N57862
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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING ETOPS CHECKS THE MECHANICS NOTICED NR 2 WHEEL WAS MISSING THE HUB CAP. FOUND A PIECE OF HUB CAP ATTACHED AT THE 6 O'CLOCK POSITION SUGGESTING THE HUB CAP BROKE OFF AT SOME POINT. NO DAMAGE NOTED AT AFFECTED AREA. HUBCAP WAS REPLACED AND AIRCRAFT WAS DISPATCHED. REPLACED MISSING HUB CAP ON JUNE 27 IN SFO. HUB CAP INSTALLED NEW HUB CAP ON #2 MLG WHEEL REF IPC 32-45-01 AND AMM32-45-01.
R1 DOOR WILL NOT ARM, AND NOW WILL NOT DISARM COMPLETELY. FOUND DEBRIS INLINE WITH GIRT BAR ATTACHMENT POINTS. CLEARED THE SAME. OPERATED DOOR THRU ARMED/ DISARMED SEVERAL TIMES. OPS SATISFACTORY. NO FURTHER ACTION REQUIRED. OK TO CONTINUE.
OVERHEAD LIGHTING AT L1 DOOR FOUND INOPERATIVE ON ARRIVAL AT GATE, PROBLEM WAS RESOLVED. OPERATED FWD GALLEY LIGHTS WITH SLIDE ARMED & DISARMED, AS WELL AS WITH FLIGHT DECK DOOR OPEN AND CLOSED. ALL WORKS PROPERLY. GOOD FOR SERVICE.
ACCOMPLISH INITIAL INSPECTION OF RT WING UPPER SKIN FASTENER HOLES #1-18 IAW PART 2C OF THE LATEST REVISION OF EC/RA 5720-03571 ON OR BEFORE THE AIRCRAFT REACHES 25,379 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES THEREAFTER.
REPAIR ON THE FUSELAGE SKIN BETWEEN STA 1540 - 1560 AND STR 27R - 29R AT LAVATORY SERVICE DOOR CUTOUT PER THE LATEST REVISION OF EC/RA 5330-07636
ACFT SMELLS OF VAPOR & BURNING OIL WITH APU & ENG BLEED. REPLACED RECIRCULATION FILTERS IAW 21-25-02/401. RAN APU AND BOTH ENGINES ONE AT A TIME. THE ODOR WAS ONLY NOTICEABLE WHEN USING THE APU BLEED. ENINE RUNS WERE NORMAL. SUGGEST PLACING APU BLEED ON MEL.
WHILE RUNNING THE APU BLEED THERE IS A STRONG ODOR IN THE CABIN. TS APU FOR SOUCE OF ODOR/OIL LEAKS. ACCOMPLISHED AMM 21-00-01-002-001 REMOVAL OF OIL CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEMS. RAN PACK FOR SEVERAL HOURS. ODOR IS NO LONGER PRESENT FROM PACKS
CREW REPORTS AUTO SHUTDOWN OF APU AFTER CREW NOTICED & WAS INFORMED OF SMOKE & ODOR COMING FROM VENTILATION SYS. CREW SHUTDOWN PACS & APU BLEED FOLLOWED BY APU AUTO SHUTDOWN. STARTED APU, TURNED ON APU BLEED, TURNED PACKS 1 & 2 ON, APU OIL 2197 SMELL & SMOKE FILLED CABIN & COCKPIT. OPEN UP APU COMPARTMENT FOUND OIL DRIPPING FROM TOP OF APU GEARBOX COOLING FAN AREA. FOUND GEARBOX CHIP DETECTOR FULL OF FERROUS MATERIAL. APU ECB FAULTED APU HIGH OIL TEMP WITH AUTO SHUTDOWN. INSPECTED TAILPIPE & TURBINE WAS DRY. STARTED SECTION G. REMOVE APU. ACCOMPLISHED STEPS G (2) -(14A) REMOVED APU IAW TASK 49-11-01-004-107 PREVIOUS FIREWALL INSPECTION DISCREPANCIES CORRECTED AND FIREWALL, MOUNTS AND SEALS SERVICEABLE PER IDT 09-10-05. COMPLETED APU INSTALL THROUGHT STEP H.2.E PER AMM: 49-11-01-404-108. CONTINUE INSTALL FROM STEP H.2.F AND ON. CONTINUED INSTALLATION OF APU IAW AMM 49-11-01-404-108 FROM STEP 5.H.(2)(F) TO STEP 5.I.(26). ALSO INSTALLED FUEL MANIFOLD DRAIN TANK IAW EC/RA 4911-01104. VERIFIED INSTALLATION OF REPLACEMENT APU REF MM 49-11-01-404-108 VERIFIED STEPS 5.I.(26) TO 5.I(28) OF MM 49-11-01-404-108 HAVE BEEN COMPLETED. GMM 09-25-05.
CREW REPORTS HEAVY ELECTRICAL BURNING SMELL IN FLIGHT DECK AND THROUGH OUT THE CABIN WITH VISIBLE GREY SMOKE THROUGHOUT AIRCRAFT. LOCKING UNLOCKED WAS NOT AN ELECTRICAL SMELL. STARTED APU, TURNED ON APU BLEED, TURNED PACK 1 AND PACK 2 ON, APU OIL 2197 SMELL AND SMOKE FILLED THE CABIN AND COCKPIT. OPEN UP APU COMPARTMENT FOUND OIL DRIPPING FROM TOP OF APU GEARBOX COOLING FAN AREA.FOUND GEARBOX CHIP DETECTOR FULL OF FERROUS MATERIAL. APU ECB FAULTED APU HIGH OIL TEMP WITH AUTO SHUTDOWN. INSPECTED TAILPIPE AND TURBINE WAS DRY. SEE PHOTO ATTACHED. SEE LOG PAGE 6289098. PER CAPTAIN GRANT PROOPS THERE WAS NO ELECTRICAL SMELL.
BIRD STRIKE ON RADOM. PERFORMED BIRD STRIKE INSPECTION. AND INSPECTIONS, INCLUDING RADOME, NO DELAMINATION OR DAMAGE FOUND.OK TO CONTINUE.REF AMM TASK 05-51-18-212-001
ACCESS PANEL 443JL IS MISSING FROM THE INBD SIDE OF NR 2 PYLON. INSTALLED ACCESS PANEL 443JL IAW MM 54-53-01. SECURED.
R ENG OVHT AT FL360. WENT AWAY AFTER R EPR REDUCED BY .02. R OVH T DET STATUS ALSO. PER CREW ALSO GOT STRUT OVERHEAT EICAS MOMENTARILY ACP FIM 26-11 TASK 802 ENGINE FIRE/OVERHEAT DETECTION SYSTEM BITE . STEPS 1-6 COMPONENTS AND INTERFACE WIRING ARE CHECKING OK. PERFORMED ENG #2 HIGH POWER RUN 10 MIN N1 85% / 5 MIN N1 70%.. REF POWER PLANT OPERATION LIMITS REFERENCE: TASK 71-00-00-992-005-R00.. OPS CHK GOOD . NO FAULTS NOTED.
R OVHT DET STATUS MSG FOLLOWED BY R ENG OVHT CAUTION. COMPLIED W ITH QRH. WENT AWAY WITH IDLE DEBRIEFED FLIGHT CREW, ADVANCED THROTTLES AT LANDING, MSG DID NOT REAPPEAR. HAS HISTORY REF LP 5883831. PERFORMED FLOWCHART 26-11 FAULT TREE 803. VERIFIED NO PRESSURE RELIEFE DOORS#2 ENG WERE OPEN ON WALKAROUND. PERFORMED 26-11 FAULT TREE 802 ENG OVHT BITE TEST NO FAULTS NOTED. PERFORMED RIGHT ENG EEC BITE CHECK AMM REF 73-21-00-902-001-R01 FAULT D8 SHOWS BUT HAS NO SYSTEM EFFECTS. LEAK CHECKED ALL PNEUMATIC DUCTING FOR #2 ENGINE & PYLON REF AMM 36-11-09-782-030-001. NO LEAKS FOUND LEAK CHKD GOOD IN PREVIOUS HISTORY IT WAS SUGGESTED TO REPLACE AFOLTS CARD #5 AS PRECAUTIONARY. R & R AFOLTS CARD 5 M10426 IRT AMM 26-10-01-024-001 OVHT TESTS PASSED. SUGGEST HIGH-POWER RUN-ON ENGINE #2 TO CHECK FOR OVERHEAT LIGHT.CIRCUIT, RAN #2 ENG AT TAKEOFF POWER FOR SEVERAL MINUTES, NUMEROUS TIMES. NO OVERHEAT STATUS MSG OR CAUTION DURING RUN.
DOOR 2L SLIDE COVER LOOSE ADJUSTED 2L DOOR BUSSLE, INSTALLATION AND RIGGING NOT AFFECTED
POSSIBLE BIRD STRIKE OUT OF 10K, SOMTHING DID MAKE CONTACT WITH ACFT. ODOR DETECTED INSPECTED ACFT FOUND NO EVIDENCE OF A BIRDSTRIKE OR IMPACT OF SPECIFIED AREA IAW AMM TASK 05-51-18-212-001
EMERGENCY POWER RESERVOIR CHECK PROCEDURE - INSTALLED SAFE DOOR PINS FOR DOOR SLIDE. INSTALLED EMARGENCY RESERVOIR SAFETY PINS L4 FOR GIRT BAR LUBE. REMOVED SAFE DOOR PINS AND RESERVOIR SAFETY PINS L4 VERIFIED SAFETY PINS ARE REMOVED ON L4 DOOR SLIDE AND POWER RESERVIOR.QC238542
GEAR DISAGREE EICAS ON TAKEOFF FROM DCA PER CREW GEAR DISAGREE EICAS ONTAKEOFF. RIGHT NOSE GEAR LIGHT ILLUMINATED W/GEAR IN UP/OFF POSITION. CREW DEBRIEF ON ARRIVAL AT IAD: AMBER GEAR TRANSIT/DISAGREE LIGHT ILLUMINATED WITH ASSOCIATED GEAR DISAGREE EICAS MESSAGE DURING TAKEOFF AND GEAR RETRACTION. CREW RAN CHECKLISTS AND AFTER PREPARING FOR ARRIVAL GEAR WAS EXTENDED, EICAS MESSAGE EXTINGUISHED AND THE AMBER GEAR TRANSIT/DISAGREE LIGHT ALSO EXTINGUISHED. NOSE AND BOTH MAIN GEARS BOTH SHOWED GREEN DOWN AND LOCKED FOR LANDING. ATTACHED PHOTO FOR REFERENCE OF THE GEAR TRANSIT/DISAGREE LIGHT. FIM TASK 32-61 TREE 802. PSEU BITE SHOWS FAULT CODE 32-09101 ON FLIGHT 0. NO CURRENT FAULTS. COMPLETED FIM TASK SUPPORT 32-09-03/301 REPLACED PSEU PER AMM 32-09-04 BITE TESTS NORMAL. SWUNG LANDING GEAR SEVERAL TIMES WITH NO FAULTS PRESENT. .R&R PSEU BOX REF AMM 32-09-04-404-009,
R FWD ENT DOOR EICAS C THE RIGHT FORWARD ENTRY DOOR IS NOT LATCHED MOMENTARY CAUTION MSG AT FL330. PRESSURIZATION NO RMAL. DOOR HAN DLE MOVING IN TURBULENCE DEBRIEF PILOTS AND FLIGHT ATTENDANT. PER WRITEUP NO PRESS ISSUES. ALSO PILOTS INDICATED THAT THE MESSAGE WAS MOMENTARY AND DID NOT COMEBACK FOR THE REST OF THE FLT. CLEAN RH FWD ENTRY DOOR INDICATION SWITCH CYCLE DOOR SEVERAL TIMES OPS CHECK NORMAL PER AMM 52-11-00-862-077.
UNNATURAL SMELL IN FLIGH T DECK DURING ALL PHASES OF FLIGHT. FAS ADVISE NO ODOR IN CABIN SUBMITTED FORM TO TOMC FOR SMELL IN FD. REF FIM TASK 21-00-01/301 FOUND NOTHING THAT PRODUCES AN ODOR IN FLIGHT DECK AND CREW STATED SMELL DID NOT SMELL LIKE ELECTRICAL ISSUE. PERFORM SNIFF CHECK IN FWD EE COMPT WITH NO CONCERNABLE ODORS NOTED. WALKED AROUND A/C WITH NO LEAK ISSUES NOTED. NO HISTORY IN RECORDS.
R GEN OFF EICASTALKED WITH CREW UPON ARRIVAL. THEY SAID THEY LOST AFT GALLEY POWER AND AFT LAV STOPPED WORKING. THEY THEN GOT THE R GEN CONT OFF LIGHT, THEN THEY GOT THE R GEN DRIVE LIGHT ALONG WITH THE R CTR FUEL PUMP OFF LIGHT ON. THEY DID NOT DISCONNECT THE RIGHT GENERATOR. THEY ALSO SAID THEY GOT R ELEC HYD PUMP OFF LIGHT AND NOTICE C/B WAS TRIPPED , RESET AND WAS OKAY. OIL LEVEL CHECKED GOOD. PERFORMED FIM 24-20 TASK 801 AND 1ST MESSAGE IS "OVER FREQ TRIP" . CURRENT EICAS MSG R IDG TEMP SENS FOUND MESSAGES: OVER FREQ TRIP, SHORTED PMG, IDG/PMG/WIRING, IDG/OIL OUT BULB WIRING, IDG/OIL IN BULB WIRING, UNDER FREQ TRIP, SHORTED PMG TRIP, AND GEN/FIELD WIRING/GCU ON BPCU BITE, RH GEN SYSTEM. REF FIM 24-20 TASK 802 TABLE 202 WITH OVER FREQ TRIP AND IDG/PMG/WIRING FAULTS OCCURING AT SAME CHANNEL, MUST REPLACE RH IDG. REMOVED RH ENG IDG REF AMM 24-11-01-024-001. INSTALLED REPLACEMENT RH ENG IDG REF AMM 24-11-01-424-002 UP TO AND INCLUDING STEP 3. H. (2). BEGIN AT 3. H. (3). IDG IS INSTALLED IN QAD RING AND BOLT IS SAFETIED. INSTALLED FEEDER CBLES TO IDG. REF AMM TASK 24-11-01-424-002 STEP H 7 C/W IDT REQUIREMENTS REF. GMM 09-10-05. FEEDER CABLES INSTALL ON R/H ENG. ACCOMPLISHED IDLE RUN FOUND ALL PARAMETERS NORMAL, ACCOMPLISHED ALL ASSOCIATED TEST AND INSTALLATIONS TO COMPLETION WITH NO DEFECTS NOTED.
DOOR 1R EXCESSIVELY LOUD SQUEELATTACHED PHOTO'S TAKEN ON RIGHT SIDE OF AIRPLANE ABOVE DOOR 1 RIGHT. CREW DEBRIEF: F/O THOUGHT HE HEARD NOISE COMING FROM FWD LOWER DOOR AREA. DEADHEADING F/O WENT FWD TO HELP EVALUATE AND INDICATED NOISE WAS COMING FROM ABOVE GALLEY. ALL CREW SAID NOISE LEVEL AND PITCH CHANGED WITH SPEED/POWER SETTING. DOOR SEAL VISUAL INSPECTION REVEALED NO OBVIOUS DEFECTS. CABIN CREW INDICATED THEY HEARD THE NOISE DURING TAXI AND MORE INTENSLEY DURING DEPARTURE. NOISE MODERATED AFTER POWER REDUCTION/LOWER ALTITUDE AND SPEED PRESSURIZED AIRCRAFT AND FOUND LOUD SQUEAL AT LOWER EDGE OF DOOR THRESHOLD PLATE AT CENTER, AND AFT CORNER. REMOVED THRESHOLD PLATES AND FOUND NO SEALANT IN THE PRE-PACK AREA OF THE CENTER PLATE, AND INSUFFICENT SEALANT ON THE CORNER PLATE. SEE PICS CLEANED AND REINSTALLED THRESHOLD PLATES WIRH PROPER SEALANT APPLICATION IAW AMM 53-13-01-424-003. APPLIED POLYSULFIDE SEALANT BMS5-95. B 1/2 AT 15:30 ON 06/18/24. WILL REQUIRE PRESSURIZATION FOR THRESHOLD LEAK CHECK. PARTS USED: 00-0609-3-9664,QTY :1 PRESSURIZED AIRCRAFT FOR R1 DOOR LEAK CHECK IN REF AMM 05-51-24-702-001. FOUND DOOR TO BE MAKING NOISE BETWEEN 3-4.5 DIFFERENTIAL. AT 5 DIFFERENTIAL NOISE FROM INSIDE STOPPED. HOWEVER AIR LEAKAGE WAS FOUND AT ALL PRESSURE DIFFERENCES ON THE ADD EMP:U413233 OUTSIDE. LOCKED FOR BOEING DISPOSITION DOOR 1R IS SERVICEABLE PRESSURIZED AND NO LEAKS NOTED . WAITING ON REPLDOOR 1R IS SERVICEABLE PRESSURIZED AND NO LEAKS NOTED REF AMM 05-51-24-702-001.
APU DOOR INLET SURROUND STRUCTURE HAS CORROSION AT I/B FWD CORNE R, O/B FWD EXTENDING 10" I/B AND AFT O/B,
FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS BETWEEN F.S. 365.2 5 AND 377.7 AT LBL 25 (LEFT TUNNEL OF MEC) IS CRACKED
REF AMES NR 170224-0200-0211 GEN ITEM 53-5310-1-2626 CRACK FOUND THROUGH FASTENER ON FRAME IN UPPER CABIN R/H SIDE ST A 1580 FOR OVER HEAD BIN ATTACH BRACKET ABOVE STR 9 REPAIRED CRACK THROUGH FASTNER ON FRAME IN UPPER CABIN R/H SIDE STA 1580 ABOVE STRINGER 9 IAW B757 300 SRM 53-00-07-2R-8.
CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1500-1520 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED FLOOR SUPPORT IAW BOEING 757 SRM 51-40-02 P AR 4. SEE BACK AND PARTIAL WORK SHEET 40 FOR PARTIALLED WORK.
CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1260-1300 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1260-1300BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK FOR PARTIAL WORK.
CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1320-1340 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1320-1370 AT BLO IAW BOEING 757 SRM 51-40-02 PAR 4. SEE BACK AND PARTIALLED WORK
CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1420-1440. REMOVED AND REPLACED FLOOR SUPPORT AT BS 1420-1440 BL0 IAW BOEIN G 757 SRM 51-40-02 PAR 4, SEE BACK FOR PARTIALLED WORK.
REF AMES NR 170224-0100-00175 GEN ITEM EA 5100-02129 REV H OP 00 1 DURING AGING INSPECTION, FOUND L-BRACKET CRACKED FOR FUSELAGE FA IRING SUPPORT CRACKED, JUST AFT OF RWW RBL-12
REF AMES NR 170224-0100-0149 GEN ITEM 53-5310-1-2606 FLC FS676 LBL24 SLOPE WALL FLOOR SUPPORT CRACKED. REPAIRED SLOPE WALL FLOOR SUPPORT FS676 LBL24 IN FLC IAW B757 SR M 51-70-0G-0 TABLE 1
REF AMES NR 170224-0100-0068 GEN ITEM EA 5100-02244 REV G OP 003 ALC PANEL 151AF HAS A CRACK
REF AMES NR 170224-0100-0069 GEN ITEM EA 5100-02244 REV G OP 003 ALC FLOOR PANEL 153AF CRACKED
GENERATING ITEM B757-20-3-0065: FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS (LEFT TUNNEL OF MEC) BETWEEN F.S. 365.25 AND 377.7 AT BL 0 IS CRACKED (MARKED WITH STREAMER 70209). REPORTED BY V92 9433. REPAIRED FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAM BETWEEN FS AND 365.25 AND 377.7 BL 0 IAW B757 SRM 53-10-51-2R-1 REPAIR 1.
FOUND CRACKED SUPPORT RIB AT STATION 365.25, JUST ABOVE WIRING B UNDLE #91177 REF AMES NR 170224-0100-0064
RIGHT FMC FAIL LIGHT IS ON LP 7452038 MEL 3461AK WAS CLEARED. MUST REPLACE R FMC REF AMM34-61-01-024-001-002 UNLOCKED TO CLEAR WITH R FMC R&R FMC IN SFO WITH TT# 1524492 AC 0862 REF IPC EQUIPMENT AND SOFTWARE INSTL- MAIN ELECTRONICS EQPT CTR FMC REFERENCE: CYC CB NO HELP REQUEST MEL COMPLIED WITH MEL 34-61-01-08. RIGHT FMC FAIL DEFERRED REF MEL 3461AK. COMPUTER, FLT M OFF 19-3461-9-0004 9107 ON 0000 COMPUTER, FLT M OFF 19-3461-9-0004 9107 ON 19-3461-9-0004 9498 RPLD R FMC COMPUTER REF AMM 34-61-01-424-005-002 AND VERIFIED ALL SOFTWARES ARE IDENTICAL TO FMC L (OP PROGRAM, OPC, AMI, FIDO, & NAV DATABASE). REF GMM 5-35-40, PERFORMED CAT LLL CHECK TEST 30 AT THE MCDP AND TEST PASSED. FULL CAT LLL CAPABILTIES ADD EMP:U076986,U410201 RESTORED.
LT HYD QTY EICAS C, LEFT HYDRAULIC RESERVOIR QUANTITY IS LOW, HYD AUTO EVEN T RAN CHKLIST IAW QRH. AFT ER SECURING BOTH L PUMPS RUDDER RATIO DISPLAYED. QTY SLOWLY RETURNED NORMAL & LANDING WITH ALL MESSAGES & INDICATIONS RETURNING TO NORMAL. CREW STATED LT HYD QTY DROPPED TO .37 WITH RF INDICATION. FOLLOWED QRH TURNED OFF LT ENG & LT ELEC HYD PUMPS AND LT YAW DAMP. LT QTY INDICATION SLOWLY RETURNED TO NORMAL .90. CREW TURNED PUMPS BACK ON FOR APPROACH IAW FIM 29-33 FAULT TREE 803. REPLACED LT HYD RESERVOIR 99-2936-9-9002, QTY TRANSMITTER IAW AMM 29-33-01. OPS CHECKED SYS WITH NO DEFECTS OR PARTS USED.
ABNORMAL FUEL INDICATION S CREW INFO: FUEL CONFIG LIGHT DISPLAYED. CROSS FEED CLOSED, NO DRIP STICKED FUEL TANKS AND THEY COINSIDE WITH COCKPIT FUEL IN CENTER TANK, ENG FUEL BURN WAS EQUAL, RIGHT WING FUEL INDICATIONS. LEVEL WAS GOING DOWN WHILE THE LEFT WING WASN''T. CAPT WATCHED FOR 20 MINIUTES AND SAW NO CHANGE. HE REPORTS THAT THE AIRCRAFT WAS FLYING LEFT WING HEAVY. STARTED TROUBLESHOOTING BY OPERATING FUEL PUMPS AND VALVES IN 2) RH FUEL PUMPS ON, XFEEDS OPEN, DEFUEL/ XFER VLVS CLOSED, LH 3) RH FUEL PUMPS ON, XFEEDS OPEN, DEFUEL/ XFER VLVS CLOSED, LH 4) RH FUEL PUMPS ON, XFEEDS CLOSED, RH DEFUEL/ XFER VLV OPEN, LH RAN BOTH ENG. AT IDLE FOR 30 MIN. WITH ALL BOOST PUMPS ON FUEL THE FOLLOWING CONFIGURATIONS. 1) RH FUEL PUMPS ON, XFEEDS SPAR VLV CLOSED. (RH TANK, CTR TANK AND LH TANK ENG FEED SPAR VLV OPEN. (ENG FEED MANIFOLD PRESSURIZED TO FUEL CONTROL OF SPAR VLV CLOSED. (PRESSURE FUELING MANIFOLD PRESSURIZED ONLY TO WAS ONLY BURNED OUT OF THE CENTER TANK. WITH CENTER TANK BOOST CLOSED, DEFUEL/ XFER VLVS CLOSED, LH SPAR VLV CLOSED. (ONLY RH MANIFOLD PRESSURIZED UP TO LH SPAR VLV) - AFTER 1 HR NO LEFT ENG) - AFTER 1 HR NO MOVEMENT. TANK FILL VLVS.) - AFTER 1 HOUR NO MOVEMENT. PUMPS OFF FUEL BURNED OUT OF THE WING TANKS AT THE SAME RATE. ON TANK AND RH SIDE OF CTR TANK ENG FEED MANIFOLD PRESSURIZED) - MOVEMENT. ADD EMP:U104393 ADD EMP:U104393 LEAKS NOTED AFTER 1 HR NO MOVEMENT. ADD EMP:U104393 ADD EMP:U104393
(B757-06-3-0253) EXTERIOR FUSELAGE L/H SIDE, 3EACH DENTS ON THE FUSELAGE SKIN BTWN BS 740 AND BS 760 AND BTWN STRINGERS S-15L AN D S-17L. REF HAECO GSO NRC #9286611 REPAIR ACCOMPLISHED IAW HAECO REO-G23222 AND ECRA 5331-02232. PG 2, PART 1,ITEM 2 REQUIRES TO GENERATE A DIP TO "PERFORM AN INSP- ECTION PER PART 2 2 OF ECRA 5331-02732 ON OR BEFORE 65,800 TOTAL ADD EMP:V932675 AIRCRAFT FLIGHT CYCLES
B757-06-3-0222, ZONE 100, LOWER HALF FUSELAGE, STA 1605, AFT OF WASTE DRAIN DOOR, SKIN IS DENTED FROM INSIDE HAECO/GSO LOG 9286586, V899290 2EA DENTS AT STA 1605 R/H SIDE AFT OF WASTE DR, GOUGE 0.018 DEEP GOUGE''S NOT ALLOWED. OUT OF LIMITS PER SRM 53-00-01. COMPLETED SKIN REPAIR PER SRM 53-00-01 REPAIR 29, CAT B, ZONE A REPAIR. INSP REQUIREMENTS ARE 37,500 TOTAL FC FROM ACFT DELIVERY OR 6000 FC INTERVALS AFTER REPAIR ACCOMPLISHMENT WHICHEVER COMES FIRST. INSP METHOD IS HFEC, REF NDT PT6, 51-00-01, SRM 53-00-01-2R-29 REPAIR 29, TABLE 206. HAECO LOG 9286586, V932655, QC387 TOTAL FLT CYCLES AT TIME OF REPAIR = 15,829 RPR29 -INSP REQUIREMENTS ARE 37,500 TOTAL FC FROM ACFT DELIVERY OR 6000 FC INTERVALS AFTER REPAIR ACCOMPLISHMENT WHICHEVER COMES FIRST. TOTAL FLT CYCLES AT TIME OF REPAIR = 15,829. AFT OF WASTE DRAIN DOOR, SKIN IS DENTED. SRM 53-00-01-2R-29 TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED Q/C REVIEWED. RECORDS UPDATE...KJB QC REVIEWED Q/C REVIEWED. RECORDS UPDATE...KJB RIR: 6,000 F/C FROM REPAIR AT 15829 F/C....KJB
EMERGENCY LIGHT BATTERY PACK M11490 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11490 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.
EMERGENCY LIGHT BATTERY PACK M11489 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11489 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.
FLAP ASYMMETRY EICAS INDICATION AFTER FLAP RETRACTION ON TAKEOFF. RH FLAP NEEDLE STUCK WITH NO FLIGHT CHARACTERISTICS NOTICED. FLAPS INDICATION DID RETURN TO NORMAL ON FLAP EXTENSION FOR LANDING USING NORMAL FLAPS. REMOVED AND REPLACED FLAP POSITION IND. NO JOY. REINSTALLED ORIGINAL, MORE T/S REQUIRED. WHILE WORKING FIM 27-51-00-815-812 INDICATOR IS SPLIT IN NORMAL AND ALT CONTROL FROM 0 TO 15 UNITS THEN NORMAL TO FULL TRAVEL. WHEN TAPPING ON GAUGE WHILE MOVING FLAPS, INDICATION IS NORMAL WITHOUT A SPLIT, NEEDS INDICATOR REPLACED THEN VERIFY FIX. VERIFIED INDICATOR HAS PLAY IN NEEDLES, PART ORDERED IS BAD FROM STOCK, NEEDS NEW INDICATOR ORDERED AOG, P# 215-016-001. ACP FIM 27-51-00-815-805 ACP FSEU BITE AND FOUND NO MESSAGES, CHECKED POSITION TRANSMITTER VALUES THRU FSEU 1 AND 2 PER TABLE A FIG 502 AMM 27-58-01-825-003 ALL READINGS WITHIN TOLERANCES. PER TOMC REQUEST, PRECAUTIONARY RMV. & RPLC. RIGHT T/E FLAP TRANSMITTER REF. AMM 27-58-01, OPS CHECK GOOD, POSITION TRANSM. VALUES THRU FSEU 1&2 ARE WITHIN LIMITS REF. TABLE "A" FIG 502. OK TO CONTINUE.
FOUND FOWARD EXIT SIGN AT DOOR 3 RIGHT INOP REMOVED CEILING PANEL ABOVE DOOR 3 RIGHT FOR TROUBLESHOOTING AND REMOVED DADO PANEL JUST AFT OF DOOR 3 RIGHT RANG OUT BOTH WIRES ON LIGHT FORWARD FOR DOOR 3 RT AND FOUND AN OPEN ON GROUND WIRE REF AWD 33-51-22, PG 905 SHEET 1. ACCOMPLISHED REPAIR PER ECRA3351-01266 AND REF SWPM 20-30-12. EM ERGENCY LIGHTS WORKING NORMALLY. CKS OK.
SUBSTASK:B757-53-3-0569: MAIN CABIN, R4 DOOR, ABOVE THE LOWER GATE HAS CUT MARKED SAA-072/61 OFF AIRCRAFT. REF ON REF N/R 0053913. ACCOMPLISHED REPAIR AT MAIN CABIN, R4 DOOR INNER SKIN BETWEEN 165 8.31 TO STA 1652.19 PER EC/RA 5210-03021. WORK WAS ACCOMPLISHED ON ST-ENG N/R 0053913 AND INSPECTED. SEE ABOVE FOR MAINTENANCE DETAILS.
REMOVED CORROSION AT R2 DOOR LWR GATE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE R-2 DOOR LWR GATE ASSY P/N 19-5211-3-0 709 IAW SRM 52-10-02 FIG 101 AD 1 AND 51-40-02 PARAG 4. WORK ACCOMPLISHED, EA 5210-01363 REV F: R2 DOOR LWR GATE HAS CORROSION. MARKED 014- 26. REF NR 0053642. SEE ABOVE FOR MAINTENANCE PERFORMED.
SECONDARY FINDING ZONE 200 OPEN, FLOOR CROSSBEAM AT STA 395 HAS SEVERAL AREAS OF CORROSION, 22-87. REF NR 0053995. REMOVED DAMAGED CROSSBEAM IAW SRM 51-40-02, FABRICATED NEW SUPPORT FLOOR CROSSBEAM IAW DWG 141N5162, INSTALLED NEW SUPPORT CROSSBEAM, P/N 141N5162-142 AT MAIN CABIN STRUCTURE SUPPORT FLOOR AT STA 395 IAW DWG 141N5162 AND SRM 51-40-02. WORK WAS ACCOMPLISHED ON N/R 0053995.
SUBTASK ZONE 200 OPEN, LAV A SUPPORT FITTING AT STA 340 B/L 0 IS CORRODED. REF N/R 0053993 REMOVED AND REPLACED NEW FITTING P/N 65N57839U2, BATCH 000347007 6, PO NO:SAG7990580 AT MAIN CABIN FWD LAVATORY FLOOR AT STA 340, PER SRM 51-40-02. WORK WAS ACCOMPLISHED ON N/R 0053993. REMOVED AND REPLACED NEW FITTING P/N 65B7839U2, BATCH 0003470076 , PO. NO: GAG1990580 AT MAIN CABIN FWD LAVATORY FLOOR AT STA 340 PER SRM 51-40-02. SUPPLEMENT 86912. COMPLETED ON NR 00 53993. REF INFO ABOVE. PER SRM 51-40-02.
SECONDARY FINDING ZONE 200 OPEN, FWD GALLEY FLOOR FITTING AT STA 365 IS CORRODED AND PITTED. REF N/R 0053994 REMOVED AND REPLACED NEW FITTING P/N 415N4007-11, BATCH 00034697 25, PO NO:SAG1900502 AT MAIN CABIN FWD GALLEY FLOOR AT STA 365 PER SRM 51-40-02 AND AMM 20-11-00-912-001, USED (T /W) ID:11-706 DATE OF DUE 11SEP19.WORK WAS ACCOMPLISHED ON N/R 0053994.
SECONDARY FINDING: AFTER REMOVAL OF LAV C, STA 1310 LBL 30 L/INB D SEAT TRACK FITTING HAS CORROSION. REF N/R 0053696. REPAIRED SEAT TRACK AT MAIN CABIN STA 1260 TO 1320 LBL 24.7 IAW SRM 53-00-52, REPAIR 3 FIG 201. ESFR NO.1021543. SEE SUPPLEMENT 85562. WORK ACCOMPLISHED AND RECORDED ON NR 0053 696. INSPECTION COMPLETED AND ACCEPTED.
AFT CARGO COMP. FLOOR STR AT APPROX. FS1374 RBL 1610HAS CORRODED NUT PLATE. 56-006. REF VTSAA N/R 0053546. REPAIRED STRINGER AT AFT CARGO COMPARTMENT FS 1374 RBL 1610 IAW B757-3 SRM 53-00-53 REPAIR 1. ESFR NO.1021541. SEE SUPPLEMENT 85 533.
AFT CARGO COMP, FLOOR STR AT APROX FS1374 LBL 7 .55 HAS CORRODED NUT PLATE. 56-005. REF VTSAA N/R 0053543. REPAIRED STRINGER AT AFT CARGO COMPARTMENT FLOOR STR AT FS 1374 LBL 7.55 IAW B757-3 SRM 53-00-53 REPAIR 1. SEE SUPPLEMENT 85534. ESFR 1021540. WORK ACCOMPLISHED AND RECORDED ON ST-SAA NR 0053543 BY MECH V925086, INSPECTED BY V919831.
(B757-06-3-0243) AFT CARGO COMP. FLOOR STR AT APPROX FS1330 RBL 7.55 NUT PLATE HAS CORROSION. 56-012. REF NR 0053578. REMOVED DAMAGED AREA OF STRINGER @ STA 1330 RBL 7.55, FABBED REP AIR -7 CHANNEL AND INSTALLED -7 IAW SRM 53-00-53 REPAIR 1. SEE SUPPLEMENT 85544. WORK ACCOMPLISHED AND RECORDED ON NR 0053578. INSPECTION COMPLETED AND ACCEPTED.
EMERGENCY LIGHT WIRE FELL OFF. SECURED SWITCH GUARD WIRE, OPS CHECKED GOOD
L3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. CHECKED NORMAL.
FIRST OFFICER`S ALTIMETER HAS OFF FLAG AND FROZE AT FL 320, NO FLAG PRESENT. ACCOMPLISHED AIR DATA TEST IAW AMM 34-12-00, TESTED OK.
L2 DOOR FLASHLIGHT LED NOT WORKING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY, CHECKED OK IAW AMM 25-64-00-902-037.
L AC BUS OFF L GEN CONT OFF FOLLOWED CHECKLIST AC BUS/GEN CONT RESTORED. LEFT GCB AND IDG REPLACED REPLACED #1 IDG REF AMM 24-11-01 OP CK NORMAL AND LEAK CK GOOD. REPLACED LEFT GENERATOR RELAY C901 REF AMM 24-22-03
R1 & 4 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. REPLACED THE LAMPS, CHECKED NORMAL IAW AMM 33-51-00.
DENT AT FUSELAGE STATION 640, BETWEEN STRINGER 17L - 18L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 AD1 FIG.101 DETAIL III. REPAIRED FUSELAGE SKIN AT STATION 640, BETWEEN STRINGER 17L - 18L IAW SRM 53-00-01 REPAIR 3 FIG 201. THIS IS CATEGORY B REPAIR WITH REPETITIVE INSPECTION IAW SRM 53-00-01 REPAIR 3 FIG 201 PAGE 207 TABLE V.
AT FL 360 RT ENG VIB WENT INTO AMBER BAND TWICE, MAX 2.7. FOLLOWED QRH, PROBLEM DID NOT RETURN DURING DIVERSION REF FIM 71-05-00-815-808-ROO. INSPECTED MAG CHIP DETECTORS & OIL FILTERS. FOUND TO BE CLEAN. RAN ENG, OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE. SEE LOG PAGE 8114668 FOR VIBRATION SURVEY.
RIGHT HYD QTY LOSS TO .43-TURNED OFF RT PUMPS & LOSS STOPPED. PUMPS ON FOR LANDING. FOUND LEAK ON NR 2 ENG PYLON DRAIN.DIFF PRESS SWITCH LEAKING AT MODULE. REPLACED O-RINGS REF IPC 29-11-17-02 ITEMS 245/246. LEAK CK`D GOOD. SERVICED RT HYDS PER CREW NO LOSS OF PRESSURE. (NO LOW PRESSURE LIGHTS)
DURING FLIGHT 2 STATUS MESSAGES CAME ON AT THE SAME TIME: LDG GEAR MONITOR AND NOSE A/G DISAGREE. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT REF 757-300 AMM 32-09-0 4-004-001. OPS CHECKS GOOD. REF 757-300 FIM 31-41-00/101 FIG 109 FOR ERASE NOSE A/G DISAGREE EICAS MSG. ROTABLE PARTS CHANGE WAS INDICATED - TT 1412649, S/N OFF 00029 IPC REFERENCE.
AFT CARGO DOOR EXTERIOR SKIN FWD LWR CORNER FOUND PREVIOUS REPAIR DOUBLER WITHOUT RECORD. PREVIOUS ATA REPAIR. PREVIOUS REPAIR DOUBLER REMOVED. INSTALL NEW DOUBLER AS PER SRM 52-30-01, REPAIR 4, FIG 201 AT STA 1383-1388. FWD LWR AFT CARGO DOOR EXTERIOR SKIN. PLACED ON A DIP AS PER NOTE C SRM 52-30 01, TO INSPECT WITHIN 3,000 FLIGHT CYCLES AFTER THE REPAIR IS INSTALLED, 52-DIP CONTROL NUMBER 03775. REINSPECT AFT CARGO DOOR SKIN FWD LWR CORNER STA 1383-1388 SRM 52-30-01 PG 201 CATEGORY B REPAIR 4 TABLE IV EVERY 3000 FLIGHT CYCLES (LFEC NDT PART 6,53-00-06) DIP CTL 03775 LIMIT: 1) RIR: EVERY 3000 F/C.
EXTERNAL SKIN STA 480-500 S19R-22R STATIC PORT SURROUNDING AREA FOUND PREVIOUS DOUBLER REPAIR NOT PER SRM. BS 480-500, S19R-224 STATIC PORT SURROUNDING AREA DOUBLER REPAIR REPLACED AND INSTALLED AS PER SRM 53-00-01 REPAIR 8 FIG 201. DIP RAISED FOR SUBSEQUENT INSPECTION AFTER 37.5K CYCLES & EVERY 12K CYCLES THEREAFTER. SRM 53-00-01 REPAIR 8 FIG 201 TABLE II 53-DIP, CONTROL 03773. WORK PERFORMED BY SJ832. INSPECT EXTERNAL SKIN REPAIR STA 480-500 S19R-22R AT INITIAL THRESHOLD 37,500 FLIGHT CYCLES ,THEN REPEAT INSPECTIONS (LFEC)AT 12,000 FLIGHT CYCLE PER SRM 53-00-01 REPAIR 8 TABLE II DIP CTL # 03773 LIMIT: 1) INIT: W/I 37500 F/C. INIT WILL AUTO-ITO TO.
FX - EXTERNAL SKIN STA 580-600 S16L-17L FOUND PREVIOUS DOUBLER REPAIR. PREVIOUS DOUBLER REMOVED AND DISCARD AS PER SRM 51-40-02 AND SKIN REPAIRED AS PER ECRA 5330-04002 REV- AT STA 600 BETWEEN STR 16L AND STR 17L AND FORM 44.0008 ATTACHED ITEM 1 TO ITEM 19 ACCOMPLISHED. REFER TO LOG PAGE 8340767 FOR PERMANENT REPAIR DIP.
EXTERNAL SKIN STA 1560 S28L-S29L FOUND PREVIOUS DOUBLER REPAIR WITHOUT RECORD. FUSE EXT SKIN DOUBLER REPAIR REPLACED AND INSTALLED AS PER SRM 53-00-01 REPAIR 3 FIG 201. FORM 44.0008 ITEMS 1 TO 17 ACCOMPLISHED. DIP RAISED FOR REPEAT INSP AFTER 37.5K CYCLES, EVERY 3K OR 6K AS APPLICABLE REF SRM 53-00-01 REPAIR 3 FIG 201 TABLE V 53-DIP C/N 03714. INSTALLED FUSELAGE SKIN REPAIR, STA 1560, STR 28LT TO STR 29LT. INITIAL THRESHOLD IS 25,000 FLT CYC PER SRM 53-00-01, REPAIR 3 FIG 201 PER TABLE V, INSPECT AND INTERVALS OF 3000 FLT CYC THEREAFTER LFEC PER CHART V OF SRM REPAIR AT 37,500 TOTAL FLT CYC`S, THEREAFTER EVERY 3,000 FLT 53-00-01 REPAIR 3 OF PG 207. NOTE DOUBLER THICKNESS REPORTED TO CYC`S FOR HFEC OR 6,000 FLT CYC`S FOR LFEC INSPECTIONS. CAT B BE .064 THICK, CATEGORY B REPAIR. REPAIR. 1) INIT: W/I 25000 F/C. INIT WILL AUTO-ITO TO 2) RIR: EVERY 3000 F/C THEREAFTER (M&E 53-9953-8-0340).
EXTERNAL SKIN STA 760-765 S16L - S17L FOUND PREVIOUS REPAIR DOUBLER WITHOUT RECORD. EXISTING DOUBLER REPAIR REMOVED & REPLACED AS PER SRM 53-00-01 FIG 201 REPAIR 3. FORM 44.0008 ITEMS 1 TO 16 ACCOMPLISHED. DIP RAISED FOR REPEAT INSPECTION AFTER 37.5K CYCLES, EVERY 3K OR 6K CYCLES AS APPLICABLE. REF SRM 53-00-01 REPAIR 3 FIG 201 TABLE V CONT# 03713. WORK PERFORMED BY SJ821 INSTALLED FUSELAGE SKIN REPAIR, STA 760 TO 765, STR 16LT TO STR. INITIAL THRESHOLD IS 25,000 FLT CYC 17LT PER SRM 53-00-01, REPAIR 3 FIG 201 PER TABLE V, INSPECT AND INTERVALS OF 3000 FLT CYC THEREAFTER LFEC PER CHART V OF SRM REPAIR AT 37,500 TOTAL FLT CYC`S, THEREAFTER EVERY 3,000 FLT 53-00-01 REPAIR 3 OF PG 207. NOTE DOUBLER THICKNESS REPORTED TO CYC`S FOR HFEC OR 6,000 FLT CYC`S FOR LFEC INSPECTIONS. CAT B BE .090 THICK, CATEGORY B REPAIR. REPAIR. 1) INIT: W/I 25000 F/C. INIT WILL AUTO-ITO TO 2) RIR: EVERY 3000 F/C THEREAFTER (M&LE 53-9953-8-0342).
B757-53-3-0010 FX - EXTERNAL SKIN STA 500-520 RT WINDOW FRAME FOUND DOUBLE REPAIR. WINDOW FRAME REPAIRED AS PER SRM 56-20-02 FIG 201, REPAIR AT STA 500-520 RT THIS REPAIR IS CATEGORY A AND FORM 44.0008 ATTACHED ITEM 1 TO 15 ACCOMPLISHED.