N814UA
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
UPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND FR67 FRAME TO HAVE MULITPLE ELONGATED FASTENER HOLES. REMOVED AND REPLACED RT FR67 FRAME IAW SRM 51-44-11 AND 51-42-11.
UPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND DOOR SILL TO HAVE CORROSION AND MULTIPLE ELONGATED FASTENER HOL ES. REMOVED AND REPLACED R2 DOOR SILL IAW A319 UAL SRM 51-44-11 AND 51-42-11.
Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD RECIEVED ECAM ON T/O AFTER POWER BROUGHT UP DEBRIEFED CREW, PUMPS RUN TIME DID NOT EXCEED 5 MINUTES AFTER RUNNING. PERFORMED INSPECTION OF DPI REF 29-00-00-280-006. NO LOW LEVEL WARNING. UPON INSPECTION FOUND ORING FOR FIN ID 3094GM DEFECTS NOTED.PARTS USED: 40-0595-3-1665,QTY :1 CHECK VALVE EXTRUDED. REMOVED AND REPLACED REF AMM 29-00-00-910-003. LEAK CHECK GOOD WITH YELLOW, AND ALL SYS INFORMATION ONLY UPDATE. FLAGGING AS SDR
FUEL CAP MISSING APPLY CDL 28A INOP STICKER APPLIED IN FLIGHT DECK DISPATCH DESK: 24 NAME: RB DATE: 22-DEC-23- APPROVED CDL FOR MISSING FUEL CAP. INSTALLED NEW FUEL CAP AND NOTICED THE ADJUSTMENT IS NOT CORRECT.(SEE PICTURES). NECESSARY ADJUST THE FUEL CAP AS PER AMM 28-25-41-400-005-A. CAP WAS MISSING ON ARRIVAL, INSTALLED NEW CAP.
ENG 2 BLEED LEAKECAM...SHUT BLEED OFFPER ECAM PERFORMED LEAK CK / ENGINE RUN ON ENG 2. NO LEAKS NOTED. NO MESSAGES, BITE CK OF BMC SHOWED NO FAULTS. PFR SHOWED NO CURRENT FAULTS. ALL WORK IAW AMM 36-22-16. OK FOR CONTINUED SERVICE. PERFORMED LEAK CK / ENGINE RUN ON ENG 2. NO LEAKS NOTED. NO MESSAGES, BITE CK OF BMC SHOWED NO FAULTS. PFR SHOWED NO CURRENT FAULTS. ALL WORK IAW AMM 36-22-16. OK FOR CONTINUED SERVICE.
R/H EMERGENCY EXIT FWD FRAME CRACKED PER HAECO LCQ N/R 9294845/ 24845 GEN BY REMOVED AND REPLACED RH EMERGENCY EXIT FWD FRAME IAW UAL SRM 51- 72-11-911-001
AFT CARGO PIT STRINGER 31R AT FR65 HAS CORROSION JUST FWD OF OUT FLOW VALVE PER HAECO LCQ N/R 9294579/24579 GEN BY V926223
R2 DOOR SILL HAS CORROSION AT FR66 AND FR68 PER HAECO LCQ N/R 9294633/24633 GEN BY V061603
HYD RESERVOIR FILL CONNECTOR SPINS UNABLE TO ATTACHED SERVICER SERVICEABLE NON-COSMETIC INT DIP ABLE TO SECURE HYD FILL CONNECTION LOCKING PLATE TANGS FOR CONTINUED SERVICING THRU QUICK DISC SERVICE PORT. REQ CARRY APPROVED PER GMM 05-30-06. AT NEXT MAINTENANCE TOMC-APPROVAL FROM SC1ELBYC COMMENT OPPORTUNITY WITHIN THE NEXT 30 DAYS, REPLACE THE HYDRAULIC FILL CONNECTION AND FLANGE, REF IPC 29-16-04-03, PART #''S AE96993E AND 3222-4. FIM # 1007 GM SEE PICTURE. QC RECORDS UPDATE.....HC QC REVIEWED T/A : 30 DAYS.....HC/U389717 REPLACED CONNECTOR AND BACKING PLATE. LEAK CHECKS GOOD AND NO LONGER SPINS. TOMCQC REV PERFORMED
ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD FOUND YELLOW HYDRAULIC SYSTEM VERY LOW, SERVICED WITH 3 GALLONS RAN YELLOW HYDRAULICS FOR 2+ HOURS WHILE CYCLING FLIGHT MAIN WING FUEL TANKS AND INSPECTED FOR POSSIBLE HYDRAULIC HYDRAULIC FLUID. T/S PER TSM 29-13-00-810-805-A AND CONTROLS, INSPECTED WHEEL WELLS, APU COMPARTMENT, TAIL CONTAMINATION, NONE DETECTED. ENCLOSED PHOTO OF HYDRAULIC LEVELS 29-13-00-810-801-A. NO LEAKS FOUND. PERFORMED LEAK CHECK IN REF COMPARTMENT HOLE(COMPARTMENT 321AR) WITH NO VISIBLE LEAKS OR AT RELEASE. A/C OK FOR SERVICE. TO AMM 29-00-99-200-001-C1. RAN #2 ENG AND DEPLOYED REVERSER, HYDRAULIC QUANTITY REDUCTION. SUMPED FUEL FROM LEFT AND RIGHT
ON OR BEFORE AIRCRAFT N814UA (4014) ACCUMULATE 37,170 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION OF THE LH WINDOW FRAME CONTINUITY FITTING AREA AROUND THE INSTALLED WASHERS PER PART 2 STEP 1 OF THE LATEST REVISION OF EC 5311-02875, THERE AFTER REPEAT INSPECTION AT 5,621 FLIGHT CYCLES INTERVARLS, LTPR NR# 5001172132-0010. GENERATED IN ERROR, SEE ELB LP 9443051.
DEEP SCRATCH FOUND ON RH SLAT NO.3 INBD TRAILING EDGE SIDE CAUSED BY RUBBING ON 622BT PROTRODING SCREW HEAD. REQUIRES FURTHER EVALUATION. LTPR NR# 5001173902-0010. CREATED DMG REF GMM 06-35-05. THIS IS A CAT "A" RPR WITH NO REINSPECTION REQUIRED. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 57-44-21-300-011. THIS IS A CAT "A" RPR. BY LHT TECH 5H0885 & INSP 5H0619.
*EMERGENCY DECLARED* HYD Y RSVR LO LVL ECAM AT CRUISE. LOST YELLOW SYSTEM AND ACCUMULATOR. PYLON LEAKING,PART. # D2901010201200,TUBING REMOVED NEED TO BE INSTALLED. INSPECTED HYDRAULIC LEAK AT #2 ENGINE AND FOUND TUBING IN THE LOCKED FOR POSITIVE FIX. CONTACT TOMC BEFORE CLEARING ITEM. . #2 ENGINE PANEL 423AL WAS REMOVED TO FACILIATE MX. UNLOCKED FOR FIX INSTALLED INLET LINE ON HYDRAULIC FILTER CANISTER ON #2 PYLON REF AMM 78-37-00 PERFORMED IDLE RUN REF AMM 71-00-00 NO LEAKS NOTED AT THIS TIME ALSO INSTALLED PNL 423AL .
AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. GEAR DOORS OPERATED NOR MALLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT NLG FOR ANY OBVIOUS DEFECTS AND REPORT TO TOMC LOCKED FOR GEAR DOWN FERRY.
BATTERY PACK FOR 13WL WILL NOT PASS CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK 13WL AND OP CHECKED GOOD IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A.
REF EA 5330-05216 REV A STEP 3.2 #4 HOLE IS CRACK ON THE ALUMINUM PRESSURE DECK PANEL ONLY. REPAIRED #4 HOLE ON PRESSURE DECK PANEL REF. EC/RA#: 5331-02602. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5331-02602 ON OR BEFORE THE AIRCRAFT REACH 85,846 TOTAL AIRCRAFT FLIGHT CYCLES OR 181,696 TOTAL AIRCRAFT FLIGHT HOURS WHICHEVER C OMES FIRST. PLANNING TO CONTACT ENGINEERING AFTER 73,000 TOTAL A IRCRAFT FLIGHT CYCLES BUT BEFORE 75,000 TOTAL AIRCRAFT FLIGHT 36 HOLES CYCLES FOR INSPECTION REQUIREMENTS AT LHS PRESSURE PANEL FR 35- CORRECTION SHOULD READ 85746 TOTAL AIRCRAFT FLIGHT CYCLES NOT 85846. PLANNING TO CONTACT ENGINEERING AFTER 73,000FC BUT BEFORE 75,000 FC. OK TO DIP TILL THE AIRCRAFT REACHES 85,846 FC OR 181,696 FH. TOMC-APPROVAL FROM SC1ELBYC COMMENT UPDATE TO REF FLEET CYCLE NON-ROUTINE NUMBER 9726376 FOR RII AND BUYBACK. QC REVIEWED RECORDS UPDATE QC REVIEWED INIT: PLN/ENG >73,000 <75,000 TAFC T/A: 85,846 TAFC OR 181,696 TAFH..........LT/U224600
WX RADAR INOP.WR ANT AND WR R/T MSGON BOTH NDS WXR R/T PN ON : 066-50008-0409 SN ON: 10041 SN OFF: 10065 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1365535 SN OFF 0065 TRANSCEIVER, WX OFF 31-2311-9-0001 0065 ON 31-2311-9-0001 8041 REMOVED AND REPLACED WEATHER RADAR DRIVE UNIT AND WEATHER RADAR TRANSCIEVER OPS CHECK SAT NO THER DEFECTS NOTED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1119594 SN OFF 4858 PEDESTAL, CANNE OFF 31-3417-9-0001 4858 ON 31-3417-9-0001 9375 REF MM34-41-11 AND 34-41-33.
HAD AUTOBRAKE FAULT ECAM. WHICH SHOWED NORM BRAKES INOP WHICH I S NAGAINST MEL. INTERVIEWED CREW: FLIGHT CREW STATED THAT ECAM MESSAGE CAME ON DURING CRUISE AND THEN WENT AWAY. MESSAGE RETURNED AGAIN DURING LANDING/ROLL OUT. ALSO, THERE IS A NOTICEABLE SHUDDER AS THE AIRPLANE CYCLED BETWEEN NORMAL AND ALTERNATE BRAKING SYSTEM. PREVIOUS LEGS, GOING AS FAR BACK AS DECEMBER 28. BITE OF BSCU ALSO FAULTS 23GG. NUMEROUS 23GG FAULTS IN PFR FAULTING "BRK SELECTOR VALVE(23GG)/L G HYDRAULIC PIPE". ADDED SDR FLAG. REF LOG PAGE 8684103 FOR PARTS REPLACED AND OPERATIONAL CHECKS PERFORMED. OPS CHECK NORMAL NO FAULTS. REF LOG PAGE NUMBERS 8687300 FOR THE THROTTLE VALVE RPL. LOG PG 8687277 FOR THE AUTO BRAKE SELECTOR RPL. LOG PG 8687440 FOR THE BRAKE PRESSURE TRANSUCERS 11GG, 13GG RPL. LOG PG 8687308 FOR THE NORMAL BRAKE SELECTOR RPL. ACP OPS CHECK OF NORMAL BRAKING SYSTEM PER AMM32-42-00 AND OPS CHECK OF ALTERNATE BRAKE SYSTEM.
BRAKES SYS NR 1 FAULTED. RESET THE NOSE WHEEL STEERING ONCE, MESSAGE STILL DISPLAYED. RAN BSCU SYSTEM TESTS. FAULTS ON BSCU 1 BRAKE PEDAL TRANSMITTER 9GG. REPLACED THE BRAKE PEDDAL TRANSMITTER IAW MM 32-42-47. BITE TESTED BSCU 1 AND 2. NO FAULTS.
L2 DOOR AFT LOWER CORNER FITTING HAS CORROSION. REMOVED AND REPLACED L2 DOOR AFT LOWER CORNER FITTING IAW SRM 51-42-11-001.
CABIN EMERGENCY LIGHTS FAILED TO TEST, EPSU REMOVED & REPLACED IAW AMM 33-50-00, OPS CHECKED GOOD.
FOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, REPLACED L1 AND LEFT EMERGENCY DOOR BATTERY PACKS. SYSTEM OPS NORMAL.
STANDBY ALTIMETER INDICATION ERRONEOUS AT FL370 STBY ALT READS FL358. ACCOMPLISHED FUNCTIONAL TEST REF AMM34-21-00. STBY ALT NEEDLE STICKS. REPLACED STBY ALTIMETER REF AMM34-21-22 OPS CHECKS NORMAL.
RT FUSE SKIN AT FR35 STR 30R HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM RPR ACP IAW ECRA 5330-05813 PART 1.
LT FUSE SKIN AT FR35 STR 30L HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM REPAIR ACP IAW EC RA5330-05813 PART 1.
R1 DOOR SILL FWD GIRT BAR FITTING AREA CORROSION AROUND FWD OUTBD, AFT INBD, & AFT OUTBD HOLE AT FR20 STR23. REMOVED CORROSION BY SPOT FACING ALL 3 HOLES ON FR20 .017 .025 .020 MATERIAL REMOVED & FOUND TO BE IN LIMITS IAW A319 SRM53-11-14 FIG 108 PARA 7B FAB 3 EA FILLER WASHERS IAW SRM 53-11-14 FIG 108 SHT 5 NDT INSP NTM51-10-08 FOR SPOT FACE AREA & NTM 51-10-01 FOR ROTORY SCAN AND NO DEFECTS FOUND. INSTALLED REPAIR WASHERS IAW SRM53-11-14 FIG 108 SH T2 SRI53-11-14-1-001 FIG 108 PARA 3A TABLE 102
FWD CARGO THRESHOLD WEB HAS CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-21-13 PG 101-104.
L2 DOOR CUTOUT FWD LOWER CORNER HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11.
L2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.
AFT CARGO DOOR SILL CORROSION NUMEROUS AREAS BETWEEN FR59 & FR56. REMOVED AND REPLACED AFT CARGO SILL IAW SRM 51-42-11.
AFT CARGO BAY SUPPORT PLATE JUST INBD OF DOOR SILL CORRODED AROUND FWD-TIE DOWN AT FR56. REMOVED AND REPLACED WITH NEW THRESHOLD PLATE AT AFT CARGO LOWER DOOR FROM FR55.5 TO FR59 IAW SRM 51-42-11.
AFT PIT THRESHOLD CONNECTION HAS CORROSION. REMOVED AND REPLACED AFT PIT THRESHOLD SHEET CONNECTION IAW 51-42-11.
FR 70 STR 23 RT, AFT CORNER LOWER PANEL HAS CORROSION ON PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11.
RT WW SHEAR PLATE SUPPORT FRAME BETWEEN FR69-FR90 FOUND TO HAVE CORROSION. REMOVED AND REPLACED RT SHEAR PLATE SUPPORT FRAME IAW SRM 51-72-11.
CENTER FUEL TANK PUMPS WILL NOT TURN ON AFTER FLAP SLAT RETRACTION. CYCLING OF AUTO FUEL FEED PB SWITCH FROM AUTO TO MANUAL, NO HELP. UNABLE TO MOVE FUEL OUT OF CTR FUEL TANK. NO INFLIGHT RESET AVAILABLE, ACFT DIVERTING, BOTH CTR TANK GFIS & FQIC WERE REPLACED. OPERATIONS CHECKED OK.
CREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS, CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSELAGE OR WINGS. SUSPECT AIR IN SYS. RAN NR 1 ENG & OPERATIONS CHECKED FLIGHT CONTROL SYS. NO LEAKS NOTED GREEN HYD QTY HAD NO CHANGE.
CREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS & CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSELAGE OR WINGS. SUSPECT AIR IN SYS. RAN NR 1 ENG & OPERATIONS CHECKED FLIGHT CONTROL SYS, NO LEAKS NOTED, GREEN HYD QTY HAD NO CHANGE.
CREW RETURNED TO THE FIELD DUE TO MLG NOT RETRACTING WHEN SELECTED UP. AHM IS FAULTING THE LT GEAR EXTEND PROX SENSOR 21GA. REPLACED 21GA SENSOR DUE TO CORROSION. REPLACED LT MLG MAIN GEAR HARNESS CONNECTOR INSIDE J BOX. REPLACED LT 1M HARNESS, LT 2M ENHANCED HARNESS. GEAR SWING WITH NO DEFECTS NOTED
R2 DOOR SILL HAS CORROSION AT FRAME 66. REPLACED R2 DOOR SILL IAW SRM 51-44-11 & 51-42-11.
R2 DOOR CUT OUT AFT CORNER FITTING AT FRAME 68 IS CORRODED. REMOVED & REPLACED FITTING IAW SRM 53-41-14 FIG 101.
SHAPE SILL ON R2 DOOR SILL IS CORRODED. R & R DOOR SILL IAW SRM 53-41-14 FIG 101.
FRAME 66 R2 DOOR FWD CORNER FITTING CORRODED. R & R CORNER FITTING IAW SRM 53-41-14 FIG 101.
RIGHT NR 2 DOOR FRAME 68, NR 7 DOOR STOP, LOWER INBD HOLE HAS CRACK INDICATION. REAMED HOLE IAW SRM 52-41-12 FG 202, NDT INSPECTION IAW 51-10-01 & NO CRACK NOTED. FABRICATED FREEZE PLUG & WASHER & INSTALLED IAW 53-41-12.
L2 DOOR SILL FRAME 68 HAS CORROSION AROUND THE LAST TWO NUTPLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION & FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-41-14 PARA 5A FIG 201 REPAIR PRINCIPLE 5.
EMERGENCY LIGHT OPERATIONAL TEST FAILED. EPSU BATTERY AFT LT DISPLAYED AFTER TEST. RESET AFT LT EPSU BATTERY. TESTED GOOD.
FAILED EMER LIGHT TEST FWD FLIGHT ATTENDANT PANEL. EPSU BATTERY EMER LIGHT REPLACED BOTH LT & AFT LT BATTERIES AMM 33-51. TEST NOW OK.
DURING PASS O2 DROP CHECK FOUND O2 MASK COMPARTMENT DOOR AT DOOR 2L DID NOT RELEASE DURING TEST. R & R EMERGENCY O2 CONTAINER & GENERATOR AT DOOR 2L. OPERATIONS CHECKED GOOD AT THIS TIME.
NICK ON FAN BLADE ENG 1. ENG 1 SNV10771 IAW MT72-007 FOR BLADES NUMBERING IAW AMM 72-31-11-200-010-B PARA 4B FOR ALLOWABLE DAMAGE LIMITS. REPLACED NR 19 FAN BLADE IAW AMM 72-31-11400-010-D13. ACCOMPLISHED VIBRATION SURVEY IAW AMM 71-00-00-700 -022, CHECKED GOOD.
APU WONâT START AFTER 2ND ATTEMPT. TRIED CYCLING THE APU CONTROL BREAKERS, NO HELP. INLET DOOR STUCK IN THE PARTIALLY OPEN POSITION & APU IS INOPERATIVE. IAW MEL CB L41 & L42 OPENED & TAGGED. ACCOMPLISHED TSM 49-00-00-810-899 -A REPLACED APU MOTOR STARTER IAW AMM 49-42-51PB401. APU STARTED TWICE WITH NORMAL OPERATIONS OK FOR SERVICE.
EXCESSIVE NOSE WHEEL VIBRATION AT 100 KTS & ABOVE UNTIL SLOWED IN WW ON TAKEOFF. LUBED NOSE WHEEL TORQUE LINKS, REPLACED ALL FOUR MLG TIRES IAW MT32-24 & OPBLM HIPPLE CORRECTED ATA.
EMERGENCY OXYGEN CONTAINER AT ROW 10ABC NEEDS PERMANENT INSTRUCTIONS PLACARDS. NO PARTS AT MEXJL, INSTALLED INTERIM PLACARDS. INSTALLED PERMANENT DECAL.
IAW CF 270 MANUAL DROP TEST, SEATS 31ABC DID NOT DROP. IAW SERVICE TIP MT 35-002 REPACKED MASKS, OPERATIONS CHECKED OK.
IAW CF270 MANUAL DROP TEST, SEATS 34DEF DID NOT DROP. IAW SERVICE TIP MT 35-002 REPACKED MASKS AT SEATS 34DEF, OPERATIONS CHECKED OK.
IAW CF270 MANUAL DROP TEST, SEATS 34ABC DID NOT DROP. IAW SERVICE TIP MT35-002 REPACKED MASKS AT SEATS 34ABC.
IAW CF270 MANUAL DROP TEST, SEATS 30ABC DID NOT DROP. IAW SERVICE TIP MT35-002 REPACKED MASKS, OPERATIONS CHECKED OK.
IAW CF270 MANUAL DROP TEST, SEATS 10ABC DID NOT DROP. REPLACED EMERGENCY OXY CONTAINER IAW MM.
IAW CF270 MANUAL DROP TEST, SEATS 1AB DID NOT DROP. REPLACED EMERGENCY OXY CONTAINER IAW MM 35-21-41.
IAW CF270 MANUAL DROP TEST, SEATS 24DEF DID NOT DROP. REPLACED EMERGENCY OXYGEN CONTAINER.
IAW CF270 MANUAL DROP TEST, SEATS 32DEF DID NOT DROP. IAW SERVICE TIP MT 35-002 REPACKED MASKS AT SEAT 32DEF, CHECKED OK.
BATTERY 2 FAULT. REPLACED NR 2 BATTERY & NR 2 BCL IAW MM, ALL OPERATIONS TESTED GOOD.
ACCUMULATOR PRESSURE BLEEDS OFF WHEN BREAKS SET. FOUND O-RING LEAKING ON ACCUMULATOR SERVICING PORT REPLACED, OPERATIONS CHECKED GOOD ON GROUND.
NR 1 ENG BLEED AMBER ON BLEED PAGE, 150C. CFDS FAULT RECORDED FAN AIR-V 9HA1 OR THERMOSTAT 7170 HM1, IAW TSM 36-11-00-810-849A. THERMOSTAT FAN AIR CTL PCN 644-0035. R & R THERMOSTAT IAW AMM, LEAK CHECKED GOOD.
ELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC NR 1 IAW MM 27-93-34 AFS & LAND VERIFICATION TESTED NORMAL IAW MM 22-96-00 & MM 22-97-00. AC RETURNED TO FULL CAT III CAPABILITY.
OXYGEN MASKS ROW 8 ABC DISLODGED. SECURED OXYGEN MASKS AT ROW 8 ABC. ACCOMPLISHED CHECK IAW AMM TASK 35-23-00-710-001, CHECKED OK.
LOUD SQUEAL IN COCKPIT AT 8.0 PSI. NO CHANGE IN TONE OR VOLUME DURING DESCENT. INSPECTED CAPTAIN'S AND F/O'S WINDSHIELDS. FOUND A SECTION OF THE CAPT'S HUMP SEAL THAT HAD A ROUGH WAVINESS AT THE UPPER LEFT CORNER, REF: MT 56-005. ACCOMPLISHED INTERIM REPAIR WITH SPEED TAPE AND ASKED FOR OUTBOUND CREW TO COMMENT IF SQUEAL NOISE FIXED OR SUBSIDES. INF- :PER INBD CREW FLT 272-25, NO NOISE WAS HEARD. NEED TO PERFORM MT 56-05. OK FOR SERVICE AT THIS TIME.
FOUND A POPPED SCREW-RIVET OUT AT THE HYD SYSTEM ACCESS PANEL ON THE A-CRAFT BELLY. SECURED SCREW WITH TAPE PER CDL SCREW LOCATION PNL 197BB IS 8 FROM THE TOP CORNER & 7 FROM THE BOTTOM CORNER LEADING EDGE NOT IN FRONT OF ANY SERVICE PANELS PER AMM 53-35-00-200-002-A TO BE REPAIRED WITHIN 10 FLT CYCLES. PARTS ORDERED PCN 756-0267 PCN 756- 1061 SCREWS & 754-2551 NUT PLATE.
VERY FINE HIGH PITCHED SQUEAL COMING FROM FLT DECK CEILING CABIN, ALTITUDE 7900FT. REPAIRED UPPER SECTION OF CAPT WINDOW SEAL.
CREW REPORT: CAPTAINS FWD WINDOW HAS A PRESSURE LEAK PSI8 CAB ALT 7400FT. UPON FURTHER INVESTIGATION FOUND WINDOWS NOT TO BE LEAKING. POST'S BETWEEN FWD COCKPIT WINDOW AND SLIDING WINDOW LEAKING AT SEAM. FOUND BOTH SLIDING WINDOW SEALS WORN. FOUND L2 & R2 WINDOW SEALS BAD NEED REPLACEMENT. REMOVED & REPLACED PER AMM. PERFORMED PRESSURE CHECKS. CHECKS GOOD.
F/O SEAT PEDALS ADJUSTMENT ASSEMBLY LOOSE. TRIMMED OFF LOOSE PIECES AND APPLIED SPEED TAPE AS NEEDED. REPLACED PEDAL ADJUSTMENT ASSY PER MM. REPLACED PLATE AS PER ABOVE INSTRUCTIONS.
FLAP HANDLE JAMMED AT FLAP 1 POSITION - TOOK SEVERAL ATTEMPTS TO GET IT TO FLAP 2, TRIGGER FLAP SLAT CONTROL LEVER AND FLAP HANDLE COMMAND SENSOR UNIT. GRND OP'S OK.
YELLOW-GREEN PTU LEAKING. REPLACED GREEN-YELLOW PTU. BLED SYSTEM AND CHECKED FOR LEAKS. CHECKED OK. OPS CHECK ACCOMPLISHED ON SMC 18.
MAINTENANCE STATUS MESSAGE AIR BLEED DISPLAYED ON THE LOWER ECAM SCREEN.
RT BRAKE VERY SOFT WEAK SPLIT PEDALS FOR EVEN BRAKING.
AT LANDING GEAR DEPLOYMENT A-C ROLLED HARD LEFT. HALF CONTROL. STICK INPUT TO STOP ROLL. SAMC TEXT: *UPDATE* NO WIND OR WAKE PRESENT WHEN ROLLING MOMENT OCCURED. INBD CREW REPORTS A-S 190 KTS, FLAPS 1, SPEED BRKS FULLY EXTENDED, ROLL OCCURRED AT MOMENT GEAR DEPLOYED. PERFORMED LM2228, GEAR SWING AND SPOILERS CHECKED GOOD. ELAC REPLACED ON SEQ 2192003.
DENT FOUND AFT OF DOOR 1L, DENT IS 1 INCH LONG BY 1.25 INCH LONG. SAMC TEXT: DENT IS .06 DEEP AND REF SRM IS OK FOR CONTINUED SERVICE UP TO 3000FC. PERMANENT REPAIR MUST BE ACCOMPLISHED BY PTC 20764. OK TO CF REF SRM 53-11-11. CARRIED FORWARD PER SAMC.
ELT IS BROKEN ABOVE SEAT 1EF. REPLACED ELT.
RAT OUT MESSAGE ON ECAM HYD PAGE APPEARED & SHOWED GREEN RAT EXTENSION THEN SHOWED NORMAL. REPLACED RAT EJECTION JACK (2454GE) IAW AMM.
RAT DEPLOYED INDICATION ON ECAM. VERIFIED NOT DEPLOYED. CREW COMMENT: MSG GOES ON AND OFF INTERMITTENTLY. FOUND RAT STOW SW WIRE INSULATION DAMAGE REF ASM 29-22-00 CONNECTOR C-C PIN B. RESTORED INSULATION. NO STRAND DAMAGE. RAT IND NORMAL. STOWED RAT AFTER REPAIR.
CAPTS O2 MASK MIC INOPERATIVE. REPLACED CAPT'S O2 MASK & O2 MASK BOX.
OIL ODOR IN CABIN. F/A THINKS IT COULD BE ASSOCIATED WITH OVERHEAD LIGHTS. OIL ODOR FROM APU, RAN ENGS NO ODOR. APU BLEED INOPERATIVE, APU USEABLE FOR ELEC. OPERATED ALL OVERHEAD LIGHTS IN FWD & AFT GALLEYS, AND CABIN CEILING LIGHTS AT MAX BRIGHT. (GROUND EXTERNAL POWER USED). NO ELECTRICAL ODOR NOTED THRUOUT ACFT. ACCOMPLISHED PACK BURNOUT PER MM, ISOLATED ENG BLEED HP AND IP VALVES AND APU. SLIGHT ODOR ORIGINALLY FROM APU, PACK BURNOUT ACCOMPLISHED NO ODOR NOTED. APU BLEED DUCT CLEAN, NO OIL FOUND.
MODERATE TAIL VIBRATION, RTFL. VIBRATION CHECKLIST FILLED OUT BY CREW, SHOWS VERTICAL BOUNCE. FOUND PLAY AT ELEVATOR SERVO CONTROL ROD ENDS, REPLACED ELEV SERVO CONTROLS 34CE4 AND 34CE3 IAW AMM AND ROD ENDS OF SERVO CONTROLS 34CE1 AND 34CE2 IAW AMM, TESTS OK. VIBRATION TBS WAS FOLLOWED.
CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: LT SIDE RED HARNESS INFLATION TAB BROKEN. SAMC TEXT: **UPDATE** SWAP CAPT O2 MASK ASSY WITH 2ND OBS SEAT. SWAPPED CAPT O2 MASK TO 2ND OBS SEAT LOCATION. CAPTAIN'S MASK USEABLE, 2ND OBS MASK INSTALLED IN BOX, BUT NOT CONNECTED. CREW O2 PRESSURE GOOD. 2ND OBS SEAT INOPERATIVE.
AFTER LOWERING FLAPS FOUND BIRDSTRIKE TO LT OTBD FLAP L/E. FLAP HARD POINTED, CONT WITH HOOKUPS, RIG-OPS CKS & TEST FLY PLAN IN PM. LAP REPLACED MOC ON W-U H8607S, IAW MM. ACCOMPLISH TEST FLIGHT FOR LT OTBD FLAP BEING REPLACED. FLAPS GOOD. LATERAL-DIRECTIONAL TRIM GOOD.
MED 2L OXYGEN COMPT FAILS DROP CHECK. ACCOMPLISHED MASK ADJUSTMENT.
SEAT 23 D,E,F OXYGEN COMPT FAILS DROP CHECK. CORRECTLY RESTOWED MASKS, DROP TEST OK.
SEAT 22 A,B,C OXYGEN COMPT FAILS DROP CHECK. CORRECTLY RESTOWED MASKS, DROP TEST OK.
SEAT 12 A,B,C OXYGEN COMPT FAILS DROP CHECK. CORRECTLY RESTOWED MASKS, DROP TEST OK.
SEAT 1C,D OXYGEN COMPT. FAILS DROP CHECK. REPLACED CONTAINER ASSY DUE TO BROKEN HINGE, DROP TEST OKAY.
MED 2R OXYGEN COMPT FAILS DROP CHECK. ADJUSTED COSMETIC SEAL ON DOOR PANEL TO PREVENT BINDING. DROP TEST OK.
AFT LT AFT LAV OXYGEN COMPT FAILS DROP CHECK. ACCOMPLISHED MASK ADJUSTMENT.
PAX O2 MODULE DROPPED ABOVE SEATS 14DEF. VERIFY O2 GENERATOR NOT FIRED, RESTOW MASKS AND APPLY MEL. SEATS 14DEF ARE PLACARDED INOP AND NOT TO BE OCCUPIED UNTIL DROP CHECK FOR O2 MASKS IS ACCOMPLISHED. RESTOWED MASKS IAW AMM. DROP TEST OK.
LT OVERWING SLIDE OUT OF CONTAINER PARTIALLY DEPLOYED. DETERMINED THAT SLIDE RAFT PARTIAL DEPLOYMENT WAS DUE TO AMT INSERTING SAFETY PIN WITH THE INFLATION RESERVOIR VALVE REGULATOR PIN HOLE MISS-ALIGNED. A SERVICEABLE SLIDE RAFT WAS PROCURED AND WAS INSTALLED ON ROUTINE TASKCARD 4R2592012 BY MAE MECH AND INSP BY QC ON TASKCARD LISTED ABOVE & BASE N-R C2651L.
DENT IN FUSELAGE RT SIDE FWD OF FRAME 8. CTR OF DENT IS 10 INCHES FROM FIXED WINDOW CUTOUT. EDDY CURRENT SHOWS NO CRACKS. DENT WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED LOCATED AND DRILLED DOUBLER REPAIR. FABRICATED DOUBLER IAW SRM. OK TO INSTALL. INSTALLED REPAIR DOUBLER. MARKED REPAIR.
FLAPPING NOISE FROM DOOR 2R AREA, RTFL. CHECKED ALL AREAS ON RT SIDE OF ACFT INCLUDING EE BAY ON BOTH SIDES. CHECKED ALL DOOR SEALS, CARGO COMPT. FWD AND AFT, FWD NOSE GEAR DOORS, AND ALL ACCESS PANEL DOORS. NO PROBLEMS FOUND. CONTACTED OPBLM ABOUT ACTION TAKEN AND THEY CONCURRED. CONTROLLER AND MANAGER CONCURR THAT THE AIRPLANE CAN BE RELEASED BACK TO SERVICE.
CREW 02 FITTING STRIPED, UNABLE TO SERVICE 02. REPLACED FILL PORT AND SERVICED.
N/G VIBRATION, RTFL. TROUBLESHOOTING, FOUND THE NR 1 LGCIU WITHIN AIR FAULTS. REPLACED THE NR 1 LGCIU, SYS CHECKED OKAY. ALSO REPLACED LGCIU 2 IAW LM2905.
WHILE ACCOMPLISHING EMERGENCY LIGHTS CHECK DURING 3SVC GOT FAULT, EPSU BATTERY EMER R. REPLACED BATTERY RIGHT SIDE, TESTS OKAY.
FIRST OFFICER FWD O2 MASK INOP. PLASTIC VALVE COVER BROKEN. REPLACED QUICK DONNING MASK.
JET BRIDGE FORCED UP AGAINST BOTTOM OF DOOR 1L, WEIGHT OF AIRCRAFT RESTING ON DOOR, UPPER HINGE BUSHING PUSHED OUT OF HINGE, UPPER HINGE BOLT CONTACTING DOOR FRAME STRUCTURE. NOSE STRUT CAME DOWN WHEN JET BRIDGE WAS MOVED DOWN. REPLACED UPPER HINGE FITTING AND RE-INSTALLED DOOR. SECURED WIRING HARNESS, INSULATION BLANKETS AND ALL LININGS. COMPLETED DOOR INSTALLATION AND CHECK. PRESSURIZED CABIN NO LEAKS NOTED.
THE 14C AND 23C EMERGENCY EXIT LIGHTS ON SEAT EDGES ARE MISSING COVERS AND BULBS, WIRES EXPOSED. REPLACED EMERGENCY GEN LIGHTS ASSY, OPS CHECK OK.
DOOR 2R WILL NOT FULLY ARM, HANDLE STICKS OUT .5 INCH CAUSING FLIGHT DECK INDICATIONS. FOUND WATER IN DOOR ARMING CABLE. REPLACED DOOR 2R CABLE AND SLIDE ASSY.
ARMING LEVER STIFF CAUSING SLIDE DEPLOYMENT. SUSPECT FREEZING TEMPS AND MOISTURE. REMOVED BUSTLE, APPLIED HEAT TO MECHANISM UNTIL ABLE TO GET FREE MOVEMENT OF ARMING MECH. ACCOMPLISHED REPLACEMENT OF THE GIRT BAR PRECAUTIONARY. REPLACED DOOR SLIDE.
EMERGENCY LIGHT TEST IS FAULTY, AFT BATTERY PACK. REPLACE BATTERY PACK.
LEFT VERTICAL STAB PANEL 322AL HAS CRACK 13.5 INCHES LONG, 4.25 INCHES BELOW TOP OF PANEL AND 9 INCHES AFT OF CENTER LINE. REMOVED AND REPAIRED PANEL.
FLOORBEAM CORRODED (MARKED ). REMOVED FLOORBEAM. TRANSFERRED BRACKETS ONTO NEW FLOORBEAM. INSTALLED FLOORBEAM.
FLOORBEAM 190 CORRODED (MARKED). REMOVED BEAM. INSTALLED NEW FLOORBEAM.
FLOORBEAM 150 CORRODED (MARKED). REMOVED FLOORBEAM. TRANSFERRED BRACKETS ONTO NEW FLOORBEAM. CONNECTED FLOORBEAMS 150 AND 95 TOGETHER AND HAVE THEM IN PLACE. INSTALLED FLOORBEAM.
FLOORBEAM 185 CORRODED (MARKED). REMOVED CORROSION. ASSEMBLY OF FLOORBEAM COMPLETED. PAINTED & INSTALLED FLOORBEAM.
FLOORBEAM 145 CORRODED (MARKED). ASSEMBLED FLOORBEAM. INSTALLED BOLTS AND PAINTED. INSTALLED FASTENERS TO COMPLETE FLOORBEAM AND PAINTED.
FLOORBEAM 140 CORRODED (MARKED). COMPLETED BEAM ASSY. PAINTED FLOORBEAM & INSTALLED BOLTS. INSTALLED FLOORBEAM.
DOOR SILL 2R CORRODED (MARKED). REMOVED SILL PAN. PICKED UP HOLES IN NEW SILL PAN & INSTALLED CLIPS. INSTALLED SILL PAN. INSTALLED ALL FASTENERS THROUGHT EXTERNAL SKIN & FRAME STA 67. INSTALLED REST OF FASTENERS & SPLICE. INSTALLED FASTENERS AT LWR & AFT SIDE 2R SEAL PLATES.
RT SHEAR PLATE CORRODED (MARKED). REMOVED PLATE. PICKED UP HOLES. INSTALLED FASTENERS. INSTALLED SHEAR PLATE.
FLOORBEAM 80 CORRODED (MARKED). *S/D* REMOVED FASTENERS FROM FWD SPLICE. ASSEMBLED BEAM 80. INSTALLED FASTENERS IN SPLICE AND LATERAL BEAM CONNECTIONS. BEAM COMPLETED & INSTALLED.
FLOORBEAM 175 CORRODED. *S/D* REMOVED BEAM AND AFT 2 PROFILES. BEAM PARTIALLY INSTALLED AND IN PLACE. INSTALLED BEAM, AFT FASTENERS AND FWD TOP FASTENERS.
ACFT FAILED CABIN EMERGENCY LIGHT CHECK ITEM 2 ON 3 SVC. POWER SUPPLY FAULT/FAILURE. REPLACED POWER SUPPLY 11WL AND RELAMPED 63WL, 61WL. OPS CHECK NORMAL AFTER MTX.
FLIGHT ATTENDANTS STATED FELT SUBSTANTIAL VIBRATION IN AFT CABIN AND FORWARD CABIN FOR ABOUT 1 MIN. FOUND EXCESSIVE RUDDER FREE PLAY IN THE SERVO ROD ENDS. REPLACED ALL THREE RUDDER SERVO ROD ENDS. AT HMV, RUDDER HINGE BEARINGS REPLACED, ELEV HINGE BEARINGS REPLACED AND LEFT ELEV GREEN SYS SERVO FAILED FREE PLAY CHECK AT HMV. REPLACED LEFT ELEV GREEN SERVO.
LIGHT AIRFRAME VIBRATION PASSING 320 KIAS AT FL240 ON CLIMB-OUT. VIBS STOPPED AS CREW SLOWED BACK THROUGH 320 KIAS. FOUND WORN ROD ENDS ALLOWING PLAY IN CONTROL SURFACES AND GEAR DOORS. REPLACED WORN ROD ENDS IN LT GREEN ELEVATOR, RT YELLOW ELEVATOR. ALSO REPLACED LT INBD AND RT OTBD ELEVATOR PCA'S AFTER FAILING FREE PLAY CHECK. REPLACED LT AND RT AFT GEAR DOOR HINGE BUSHINGS AND LOWER ATTACH ARM BUSHINGS.
FOUND RAM AIR TURBINE BLADE HAS DAMAGE AND BLADE MATERIAL PEELED BACK. [SUP 05-16-07] RAT WAS DEPLOYED FOR MAINTENANCE 3 SEGMENTS PRIOR IN LAX AND DID NOT HAVE ANY DAMAGE NOTED AT THAT TIME. DAMAGE TO TURBINE BLADE WAS DISCOVERED PRIOR TO AN AD RELATED INSPECTION IN BOS AND RAT WAS REPLACED. SUSPECT DAMAGE TO TURBINE BLADE WAS INCURRED DURING STOWAGE POST LAX MAINTENANCE ACTIVITY.
EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN OFF POSITION. FOUND NO-SMOKING SWITCH IN AUTO. EMERGENCY EXIT LIGHTS WORK AUTOMATICALLY WHEN THE NO-SMOKING SWITCH IS IN THE AUTO POSITION AND THE LANDING GEAR IS EXTENDED. NORMALLY THE NO-SMOKING SWITCH IS OFF OR ON.
SIGNIFICANT AIRFRAME VIBRATION DURING CLIMB. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED ELEVATOR AND RUDDER CHECK. RIGGED BOTH ELEVATORS 0.5 NOSE UP. LEFT ELEVATOR BLUE SERVO ACTUATOR ROD END REPLACED. RIGHT MLG OUTER DOOR SEAL AFT SECTION LOOSE, REPLACED SEAL.
EPSU FWD LEFT FAULT DURING EMERGENCY LIGHT TEST.
RETURN TO FIELD WITH A NR 2 BLEED AIR FAULT. BLEED AIR FAULT GENERATED BY NR 2 BLEED SYSTEM OVERTEMPERATURE. FOUND FAULTY FAV THERMOSTAT,
DURING CLIMBOUT NR 2 ENGINE SHUTDOWN DUE TO FMU ECAM WARNING. FUEL METERING UNIT (FMU) REPLACED,
RETURNED TO ORD UNDER AMBER ALERT DUE TO ELECTRICAL PROBLEMS.
DOOR 1R PRESSURE LIGHT ILLUMINATED. *S/D* CHECKED THE GIRT BAR FOR DEBRIS, CYCLED THE DOOR CLOSED, AND ARMED AND DISARMED THE DOOR. ALL OPERATED NORMALLY.
APU FIRE DISCHARGE LIGHT IS ILLUMINATED. RED DISCHARGE INDICATOR IS PRESENT ON AIRCRAFT.