N822UA
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 | 2025-07-18 – 2025-07-18 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2025-07-18 – 2025-07-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE D HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 2 O`CLOCK DIRECTION, 60% S.H. REPAIRED HOLE D & ASSOCIATED HOLE C AT FR 20 LEFT, UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR
RIGHT FR 20 DOUBLE JOGGLE LOWER AREA HOLE 12 HAD A CRACK INDICATION IN FRAME LAYER AT 6 O`CLOCK DIRECTION, 25% S.H. REPAIRED HOLE 12 AND ASSOCIATED HOLE 11 AT FR 20 RH LOWER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, REPAIR CATEGORY B.
LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE 6 HAD A CRACK INDICATION IN FRAME LAYER A 2 O`CLOCK DIRECTION, 60% S.H. REPAIRED HOLE 6 & ASSOCIATED HOLE 5 AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B.
LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE A HAD A CRACK INDICATION IN FRAME LAYER AT 2 O`CLOCK DIRECTION, 70% S.H. REPAIRED HOLE A AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR.
LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE B HAS CRACK INDICATION IN FRAME LAYER AT 2 O`CLOCK DIRECTION, 100% S.H. REPAIRED HOLE B AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR.
LEFT FWD WINDSHIELD WINDOW FRAME CENTER POST CONTINUITY FITTING MOST INBD FASTENER HOLE HAS 2 CRACK INDICATIONS 100% SH, AT THE 10:00 O'CLOCK AND 6:00 O'CLOCK POS. FWD LOOKING AFT. PER AAR LCQ NON ROUTINE 9298444/36444. ACCOMPLISHED INTERIM RPR AT LEFT FWD WINDSHIELD FR CTR POST LWR NODE MOST INBD FASTENER HOLE #D IAW ECRA 5311-03443 PART 1.1.
RIGHT FWD WINDSHIELD WINDOW FRAME CENTER POST CONTINUITY FITTING MOST INBD FASTENER HOLE HAS A CRACK INDICATION 100% SH AT THE 5 :00 CLOCK POS. FWD LOOKING AFT PER AAR LCQ NON ROUTINE 9298445/3 6445 ACCOMPLISHED INTERIM RPR AT LEFT FWD WINDSHIELD FR CTR POST LWR NODE MOST INBD FASTENER HOLE #D IAW ECRA 5311-03443 PART 1.1. ALL WORK ACCOMPLISHED ON AAR NR 9298444. SEE LOG PAGE 8475006 WITH DIP INSP LIMITS PER ECRA 5311-03443 PART 1.2.
LEFT FR 68 GUSSET NR 2 HAS THREE HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 68 GUSSET NR 2 WITH FABRICATED PART MATE RIAL 202473-063 IAW SRM 51-42-11/001, & SRM 51-31-00/001.
LEFT FR 66 GUSSET NR 6 HAS (3EA) HOLES WITH A OUT OF ROUND CONDITION HOLES NR 2, NR 3 FROM TOP ARE STEPPED. REMOVED AND REPLACED LH FR66 GUSSET #6 WITH PART D5348002075802 IAW SRM 51-72-11-911-001 AND SRM 53-41-12-300-018.
LEFT FR 68 GUSSET NR 6, HAS 3 HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 68 GUSSET NR 6 WITH PARD D5348002075202 IAW SRM 51-72-11-911-001 AND 51-42-11/001.
LEFT FR 69 GUSSET NR 4 HAS (5EA) HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR68 GUSSET NR 4 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/ 001, & SRM 53-41-12-300-018.
LEFT FR 66 GUSSET NR 7, HOLE NR 1, GUSSET NR 8, HOLE NR 2, HAS AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 66 GUSSET NR 7 & 8 WITH PART 2EA D534 800207 5802 IAW SRM 51-72-11-911-001 SRM 51-42-11/001.
LEFT FR 68 GUSSET NR 7 HAS (4EA) HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPACED LT FR 68 GUSSET NR 7 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44- 11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/0 01, AND 53-41-12-300-018.
LEFT FR66 GUSSET NR 4 HOLE 3 FROM TOP HAS AN OUT OF ROUND CONDITION WITH CHAMFER. REMOVED AND REPLACED LT FR66 GUSSET NR 4 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/001, AND SRM 53-41-12-300-018.
LEFT FR66 GUSSET NR 5 HAS (3EA) HOLES WITH A OUT OF ROUND CONDTI ON WITH CHAMFER. REMOVED AND REPLACED LT FR66 GUSSET NR 5 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/001, AND SRM 53-41-12-300-018.
EPSU BATTERY AFT LIGHT MESSAGE POPULATED WHEN PERFORMING EMERGENCY LIGHT TEST VIA PTP. NO SYS OK. REMOVED AND REPLACED EPSU BATTERY AFT LIGHT PER PTP IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A . PERFORMED OPS CHECK OF THE EMERGENCY POWER SUPPLY UNITS, BITE-CHECK IAW TASK CARD 18-3351-1-0003. OPS CHECK GOOD, SYSTEM OK. LED CAME ON.
ENG 1 COMPRESSOR VANEECAM CREW REPORTED THAT ABORTED T-OFF AT 70 KNOTS. (LOW SPEED). DUE TO #1 ENG SN. V10406 (TSI= 1990 HRS / 1082 CYC) DUE TO ENG1 COMP VANE ECAM. FADEC 1A SHOW ENG1 COMP VANE CH. A VSV ACT / HC/ EEC1 CELL 38 (FAULT CODE SVATK). AHM SHOW DURING START CHA AND CHB HIT VSV ACT / HC/ EEC1. REMOVED #1 ENGINE VSV ACTUATOR REF AMM TASK 75-32-41-000-010-A. INSTALLED #1 ENGINE VSV ACTUATOR PER AMM 75- 32-41 UP TO STEP 5. CLOSE UP. RIG PINS HAVE BEEN REMOVED. ACCOMPLISED IDT INSPECTION TO VERIFY RIG PINS ARE REMOVED. COMPLETED INSTALLATION FROM STEP 5 TO COMPLETION. ACCOMPLISHED IDLE LEAK CHECK PER AMM 71-00-00-710-012-B AND HIGH POWER ASSURANCE RUN PER AMM 71-00-00-710-013-C. NO ECAM MESSAGES AND NO FAULTS RELATED TO #1 ENGINE.
DOOR 2R SLIDE PRESS GAUGE IN THE RED. FOUND WITHIN LIMITS REF AMM 25-62-00-210-001-A GAUGE MODEL A.
LARGE SWERVE AT 90KTS, REJECTED. SUSPECT BRAKE GRABBED. REMOVED AND REPLACED LT OTBD BRAKE IAW AMM TASK 32-42-27-400-001-A. OPS CHECKED GOOD.
EMERGENCY EXIT LIGHT ROW 22D ILLUMINATES INTERMITENTLY OVERHEAD LIGHT SEAT 22D ILLUMINATING RED. DEACTIVATED LIGHT SUFFICIENT LIGHTING IN CABIN. COMPLIED WITH MEL 3320A LIGHT IS A CABIN OVERHEAD LIGHT, NOT AN EMERGENCY LIGHT. PLACE ON MEL 3320A. PULLED AND COLLARED MOOD LIGHTING E1, CIELING FWD H5 BREAKER ON P2000VU SUPPLEMENT 33-28-00. PULLED H5 PER SUBTASK 33-28-00-861-002. H5 BREAKER PULLED CIELING, FWD, RIGHT. ALL OTHER LIGHTS WORK NORMALLY. PLACED ON MEL 3320A. RELAMPED AND REMOVED MEL. REF 33-20-00. OPS CHECK GOOD.
DOOR 2R PRESSURE RED INSPECTED SLIDE PRESSURE REF AMM 25-62-00; PRESSURE IS WITHIN LIMITS AT THIS TIME.
DOOR 2R HARD TO DISARM. LEVER SEEMS TO HANG UP ON SOMETHING. POP PINGSOUND. NOT PRESSURIZATN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CHECK THE OPERATION OF THE EMERGENCY ESCAPE SLIDE ARM AND DISARM FUNCTION AFTER YOU ACCOMPLISH THE RENDER SAFE CHECKLIST. PER AMM TASK 52-10-00-720-005-A. UPTO SUBTASK 52-10-00-410-066-A STEP "C'. CONTYACT TOMC WITH FINDINGS. MAC METER INITIATED FOR. CHECKED THE OPERATION OF THE EMERGENCY ESCAPE SLIDE ARM AND DISARM FUNCTION AFTER YOU ACCOMPLISH THE RENDER SAFE CHECKLIST. PER AMM TASK 52-10-00-720-005-A. INCLUDING SUBTASK 52-10-00-410-066-A STEP "C'. NO DEFECTS NOTED WITH DOOR OPERATION. CHECKED THE OPERATION OF THE EMERGENCY ESCAPE SLIDE ARM AND DISARM FUNCTION AFTER YOU ACCOMPLISH THE RENDER SAFE CHECKLIST. PER AMM TASK 52-10-00-720-005-A. INCLUDING SUBTASK 52-10-00-410-066-A STEP "C'. NO DEFECTS NOTED WITH DOOR OPERATION.
ON TAKEOFF ROLL CA AIRDATA LOST UPDATED MANHOURS REQUIRED. CONTINUED WITH TSM 31-63-82-810-801-A. STILL HAVE ADC 1 BUS FULT IN I/P TEST. REMOVED AND REPLACED ADIRU 1 REF AMM 34-12-34-000-001-A/34-12-34-400-001-A. INSTALLATION TESTS PASSED. STILL MISSING AIR DATA ON CAPT SIDE. SWAPPED DMC 1 AND UPDATE FOR PARTS TRANSACTION. FAULT DID NOT PERSIST ON CAPT OR F/O SIDE. RETURNED DMC 1 AND 2 TO ORIGINAL POSITIONS. SUSPECT DMC 1 INSTALLED IS BAD FROM STOCK. DMC S/N 2036 WAS PREVIOUSLY REMOVED FOR DMC FAULT ON UPPER ECAM. DMC NIS DEN. REPLACED DMC WITH P/N 9615325060. REF AMM 31-63-34-400-001-A. AND IPC 31-62-08-02. OP CHECK GOOD. ACCOMPLISHED AUTOLAND TEST CHECKS GOOD.
ON MARCH 24, 2024 WHILE PERFORMING A CABIN CHECK, 2 SERVICE, AND LIFE VEST WRITE UPS ON A/C 4022 FOUND MULTIPLE SEAT ASSEMBLY ATTACH BOLT SAFETY LOCKS NOT PROPERLY INSTALLED OR DAMAGED. WHILE TRYING TO INSTALL CLIPS THE CORRECT WAY DISCOVERED 7 ROWS OF SEATS, ALL ON THE L/H SIDE OF THE AIRCRAFT, WERE NOT SET INTO SEAT TRACKS CAUSING THE CLIPS THE INSTALL THE WRONG WAY. FOUND THE TRACK FITTINGS ON SEAT ASSEMBLY TO BE SET ON TOP OF SEAT TRACKS AND NOT ENGAGED IN SEAT TRACKS. DISCREPANCIES WRITTEN ON LOG PAGES 7440786, 7440783, 7440776, 7440768, 7440759, 7440755, 7440741.
AFT BULK HEAD FR 65 R/H 32 SKIN AND STRINGER CORROSION PER HAECO LCQ NR 9290590/22590 GENERATED BY V798788 PART 3 OF THE LATEST REVISION OF ECRA 5341-01379 ON OR BEFORE 20 LATEST REVISION OF ECRA 5341-01379 ON OR BEFORE 20 SEP 2023. TOLERANCE UNDER 14CFR 26.43(D) AND WILL LIKELY BE MADE PERMANENT SEP 2023. NOTE TO PLANNING: ECRA 5341-01379 IS BEING EVALUATED FOR DAMAGE WITH REPEAT INSPECTIONS. REPAIR AT FUSELAGE SKIN LAP JOINT AT FR65-66, STR31-32RH REQUIRES DIP TO ACCOMPLISH PERMANENT REPAIR PER PART 3 OF THE CARRY APPROVED PER ECRA 5341-01379. ACCOMPLISH A PERMANENT TOMC-APPROVAL FROM SC1ELBYC COMMENT REPAIR PER PART 3 OF THE LATEST REVISION OF EC/RA 5341-01379 ON OR BEFORE 20SEP2023. COMPLIED WITH RII UPON FURTHER REVIEW, DAMAGE DESCRIPTION AND LOCATION IS AS ACCOMPLISHED INTERIM REPAIR, PART 1 WITH NO DEVATIONS IAW ECRA QC FOLLOWS; CORROSION DAMAGE ON FUSELAGE SKIN LAP JOINT AT FR65-66, 5341-01379 CORROSION DAMAGE ON FUSELAGE SKIN LAP JOINT AT STR31-32RH. FR65-66, STR31-32RH. AREA REQUIRES DIP TO ACCOMPLISH PERMANENT REPAIR AT FUSELAGE SKIN LAP JOINT AT FR65-66, STR31-32RH PER ADD EMP:V061737 QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
STR31R PRODUCED CRACK INDICARIONS APPROX. 7 INCHES FWD FR66 BELO W THE OUTFLOW VALVE DURING HFEC INSPECTION.GENERATED AT HAECO LC Q PER NR 9290886 (22886) BY V061690 REMOVED AND REPLACED STR31 RT IAW A319 SRM 51-72-11 ACPM BY V052 030
FR 68 LH AT STR 22 WEB FLANGE HAS CRACK INDICATION IN RADIUS ABO VE LOWER IB DOOR STOP BOLT APPROX .750 INCHES LONG STARTING AT I B RADIUS PER HAECO LCQ NR 9290477/22477 GENERATED BY V892444 48667 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION AT OR BEFORE 48667 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT THEREAFTER. INTERVALS NOT TO EXCEED 3200 FLIGHT CYCLES, THEREAFTER. INSPECTION AT INTERVALS NOT TO EXCEED 3200 FLIGHT CYCLES, REQUIRES DIP TO ACCOMPLISH INITIAL INSPECTION AT LH FR68, STR22 REPAIR AREA PER PART 2A OF LATEST REVISION OF ECRA 5341-01373 ON CARRY APPROVED PER ECRA 5341-01373. ACCOMPLISH INITIAL TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION PER PART 2A OF THE LATEST REVISION OF EC/RA 5341-01373 ON OR BEFORE 48,667 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,200 AIRCRAFT FLIGHT CYCLES, THEREAFTER. THE CURRENT PTC IS 32,167. COMPLIED WITH RII UPON FURTHER REVIEW, DAMAGE AREA AND DESCRIPTION IS AS FOLLOWS: INTERIM REPAIR ACCOMPLISHED TO LH FR68, STR22 DOOR STOP #1 FRAME QC L/H FR68, STR22 DOOR STOP #1 FRAME STIFFENER CRACKED APPROX STIFFENER IAW ECRA 5341-01373 WITH NO DEVIATIONS. REQUIRES DIP .750 INCHES LONG STARTING AT I B RADIUS TO ACCOMPLISH INITIAL INSPECTION AT LH FR68, STR22 REPAIR AREA ADD EMP:V929087 PER PART 2A OF LATEST REVISION OF ECRA 5341-01373 ON OR BEFORE QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
AFT CARGO FR 59 STR 38 SIGNS OF CORROSION (A3NB 53-4-6179). GENE RATED BY V798788 PER NR 9290613 (22613) AT HAECO LCQ. REMOVED AND REPLACED STRINGER 38RT FR59 IAW A319 SRM 51-72-11. P ERFORMED BY V052030 AND INSP BY V892285.
AFT CARGO BETWEEN FR 54 AND FR 55 LST 43 CORROSION PER HAECO LCQ NR 9290598/22598 GENERATED BY V798788 REPAIRED STR 43 LEFT IN AFT CARGO PIT BETWEEN FRAME 54-55 IAW A3 19 SRM 53-41-13-300-10 ACMP BY MECH V052030 INSP BY V935513
AFT CABIN AT R2 FRAME 68 HAS CORROSION AROUND NUT PLATE HOLE(A3N B-53-3-6357) GENERATED AT HAECO LCQ PER NR 9290811 (22811) BY V0 52030 LE REWORK =0.020?. REWORK IS BEYOND ALLOWABLE LIMIT. REPAIRED DI WITH AN INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLT 24000FLT C S, FH NOT RELEVANT IAW SRI 53-43-12-205-002. WRK BY V929057 SCREPANT AREA IAW SRM 53-41-12-300-001, REPAIR IS A CAT B REPAIR YCLES, FH NOT RELEVANT, SUBSEQUENT DVI INTERVALS 24000 FLT CYCLE REMOVED CORROSION IAW SRM53-41-12-283-001. BLENDED AREAS SMOOTH. NOMINAL THICKNESS =0.098?, MATERIAL REMOVED 0.0395. MAX ALLOWAB
AFT L2 DOOR SILL FASTENER HOLE CORRODED AT FRM 66 PER HAECO LCQ N/R 9290545/22545 GENERATED BY V937268 REMOVED AND REPLACED L-2 DOOR SILL AT FRM 66-68 IAW A319 SRM 51- 72-11-911-001 ACMP BY MECH V061630 INSP V061757
AFT CARGO ENTRY DOOR FLOOR PANEL HAS CORROSION PER HAECO LCQ N/R 9290604/22604 GENERATED BY V798788 REMOVED AND REPLACED AFT CARGO ENTRY DOOR COVER SHEET/DOOR FLOOR PANEL IAW A319 SRM 51-72-11 DND SRM 51-42-11 ACMP BY MECH V9290 87 INSP V061757.
AFT R2 DOOR SILL CORRODED MULTIPLE PLACES PER HAECO LCQ N/R 9290 546/22546 GENERATED BY V937268 REMOVED AND REPLACED R-2 DOOR SILL AT FR 66-68 IAW A319 SRM 51-7 2-11-911-001 ACMP BY MECH V061650 INSP V061757
AFT CABIN WET AREA RH FR68-FR69 O/B TRAY FASTENER HOLES ELONGATE D PER HAECO LCQ N/R 9290816/22816 GENERATED BY V061629. FABRICATED TRAY AT AFT CABIN WET AREA R/H FR68-69 O/B IAW A319 D RAWING 18D53480019 & REMOVED & REPLACED OLD TRAY IAW A319 SRM 51 -72-11-911-001 ACMP BY MECH V929087 INSP V061757.
LH E&E COMPARTMENT FR 11 WEB SUPPORT CRACKED PER HAECO LCQ N/R 9 290215/22215 GENERATED BY V798788 REMOVED/REPLACED WEB @ FR11 L/H IAW A-319 SRM TASK 51-42-11/001. SRM TASK 51-44-11/001 AND SRM 51-21-11/001 PER MECH V929087 INS P V061757.
AFT WET AREA LH SHEAR PLATE BETWEEN FRM 69 AND 70 FASTENER HOLE CORRODED (A3NB-53-3-6357) PER HAECO LCQ NON ROUTINE 9290558/2255 8 GENERATED BY V937268 REMOVED AND REPLACED CORRODED SHEAR PLATE AT L/H AFT WET AREA BE TWEEN FR 69+70 IAW A319 SRM 51-42-11/001+51-72-11-911-001 GENERA TED BY V929087
RH INTERNAL EMERGENCY DOOR FWD AND AFT WEB SUPPORTS SIGNS OF CRACK (SUPPORT TASK). GENERATED BY V798788 AT HAECO LCQ PER NR 9290 486 (22486). REMOVED AND REPLACED RH EMERGENCY DOOR FWD AND AFT WEB SUPPORTS IAW A319 SRM 51-42-11/001 PARG. E. PERFORMED BY V929087
R/H RUDDER SIDE PANEL PRODUCED AN INDICATION OF WATER INGRESS AP PROX. 178-186INS. FROM BOTTOM AND 2-6INS. FROM T/E. {A3NB-55-3-6 024} PER HAECO NON ROUTINE 9290079/22079 GENERATED BY V061690 AT HAECO LCQ REPAIRED RUDDER PN D5547100200000B TS-2319 178 TO 186 IN FROM BO TTOM 2 TO 6 IN FROM T/E ZONE F IAW A319 SRM 55-41-13-300-024 CAT EGORY A REPAIR PERFORMED BY V080675 INSP V304077
THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/08/22. PDA 3 FOUND FUEL CAP MISSING. INSTALLED CAP COUPLING REFUEL UNDERWING NOW OK.
REFERENCE ECRA 5310-07862 LH FR4 LATERAL WINDOW FRAME UPPER STIF FENER-INTERIM REPAIR. PER PART 1 STEP "8" "BEFORE FURTHER FLIGHT PERFORM A PERMANENT REPAIR PER PART 3 OF ECRA 5310-07862 ." ACCOMPLISH A PERMANENT REPAIR AT LH LATERAL WINDSHIELD FR 4 STIF FENER PER PART 3 OF LASTEST REVISION OF ECRA 5310-07896 ON OR BE FORE THE AIRCRAFT REACHES 50,921 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH A PERMANENT REPAIR AT LH LATERAL WINDSHIELD FR4 UPPER STIFFENER PER PART 3 OF LATEST REVISION OF ECRA 5310-07896 ON OR BEFORE THE AIRCRAFT REACHES 50,921 TOTAL AIRCRAFT FLIGHT CYCLES.
PDA 2 REFUELING CAP FOUND MISSING BY FUELER.
(SUPPORT TASK) EEPL WIRING HARNESS FOUND DAMAGED AT SEAT ROW 22A BC. N/R 9617226. REMOVED AND REPLACED EEPL WIRING HARNESS FOR SEAT ROWS 21ABC AND 22 ABC IAW AMM 33-51-22-400-802C1. OPS CHK GOOD IAW AMM 33-51-00-710-008-A.
AIR RETURN. AFTER LIFT OFF RECEIVED RECEIVED AVEC EXTRACT FAN FAULT WITH BLOWER FAN ON MEL. UNABLE TO PRESSURIZE AC. FOUND AIR INLET CHECK VALVE STUCK OPEN. VALVE DID CLOSED AFTER CLAMP WAS REMOVED. NEW VALVE AND CLAMP PLACED IN FLT DECK. REPLACED AIR CHECK VALVE PER AMM 21-26-56. TESTS GOOD. PRESSURIZED PER JRH 2-40-80. ALL TESTS GOOD.
CABIN EMERGENCY LIGHT TEST FAILED. FAULTED LEFT FWD EPSU, REPLACED POWER SUPPLY UNIT AND BATTERY PACK, TESTED, NO FAULTS IAW AMM 33-51-38.
FWD LT ENTRY DOOR, EMERGENCY LIGHT, ON THE LOWER FWD WALL, OTBD OF FA SEAT, IS MISSING THE LENS. REPLACED THE LENS. OPS CHECKED GOOD.
G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND SAFETY VALVE 49GA IN RIGHT WHEEL WELL DAMAGED AND CAUSING FLUID LOSS. REPLACED LANDING GEAR SAFETY VALVE IAW AMM 32-31-17. SERVICED GREEN HYD IAW AMM12-12-29. TESTED NORMAL IAW AMM32-33-00. MOTORED ENG 1 IAW CHECKLIST, GREEN HYD ATTAINED 3000PSI.
DURING CABIN EMERGENCY LIGHTS OPERATIONAL CHECK THE TEST FAILED, MESSAGE ESPU BATTERY FWD L 33-51-38. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL IAW 33-51- 38. OPS CHECK GOOD.
NR 2 ENGINE INCREASING SURGE DURING CLIMB, CLOSE TO NORMAL AT IDLE. FOUND J1 EEC CONNECTOR LOOSE. SECURED, PERFORMED POWER ASSURANCE RUNS TWICE. ALL ENGINE PARA NORMAL
DUE TO 2L DOOR SLIDE DEPLOYMENT, EMER CYLINDER DIAPHRAGM SHOULD BE REPLACED. REPLACED 2L DOOR EMER CYLINDER DIAPHRAGM IAW AMM 52-13-14. CHECKED OPERATIONS, ALL GOOD.
EMERGENCY POWER SUPPLY UNIT BATTERY FWD LT, FAULT WHEN PERFORMING EMER LIGHTS TEST. CLEANED CONNECTOR, OPERATIONS CHECKED NORMAL IAW AMM 33-51-38-000-001.
EMERGENCY POWER SUPPLY UNIT BATTERY EMER RT, FAULT WHEN PERFORMING EMER LIGHTS TEST. CLEANED CONNECTOR ON POWER SUPPLY, OPERATIONS CHECKED NORMAL IAW AMM 33-51-38-000-001.
FOUND FWD AFT LAVATORY OXYGEN MASKS DROPPED. RE-PACKED MASKS IAW AMM 3 5-21-43-550-801-A. REQUIRES MANUAL RELEASE CHECK IAW AMM 35-23-00-7 10-001-A.
FUEL TANK LANDING BETWEEN RIB 18 - 19 HAS 3 EACH HOLES ELONGATED AT HOLES G, C & B. REPAIRED IAW ECRA 5720-02680.
RIGHT AFT PASSENGER CREW DOOR STOP FITTING HOLES AT FRAME 66 WEB. FIRST STOP FITTING ABOVE FLOOR UPPER OUTBOARD HOLE IS CRACKED AT 5 O CLOCK. REPAIRED IAW SRM 53-41-12 PAR 5 E FIG 204.
RIGHT SIDE BOX UPPER FLANGE AT FRAME 43 HAS A CRACK AT AFT HOLE 6 O CLOCK POSITION. ACCOMPLISHED ON EA 5331-01704 RIGHT SIDE BOX BEAM FRAME 43.
LEFT SIDE BOX BEAM UPPER FLANGE AT FRAME 43 CENTER & AFT HOLE, CENTER HOLE AT 12 O CLOCK & AFT HOLE 6 O CLOCK POSITION, CRACKED. REPAIRED IAW EA 5331-017 04 LEFT SIDE BOX BEAM FRAME 43.
RIGHT ELEVATOR SKIN UPPER SURFACE HAS 8 TRAPPED WATER INDICATIONS. ALL 8 AREAS HAVE BEEN REPAIRED IAW SRM 55-21-11 PARA 5D.
LEFT ELEVATOR SKIN UPPER SURFACE HAS 9 TRAPPED WATER INDICATIONS. ALL 9 AREAS HAVE BEEN REPAIRED IAW SRM 55-21-11 PARA 5D OR 5E ON NR'S 49270, 49271, 49272, 49273, 49274, 49275, 49276, 49277 & 49278. SEE ECRA 5520-01463 FOR REPAIR SCHEME & MAPPED LOCATIONS.
EPSU BATTERY FWD LT MSG AFTER EMER LIGHT TEST. ACCOMPLISHED EPSU TEST FAULT MSG EPSU BATTERY LT DISPLAYED. REPLACED LT EPSU BATTERY IAW AMM 33-51-38. TEST OPERATES NORMAL.
EMERGENCY LIGHT TEST FAILED ON 2 SVC. REMOVED & CLEANED BATTERY CONTACTS IAW MM 33-51-00. OPERATIONS CHECKED GOOD.
NR 1 ENG FIRE EXT SUB FUNCTIONS TEST FAILED STEPS D4 & D5 OF TASK CARD 4R2640019 SEQ NR 358. THE VLV G PUMP FIRE FAILED TO CLOSE WHEN NR 1 ENG FIRE SWITCH WAS RELEASED. DUE TO THE INTERMITTENT OPERATION OF THE NR 1 ENG HYD FIRE VLV 1046G K, WE NEED TO REPLACE VLV 104GK IAW IPC 29-11-05-03B ITEM 190C & AMM 29-11-52 PG BLOCK 401. HYD FIRE VLV 1046GK REPLACED & FUNCTIONAL TEST ACCOMPLISHED ON DOCK WU W9162V.
NR 2 ENG PYLON FWD FIRE EXTINGUISHING BOTTLE SQUIB 5WE2 CONDUIT TORN & MISSING SECTION WIRE INSULATION, WEARING ON METAL CLAMP. REPLACE WIRE 2621-0003- CF20 FROM CONNECTOR 5WE2A TO CONNECTOR 474VC IAW WDM 26-21-03 ESPM 20-44-16 & ESPM 20-32-22.
SEAT 1E-F O-2 MASKS DROPPED ON TAKE-OFF. THEY ARE NOT ACTIVATED, REPACKED O2 MASKS. DEFERRED DROP CHECK IAW MAINT TIP 35-002.
EMERGENCY LIGHT TEST ON PTP FAIL. REPLACED BATTERY. OPS TEST IAW AMM 33-51-00-710-001, OK.
CREW REPORTED AFT INTERPHONE HANDSET WILL NOT HANG UP, BLOCKING CABIN COMMUNICATIONS. REPLACED CRADLE ASSY, CHECKED GOOD.
INTERPHONE IS INTERMITTENT AT LOCATION NOT SPECIFIED. CREW COMMENTS: CONTINUE NO METHOD TO COMMUNICATE IN FLT. INTERPHONE SYSTEM WAS WORKING IN IAH ON CHECK. REPLACED HANDSET, OP CHECK NORMAL.
METAL FAIRING PIECE ON TOP OF ENGINE 1 COWL IS STICKING UP. INSPECTED BULLNOSE SEAL AND SECURED FAIRING WITH 3 LAYERS OF SPEED TAPE PER MT54-009. TAPE MUST BE CHECKED AFTER EACH FLIGHT. PART NUMBER NEEDED IS PCN 110-2303. RPL- :REPLACED METAL HINGE COVER INBD REVERSER COWL NR 1 ENGINE.
CRACK FOUND ON NR 2 EXHAUST CONE AT 2 O`CLOCK POSITION 3-4 INCHES FROM END OF CONE. CRACK IS 1 INCH AND EXTENDS 1-4 INCHES INTO ZONE 3 IAW AMM. CONE REPLACED IAW ECRA 7811-01189.
NEED TO PERFORM LAND VERIFY, DUE TO CHANGE OF RIGHT AOA VANE AND LM5625 AND CH0639. PERFORMED LAND VERIFY IAW AMM 22-97-00, LAND VERIFY TEST PASS, AC REMAINS IN FULL CAT CAPABLE I STATUS. R&R FO'S AOA & PHC IAW AMM, INSTALLATION ONLY. SEE SMC1 FOR O 'S CHKS THAT FAILED WHEN IR2 SELECTED 2 ON. SHOWING PARTS R&R AND MRDATA TRANSACTIONS ONLY. T-S FOUND RT AOA AT FAULT. RANDR IAW AMM TASK 341119000001, OPS CHK GOOD.
NR 1 ENGINE INBOARD REVERSER HINGE SEAL PEELED AT AFT END. FOUND FLEX SEAL ON NR 1 ENGINE 54-57-22-07. DAMAGE 5" STICKING UP. REPLACED SEAL FILLER. REPLACED SEAL FILLER.
PANEL FASTENER LOOSE NEAR RIGHT PACK INLET. REPLACED NUT PLATES AND SCREWS ON PANEL 192KB.
F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). REPLACED F/O O2 MASK PER AMM.
RIGHT SIDE OF FCU LOOSE. SECURED RIGHT SIDE OF FCU PANEL.
EPSU INT LOAD EMER R' FAULT WHEN PERFORMING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK AND TESTED OKAY.
SMOKE LAVATORY SMOKE DETECTOR FAULT ON UPPER ECAM. REPLACED FWD SMOKE DETECTOR. TESTED OK PER AMM 26-17-15.
BRACKET FOR HALON EXTINGUISHER ON AFT WALL BROKEN. REPLACED AFT CABIN FIRE EXT BRACKET.
AFT GALLEY SMOKE SMELL AFTER ENGINE START WITH APU SHUT DOWN. SAMC TEXT: WITH AFT GALLEY EQUIPMENT SHUT OFF SMELL DISSIPATED. OPEN UP AFT GALLEY CEILING AND AFT GALLEY ELECTRICAL PANEL - PERFORM GVI OF AREA. DE-POWERED GALLEY REF MM, OPENED UP AFT GALLEY C-B PANEL: NO DAMAGE OR SMOKE SMELL NOTED. OPENED AFT GALLEY CEILING PANEL: NO SMOKE SMELL OR DAMAGE SEEN. RE-INSTALLED PANELS. PERFORMED TSM 49-00-00 287, NO DEFECTS NOTED. NO VISUAL LEAKS AND NO FUMES WITH APU RUNNING UNDER ELEC AND AIR LOAD.
CORROSION AT AFT PIT S42L, JUST AFT OF FRAME 51. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW ANGLE IAW DWG 10D53471007 ON NR C4163K, C4307K BY NR 308152 AND INSPECTED BY LC61.
R2 DOOR SILL HAS CORROSION ADJACENT TO GIRT FITTING AT FRAME 68. REPLACED R2 DOOR SILL.
CREW REPORT: CREW OXYGEN IS BELOW MINIMUMS. SERVICED O2. INITIAL READING WAS 790 PSI AND SERVICED TO FULL 1850 PSI. OXYGEN LEAK RECURRED. LOST 200 PSI IN 2HR 20MIN OF FLT TIME. SERVICED O2 SYSTEM TO 1890 PSI. APPLIED LEAK CHECK TO O2 BOTTLE CONNECTIONS. NO DEFECTS FOUND. SUSPECT PRESS REG & TRANSMITTER HAS INTERNAL LEAK. ACCOMPLISHED LEAK CK AND REPLACED PRESS REG & TRANSMITTER. OPS ARE NORMAL.
ACFT EXPERIENCED A PRESSURE DROP ON DESCENT. PFR SHOWS ECAM MSG 'CAB PR LO DIFF PR' AND 'CAB PR SAFETY VALVE OPEN'. PER TROUBLESHOOTING FOUND BOTH SAFETY VALVES AT FAULT. REPLACED BOTH SAFETY VALVES 6HL AND 7HL. OPS NORMAL.
CABIN EMERGENCY LIGHT TEST FAILED. POWER SUPPLY IN INOPERATIVE. REPLACED EPSU POSITION 12WL, TESTS OKAY.
GREEN HYD RESERVOIR LOW LEVEL MESSAGE, RTFL. ECAM PAGE CONFIRMS FLUID LOSS. SERVICED ALL HYD RSVR TO FULL. REPLACED NR 1 ENG GREEN EDP AND CASE DRAIN FILTER. THERE WAS NO METAL OR ANY EVIDENCE OF FAILURE. NO LEAKS PRESS 3000 PSI. MX FOUND A BLOWN STEEL BRAIDED HYD LINE ON THE UNLOCKING ACTUATOR IN THE NLG WHEEL WELL. REPLACED RT NLG UNLOCK ACT BRAIDED HYD PRESS LINE, NO LEAKS. DUE TO FREEFALL GEAR EXTENSION ACCMP'D AMM TASK TO PUT SYSTEM BACK INTO NORMAL MODE. ACP TASK REF AMM, NO FURTHER DISCREPANCIES.
EMERGENCY EXIT LIGHTS ILLUMINATE IN THE CABIN WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE OFF POSITION ON THE OVERHEAD PANEL 25VU WHEN AC POWER IS REMOVED FROM THE AIRCRAFT. REPLACED 126RH PANEL (AFT ATTENDANT). BITE AND EMERGENCY LIGHT CHECKS OKAY.
ALL LAVS - O2 MASK COMPTS - HOOK AND LOOP DETACHED FROM FABRIC, WHICH PUSHES MASKS OUT WHEN DOOR OPENS, MASKS DID NOT DROP IN 'D' LAV. FROM BASE W-U J7589B. REATTACHED HOOK AND LOOP TO FABRIC, MASK REPACK ON OV-JIC 4R3590091.
BURNING ELEC ODOR NEAR ROW 13. TURNED OFF CAB FANS AND ODOR DISSIPATED. FOUND READING LIGHT POWER SUPPLY ABOVE 15 DEF INOP. POWER SUPPLY IS DEACTIVATED AND SECURED. CALL LIGHTS OKAY. READING LIGHTS AT 15DEF INOP.
FOUND DENT JUST BELOW OUTFLOW VALVE PROTRUDING OUTWARD. REPAIRED DAMAGE IAW UA-EVA 73169.
REF LOG NR 3 ON EMERGENCY LIGHTS REMAIN ON WITH POWER OFF. ACCP TEST OF EMERGENCY LIGHT SYSTEM FROM FWD PANEL. FAULT SHOWS EMERGENCY LIGHT L INTERNAL LOAD FAULT AND NO COMM FAULTS WITH FWD, MID & AFT EPSU'S. REPLACED NR 1 CIDS DIRECTOR, LIGHTS CHK OK.
F/A REPORTED PLASTIC BURNING ODOR NEAR DOOR 2L. SMELL GONE AFTER 5 MINUTES.
F/A REPORTED PLASTIC BURNING ODOR NEAR DOOR 2L. SMELL GONE AFTER 5 MINUTES. REMOVED COFFEEMAKERS, RAN CHILLERS, CHECKED AFT LAVS AND AFT LAV HEATERS, CHECKED AFT CARGO COMPARTMENT. NO PLASTIC OR BURNING SMELL NOTED. RE-INSTALLED COFFEEMAKERS.
21AUG ORD CF -T : NR 2 ENG RIGHT SIDE FAN COWL GOUGED APPROX 3 INCHES FROM REAR ABOUT 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-71852, NO DELAMINATION PRESENT & APPLIED SPEED TAPE. RECHECK REPAIR AT NEXT A01 CHECK, REPAIR WITHIN 500 FLIGHT HOURS NOT TO EXCEED PTT 34736.
LAVATORY DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN, SMOKE. REPLACED LAV A SMOKE DETECTOR- NO MSGS.
LAVATORY SMOKE DETECTOR FAULT ON UPPER ECAM. FOUND SMOKE DETECTOR FAILURE. REPLACED SMOKE DETECTOR IN FWD LAVATORY. ALSO REPLACED SECURITY SEALS, JUNE 22.
FLIGHT DIVERTED UNDER AMBER ALERT DUE TO A CRACKED WINDSHIELD. FOUND MOISTURE PENETRATION AT BUSS BAR CAUSING DELAMINATION, SCRAPPED WINDOW. REPLACED CAPTAIN'S WINDSHEILD AND CAPT WINDOW HEAT COMPUTER.
FLIGHT DIVERTED DUE TO LOSS OF GREEN HYD SYSTEM. [06-22-07] OPERATIONAL CHECKS FOUND GREEN HYDRAULIC SYSTEM PRESSURE AND FLUID LEVELS TO BE NORMAL, BUT WAS REPORTING LOW. FURTHER FAULT TRACING FOUND THE WIRING IN THE NR 1 EDP PRESSURE SWITCH CONNECTOR WAS DAMAGED AND CAUSING AN INTERMITTENT SHORT. REPLACED THE SWITCH CONNECTOR.
RETURN TO FIELD DUE TO AN EXTRACT FAN FAULT. ECAM EXTRACT FAN FAULT DISPLAYED AFTER TAKEOFF. REPLACED BLOWER FAN AND AVIONICS FILTER. OPS. TEST PER 21-26-00. OPS CHECKS GOOD.
RETURN TO FIELD UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM FAILURE. FOUND CUT SEAL ON HYDRAULIC LINE. REPLACED SEAL, FOUND GREEN RESERVOIR WITH THREE GALLONS OF HYD FLUID. RESET MANUAL GEAR EXTENSION. SERVICED SYSTEM TO FULL. RAN ALL HYDRAULIC PUMPS, NO LEAKS FOUND.
WHITE EEL LIGHTS ARE INOPERATIVE AT ROWS 6 ABC AND 20 ABC. REPLACED EEL LIGHTS. OPS CHECKED NORMAL.
FLIGHT EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE. REPLACED THE HYDRAULIC SAFETY VALVE.
RETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. CAUSE OF STALL WAS FOUND TO BE LIBERATED SECTION OF HIGH PRESSURE COMPRESSOR (HPC) 5TH STAGE BLADE. LIBERATION CAUSED DOWNSTREAM DAMAGE, INCREASED TIP CLEARANCE, AND REDUCED SURGE MARGIN OF HPC TO STALL POINT.
ECAM GREEN HYDRAULIC LOW QUANTITY FL 370 CRUISE. *S/D* FOUND STRONG LEAK ON GREEN HP MANIFOLD PRESSURE LINE. REPLACED O-RING, CKD FOR LEAKS THROUGHOUT AREA AND NO LEAKS FOUND.
RECEIVED UNCOMMANDED YAW INPUT WHICH RESULTED IN AUTOPILOT DISENGAGEMENT. *S/D* YAW DAMPER ACTUATOR HAS BEEN ISOLATED AS THE PROBLEM. THIS UNIT HAS NOT BEEN REPLACED ON THE AIRCRAFT AS OF 2/21/99. BUT THERE IS NO UNCOMMANDED YAW INPUT WITH THE YAW DAMPER NR 1 DISCONNECTED AND THE HYD LINES CAPPED AND STOWED. THIS UNIT IS A KNOWN PROBLEM UNIT, ESPECIALLY ON THE NR 1 SIDE (LEFT). THE LEFT SYSTEM SEES A HIGHER CYCLE RATE FROM THE HYD SYSTEM AS CONFIRMED ON AIRBUS MESSAGE 953.0811/99.