N416UA

Part: FUEL CAP — MISSING (FUEL COUPLING) · airframe 88,930 hrs · 34,712 cycles

REFUEL COUPLING CAP MISSING. NONE IN STOCK AT TPA. M&E 31-2825-9-0001. PARTS NEEDED ADDED TO MATERIAL LIST NIS TAMPA. NO FUEL CAPS IN STOCK TPA, NO LEAKAGE NOTED ON FUEL FILL PORT. MEL APPLIED AND PARTS UPDATED. DISPATCH DESK: 33 NAME: T A DATE: 14-JUL-22- OK TO DEFER MISSING FUEL CAP PER CDL 28A. THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/15/22.REFUEL COUPLING CAP MISSING. NONE IN STOCK.R&R REFUEL COUPLING CAP, OPS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: FITTING — CHAFED (RT MLG WW) · airframe 82,877 hrs · 32,039 cycles

RMLG W/W AT KEEL BEAM - DOOR FITTING FWD LUG HAS A AREA WITH CHA FING AROUNDTHE BOLT SUPPORT TASK AD RELATED PER HAECO LCQ NR 92 92371 REMOVED R/H FWD HINGE FITTING AND R/H ACTUATOR FITTING REAMED AN D INSTALLED FREEZE PLUGS IN BOTTOM PANEL AND LONGERON LAYERS LOC ATED DRILLED AND INSTALLED REPLACEMENT HINGE AND ACTUATOR FITTIN G IAW EC/RA 5331-02528

Part: SKIN — CORRODED (RT WING) · airframe 82,877 hrs · 32,039 cycles

RH WING TOP SKIN UPPER SURFACE RIB 25+7" 2" AFT OF FIXED L/E SKI N HAS CORROSION ON HAECO LCQ REF 9292401 SPEC A3NB-05-3-6104. NR GENERATED BY V061595 HAECO TECHNICIAN V061619 AND QC LC-111 REPAIRED RH WING TOP SKIN AND RIB 25+7" 2"AFT OF FIXED LE SKIN IAW ECRA 5721-01435 PART 1 .CREATE DIP LP TO ACCOMPLISH THE PERMANENT REPAIR AT RH WING TOP ADD EMP:V061619 PANEL 2 UPPER SURFACE FRONT SPAR RIBS 25-26 PER PART 3 OF ECRA 5 721-01435 ON OR BEFORE 18MAY2020. PLANNING TO CONTACT ENGINEERIN G AFTER 18APR2020 BUT BEFORE 01MAY2020 FOR PERMANENT REPAIR. ACCOMPLISH THE PERMANENT REPAIR AT RH WING TOP SKIN PANEL 2 UPPER SURFACE FRONT SPAR RIBS 25-26 PER PART 3 OF ECRA 5721-01435 ON OR BEFORE 18MAY2020. PLANNING TO CONTACT ENGINEERING AFTER 18APR2020 BUT BEFORE 01MAY2020 FOR PERMANENT REPAIR.? TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RECORDS UPDATE QC REVIEWED INIT: PLN/ENG >4/18/20 <5/1/20 T/A: ON OR BEFORE 18MAY20...AN/U345625

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 82,877 hrs · 32,039 cycles

AFT CABIN FLOOR STRUCTURE - L/H SHEAR PLATE HAS A 1/2" CRACK FRA ME 69-70 A3NB-53-3-6222 PER HAECO LCQ NR 9292154 GENERATED BY V8 92441 REMOVED AND REPLACED NEW SHEAR PLATE AT AFT CABIN FLOOR STRUCTUR E L/H FR69-70 IAW A320 SRM 51-72-11-911-001 WORK ACCOMPLISHED BY V061619 INSPECTED BY LC-09 V892441

Part: COVER — MISSING (TE FLAP) · airframe 81,759 hrs · 31,517 cycles

RT WING #2 MOVABLE FLAP TRACK FAIRING MISSING INBOARD COVER FOR ATTACHMENT BOLT. COMPLIED WITH CDL DISPATCH DESK: 36 DATE: 01-JUL-19- APPROVED COMPLIED WITH CDL INSTALLED NEW COVER.

Part: ANGLE — DEFECTIVE (FRAMES 35-36) · airframe 81,461 hrs · 31,393 cycles

ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5330-06559 ON O R BEFORE 03 DEC 2019. PLANNING TO CONTACT ENGINEERING AFTER 01 O CT 19 BUT BEFORE 31 OCT 19 FOR THE PERMANENT REPAIR. PART 1 HAS BEEN COMPLIED WITH IN THIS ECRA 5330-06559. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5330-06559 ON O R BEFORE 03 DEC 2019. PLANNING TO CONTACT ENGINEERING AFTER 01 O CT 19 BUT BEFORE 31 OCT 19 FOR THE PERMANENT REPAIR. PART 1 HAS BEEN COMPLIED WITHIN THIS ECRA 5330-06559. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5330-06559 ON O R BEFORE 03 DEC 2019. PLANNING TO CONTACT ENGINEERING AFTER 01 O CT 19 BUT BEFORE 31 OCT 19 FOR THE PERMANENT REPAIR. PART 1 HAS BEEN ACCOMPLISHED. OPBLM CHRISTIANSEN TOMC-APPROVAL FROM SC1ELBYC COMMENT **LH AND RH FR 35-36 PRESSURE PANEL CRACKS, INTERIM REPAIR REFER ENCED IN ECRA 5330-06559. OPBLM CHRISTIANSEN QC REVIEWED. QC REVIEWED. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5330-06559A ON OR BEFORE 03 DEC 2019. PLANNING TO CONTACT ENGINEERING AFTER 01 OCT 19 BUT BEFORE 31 OCT 19 FOR THE PERMANENT REPAIR. PART 1 HAS BEEN COMPLIED WITH PER ECRA 5330-06559A. DEC 2019.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 77,413 hrs · 29,633 cycles

DURING EMERGENCY LIGHT CHECK, FOUND THE LEFT OVERWING EMERENCY POWER SUPPLY UNIT WITH INTERIOR LIGHT FAULT AND EXTERIOR LIGHT FAULT. REMOVED AND REPLACED THE POWER SUPPLY CONTROL UNIT AND BATTERY IAW AMM 33-51-38, PERFORMED EPSU OPS CHECK IAW AMM 33-51-38 AND OPS CHECKED GOOD. SYSTEM CHECKED OK, NO FAULTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 77,292 hrs · 29,579 cycles

RIGHT FWD AND AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. INSPECTED EMERGENCY EXIT DOOR. NO FAULTS NOTED, ALL INDICATONS NORMAL.

Part: CONNECTOR — UNSECURE (LIGHT MODULE) · airframe 77,292 hrs · 29,579 cycles

RIGHT FWD AND AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, SHOWS NOT CLOSED IN FLIGHT. ACFT PSI NORMAL. FOUND SLIDE ARM LIGHT MODULE PARTIALLY DISCONNECTED. SECURED IAW AMM 52-73-21. SYS OPS NORMAL,

Part: SKIN — CORRODED (FRAMES 54-55) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO SKIN BETWEEN FRAMES 54 - 55, STRINGERS 43R - 43L AROUND DOMENUTS HAS SPOTS OF CORROSION. ACCOMPLISHED A REPAIR IAW SRM 53-00-300-013.

Part: FITTING — DAMAGED (RT MLG DOOR) · airframe 77,001 hrs · 29,433 cycles

RIGHT FWD MLG DOOR FITTING DAMAGED. REMOVED AND REPLACED THE RT FWD MLG DOOR FITTING IAW SRM 51-72-11, PARA 2.

Part: STRINGER — CORRODED (FRAMES 53-60) · airframe 77,001 hrs · 29,433 cycles

STRINGER 42L, FRAMES 53 - 60 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11 -911-001.

Part: STRINGER — CORRODED (FRAMES 57-58) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO BAY FRAMES 57 - 58, STRINGER 43L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

L-2 DOOR SILL/THRESHOLD CORROSION 9 EA LOCATIONS FROM FRAME 66 TO FRAME 68. REMOVED AND REPLACED L-2 DOORSILL BETWEEN FRAMES 66 TO FRAME 68 ON MAIN CABIN IAW SRM 51-42-11-001 PARAGRAPH D, 2 AND F.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

THRESHOLD PLATE HAS CORROSION TOP SURFACE AROUND 2EA NUTPLATES. REMOVED & REPLACED FWD CARGO THRESHOLD PLATE PN D5323058520007 IAW SRM 51-72-11-911-001. TOPCOATED IAW SRM 51-75-12-00 1 PARAGRAPH 3.

Part: SHEAR TIE — CORRODED (FRAME 55) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO BAY FRAME 55, STRINGER 41 - 42L SHEAR TIE HAS SURFACE CORROSION. REMOVED THE SHEAR TIE AND CLEANED THE CORROSION, AND REINSTALLED. THE SHEAR TIE WAS FOUND TO BE IN LIMITS AFTER CORROSION REMOVAL IAW DWG D534 70757HBD0001 AND SRM 57-72-11

Part: DOOR FRAME — CRACKED (FRM 68) · airframe 77,001 hrs · 29,433 cycles

LEFT AFT PAX DOOR CUTOUT, FRAME 68 DOOR STOP FITTING 1, LOWER INBOARD HOLE IS CRACKED IN FRAME LAYER AT THE 6:00 POSITION. REPAIRED DOOR FRAME IAW SRM 53-41-12-300-011, SHEET 2, FIGURE 20111, PG 44.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO COMPARTMENT FR53 STRINGER 41L-42L CLEAT HAS SURFACE CORROSION. REMOVED AND REPLACED CLEAT AT FR53 STR 41L-42L IAW SRM 51-72-11.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO COMPARTMENT FR 54 STRINGER 43L-44 CLEAT HAS SURFACE CORROSION. REMOVED & REPLACED CLEAT AT FR54 STR43L-44 IAW SRM 51-752-11.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO COMPARTMENT FR 55 STRINGER 42L-43L CLEAT HAS SURFACE CORROSION. REMOVED AND REPLACED CLEAT AT FR 55 STR 42L-43L IAW SRM 51-7 2-11.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO FR57 STRINGER 39L-40L CLEAT HAS SURFACE CORROSION. REMOVED AND REPLACED CLEAT AT FR57 STR 39L-40L IAW SRM 51-7 2-11.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 77,001 hrs · 29,433 cycles

R2 DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-11-001, PAR G, 2R AND 2F AND MT 53-025 PG. 4 ITRM 48,

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 77,001 hrs · 29,433 cycles

LEFT WING L/E CAVITY SUPPORT ANGLE CRACKED, OTBD OF THE NR 7 SLAT TRACK. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-42-11, PARA. D, E,

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO COMPARTMENT FR62 STRINGER 40R HAS SURFACE CORROSION. REPAIRED AFT CARGO COMPARTMENT STRINGER 40R BETWEEN FR61-FR63 PER SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO COMPARTMENT FR57 STRINGER 39L HAS SURFACE CORROSION. REPAIRED AFT CARGO COMPARTMENT STRINGER 39L BETWEEN FR56 AND FR5 8 PER IAW SRM 53-00-13-300-001.

Part: SPAR — CRACKED (LT ELEVATOR) · airframe 77,001 hrs · 29,433 cycles

LEFT ELEVATOR FWD SPAR HAS A CRACK. REPAIRED THE LT ELEVATOR SPAR IAW SRM 55-21-18-300 -002.

Part: FITTING — CORRODED (FWD CARGO DOOR) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO DOOR FRAME AFT CORNER FITTING CORRODED IAW SRM 51-72-11-911-001. REMOVED & REPLACED THE CORNER FITTING IAW SRM 51-72-11-911-001.

Part: FITTING — DAMAGED (AFT CARGO DOOR) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO DOOR CUT OUT NR 2 LOCKING FITTING GOUGED. REMOVED THE GOUGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-46-11-283-001. INSTALL A NEW LOCKING FITTING IAW SRM 51-72-11-911-001, AND 51-42-11-001.

Part: STRINGER — CORRODED (FRAMES 53-60) · airframe 77,001 hrs · 29,433 cycles

STRINGER 41L, FRAMES 53 - 60 FOUND CORRODED. R & R THE STRINGER IAW SRM 51-72-11-911-001.

Part: FRAME — CORRODED (FRM 66) · airframe 77,001 hrs · 29,433 cycles

R2 DOOR, FRAME 66, ONE INCH ABOVE THE DOOR SILL HAS CORROSION. REPAIRED IAW SRM 53-41-12-300-002, SRM 51-11-12-001, TABLE 00110, AND GMM 03-20-20, FIG 1.

Part: DOOR FRAME — CRACKED (FRM 68) · airframe 77,001 hrs · 29,433 cycles

RIGHT AFT DOOR CUTOUT FRAME 68, STOP FITTING NR 1 LOWER INBOARD HOLE IS CRACKED IN FRAME LAYER AT 6:00 AND 12:00. REPAIRED THE DOOR FRAME IAW SRM 53-41-12-300-011.

Part: THRESHOLD — CORRODED (FRAMES 25-28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO DOOR THRESHOLD FRAMES 25 - 28, HAS SURFACE CORROSION. REMOVED & REPLACED THE THRESHOLD IAW SRM 5 1-72-11-911-001.

Part: FITTING — CORRODED (CARGO DOORWAY) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO DOORWAY, FWD CORNER FITTING HAS CORROSION, REMOVED & REPLACED THE FITTING IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 40 - 41R SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: PLATE — CORRODED (LAVATORY VENT) · airframe 77,001 hrs · 29,433 cycles

LAVATORY EXHAUST VENT REINFORCEMENT PLATE CORRODED ON INTERIOR SIDE. REMOVED THE PLATE IAW SRM 51-42-11-001, FABRICATED A NEW LAVATORY EXHAUST VENT REINFORCEMENT PLATE AND INSTALLED IAW SRM 51-42-11-001, PAR E.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 40 - 41R SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 30, STRINGERS 43R - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 43L - 43R SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FORWARD CARGO BAY, FRAME 34 BETWEEN STRINGERS 41 - 42L, HAS THE SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · airframe 77,001 hrs · 29,433 cycles

AFT CARGO BAY FRAMES 58 - 59 LT FLOOR SUPPORT HAS SURFACE CORROSION. REMOVED AND REPLACED IAW SRM 51-72-11-911-001,

Part: FITTING — CORRODED (L2 DOOR) · airframe 77,001 hrs · 29,433 cycles

CORROSION ON THE L2 DOOR FWD CORNER FITTING. REMOVED AND REPLACED CORNER FITTING AT FRAME 66 IAW SRM 51-42-11-001, PARAGRAPH F.

Part: FITTING — CORRODED (L2 DOOR) · airframe 77,001 hrs · 29,433 cycles

L2 DOOR, AFT LOWER CORNER FITTING CORRODED. 3 INCHES FORWARD OF FRAME 68. REMOVED AND REPLACED THE CORNER FITTING IAW SRM 51-42-11-001, PARAGRAPH D AND F.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAMES 30-31, STRINGER SPLICE 43L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAMES 30 - 31, STRINGER SPLICE 41L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAMES 30 - 31 STRINGER SPLICE 42L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: STRINGER — CORRODED (FRAMES 58-64) · airframe 77,001 hrs · 29,433 cycles

STRINGER 41R, FRAMES 58 - 64 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 57-42-11 PARA 2.E, & 2.F, PROTECTED AREA IAW SRM 51-23-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 28, STRINGERS 42 - 43R SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 39 - 40L, SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 41 - 42L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 30, STRINGERS 40 - 41R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 42 - 43R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 28, STRINGERS 40 - 41L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 40 - 41R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 28, STRINGERS 42 - 43L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 33, STRINGERS 43 - 44R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 41 - 42R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 39 - 40L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 40 - 41L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51- 72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 32, STRINGERS 39 - 40L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 39 - 40L, THE SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 26, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72-1 1-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGER 40 - 41L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 42 - 43R SHEAR TIE CORRODED. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 39 - 40R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 42 - 43R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 41 - 42R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 39 - 40R, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 28, STRINGERS 43L - 43R, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 34, BETWEEN STRINGERS 42 - 43R SHEAR TIE CORRODED. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 42 - 43R, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 30, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 34, BETWEEN STRINGERS 42 - 43L, SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGER 39 - 40L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 43R - 43L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FORWARD CARGO BAY, FRAME 34, BETWEEN STRINGERS 43 - 44L SHEAR TIE CORRODED. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 30, STRINGERS 40 - 41L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 40 - 41R SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 40 - 41L SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 32, STRINGERS 40 - 41L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 33, STRINGERS 42 - 43L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 41 - 42R, SHEAR TIE HAS SURFACE CORROSION. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 34, BETWEEN STRINGERS 41 - 42R SHEAR TIE CORRODED. R & R THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 26, STRINGERS 42 - 43R, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51- 72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 34, BETWEEN STRINGERS 40 - 41L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 29, STRINGERS 41 - 42R SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-7 2-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 29, STRINGER 40 - 41L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-7 2-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-7 2-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 26, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72-1 1-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 31, STRINGERS 37 - 38L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 30, STRINGERS 41 - 42L, SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 26, STRINGERS 40 - 41L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72-1 1-911-001.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 28, STRINGERS 41 - 42L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 32, STRINGER 41 - 42R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 31, STRINGERS 43R - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 27, STRINGERS 42 - 43L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 31, STRINGER 42 - 43R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 20) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 30, STRINGER 41 - 42R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY FRAME 30, STRINGERS 42 - 43R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 30, STRINGERS 39 - 40L SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 27, STRINGERS 43L - 43R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 26) · airframe 77,001 hrs · 29,433 cycles

FWD CARGO BAY, FRAME 26, STRINGERS 43L-43R SHEAR TIE HAS SURFACE CORROSION. REMOVED & REPLACED SHEAR TIE IAW SRM 51-72- 11-911-001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,670 hrs · 29,291 cycles

EMERGENCY LIGHT TEST FAULTS DOOR 1 LEFT. REPLACED DOOR 1 LEFT BATTERY AND TEST PER MM 33-51-38. CHECKS NORMAL.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 75,846 hrs · 28,922 cycles

EMERGENCY LIGHT TEST FAULT RT BATTERY PACK. REPLACED THE RIGHT BATTERY PACK IAW AMM 33-51-38-000-002A, AND 33-51-38-400-002A. OPS CHECKED OK.

Part: STRUT — FAULTY (TE FLAP) · airframe 75,696 hrs · 28,858 cycles

FLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. REF LOG PG 4359813 LINK ASSY BUSHING RR, REF LOG PG 4359903 RT I /B AND O/B ROLLERS RR, REF LOG PG 4359750 LT I/B O/B ROLLERS RR, REF LOG 4360620 LT INTERCONNECTING STRUT RR, REF LOG 4360607 RT INTERCONNECTING STRUT RR. PERFORMED OPERATIONAL TEST OF THE FLAP SYSTEM AMM 27-54-00-710-001-A, OPERATIONAL CHECK GOOD

Part: COMPUTER — MALFUNCTIONED (FLAP/SLAT SYS) · airframe 75,586 hrs · 28,813 cycles

FLAPS LOCKED, ALIGNMENT FAULT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. PFR SHOWED F/CTL FLAPS LOCKED WITH ASSOCIATED FLP1 & FLP2, CHECKED LT MECH DRIVE FAILURE MESSAGE. PERFORMED TSM 27-51-00-810-819A. VERIFIED A PPU DATA WITHIN LIMITS. RESET WTB. PERFORMED VISUAL INSPECTION OF FLAP TRANSMISSION ASSY. PERFORMED VISUAL INSPECTION OF APPU (29CV) ZERO DATUM MARK. MARKS ARE ALIGNED AND NO WATER PRESENT. PERFORMED OPERATIONAL TEST OF FLAP & SLAT SYSTEMS. REPLACED THE NR 1 SFCC IAW MM 27-51-34-400-001-B. COMPLIED WITH SFCC BITE IAW MM 27-81-00, AND 27-51-00. COMPLIED WITH OPS CHECK OF FLAP & SLAT SYSTEM IAW MM 27-54-00. NO FAULTS NOTED. COMPLIED WITH LAND TEST IAW MM 22-97-00. NO FAULTS NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 60,953 hrs · 24,791 cycles

CABIN EMERGENCY LIGHTS TESTED WITH A FAULT MESSAGE. RESET SYSTEM, ALL CHECKED GOOD

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 67,313 hrs · 25,292 cycles

CREW REPORTS NLG WILL NOT RETRACT AFTER TAKEOFF. RETURN TO FIELD, OVERWEIGHT LANDING.

Part: CABLE — FAULTY (L2 DOOR) · airframe 66,262 hrs · 24,877 cycles

AT CRUISE DOOR 2L SHOWED NOT ARMED. FLIGHT ATTENDANT MOVED HANDLE SLIGHTLY TO ARM, HANDLE NOT FLUSH. DOOR WAS ARMED AT DEPARTURE IN FLIGHT HANDLE MOVED. RESEATED & HANDLE MOVED AGAIN WITH NOT ARMED MESSAGE ON ECAM. REPLACED ARMING FLEX CABLE IAW AMM 52-13-22.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,972 hrs · 24,758 cycles

DENT AT FRAME 15 LT SIDE OF FUSELAGE APPROX STRINGER 20, CF9073. MEASURED DENT & FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLER IAW SRM 53-00-11 FIG 240. REPAIR REQUIRES RE-INSPECTION 60000 FLIGHT CYCLES AFTER REPAIR EMBODIMENT IAW SRM 53-00-11 PG 289 TABLE 224.

Part: FRAME — DENTED (FUSELAGE) · airframe 65,972 hrs · 24,758 cycles

DENT AT FRAME 15 LT SIDE OF FUSELAGE APPROXIMATELY STRINGER 20. MEASURED DENT & FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLER IAW SRM 53-00-11, FIG 240.

Part: SKIN — GOUGED (FUSELAGE) · airframe 65,972 hrs · 24,758 cycles

FUSELAGE GOUGE BETWEEN FR 1 & 2 ON BELLY. INSTALLED DOUBLER REPAIR IAW SRM53-00-11 FIG 244.

Part: DRAIN VALVE — LEAKING (RT WING) · airframe 65,854 hrs · 24,717 cycles

FUEL DRIPPING FROM RT WING. INBD OFF WING VENT. REPLACED WATER DRAIN VALVE, LEAK CHECKED GOOD.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 65,759 hrs · 24,681 cycles

CREW REPORTS EVIDENCE OF BIRD STRIKE ON THE FAN EXIT GUIDE VANES OF THE NR 1 ENGINE AT THE 6 O'CLOCK POSITION.

Part: PACKING — LEAKING (GREEN SYSTEM) · airframe 65,640 hrs · 24,631 cycles

GREEN SYSTEM HIGH PRESSURE MANIFOLD LEAKING RT WW CENTER CEILING AREA. REPLACED UNION & PACKING FOR GREEN SYSTEM HIGH PRESSURE MANIFOLD IAW IPC 29-11-15-05 PAGE 1 OF 12 ITEM 50 & ITEM 60.

Part: CVR — NO TEST (COCKPIT) · airframe 65,152 hrs · 24,439 cycles

SQUEAL WHEN CVR TESTED. SQUEAL EXISTS WITH ALL MICS DISCONNECTED & SPEAKERS OFF AND CVR TEST SQUEALS.

Part: TILLER — UNSECURE (COCKPIT) · airframe 65,154 hrs · 24,440 cycles

CAPTAIN'S NOSE WHEEL STEERING PEDALS DISCONNECT PUSH BUTTON INOPERATIVE. DURING PROCESS OF TROUBLESHOOTING, FOUND CAPTAIN'S TILLER HANDLE NOT FULLY SEATED. REMOVED HANDLE AND REINSTALLED. CAPTAINS DISCONNECT SWITCH, OPS CHECKED NORMAL.

Part: SMOKE DETECTOR — DAMAGED (FWD LAVATORY) · airframe 65,109 hrs · 24,424 cycles

FORWARD LAVATORY SMOKE DETECTOR SECURITY SEAL MISSING AND THE DETECTOR HAS BEEN PARTIALLY OPENED. MOUNTING FOR DETECTOR IS CRACKED, BUT DETECTOR IS SECURE. DETECTOR INOP. SMOKE DETECTOR IS SECURED IN PLACE. NEED HSG ASSY AND NEW DETECTOR. REPLACED LAV "A" SMOKE DETECTOR ASSY, OPS CK GOOD.

Part: DRAIN LINE — CLOGGED (LAVATORY) · airframe 65,067 hrs · 24,404 cycles

FORWARD AFT LAVATORY SINK DRAIN INOPERATIVE. DEFERRED. RDF-T : FOUND LAVATORY WATER SHUTOFF VALVE UNDER SINK IS LETTING WATER BY CAUSING INBOUND LOG NR 1. FLIGHT ATTENDANT PEELED BACK CLEAR TAPE TO LET WATER DRIP INTO SINK. SINK WAS HALF FULL WATER AS SINK DRAIN LINE FOUND CLOGGED.

Part: DRAIN LINE — CLOGGED (LAVATORY SINK) · airframe 65,067 hrs · 24,404 cycles

CREW LAVATORY SINK DRAIN INOPERATIVE. FOUND LAVATORY WATER SHUTOFF VALVE UNDER SINK IS LETTING WATER BY, CAUSING INBOUND CLOG. F/A PEELED BACK CLEAR TAPE TO LET WATER DRIP INTO SINK. ON ARRIVAL, SINK WAS HALF FULL WATER AS SINK DRAIN LINE FOUND CLOGGED.

Part: B-NUT — LEAKING (LT WING) · airframe 64,860 hrs · 24,321 cycles

FLUID ACTIVELY DRIPPING FROM LT WING JUST UT ENG 1. FOUND PRESSURE LINE B-NUT LOOSE ON NR 3 LT WING SPOILER, TIGHTEN AND NO LEAKS NOTED.

Part: SKIN — DAMAGED (WING) · airframe 45,026 hrs · 16,076 cycles

LEFT & RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, & 540NB.1EA HOLE AT EACH PANEL. PANEL IS 540RB PER AIRBUS RAS-BAE-1005046-200 7. ACP INSPECTION PER ECRA 5720-02377. FOUND NO DAMAGE,ALL FASTNERS SECURED. (ORIGINAL DIFFICULTY DATE IS 5/31/2008, MORE THAN 5 YEARS OLD, CHANGED TO ENTER INTO THE SYSTEM.)

Part: WIRE — EXPOSED (SEAT 20A) · airframe 64,563 hrs · 24,210 cycles

20A WIRES EXPOSED IN ARMREST. SECURED WIRES.

Part: TUBE — OUT OF POSITION (PSU) · airframe 64,099 hrs · 24,019 cycles

OXYGEN PANEL DOOR FELL OPEN 24DEF. MASKS DID NOT DEPLOY. OXY DOOR DID NOT OPEN. THE RUBBER TUBING ALONG THE PSU CAME OUT AND CAUSED THE PSU TO DROP SLIGHTLY. INSTALLED TUBING AND PSU INTO PLACE.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 63,749 hrs · 23,885 cycles

HYD Y RSVR LO LEVEL MSG DURING LANDING ROLLOUT. CREW ALSO HAD HYD Y ENGINE 2 PUMP LO PR AND HYD Y SYSTEM LO PR MESSAGES. HYD SYSTEM PAGE SHOWS LOSS OF FLUID. FOUND A BROKEN LINE TO INBOARD SYNC LINE. REPLACED LINE & SERVICE YELLOW HYD TO FULL. CYCLED NUMBER 2 THRUST REV, NO LEAKS NOTED. PCN 222-0239

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 63,519 hrs · 23,794 cycles

NR 1 BRAKE DRAGING, NEEDED EXTRA POWER TO TAXI AND PULLED LEFT AND HOT BRAKE AFTER TAKEOFF. BLED BOTH YELLOW AND GREEN HYDRAULIC BRAKE SYSTEMS PER MM FOR BRAKES 1 AND 2. ACFT WENT FOR TAXI TEST AND CREW REPORTS ALL BRAKE OPERATION NORMAL. TEMPS NORMAL AND NO EXCESSIVE POWER NEEDED TO MOVE ACFT.

Part: FAIRING — VIBRATION (FUSELAGE) · airframe 63,000 hrs · 23,600 cycles

VIBRATION AND AUDIBLE RUMBLE FELT AND HEARD THRU OUT THE FLIGHT DECK. DUE TO "SCORE" ON VIB REPORTING SHEET, APPLY SPEED TAPE TO BELLY FAIRING SEALS IDENTIFIED IN MT53-004. CREATE CF WITH "AK" AS REPAIR LIMIT AND "D" IN METERS. PERFORMED MT53-005 AND BELLY FAIRING SEALS SCORED HIGHEST. INSPECTED NOSE GEAR DOORS, EXT PWR DOOR, RADOME AND BELLY FAIRINGS. SECURED PANELS 191 & 192 DT WITH SPEED TAPE PER MT 53-004. DL1207 CREATED TO MONITOR.

Part: SPAR — GOUGED (NR 1 PYLON) · airframe 62,334 hrs · 23,321 cycles

NR 1 PYLON AFT FIXED FAIRING HAS DEEP GOUGE ON LOWER SPAR. WELD REPAIRED GOUGE IAW A320 SRM 54-50-00 AND 54-54-11, REPAIR REQUIRES RE-INSPECT AT NEXT C-CHECK PER SRI 54-50-00, TBL 105.

Part: ACTUATOR — DETERIORATED (HORIZ STAB) · airframe 62,334 hrs · 23,321 cycles

THS ACTUATOR BALLSCREW LOWER STOP INTERIOR IS DETERIORATED AND SWELLING. REMOVED AND REPLACED THS ACTUATOR IAW AMM

Part: CABLE — BROKEN (EMERGENCY EXIT) · airframe 62,334 hrs · 23,321 cycles

EMERGENCY DOOR HATCH CABLE BROKEN RIGHT SIDE REMOVED & REPLACED OVERWING RESERVOIR. FUNCTION & OP CHECK GOOD IAW A320 MM. ON N-R V9746K.

Part: LANYARD — FRAYED (EVAC SLIDE) · airframe 62,334 hrs · 23,321 cycles

L1 DOOR SLIDE LANYARD IS FRAYED WHERE ATTACHED TO GIRT BAR. REMOVED & REPLACED SLIDE ASSY IAW A320 MM.

Part: UNKNOWN — MALFUNCTIONED (LAVATORY) · airframe 62,223 hrs · 23,269 cycles

EN ROUTE LAVS STARTED TO OVERFLOW. LAV WASTE LEVEL INDICATOR SHOWS FULL. INDICATOR SHOWS OK BEFORE AND AFTER SERVICING LAVS. SENSOR CLEANED OFF FROM LAST SEVERAL DAYS SERVICING.

Part: INDICATOR — INOPERATIVE (RUDDER) · airframe 61,799 hrs · 23,103 cycles

RUDDER TRIM POSITION INDICATOR INOP. REPLACED RUDDER TRIM INDICATOR.

Part: RADIO — INTERFERENCE (NR 2 VHF SYSTEM) · airframe 61,698 hrs · 23,060 cycles

CAPT VHF RADIO SOUNDS SCRATCHY WHEN ON PA WITH MINITEL. OK WHEN INTFN OR CABIN OR VHF 1-2, REPLACED CAPT MINITEL.

Part: TRANSDUCER — FAULTY (ELEVATOR) · airframe 61,588 hrs · 23,013 cycles

CREW REPORTS ELAC 1 FAULT WITH PITCH TRANSIENT(JOLT). ACFT RETURNING TO THE FIELD OPBLM FIELDS. REPLACED SIDE STICK TRANSDUCERS 4CE1 AND 4CE2, ELACS 1&2. COMPLETED WIRING CHECKS, SEE SEQ#5886050 & 5886049 FOR WORK ACCOMPLISHED. REPLACED RT ELEVATOR OUTBOARD ACTUATOR SERVO VALVE, SEE SEQ#5886051 FOR WORK ACCOMPLISHED.

Part: TRANSDUCER — FAULTY (COCKPIT) · airframe 61,588 hrs · 23,013 cycles

ELAC FAULT, RTFL SUPPLEMENTAL DATA UPDATE REPLACED CAPTAINS SIDE STICK ROLL TRANSDUCER (4CE1). REPLACED FIRST OFFICERS SIDE STICK ROLL TRANSDUCER (4CE2) PER MM. REPLACED ELAC NR 1 AND 2. REPLACED RT. BLUE SYS. SERVO VALVE, OPS CHECKED NORMAL.

Part: BALLAST — ODOR (GALLEY LIGHTS) · airframe 61,371 hrs · 22,920 cycles

BURNING SMELL FROM AFT GALLEY W- COFFEE AND CHILLERS ON. FOUND AFT FA PANEL LOCKED UP, CYCLED POWER AND FAULT CLEARED. REPLACED BOTH AFT OVERHEAD LIGHTS ASSEMBLIES & BALLAST AND RELAMPED. GROUND CHECKED OKAY.

Part: TRANSCEIVER — INTERMITTENT (VHF COMM) · airframe 60,721 hrs · 22,654 cycles

VERY HIGH FREQUENCY RADIO (VHF) 2 INOP - COM 999. CREW COMMENTS: SQUELCH IS INOPERATIVE INTERMITTENTLY. REPLACED NR 2 VHF, RADIO CHECK OKAY.

Part: SWITCH — DIRTY (FIRE DETECTION) · airframe 60,582 hrs · 22,593 cycles

ENG 1 AGENT DISCHARGE LIGHT ILL. DISCHARGE LIGHT ON INTERMITTENTLY WITH PUSH OF TEST BUTTON ON OVERHEAD FIRE PANEL. CLEANED TEST SWITCH AND ACCOMPLISHED TEST OF ENG-1 LOOP-SQUIB OPERATIONAL TEST. TESTS NORMAL.

Part: SWITCH — FAULTY (FIRE WARNING) · airframe 60,582 hrs · 22,593 cycles

ENG 1 AGENT DISCHARGE LIGHT ILL. DISCHARGE LIGHT ON INTERMITTENTLY WITH PUSH OF TEST BUTTON ON OVERHEAD FIRE PANEL. CLEANED TEST SWITCH AND ACCOMPLISHED TEST OF ENG-1 LOOP-SQUIB OPERATIONAL TEST. TESTS NORMAL.

Part: VALVE — LEAKING (HYDRAULIC SYS) · airframe 59,942 hrs · 22,315 cycles

NR 1 ENG PUMP FIRE VALVE LEAKING. LEAK FOUND WHILE TROUBLESHOOTING LM2480. REPLACED NR 1 ENG PUMP FIRE VALVE REF MM. NEW VALVE FAILED OP CHECK DUE TO INDICATION ON LOWER ECAM DID NOT WORK. INDICATION ON VALVE WORKS NORMAL LT. REPLACED VALVE, NO LEAKS NOTED.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 59,572 hrs · 22,150 cycles

AT GEAR RETRACTION, AFTER TAKEOFF, CREW HEARD A LOUD BANG FROM NOSE GEAR AREA. PLEASE INSPECT NOSE GEAR, WHEEL WELL & IMMEDIATE AREA FOR ANY DEFECTS OR ABNORMALITIES. REPORT FINDINGS TO SAMC. SAMC TEXT: RADOME DAMAGED, PART MOVING IN. REPLACED RADOME.

Part: EPSU — FAULTY (CABIN) · airframe 59,240 hrs · 22,008 cycles

REF A-CK JIC 4-2020 ITEM 24 FAILS EMERGENCY LIGHTS BATTERY CAPACITY TEST MSG DISPLAYED AFTER TEST BATTERY CAP EMER R. REPLACED BATTERY, NO HELP. SUSPECT EPSU. REPLACED EPSU, OP CHECKS OKAY.

Part: DIRECTOR — MALFUNCTIONED (NR 2) · airframe 59,140 hrs · 21,967 cycles

CABIN PA-INT HANDSETS INOPERATIVE. RESET CIDS: NO HELP. SWAP CIDS DIRECTORS. SWAPPED THE NR 1 AND NR 2 CIDS DIRECTORS. BEFORE THE NEXT REVENUE DEPARTURE REPLACE THE NR 2 CIDS DIRECTOR MR23731-38 PCN582-9022 PER AMM. REPLACED NR 2 CIDS DIRECTOR PER MM, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 59,098 hrs · 21,943 cycles

(INT LOADS FWD LT) MSG SHOWS AFTER EMERGENCY LIGHTS TEST. ON CABIN CIDS DISPLAY. PLACED SLIDE LIGHT BYPASS TEST PLUG, ONE AT A TIME AT EACH DOOR SLIDE. MSG REMAINS EACH TIME. REMOVED CONNECTOR ON FWD LEFT BATTERY ABOVE CEILING PANEL AT DOOR 1L. CLEANED CONTACT POINTS & RECONNECTED. TESTED BOX-SYS OK-RESULTS. PERFORMED EMERGENCY LIGHT TEST THREE TIMES. RESULTS TEST OK THREE TIMES.

Part: B-NUT — LEAKING (LT MLG) · airframe 59,071 hrs · 21,928 cycles

HYD FLUID LEAKING FROM LEFT MAIN LANDING GEAR AND AROUND LEFT GEAR DOOR BELLY AREA. ACCOMPLISHED LM1665. FOUND IN LT GEAR AREA LINE WITH LOOSE B-NUT. SECURED B-NUT AND LEAK CHECKED NO LEAKS NOTED. ALSO ACCOMPLISHED LM1663 AND LM1664.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 58,995 hrs · 21,891 cycles

LEFT WHEEL WELL HAS FLUID LEAK. FLUID LEAK FOUND ON PREFLIGHT WALKAROUND. REPLACED LT MLG RETRACT ACTUATOR. REPLACED PIN (P/N 201590900 - SERIAL# HP11183 - (POSIT LH). ACCOMPLISHED OPS CHECK. NO LEAKS NOTED.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 58,312 hrs · 21,599 cycles

DOOR 2L LAVATORY SMOKE DETECTION INOP. LAV INOP DO NOT USE. LAV DOOR LOCKED AND WASTE RECEPTACLE TAPED CLOSED. REPLACED LAV SMOKE DET, NO HELP, NEED FURTHER TROUBLESHOOTING. REPLACED SMOKE DETECTOR.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 57,819 hrs · 21,378 cycles

FO'S WINDSHIELD HEAT IS INOP. REPLACED WINDOW HEAT CONTROLLER NR 2. BITE TEST OKAY.

Part: WIRE — SHORTED (FUSELAGE) · airframe 57,350 hrs · 21,179 cycles

FOUND WIRE 7109-B DAMAGED AND SHORTING TO SHIELD. DAMAGE IS IDENTIFIED WITH MASKING TAPE NEAR MIDDLE BLOWOUT PANEL, FWD PIT FWD BULKHEAD. REPLACED WIRE 7109-A AND 7109-B FROM TERMINAL BLOCK 1842VT TO BENCH PLUG AD OF SFCC-2. OPS CHECK AND TESTS ACP, CHECK OKAY.

Part: PUMP — FAULTY (FUEL CELL) · airframe 57,343 hrs · 21,176 cycles

IAW INBD CREW ZERO FUEL IN CTR TANK UPON DEPARTURE. ON ARRIVAL AT DESTINATION, FOUND 480 LBS OF FUEL IN THE CTR TANK. REMOVED JET ADAPTOR ASSY FROM SCAVENGE JET PUMP 66QM AND CHECKED FOR BLOCKAGE, FOUND ASSY AND JET PUMP CLEAR OF ANY BLOCKAGE. REPLACED FQIC PER MM AS A PRECAUTION. ACCOMPLISHED BITE TEST AS REQUIRED. FQIC TESTED GOOD. NO DEFECTS NOTED. REPLACED BOTH RT & LT CENTER FUEL TANK FUEL PUMP CANISTER CHECK VALVES AND LT CENTER TANK FUEL PUMP.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,306 hrs · 21,155 cycles

NOTICED ELECTRICAL BURNING ODOR IN CABIN. CREW REPORTED GEN 1 FAULTED SEVERAL TIMES ON TAXI OUT, NUMEROUS FAULTS REPORTED ON BUSS 1 THRU CFDS. AFTER APU PUT ON LINE, WITH ENG 2 POWERING BUSS 2, IT APPEARED GEN 2 HAD PROBLEMS REFLECTED BY A FAULT LIGHT & FLICKERING LIGHTS. INSPECTED CONNECTORS AT FIREWALL ON BOTH EINGINES. NO DISCREPANCY FOUND. RAN APU AND BOTH ENGINES WITH BOTH PACK OPERATING, CYCLED LT AND RT GENERATORS ON & OFF, DID NOT DETECT AN ELECTRICAL ODOR IN CABIN OR COCKPIT. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,302 hrs · 21,152 cycles

MAJOR REPAIR. AFT PIT CORROSION AT FRAME 52A STRINGER 38R AND 39R. REO L01295 AND A-B RAS-DAHAM-4033757-2011 THIS REPAIR IS CONSIDERED MINOR WITH NO SUPPLEMENTAL INSP REQUIRED. PERMANENT REPAIR. CORROSION REMOVED IAW SRM. NDT IAW NTM, NO RELEVANT INDICATIONS. MAX DEPTH OF .059 WITH .177 REMAINING. INSTALLED FILLER. NR M6876L & M6907L BY 311041 AND INSPECTED BY LC100.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,302 hrs · 21,152 cycles

CORROSION ON STR 43R BETWEEN FRAMES 57 & 58. MAJOR REPAIR ACCOMPLISHED: REPLACED FACTORY STR SECTION REF SRM FIG 201 ON NR M6636L.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,302 hrs · 21,152 cycles

CORROSION ON STR 43L BETWEEN FRAMES 54 AND 60. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRINGER REPAIR IAW SRM ON NR M6607L.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,302 hrs · 21,152 cycles

CORROSION ON S43L AFT FRAME 31 IN FWD PIT. EVALUATED CORROSION AND FOUND IT OUT OF LIMITS OF SRM. REMOVED DAMAGED SECTION & FAB AND INSTALLED NEW SECTION & REPAIR SPLICES FROM FR 30 TO FR 31. THIS REPAIR VALID UNTIL 31DEC 2013 ONLY.

Part: STRINGER — CORRODED (STR 42L) · airframe 57,302 hrs · 21,152 cycles

CORROSION ON STRINGER 42L BETWEEN FRAMES 56 & 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICED STRINGER REPAIR IAW SRM ON NR M6637L.

Part: CLAMP — BROKEN (BLUE HYD LINE) · airframe 56,952 hrs · 20,993 cycles

BLUE HYD LOW QTY ECAM, FLIGHT DIVERTED. FOUND HYDRAULIC FLEX HOSE ASSY LEAKING AT BROKEN ATTACH CLAMP. PRESSURE LINE FROM BLUE PUMP, P/N AE707414-2 AOG# X3601. REPLACED BLUE SYS HYD PRESSURE LINE AND CLAMP FROM EMDP. PRESSURIZED AND LEAK CHECKED LINE. NO LEAKS NOTED.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 56,305 hrs · 20,667 cycles

EMERGENCY LIGHT TEST FAULTS BATTERY AFT LEFT. REPLACED BATTERY AT 13WL, OPS CHECKS GOOD.

Part: WIRE — BROKEN (OXY GENERATOR) · airframe 56,305 hrs · 20,667 cycles

WHILE REINSTALLING AFT LT DOOR OVERHEAD PANEL FOUND BROKEN WIRE ON THE OXYGEN GENERATOR. REPLACED O2 GEN ASSY, ACP O2 MASK DROP, CHECKED OK.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 56,184 hrs · 20,615 cycles

EMERGENCY LIGHT TEST AT CIDS PANEL. REPLACED BATTERY AT POS 11 WL, OP CKS OK.

Part: ENGINE — SPARKS (NR 2 EXHAUST) · airframe 56,034 hrs · 20,551 cycles

IAW CREW: ABORTED TAKEOFF DUE TO FELT NOSE GEAR VIBRATION. ACCOMPLISH FULL TROUBLESHOOTING PROCEDURE FOR ENG STALL TSM. DEBRIEFED CREW ON RETURN. CREW STATES PASSENGER AT ROW 21 SAW SPARKS AND FLAME OUT OF NR 2 ENGINE EXHAUST. POST FLIGHT REPORT INDICATES ECAM WARNING: ENG 2 STALL AND FAILURE MESSAGE: VSV MECH-BLEED VALVE V-LPC2 SOURCE EIU2 FADEC. REMOVED AND INSTALLED ENGINE. ENGINE INSTALLATION COMPLETED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 56,024 hrs · 20,545 cycles

CABIN EMERGENCY LIGHT TEST, 'BATTERY EMER'. REPLACED BATTERY IN EMERGENCY LIGHT POWER SUPPLY. BELOW THE RT OVERWING HATCH IAW AMM. OPS CKD GOOD. REPLACED BATTERY.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 55,404 hrs · 20,259 cycles

LOSS OF THE YELLOW HYD FLUID. FOUND LEAK FROM RT ENG PYLON SIDE FIREWALL DISCONNECT, LINE ON AOG ETA OPEN. INSTALLED RING LOCK REPAIR ON HYD LINE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 54,194 hrs · 19,663 cycles

G HYD SYS LOSS. ACCOMPLISHED FREEFALL EXTENSION. NR 1 ENG EDP WAS TURNED OFF APPROX 1 MINUTE AFTER SYS PRESSURE WENT TO 0-PSI. LEAKING LINE IDENTIFIED IN PYLON. REPLACED GREEN SYS EDP. REPLACED EDP FILTER AND GREEN SYS CASE DRAIN FILTER REPLACED PRESS LINE FOR NR 1 ENG REV CONTROL. LEAK CHECK NORMAL.

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 49,455 hrs · 17,709 cycles

BATTERY EMERGENCY R DISPLAYED AFTER CHECK OF CABIN EMERGENCY LIGHT TEST. *S/D* WEAK BATTERY. REPLACED BATTERY PER MM. TEST OK.

Part: O-RING — FAILED (PTU CHECK VALVE) · airframe 48,745 hrs · 17,464 cycles

LOSS OF PRESSURE IN YELLOW HYD SYSTEM. FLT RTFL. YELLOW ELECTRIC HYD PUMP IS LEAKING. REPLACED O-RING ON PTU CHECK VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,618 hrs · 17,419 cycles

15C EMERGENCY LIGHT INOP. RELAMPED. OP CK GOOD.

Part: LIGHT — INOPERATIVE (SEAT 22A) · airframe 48,287 hrs · 17,300 cycles

EMERGENCY LIGHT INOP AT SEAT 22A. REPLACED LIGHT AND HARNESS. CHECKS OKAY.

Part: CONTROL UNIT — INTERMITTENT (BSCU 2) · airframe 48,231 hrs · 17,280 cycles

ACFT PULLS STRONGLY TO THE RIGHT. REQUIRES LEFT TILLER AND OR LEFT BRAKE INPUT. REPLACED NOSE WHEEL STEERING CONTROL VALVE,REPLACING BSCU AND CAPT'S TILLER TRANSMITTER- ALL MTC SEEMS TO HAVE FIXED ISSUES WITH STEERING, A/C TAXI TEST PERFORMED AND PASSES- A/C TRACKS STRAIGHT WITH NO TILLER.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 48,224 hrs · 17,276 cycles

CREW O2 LOW, NEEDS SERVICE (1520PSI). SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, NO LEAKS WERE NOTED AT THE TIME OF SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,004 hrs · 17,213 cycles

SEAT MOUNTED AISLE EMERGENCY FLOOD LIGHT AT SEAT 22C INOP. LAMP INOP. RELAMPED, OPS CHECKED NORMAL.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 47,835 hrs · 17,153 cycles

CREW REPORT: 2R DOOR ARMED BUT THEN DISARMED AND WOULD NOT ARM AGAIN. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, DOOR ARMS AND DISARMS NORMALLY.

Part: LIGHT — NO TEST (CABIN) · airframe 46,985 hrs · 16,814 cycles

AFT LEFT DOOR FAILED EMERGENCY LIGHT TEST.

Part: OXYGEN MASK — LEAKING (1ST OBSERVER'S) · airframe 46,342 hrs · 16,571 cycles

THE 1ST OB'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: O2 FLOWS CONTINUOUSLY. SUPPLEMENTAL DATA UPDATE CAUSE: REGULATOR LEAKING ON O2 MASK. REPLACED MASK ASSY AND PROPERLY RESTOWED. SERVICED O2 SYSTEM TO PROPER LIMIT.

Part: CONTROL MODULE — FAULTY (NLG STEERING) · airframe 46,314 hrs · 16,556 cycles

NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* NOSE GEAR STEERING MODULE FAULTY. REPLACED NOSE GEAR STEERING SERVO CONTROL MODULE.

Part: VHF COMM — MALFUNCTIONED (COCKPIT) · airframe 46,045 hrs · 16,454 cycles

FLT CREW EXPERIENCED DIFFICULTIES TRANSMITTING VIA VHF RADIO SHORTLY AFTER TAKEOFF. DECISION MADE TO DIVERT FLIGHT.

Part: EXTINGUISHER — READS LOW (COCKPIT) · airframe 45,514 hrs · 16,251 cycles

FIRE EXTINGUISHER PSI IN COCKPIT LOW. LOSS OF PRESSURE IN BOTTLE (FIREXT) REPLACED HALON FIRE EXT IN COCKPIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,043 hrs · 16,083 cycles

SEAT 11C EEL LIGHT RED HAS 1 OF 2 LAMPS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,043 hrs · 16,083 cycles

FWD BULKHEAD EMERGENCY EXIT SIGN HAS 1 LAMP OUT, CTR AISLE OVERWING FWD EXIT SIGN HAS 3 EA LAMPS INOP, CTR AISLE AFT SIDE OVERWING EXIT SIGN HAS 4 EA LAMPS OUT, LEFT OVERWING EXIT SIGN HAS 1 EA LAMP INOP, RIGHT AFT DOOR OVERHEAD EXIT SIGN HAS 2 EA LAMPS INOP & RIGHT AFT DOOR AFT LWR SIDE WALL EXIT SIGN HAS 1 LAMP INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,043 hrs · 16,083 cycles

SEAT 19C EEL LIGHT HAS 1 OF 2 LAMPS INOPERATIVE.

Part: SKIN — DAMAGED (WINGS) · airframe 45,026 hrs · 16,076 cycles

LEFT AND RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, AND 640NB, 1EA HOLE AT EACH PANEL.

Part: BLADES — FRACTURED (NR 2 ENGINE) · airframe 44,624 hrs · 15,929 cycles

ENGINE NR 2 STALLED AT FL360 MACH .78, STALL CLEARED, STALL RECURRED AND CLEARED. EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. [07-24-07] HPC BORO REVEALED QTY. 2 STAGE 6 BLADES FRACTURED AT MID SPAN.

Part: COMPRESSOR — STALLED (LEFT ENGINE) · airframe 44,500 hrs · 15,878 cycles

POSSIBLE ENGINE COMPRESSOR STALL ON TAKEOFF. SUSPECT LEFT ENG. NO ECAM, PFR SHOWS NR 2 ENGINE COMPRESSOR STALL. [SUP 05-18-07] QTY 2 STAGE 6 HPC BLADES LIBERATED AT MID-SPAN WITH DOWNSTREAM DAMAGE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENG FIRE) · airframe 41,565 hrs · 14,807 cycles

ON DESCENT INTO ORD, NR 1 ENGINE FIRE INDICATION LIGHT CAME ON FOLLOWED BY NR 2 ENGINE FIRE LIGHT. NR 1 ENGINE FIRE LIGHT WENT OUT. REPLACE NR 2 FDU PER AMM26-12-34, REF TSM 26-21-00-810-820.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,227 hrs · 14,693 cycles

EMERGENCY PATH LIGHTS FOUND INOP FROM ROW 1 TO 5. CHECKED SYSTEM ACCORDING TO ASM 33-51-00 AND FOUND FAULT ON BATTERY POWER SUPPLY 110WL1. REPLACED UNIT DESCRIBED, TEST GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 41,181 hrs · 14,681 cycles

EEL LIGHT WILL NOT TURN ON AT ROWS 15,16 & 17. SECURED CONNECTOR 7260VC6, OPERATION NORMAL.

Part: LIGHT — NO TEST (CABIN) · airframe 40,746 hrs · 14,515 cycles

EMERGENCY LIGHTING CHECK FAILS 3 SERVICE TESTS. REPLACED LEFT FRONT BATTERY PACK. SYSTEM TESTED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,497 hrs · 13,672 cycles

EMERGENCY EXIT LIGHT OUT AT SEAT 6ABC. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 6ABC

Part: BLADE — FAILED (NR 1 ENGINE) · airframe 35,722 hrs · 12,691 cycles

AT 10,000 FT THROTTLE AT NORMAL SETTING JUST ABOVE IDLE, LOUD NOISE WAS HEARD FROM NR 1 ENGINE. EGT WENT RED AND VIBRATION INDICATION STAYED AT 6.0. REPLACED NR 1 ENGINE. TEARDOWN REVELAED A STAGE THREE BLADE FAILED IN THE DOVE TAIL AREA. THIS PROBLEM IS NOT LIMITED TO ANY ONE PART NUMBER. OEM IS DEVELOPING A NEW DESIGN C3 BLADE FOR FLEET INCORPORATION.

Part: RAM AIR TURB — INOPERATIVE (EXTERIOR) · airframe 33,474 hrs · 11,901 cycles

RAT DOES NOT WORK. WOULD NOT PRESSURIZE BLUE SYSTEM OR PROVIDE ELECTRICAL POWER. TEST BOX MALFUNCTIONED CAUSING ERONOUS INDICATIONS.

Part: ANNUNCIATOR — FAILED (COCKPIT) · airframe 33,001 hrs · 11,723 cycles

ABORTED TAKEOFF AT 110 KNOTS DUE TO LOSING BOTH FLIGHT MODE ANNUNCIATORS. PROBLEM COULD NOT BE DUPLICATED ON GROUND. POST FLIGHT REPORT DID NOT INDICATE ANY FAULT. FMGC1 WAS REPLACED AS A PRECAUTION. OPERATIONS CHECK NORMAL.

Part: IDG — OVERTEMP (NR 1 ENGINE) · airframe 27,580 hrs · 9,646 cycles

ABORTED TAKEOFF AT 80 KNOTS DUE TO LEFT ENGINE IDG FAULT LIGHT. NR 1 ENGINE IDG FAULT LIGHT CAME ON DURING TAKEOFF. NR 1 IDG REMOVED AND REPLACED.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 26,935 hrs · 9,377 cycles

AIRCRAFT UNABLE TO MAINTAIN PRESSURE. VALVE REPLACED ALONG WITH THE AVIONICS COMPUTER.

Part: PRESSURE SWITCH — LEAKING (APU) · airframe 19,333 hrs

STRONG ODOR MOSTLY IN AFT CABIN AND ON FLIGHT DECK. FLEW WITH CABIN FANS OFF, HI FLOW, AND NR 1 PACK OFF. BECAME TOLERABLE. *S/D* ISOLATED OIL SMELL TO APU. REPLACED APU REF MM 49-11-98.

Part: WINDOW — NOT LATCHED (LT COCKPIT)

ABORTED TAKEOFF AFTER PILOTS WINDOW OPENED AT 80-90 KTS. PILOTS REPORTED WINDOW WAS NOT FULLY LOCKED. *S/D* CAPTAIN'S SLIDING WINDOW WAS NOT FULLY LOCKED. RED-COLORED RELEASE BUTTON ON WINDOW HANDLE POPS UP WHEN THE WINDOW IS LOCKED. THIS SERVES AS A VISUAL INDICATION. ENSURING THAT WINDOW IS FULLY CLOSED AND LOCKED PRIOR TO TAKEOFF HAS BEEN AND REMAINS AN ELEMENT OF THE FLIGHT CREW'S PREFLIGHT CHECKLIST.

Part: FAN — FAILED (E & E COMPT)

VENT EXTRACT FAN BLOWER ECAM MESSAGE. CREW REPORTED SLIGHT VIBRATION IN COCKPIT AND SMOKE FROM AVIONICS COMPARTMENT.

Part: STRUT — REQUIRED SERVICE (NLG)

LANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO DEN. *S/D* ECAM L/G SHOCK ABSORBER FAULT. SECURED LOOSE SENSOR TARGET. PERFORMED NLG STRUT SVC.

Part: PROX SENSOR — MALFUNCTIONED (LANDING GEAR)

ECAM MESSAGE SHOCK ABSORBER FAULT. CB RESETS ON LGCIU'S, NO HELP. DIVERTED TO DENVER AMBER ALERT. *S/D* CFDS INDICATED PROX SENSOR 24GA AT FAULT. REPLACED SENSOR PER MM 32-31-73.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHTS INOP AT 16ABC, 17, 18, 22, 23, 24ABC.

Part: LIGHT — BROKEN (CABIN)

EMERGENCY LIGHT BROKEN OFF.

Part: LIGHT — MALFUNCTIONED (CABIN)

RIGHT REAR OVER WING EMERGENCY EXIT LIGHT CAME ON IN LIGHT TURBULENCE. PROBLEM COULD NOT BE DUPLICATED AND CAUSE COULD NOT BE DETERMINED. UPON SUBSEQUENT REINSPECTIONS, NO PROBLEM COULD BE FOUND.

Part: SLIDE — LEAKING (LT OFF WING)

LEFT HAND OFF WING ESCAPE SLIDE REMOVED FOR FIRST OVERHAUL WAS FOUND TO HAVE NUMEROUS AREAS OF POROSITY AND A SEAM LEAK ON THE CROSS TUBE WHICH CAUSED THE UNIT TO FAIL AN AIR RETENTION TEST. PATCHED AND REPAIRED DAMAGED AREAS PER VENDORS MANUAL.

Part: PROXIMITY SENSOR — OUT OF ADJUST (FWD CARGO DOOR)

AT FL 310, RECEIVED ECAM MESSAGE THAT FORWARD CARGO DOOR OPEN. NO PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA: UPDATE PROXIMITY SENSORS WERE FOUND OUT OF ADJUSTMENT. ADJUSTED SENSORS AND OPERATIONALLY CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATED NORMAL.