N462UA
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 | 2008-01-25 – 2008-01-25 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2008-01-25 – 2008-01-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SEVERE ENG 2 VIBRATION IN SEVERE ICING COND. FLIGHT CREW REPORT THAT ON DESCENT ENGINE RETURNED TO NORMAL OPE RATIONAL MODE WITH NO VIBRATION NOTED. ACCOMPLISHED INSPECTION OF ENGINE AS REQUIRED PER TSM 77-30-00-810-827-A FOR HIGH N1 VIBRATION LEVEL ON ENGINE 2 AND A VISUAL INSPECTION OF THE NR 2 ENGINE IAW AMM 72-00-00-200-01 0-A FOR INSPECTION OF THE ENGINE AFTER SLUSH INGESTION WITH NO DEFECTS NOTED.
CABIN PRESSURE CABIN DOOR WARNING LIGHTS FRONT/AFT FLASHING ECAM PRESS ZERO. COULD NOT DUPLICATE FAULT, TESTS PASSED, REMOVED AND REPLACED CABIN-PRESSURE DETECTION PRESSURE-SWITCH (FIN 14WN) PER AMM 52-73-12, OPS CHECK GOOD, DOOR FLASHES AND THEN TURNS OFF PROPERLY.
CRACKS OF 1.062" AND 0.218" OF LENGTH AT RH SIDE AFT PASSENGER/C REW DOOR CUTOUT UPPER CORNER RADIUS ABOVE STR 8 AND FR 68 WEB JO INT TO DOOR FRAME. GEN BY V947494 ON HAECO LCQ NR 9292561 / 3456 1 ACCOMPLISHED INTERIM RPR AT RH FR68 STRG 8R FR WEB STIFFNER AND FASTENERS HOLES IAW ECRA 5341-01481 PART1.1. DIP CREATED TO ACCOMPLISH A PERMANENT RPR AT RH FR68 STRG8R FR WEB STIFFINER AND FASTENER HOLES PER PART 3 OF THE LATEST REV OF ECRA 5341-01481 ON OR BEFORE 02-NOV-25. IAW ECRA 5341-01481 PART1.2. OK TO CARRY CRACKS OF 1.062" AND 0.218" OF LENGTH AT RH SIDE AFT PASSENGER/C REW DOOR CUTOUT UPPER CORNER RADIUS ABOVE STR 8 AND FR 68 WEB JO INT TO DOOR FRAME INTERM REPAIR TO ACCOMPLISH A PERMANENT REPAIR AT RH FR68 STGR8R FRAME WEB STIFFENER AND FASTENER HOLES PER PART 3 OF THE LATEST REVISION OF ECRA 5341-01481 ON OR BEFORE 02-NOV-25. TOMC-APPROVAL FROM SC1ELBYC COMMENT IN REF TO ECRA 5341-01481
AFT LAV SERVICE DOOR HAS OVER SIZED HOLE ON LATCH ATTACH HOLES. REMOVED AND REPLACED AFT LAV SERVICE DOOR IAW A320 AMM 52-42-11- 400-001.
FWD CARGO CORROSION ON STRINGER 40L FR 30. R & R SECTION OF STRINGER 40LT AND INSTALLED STRINGER REPAI R FR29-32 IAW A320 SRM 53-21-13-300-018 ACP RII INSP AS REQUIRED LC-81.
CRACK INDICATION AT LH FR 66 DOOR STOP #1 AT 6 OCLOCK POSITION L OWER I/B HOLE. REPAIRED LWR INBD HOLE ON FR 66 DOOR STOP #1 WITH BUSHING AND REPAIR WASHER. FINAL REAM .2820 IAW SRM 53-41-12-300-010 HFEC ACCOMPLISHED WITH NO FINDINGS.
DOUBLE JOGGLE AT RT FR 20 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER, 3 DIRECTION, 100% S.H. REPAIRED HOLE #6 AT RH FR20 DOUBLE JOGGLE WITH BUSHING AND RPR WASHER IAW SRM 53-11-12-300-012. FINAL REAM .2800 THIS IS A CAT B. COMPLETED DOUBLE JOGGLE AT RH FR 20 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER, 3 DIRECTION, 100% S.H. REPAIRED HOLE #6 AT RH FR20 DOUBLE JOGGLE WITH BUSHING AND RPR WASHER IAW SRM 53-11-12-300-012. FINAL REAM .2800 THIS IS A CAT B.
RH ELEVATOR O/B RIB I/B SIDE HAS CORROSION. REMOVED RIB ON RH ELEVATOR O/B RIB IAW A320 SRM 51-42-11/001, RE PLACED RIB ON RH ELEVATOR O/B RIB IAW A320 SRM 51-42-11/001.
L/H ELEVATOR HAS LIQUID INGRESS AT 107.5 IN FROM I/B EDGE, 18.5I N FROM TRAILING EDGE, 1.5IN DIAMETER GENERATED BY V061632 ON H ECO LCQ NR 9292772/34772 ESFR ENTRY REPAIRED LH ELEVATOR 107.5 IN FROM I/B 18.5 IN FROM T/E 1.5 IN D IA IAW A320 SRM 55-21-11-300-004. CATEGORY A REPAIR DRILLED WITN ESS HOLES IAW A320 AMM 55-20-00-200-006-A PARA 2A (6) FOUND NO L IQUID. PERFORMED BY V061628
FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-43R.
AFT WET AREA STRG 24RH ANGLE SPLICE CORRODED @ FRM 70. GENERATED BY V937268 ON HAECO LCQ NR 9292694/34694 SFR COMPLETED FOR LP 4361893 REMOVED SPLICE ON AFT AREA STGR 24RH FR 70 IAW A320 SRM 51-42-11 /001 REV 152 REPLACED SPLICE ON AFT AREA STGR 24RH FRM 70 IAW A3 20 SRM 51-42-11/001 REV. 152 ACMP BY V947495 INSP BY V901665
CRACK INDICATION AT RH FR68 DOOR STOP #1 AT 6 OCLOCK HRS POSITIO N LOWER I/B HOLE. ESFR COMPLETED
FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-F3R. FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-43R ESFR COMPLETED REMOVED AND REPLACED FWD CARGO CLEAT AT FR31 STR 42R-43R IAW A32 0 SRM 51-72-11-911-001.
R2 PAX DOOR LOWER FWD CORNER ANGLE FITTING CORRODED. GENERATED B Y V937268 PER HAECO LCQ NR 9292674/34674. REMOVED AND REPLACED CORNER FITTING AT R-2 PAX DOOR LOWER FWD IAW A320 SRM 51-42-11, SRM 51-72-11 REMOVED AND REPLACED CORNER FITTING AT R2 PAX DOOR LOWER FWD IAW A320 SRM 51-42-11 SRM 51-72-11 ACMP BY MECH V917176 INSP BY N07 8570
FWD CARGO CLEAT HAS CORROSION FR 31 STR 43R-43L. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R-43R IAW A320 SRM 51-72-11-911-001 WPB V061616. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R- 43A IAW A320 SRM 51-72-11-911-001.
FWD CARGO STRINGER SPLICE HAS CORROSION FR 31 STR 41L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR41L I/A/W A320 SRM 51--42-11-001. W/P/B V075620 REMOVED AND REPLACED FISHPLATE(SPLICE) @ FWD CARGO FR31 STR 41L IAW A320 SRM 51-42-11/001.
FWD CARGO STRINGER SPLICE HAS CORROSION FR 31 SRT 43L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR43L IAW 51-72-11. REMOVED AND REPLACED FISHPLATE SPLICE @ FWD CARGO FR 31 STR 43L IAW A320 SRM 51-72-11-911-00.
FWD CARGO CLEAT HAS CORROSION FR 31 STR 41R-42R. INSTALLED CLEAT @ FWD CARGO FR 31 STR 41R-42R I/A/W A320 SRM 51-72-11. W/P/B V075620 REMOVED AND REPLACED CLEAT FWD CARGO FR31 STR 41R-42R IAW A320 S RM 51-42-11-001 P6.
L/H FWD EMERGENCY EXIT HATCH FWD. VERTICAL FRAME IS CRACKED. COMPLETED L/H FWD EMERGENCY EXIT FWD VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-72-11-911-002.
R/H AFT EMERGENCY EXIT DOOR FWD VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR FWD VERTICAL SEGMENT REMOVED AND REPL ACED IAW A320 SRM 51-42-11/001 51-72-11-911-002.
R/H AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME SEGMENT REMOVED AN D REPLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002.
L/H AFT EMERGENCY EXIT HATCH AFT. VERTICAL FRAME IS CRACKED. COMPLETED L/H AFT EMERGENCY EXIT AFT VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002
R/H ELEVATOR HAS LIQUID INGRESS AT 146IN FROM I/B END, 5IN FROM TRAILING EDGE, 1.5IN DIAMETER.
R/H ELEVATOR HAS LIQUID INGRESS AT 168.5IN FROM I/B END, 4.5IN F ROM TRAILING EDGE, 1IN DIAMETER.
R/H ELEVATOR HAS LIQUID INGRESS AT 74.5 FROM I/B END, 8IN FROM T RAILING EDGE, 1IN DIAMETER. GENERATED BY V061632 ON HAECO LCQ NR 9292782/34782 ESFR COMPLETE REPAIRED RH ELEVATOR 74.5 IN FROM I/B 8 IN FROMT/E 1.5IN DIAMETE R IAW A320 SRM 55-21-11-300-005 CATEGORY A REPAIR.
R.H ELEVATOR HAS LIQUID INGRESS AT 180.5IN FROM I/B END, 10IN FR OM TRAILING EDGE. 1IN DIAMETER. REPAIRED RH ELEVATOR 180.5 IN FROM I/B 10IN FROM T/E 1.5IN DIAME TER ZONE A IAW A320 SRM 55-21-11-300-005 CATEGORY A REPAIR
LH ELEVATOR HAS LIQUID INGRESS AT 138 IN FROM INBOARD EDGE, 5.5I NIN FROM TRAILING EDGE, 1IN DIAMETER REPAIRED LH ELEVATOR IAW A320 SRM 55-21-11-300-005
LH ELEVATOR HAS LIQUID INGRESS AT 52 IN FROM INBOARD EDGE, 5 IN FROM TRAILING EDGE, 2 IN DIAMETER.
RH AFT TI-ANGLE IS CRACKED. ESFR COMPLETED REMOVED SECTION-CONNECTING (TI-ANGLE) ON RH AFT FR41-42 KEEL BEA M IAW A320 SRM 51-42-11/001 REV 152 REPLACED SECTION CONNECTING (TI-ANGLE) IAW A320 SRM 51-42-11/001 REV 152.
R2 DOOR LOWER AFT CORNER ANGLE FITTING CORRODED. ESFR COMPLETE RMVD + RPLCD CORNER FITTING AT RE PAX DOOR LWR AFT IAW A320 SRM 51-42-11 + SRM 51-72-11.
L2 PAX DOOR LOWER FWD ANGLE FITTING CORRODED. ESFR COMPLETE R & R CORNER FITTING AT L2 PAX DOOR LWR FWD IAW A320 SRM 51 -42-11 + SRM 51-72-11
AFT WET AREA FLOOR SUPPORT Y160.5 FASTENER HOLES CORRODED APPROX. 5 " FWD OF FRM 70. ESFR COMPLETE RMVD CORROSION ON FLOOR SUPPORT Y160.5 FOUND OUT OF LIMITS RMVD DMG FLOOR SUPPORT Y160.5 RECEIVED NEW FLOOR SUPPORT RPLCD COMPONENTS TRANSFERRED DRILL HOLES + DEBURR + INSTALLED NEW FLOOR SUPPORT Y160.5 ON AFT WET AREA FR68-FR70 IAW A320 SRM 53-41-14-283-009/SRM 51-42-11 / SRM 51-72-11-911-001.
LH AFT TI-ANGLE IS CRACKED. RMVD TI-ANGLE IAW A320 SRM 51-42-11/001 REV.152 RPLCD TI-ANGLE O N LH AFT FRM 41-42 KEEL BEAM IAW A320 SRM 51-42-11/001 REV.152
OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAILED TEST. EPSU BATTERY AFT L MESSAGE CAME UP. REPLACED EMER LIGHT BATTERY AT DOOR 2L. EMER LIGHT TEST AT PTP PANEL PASSED.PARTS USED: 18-3351-3-0001,QTY :1
PRESSURIZATION OUTFLOW VALVE STUCK FULL OPEN. UNABLE TO PRESSURI ZE IN AUTO OR MANUAL. ON TAXI OUT, DEICE, TAKE OFF OUTFLOW VALVE STUCK OPEN, FLIGHTCREW HIT DITCHING SWITCH WHILE DEICING STILL DID NOT CLOSE. ON GROUND CABIN PRESSURE SWITCHED TO MANUAL CLOSE AND CLOSED,SWITCHED TO AUTO AND OPENED TO FULL OPEN. PHOTO ADDED SDR FLAGGED PREFORMED LAST FLT FAULTS, PREVIOUS FAULTS, CLASS 3 AND TEST/ CALIBRATION ON BOTH CPC, NO FAULTS FOUND, PREFORMED SAME CHECKS ON BOTH BMC WITH NO FAULTS FOUND. PRESSURIZED ACFT NO PORBLEMS FOUND WITH PRESSURIZATION RAN BOTH ENG VERIFIED BLEED SYS TO OPERATE NORMALY AND VEIRFIED MANUAL MODE WORKS ON CABIN PRESSURIZATION, PRESSURIZATRION CHECK GOOD VERIFIED DITCHING SYS CLOSED OUTFLOW VALVE NORMALY R&R OTBD SAFETY VALVE (6HL) REF AMM 21-31-52. REMOVED INBD SAFETY VALVE (7HL) REF AMM 21-31-52. WAITING FOR NEW ONE TO ARRIVE R&R INBD SAFETY VALVE (7HL). REF AMM 21-31-52. OPS CHECK GOOD.ADD EMP:U379654 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1338313 SN OFF 2326 VALVE, SAFETY O OFF 31-2131-9-0001 2326 ON 31-2131-9-0001 1320 PRESSURIZED THE A/C PER TOMC TO 7.9 AND LET IT SIT FOR 5 MINUTES. MAINTAINED PRESSURE NO PROBLEM. REF AMM 05-53-00-780-002-A01. CHANGED BOTH SAFTEY OUTFLOW VALVES 6HL AND 7HL PRECAUTIONARY.
FUEL CAP MISSING AT DEPARTURE. FUEL CAP MISSING AT ARRIVAL. REFUEL CAP NON STOCK SFO. M&E COMPLIED WITH IAW CDL 28A 18-2825-3-0037. REQUEST CDL 28A ADD EMP:401062 DISPATCH DESK: S11 NAME: D.C. DATE: 23-NOV-23- OKAY TO CDL 28A.
F/CTL FLAP SYS 1 FAULT ON CLB OUT. FLAP IND FLAPS2 AND INDICATI NG NOT RETRACTED. ADDED PHOTO OF PFR PER TSM 27-51-00-810-811-A, PERFORMED SFCC SYSTEM OPERATIONAL AND AMM 27-51-34-400-001. PERFORMED BOTH OPERATIONAL TEST OF THE 31-2750-9-0001,QTY :1 TESTS REF AMM 27-54-00-710-001. OPS TEST GOOD, NO FAULTS FOUND. FLAP AND SLAT SYSTEMS REF AMM 27-54-00-710-002-A AND OPERATIONAL ROTABLE PARTS CHANGE WAS INDICATED - TT # 1835642 SN OFF 2523 REF LP 5106508 AS CSU (51CV) WAS JUST CHANGED. REMOVED AND TEST OF THE FLAPS (AGAIN) REF AMM 27-54-00-710-001. BOTH OPS REPLACED SFCC 1 (21CV) PRECAUTIONARILY REF AMM 27-51-34-000-001 TEST GOOD, NO FAULTS NOTED AT THIS TIME. PARTS USED: COMPUTER, SLAT OFF 31-2750-9-0001 2523 ON 31-2750-9-0001 2253
TOILET SERVICE PANEL HAS 2EA CRACKS ONE ABOVE EACH HINIGE REPAIRED TOILET SERVICE PANEL (2EA CRACKS) PER SRM 53-41-79-300- 001. EMP: V934143 WC: 54348 STA: ST ENG BFM ALL INSPECTIONS ACCOMPLISHED ON STENGINEERING NRC 54348 AT BFM
DURINIG ROTO INSP OF THE FRAME FOOT AT RH FR43. CRACK INDICATION NOTED IN THE FASTNER HOLE AT 3 O''CLOCK (VIEW LOOKING FWD) ON BO TH LAYERS REPAIR BEFORE NEXT FLIGHT REAMED HOLE INCRENNETALLY STEP BY STEPS WITH NDT INSPECTION AFTE R EACH REAMED TO MAX SIZE (0.4000") FRAME REPLACEMENT REQUIRED I AW DWG R5337022 AND EA# 5330-06692 OPT 4. EMP: V940362 WC: 54690 STA: ST ENG BFM ALL INSPECTIONS ACCOMPLISHED ON STENGINEERING NRC 54690 AT BFM
DURING THE THERMOGRAPHIC INSPECTION OFTHE RIGHT ELEVATOR UPPER S URFACE 8EA. WATER INDICATION WERE NOTED AND MARKED IN RED. REMOVED RH ELEVATOR, REPAIRED AND INSTALLED IAW AMM 27-34-41-000 SRM 55-21-11-300-003; SRM 51-75-12; SRM 51-21-11; SRM 55-21-15; -001A; SRM 51-25-11; SRM 51-25-12; SRM 55-20-00-283-001; SRM 55- SRM 55-26-41-300-003, AMM 27-34-41-400-001-A. WC: 5 21-11-300-005; SRM 51-77-11-911-012; SRM 55-21-11-300-016; SRM 5 4796 STA: ST ENG BFM 1-42-11; SRM 51-77-11-911-014; SRM 55-21-11-300-005
TOILET SERVICE PANEL HAS 2EA CRACKS ONE ABOVE EACH HINIGE
RH FWD AVIONICS DOOR HAS LIGHTING STRIKE REPAIRED FWD AVIONICS DOOR IAW A-320 SRMM 52-41-00-300-001 FIG 01 SHEET 02, THIS REPAIR IS CATEGORY "A" WC# 54341 EMP V936039
DURINIG ROTO INSP OF THE FRAME FOOT AT RH FR43. CRACK INDICATION NOTED IN THE FASTNER HOLE AT 3 O''CLOCK (VIEW LOOKING FWD) ON BO TH LAYERS REPAIR BEFORE NEXT FLIGHT
RH FWD AVIONICS DOOR HAS LIGHTING STRIKE REPAIRED FWD AVIONICS DOOR IAW A-320 SRMM 52-41-00-300-001 FIG 01 SHEET 02, THIS REPAIR IS CATEGORY "A" WC# 54341 EMP V936039
ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD ECAM PROC COMPLETEDACCUMULATOR STILL OK STARTED PARTIAL REMOVAL OF ACCUMULATOR AS PER AMM TASK 29-13-42-000-001-A UP TO AND INCLUDING STEP 3. D. LOCKING LOG FOR MX TO DETERMINE SOURCE OF LOSS. SERVICED YELLOW SYSTEM AND PRESSURIZED AND FOUND YELLOW POWER PICTURE FOR REFERANCE ENCLOSED. ACCUMULATOR TO BE LEAKING, FOUND LOOSE B-NUT ON TOP OF ACCUMULATOR LOOSE, RE TORQUED RECHECHED AND STILL LEAKING, SUSPECT EITHER BAD O-RING OR BAD UNION, HAVE BOTH IN STOCK, FOUND LEAK REMOVED AND REPLACED UNION AND O-RING FROM YELLOW POWER 00-0594-3-1415,QTY :1 ACCUMULATOR IN REFERENCE WITH TASK 29-13-42-400-001-A. VERIFIED YELLOW SYSTEM HOLDS PRESSURE. OPS CHECK GOOD , NO LEAKS DETECTED. PARTS USED: 40-0595-3-1983,QTY :1 ADD EMP:U389333
EVAC COMMAND ALARMSOUNDED DURING TAKEOFFROLL AT HIGH SPEED. LOCKING DUE TO MULTI CIDS 1 & 2 FAULT AFTER T/O UNLOCKING FOR UPDATE UNABLE TO PRODUCE FAULTS. FOUND FAULT HISTORY OF COMMUNICATION ERRORS IN POST FLIGHT REPORT. PRECAUTIONARILY R&R BOTH CIDS DIRECTORS PER AMM 23-73-34/401 CONFIG 00. OPS CHECK GOOD. PARTS USED: 31-2300-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1871287 SN OFF 6319 TT # 1775955 SN OFF 3204 UNIT, DIRECTOR- OFF 31-2300-9-0002 6319 ON 31-2300-9-0002 6685 UNIT, DIRECTOR- OFF 31-2300-9-0002 3204 ON 31-2300-9-0002 4362
PDA 3 REF LP 8457922 MISSING FASTENER #1 ENGINE PYLON PANEL 472BR LOG GENERATED UNDER GMM 02-30-95 .REMOVED PANEL AND INSTALLED NEW NUT PLATE. RE INSTALLED PANEL AS PER LP 8457922
L1 FR 16, DOOR STOP #7, IB UPPER AND LOWER HOLES HAVE CRACK INDI CATIONS IN INTERCOSTAL @ 5 O''CLOCK DIRECTION PER HAECO LCQ NON R OUTINE 9294084 . OPEN
FLY #349 ORD TO IAD. ABOUT 20 MILES OUT OF ORD HEADING EAST. FLEW INTO A HAIL STORM, OUT OF NOWHERE. WAS FLYING AT 250 KNOTS, AT 13,000 FEET. CAPTAINS WINDOW WAS DAMAGED ALMOST EVERY WHERE. FIRST OFFICERS WINDOW HAS A LARGE CRACKS ACROSS WHOLE WINDOW AND 4 HITS ON TOP RIGHT OF WINDOW . AC GAVE ONLY ONE EXAM MSG, WINDOW HEAT. CREW DID NOT NOTICE ANY PROBLEMS WITH AIRCRAFT AND ENGINES. LANDING NML AT THE AC WEIGHT OF 145. SEE ATTACHED PHOTOS.
PDA 2 ON WALK AROUND FOUND FUEL CAP MISSING MADE LOGPAGE SDR ADDED PARTS NEEDED PLACED MISSING FUEL CAP ON CDL. DDP COMPLIED WITH. DISPATCH DESK: 12 DATE: 07-MAR-20- CDL APPROVED. PLACED MISSING FUEL CAP ON CDL. DDP COMPLIED WITH. REPLACED MISSING FUEL PANEL CAP
NO WATER PRESSURE THROUGHOUT AC DURING FLT, WATER QTY INDICATES FULL ON FAP. REPORTED BY CREW TOMC SMITH FOUND ICE BUILDUP AT OVERFLOW / TANK DRAIN PANEL. AFTER THAWING POPPED. REMOVED FWD PIT AFT BULKHEAD PANEL AND FOUND OVERFLOW VLV TANGLED WITH INSULATION. SECURED INSULATION, RESET CB, ACTUATED OVERFLOW VLV. OPS NORMAL, LEAK CHECK GOOD. SYSTEM ADD EMP:U117370 AND REMOVING ICE FOUND OVERFLOW NOT FULLY CLOSED AND AFT CB REINSTALLED PANEL. CONFERRED WITH MCNEELY AND SMITH. HOLDING PRESSURE AND WATER PRESSURE GOOD IN LAVS AND GALLEYS.
LEFT MIDDLE FLAP TRACK FAIRING MISSING TWO BOLT COVERS. INSTALLED FLAP TRACK FAIRING BOLT COVERS AND CREATED PDA 3 WRITE UP
LT FRAME 35 STRINGER 30 HOLE 2 IS CRACKED IN SIDE SHELL LAYER AT 5:00 OUTBOARD LOOKING INBOARD A3NB-53-3-6315 PER NON ROUTINE 9296254 INTERIM REPAIR ACCOMPLISHED PER ECRA 5331-02382 PART 1. A PERMANENT REPAIR NEEDS TO BE ACCOMPLISHED PER PART 3 OF ECRA 5331-0238 2 ON OR BEFORE THE AIRCRAFT REACHES 36398 TOTAL AIRCRAFT FLIGHT CYCLES OR 85121 TOTAL AIRCRAFT FLIGHT HOURS, WHICHEVER COMES FIRST. PLANNING TO CONTACT ENGINEERING AFTER 34398 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 35398 TOTAL AIRCRAFT FLIGHT CYCLES FOR MADE PERMANENT WITH REPEAT INSPECTIONS. ATED FOR DAMAGE TOLERANCE UNDER 14CFR26.43(D) AND WILL LIKELY BE THE PERMANENT REPAIR. NOTE TO PLANNING: THIS ECRA IS BEING EVALU OR 85121 TOTAL FLT HOURS,
FWD CARGO FR32 CLEAT STR 43R TO STR 42R CORRODED A3NB-52-3-6105 PER NON ROUTINE 9296790. REMOVED AND REPLACED CLEAT ON FRAME32 STR 43R TO STR 42R IAW SRM 51-42-11.
AFT PIT STRINGER 37R BETWEEN FR58-59 HAS CORROSION ON REF 9297030 SPEC A3NB-05-3-6026. PERFORMED STGR SPLICE REPLACE/REPAIR IAW SRM53-00-13-300-001 FRO M FR58 TO 8"AFT OF FR59. ECRA5341-01166 GENERATED TO ALLOW SUBST ITUE MATERIAL USE FROM SRM. REPAIR REQ''S REINSPECT AT 60,000FC OR 120,000FH FROM REPR EMBODIMENT WHICHEVER COMES FIRST IAW SRI5 3-00-13-205-001 TBL05.
LT BETWEEN FR35 & 36 HAS 60 HOLES. HOLE NUMBER 16 IS CRACKED IN THE 7 ''CLOCK POSITION. ALL OTHER HOLES I/B OF CUT OUT HAVE NO REJECTABLE INDICATIONS. HOLES O/B & ALL HOLES IN CROSSBEAM ATTACHMENT HAVE OUT OF ROUND/REJECTABLE DAMAGE. REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE ON REF 9296967 AD RELATED (2018-06 -04). WHILE ACCOMPLISHING EA5330-05216 INSPECTION SEVERAL HOLES WERE FOUND TO BE CRACKED. ACCOMPLISHED REPAIR PER PART 1 OF ECRA5331-0 2380. DTA, ACCOMPLISH PERMANENT REPAIR AT FUSELAGE FR35-36R PRESSURE PANEL HOLES PER PART 3 OF ECRA5331-02380 ON OR BEFORE 2 5OCT2019. PLANNING TO CONTACT ENGINEERING AFTER 25AUG2019, BUT BEFORE 25SEP2019 FOR PERMANENT REPAIR.
AFT CARGO STRINGER 41 RT FRAME 59 CORROSION A3NB-05-3-6026 PER NON ROUTINE 9296887. REMOVED CORROSION ON STR41RH AT FR59 ORIG.142 REMAINING .096 MAT LOSS .046 L=3W=.5 FOUND TO BE OUT OF LIMITS IAW SRM 51-73- 00 REMOVED AND REPLACED STR41RH FROM FR58 TO FR64 IAW SRM 5 1-42-11-001 AND 51-72-11-911-001 REMOVED DOT Y275.
LT ELEVATOR OB PCU ATTACH POINT BUSHING BORE CORRODED A3NB-55-3-0001 PER NON ROUTINE 9297051 REMOVED AND REPLACED LT ELEVATOR PCU ATTACH FITTING IAW SRM 53-26-47-300-003 CATEGORY A PERMANENT PREPAIR.
LT FWD EXIT DOOR INTERNAL STRUCTURE AFT INTERCOASTAL CRACKED. REMOVED AND REPLACED THE INTERCOASTAL IAW SRM 51-72-11-911-001.
RH ELEVATOR IB AND OUTBD PCU ATTACH FITTINGS CORRODED AT BUSHING BORES A3NB-55-3-0001 PER NON ROUTINE 9297050. REMOVED AND REPLACED RH ELEVATOR I/B AND OUTBOARD PCU ATTACH FIT TINGS IAW A320 SRM 55-26-47-300-003.
FWD CARGO STR41RT SPLICE JUST FWD OF FR31 HAS CORROSION A3NB-52- 3-6105 PER NON ROUTINE 9297041. REMOVED AND REPLACED FWD CARGO SPLICE AT FR31 STR41R IAW A320 SR M 51-42-11
AFT CARGO TORQUE BOX WEB CORROSION MANY SPOTS. REMOVED AND REPLACED AFT CARGO TORX BOX WEB IAW A320 SRM 51-72-11.
L-1 DOOR CUTOUT FR-16 DOOR STOP NR 1 LOWER INBOARD HOLE CRACKED IN FRAME INTERCOSTAL PER NON ROUTINE 9296414 ACCOMPLISHED INTERIM REPAIR PER ECRA 5311-02133. IT IS REQUIRED TO ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT THE LT FR16 DOOR STOP NR 1 AS PER PART 2OF ECRA 5311-02133 ON OR BEFORE THE AIRCRAFT REACHES 37898 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH THE REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12900 AIRCRAFT FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS ARE FOR AS PER PART 1 OF THIS ECRA IS CONSIDERED PERMANENT PROVIDED 2133 PART 2. PER ECRA 5311-02133 PART 3 THE REPAIR ACCOMPLISHED LT FR16 DOOR STOP FITTING NR 1 HOLE NR 3 AND HOLE NR 4 PER ECRA 5311-0 ALL THE STATED INSPECTION REQUIREMENTS PER PART 2 OF THIS ECRA A RE COMPLIED WITH. DOOR STOP NR 1 AS PER PART 2 OF EC/RA 5311-02133 ON OR BEFORE THE AIRCRAFT REACHES 37,898 TOTAL FLIGHT CYCLES. ACCOMPLISH THE REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,900 AIRCRAFT FLIGHT CYCLES THEREAFTER. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT THE LT FR 16 TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
L2 DOOR EVACUATION SLIDE ASSY GIRT BAR CNTR PAACHUTE PIN IMPROPERLY ROUTED A3NB-25-3-6099 PER NON ROUTINE 9297148. INSTALLED AND PROPERLY SAFETIED PARACHUTE PIN ON L2 DOOR GIRT BAR SLIDE IAW A320 AMM 25-62-44-420-064A
RH DOOR STOP AT FR16 FTG 7 I/B LOWER HOLE HAS REJECTABLE CRACK I NDICATION PER HAECO LCQ NON ROUTINE 9296413 GENERATED BY V923744 REAMED FR16 FTG #Y I/B LOWER HOLE TO CRACK FREE CONDITION AT .28 0 IAW ECRA 5311-02124 REMOVED AND REPLACED R-1 #7 INTERCOSTAL IA W ECRA 5311-02124 PERFORMED BY V925705 MECH V913402 INSP BY LC-1 0
AFT CABIN RH SHEAR PLATE HAS A CRACK A3NB-53-3-6222. REMOVED AND REPLACED AFT CABIN SHEAR PLATE BETWEEN FRAME 68 TO FRAME 69 ON RIGHT HAND SIDE IAW A320 SRM 57-72-11-911.
L2 DOOR SILL HAS CORROSION AT FR66 A3NB-53-3-6222. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-72-11-911-001 .
R2 DOOR SILL HAS CORROSION AT FR66 AND 68 A3NB-53-3-6222. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.
DOOR LEFT FWD EMERG EXIT ECAM UPON LANDING FOUND SENSOR TARGET BY THE HANDLE TO REMOVE EMERGENCY DOOR. REATTACHED SENSOR, MESSAGE ON ECAM IS GONE. REF AMM52-73-11-400-00 3.
LT OVERWING SLIDE EXIT DOOR T/E IS DISBONDED. REPLACED SLIDE, RAMP-OFFWING LT REF MM 25-62-46/401.
L1 DOOR EMERGENCY CYLINDER IS BAD. REMOVED AND REPLACED ACTUATOR PAX DOORS REF AMM 52-11-14/401
ROW 20ABC EXIT COVER ON SIDEWALL IS MISSING. REPLACED THE COVER AND BULBS. SIGN SECURED AND LIGHT CHECKS NORMAL.
CORROSION FOUND ON STRINGER 31R AT AFT OF FRAME 65. R & R STRINGER 31R AT FRAME 64 - 67 IAW SRM 51-42-11 PARA 6 & 7.
CREW REPORTS SMOKE & ODOR FROM FWD AFT LAVATORY UNDER SINK AREA. SMOKE WAS WHITE WITH ACRID ELEC TYPE SMELL. FLIGHT ATTENDANT DISCHARGED A HALON EXTINGUISHER UNDER SINK AT WATER HEATER & TOWARD AFT AREA OF COMPARTMENT. NO CB'S TRIPPED IN FLIGHT DECK. INSPECTED LAVATORY AS REQUIRED IAW AMM 05-51-10-200-801C. FOUND FWD AFT WATER HEATER EMITTING ODOR. INSPECTED WIRING IN ADJACENT AREA, NO DAMAGE FOUND. REMOVED TOP COVER OF WATER HEATER & CONFIRMED STRONG ODOR PRESENT. DEACTIVATE & DEFER WATER HEATER.
PER A CHECK, FOUND EPSU FAULT AFT LT. REPLACED AFT LT EPSU BATTERY, OPERATIONS CHECKED GOOD.
EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 32C IAW AMM, OPERATIONS CHECKED OKAY.
ENG 2 EXHAUST TAIL CONE IS CRACKED AT FWD PORTION BETWEEN 2 & 5 O'CLOCK. APPROXIMATELY 7 TO 9 INCHES LONG. IAW AMM78-11-12 601 FOR EXHAUST CONE PCN 115-0004 ALLOWABLE DAMAGE LIMITS. REPORTED 9.0 INCH CRACK BETWEEN 2 & 5'0 CLK. IN ZONE 1, BEYOND ALLOWABLE LIMITS OF AMM 78-11-12-200-0 11-C. STOPPED DRILLED IAW ECRA 7811-01215.
ENG 1 START VLV DID NOT OPEN AT ENG START. REPLACED START VLV IAW AMM 80-13-49-400-010-B13. OPERATIONS NORMAL.
NR 1 PRECOOLER INLET PRESSURE FLUCTUATES UP TO 10 PSI WITH HP VALVE OPEN IDLE POWER. AUDIBLE.
DURING CLIMB, NOTICED NR 2 PRECOOLER OUTLET TEMPERATURE IS AMBER, INDICATOR 115 DEGREES & DECREASING. AC HAS MESSAGE OF FAN AIR V 9HA2 OR THERMOSTAT 7170 HM2. REPLACED FAN AIR THERMOSTAT. CHECKED PRECOOLER FOR MISSING COOLING TUBES NO MISSING TUBES. ACP ENGINE RUN BLEED TEMPERATURES OK & STABLE. OK FOR SERVICE
VERY LOUD SQUEAL ROW 1-2 NEAR WALL-FLOOR. PRESSURIZED ACFT IAW AMM 05 -53-00-780-03. FOUND CAPTAINS AOA SENSOR ATTACHMENT SCREWS LOOSE, SECURED. FIRST OFFICERS AOA BLANKING PLATE CLOCKED WRONG. REINSTALLED IAW MM. NO NOISE NOTED.
LOUD SQUEAL ABOVE SEAT 2A. REMOVED PSU ABOVE SEATS 2A & 2B, REMOVED SIDEWALL CEILING PANELS ABOVE ROWS 2 & 3 LT SIDE. AIR ESCAPING FROM RISER DUCT WHERE IT ATTACHES TO INDIVIDUAL AIR SUPPLY DUCT ABOVE SIDEWALL AT ROW 3, ADJUSTED & SECURED CLAMP, NO NOISE NOTED. FLIGHT ATTENDANT SAYS THERE IS A HIGH PITCH NOISE AT SEAT 1A WINDOW OPERATED PACKS, NO SQUEAL , PHYSICAL CHECK , DOOR SEAL 1L, WINDOWS AT 1A,2A,3A EXTERIOR & INTERIOR ALL APPEARS OK. VERY LOUD SQUEAL ROW 1-2 NEAR WALL-FLOOR. PRESSURIZED AC, FOUND CAPT AOA SEN OR ATTACHMENT SCREWS LOOSE, SECURED. ALSO FOUND FIRST OFFICERS AOA BLANKING PLATE CLOCKED WRONG. REINSTALLED IAW SAME MM.
EMERGENCY LIGHT PANEL AT L1 DOOR LOOSE, STICKING OUT INTO DOOR WAY. SECURED LOOSE EMERGENCY LIGHT PANEL.
NLG STRUT REPORTED FLAT WITH NO FLUID LEAKAGE. REPLACED NLG CHARGE VALVE AND O-RING AND ACCOMPLISHED NLG STRUT SERVICE REF AMM 12-12-32. NO ACTIVE LEAKS.
LEFT MLG LOCK STAY ACTUATOR HAS A RUNNING LEAK. REPLACED ACTUATOR, OPS AND LEAK CHECKED OK.
EMERGENCY LIGHTS WILL NOT PASS TEST. RESEATED CONNECTOR AT 1L, RAN TESTED OK.
EPSU UNIT RT, FAILED TEST. R & R ESPU, OPS CHECKED GOOD.
CAPTAIN REPORTED NR 2 ENGINE OIL LEAK. RAN NR 2 ENGINE AND 27 DROPS PER MINUTE COMING FROM BREATHER DUCT OUTLET RIGHT SIDE FAN COWL. SUSPECT DEOILER SEAL ASSY. REPLACED NR 2 ENGINE DEOILER SEAL. RAN ENGINE, NO LEAKS NOTED. IAW AMM. 72-60-31 & 72-61-49.
NR 2 ENGINE THRUST REVERSER FAULT, FLT DIVERTED. ON LANDING NR 2 ENGINE THRUST REVERSER FAILED TO DEPLOY. UNABLE TO DUPLICATE PROBLEM. INSPECTED WIRING ON NR 2 THRUST REVERSER, ACCOMPLISHED SEVERAL ENGINE RUNS, BITE OF NR 2 EEC ALL OK. REPLACED NR 2 EEC AS A PRECAUTION IAW MM73. ACCOMPLISHED OPS CHECKS OF EEC, RAN THRUST REVERSER SEVERAL TIMES WITH ENGINE RUNNING, NO FAULTS FOUND.
COCKPIT DOOR VERY DIFFICULT TO OPEN ONCE AIRCRAFT PRESSURIZED IN CRUISE. ADJUSTED FLIGHT DECK DOOR HEIGHT REF AMM MT52-18.
NR 1 ENGINE INTAKE LIP HAS ONE SHEARED OR BROKEN RIVET 7 O`CLOCK POSITION FORWARD ROW OF RIVETS. ONE MISSING RIVET.
G RSVR LO LEVEL EICAS, FLT DIVERTED. PER CREW GROSS LANDING WEIGHT EXCEEDED BY 800 LBS. SAMC TEXT: CREW REPORTED SMOOTH TOUCHDOWN ABOUT 180 FT-MIN. ACCOMPLISH A OVERWEIGHT LANDING INSP. NO FAULTS NOTED RLAR AT 6 NOTIFIED. FOUND O-RING DAMAGED & LEAKING ON NR 1 ENG GREEN PUMP CASE DRAIN CHK VLV. REPLACED O-RING. SERVICED GREEN SYS HYD, RAN ENG & ALL HYD PUMPS. NO LEAKS NOTED
R2 DOOR SILL HAS CORROSION AT AFT GIRT FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION FROM R2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-42-11.
EXISTING DENT (CF9042) AT FR 23 BETWEEN STR 22L-23L WAS EVALUATED & FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE & FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-11-11 FIG 212.
NR 1 ENGINE UPPER PYLON HYD LINE FWD GANG CLAMP CHAFED INTO PYLON STRUCTURE. LEFT SIDE FWD OF PRECOOLER IN TWO PLACES. AFTER BLENDING FOUND TO BE OUT OF LIMITS IAW A320 SRM. REMOVED AND REPLACED PILLAR ASSY IAW A320 SRM.
LAV D WALL PBE LOST VACUUM SEAL. REPLACED PBE IAW A320 MM.
ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN - APU. REMOVED APU. APU HOURS ON RMV'D APU 6 START ATTEMPTS 15 START CYCLES 10. ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN. REPLACED APU.
IN FLIGHT START OF APU ATTEMPTED. 8000FT 250KTS AUTO SHUTDOWN AT 20 PERCENT N1. APU CB'S COLLARED PER MEL. REPLACED APU FCU PER MM, OPERATED APU SEVERAL TIMES OK. NO LEAKS. LEADS CHECK OK. REMOVED AND REPLACED IGN BOX. OK FOR SERVICE IAW AMM.
FLIGHT ATTENDANT REPORT LOW FREQUENCY VIBRATION CENTER AISLE AROUND EXIT ROW. CYCLES ON AND OFF. FOUND TAPE TORN, NOTED RT FAIRING PANEL SEAL LOOSE AND LIFTED UP. APPLIED TAPE OVER SEAL PER MT 53-04. NO OTHER DEFECTS. FOUND SEAL IN GOOD CONDITION. REPLACED SEVERAL SCREWS TO SECURE LOOSE FAIRING PANEL.
7F HAS SHARP METAL PROTRUDING FROM THE SIDE OF THE SEAT. COVERED EDGE WITH TAPE TO REMOVE CUT HAZARD, IS INTERIM REPAIR PER GMM 05-30-06. ADJUSTED SIDE PANEL.
EMERGENCY LIGHTS TEST FAILED FWD BATTERY AND AFT BATTERY. REPLACED EPSU BATTERIES AT FWD LEFT AND AFT POSITIONS. EMER LIGHTS TEST PASSED.
F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: F/O O2 MASK FAILS SELF TEST. REPLACED WITH SERVICEABLE UNIT. OPS AND LEAK CHECK GOOD.
PTP PANEL FAILED FORWARD EPSU L. REPLACED BATTERY, OPS CHECKED GOOD.
EMERGENCY POWER SUPPLY UNIT 11WL IS OUT OF TOLERANCE. REPLACED AND OPS CHECKED EPSU 11WL AT C-03 VISIT. ALL OKAY.
CAPT COCKPIT OXYGEN PRESS TO TEST SWITCH INOP. SWAPPED BOX FROM 1ST OBS SEAT. REPLACED OBS O2 BOX, LEAK CHECKED GOOD. TESTED OKAY.
VENT BLOWER FAULT ON ECAM, FLT DIVERTED. REPLACED AVIONICS EQUIP VENTILATION COMPUTER (AVEC) PER AMM, TESTS OKAY.
LEFT WING ROOT PANEL HAS EXTERNAL DAMAGE TO ALLUMESH PLY 12 X 18 INCHES. OUT OF REPAIR LIMITS. CONTACTED SFOLE AND ORDLE, NO RELIEF. PANEL NEEDS TO BE REPLACED OR REPAIRED AT SHOP 273. PANEL REPAIR. REPLACED PANEL.
AFT GALLEY C/B R41 OUT, SMELL SMOKE IN AFT GALLEY. REMOVED OVEN R41, TO INSP WIRING, NO DEFECTS NOTED. RE-INSTALLED OVEN. PULLED AND CAPPED C/B. REPLACED COFFEEMAKER.
AFT GALLEY C/B R41 OUT ODOR OF SMOKE IN AFT GALLEY. REMOVED OVEN R41, TO INSP WIRING, NO DEFECTS NOTED. RE-INSTALLED OVEN. PULLED AND CAPPED C/B.
AFT GALLEY C/B R41 OUT, SMELL SMOKE IN AFT GALLEY. REMOVED OVEN R41 TO INSP WIRING, NO DEFECTS NOTED. RE-INSTALLED OVEN. PULLED AND CAPPED C/B. REPLACED COFFEEMAKER.
RTFL DUE TO COMPLETE ELECTRICAL FAILURE WITH LOSS OF COMMUNICATION AND INSTRUMENTS. GEAR COMMANDED TO RETRACT AND DID NOT. F/O'S PFD POWERED, BUT NO AIRSPEED OR AIR DATA INDICATIONS.
CAPTAIN'S O2 WILL NOT TEST. CAPT O2 BOX IS LEAKING. REPLACED CAPT O2 STOWAGE BOX ASSY, LEAK CHECKED ALL LINES, OPS CHECKED GOOD.
NR 1 LT DOOR SLIDE BROKEN. REPLACED SLIDE ASSY.
RAT WILL NOT STOW. *S/D* RAT SOLENOID FAULTY. REPLACED RAT SOLENOID AND PRESSURE SWITCH. RETRACTION NORMAL.
DOOR 1L SLIDE BOTTLE PRESSURE LOW. LOSS OF PRESSURE DUE TO DIAPHRAGM RUPTURED AND STRIKER PIN BROKEN. REPLACED DIAPHRAGM AND STRIKER PIN AND RECHARGED BOTTLE.
NW STEERING FAULT DISPLAYED WHEN PUTTING GEAR DOWN. [06-26-07] REPLACED STEERING SEVO CONTROL 6GC AND BSCU STEERING. DETERMINED A FAILED SENSOR 22GA, AFTER RING OUT SENSOR ON RT MAIN TRUCK INITIAL READING WAS 15 OHMS THEN SENSOR READ OPEN. SENSOR MUST READ APPROX 19 OHMS, SENSOR FAILED
R2 DOOR SILL BEAM HAS CORROSION ON UPPER SURFACE AT FRAME 66. DOOR SILL BEAM REPAIRED PER SRM 53-41-14 FIG 201.
DURING DESCENT ACFT LOST FACS & EXPERIENCED DOWNGRADED NAVIGATION. EMERGENCY DECLARED. AIRSPEED DISAGREE OCCURRED BETWEEN ADR 1 AND ADR 2. ADIRU NR 1 WAS REPLACED AND NR 2 AIRSPEED FAULT WAS PRESENT. SHOP FINDINGS FOUND THE UNIT REMOVED FROM POSITION 2 RECORDED AN INVALID LEFT STATIC PRESSURE INPUT. ADIRU NR 2 WAS REPLACED. OPERATIONS CHECK NORMAL.
NUMBER 1 ENGINE OIL LEAK IN FLIGHT. QUANTITY DECREASED FROM 10.5 TO 3.5. SMOKE IN TAILPIPE AND TURBINE AREA AFTER SHUTDOWN. OIL LEAK CAUSED BY OIL LEAKING FROM NR 5 BEARING COMPARTMENT INTO HOT GASPATH AREA, GENERATING SMOKE AT ENGINE SHUTDOWN. LEAK CAUSED BY EXCESSIVE OIL "COKING" DEPOSITS IN BEARING COMPARTMENT AREA. OSV HAS REVIEWED AND CORRECTED PROCESS THAT ALLOWED THIS OVERSIGHT.
CREW REPORTS HOT BRAKES ON CLIMB OUT WITH GEAR DOWN. SUPPLEMENTAL DATA UPDATE ORIG INDICATION 370 DEG, CLIMBED TO 425 DEG. SUSPECTED INDICATION PROBLEM, BRAKE TEMP CHECKS NORMAL. BSCU BITE CHECK AND PREVIOUS LEG REPORT FAULT BRAKE TEMPERATURE MONITORING UNIT 3GW. REPLACED MONITOR.