N417FE

Part: IRU — MALFUNCTIONED (ZONE 100) · airframe 45,080 hrs · 22,782 cycles

NR 1 IRS FAULT ON TAKEOFF. RELEASED FOR SERVICE IAW MEL: 34-25-01 CATEGORY: C EXPIRATION: 03OCT10 SWAPPED NR1 AND NR3 IRU, REF AMM 34-25-34-04 AND NR1 SYS TEST IAW AMM 34-25-00-05, PLACED NR3 POSITION ON DEFERRED IAW MEL. "MEL 34-25-01: IRU NR 3 - INOP.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,038 hrs · 22,746 cycles

EMERGENCY LIGHTS TEST FAILED FROM THE COURIER AREA PUSHBUTTON. R & R EMERGENCY POWER SUPPLY BATTERY, TEST GOOD IAW AMM 33-51-14.

Part: ACTUATOR — FAILED (R1 DOOR ASSIST) · airframe 45,038 hrs · 22,746 cycles

R1 DOOR EMERGENCY CYLINDER ACTUATOR FAILED TEST. REMOVED AND REPLACED THE EMERGENCY CYLINDER ACTUATOR IAW AMM 52-10-14-4. SERVICED ACTUATOR IAW AMM 52-10-14-4. PERFORMED INSPECTION CHECK AND CHECKED GOOD IAW AMM 52-10-14-6.

Part: FITTING — CRACKED (ZONE 700) · airframe 45,038 hrs · 22,746 cycles

LT NLG DOOR ACTUATOR MOUNT FITTING SHOWS CRACK INDICATION ON THE OTBD AFT CORNER OF THE FITTING. R & R LT NLG DOOR ACTUATOR FITTING IAW SRM 51-40-21, PARA 5 & 7. TESTED GOOD IAW AMM 32-31-16-04.

Part: STRUCTURE — WORN (NR 3 SPOILER) · airframe 45,038 hrs · 22,746 cycles

LT WING SPOILER NR 3 T/E SILL IS WORN (KNIFE EDGE). R & R LT WING NR 3 SPOILER T/E RUB STRIP IAW SRM 51-40-21.

Part: ATTACH ANGLE — CRACKED (NR 1 PYLON) · airframe 45,038 hrs · 22,746 cycles

NR 1 PYLON-TO-ENGINE FWD ATTACH MOUNT, INBD UPPER ATTACH ANGLE IS CRACKED. R & R NR 1 PYLON TO ENGINE FWD ATTACH MOUNT, INBD UPPER ATTACH ANGLE SHEET IAW SRM 51-40-21, PARA 5 AND SRM 51-72-10.

Part: ATTACH ANGLE — CRACKED (ZONE 400) · airframe 45,038 hrs · 22,746 cycles

NR 1 PYLON-TO-ENGINE FWD ATTACH MOUNT OTBD UPPER ATTACH ANGLE IS CRACKED. REMOVED BLEED AIR DUCT, LOWER NR 1 PYLON TO GAIN ACCESS. R & R NR 1 PYLON OTBD FWD ATTACH MOUNT, UPPER ATTACH ANGLE SHEET IAW SRM 51-40-21. REINSTALLED BLEED AIR VALVE IAW AMM 20-21-12-0.

Part: SKIN — DELAMINATED (NR 2 SPOILER) · airframe 45,038 hrs · 22,746 cycles

NR 2 RT WING SPOILER LOWER SURFACE T/E IS DEBONDED AT THE OTBD HALF. REPAIRED DEBOND OF T/E ON NR2 SPOILER BY INJECTING AND RIVETING AREA IAW SRM 57-70-00 AND EA 6-5750-136689, " WINGS - RT NR2 SPOILER T/E DELAMINATED".

Part: RIB — CHAFED (ZONE 400) · airframe 45,038 hrs · 22,746 cycles

NR1 PYLON AFT FAIRING RIB 19 WEB IS CHAFED. R & R RIB 19 ASSY IN THE NR1 PYLON AFT FAIRING IN REF TO SRM 51-40-21, PARA 6 AND PARA 13.

Part: ANGLE — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

NR 2 PYLON AFT STRUCTURE, FWD / RT INBD VERTICAL ANGLE IS FRETTED. BLENDED OUT DAMAGED AREA IAW SRM 51-73-10, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-00, FIG 10, PG 111 (MORE THAN 25 PERCENT). REMOVED RIB. INSTALLED NEW RIB PN A5451521950100 IAW SRM 54-54-11, FIG 1, SECTION "D", ITEM 55, PG 2; PO 688715.1. R & R NEW RIB IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 45,038 hrs · 22,746 cycles

PANEL 147 AF IS DAMAGED AT BOTH EDGES. FABRICATED NEW FLOOR PANEL 147 AF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 45,038 hrs · 22,746 cycles

INSIDE TAIL COMPARTMENT ACCESS DOOR 313 AL CATWALK IS DELAMINATED. FABRICATED NEW FLOOR PANEL 313 AL IAW DWG SRZ 25-005, REV "H".

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

BULK CARGO PIT SIDEWALL PANEL 161 AW IS CORRODED ON THE BOTTOM SKIN. FABRICATED NEW SIDEWALL PANEL 161 AW IAW DWG SRZ 25-005, REV "H".

Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 45,038 hrs · 22,746 cycles

FWD CARGO COMPARTMENT FLOORBOARD 131 HG IS DELAMINATED. FABBED NEW FLOORBOARD 131 HG IAW DWG SRZ 25-005, REV "H".

Part: MANIFOLD — DAMAGED (CASE COOLING) · airframe 45,038 hrs · 22,746 cycles

NR 2 ENGINE INBD TURBINE CASE COOLING MANIFOLD HAD ELONGATED BOLT HOLES. REPAIRED AND INSPECTED NR 2 ENG INBD TURBINE CASE COOLING MANIFOLD IAW MM 72-09-76-30, REPAIR NR 9. MANIFOLD REMOVED; REINSTALLED, AND LEAK CHECKED ON N/R N00322.

Part: MANIFOLD — DAMAGED (NR 2 ENGINE) · airframe 45,038 hrs · 22,746 cycles

NR 2 ENGINE OTBD TURBINE CASE COOLING MANIFOLD HAS HAS HOLES WORN IN THE MAIN DUCT CONNECTION. REMOVED, REPAIRED AND REINSTALLED NR 2 ENG OTBD TURBINE CASE COOLING MANIFOLD IAW AMM 75-24-10-4. LEAK CHECK GOOD IAW AMM 71-00-00-5-03.

Part: DUCT — WORN (BLEED DUCT) · airframe 45,038 hrs · 22,746 cycles

NR 2 ENGINE INBD SIDE HAS FASTENERS LOOSE ON BLEED AIR DUCT. REMOVED, REPAIRED AND REINSTALLED NR 2 ENG INBD BLEED AIR DUCT AND MANIFOLD IAW AMM 75-24-10-4. LEAK CHECKED GOOD IAW AMM 71-00-00-5-03.

Part: MANIFOLD — WORN (LT BLEED SYS) · airframe 45,038 hrs · 22,746 cycles

(1) ENGINE LPT TCC LT BLEED AIR CONNECTOR HAS A LOOSE BOLT. R & R AND REINSTALLED THE NR 1 ENG LT TURBINE CASE COOLING MANIFOLD AND DUCT IAW A310-200 AMM 75-24-09-01. LEAK CHECKED GOOD IAW AMM 71-00-00-5-03.

Part: ATTACH ANGLE — CRACKED (ZONE 400) · airframe 45,038 hrs · 22,746 cycles

NR 2 PYLON; RT SIDE PANEL VERTICAL ATTACH ANGLE FOR ACCESS PANELS 422DR & 424 CR IS CRACKED AT THE UPPER EDGE. REMOVED CRACKED BRACKET AND INSTALLED NEW CRACKED BRACKET PN A5461132150500, PO 688783.1 IAW SRM 51-72-10 PARA 5 AND 6.

Part: ACCESS PANEL — CHAFED (ZONE 100) · airframe 45,038 hrs · 22,746 cycles

A/C ACCESS PANEL 148CZ UPPER LIP END AND CTR IS GOUGED AT FRAME 47 - FRAME 47. BURNISHED UPPER LIP ON GOUGED AREA AND FOUND OUT OF LIMITS IAW SRM 51- 73-10, PARA D. FABRICATED NEW UPPER LIP IAW DWG 15A25513129. MATERIAL ID EXTRUSION PN NSA346044, PO 664242. REMOVED OLD UPPER LIP AND INSTALLED NEW IAW SRM 51-40-21. ALODINED & PRIMED IAW SRM 51-21-10. PAINTED IAW SRM 51-23-10.

Part: SUPPORT ANGLE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

DORSAL FIN RT SIDE FWD SUPPORT ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398197220100 IAW SRM 51-74-10 AND 51-40-21, FIG 9, PARA 7, PG 24.

Part: SUPPORT ANGLE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

DORSAL FIN, RT SIDE SUPPORT SPLICE ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398192920100 IAW SRM 51-74-10, AND 51-40-21, FIG 9, PARA 7, PG 24.

Part: HOUSING — CORRODED (RT WING) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

RT WING AILERON D4 HINGE BEARING HOUSING IS CORRODED.

Part: BRACKET — CRACKED (ZONE 400) · airframe 45,038 hrs · 22,746 cycles

NR 2 PYLON OTBD RIB 8 BRACKET IS CRACKED AND FASTENER ATTACH HOLES ARE OVERSIZED RIB 8 - RIB 8 R & R BRACKET IAW SRM 51-40-20, PARA 6 & 7.

Part: FAIRING — CRACKED (RUDDER) · airframe 45,038 hrs · 22,746 cycles

FWD RUDDER FAIRING IS CRACKED REMOVED FAIRING REF A310-200 SRM 51-40-20. REPAIRED FWD RUDDER FAIRING REF EA 6-5350-136682. REMOVED AND REINSTALLED FWD RUDDER FAIRING IAW SRM 51-40-20. REMOVED AND REPALCED DAMAGED RIB IAW SRM 51-40-20.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 45,038 hrs · 22,746 cycles

NR 2 PYLON, INTERNAL STRUCTURE WEB IS CRACKED FWD LT SIDE OF THE PRECOOLER STRUCTURE BOX. REMOVED & REINSTALLED SUPPORT BRACKET IN REF TO SRM 51-40-21, PARA 5. STOP DRILLED CRACK AND INSTALLED REPAIR BOUBLER IN REF TO SRM 54-50-00, FIG 203.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

AFT CARGO COMPARTMENT, UPPER MAIN CARGO DECK FLOORBEAM AT FRAME 54.3 HAS CORROSION AROUND A FASTENER HOLE, LT SIDE, BL-41L. REPAIRED FLOORBEAM IAW EA 6-5310-136372 "FUSELAGE - CROSSBEAM AT FR 54.3, CORROSION ON LOWER FLANGE".

Part: SUPPORT ANGLE — CORRODED (VERTICAL STAB) · airframe 45,038 hrs · 22,746 cycles

DORSAL FIN RIGHT SIDE; AFT SUPPORT ANGLE IS CORRODED. REMOVED CORROSION WITH MORE THAT 50% MATERIAL LOSS, OUT OF LIMITS IAW A310-200 SRM 51-74-10. REMOVED AFT SUPPORT ANGLE AND DRILLED UP NEW SUPPORT ANGLE; DEBURRED, INSTALLLED, SEALED AND PAINTED IAW A310-200 SRM 51-40-21, FIG 9, PARA 7, PG 24, 51-40-44; 51-75-10 AND 51-76-10.

Part: STRUCTURE — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

NR 1 PYLON SPIGOT FITTING BORE HAS CORROSION. CLEANED NR 1 PYLON SPIGOT FITTING BORE IAW SB A310-54-2019, REV 3. MEASURED HOLE WITH MIC T8723B AND FOUND TO BE LESS THAN 4.728 IAW S/B A310-54-2019, REV 3. CAD PLATED BORE IAW SRM 51-21-10.

Part: TEE FITTING — CRACKED (LT WING) · airframe 45,038 hrs · 22,746 cycles

LT TEE FITTING HOLE "C" SHOWS A CRACK INDICATION WHILE PERFORMING BHEC FOR NDT. CONTACT ENGINEERING. ENGINEER SHALL COORDINATE A REPAIR WITH ACFT MFG THAT IS ACCEPTABLE TO THE FAA OR DGAC. REPAIRED HOLE IAW EA 6-5710-136669, TITLE "WINGS - EO 5710-7-3322-CTR WING LOWER SKIN TEE FITTING AT RIB 1 AND STIFFENER 8 (LT)". REINSTALLED STIFFENER IAW SRM 51-40-21, PARA 7.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

NR 2 PYLON INTERNAL, SPIGOT BEARING IS COVERED WITH A BROWN LAYER AND THE CUTOUT CIRCUMFERENCE IS PACKED WITH RUST DUST. ACCESS 483 AL. CLEANED NR 2 PYLON SPIGOT FITTING BORE IAW SB A310-54-2019, REV 3. MEASURED HOLE WITH MIC T8723B AND FOUND TO BE LESS THAN 4.728 IAW S/B A310-54-2019, REV 3. CAD PLATED BORE IAW SRM 51-21-10. REMOVED AND REPLACED NR 2 PYLON SPIGOT BEARING IAW AMM 54-51-78-4 AND EA 6-5450-136673.

Part: FAN BLADE — CRACKED (NR 2 ENGINE) · airframe 45,038 hrs · 22,746 cycles

NR 2 ENGINE FAN BLADE NR 9 HAS CRACK IN RADIUS OF MID SPAN SHROUD. R & R NR 2 ENGINE NR 9 FAN BLADE AND NR 29 FAN BLADE IAW FDX A310-200 MM 72-21-02-4. BLADES WERE A MATCHED PAIR. NO FUTHER ACTION REQUIRED IAW FDX A310-200 MM 72-21-02-4 PARA. 3.C.

Part: FLOOR PANEL — DAMAGED (E/E BAY) · airframe 45,038 hrs · 22,746 cycles

E&E COMPARTMENT FLOOR PANEL 122 PF HAS EDGE DAMAGE.

Part: FLOOR PANEL — DAMAGED (E/E BAY) · airframe 45,038 hrs · 22,746 cycles

E & E COMPARTMENT FLOOR PANEL 122 LF HAS EDGE DAMAGE.

Part: FLOOR PANEL — DAMAGED (BS 1711-1976) · airframe 45,038 hrs · 22,746 cycles

FWD CARGO PIT FLOOR PANEL 131 RF IS DAMAGED. REPAIRED EDGE DAMAGE TO FWD CARGO PIT FLOOR PANEL 131 RF IAW SRM 53-10- 20, FIG 202; PARA 9-B.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,038 hrs · 22,746 cycles

E&E COMPARTMENT, COCKPIT FLOOR STRUCTURE, FRAME 10, RT SIDE, CLIP ANGLE SUPPORT IS CRACKED; LOCATED JUST ABOVE THE TENSION REGULATOR CONTROL ROD FWD SIDE OF FRAME 10. REMOVED DAMAGED CLIP ANGLE SUPPORT FROM E&E COMPARTMENT FLOOR STRUCTURE IAW SRM 51-40-10. FABRICATED NEW CLIP ANGLE SUPPORT. LOCATED, DRILLED AND INSTALLED IAW DWG 12A53610804, ISSUE "M". ALODINED IAW SRM 51-21- 10. PRIMED AND TOPCOATED IAW SRM 51-23-10.

Part: FLOOR PANEL — DAMAGED (E/E BAY) · airframe 45,038 hrs · 22,746 cycles

E&E COMPARTMENT FLOOR PANEL 122 JF HAS CORNER DAMAGE.

Part: DOUBLER — CRACKED (MLG DOOR) · airframe 45,038 hrs · 22,746 cycles

LEFT MAIN LANDING GEAR INBD DOOR DOUBLER AT THE HINGE LIP EDGE IS CRACKED. REMOVED CRACKED DOUBLER LT MLG IR DOOR AFT. END, FABRICATED AND DRILLED DOUBLER IAW DWG. A52810176. ALODINED, PRIMED AND PAINTED DOUBLER IAW SRM 51-21-10, 51-23-10. INSTALLED DOUBLER IAW SRM 51-40-21 PARA.7 PART MARKED IAW GMM 7-0-1001-1.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 45,038 hrs · 22,746 cycles

MAIN CARGO COMPARTMENT AT FRAME 39; 30 INCHES LT OF C/L; FLOORBOARD IS PUNCTURED AND CRUSHED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,038 hrs · 22,746 cycles

FUSELAGE INTERNAL STRUCTURE ,UNDER THE BULK CARGO FLOOR SUPPORT 48R HAS CORROSION FROM FRAME 66 TO FRAME 67. REMOVED CORROSION. TOTAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-17-14, PARA 1, PG 1. REMOVED AND REPLACED FLOOR SUPPORT SECTION AND SPLICE IAW SRM 51-40-21, PARA 6 & 7. ALODINED AND PRIMED IAW SRM 51-21-10. PAINTED IAW SRM 51-23-10. REMOVED AND REINSTALLED WEB IAW SRM 51-40-21. REMOVED AND REINSTALLED DUCTING IAW AMM 21-28-10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 45,038 hrs · 22,746 cycles

AFT CARGO COMPARTMENT UPPER MCD FLOORBEAM IS CRACKED AT FRAME 54.3; RT SIDE. REPAIRED FLOORBEAM IN REF TO SRM SUPPLEMENT 53-10-15 FIG. 201

Part: FRAME — DENTED (ZONE 200) · airframe 45,038 hrs · 22,746 cycles

FUSELAGE INTERNAL STRUCTURE FRAME IS DENTED AT FRAME 54.2, STRINGER 13L. REPAIRED FRAME AS REQUIRED IAW EA 6-5310-123550.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOOR STRUCTURE SEAT TRACK HAS EXFOLIATION CORROSION FROM FRAME 18 TO FRAME 19, LBL 28. R & R SEAT TRACK IAW SRM 51-40-21 AND SRM 53-10-16, FIG 208, PARA 6.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS PUNCTURED IN SEVERAL AREAS FROM FRAME 19.0 TO FRAME 22.0; LBL 60.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 45,038 hrs · 22,746 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS PUNCTURED AT FRAME 23; 50 INCHES LT OF C/L.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS CRUSHED FROM FRAME 32.0 TO FRAME 34.0; LBL 67.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 45,038 hrs · 22,746 cycles

MAIN CABIN FLOORBOARD 241 PG IS CRACKED AT THE AFT ENDS.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 45,038 hrs · 22,746 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS PUNCTURED/ DENTED AT FRAME 38; 70 INCHES LT OF C/L.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 45,038 hrs · 22,746 cycles

MAIN CARGO COMPARTMENT FLOORBOARD IS PUNCTURED AT FRAME 20; 50 INCHES LT OF C/L.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS PUNCTURED IN SEVERAL AREAS FROM FRAME 23.0 TO FRAME 24.0; LBL 40.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOOR BOARD IS CRUSHED FROM FRAME 24.0 TO FRAME 32.0; LBL 67.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 45,038 hrs · 22,746 cycles

MAIN CABIN FLOOR PANEL NR241 QK EAR IS BROKEN AT FRAME 43L TO FRAME 44L.

Part: FLOORBOARD — CRACKED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD NR 261 IS CRACKED FROM FRAME 74 TO FRAME 77; LBL 60 TO LBL 70.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS PUNCTURED IN SEVERAL AREAS FROM FRAME 22.0 TO FRAME 24.0; LBL 60.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS PUNCTURED IN SEVERAL AREAS FROM FRAME 24.0 TO FRAME 26.0; RBL 20.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD NR 252 WH IS PUNCTURED FROM FRAME 60 TO FRAME 62; RBL 60 TO RBL 80.

Part: FLOORBOARD — DELAMINATED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS DELAMINATED FROM FRAME 19.0 TO FRAME 22.0; LBL 67.

Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS PUNCTURED IN SEVERAL AREAS FROM FRAME 22.0 TO FRAME 24.0; LBL 20.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 45,038 hrs · 22,746 cycles

MAIN CABIN FLOORBOARD, 242 GF, IS CRACKED.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS CRUSHED IN SEVERAL AREAS FROM FRAME 24.0 TO FRAME 25.0; LBL 40.

Part: FLOORBOARD — BROKEN (MAIN DECK) · airframe 45,038 hrs · 22,746 cycles

MAIN DECK FLOORBOARD IS BROKEN FROM FRAME 34.0 TO FRAME 37.0; RBL 67.

Part: ENGINE — SHUTDOWN (ZONE 500) · airframe 44,832 hrs · 22,657 cycles

ON LANDING ROLL, AT APPROX 80 KTS, NR 1 ENG SHUTDOWN. NR 1 UNLOCK LIGHT REMAINED ON, EGT WAS NOTED AT 670 DEG C AS N1 AND N2 DECRESED TO "0". NO OTHER DAMGE WAS NOTED. FUEL LEVER WAS SELECTED OFF. FIRE HANDLE WAS TESTED TO ENSURE NO MISSING FIRE INDICATION AND TAXI RESUMED TO BLOCK-IN. IAW ENGINEER, ENGINE APPROVED FOR REMOVAL. REMOVED AND REPLACED NR 1 ENG IAW WORKCARD 44T0102-1 AND WORK CARD 44T0704-1. OPS CHECKED ALL INDICATION AND PARAMETER NORMAL.

Part: UPLOCK — MALFUNCTIONED (MLG) · airframe 44,109 hrs · 22,319 cycles

WHEN RAISING LANDING GEAR ON TAKEOFF, HEARD LOUD BANG AND INCREASING NOISE. THEN AFTER SEVERAL SECONDS, BETWEEN 1000-1500FT, RECEIVED AMBER ECAM ALERT MLG RETRACTION FAULT. ALL DOOR LIGHTS WERE AMBER. COMPLIED WITH QRH PUT MLG DOWN. NORMAL INDICATIONS UNEVENTFUL LANDING. REMOVED AND REPLACED THE RT MLG UPLOCK ASSY AS PER AMM 32-31-44-4. HAND OVER THE TESTS AND LEAK CHECK TO THE NEXT SHIFT. PERFORMED MLG FREE FALL EXTENSION FUNCTIONAL TEST AS PER AMM32-33-00-5 AND PERFORMED MLG NORMAL EXTENSION AND RETRACTION FUNCTIONAL TEST AS PER AMM 32-31-00-5, NO ABNORMALITY AND HYD LEAKAGE FOUND.

Part: TRANSMITTER — INOPERATIVE (ENG OIL PRESSURE) · airframe 44,102 hrs · 22,314 cycles

AFTER TAKEOFF NR 1 ENG OIL PRESSURE FELL TO 0. ENGINE SHUT DOWN. QTY REMAINED NORMAL. OPENED ENGINE COWL AND NO OIL LEAK NOTED. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER IAW AMM 79-33-11-4. LEAK CHECK CARRIED OUT AND OIL PRESSURE NORMAL. CLOSED FAN AND THRUST REVERSER COWL DOORS IAW AMM 71-13-00. A/C OK FOR SERVICE.

Part: BLEED VALVE — FAILED (NR 1 AC PACK) · airframe 43,072 hrs · 21,816 cycles

NR 1 PACK FAULT, XFEED WOULD NOT OPEN, RESET BREAKERS STILL INOP. THE NR 1 HP BLEED VALVE IS ON MEL 36-11-03. REPLACED THE PNEUMATIC CROSSBLEED VALVE 16HV PER AB MM 36-12-11-4, OPS CK OK, ALL ACCESS PANELS IN WHEEL WELL CLOSED UP. REMOVAL/INSTALLATION, OFF MFG 398504-2 POS ONL SRL 1826 TAG 4300C8 ON MFG 398504-2 SRL 2324 TAG 90755A.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 41,925 hrs · 21,163 cycles

ON CLIMB-OUT THRU 250 CAB PRESS ADVISORY V/S 2500/ MIN SWITCHED TO NR 1 REG NO HELP. NR 1 REG SYSTEM PAGE NORMAL BUT CABIN PRESSURE STILL CLIMBING AT 2500 FT/MIN. INITIATED EMERG DTCS ECAMS INCLUDED: VENT BLOWER LO FLOW, NR 1 CAB REG FAULT AND NR 1 CAB PRESS VALVES FAULT, NO HELP ON RED TABS, QRH, AIR TURN BACK TO VHHH MEL/CDL: 21-31-02-A. REMOVED AND REPLACED NR 1 CABIN PRESS CONTROLLER AND SYS NR 1 AFT PRESS REGULATING VLV PER MM.

Part: CONTROL MODULE — INOPERATIVE (MLG) · airframe 41,898 hrs · 21,152 cycles

UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. HANDLE WOULD NOT RAISE ABOVE NEUTRAL DETENT EITHER SYS 1 OR 2. LANDING GEAR CONTROL HANDLE MODULE REPLACED AS AMM 3, 2-31-11-4. GEAR NORMAL EXTENSION/RETRACTION TEST CARRIED OUT AS PER AMM 32-31-005. FOUND SATISFACTORY. LANDING GEAR ELECTRO VALVE INSPECTION/CHECK CARRIED OUT FOUND SATISFACTORY. WORK CARRIED OUT BY L3885, OFF MFG 224TS05Y.

Part: SEAL — DIRTY (COCKPIT) · airframe 41,810 hrs · 21,112 cycles

REJECTED TAKEOFF AT 115 KTS DUE TO INCREASING COCKPIT NOISE AS IF CAPT'S WINDOW SEAL RUPTURED. INSPECTED CAPT'S SLIDING WINDOW SEAL, FOUND DEBRIS. CLEANED DEBRIS AND RESEATED WINDOW SEAL. PRESSURIZATION CHECK PER MM21-31-00-5. NO LEAK FOUND. A/C OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 40,789 hrs · 20,652 cycles

LOST GREEN HYD SYSTEM, QUANTITY INDICATED EMPTY, PRESS ZERO. FLUID SERVICING ON GOING DUE CONTENTS LOW ON THE TANK GAUGE, A LITTLE OVER 1 GAL. PRESSURIZED GREEN SYSTM - FLEX HOSE RT DOOR ACTUATOR BUSTED. REPLACED FLEX HOSE WITH P/N 171141-8CR 0430. MOCC AND ENGG NOTIFIED. SECURED FITTINGS AND LEAK CHECKED - NEG. FURTHER OPS CHECKED DOORS, OK. COMPLIED EA 6-2023-102878 W/ REF TO AMM SUPP 23 23 11 0 PARA 5.F (2). NR 1 EDP REMOVED AND REPLACED DUE TO PARTICLES IN FILTER.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 40,776 hrs · 20,646 cycles

PDIS 417, 21-30, 0009646, 28JUL06 SIN, AFTER TAKEOFF RECEIVED ECAM ALERT (EXCESS CAB ALT) WENT TO RED TABS AND COULD NOT CONTROL CABIN PRESSURE. ON ECAM NR1 OUTFLOW VALUE OPEN , NR2 OUTFLOW CLOSED FACT, 28JUL06 09:49 SIN R R/I NR1 CABIN PRESSURE CONTROLLER AND PERFORM TEST ON CABIN PRESSURE CONTROLLER AND OK IAW MM21-31-00-5-01. PERFORM VISUAL CHECK ON NR1 OUTFLOW VALVES (FWD AND AFT) IN OPEN AND CLOSED POSITION AND FOUND OK. R/I 28JUL06 09:50 SIN R R/I FROM FACT, OFF MFG 82010B040901, POS LT, SRL 235 ON MFG 82010B040901 SRL 337

Part: TRANSMITTER — MALFUNCTIONED (OIL PRESSURE) · airframe 39,287 hrs · 19,975 cycles

NR 1 ENG HI OIL PRESS, DURING CLIMB POWER, ECAM SELECTED NR 1 OIL PRESS 100 PSI AMBER. NO CAUTION LIGHT ALL OTHER ENG NORMAL. THEN AT FL 280 GOT INTERMITTENT HI PRESS CAUTION LIGHT. THROTTLE RETARDED TO IDLE IN DESCENT THEN OIL PRESS TO 38 PSI, NR 1 AND GOT ENG ADV FOR LOW OIL PRESS. ENG OIL PRESS INDICATOR THEN GREEN 38-48 PSI IN DESCENT. R & R NR 1 ENGINE OIL PRESSURE TRANSMITTER AS PER MM 79-33-11-4-03. RAN NR 1 ENGINE AS PER A310 JRH. ALL INDICATION NORMAL. OPS CHECK "SATIS".

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 39,274 hrs · 19,969 cycles

ON TAKEOFF ROLL AT 40 PERCENT N1 WHEN TOGA BUTTONS DEPRESSED NR 1 ENG ADVANCED, NR 2 ENG DID NOT. REJECT AT LESS THAN 20 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-A. R AND I TCC PER MM 22-36-34-4 AND PERFORMED ADJUSTMENT AND TEST PER MM 22-30-00-5 ALL TEST PASSED.

Part: BLEED VALVE — MALFUNCTIONED (NR 2) · airframe 39,030 hrs · 19,857 cycles

AFTER TAKEOFF FROM LISBON HAD NR 2 BLEED VALVE FAULT. DURING RETURN TO LISBON RESET NR 2 BLEED AND FOUND FOLLOWING CONDITIONS: AT 3000 FT NR 1 BLEED TEMP 175 / NR 2 BLEED TEMP 175. THE OVERHEAT WITHIN 2 MINS AT 210 - 220 WITH SUBSEQUENT BLEED VALVE NR 2 FAULT. ON GROUND WITH HP VALVE SELECTED OFF, EVEN AT INCREASE POWER SETTINGS NO PROBLEM NOTED. FAN AIR VALVE REPLACED IAW AMM 36-11-16-4. NO FAULD FOUND ON ENGINE RUN-UP,PERFORMED IAW AMM 71-00-00-5.

Part: PROXIMITY SWITCH — DIRTY (NLG) · airframe 38,664 hrs · 19,621 cycles

LOWERING GEAR ON APPROACH EDDF NOSE GEAR NO GREEN DOWN INDICATION, DOOR LIGHT ILLUMINATED BOTH SYSTEMS. RECYCLED 3 TIMES, SAME RESULT. EXECUTED GO-AROUND. ON CLIMBOUT NOSE GEAR SHOWED DOWN AND LOCKED, BOTH SYSTEMS. T/S PER WD 32-61-02,32-62-01 AND 32-62-02. CLEANED PROX SW C/P'S. NO FAULTS INDICATED ON PROX BITE UNIT. LUBRICATED NLG PER W/C 05T0001. PERFORMED GEAR SWING PER W/C 47T0011. CYCLED GEAR 3 TIMES EACH SYSTEM, ALL INDICATIONS NORMAL.

Part: FITTING — LOOSE (OIL FILTER HOUSE) · airframe 36,555 hrs · 18,194 cycles

NR 1 ENGINE SHUT DOWN ON DESCENT DUE TO ZERO OIL QUANTITY AND FLUCTUATING OIL PRESSURE. ECAM ADVISORY ENGINE NR 1 OIL QTY LOW ADVISORY CAME ON AT LEVEL OFF ALT OF FL300. THE NR 1 THROTTLE WAS REDUCED TO IDLE FOR REMAINDER OF FLT UNTIL THE OIL PRESSURE FLUCTUATED IN THE DESCENT. ENGINE OIL LOW PRESSURE CHECK LIST AND PROCEDURE WITH SINGLE ENGINE OPERATION WERE ACCOMPLISHED. ATT CPH MTC. PLS PERFORM ENGINE WIND MILLING INSPECTION IAW A310-200 M/M BUS DESK FACT LEAK TRACED TO LOOSE FITTING ON ENGINE OIL FILTER HOUSING AT OIL FILTER PX DIFFERENTIAL SWITCH RESTRICTOR. INSERT FOUND DAMAGED. REPAIR CARRIED IAW MM.

Part: PLACARD — UNLOCKED (LM CABIN DOOR) · airframe 34,847 hrs · 17,161 cycles

01-273 ECAM CAUTION IND LM CABIN UNLOCKED. INSTALLED PLACARD.

Part: BUSHING — CORRODED (NLG) · airframe 34,012 hrs · 16,726 cycles

NOSE LANDING GEAR - AFT REMOVAL OF RT NLG SWIVEL BEARING FOUND BUSHING AT FITTING WITH CORROSION. *S/D* REMOVED AND REPLACED BUSHING PER SRM 51-72-20.

Part: ANNUNCIATOR — INOPERATIVE (COCKPIT) · airframe 33,644 hrs · 16,532 cycles

NO CAPTS FMA ON BEGINNING OF T/O ROLL. EFIS SGU NR 2 INOP.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 33,056 hrs · 16,193 cycles

LT MAIN CABIN DOOR UNSAFE. NO PRESS CHG BUT COULD NOT HEAR NOISE, LIGHT STAYED UNTIL TOUCHDOWN.

Part: INDICATOR — FAILED (COCKPIT)

ENGINE TRIM FAULTED, NR 1 EPR (ANALOG POINTER AND DIGITAL READOUT) INOP.

Part: CSD — FAILED (LT ENGINE)

DURING CRUISE, IDG OIL OUTLET FLASHING ADVISORY CAME ON NR 2 DISCONN START TEMP AROUND 135 DEG CELSIUS. AIR/OIL COOLER INOP. SECURE OPEN RAN ENG AT 85 PERCENT N1 TEMP AT 48C, DEFERRED OIL COOLER VALVE PER MEL 75-1B. *S/D* REMOVED AND REPLACED AIR/OIL HEAT EXCHANGE VALVE, LT CSD FUEL/OIL COOLER, IDG PER MM 24-11-24, 24-11-26, 24-11-11. LEAK CHECK GOOD.

Part: COMP BLADE — DAMAGED (NR 1 ENGINE)

98-0110 - STA-DFW - AFTER ROTATION AND DURING CLIMB, EXPERIENCED A SEVERE VIBRATION FROM NR 1 ENG. WHEN POWER PULLED BACK BELOW 1.2 EPR, VIBRATION WOULD STOP, NO ABNORMAL READING NOTED ON VIBRATION METER. NOTICED NEED FOR RUDDER TRIM DURING CLIMB. REMOVED NR 1 ENG NOSE COWL, FAN BLADES, FRONT CASE PER M/M 71-11-00, 72,23-00, 72-10-00 SEE LOG 01039388 FOR NOSE COWL INSTALLATION. INSTALLED FRONT FAN CASE PER JTPD-7R4 SEC 72-33-00 RUB WEAR CHECKED OK AFTER RUN PW INSPECT XC374 EVM ON ENG RUN 0.4 RAN ENG PER JRH INSTALLED FAN BLADES PER PW SEC 72-31-00.

Part: FUEL PUMP — MALFUNCTION (NR 2 ENGINE)

DURING T/O ROLL WITH T/O POWER SET, NR 2 ENG POWER STARTED FLUCTUATING. EEC OFF DUE NR 2 ENG EPR DEFERRED. REPLACED NR 2 ENG FUEL PUMP, FUEL CONTROL AND ENGINE VANE AND BLEED CONTROLLER. ENGINE RUN-UP CHECK OK.

Part: DUCT — SEPARATED (NR 2 ENGINE)

NR 2 ENG TEMP ADV IN CRUISE WITH NR 2 NAC TEMP = 270 DEGREES C, FOLLOWED BY NR 2 THROTTLE WOULD NOT MOVE, FOLLOWED BY NR 2 BLEED FAULT. SHUT DOWN ENG NR 2 TO LAND, ALL OTHER ENG PARAMETERS PRIOR TO SHUTDOWN NORMAL. NR 2 OIL PRESS WAS NOT OBSERVED PAST SHUTDOWN. *S/D* ON NR 2 ENG FOUND PNEUMATIC SUPPLY DUCT SEPARATED AT CLAMP, HEAT DAMAGE TO GEN CABLES AND SEVERAL OTHER WIRE HARNESSES. ALSO, WIRE PLASTIC SPIRAL MELTED AROUND THROTTLE CABLE. REMOVED NR 2 ENG FOR OTHER MAINT. REMOVED AND REPLACED MAIN ENG HARNESS, REINSTALLED NR 2 ENG, OPS NORMAL.

Part: GCU — MALFUNCTIONED (NR 1)

NR 1 GENERATOR FAULT WITH INTERMITTENT NR 1 IDG FAULT. GENERATOR DID RESET BUT STILL HAD NR 1 IDG FLASHING. *S/D* PERFORMED OPS CHECK OF AIR/COOLER, CHECKS GOOD. REMOVED AND REPLACED NR 1 GCU, OPS CK'D GOOD.