DAMAGED. OK TO CONTINUE PER MEL. RDF-P :EEPL HARNESS ASSY PCN 160-0100 AND EXIT LIGHT P/N BR9644-1. -RDF-P :VERIFIED PART# NEED 566-1162 & POWER AT CONNECTOR. REPLACED LIGHT ASSY FOR EEPL LIGHT OPS CHECK OK.
RT ELEVATOR FAILED PCA BELLCRANK CHECK. FOUND RT ELEVATOR EXCEEDS 1 INCH LIMITS BETWEEN LEFT & CENTER HYD SOURCES. INSPECTED AND ADJUSTED ELEVATOR PCA IAW AMM. ELEVATOR CHECKED GOOD.
NR 2 PYLON, HEAVY COKING AROUND INBD LOWER PYLON HEAT SHIELD AREA. REMOVED CLOG FROM AFT PYLON DRAIN TUBE OUTLET.
RIGHT ENG START VALVE LIGHT DID NOT EXTINGUISH AFTER ENG SWITCH MOVED TO GND. GOT AIR TO ENG. REPLACED STARTER CTR VALVE RT ENG PER MM. ACP CHECK OK. RAN NR 2 ENGINE PER JRH. ALL OPS AND INDICATION NORMAL.
L ENG ANTI-ICE EICAS. REPLACED L ENG ANTI-ICE VALVE PER MM, OPS TEST OKAY.
EICAS MSG ENG ANTI- ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SW ON POSITION 1. TROUBLESHOOT PER MM, REPLACED IAW MM,OPS CHECKED NORMAL.
CAPTAIN'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN VISIBILITY IS AFFECTED. NR 3 LT WINDOW NEEDS REPLACEMENT. WINDOW REPLACED.
1ST OFFICER'S FIXED SIDE-FORWARD WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN VISIBILITY IS AFFECTED. REPLACED NR 2 RIGHT OPENABLE WINDOW PER MM.
FORWARD EQUIPMENT COOLING SUPPLY FAN ON EICAS. REPLACED COOLING FAN, CHECKED GOOD.
RIGHT PACK 'AUTO' TEMPERATURE CONTROL SYSTEM(S) INOPERATIVE. DEFERRED PER SAMC. REPLACED RT PACK TEMP CONTROLLER PER MM. CLEANED ALL CABIN TEMP SENSOR SCREEN. RT PACKS OP NORMAL.
EMERGENCY LIGHTS INOP SEATS 3, 4, 5, 6. FOUND EEL POWER CABLE CUT FROM POWER SEAT UNDER SEAT 3. REPAIRED AND SECURED. OPS GOOD.
UPON DEPARTURE FA REPORTED IFE SYS WOULD NOT WORK, FLIGHT WOULD NOT OPEN. INFORMED TO DEFER ITEM. INSTALLED SC-A. SYS OPS CHECK OK.
EMERGENCY EXIT LIGHTS CONNECTED TO POWER SPLY M1209 DO NOT COME ON WHEN FWD & AFT ATTENDANT TEST SWITCH IS PUSHED, WORKS NORMAL WHEN FLT DECK SWITCH IS ON OR ARMED AND POWER IS OFF. FOUND WIRE W1222-106-22 MIS-PINNED, CORRECTED REF WDM. OP CHECKED OKAY.
GEAR LEVER STIFF. SUGGEST REPLACING MAIN LANDING GEAR SELECTOR VALVE ACCT BINDING, SHUTTER FELT WHEN ISOLATED FROM NLG SEL VLV WHEN OPERATING GEAR HANDLE UP. VLV ON AOG E4252 PART NUMBER 1U1302-1. MAIN LANDING GEAR SELECTOR VLV PER MM.
CREW REPORTS AFTER ENG START, THE APU BLEED VALVE APPEARS TO BE STUCK CLOSED. WITH SW ON, NO DUCT PRESSURE AND APU BLD SW VALVE LIGHT IS ON, WITH SW CLOSED, NO DUCT PRESSURE AND APU BLEED SWITCH VALVE LIGHT STILL ON. CYCLED SWITCH NUMEROUS TIMES AND NO HELP. RETURN TO BLOCK. DEFERRED IN ACC, WITH MEL. REPLACED APU SHUTOFF VALVE PER MM, OPS OK.
EXTREME EFFORT REQUIRED TO RAISE GEAR LEVER TO UP. MUST BE FIXED BEFORE REVENUE FLT. REPLACING LANDING GEAR CONTROL MODULE. NEED 8 BOLTS 926-0380 FOR NOSE JACK FIXTURE. LANDING GEAR CONTROL MODULE HAS BEEN REPLACED. GEAR NEEDS A GEAR SWING PER SFO STATION MANAGER TO VERIFY FIX. ACCOMPLISHED GEAR SWING. GEAR HANDLE IS SMOOTH IN OPERATION FOR EXTENSION AND RETRACTION. NO DEFECTS NOTED.
WEATHER RADAR FAILED. WXR RT WEAK DISPLAYED. INOP PER MEL. REPLACED WXR TRANSCEIVER AS PER MM.
APU BLEED WILL NOT OPEN TO START SECOND ENGINE. UNABLE TO DUPLICATE ON ENG INE RUN AFTER RETURN TO GATE. REPLACED K495 RT BLEED AIR ENGINE START RELAY AS PRECAUTION IAW FIM FAULT CODE. ALSO NOTED DEFECT WITH APU BLEED SWITCH ON 2ND ENGINE RUN. REPLACED SWITCH. RAN ENGINE. OPS NORMAL.
APU VALVE DISAGREE LIGHT DISPLAYED. VALVE CLOSED NORMALLY AND CB PULLED AND COLLARED. APU BLEED WOULD NOT OPEN AFTER STARTING LT ENG. AFTER ACFT RETURNED TO GATE AND LT ENG SHUTDOWN, APU BLEED VALVE OPERATED NORMAL. CHECK APU SHUTOFF VALVE INTERLOCK CIRCUITRY. OTHER POSSIBLE CAUSE: APU BLEED CHECK VALVE. OPS CHECK THIS ITEM WHILE STARTING BOTH ENGS BEFORE CLEARING THIS DF ITEM. FOUND LT ENGINE INDICATION INTERMITTENT AT BLEED SWITCH AND UPPER EICAS ADVISORY MESSAGE, REPLACED THE LT BLEED AIR CONTROL CARD, OPS NORMAL.
LEFT THRUST REVERSER OPENING ACTUATOR INOP. REPLACED OPENING ACTUATOR REF AMM. OPS NORMAL.
CREW REPORTS NO WATER PRESSURE THROUGHOUT ACFT. POTABLE WATER FILL VALVE LEAKING AIR IN CLOSED POSITION. CONTROL ROD DISCONNECTED FROM VALVE. REPLACED BORROWED WATER FILL VALVE IN AFT PIT, NO HELP. FOUND WATER SYS AIR COMPRESSOR INOP. REPLACED POTABLE WATER SYS AIR COMPRESSOR IAW MM. PRESSURIZE THE POTABLE WATER SYS, AIR COMPRESSOR WILL NOT STOP RUNNING. FOUND DAMAGED LINE ON AIR COMPRESSOR. REPLACED LINE, NO HELP. CB FOR COMPRESSOR PULLED AND COLLARED. AIR SUPPLY LINE AT TOP OF WATER TANK BLOCKED. TEMP LINE INSTALLED. REPLACED AIR SUPPLY LINE ON TOP OF AIR TANK. INSTALLED AIR LINE. WATER SYS OPS NORMAL.
FLAPS WILL NOT DEPLOY IN THE ALTERNATE POSITION. REPLACED FLAP ELECTRIC MOTOR PER MM BUT FLAPS WILL STILL NOT DEPLOY. NO PWR ON CONN D2312. SECURED BACK CONN D2312. FOUND FLAP BYPASS VALVE MIGRATED, RESECURED PIN, OPS CHECKED NORMAL.
FOUND CORROSION AT SATCOM LEFT ANTENNA. REPLACED LT SATCOM HIGH GAIN ANTENNA AND FWD AND AFT ANTENNA CABLES ON RT AND LT ANTENNAS. ACCOMPLISHED SATCOM SYS TEST, CHECKED NORMAL.
ACARS NO COMM MOST OF FLIGHT. IAW FIM 23-25-00-101 PARA D(B)UP TO STEP 4 ITEM REPLACED. DID FIND CONNECTORS LOOSE FROM SHIELDS AT HIGH POWER RELAY D2673, D2675. HIGH GAIN SYS LOGS ON FOR APPROX 90 SECONDS THEN SEARCHES AGAIN. CYCLE RESTARTS. HIGH PWR RELAY, PORT BSU, PORT LNA-DIP REPLACED PRECAUTIONARY. LOW GAIN SYS OPS NORMAL. CONNECTORS KN59329M06 PLACED ON PRECAUTIONARY.
SATCOM INOPERATIVE. RESET, NO HELP. SATCOM MENU NOT AVAILABLE ON CDU. HIGH AND LOW GAIN NOT AVAILABLE. REPLACED SATELLITE DATA UNIT PER MM. OPS CHECKED NORMAL.
MAIN BATTERY CHARGER STATUS MESSAGE. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER, MESSAGE CLEARED AND OPS OK.
LT OVER WING FUEL LEAK, FLIGHT DIVERTED. REPLACED LT OVERWING FUEL CAP.
EICAS MESSAGE MAIN BATTERY CHARGER. BATTERY BAD. REPLACED MAIN BATTERY IAW MM.
C HYD SYS MAINT STATUS MSG CAME ON SHORT FINAL. OPERATED C1 AND C2 PUMPS ONE AT A TIME. C2 ONLY PUTTING OUT 2510 PSI. SHOULD BE 2800-3200 PSI. DEFERRED FOR NO TIME. AIR DRIVEN PUMP & C1 PUMP OK. REPLACED C HYD SYS C2 ACMP, NO HELP. SUSPECT PRESS TRANSMITTER SWITCH. PERFORMED CTR SYS INTERNAL LEAKAGE CHECK FOUND INBD AILERON WITH HEAVY CURRENT DRAW, CAPPED LT INBD PCA AND HAD NORMAL CURRENT DRAW COMPARED WITH C-1. REMOVED LT INBD PCA. REPLACED LT IB AILERON ACTUATOR. OPS CHECK GOOD. NO LEAKS. CTR HYD PRESSURE CKS NORMAL
COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY, OPS CKD OK.
RT BLEED INOP NO PRESSURE CYCLED CB'S AND SW NO HELP. POWERED ENG UP TO 63 PERCENT N1, NO HELP. REPLACED NR 2 ENG PRSOV (773288-7-8-10 / 29) AND PRV. BITE TEST BLEED AIR CONT SHOWED PRV FAIL. RAN ENGINE, STILL NO BLEED PRESSURES. REPLACED PRV CONTROLLER. RAN ENG. DUCT PRESSURE NORMAL.
RUDDER TRIM INOP, FLIGHT DIVERTED. ACTUATOR FOUND DEFECTIVE. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED RII INSPECTION OF RUDDER TRIM ACTUATOR INSTALLATION. VISUAL FLT CONTROL MOVEMENT CHKS ACCOMPLISHED. ALL OPS & INDICATIONS NORMAL.
ON RETRACTION GEAR HANDLE WAS VERY DIFFICULT TO MOVE THROUGH TOP THIRD OF TRAVEL. REPLACED MLG CONTROL LEVER MODULE.
ON WALK AROUND NOTED LOUD NOISE COMING FROM APU AREA SUSPECT AIR LEAK AT PNEUMATICS BLEED VALVE. SHUTOFF OFF APU BLEED NOISE STOPPED. SECURED CLAMP FURTHER TROUBLESHOOTING FOUND POTABLE WATER PRESSURIZATION LINE BROKEN FROM APU PNEU DUCT BULK PIT LT AFT SIDE. REMOVED APU BLEED DUCT SECTION IN AREA OF DAMAGED FITTING FOR REPAIR OR REPLACEMENT. (DUCT IS IN SHEETMETAL SHOP.) REPAIRED DUCT. WELDED FITTING IN. REINSTALLED ORIGINAL APU BLEED DUCT AFTER REPAIR AND LEAK CHECK. NO LEAK PRESENT.
LT PACK OFF LIGHT WILL NOT COME ON WITH PACK OFF. CHECKED AND RESECURED LT PACK FLOW CONTROL CARD, PACK OPS NORMAL EICAS AND LIGHT INDICATION SHOWING WITH PACK SWITCH OFF.
FAN COWL HOLD OPEN ROD ON ENG NR 2 O/B SIDE, IS BROKEN AND UNUSABLE. REPLACED NR 2 ENG O/B FAN COWL HOLD OPEN ROD ASSY.
EMERGENCY EXIT LENS COVER LOOSE AT 2R. SECURED LENS ON EMERGENCY LIGHT. OP CHECKED OKAY.
CHRONIC HYD TXF RT & CTR. CONDITION SUGGESTS FLUID XFER VIA ANTISKID SHUTTLE VALVES. REPLACED RT INBOARD SHUTTLE VALVE. NO LEAKS NOTED.
AN 1800 LB FUEL IMBALANCE DURING CENTER TANK PUMP USAGE. AND 20.0 LB REMAINING IN CENTER TANK. REPLACED RIGHT CENTER OVERRIDE PUMP, LEAK CHECKED. NO LEAKS NOTED. OPS CHECKS GOOD.
TWO (2EA) AISLE EEL LIGHTS ABOVE SEATS 2A & 6A ARE INOP. NO VOLTAGE AT LIGHT ASSY'S. WILL NEED SEAT 1A REMOVED TO ACCESS BATTERY CHARGER- POWER SUPPLY TO T-S. ESTIMATE 3 SHIFTS. POWER SUPPLY PCN 563- 1046, 2EA. ADJACENT (OPPOSITE SIDE) AISLE LIGHTS OPERATE NORMAL. REPLACED BATTERY CHARGER (POWER SUPPLY). ACP OP TEST.
RECEIVED MSG, L OIL FILTER STATUS AFT ENG START. NO CONTAMINATION IN C-D'S OR FILTERS. REPLACED MAIN OIL FILTER. RAN ENGINE, NO LEAKS DETECTED. CHIP DETECTORS CLEAN. NEED TO REPLACE DIFF PRESS SWITCH AT FIRST OPPORTUNITY. REPLACED DIFF PRESS SWITCH. NO DEFECTS NOTED.
ELECTRICAL PROBLEMS IN THE CABIN. FOUND AFT CABIN LAV-OCC SIGN L403 BAD. WILL NEED A NEW ONE. ALSO FOUND BROKEN GROUND WIRE HANGING LOOSE IN LAV M1284 DOOR SWITCH. REPAIRED BROKEN GROUND FOR DOOR SWITCH. RELAMPED HANDICAPPED LIGHT SWITCH S11 FOR LAV M1284. FOUND LAV -OCC LIGHT ASSY L402 BAD, WILL NEED A NEW ONE. FOUND ABOUT A DOZEN STIR STICKS. REPLACED BAD LIGHT ASSY.
DOOR 2R O2 BOTTLE LOW PRESSURE. REPLACED O2 BOTTLE.
ADP LOW PRESS LIGHT AND EICAS MSG ON TAKEOFF DURING GEAR RETRACTION & FLAPS 5 TO 1. REPORTED BY CREW. REMOVED AND REPLACED ADP. NO HELP. STILL NEED TO LEAK CHECK, NEEDS FURTHER TROUBLESHOOTING. REPLACED MOD. AIR DRIVEN PUMP AND ADP REG AND SHUTOFF VALVES (3214334-3-33). LEAK AND OPS CHECK NORMAL.
DURING CRUISE, CENTER FUEL TANK REFILLED ITSELF FROM 700 LBS TO 1400. FUEL CONFIG LIGHT LIT. ACCOMPLISHED FQ BITE, FOUND 'CT DENS RESISTOR UNREADABLE'. REPLACED CTR TANK DENSITOMETER.
RT WING NR 7 LEADING EDGE SLAT CLOSURE PANEL DAMAGED. REINSTALLED REPAIRED PANEL. OPS CHECK NORMAL, FAIR GOOD. REPAIRED PER GN-MM 1-0-1-24.
NR 2 ENG ACOUSTIC LINER 8 O'CLOCK POS DAMAGED. NR 2 ENG INNER ACOUSTIC PANEL 8 O'CLOCK POSITION CRACKED 4.5 INCHES FORWARD OF LPC BLADES. REPLACED NR 2 ENG NOSE COWL.
LT OVERWING INFLATION HOSE IS FLATTENED 12 INCHES AT THE SLIDE COMPARTMENT ELBOW. SLIDE REPLACED.
LT OVERWING INFLATION HOSE IS FLATTENED 12 INCHES AT THE SLIDE COMPARTMENT ELBOW. SLIDE REPLACED.
LEFT OVERWING SLIDE COMPARTMENT, DISCONNECT HOUSING IS BROKEN. REPLACED DISCONNECT HOUSING. REINSTALLED LT DISCONNECT CAM ASSY. EXAMINED INFLATION CABLE FOR FREEDOM OF MOVEMENT, CHECKS GOOD.
DOOR L1 SLIDE COMING UNLACED. INSTALLED NEW SLIDE AT DOOR L-1.
LEFT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 4 IS SCORED. INSTALLED NEW LATCH, OPS CHECKS GOOD.
LEFT OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH FAILED EDGE MARGIN CHECK. INSTALLED NEW NR 3 LATCH, OPS CHECKS GOOD.
RT SIDE FUSELAGE DAMAGE FROM STA 1131 TO 1175 STRINGERS 18R TO 20R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPAIR DOUBLER TRIPLER AND FILLER REPAIR.
WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS.
WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS. REPLACED EEL LIGHT STRIP AND COVER.
SECOND OBSERVER O2 MASK MIC WIRE IS FRAYED. *S/D* FOUND MIC WIRE FRAYED. REPLACED 2ND OBS O2 MASK PER MM 35-11-51. AC OK FOR SERVICE.
LT PACK INOPERATIVE - REHEATER INLET DUCT CRACKED. *S/D* SUSPECT IMPROPER INSTALLATION. REPLACED LT PACK REHEATER DUCT PER MM 21-51-21. OP CHECKS NORMAL. AC OK FOR SERVICE.
LEFT ENG BLEED AIR VALVE WILL NOT OPEN. DUCT PRESSURE ON LEFT SIDE IS ZERO. ADVANCED ENG POWER AND STILL NO HELP. FOUND PRESSURE REGULATING VALVE TO BE FAULTY. REPLACED PRV, RAN ENGINE OP CHECKED GOOD. AC OK FOR SERVICE.
REF SMC001 ON EEL STRIP BROKEN, NEW STRIP IS IN PLACE AND WILL REQUIRE SPLICING AND RE-ASSEMBLY OF EEL STRIP CABLE PROTECTIVE COVERS AND CARPET. FOUND LIGHT ASSEMBLY BROKEN. SPLICED IN SECTION OF EEL LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.
FWD EQUIPMENT VALVE EICAS MSG ON LANDING. FOUND OVERBOARD VALVE AND COOLING CONTROL PANEL FAULTY. REPLACED FORWARD OVERBOARD VALVE, AND EQUIPMENT COOLING CONTROL PANEL. OP CHECKS NORMAL. AC OK FOR SERVICE.
EMERGENGY LIGHT L313 AT DOOR IL HAS BROKEN WIRE. LIGHT ASSY LOCATED AT FWD UPPER CORNER OF DOOR FRAME VISIBLE FROM OUTSIDE WITH DOOR OPEN. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REPAIRED WIRE AND OP CHECK GOOD. AC OK FOR SERVICE.
EMERGENCY LIGHT ON FLOOR 1E PLASTIC IS MISSING.
NR 1 ENGINE HAS THE L BLEED OFF EICAS MSG AND L-BLEED OFF LIGHT ON WITH BLEED SELECTED. REPLACED ISOLATION BYPASS CHECK VALVE. FOUND DIRECT SHORT AT PRSOV CONNECTOR. FOUND D22 CONNECTOR ON PRSOV BAD. REPLACED SAME. OPS CHECKED GOOD. REPLACED PRSOV. LEAK & OP CHECKS GOOD.
RTFL DUE TO CENTER HYDRAULIC PUMP PROBLEM. REPLACED HYDRAULIC AIR DRIVEN PUMP. ALSO REPLACED HYD LINES & PUMP MOUNTS. PERFORMED SYSTEM CHKS. OK FOR SERVICE.
ELECTRICAL BURNING ODOR IN MID GALLEY AREA AND AIRCRAFT RETURNED TO BLOCKS. INSP GALLEY AREA AND OVERHEAD AREA FOR EVIDENCE OF BURNING NO OBVIOUS SIGHT OF SMOKE OR BURNING. FIRE BRIGADE PERFORMED HEAT DECTECTOR EQUIPMENT NO SIGN FOUND.NO HISTORY () INSP CHILLERS ALL OK.
DURING EQUIP COOLING TEST, SMOKE LIGHT DOES NOT COME ON AND NO FWD EQUIPMENT SMOKE ADVISORY MESSAGE. RELAMPED SMOKE DETECTOR. OPS CK OK PER JC EQUIP COOLING TEST.
OXYGEN MASK DEFECTIVE AT 2.(1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: O2 MASK INFLATABLE BAND BURST.
BEZEL IS MISSING FROM EEL LIGHT AT ROW 18 BC.
EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE LEFT AISLE.
EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE RIGHT AISLE.
EEL LIGHT INOP LOCATED MID ZONE LAVATORY LEFT & RIGHT AISLES.
RIGHT SIDE BUSINESS CLASS EXIT STRIP LIGHTING ON AND OFF INTERMITTENTLY. PER FLT ATTENDANT, THE RT SIDE IN FIRST CLASS ONLY & AROUND DOOR 1R HAD THE PROBLEM. REPLACED POWER SUPPLY M1552. CHECKS GOOD.
CABIN FLOORBEAM AT BS 368 AND RBL 58 HAS 2 EACH MISDRILLED HOLES, ONE THROUGH UPPER CHORD AND WEB AND THE OTHER IN THE UPPER CHORD RADIUS. CUTOUT DAMAGE IN WEB AND OVERSIZED THE 2 MISDRILLED HOLES. FABRICATED 1 REPAIR ANGLE FOR THE FWD AND AFT SIDE OF THE FLOORBEAM WEB. FABRICATED AND INSTALLED FILLERS.
EEL LEAD WIRE BROKEN. REMOVED AND REPLACED EEL LIGHT BARS PER MM 33-51-10 AND OPS CHECK GOOD PER MM 33-51-00 ON N-R 25692.
RIGHT SIDE EXTERNAL OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. TROUBLESHOT AND FOUND BAD LAMP. REMOVED AND REPLACED LAMP. OPS CHECKS GOOD.
CABIN FLOORBEAM STA 246 VERTICAL STIFFENER AT FWD FACE, RBL 11, CRACKED AT BEND RADIUS. [08-14-07] REMOVED AND REPLACED VERTICAL STIFFENER PER SRM 53-10-51, PARAGRAPH 3. AIRPLANE READY FOR SERVICE. SUSPECT FATIGUE EXACERBATED BY ASSEMBLY PRE-LOAD.
FWD CARGO PIT TORQUE FLOOR GOUGED FWD AND AFT OF PDU 8C, RBL 5, STA 560. [08-14-07] FOUND OUT OF LIMITS. FABRICATED NEW PANEL PER BAC DWR 451T2504. INSTALLED NEW PANEL PER SRM51-40-02. AIRPLANE RETURNED TO SERVICE READY.
RIGHT OVERWING SLIDE CYLINDER LWR INFLATION HOSE IS KINKED AND COLLAPSED. [08-07-07] REPLACED HOSE IAW 20-10-10. SLIDE PROBLEM ROOT CAUSE: SLIDE & INFLATION HOSE ARE IN AN AREA CONTAINING MANY HYDRAULIC LINES & SERVICING ACCESS; SUSPECT HOSE DAMAGED BY SKYDROL CONTAMINATION. SLIDE & AIRCRAFT OK FOR SERVICE.
RIGHTHAND OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH WORN. REMOVED & REPLACED LATCH AND KEEPER.
LEFT OVERWING SLIDE DOOR NR 2 LATCH BINDING. [08-08-07] REPLACED AND ADJUSTED LATCH PER MM25-65-98. DOOR 2 LATCH MOVES FREELY. SLIDE & AIRCRAFT OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SLIDE LATCHES EXPERIENCE FRETTING CAUSED BY VIBRATION & EXCESSIVE CLEARANCE CAUSED BY WEAR.
FWD GALLEY FLOOR AREA, STA 246 AT RBL 72 AREA, BULKHEAD WALL, LOWER FLOOR CHORD CORRODED UNDER SHEAR WEBBING, FWD EDGE. REMOVED DAMAGED SECTION OF CHORD, RBL 49 TO RBL 72. FABRICATED & INSTALLED SPLICE & REPAIR ANGLES.
CREW REPORTS LOSS OF LEFT GENERATOR. [SUP 05-04-07] REPLACED LEFT ENGINE INTEGRATED DRIVE GENERATOR. RAN UP ENG PER JRH 2-6-1, IDG OPERATED NORMALLY. OUTBOUND TRIP DID VERIFICATION TEST AND IDG OPERATED OK. SUSPECT INTERNAL WEAR LED TO FAULTY HERTZ OUTPUT & MISMATCH WITH OTHER A/C GENERATOR.
DOOR 1R SLIDE PRESSURE READS BELOW SERVICEABLE LIMIT. REPLACED R1 DOOR SLIDE PER MM 25-66-01. CAUSED BY SUSPECT SEAL LEAKAGE AT BOTTLE CONNECTION.
EICAS MSG 'LDG GEAR MONITOR' DISPLAYED WITH LDG GEAR UP AND LOCKED. FOUND ALL EXCEPT 4 CIRCUIT CARDS DISLODGED IN PSEU. REMOVED AND REINSTALLED ALL CIRCUIT CARDS.
NR 1 ENG PYLON INBOARD SIDE 2 INCH CRACK OUTER SKIN OUT OF INSPECTION PANEL CUTOUT.
SQUIB TEST ON EMERGENCY ESCAPE SLIDES WILL NOT TEST. REPLACED RIGHT AND LEFT SQUIB BATTERY PACKS PER AMM 25-65-17. SQUIB TESTS GOOD.
DIVERTED TO YBG DUE TO ELECTRICAL ODOR AND FUMES IN FLIGHT DECK. CHK'D FOR BURNED WIRING AND PROBLEMS WITHIN E&E COMPARTMENT. NO EICAS MESSAGE NOTED BY FLIGHT CREW. CLEANED DIRTY OVENS AT FWD GALLEY. CHECKED WIRING AND COMPONENTS IN AREA AND FOUND NO DISCREPANCIES. OP CHECKS OK FOR SERVICE.
BOTH ASPIRATORS STAYED OPEN DURING SLIDE DEPLOYMENT.
LEFT OVERWING SLIDE PACK TRIGGER BROKEN. REPLACED SLIDE. AIRCRAFT RELEASED TO SERVICE. ROOT CAUSE WAS SLIDE PACK TRIGGER BROKEN DURING INSTALLATION.
RIGHT INBOARD AFT FLAP, CENTER HINGE FITTING CRACKED ON OUTBOARD SIDE IN COVE AREA. *S/D* THE RIGHT INBOARD AFT FLAP, CENTER HINGE FITTING, WAS FOUND CRACKED ON THE OUTBOARD SIDE IN THE COVE AREA. REPAIRED FITTING PER 767 SRM 57-53-02.
NR 1 AND NR 2 LATCHES EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED LATCHES.
DIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4 WAS FOUND ATTACHED TO THE AIRCRAFT. THE FIVE FASTENERS ATTACHING FORWARD HINGE ASSY TO THE FORWARD INLET DOOR WERE SHEARED. AFT INLET DOOR ASSY P/N 213T3009-1 WAS FOUND WITH NO VISIBLE STRUCTURAL DAMAGE. THE EIGHT FASTENERS INCLUDING THE COLLARS, ATTACHING THE AFT INLET DOOR ASSY TO AFT HINGE ASSY P/N 213T3108-4 WERE MISSING. BLOCKS AND ATTACHING HARDWARE WERE STILL INSTALLED ON THE AFT INLET DOOR. ACTUATOR WAS REPORTED TO HAD BEEN REPLACED.
FOUND WIRES W298-021-08, W1046-913-08, W1046 -012-10, W1046-028-12. BURNED AT TB 5132 TERMINAL BLOCK INSIDE P37. REPLACED TERMINAL STRIP TB5132 IN P37 PANEL.
RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER.
MAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED.
NR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MIDSPAR WEB.
LEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES.
FLIGHT DIVERTED DUE TO WX RADAR FAILURE. CREW REPORTED WX RADAR INOP. DOES NOT PAINT AND GREEN ARC ON DISPLAY. ALSO, NO GROUND RETURNS. ( THE GREEN ARC IS A FLAT PLATE ANTENNA ANOMALY THAT DOES NOT AFFECT WX RADAR PERFORMANCE.) MAINTENANCE REPLACED THE WX RADAR CONTROL PANEL AND THE WX RADAR SCANNER. THERE HAVE BEEN NO RECURRING PROBLEMS INVOLVING WX RADAR PERFORMANCE.
EMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY.
SMOKE ALARM WENT OFF IN AFT LAV. NO SMOKE OBSERVED AND FLIGHT LANDED UNEVENTFULLY. SUPPLEMENTAL DATA UPDATE THE AFT CENTER LAV SMOKE DETECTOR WAS AT FAULT. THE UNIT WAS REPLACED WITH P/N PU90-461R3 (PCN 563-3542) . THE SYSTEM CHECKED FINE AFTERWARD.
EEL LIGHTING DAMAGED AT RIGHT HAND BUSINESS CLASS GALLEY. REPLACED TWO DAMAGED EEL LIGHTING STRIPS. REPAIRED DAMAGED POWER LEAD AND INSTALLED NEW LIGHTING COVER STRIP.
FORWARD PIT STATION 287 LEFT HAND SIDE, STRINGER 26L TO 29L TEAR STRAP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED
AFT PIT FLOORBEAM T-CAP CORRODED RBL 8, STATION 1197.66. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIRED.
AFT PIT FLOORBEAM T-CAP CORRODED UNDER NUT PLATE STRINGER 33L STATION 1197 + 110. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIRED.
AFT PIT FLOORBEAM T-CAP CORRODED ABOVE STRINGER 36L, STATION 1153. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP.
AFT PIT FLOORBEAM T-CAP LOWER SURFACE HAS CORROSION AT STATION 1197+132 AT STRINGER 33L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.
CABIN C-ZONE STATION 852, LBL 54, UPPER TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM TRANSBEAM SPLICE.
E+E BAY AT STATION 287, STATION 26R END FITTING NEEDS TO BE RE-FABRICATED TO FACILITATE STRINGER REPAIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW STRINGER END FITTING.
STATION 287 RT, FUSELAGE SKIN CREASED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN DAMAGE AND INTERNAL BULKHEAD CHORD ANGLE.
BODY STATION 1131 LBL 35 LOWER STRAP DOUBLER CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRAP.
BODY STATION 347 LBL 88 WL 200 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.
BODY STATION 347 LBL 48-88 T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES.
BODY STATION 852 LBL 33 TRANSBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION AND SPLICES.
PYLON SPAR ANGLE, LEFT AFT SPLICE CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE PLATE.
RIGHT ENGINE SURGED AND STALLED, FLAMES WERE COMING FROM THE FRONT AND BACK AFTER TAKEOFF. REPLACED ENGINE.
ON DESCENT OUT OF 8,000 FEET AUTOPILOT SPD 210, FLAPS 5-WHEN SPEED BRAKE DEPLOYED PAST 1-2 TOWARDS FULL. AC REMAINED WINGS LEVEL, BUT YOKE SHOWED 2 1-2 TO 3 DEG ON STATUS PG RT INBOARD AILERON ALMOST FULLY DEFLECTED DOWN. OK WITH NO SPEED BRAKE. UNEVENTFUL LANDING.
SHORTLY AFTER LANDING GEAR HANDLE RAISED, SHUDDER FELT WITH LOUD ''BANG '' SOUND. *S/D* FOUND TR MLG TRUCK POSITION ACTUATOR HAD INTERNALLY FAILED ON GEAR RETRACTION. REPLACED ACTUATOR.
COMPRESSOR STALL AT 19,000 FEET, 2 ADDITIONAL MOMENTARY COMPRESSOR STALLS ON APPROACH.
EMERGENCY FLASHLIGHT RT SIDE CROSS AISLE FWD OF 15CDE NOT FLASHING. *S/D* REPLACED BATTERY KIT AND TESTS OK.
STRONG BURNING RUBBER SMELL IN FIRST FOUR ROWS OF BUSINESS CLASS. DIVERTED TO PHL. A DETAILED CHECK OF THE AREA WAS ACCOMPLISHED AND NO PROBLEMS WERE FOUND. A SEARCH OF THE AMIS DATABASE HAS BEEN ACCOMPLISHED AND NO FAULTS COULD BE ATTRIBUTED TO THIS EVENT. THE AIRCRAFT HAS CONTINUED TO OPERATE WITHOUT FURTHER INCIDENT.
FLOOR EMERGENCY LIGHT AT SEAT 11 ON RIGHT SIDE INOPERABLE. REPLACED FLOOR EMERGENCY LIGHT, OPERATIONS CHECK NORMAL.
RETURNED TO FIELD WITH NR 2 ENGINE SHUTDOWN, DUE TO LOW OIL QUANTITY. FOUND CHIP DETECTOR LYING IN COWL. CHANGED PROCEDURES TO REQUIRE LOCKWIRE OF THESE CHIP DETECTORS.
SHUTDOWN LEFT ENGINE DUE TO COMPRESSOR STALLS AND LANDED UNDER AMBER ALERT. EIGHTH STAGE BLADE FAILED, DUE TO SEVENTH STAGE INNER SHROUD DOWL PIN LIBERATION.