N801UA
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 | 2011-05-09 – 2011-05-09 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2011-05-09 – 2011-05-09 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FUEL CAP MISSING PLACED ON CDL DDP C/W. INSTALLED NEW FUEL CAP REF AMM 28-25-41.
DIRTY SOCK/OIL ODOR IN FLT DECK AFTER GEARDOWN ON FINAL APPROACH. PERFORM AMM 05-50-00-810-831-A IDENTIFICATION OF THE CAUSE FOR CABIN ODOR, SMOKE OR FUME, AND TSM TASK 71-00-00-810-801-A SMOKE AND/OR OIL SMELL IN THE CABIN DUE TO AN ENGINE LEAKAGE. ACCOMPLISHED TSM 05-50-00-810-831-A, FOUND THROTTLE VALVE LEAKING HYD FLUID. ACCOMPLISHED TSM 71-00-00-810-801-A ON ENG 1 & 2 WITH NO DIRTY SOCK/ OIL SMELL AT VARIOUS POWER SETTINGS WITH ENGINES SUPPLING RESPECTIVE BLEEDS. NO ODOR PRESENT DURING OR AFTER RUNS.
FUEL SMELL STILL DETECTABLE IN THE CABIN. REMOVED AND REPLACED BOTH RECIRCULATION FILTER CARTRIDGE PER AMM 21-21-41-400-001-A OPS TEST NORMAL, NO FUEL SMELL A THIS TIME, OK FOR SERVICE.PARTS USED: 31-2121-3-0008, QTY :1 ADD EMP: U114389
FWD CABIN CURTAIN HOLDBACK DEVICE TORN. REMOVED AND REPLACED FWD CURTAIN TIE BACK. OPS CK NORMAL.
OVRHD BIN 1F INOP OVERHEAD BIN 1 EF WONT LATCH CLOSED MEL 2528AF REJECTED 2528AF IS FOR THE OVERHEAD BIN STORAGE BOX LOCK, NOT THE OVERHEAD BIN DOOR ITSELF..MEL 2528AL IS FOR THE OVERHEAD STOWAGE BIN DOOR SECURED CLOSED. COVER PLATE/RETAINER BROKEN ALLOWING ACTUATOR ROD END TO POP OFF. BIN HAS EMERGENCY EQUIPMENT THAT IS CONSIDERED NOT USABLE AND INDIVIDUALLY DEFERRED OK TO APPLY MEL 2528AL FOR OVERHEAD BIN DOOR SECURED CLOSED, SEE ADDITIONAL LOG FOR EMERGENCY EQUIPMENT PLACED ON MEL. FLAGGING SDR DUE TO EMERGENCY EQUIPMENT DEFERRAL MEL 2528AL REJECTED FOR SIGNOFF REPLACED BROKEN SIDE COVER/RETAINER, BIN OPS OKAY.
SLIDE PRESSURE DOOR 1R BORDERLINE. NEEDS SERVICING SOON. CHECKED DOOR 1RT RESERVOIR PRESSURE AND FOUND IN THE GREEN BAND PER GAGE MODEL "A". PER AMM TASK 25-62-00-210-001-A. NO OTHER DEFECTS NOTED. VERDEJO, ISSAC (V950090) CHECKED DOOR 1RT RESERVOIR PRESSURE AND FOUND IN THE GREEN BAND PER GAGE MODEL "A". PER AMM TASK 25-62-00-210-001-A. NO OTHER DEFECTS NOTED. ADD EMP:V950090
RH EPSU BATTERY FAULT REPLACED RH OVERWING EPSU IAW AMM 33-51-38, OPS CHECK GOOD.
HYD Y RSVR LO LVL FOUND FWD UNION ON FIN 2577GM(DUAL DIST BRAKE VLV) LEAKING. REPLACED DAMAGED PACKING ON 2577GM REF MM 32-43-14, SERVICED YELLOW SYS BACK TO NORMAL, CHECKED ENG 2 HYD PUMP CASE DRAIN DPI AS PRECAUTIONARY AND IT IS NOT POPPED OUT. DRY MOTORD ENG 2 SUPPLYING YELLOW SYS NOMINAL PRESS WITH NO ISSUES. OPS CHECK GOOD OF 2577GM NO LEAKS NOTED. AC OK FOR SERVICE.
DOOR 2R LIFE RAFT PANCOVER LOCKING LATCHLOOSE ATTEMPTED TO FIT MULTIPLE DIFFERENT SLIDE COVERS ON DOOR 2R, NO FIX. LATCHES DO NOT LINE UP PROPERLY. WORK DONE IN REF WITH AMM 25-62-44. SUSPECT FRAME OF SLIDE WARPED/BENT, SEE ATTAHCED PICTURES FOR CLARIFICATION. ORIGINAL SLIDE COVER LEFT IN FIRST CLASS SEATS. ADJUSTED LATCHES ON COVER AND REINSTALLED COVER. COVER FIT WELL AND IS SECURED. REF SRM.51-42-21
RIGHT BRAKE PRESSURE INDICATES 3000 PSI CONTINUOUSLY VERIFIED NO BSCU FAULTS AND APPLIED INOP STICKER ADJACENT TO TRIPLE VERIFIED NO BSCU FAULTS AND APPLIED INOP STICKER ADJACENT TO TRIPLE INDICATOR. DEFERRED DIRECTLY BY TOMC COULD NOT REPLACE INDICATOR DUE TO WORKING HIGHER PRIORITY ITEMS AND WORKLOAD.
EMERGENCY EXIT LIGHTS ILLUMINATED W/SWITCHIN ARM CYCLED NO SMOKING SIGN SWITCH AND ALL LIGHTS OPS CK GOOD.
CABIN LOST PRESSURIZATION AT FL240 LOCKED FOR SIGNOFF ITEM UNLOCKED BY TOMC. POST FLIGHT REPORT AND ECS REPORT 19 ATTACHED. PFR AND ECS REPORT 19 ROTABLE PARTS ADDED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1681100 SN OFF 2338 ROTABLE PARTS ADDED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1543969 SN OFF 5466 IPC REFERENCE # 21-31-04 VALVE, SAFETY O OFF 31-2131-9-0001 5466 ON 31-2131-9-0001 5782 VALVE, SAFETY O OFF 31-2131-9-0001 5466 ON 0000 PER MANAGEMENT REQUEST, R&R 6HL AND 7HL CABIN PRESSURE SAFETY VALVES PER AMM 21-31-52-000/400-001-A. OPS CHECK AND ECAM INDICATION OF THE SAFETY VALVES GOOD.
YELLOW SYSTEM HYD QTY DEPLETED. LOW PRESS LIGHT ILLUMINATED. PER PILOTS. REF 7141314 AIR RETURNED PER FLT CREW HYD PUMP WAS TURNED OFF WITHIN 1 MIN OF LOW PRESS FOUND YELLOW SYSTEM PTU MANIFOLD LEAKING FROM PLUG ON THE BOTTOM FOUND CHECK VALVE ON BOTTOM OF MANIFOLD ORING POPPED OUT ,REF INDICATION. OF THE MANIFOLD CASE. IPC 29-13-03 ITEM 40 ORDERED ORING AT STORES PICK UP AREA. INSTALLED NEW O-RING ON THE PTU MANIFOLD 3094GM. LEAK CHECK GOOD.NO LEAKS NOTED. OPS CHECK GOOD FOR PTU. NO FURTHER DEFECTS NOTED. REF AMM TASK 29-13-15/401.
WASTE TANK LINE FWD OF THE WASTE TANK, SEPARATED DUE TO FAILED CLAMP. LOCKED FOR MAINTENANCE FERRY TO ORD. POSITIONED THE WASTE LINE CLAMP SLEEVE BETWEEN THE SEPARATED WASTE LINES AND SECURED WITH SPEED TAPE FOR THE MAINTENANCE FERRY. ORD MX REPLACED CLAMP. ALL 3 LAVS INOP DUE TO SEPERATED WASTE LINE. POSITIONED WATER SUPPLY VALVES TO CLOSED IN ALL THREE LAVS. LOCKED AND PLACARDED ALL THREE LAVS, INOP DO NOT ENTER MEL 3830S APPLIED. R & R FAULTY CLAMP AND REPLACED 2 O-RINGS FOR TOILET DRAIN LINES REF AMM 38-30-00-410-002-A. RAN EACH LAV SEPARATELY MULTIPLE TIMES. NO LEAKS DETECTED. OPA CHECK GOOD.
FUELER REPORTS MISSING WING FUEL CAP. REQ CDL. CAP MISSING PLACED ON CDL DDP C/W
ABNORMAL AIRFRAME VIBRATION FLAPS 1 IN CLMB FLAPS 2 3 4 IN DESEN T REPAIR REF SRM 53-45-00-005. DAILY REINSPECT OF TAPE REQ. SEAL FLT HOURS. TO BE REPLACED AT EARLIEST OPPORTUNITY BUT NOT LATER THAN 600 FOUND AFT RIGHT EDGE SEAL LOOSE ON BELLY FAIRING PANEL 198MB. AREA IS BELOW AFT CARGO DOOR. APPLIED SPEED TAPE FOR TEMP DIP APPROVED FOR CARRY BY TOMC PER SRM SRM 53-45-12-300-005. TOMC-APPROVAL FROM SC1ELBYC COMMENT APPLIED SPEED TAPE FOR TEMP REPAIR TO PANEL 198MB REF SRM 53-45-00-005. DAILY REINSPECT OF TAPE REQ. SEAL TO BE REPLACED AT EARLIEST OPPORTUNITY BUT NOT LATER THAN 600 FLT HOURS. VERIFIED NORMAL OPS OF FLAP AND SLAT SYSTEM REF AMM 27-54-00.
OPS CHECK FAILED FOR EMERGENCY LIGHTS, N0.2 SERVICE CHECK STEP 1 4 PER STS NR0040 REMOVED AND REPLACED 12 WL AND 11 WL BATTERY OF THE ESPU IAW AMM REMOVED AND REPLACED 12 WL AND 11 WL BATTERY OF THE EPSU IAW AMM 33-51-38. PERFORMED OPERATIONAL CHECK EPSU IAW AMM 33-51-00 OPS 33-51-38. PERFORMED OPERATIONAL CHECK EPSU IAW AMM 33-51-00 OPS CHECK GOOD PER STS NE0040 V943302 CHECK GOOD. PER STS NR0040 V943302 REMOVED AND REPLACED 12 WL AND 11 WL BATTERY OF THE EPSU IAW AMM 33-51-38. PERFORMED OPERATIONAL CHECK EPSU IAW AMM 33-51-00 OPS CHECK GOOD. PER STS NR0040 V943302
FUEL CAP MISSING REPORTED BY RAMP ACP MEL REQUIREMENTS. INSTALLED SERVICABLE FUEL CAP AND LANYARD.
THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/20/22. PDA 2 #1 ENG OUTBD T-R TO PYLON FLEX SEAL - AFT MOST LOCATION - CRACKED AND MISSING PIECE AT FWD CORNER. REPLACED #1 ENG OUTBD T-R TO PYLON FLEX SEAL, ALL OK.
PDA 2 #1 ENG INBD T-R TO PYLON FLEX SEAL - SECOND FROM AFT - CRACKED AND MISSING PIECES..SEE PHOTO INSPECT TAPE EACH FLIGHT PER PART 2A AND PERMANENT REPAIR WITHIN 50 FLIGHT HOURS. REF ECRA 5450-02357 REV-B FIG 3 ITEM 110 AFT EDGE CRACKED AND MISSING SEGMENT...PERFORMED INTERIM REPAIR PART 1D, ISSUE DIP TO ENG1 I-B (R/H/S) PYLON FLEX SEAL INTERIM REPAIR WITH SPEED MUST TOMC-APPROVAL FROM SC1ELBYC COMMENT BE CHECKED PRIOR TO EACH FLIGHT ("M" IN THE METER) AND MUST REPAIR WITHIN 50 FH. PER TRM ECRA 5450-02357 REV B. CURRENT PTT IS 75169. PHOTO ADDED REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
CORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010. CORROSION ON DR SILL BEAM FR66-FR68 STGR 23RH. PERFORMED REWORK REPLACEMENT OF RH DOOR SILL BEAM IS REQUIRED, PERFORMED ON DOOR SILL BEAM, THE REWORK ON DOOR SILL BEAM RH WAS BEYOND REPLACEMENT OF DOOR SILL BEAM IAW A319 SRM 51-72-11 AND 51-42-11 ALLOWABLE LIMITS AND NO APPLICABLE REPAIR ON THE REWORKED AREA REV.139. AS PER A319 SRM TASK 53-41-14-300-001, FIGURE 01 REV.139.
CORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010.
CRACK FOUND ON FUSELAGE AT FR35 LH STRG 30L HOLE#2. DAMAGED REPAIRED IAW ECRA 5331-02884, WORK ACCOMPLISHED BY 5H0356 & INSPECTED BY 5H0619.
CRACK FOUND ON FUSELAGE AT FR35RH STRG 30R HOLE#2. DAMAGED REPAIRED IAW ECRA 5331-02884, WORK ACCOMPLISHED BY 5H0356 & INSPECTED BY 5H0619.
DURING INSPECTION OF THE BULK CARGO COMPARTMENT FOUND CORROSION IN FRAME 64 TO FRAME 65 STR 33 TO 25 REQ. EVALUATION AS NOTED ON LTPR NR# 5001118110-0020. INSPECTION PERFORMED ON AFT CRG COMPARTMENT, FOUND CORROSION ON CONSIDERED MAJOR AND PERMANENT CATEGORY A WITH NO INSPECTION CLIP LOCATED AT FR65 BTW STGR 29RH-31RH IS BEYOND ECONOMICAL REQUIREMENTS IAW A319 SRM TASK 51-72-11-911-001 REV.140. WORK REPAIR DUE TO HEAVY CORROSION AND REQUIRES REPLACEMENT. ACCOMPLISHED BY 5H0348 AND INSPECTED BY 5H0619. REPLACEMENT OF CLIP LOCATED AT FR65 BTW STGR 29RH-31RH IS
LH FLAP TRACK 2 AFT ATTACH BOLT 9 REQ EVA (A3NB-57-3-6286, SEQ# 1501).DURING INSTALLATION OF LH FLAP TRACK NO.2 BEAM, WE NOTICED A DAMAGE IN THE UPPER SURFACE. FURTHER EVALUATION IS REQUIRED AS NOTED ON LTPR NR# 5001117024-0110. DURING INSTALLATION OF FLP TRK#2 L/H WING, DAMAGE WERE FOUND AT BLENDOUT DIMENSIONS, L=57MM,W=23MM,D=0.62MM. FOR DEFECT FREE EO-A319-57-11833-00-FINAL AIRBUS INSTRUCTIONS AND COVERED BY FWD UPPER FLANGE OF BEAM #2, 70.91MM FROM THE FWD EDGE AND 19.61 CONDITION EXIST,HFEC PERFORMED IAW NTM 51-10-08 REV135. RESULTS: EC/RA# 5751-01419 MARCH 16 2022. THIS REPAIR CONSIDERED AS A MM FROM THE I/B EDGE. DAMAGE DIMENSIONS L=16.91MM,W=9.86MM, NIL FINDINGS. REPROTECTION OF THE AREA PERFORMED IAW 51-21-11 LEAVE AS IS AND NO FURTHER ACTION IS REQUIRE. REPAIR RECORDED ON D=0.49MM, SMOOTH BLEND PERFORMED IAW SRM:51-73-00 REV140. REV140 AND SRM 51-75-12 REV140. THIS REPAIR PERFORMED BY UAL LOGBOOK NO. 8161678.
DURING INSPECTION OF THE BULK CARGO COMPARTMENT FOUND CORROSION IN FRAME 64 TO FRAME 65 STR 33 TO 25 REQ. EVALUATION, AS NOTED ON LTPR NR# 5001118110-0040.
CORROSION ON AFT CABIN FLR DR SILL BEAM FR.68 LH (A3NB-53-3-6187 ZONE:200 SEQ#618) AS NOTED ON LTPR NR# 5001115247-0010. CORROSION FOUND AT L2 DOOR SILL BEAM ADJACENT TO FR 68. REWORKED NO FURTHER ACTIONS REQUIRED. PERFORMED IAW SRM 51-74-00. AFTER REWORK WAS PERFORMED, THE AREA IS OUT OF LIMITS IAW SRM 53-41-14-283-002 FIGURE 002, SHEET 01. REPLACEMENT L2 DOOR SILL WAS PERFORMED IAW SRM 51-72-11-911-002.
PDA 2 #1 ENG OUTBD SIDE T-R TO PYLON AFT MOST FLEXSEAL SEGMENT MISSING AT FWD END -- SEE PHOTO PHOTO ADDED REF ECRA 5450-02357 REV-B FIG 3 ITEM 120. THE AFT EGDE OF FLEXSEAL ITEM 120 IS INTACT AND NOT DAMAGED. PERFORMED INTERIM REPAIR PER PART 1D OF ECRA 5450-02357. ISSUE DIP TO ACCOMPLISH VISUAL INSPECTIONS PER PART 2A ONCE EVERY FLIGHT CYCLE AND ACCOMPLISH PERMANENT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS. ENGINE 1 OUTBOARD INTERIM REPAIR TO FLEX SEAL REQUIRES INSPECTION PRIOR TO EACH FLIGHT FOR TAPE BEING IN TACT. REPLACEMENT OF FLEX SEAL REQUIRED WITHIN 50 FLT HRS. REF. ECRA 5450-02357 TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
RT MLG FWD DOOR HINGE FITTING 2 BROKEN HI-LOCKS MOST OBD SUP TAS K PER HGR NR9290353 GEN AT HAECO LCQ. UPDATING THE ATA CHAPTER TO 5300 ACCOMPLISH INTERIM REPAIR PER EC/RA 5311-02357 ACCOMPLISH PERMANENT REPAIR PER PART 3 OF EC/RA 5311-02357 ON OR BEFORE 03 JUL 2020, PLANNING TO CONTACT EG AFTER 01 JUN 2020 BUT BEFORE 15 JUN 2020 FOR PERMANENT REPAIR 01-JUN-2020 BUT BEFORE 15-JUN-2020 OK TO DIP TILL 03-JUL-2020, PLANNING TO CONTACT EG AFTER TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
RH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLES 2,3,4,14,16,18 ,19,20,21,22,24,25,26,27,28 ARE CRACKED IN THE PRESSURE PANEL. H OLE 2 IS ALSO CRACKED IN THE CORNER FITTING SUPPORT TASK AD 2018 -06-04 PER HAECO LCQ NR 9290282 GENERATED ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02550 PART 1.ALL WORK ACCOMPLISHED ON HAECO NR 9290282.INSPECTIONS REQUIREMENTS FOR EC RA 5331-02550 ACCOMPLISHED ON LP 4162286 AND LP 4163200 RII INSP ACP
LH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLE 2,3,4,14,15,16, 17,19,20,22,23,24,25,26,27 AND 28 ARE CRACKED TO THE PRESSURE PA NEL. HOLE 28 IS ALSO CRACKED IN THE TITANIUM ANGLE SUPPORT TASK AD 2018-06-04 PER HAECO LCQ NR 9290281 GENERATED ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02552 PART 1.1 ALL WOR K ACCOMPLISHED ON HAECO NR 9290281.DIP INSPECTIONS ACCOMPLISHED ON LP 4170731,4170926,4171282 AND 4171103. RII INSP ACP
AT 3500FT MSL, CARGO DOOR OPEN ECAM, AFT CARGO DOOR INDICATED OPEN. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. CHECK AFT CARGO DOOR MEL 5270D. MAC METER INITIATED FOR WITH VENDOR, MAC RELATED WORK ORDER 000000001914103 AND PRTR, REPLACED HANDLE FLAP MECHANISM SPRING. PER AMM 52-32-21-400-002- A OPS NORMAL, NO DOOR RIG ADJUSTMENT DISTURBED. REPLACED HANDEL FLAP MECHANISM SPRING. PER AMM 52-32-21-400-002- A OPS NORMAL NO DOOR RIG ADJUSTMENT DISTURBED.
AFT CARGO DOOR ECAM. OPERATED AFT CARGO DOOR SEVERAL TIMES PER AMM52-32-00-710--001-A. OPERATIONAL CK GOOD.
IN FLT, THE CABIN LIGHTS FLICKERING ALONG WITH THE EMERGENCY LIGHTS. SEAT BELT CHIME DING INTERMITTANT. PERFORMED HIT CIDS2 DATA INTM FAIL AT FLT PH 06. RESET CIDS DIR2 AT CFDS. ALL CIDS LIGHT COTROL. FUNCTIONS NORMAL IAW AMM23-73-00.
EMERGENCY EXIT SIGN MISSING. REPLACED THE SIGN ASSY. OPS CHECKED GOOD IAW AMM 33-00-00.
R2 DOOR SLIDE SOFT COVER RELEASE CABLE SAFETY BROKEN. INSTALLED A SLIDE.
EMERGENCY LIGHTS ILLUMINATE WITH THE SWITCH ARMED. EMERGENCY LIGHTS GO OUT AFTER RECYCLING TO OFF THEN ARMED. RESET CID SYS, ALL LIGHTS CHECKED NORMAL IAW 33-23-00
L2 DOOR SLIDE ARM LIGHT ON ECAM PAGE ILLUMINATED AFTER DOOR CLOSED. REMOVED AND REPLACED THE SLIDE ARMED LIGHT IAW AMM 52-73-21-400-002-A AND TSM 52-13-00-810-803-A.
EMERGENCY LIGHTS TEST FAILED AT PTP PANEL CABIN EMERGENCY POWER SUPPLY AND BATTERY POS 13WL WERE REPLACED IAW AMM 33-51-38 PG BLOCK 401 OP TEST IAW 33-51-38-740-050
EXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.
SMALL DENT FOUND ON RT FUSELAGE, ONE FOOT ABOVE UPPER WINDOW LINE & 7 WINDOWS AFT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41- 11 FIG.101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG 231, PG 503-504.
R2 DOOR SILL FRAME 66 - 68 CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM53-41-14 PARA 5A FIG 201.
LEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.7.
LEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.
LEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.
LEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.
LEFT MLG UPPER SIDE STAY BUSHING SHOWS EVIDENCE OF ROTATION. SEALANT IS SPLIT. CORROSION FOUND. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCH & FIP IAW 57000 PB8 & NTM51-80-00PB1. APPLIED FINAL FINISH CUTS DIAMETER 4.3005.
RIGHT MLG UPPER SIDE STAY BUSHING HAS EVIDENCE OF ROTATION. SEALANT FOUND SPLIT. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCHED & FPI IAW 57-00-0PR8 & NTM 51-80-00PB1. APPLIED FINAL FINISHING CUTS DIM 4.345. NO FURTHER INSPECTION REQUIRED.
EXTERNAL FUSELAGE SKIN DENTED AT THREE EACH LOCATIONS FRAME 23 & 24, STRINGER 23L & 24L. FOUND DENTS TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG 115. FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-00-11 FIG 232 PG 505 - 506.
SMALL DENT FOUND ON ARRIVAL ON RT FUSELAGE, 1 FT ABOVE UPPER WINDOW LINE & 7 WINDOWS FT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41-11. FABRICATED REPAIR DOUBLER 7 INSTALLED IAW SRM 53-00-11.
L2 DOOR SILL HAS CORROSION AT 7 E. LOCATIONS BETWEEN FRAME 66 & 68. REPAIRED THE AREA IAW SRM 53-41-14.
R2 DOOR SILL FRAME 66 - 68 CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-41-14 PARA 5A FIG 201.
ON ARRIVAL PANEL 192MB FOUND OPENED & DAMAGED. ALSO DAMAGED PANEL 192FB AC BAY RT. TWO PUNCTURES DIRECTLY BELOW PANEL 192MB. REPLACED PANEL 192MB.
O2 ABOVE 34 DEF MISSING MASK. REPLACED MISSING MASK.
'Y' SYSTEM LOW PRESSURE MESSAGE, RETURN TO FIELD. REPLACED POWER TRANSFER UNIT MANIFOLD 2-WAY VALVE. OPERATIONS & LEAK CHECKED OKAY.
FOUND TWO NOSE CONE INNER BARREL RIVETS MISSING AT THE SIX O'CLOCK POSITION. REPLACED MISSING RIVETS ON NUMBER ONE ENGINE REFERENCE MT 71-002.
ELECTRICAL DC ESS BUSS SHED ECAM, RETURNED TO FIELD. REMOVED & REPLACED DC SHED ESSENTIAL BUSS CONTACTOR, ALL OPS CHECKED NORMAL.
RIGHT WING INBD SLAT CLOSING PLATE CRACKED. RPL- :INSTALLED PANEL.
WEATHER RADAR SYSTEM INOPERATIVE, DISPLAYS ONLY WR ANT. REPLACED WEATHER RADAR TRANSCEIVER PER MM, TESTED OKAY.
OXYGEN MASK FELL OVER SEAT ROW 30 DEF. PACKED MASK. TESTED OXYGEN MASKS IAW MT 35-003. ALL TEST OKAY.
LIFE VEST LOOSE ON FLOOR ROW 25 ABC. SECURED LIFEVEST.
EVIDENCE OF BIRD STRIKE INGESTION IN NR 2 ENGINE. PERFORMED VISUAL INSPECTION OF ENGINE 2 ESN V10991 AND INLET COWL PER MT72-021. NO DAMAGE OBSERVED. BIRD DEBRIS OBSERVED ON SPLITTER FAIRING. ACP BORESCOPE OF NR 2 ENGINE, NO LIMITING DEFECTS NOTED. REF AMM 72-00-00, PG 601.
CREW REPORT: OXY MASK ON WRONG AT OXY BOTTLE OVER 1A. RE-INSTALLED MASK TO PROPER POSITION.
INOP LIGHTS ARE APU MASTER, APU START, DITCHING, CAB PRESS MODE SEL, EMERGENCY EXIT, ETC. -TS, CLEANED & CHECKED CONNECTORS AT 25VU OVERHEAD PANEL, TRIED ANOTHER 7LP ANN & INTC CARD, SAME RESULTS. RE-INSTALLED SAME 7LP INTC CARD. SUSPECT BAD ESS XFMR 35LP PER TSM 33-814-00-810-802A. ORDERED PCN 565-1216 NON-STOCK SFO OSTF W3697. REF ASM 33-14-12 SCH 12. REPLACED FUSES APU MASTER SWITCH, APU START SWITCH, AND CABIN PRESSURE MODE SELECTOR SWITCH ARE ILLUMINATING 94559 AND WORKING. STARTED APU. APU RAN AND OUTPUTS ARE NORMAL. NO FAULTS FOUND. OPS CHECK PASSED.
CREW OXYGEN IS LEAKING AT A RATE OF 50 PSI PER HOUR. REMOVED AND REPLACED FIRST OBS CRUSH WASHER FOR INLET LINE TO BOX B-NUT, AFTER T-S AND OLD WASHER LEAKING. SERVICED O2 TO FULL, LET SIT FOR ONE HOUR AND O2 PRESS DID NOT GO DOWN FROM 1770.
VIBRATION FROM NR 1 ENG, FELT IN FLIGHT DECK. NEED TO ACP TAP TEST INSPECTION OF THE NR 1 ENGINE FAN BLADES. ACCOMPLISHED TAP TEST PER AMM. ALL BLADES HAVE AN ACCEPTABLE VALUE. ACP'D LP COMPRESSOR (FAN) ONE SHOT METHOD TRIM BALANCE PER MM. OPERATIONAL TEST GOOD.
PA FAULT RETURNED. STAYS HOT AND SQUEALS. FOUND WIRE BUNDLE BEHIND F/A INBD SEAT PINCHED. REPAIRED WIRE AND RE-ROUTED BUNDLE AND SECURED, OPS CHECKED GOOD. NO FAULTS.
FQI CHANNEL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FQIC PER AMM.
CAPTAIN'S OXY MASK TEST AND RESET SLIDING SWITCH WILL NOT RESET CAPTAIN'S OXYGEN MASK. REPLACED CAPTAINS O2 BOX. CHECKS OKAY.
RT OFF WING SLIDE PANEL DELAM ALONG UPPER AFT CORNER. REPLACED ESCAPE SLIDE ASSY.
NR 2 RT MAIN DOOR EMERGENCY CYLINDER (ASSIST BOTTLE) FOUND AT 0 PRESSURE DURING 3SVC. SERVICED TO 1900 PSI LOST 200 PSI IN 20 MINUTES. REPLACED CYLINDER DIAPHRAM PER MM. PRESSURE HOLDS NOW.
R2 DOOR SLIDE ASPIRATOR IS NOT SPRING LOADED IN CLOSED POSITION. ALL OTHER SLIDES ARE SPRING LOADED IN CLOSED POSITION. REMOVED AND REPLACED R2 DOOR SLIDE ASSY.
F/O RUDDER PEDAL ADJUSTMENT HAVE NO TENSION. CHECKED BELOW RUDDER PEDALS. PNEU BUFFER "PUSHROD" HAS NO INTERNAL PRESSURE. REPLACED F/O RUDDER PEDAL. ADJ BUFFER ASSY.
AFT ELT FOAM DAMAGED AND TORN. NIS DENVER. DF REF MEL2560. REPLACED AFT CABIN TRANSMITTER EMERGENCY LOCATOR ELT PER AMM.
CREW DEBRIEF AIRCRAFT SPEED WAS .79 MACH AT FL370 AIRCRAFT EXPERIENCED EXCESSIVE TURBULENCE FOR 30 SECONDS. AIRCRAFT CLIMBED 1500FT IN 15 SECONDS. FLIGHT CREW REPORT BEING THROWN ABOUT IN SEAT AND 5 TO 6 'G -FORCE' ALONG WITH A -1 'G FORCE'. STARTED EXCESSIVE TURBULENCE INSPECTION. ACCOMPLISHED INSPECTION PER AMM. IN REFERENCE TO LM8542 REMOVED CVR. INSTALLED CVR, OP CKS OKAY.
SMOKE IN CABIN, FLIGHT DIVERTED. ATTENDANT REPORTED GETTING WHIFFS IN AFT GALLEY AREA. NO VISIBLE SMOKE SEEN. ODOR DISSIPATED DURING DECENT. NO BURNING ODOR PRESENT AT ARRIVAL. FIRE DEPT INSPECTED PITS ON ARRIVAL, NO EVIDENCE OF BURNING. ODOR WAS PRECEDED WITH RESET OF TRIPPED CB T19, CARGO FIRE EXTINGUISHING BY ABOUT 10 MINS. CB DID NOT TRIP AGAIN AND ALL INDICATIONS ARE STILL NORMAL. NO ODOR PRESENT WITH ALL SYSTEM RUNNING. ALL AREAS ASSOCIATED AT ROW 10 AND GALLEY CLEAR. VISUAL INSPECTION ACP, NO BURNING EVIDENCE FOUND.
RETURNED TO GATE DUE TO UNIDENTIFIED ODOR IN CABIN AND FLIGHT DECK. REPLACED RECIRCULATION FAN, OPS NORMAL. NO ODOR IN ACFT.
R12 FWD GALLEY OVEN IGNITED A PIECE OF PAPER CAUSING SMALL FIRE & SMOKE. HALON EXTINGUISHER USED. REMOVED AND REPLACED FORWARD GALLEY OVEN R12. OPS TEST OKAY.
IDG 1 OIL LO PR DISPLAYED ON UPPER ECAM SCREEN. - ELEC REMOVED WIRE HARNESS FROM IDG AND MEGGERED TO FIREWALL CONNECTOR NO FAULTS. RANG WIRING FROM EGIU PIN AA-5B TO GCU PIN AA-15D ALL NORMAL, NO FAULTS FOUND. REPLACED EGIU 22XU1 PER AMM. RAN ENGINE IAW JRH ALL INDICATIONS NORMAL, NO FAULTS, COULD NOT DUPLICATE. VOLTS AND FREQUENCIES STEADY, NO FLUCTUATIONS NOTED.
REF CARGO PIT FIRE BOTTLE WRITE-UP, FOUND 26VDC ON FWD SQUIB CONNECTOR WITH T19 CB PULLED. REPLACED SDCU PRECAUTIONARY, NO HELP. RANG OUT OVERHEAD PNL, WIRING FROM PNL TO SQUIBS AND PANEL TO SDCU. FOUND 26VDC ON PINS R AND S OF 2400VC A. PULLING SDCU CB'S REMOVES PWR FROM SQUIB CONNECTORS. SYSTEM IS WORKING NORMALLY AND ALL PARTS OF TEST PASS.
SHOCK ABS FAULT ECAM, RTFL. PERFORMED MAINT TIP 32-022. FOUND IN NEED OF LUBE IAW THIS MAINT TIP. ACP'D PRECAUTIONARY BITE CK OF LGCIU 1&2, NO FAULTS FOUND.
GREEN/BLUE HYD OVHT MSG, RTFL. ACP WALK AROUND, FOUND NO SIGNS OF HYDRAULIC OR OIL LEAKS. HYDRAULIC AND OIL QTY INDICATIONS ON ECAM CHECK NORMAL. FAULTS CLEARED. NO ECAM, STATUS OR MAINT MSGS DISPLAYED. RAN HYD SYS FOR 1 HR & CYC FLIGHT CONTROLS, NO MSGS. HYD QTY'S NORMAL. REPLACED OIL SCAV FILTER ELEMENT AND PACKING. MASTER C-D CLEAN & FILTER CLEAN. SUSPECT FAULT RELATED TO SDAC 1 FAULTS.
DURING CABIN EMERGENCY LIGHTS CHECK, SYSTEM TEST FAILED WITH MESSAGE 'EPSU UNIT FWD L'. REPLACED FWD EPSU, NO HELP. FOUND SHORT FOR FLOOR LIGHTS AT SEAT 6 WHICH WAS TAKING OUT THE EPSU AT DOOR 1L. REPAIRED SHORT, GROUND CHECKED OKAY.
EMERGENCY FLOOR LIGHTS INOP AT SEATS 1, 2, 8, 9 & 10. SEAT 10 WAS INOP; REPAIRED CONNECTOR. NOW 10 WORKS OK. REF WDM 33- 51-06 POST SB 33-1041 WIRE MOD TO EMERG LIGHT CIRCUITS, WORKING WITH SAMC TO FIND BASE COA FOR PWR TO THESE SEATS OR LOCATION OF BATTERY 110WT1 FROM POST COA. RECEIVED POST COA AND FOUND SHORTING FLOOR LIGHTS, REPAIRED BY SEAT 6 PER SWPM AND REPLACED EPSU. ALL LIGHTS WORK NORMAL.
NR 1 ENG BIRD STRIKE, RTFL. ON CLIMBOUT, ABOUT 800FT, CREW HEARD A LOUD BANG FOLLOWED BY A BAD ODOR AND MILD ACFT VIBRATION. ACFT HAD A BIRD STRIKE ON THE LT SIDE NR 1 ENGINE. ALL INDICATIONS WERE NORMAL. NO CABIN PREP AND CREW MADE A NORMAL LANDING. NR 1 ENG, ACCOMPLISH BIRD STRIKE BOROSCOPE ON ACCOUNT OF EVIDENCE OF STRIKE IN INLET. NR 1 ENG, 2 FAN BLADES FAILED TRANSIENT, ACOUSTICAL, PROPAGATION TEST, BLADES MARKED, REPAIR AS NECESSARY. LP COMPRESSOR BLADES AND FILLERS REMOVED. AT REMOVAL OF LP COMPRESSOR BLADES AND FILLERS FOUND 2 FILLERS ON EITHER SIDE OF BLADE LOCATION NR 2 BENT AND CRACKED. ALL BLADE NRS AND WEIGHTS RECORDED AND SENT TO ENG CONTROLLER WAITING FOR NEW BLADE CONFIGURATION. REPLACED BLADES & FILLERS. RAN NG FOR VIB CHECK, HAD 2.4 AT 1.25 EPR, AT 85 PERCENT N1 HAD 1.2 VIB. RAN CHECK TWICE. ACFT RELEASED BACK TO SERVICE.
ELECTRICAL PROBLEM, RTFL. REPLACED STROBE SWITCH, TESTS OKAY.
ODOR IN COCKPIT, FLIGHT DIVERTED. *S/D* FOUND WHC2 HAD OVERHEATED. REMOVED COVER AND FOUND CHARRED RESISTORS, THIS CAUSED BY AN INTERNAL SHORT WITHIN THE RT (F/O) WINDSHIELD. REPLACED WHC2, AND AND F/O WINDSHIELD, ALL OPS CHECKS NORMAL.
CREW OXYGEN BOTTLE NEEDS SERVICE. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME.
DOOR 1R WILL NOT ARM. CAUSE, INTERFERENCE WITH BENT FLOOR PLATE, UNKNOWN DAMAGE. REWORKED FLOOR COVER PLATE TO ALLOW CLEARANCE FOR DOOR, OPS OK.
DIVERTED DUE TO LEFT ENGINE VIBRATION. REPLACED EVM (TRANSDUCER). ENGINE RUNS WERE NORMAL AFTERWARD.
CARGO FLOORBOARD RPL S GLS PNL. MAJOR REPAIR ACCOMPLISHED AT LCQ (COA ACCOMPLISHED).
WHEN TESTING OBSERVERS O2 MASK, MASK DID NOT RESEAT AND CONTINUED TO PURGE O2. OBSERVER`S MASK LEAKING. REPLACED OBSERVERS MASK ASSY AND LEAK CHECKED. NO LEAKS NOTED.
FOUND FUSELAGE SKIN HAS A GOUGE ON THE RIGHT SIDE OF AIRCRAFT IN FRONT OF FWD CARGO DOOR. DAMAGE IS APPROXIMATELY 6" BELOW UPPER RVSM BORDER. REPAIRED GOUGE. PER AMM 51-73-11 PAGE BLOCK 801.
FOUND SEAT 12C EMERGENCY ESCAPE PATH LIGHT ON SEAT INOP. REPLACED LIGHT ASSEMBLY. OPS CHECKED OK.
CREW REPORTED THAT IN FLIGHT, HEARD A LOW RUMBLING SOUND AND EQUIP COOLING EXTRACT CB POPPED AND SHORTLY AFTER GOT SMOKE AND SMELL IN COCKPIT. REPLACED AVIONICS FAN AND OPS CHECKS GOOD.
RETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. STALL-RTF. HPC WAS BOROSCOPED, OK. FOUND BAD 7TH STG BLEED VALVE, REPLACED. NR 1 ENGINE ACCOMPLISHED BORESCOPE OF HPC 3 AND 4, NO LIMITING DAMAGE FOUND. ACCOMPLISHED 7TH STAGE BLEED VALVE SOLENOID CHECK AND 10TH STAGE BLEED VALVE SOLENOID CHECK. REPLACED UPPER 7TH STAGE BLEED VALVE. ACCOMPLISHED POWER ASSURANCE RUN ON NR 1 ENGINE ALL INDICATIONS AND PARAMETERS NORMAL AND WITHIN LIMITS. NO STALLS OR SURGES.
FOUND EMERGENCY LIGHTS FAILED 3 SVC TEST. FAULT IS EPSU BATTERY LEFT AFT. REPLACED BATTERY PACK.
GREEN HYDRAULIC SYSTEM FAILURE.
ECAM FWD CARGO DOOR AFTER TAKEOFF. ACCOMPLISHED OPERATIONAL CHECKS, NO FAULT MESSAGES INDICATED.
DIVERTED UNDER AMBER ALERT DUE TO VIBRATION IN NR 1 ENGINE. ENGINE REPLACED. HPC RUB STRIP DISBONDED CAUSING COMPRESSOR VIBRATION. ENGINE UPGRADED WITH RUB STRIP MODIFICATION.
LANDING GEAR LEVER HARD TO RAISE. *S/D* REPLACED LANDING GEAR LEVER ASSEMBLY. PERFORMED FUNCTIONAL TEST INCLUDING EXTENSION AND RETRACTION OF MAIN LANDING GEAR AND NOSE LANDING GEAR. PERFORMED CENTRALIZED FAULT DISPLAY SYSTEM LANDING GEAR CONTROL INTERFACE UNIT 1 & 2 TEST AND CHECKED STRUTS FOR PROPER INFLATION. ALL OPERATIONAL CHECKS GOOD.
CABIN EMERGENCY LIGHTS FAILED TEST. ESPU BITE SHOWS BATTERY FAULT. REPLACED BATTERY.