N67134
Registered owner: UNITED AIRLINES INC, IL (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
Maintenance disclosures
(EA 3830-01422 REV Q) AFT CARGO COMPT. AT STA. 1681.8 BILGE AREA, UPON REMOVAL BLADDER FOUND PLUG SKIN EXFOLIATED. REMOVED AND REPLACED PLATE ASSY-MOUNTING SUMP BLADDER, FLOOR DRA IN AT STA 1690 BTW STRG 29L TO 29R. IAW SRM 51-40-02- 0G0, DWG 417N2715 AND DWG 417N2710.
AFT NR 2 PYLON PAN SKIN AFT INCONEL REMOVAL FOUND ANGLE WITH CRAC. REMOVED PAN SKIN ON NR 2 PYLON FOR ACCESS IAW SRM 51-41 -02-0G-0, REMOVED ANGLE ON PYLON NR 2 PAN SKIN AFT INCONEL IAW SRM 51-41-02-0G-0, LOCATED & DRILLED NEW SUPPORT ANGLE IAW SRM 51-41-05-0G-0 , INSTALLED NEW SUPPORT ANGLE IAW SRM 51-41-02-0G-0, INSTALLED PAN SKIN IAW SRM 51-41-02-0G-0, AMM 20 -11-00-912-001.
RIGHT WING, T/E REAR SPAR WS 313, SKIN PANEL SUPPORT BRACKET CRACKED AND WITH A FASTENER LOOSE. REMOVED DAMAGE BRACKET AT R/H WING THE REAR SPAR BY WS. 3/3 IAW SRM 51-40-02, RECIEVED NEW PART, LOCATED & DRILLED IAW SRM 51-40-05, TREATED AND PRIMED IAW AMM 51-21-04-107-017 & AMM 51-21-14-370-804, INSTALLED THE NEW PART IAW SRM 51-40-02.
FWD CARGO DOOR LOWER SEAL RETAINER LOWER FWD CORNER SUPPORT CRACKED. REMOVED AND RE-INSTALLED SCUFF PLATE FOR REPAIR AT THE WELD SHOP IAW EC/RA 5310-04203 PART 3 PARMANENT REPAIR WITH TRAVELER NR T26/1869222 AND AMM 53-13-02-424-005 ON FWD CARGO DOOR LOWER FWD CORNER.
MAIN DECK LEFT BS 1620 VERTICAL CEILING BRACKET CRACKED, 16274. FABRICATED BRACKET IAW DWG 411N3141 AND SRM 51-40-0 5-0G-0. TREATED AND PRIMED BRACKET IAW SRM 51-20-01-0G- 0.
RT WING TO BODY SPRT ANGLE IS CRACKED AT BS 1040, RBL64, (BEHIND PANEL 198AR). REMOVED CLIP ANGLE AT RT WING TO BODY SUPPORT BS 1040, RBL 64, (BEHIND PANEL 198AR) IAW SRM 51-40-02-0G-0, FABRICATED NEW ANGLE, IAW DWG 149N7553 AND AMM 51-21-14-370-801, AMM 51-26-15-370-801, APPLIED TREAT, PRIMER, TOP COAT IAW AMM 51-21-04-107-01 7, AMM 51-21-14-370-801, AMM 51-26-15-370-801, INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0.
LT MLG STRUCTURE THAT ATTACH 197AL AT BS 1040 HAS ANGLE BRACKET WITH A CRACK. REMOVED ANGLE BRACKET AT LH MLG STRUCTURE THAT ATTACH 197AL AT BS 1040 IAW SRM 51-40-02-0G-0, FABRICATED NEW ANGLE IAW DWG 149N7553 AND SRM 51-40-05-0G-0, APPLIED TREAT, PRIMER, TOP COAT IAW AMM 51-21-04-107-017, AMM 51-21-14-370-801, AMM 51 -21-15-370-801, INSTALLED NEW ANGLE IAW SRM 51-40-02-0G -0.
LEFT ENG EGT INOP AT CRUISE, WORKED IN DECENT PASSING F180. PER CONVERSATION WITH THE CREW, AFTER 4 HRS INTO FLIGHT, BOTH NORMAL & STBY EGT SHOWED 23 DEGREES & GOING THROUGH FL180 WHILE DESCENDING THE INDICATIONS CAME BACK TO NORMAL & REMAINED NORMAL ON LANDING ALL THE WAY TO SHUTTING DOWN AT THE GATE. LT ENG IDLE GROUND RUN CARRIED OUT, EGT INDICATIONS ALL NORMAL.ACFT RETURNED TO SERVICE. FOUND COMPENSATING RESISTOR OUTSIDE OF TOLERANCE PER AMM 77-21-03-705-001-R00. ACCOMPLISHED FUP ON LP 8992594 & FOUND GREEN WIRES IN BETWEEN TC 16 AND TC 17 RESTING ON ENG CASE, ADJUSTED P-CLIPS TO IMPROVE CLEARANCE. REMOVED ENGINE PYLON DISCONNECT PLUG D1010P WITH REF TO WDM 71-51-22-1.1 AND EXAMINED CIRCUIT FROM PINS 6 & 7 TO EGT TERMINAL BLOCK 2. NO FAULTS FOUND. CONNECTOR IN GOOD CONDITION. CONTINUITY CHECK FROM PLUG TO TERMINAL BLOCK CHECKS GOOD. VISUALLY CHECKED CHROMEL/ALUMEL CABLES FROM THERMOCOUPLE AFT SECTION FORWARD TO EGT TERMINAL BLOCK 2 REF WDM 71-51-22-01.1, REMOVED COMPRESSOR FAIRING RT CTR/LOWER PANELS IAW AMM 72-03-01-024-007-R00 & ACCESSED TO INSPECT. NO CABLE DEFECTS FOUND. COMPRESSOR FAIRING RIGHT CTR/LOWER PANELS RE-INSTALLED. REMOVED AND REPLACED EGT COMPENSATING RESISTOR PER AMM 77-21-03-404-707-R00.
RT AC BUSS OFF, FIGHT CREW REPORTED BUSS DROPPED OFF, CABIN WENT DARK AT TIME OF FAILURE AND DID WAS NOT PICKED UP. T/S IAW WDM 71-51-22-1 AND SSM 24-23-02 . CHECKED WIRING FROM RT ENG GCU D2070B TO RT ENG IDG D1396P. ALL WIRING CHECKED GOOD. CHECKED RT ENG IDG CT CIRCUIT & FOUND AN OPEN ON PIN 13 TO 3. WILL REQUIRE IDG REPLACEMENT. REMOVED & REPLACED NR 2 ENGINE IDG IAW 24-11-01. PLACED FULL A/C LOAD ONTO #2 IDG WHILE RUNNING WITH LOAD BEING APPROX 0.70 WITH NO DEFECT NOTED TO RIGHT A/C BUS OFF OR LOAD SHEDDING ISSUES. OPS AND LEAK CHECK GOOD. REF L/PS 8010638, 8010648, 8010671, 8001666 FOR ALL WORK RELATED TO WIRINGS AND CONNECTOR. NO BPCU FAULTS NOTED. IDT ACP'D FOR INSTALLATION OF NR 2 IDG IAW REQUIREMENTS OF GMM 09-10-15.
DURING APPROACH, TE FLAP DISAGREE BETWEEN FLAPS 25 TO 30. RETRACTED TO 20DRG GA AND EICAS CLRD INSPECTED LEADING EDGE AND TRAILING EDGE FLAPS NO DEFECTS NOTED. NO EICAS MESSAGE ON ARRIVAL.FLAPS OPERATE NORMALLY HYDRAULICALLY AND ELECTRICALLY. PERFORMED FSEU BITE FAULT 303 NOTED . PERFORMED TEST OF THE POSITION INDICATING SYSTEM FOR THE TE FLAPS IAW TASK 27-58-00-705-001REV -. NO DEFECTS OR FAULTS NOTED. ALL FSEU BITE PASSED FIM 27-51-FAULT TREE 805 T/S PER FIM.
NUMBER 2 ENGINE VIBRATION REACHED 2.6 DURING CRUISE AT FL350, AMBER N1 CONDITI ON. RAN QRH, MAGNETIC CHIP DETECTORS INSPECTED, NO DISCREPENCIES FOUND IAW FIM 71-05, FAULT TREE 808 & AMM 79-00-00-216-001-R00. FOUND ECS MSG RT ENG BB VIB. & ON PERF/APU PAGE FOUND VIB. PERFORMED AVM RT BITE PROCEDURE IAW FIM 77-31-00/101. FOUND NO FAULTS, UNABLE TO PERFORM OIL FILTER INSPECTION DUE TO PRESSURE & SCAVENGER FILTER NONE AT HNL IAW FIM 71-05, FAULT TREE 808. R & R SCAVENGE OIL FILTER IAW AMM 24-11-02 & PRESSURE OIL FILTER ELEMENT IAW AMM 79-21-07. ALSO PERFORMED TEST 2 FOR LEAK CHECK. LEAK CHKD GOOD. ENGINE NR 2 PLATE SEAL FOR UPPER HP3 BLEED VALVE CUP R & R. PERFORMED ENGINE NR 2, TEST 6 - VIBRATION TEST SURVEY IAW AMM 71-00-00-715-327-R03. ENGINE NR 2 AT 1.73 EPR, N1 VIB WAS 1.1, N2 VIB WAS 0.4, N3 VIB WAS 0.2, & BROADBAND VIB WAS 1.1. NO FURTHER MAINTENANCE IS REQUIRED PER AMM 71-00-00-715-327-R03. OK TO SERVICE.
FOUND EMERGENCY EXIT PATH LIGHT PANEL BROKE ON ROW 32 ABC. ADJUSTED EMERGENCY EXIT PATH PANEL AS REQ, OPS CHECK GOOD. OK TO CONT.
EMERGENCY LIGHTS LH WING EXIT FOUND LIGHT NOT ILLUMINATING REPLACED 2 BULBS PN 1317 REF 33-50-00.
4L DOOR WILL NOT ARM, DOOR 4L GIRT BAR AFT SENSOR COVER FOUND LOOSE, RESECURED. DOOR 4L SLIDE ARMING OPERATION TEST CARRIED OUT SATIS IAW AMM: 25-66-00 REV 137. LMC APPROVED TO REINSPECT L4 DOOR AFT GIRT BAR PROX SWITCH COVER FOR SECURITY. L4 DOOR AFT GIRT BAR PROX SWITCH COVER FOR SECURITY.DOOR 4L SLIDE ARMING OPERATION NORMAL .REF AMM: 25-66-00.OK FOR SVC AT THIS TIME.
4L SLIDE LIGHT NOT ILLUM INATING WHEN DOOR IS ARMED. FOUND GIRT BAR SLIDER PROXIMITY SWITCH COVER LOOSE. SECURED THE PROTECTIVE COVER TO DOOR CUTOUT AND THRESHOLD IAW AMM 20-30-01-992-002. SLIDE ARMS WITH ARMED LIGHT ON.
DUE TO DOOR SLIDE AT 2L BEING SLOW TO INDICATE WITHIN THE GREEN BAND REPLACE THE 2L SLIDE IAW 25-66-01-401 CARRIED BY ELB REMOVED AND REPLACED L2 DOOR SLIDE PER AMM 25-66-01-404-044.NO FURTHER DEFECTS NOTED.ALL TESTS NORMAL AT THIS TIME. C/W RII INSPECTION OF L2 DOOR SLIDE, NO OBVIOUS DEFECTS NOTED AT THIS TIME.
EQUIP COOLING OVERHEAT LIGHT ON SWITCH STATUS MSG EQPT CLG FAN, FOUND CB FWD EQUIP COOLING SUPPLY FAN TRIPPED ,PUSHED BRAKER TRIPPED AGAIN .ALTN SWITCH WORKS OK. TRIPPING CB, MULTIPLE SYSTEMS ON C-B AND AN ELECTRICAL ODOR IN FLIGHT DECK UNLOCKED FOR SIGN OFF. REMOVED AND REPLACED EQUIP. COOLING FAN #1 REF AMM 21-58-06-414-007, SYS OPS CHK GOOD, NO MSGS
SPOILERS CAUTION MSG DURING DESCENT POWER IDLE. SPOILERS DEPLOY ED WITH SLIGHT BANK RIGHTBITE OF SPOILER CONTROL MODULE 1, 2, AND 3 LEFT ALL SHOW SB LVDT FAULT, THAT ITS A HARD FAULT, AND ACTIVE. FLIGHT PHASE WAS ON GROUND. ALL 3 LEFT SCM'S FAULT D873, REF FIM 27-09 FAULT TREE 807 FOR FAULT D873 WHICH SUGGESTS REPLACING LVDT ATTACHED TO CONNECTOR FOR 3L SPOILER. ALL 3 SCM'S ON RIGHTSIDE SHOW NO FAULT. SMC 2 ALSO SHOWS SPOILER SHUTDOWN, CURRENTLY NOT ACTIVE, PHASE ON GROUND. REF FIM 27-09 FAULT TREE 807. SEE PHOTOS ATTACHED FOR SCRRENSHOT OF FIM, NOT TO BE USED AS OFFICIAL DOCUMENT BUT AS REFERENCE ONLY. LVDT MFG# H913A M&E# 19-2762-9-9001. AVAILABLE RON HOLD TT 1722754. BUNDLE ROUTING BEFORE REMOVAL PICTURES RANG OUT WIRES FROM D00639B PINS K4 AND K5 TO D00873 PINS 3 AND 5, WIRES CHECKED GOOD. RANG OUT SECONDARY COIL OF LVDT FOUND 435 OHMS, SAME AS NEW LVDT. CHECKED INDUCED VOLTAGE THROUGH FULL SPEEDBRAKE HANDLE RANGE OF MOTION, FOUND 1 VAC AT FULL DOWN AND ADD EMP:U371177 8.4 VAC AT FULL EXTEND POSITION. REF WDM 27-61-13, 27-61-17 AND 27-61-18, SSM 27-61-01. REMOVED AUTO-SPEEDBRAKE MECHANISM REF AMM 27-62-02-022-008, UP TO AND INCLUDING STEP 2.H.(5). NEXT STEP 2.K. REMOVAL OF SPEEDBRAKE LVDT. COMPLETED REMOVAL OF SPEEDBRAKE LVDT REF AMM 27-62-02-022-008. TERMINATED PINS ON NEW LVDT REF SWPM 20-61-11 AND BEGAN TRANSFERRING CONNECTORS FROM OLD LVDT TO NEW LVDT DUE TO PARTS NIS AT ORD COMPLETED TRANSFER OF CONNECTORS AND ROD ENDS TO NREF LP 5314556 FOR CORRECTIVE ACTION.
DOOR 2L WILL NOT DISARM MEL REQUESTED. APPROVED MEL 2566S COMPLIED WITH MX PROCEDURE, DOOR VERIFIED ARMED/GIRT BAR ENGAGED. SLIDE ARMED LIGHT DEF TO MEL. WITH SLIDE DISARMED, LIGHT STAYS LIT VERY DIM. *DM* SUGGEST AMM TASKS SYSTEM TEST 52-11-25-735-024 AND ADJUSTMENT 52-11-25-825-001. DOCUMENT ACTIONS COMPLETED. T/S DOOR 2 L DISARMED LIGHT, FOUND SLIDE LIGHT START FLICKERING ON AND OFF WITH DOOR HALF CLOSED SUSPECT WIRING PROBLEM, OR BAD SOCKET, WILL NEED AVIONIC SUPPORT, TO CHECK WIRING AND POWER TO THE SOCKET, MEL REMAIN FOR FURTHER T/S. FOUND ANNUNCIATOR TERMINAL TOUCHING GROUNDED SURFACE. CLEARED ANNUCIATOR FROM OBSTRUCTION, NORMAL OPS. OK FOR SERVICE. REF 757-2 WDM 25-66-11
DOOR 2L SLIDE PRESSURE GAUGE NOT IN GREEN. PRESSURE IS WITHIN LIMITS AS REF IN AMM REFERENCE: TASK 25-66-01-206-041NO. 1, 2, OR 4 PASSENGER DOOR ESCAPE SYSTEM CHECK. OK TO CONTINUE.
SEAT TRACKS - LEFT / OUTBOARD - CORROSION FOUND BETWEEN STA. 1080 AND STA. 1140 FABRICATED AND INSTALLED SEAT TRACK SECTION P/N 144N5021-4 REF DWG 144N5021 AND DWG 144N5001.SFR #3849957.
AFTER PUSH HAD A SMOKY ODOR IN CABIN MAKERS IN USE AND OVENS OFF. NO VISABLE SMOKE REPORTED, ODOR OF SMELL DISSAPATED WHEN CABIN DOOR OPENED. DEBRIEFING FROM FLIGHT CREW. ODOR OF ELECTRICAL BURNING OCCURED IN ALL AREAS OF PASSENGER CABIN DURING PUSH BACK OFF GATE. BOTH ENGINES OFF, APU ON, BLEED ON, PACKS ON. COULD NOT SMELL ODOR IN COCKPIT UNTIL DOOR OPENED. FLIGHT ATTENDANTS REPORT COFFEE COMPLIED WITH AMM 05-51-58-910-801-C1 SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDITIONAL INSPECTION FOUND RT RECIRC FAN C/B POPED UNABLE TO RESET SEE L/P 3555011 FOR CORRECTIVE ACTIONS. R & R R/H AIR RECIRCULATION FAN IN REFERENCE WITH AMM 21-25-01. OPS CHECK GOOD. AND AS PRECAUTIONARY REPLACED HEPA FILTERS IN REFERENCE WITH AMM 21-25-02. OK TO CONTINUE
COCKPIT AC AIR SMELLS LIKE DIRTY CARPETS. BA D. REF FIM21-00 TASK SUPPORT, FOUND ENGINE #1 OVER SERVICED WITH OIL, SUSPECT SMELL DUE TO OVER SERVICING OF ENGINE, RAN ENGINE, NO ABNORMAL SMELLS NOTED, OK FOR CONTINUED SERVICE.
DOOR ARMED LIGHT ON DR 4L WENT OFF DURING FLIGHT. WAS ILLUMINATE D ON GROUND. REMOVED BOTTLE CAP FROM GIRT BAR ATTACH FITTING. DOOR 4L OP CK GOOD.
28C EMERGENCY ROW LT HANGING FROM HARNESS NEEDS SECURED RESECURED LIGHT, OPS CHECK GOOD, OK TO CONTINUE.
EMER LIGHT NEAR AFT DOOR R NOT ON DURING TEST RELAMPED 767 BULB. WORKS OK NOW.
CABIN ALT WARNING AT FL 380. CAB ALT INDICATED + 10000FT. OUT FL OW VALVE SHOWED FULL CLOSED. WHILE PERFORMING OUTFLOW VALVE TEST FOUND VALVE MOVEMENT ERRATIC WHEN COMMANDED. SUGGEST REPLACEMENT OF OUTFLOW VALVE PER 21-31-03-402-010. REMOVED AND REPLACED CABIN PRESSURE OUTFLOW VALVE. REF AMM DURING EXCESSIVE CABIN PRESSURE LEAKAGE TEST AMM FOUND CABIN AIR SUPPLY CHECK VALVE BOOT IN LEFT PACK 21-31-03-402-010. OPS NORMAL. R & R PRESSURE RELIEF VALVE UP TO STEP F (9) REF. AMM 21-32-01-402-009. LOWER RELIEF VALVE PASSED TEST REF. AMM 21-32-01-702-38. PERFORMED POSITIVE PRESSURE RELIEF VALVE TEST ON UPPER RELIEF VALVE. TEST PASSED.
IN FLIGHT AFTER TAKEOFF LEFT ENG OVHT WARNING TEST. TEST GOOD. LOCKING PG - MX TO CONTACT TOMC TO CLEAR FOUND NUMBER ONE ENGINE, INBOARD THRUST REVERSER, HYDRAULIC, HIGH ENGINE POWER RUN PERFORMED BY (R. BLASCHKE #093935) FAULT FLEXIBLE LINE. CHAFING ON NUMBER THREE FIRE DETECTION ELEMENT. NOTED WAS "L ENG OH LP2". REQUIRES MORE TROUBLESHOOTING. ADJUSTED FLEXIBLE LINE. NOW HAS SUFFICIENT CLEARANCE. FOUND NUMBER THREE FIRE DETECTION ELEMENT OK. PREFORMED ENGINE FIRE, UNLOCKED FOR MAINTENANCE TO CLEAR. REMOVED AND REPLACED M10276 LOOP 2 OVERHEAT CARD REF AWM PARTS UPDATED 26-11-03-101. PRESSURED UPSTREAM TO PSROV REF AMM 36-11-09-782-030-001. FOUND HIGH STAGE VAVLE LEAKING. REMOVED AND REPLACED #1 ENG NACELLE FIRE LOOP IAW AMM OVERHEAT WARNINGS DURING ENTIRE ENGINE RUN. 26-11-01-400/000-801. PERFORMED FIRE LOOP TEST IAW AMM 31-51-00. OPS CHECK GOOD. PARTS USED: 1087333,QTY :1 ADD EMP:U ROTABLE PARTS CHANGE WAS INDICATED - TT # 1087333 SN OFF 0134 RAN #1 ENG AT 1.54 EPR AND 90% N1 FOR TWO MINUTES AND NO OVERHEAT WARNINGS WERE INDICATED. ALSO COMPLETED BLEED SHIFT TEST TO FIND OUT BLEED SHIFT POINT AND RAN ENGINE FOR THREE MINUTES WITH HIGH STAGE AIR JUST BEFORE BLEED SHIFT. NO ADD EMP:U104298 DETECTOR, NACEL OFF 19-2611-9-9001 0134 ON 19-2611-9-9001 0480 UPDATED PART TRANSACTION FOR CARD ME 75-2611-9-9001. SN ON 8624. SN OFF 13542 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1514397 SN OFF 3542 IPC REFERENCE # 26-11-52-01B . REF LOG PAGES 5039164 5035159 5027914. REMOVED &
DOOR 2 L LOUD SQUEAL DURING CLIMB TO CRUISE FL310 FOUND DIRT BUILDUP ON LOWER DOOR SEAL. CLEANED DEBRIS FROM LOWER DOOR SEAL. INSPECTED DOOR SEAL IAW AMM 52-09-01. NO RIPS OR TEARS NOTED
R FWD ENTRY DOOR EICAS ON THEN FLASHES ON OFF WITH A/C MOVEMENT FAS SAY HNMDLE MOVING THERE ISNT MUCH OVER CENTER FORCE FELT. PERFORMED A VISUAL INSPECTION. FROM THE OUTSIDE THE DOOR AND HANDLE ARE FLUSH . FROM THE INSIDE THE IS NO DEBRIS IN OR AROUND THE FRAME. CREW REPORTED THAT THE HANDLE WAS COMING UP AND HITTING THE DOOR KNUCKLE KNOCKER. WHEN OPENING THE DOOR FOUND DOOR HANDLE UNLATCHING TORQUE LOW. EXTENDED LOWER GATE PUSHROD TO ACHIEVE SERVICEABLE UNLATCHING TORQUE. NO EICAS MSG NOTED WHILE DOOR CLOSED AND LATCHED. REF AMM 52-11-00-825-001. C/W GMM RII, HANDLE TORQUE WITHIN LIMITS NO FURTHER MAINTENCE ACCOMPLISH
UPON RELOCATION OF THE OVERHEAD BIN DIVIDER FOUND THAT THE LIFE RAFT LOCATED IN OVERHEAD BIN AT 11ABC AREA TO BE UNRAVELED AT THE SURROUNDING SEAM. SUPPORT TASK NSA EMX N/R 00153. REMOVED AND REPLACED LIFE RAFT IN OVERHEAD BIN OFF P/N 63800-103 OFF S/N L5372 ON P/N 63800-103 ON S/N L5661 IAW B757-200 AMM 25-64-00. DATA WAS TRANSCRIBED FROM NSA EMX NR 00153, AND HANGAR NR 7002979, WORK ACCOMPLISHED
DURING SCHEDULED PARTS CHANGE FOR PART NUMBER 75-2561-9-0003 S/N 554 LEFT OFFWING EVACUATION SLIDE RELEASE CABLE NOT HOOKED UP. SUPPORT TASK NSA EMX N/R. 00169. REMOVED AND REPLACE LEFT OFF WING EVACUATION SLIDE IAW AMM 25-65-01. OFF P/N D31393-109 OFF S/N 0554. ON P/N D31393-109 ON S/N 1449RP. DATA WAS TRANSCRIBED FROM NSA EMX NR 00169. AND HANGAR NR 7000292, WORK ACCOMPLISHED
C HYD QTY STATUS MSG AT FL370 1 HOUR FROM LAN DING. FOLLOWED CHC KLIST ISOLATED SYS. .43 RF FOUND RETURN LINE BETWEEN RT CTR PUMP AND EMP CASE DRAIN DUAL FILTER MODULE LOOSE. TIGHTENED FITTING PER AMM 29-00-98. SERVICED SYSTEM TO FULL PER AMM 12-12-01. LEAK CK GOOD. ADD EMP:118592
WASTE DISPOSAL AFT LAV M - TOILET DOES NOT FLUSH AND RINSE SERVICED LAVS. OPS CHECK GOOD
L/H CREASE BEAM INNER CORD STA 755 TO 767 HAS CORROSION REF FLEE T CYCLE LOG PAGE 9805470. LOG PAGE CREATED FOR ESFR ONLY, SEE FLEET CYCLE L/P 9805470 FOR DETAILS OF WORK ACCOMPLISHED. REPAIRED INNER CHORD PER SRM 53-00-13-2R-1 REPAIR 1. LOG PAGE FOR ESFR ONLY
HEAVY CORROSION ON FLOOR DECK JUST FORWARD OF 1720 BULKHEAD FROM RBL 4.5 TO LBL 25. THIS LOGPAGE IS FOR ESFR TRACKING AND SUBMISSION ONLY. SEE FLEET CYCLE LOGPAGE 9803781 FOR WORK PERFORMED. COMPLETED ESFR FORM, SFR#1027819 DUE TO MAJOR REPAIR OF AFT FLOOR DECK REF SRM 53-60-51-2R-17 REPAIR 17.
PDA 1 LP 6301347, #2 ENGINE, INBOARD PYLON PANEL DEPARTED AIRCRAFT ON LANDING @ RSW. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSTALL NEW PANEL INSTALL NEW PANEL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSTALL PANEL, CALL TOMC WELCH, JAMES (V926186) NEW PANEL INSTALLED REF IPC 54-53-01-05A ITEM 60. ALSO REF LP 6301347 MAC RELATED WORK ORDER 000000003008568 AND PRTR MAC METER INITIATED FOR WITH VENDOR ID V926186 WELCH, JAMES (V926186) NEW PANEL INSTALLED REF IPC 54-53-01-05A ITEM 60. ALSO REF LP 6301347 ADD EMP:V926186
FLIGHT CREW REPORTS AT 200'' AFTER TAKEOFF #2 ENGINE EGT RED EXCEEDANCE (931 DEG C) FOR 22 SEC FOLLOWED BY "R ENG OVHT" CAUTION FOLLOWED BY #2 ENGINE FIRE WARNING. FIRE HANDLE WAS PULLED, FIRE WARNING LIGHT EXTINGUISHED AND OVERHEAT CAUTION LIGHT OUT. BOTTLE WAS NOT DISCHARGED. PER ENG EXCD STATUS PAGE - #2 ENG WAS 932* FOR 29 SECONDS PER UAL ENGINEERING CLEANED ,INSPECTED, REPAIRED AND REPLACED AL L REQUIRED COMPONENTS ON NO.2 ENGINE AND PYLON IAW ECRA 5450-025 55 REV -, ECRA 0551-01094 REV - , AND ECRA 7200-05234. THIS IS T RANSCRIBED INFORMATION RECORDED ON STSAA PAPER N/R 0057975
CUSTOMER REQUEST NO ENG PYLON HAS HEAT DAMAGE AT O/B SKIN JUST A BOVE T/R TO THE KEVLAR HEAT SHIELD (96-17) REF N/R 0058000 ACCOMPLISHED ECRA 5450-02555 REV- INTERIM REPAIR ON NR 2 PYLON O/B SIDE SKIN. WORK ACCOMPLISHED AND INSPECTED.
L4 INNER SKIN HAS MULTIPLE CRACKS AT UPPER HINGE AREA ABOVE KNUCKLE BUSTER ASSEMBLY. FOUND CRACKS OUT OF LIMITS IAW SRM 52-10-01-A1 L=.90, L =.65, L=.70. CUT OUT DAMAGE AND ACCOMPLISHED ECRA 5210-03004 REV - PM L4 DOOR INNER SKIN UPPER HINGE AREA. THIS IS TRANSCRIBED INFORMATION ACCOMPLISHED AND RECORDED.
DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 1400 ABOVE STR 25L. AFT CARGO FRAME UPPER FLANGE DENT AT STA 1400 S-25L FOUND OUT OF LIMITS L=3.0, W=.85, D=.052 IAW SRM 53-00-07 FIG 101. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07-R5.
LE SLAT DISAGREE LITE CAME ON GOING INTO LIH FOLLOWED QRH AND DI VERT TO HNL RAN FLAPS SLATS SEVERAL TIMES ON GRND CKS GOOD PERFORMED FSEU BITE NO PRESENT LEG FAULTS AND NO FAULT HISTORY A/C IS OK FOR SERVICE
AMBER SPD LIM INDICATION ON BOTH ADI. VNAV WILLNOT ENGAGE. PERFORMED INIT, DUMPED, NO PROG/ALT LIMIT INFO. PERFORMED MCDP REVIEW AND TEST, NO FAULTS IAW 22-02-00-810-801-00 1. STALL WARNING TESTED IAW 27-32-00815-804-004. NO FAULTS. REMOVED AND REPLACED LEFT FMC AS A PRECAUTION. CROSSLOADED SOFTWARE AND CHANGED FF/DRAG FACTOR.IAW MM 34-61-01-024-001-002, 34-61-01-024-005-002, 34-61-00-342-009-004, AND 34-61-00-342-020-004
SMOKE FROM OVEN. REMOVED AND REPLACED AFT GALLEY OVEN IAW AMM 25-34-00. OPS CHECKED GOOD.
SEAT 20A EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.
EXIT SIGN PANEL ABOVE WINDOW EXIT IS NOT ATTACHED. SECURED THE SIGN.
INFLIGHT, BOTH LEFT AND RIGHT COMMS FAILED TO TRANSMIT, COULD RECEIVE. EMERGENCY DECLARED. R & R THE FIRST OFFICER'S PTT YOKE SWITCH WHICH WAS FOUND STUCK AND CAPTAIN'S AUDIO PANEL, ALSO R & R THE AUDIO ACCESORY UNIT, ALL OPS CHECKED GOOD IAW AMM 23-12-02, AND WDM 23-51-21.
L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE EXTERIOR EMERGENCY EXIT LIGHT AT L1 DOOR. OPS CHECKED GOOD.
R4 DOOR LINER CLIPS, THREE EACH, AT STATION 1681 ARE RUBBING INTO FRAME CAUSING GOUGES, BETWEEN STRINGER 18 - 20. BLENDED OUT DAMAGE & INSTALLED REPAIR DOUBLER IAW ECRA 5310.
DURING AGEING ACFT INSPECTION, DENT WAS FOUND ON A PREVIOUS CATEGORY B REPAIR & TOP FASTENER IN LOWER CTR SHEAR TIE AT STATION 620, BETWEEN STRINGER 15L & 16L, NO DOCUMENTATION COULD BE LOCATED ON THIS REPAIR FROM RECORDS REPORT. CUT OUT DAMAGED AREA OF SKIN & STRINGER, INSTALLED REPAIR P CONT, REQUIREMENTS REF ECRA 5330-05534 PART 1D, ECRA 5330-0553 PART 1 A - C. INITIATED DIP TO ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 46,400 TOTAL AIRFRAME FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 39,400 TOTAL AIRFRAME FLIGHT CYCLES FOR THE INSPECTION.
AFT CARGO DOOR DENT LOCATED 12" FROM BOTTOM & 18" FROM AFT SIDE, IS OUT LIMITS IAW SRM 52-30-01. DENT LOCATED ON TOP OF FRAME. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLER IAW SRM 52-30-01 REPAIR 4. INITIATED DIP TO PERFORM LFEC INSPECTION AT 37,500 TOTAL DOOR FLIGHT CYCLES FROM DATE OF DELIVERY.
EVIDENCE OF CRACKED FRAME, ACFT DISTRIBUTION RAIL ATTACHMENT BRACKET AROUND INBD RIVET, AT STATION 760L. MARKED CUT OUT DAMAGE FRAME SECTION & INSTALLED REPAIR DOUBLER IAW ECRA 5310-06731 PART 1. INITIATED DIP TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE THE ACFT REACHING 36,000 TOTAL FLIGHT CYCLES.
CABIN FRAME STATION 1640, AT UPPER L1 DOOR ARE WORN. INSTALLED REPAIR IAW ECRA 5310-06722 PART 1 STEPS 1 - 18.I.
CABIN FRAME STATION 1640, AT UPPER R1 DOOR AREA WORN. REPAIRED IAW ECRA 5310-06723, STEPS 1 - 17.
FORWARD CARGO CEILING AT STATION 600, RBL 45,5, STRAP CRACKED. REPAIRED FWD CARGO CEILING STRAP IAW ECRA 5310-06730.
FORWARD CARGO CEILING STRAP CRACKED, STATION 720, LBL25. REPAIRED STRAP IAW ECRA 5310-06729.
CABIN INTERNAL STRUCTURE FRAME CRACKED AT FASTENER LOCATION WHERE A/C DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME AT STATION 1580, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DIP TO INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST & AT INTERVALS OF 12,000 FLIGHT CYCLES THEREAFTER.
CABIN AFT WET ENTRY FLOOR STRUCTURE, FLOORBEAM UPPER CAP HAS AREAS OF CORROSION AT STATION 1640 FROM LBL 2 TO LBL 8. CUT & REMOVED DAMAGED SECTION OF UPPER T CHORD ON FLOORBEAM. FABRICATED & INSTALLED REPAIR IAW ECRA 5310-06716 & SRM 53-00-51 REPAIR 10.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1520, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DIP TO RE-INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1480, BETWEEN STRINGER 8L & 9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1540, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DIP TO RE-INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST & AT INTERVALS OF 12,000 FLIGHT CYCLES THEREAFTER IAW SRM 53-00-07 REPAIR 1 TABLE 203 ZONE 3.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1520, BETWEEN STRINGER -8L & -9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07, REPAIR 1. INITIATED DIP TO RE-INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST & AT INTERVALS OF 12,000 FLIGHT CYCLES THEREAFTER IAW SRM 53-00-07 REPAIR 1 TABLE 203 ZONE 3.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1580, BETWEEN STRINGER -8L & -9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07, REPAIR 1. INITIATED DIP TO RE-INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST & AT INTERVALS OF 12,000 FLIGHT CYCLES THEREAFTER IAW SRM 53-00-07 REPAIR 1 TABLE 203 ZONE 3.
CABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1540, BETWEEN STRINGER 8L & 9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DIP TO RE-INSPECT REPAIR 12,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST & AT INTERVALS OF 12,000 FLIGHT CYCLES THEREAFTER IAW SRM 53-00-07 REPAIR 1 TABLE 203 ZONE 3.
FLOORBEAM AT STATION 365, RBL-10, FWD FLANGE HAS CORROSION ON UPPER & LOWER SIDES. COMPLETED INSTALLATION OF REPAIR ON CABIN FLOORBEAM, STATION 365, RBL-10, FWD FLANGE IAW SRM 53-00-51 REPAIR 5.
Z ANGLE AT L2 DOOR HAS CORROSION. R & R Z ANGLE AT L2 DOOR IAW SRM 51-40-02.
FOUND GOUGES STA 647, STR 28 ACCOMPLISH A PERMANENT REPAIR IAW ECRA 5330-03686 REV A.
T/E FLAP DISAGREE ON FINAL APPROACH, RAN QRH AND LANDED FLAPS 20, TROUBLESHOT IAW FIM 27-51-00-815-805 AND 27-81-00/101, FIG 10H BLOCK 2 ALSO PERFORMED NORMAL OPS CHECK SEVERAL TIMES. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME. ACFT OK TO CONTINUE.
SUPPORT TASK- EA 4700-01015 OP14 FIG 19 STEP 3 AND 4 2 COUNTERSINK FASTENERS UNDER BRACKET P/N 012N0067-8 HAS A KNIFE EDGE CONDITION REPAIRED REF EC/RA 5300-01344 PLACED ON DIP INSPECT SKIN REPAIR PER EA 5300-01344 PRIOR TO 50,000 FLT CYCS AND REINSPECT REPAIR EVERY 3,000 FLT CYCS THEREAFTER. ACCOMPLISH INSPECTION OF THE SKIN DOUBLER REPAIR, PER THE REQUIREMENTS IN ECRA 5300-01344 REV C, PART 2, PRIOR TO 50,000 TOTAL FLIGHT CYCLES AND REPEAT EVERY 3,000 FLIGHT CYCLES THEREAFTER.
CLIMBING OUT OF 10000 FT, STRONG ELECTRICAL SMELL THROUGHOUT AIRCRAFT CABIN. NO C/B POPPED, 45 MINUTES LATER SMELL WAS ON FLT DECK. COFFEEMAKERS NR 415 & 416 BREWED ONE POT, THEN BREWERS STOPPED WORKING WHEN SMELL WAS DETECTED IN COCKPIT. PERFORMED VISUAL INSP OF CABIN PER TASK 05-51-58-910-801. FOUND AFT GALLEY PWR CONNECTOR LOOSE & GRD WIRES LOOSE FOR BOTH 415 & 416 COFFEEMAKERS. TIGHTENED ALL. RAN ENGS AND PACKS FOR EXTENDED PERIOD OF TIME, NO EVIDENCE OF ELEC SMELL PRESENT. THE 415 & 416 COFFEEMAKERS OP CHECK GOOD. OK TO CONTINUE.
CAUTION LIGHT L HYD QTY DISPLAYED. RAN CHECKLIST - ON FINAL LOST HYD SYS ON FINAL. FOUND HYD PUMP LEAKING FROM DRAIN MAST. R&R'D HYD PUMP PER 29-11-05 AMM. R&R CASES DRAIN AND PRESS FILTER- FOUND CLEAN. ON LEAK CHECK FOUND L ENG PUMP PRESS SW O-RING LEAKING. R& R O-RING- LEAK CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1252685 S/N OFF 07540 PUMP, HYD ENG D OFF 19-2910-9-0003 7540 ON 19-2910-9-0003 2863.
INSPECTION FOUND A 0.012 INCH CRACK IN BELTFRAME AT STA 231, BL 0, JUST FORWARD OF FORWARD ACCESSORY DOOR CUTOUT. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5313-01010, REV A.
SMOKE IN AFT CABIN GALLEY AREA. REPLACED OVEN PER AMM 25-32-75.
INSPECTION FOUND AN 8 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 421-471. REPAIR WAS ACCOMPLISHED IAW EA 5731-01010, REV D.
INSPECTION FOUND A 6 INCH CRACK IN LT WING LEADING EDGE SKIN. THE SKIN WAS REPAIRED IAW EA 5731-01010.
INSPECTION FOUND EMERGENCY LIGHTS AT AIRCRAFT CABIN LEFT MID SECTION INOPERATIVE. INSPECTION FOUND BATTERY PACK M10954 HAD FUSE BLOWN. THE FUSE WAS REPLACED AND THE EMERGENCY LIGHT OPERATION WAS RESTORED IAW MM 33-51-13.
THE RT OVERWING SLIDE BOTTLE PRESSURE WOULD NOT TEST. THE SLIDE BOTTLE WAS REMOVED AND REPLACED IAW MM 25-65-02 AND OPERATION CHECKED GOOD.
RAMP REPORTED DENT IN L1 DOOR (2 INCHES X 3 INCHES). REPAIRED PER SRM 53-00-01.