N420FE

Part: SKIN — DEBONDED (TE FLAP) · airframe 40,090 hrs · 15,371 cycles

RT WING, INBD FLAP WITH DEBONDING T/E BETWEEN RIB 14 AND RIB 15. IT WAS REPAIRED IN ACCORDANCE WITH SRM 57-52-12.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

NR 2 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-450 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

NR 2 LT SEAT-TRACK BETWEEN FR 38.2 AND FR40 AT Y450 FOUND CRACKED. IT WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

NR 4 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

NR 3 LT SEAT-TRACK, BETWEEN FR 38.2 AND FR 40 AT Y953, FOUND CRACKED. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-15-15.

Part: FRAME — CRACKED (ZONE 300) · airframe 40,090 hrs · 15,371 cycles

ELEVATOR - ARTIFICIAL FELL UNIT LOWER FRAME FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH AMM27-31-26 AND FEDEX EA 6-2730-113153.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

MDCC - SEAT TRACK AT Y-450 FOUND CORRODED BETWEEN FR 45 AND 54. THE PART WAS REPAIRED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6- 5310-113152.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

N00738 MDCC - SEAT TRACK AT Y-953 BETWEEN FR 45 AND FR 54 FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

N00736 MDCC - SEAT TRACK AT Y0 FOUND CORRODED BETWEEN FR 45 AND FR 54. SEAT TRACK REPLACED IN ACCORDANCE SRM 51-72-10.

Part: ADAPTER — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

MDCC - CLS ADAPTER AT FR 36 BETWEEN Y1456 AND Y1459 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

MDCC - SEAT TRACK WITH CORROSION BETWEEN FR18 AND FR19 AT Y950. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

DUMMY-TRACK Y-953 BETWEEN FR 4 AND FR 54.2 WITH CORROSION AND CRACK AT KIT CARGO ATTACHMENT AREA. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

DUMMY-TRACK AT Y-1456 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.

Part: ADAPTER — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

MDCC - CLS ADAPTER AT FR38 BETWEEN Y-450 AND Y-950 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

N00547 MDCC - SEAT TRACK AT YO FOUND CORRODED BETWEEN FR 58 AND FR 72. SEAT TRACK WAS REPAIRED IN ACCORDANCE SRM 53-10-16 FIG 202.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

DUMMY TRACK Y-450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16.

Part: TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

DUMMY TRACK Y450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. IT WAS REPLACED IAW SRM 53-15-16.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 40,090 hrs · 15,371 cycles

PREVIOUS REPAIR LOCATED ON LT OUTBD FLAP, RIB 2/3 (UPPER SKIN). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-53-12 FIG 207.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

N00577 MDCC - SEAT TRACK FOUND CORRODED AT Y1137 BETWEEN FR74/80. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: ADAPTER — CRACKED (FUSELAGE) · airframe 40,090 hrs · 15,371 cycles

MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y953 AND Y1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: PANEL — CRACKED (ZONE 400) · airframe 40,090 hrs · 15,371 cycles

PYLON NR 2, RIB 8 LT WITH CRACK AT UPPER AREA. IT WAS REPAIRED IN ACCORDANCE WITH SRM 54-51-31 FIG 201.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,090 hrs · 15,371 cycles

AFT CARGO COMPARTMENT, CORROSION FOUND ON FR 59, BETWEEN STR 28 AND 30 RH. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-13-13 FIG 202 AND FEDEX ENGINEERING AUTHORIZATION EA 6-5310-112435.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 40,090 hrs · 15,371 cycles

PREVIOUS REPAIR FOUND LOCATED ON INBD FLAP, RIB 2/4 (UPPER SKIN, TRALING EDGE). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM. NEW REPAIR ACCOMPLISHED IAW FEDEX EA 6-5710-112434.

Part: ADAPTER — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

N00568 MDCC - SEAT TRACK AT Y1447 BETWEEN FR 74 AND FR 78 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

LOWER FUSELAGE, PREVIOUS REPAIR FOUND LOCATED ON FR 74/75 AND STR 41/44 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET 1.

Part: ADAPTER — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

MDCC - CLS ADAPTER ON CABIN FLOOR FR 37 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 40,090 hrs · 15,371 cycles

UPPER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON CENTER LINE, FR 1/2 UPPER CL. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR ACCOMPLISHED IAW FEDEX EA NR 6-5330-112436 AND SRM 53-11-12 FIG 201.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT FR360/61 AND STGR 42/43. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVAL. THE EXISTING REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET1.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT, FR 17/18 AND STGR26/27. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-10-12 FIG 225 SHEET 1.

Part: SKIN — WORN (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

FUSELAGE, MISSING MATERIAL AT AFT CARGO COMPARTMENT DOOR LOWER FORWARD FRAME SKIN SURFACE AT FRAME 59A AND BETWEEN STR 41 AND 43 RT. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-17-12 AND EA 6-5310-112433.

Part: FLOORBEAM — CRACKED (BS 1499) · airframe 40,090 hrs · 15,371 cycles

FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FR21, BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 2.

Part: FLOORBEAM — CRACKED (BS 1817) · airframe 40,090 hrs · 15,371 cycles

FWD CARGO COMPARTMENT, CABIN FLOOR CROSSBEAM CRACKED AT FR 33 BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 4A.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FRAME 36 BETWEEN Y450 AND Y953. IT WAS REPAIRED IAW SRM SUPP 53-10-15 FIG 201 SHEET 2.

Part: SKIN — GOUGED (ZONE 200) · airframe 40,090 hrs · 15,371 cycles

FUSELAGE, RT FUSELAGE SKIN SURFACE WITH MISSING MATERIAL BETWEEN FR 25 AND 26/32 AT STR 29 RT AN APPROVAL FOR THE MISSING MATERIAL WAS OBTAINED. FEDEX EA 6-5330-113154 WAS ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (BS 1711) · airframe 40,090 hrs · 15,371 cycles

FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FRAME 25 BETWEEN Y- 450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 4A.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 40,090 hrs · 15,371 cycles

FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FR 37 BETWEEN Y1456 AND Y1959. IT WAS REPAIRED IAW FEDEX EA 6-5310-112431.

Part: SEQUENCE VALVE — MALFUNCTIONED (RT MLG) · airframe 38,469 hrs · 14,243 cycles

RIGHT LANDING GEAR TAKES 10 SECONDS LONGER THAN THE LEFT GEAR TO RETRACT. ECAM GEAR NOT YET WARNING FOR ABOUT 2 SECONDS. THEN NORMAL OPS WHEN GEAR EXTENDED. CLEANED RESTRICTOR VALVE. REPLACED MAINGEAR ACTUATIN G ASSEMBLY RH IAW AMM 32-31-46. REPLACED LANDING GEAR SEQUENCE VALVE RT IAW AMM 32-31-37. REPLACED RETURN FILTER GREEN HYD SISTEM IAW AMM 29-11-15. PERFORMED TEST IAW 32-31-00 OK.

Part: FIRE LOOP — DAMAGED (NR 2 ENGINE) · airframe 38,138 hrs · 13,973 cycles

AFTER T/O AT 15000FT, RECEIVED FIRE WARNING ON ENGINE NR 2. DID PROCEDURES AND RETURNED TO LLBG. TLV U-INSPECTION & T/S PERFORMED ON MTSI 26-10/9536. FIXED DIFFERED LOOP-B, FOUND TWO PLUGS ON LOOP-A SENSING ELEMENTS IN BAD CONDITION (ONE WITH RUBBER ISOLATION CRACKED & ONE WITH CERAMIC INSULATION BROKEN, SIGN OF CORROSION AND ONE PIN PUSHED IN AND THE OTHER NOT LOCKED PROPERLY). DAMAGED PLUGS WERE REPLACED. FOUND ALSO PLUGS ON PYLONE LOOPS CROSSED, FOR MORE DETAILS SEE WRI:26-10/9536

Part: LINE — LEAKING (HYD SYSTEM) · airframe 37,751 hrs · 13,700 cycles

AFTER GEAR EXTENSION GOT GREEN HYDRO SYS LOW AIR PRESSURE LIGHT. DECLARED AN EMERGENCY AND LANDED STRAIGHT AHEAD. AFTER LANDING LOW AIR LIGHT WENT OUT. TURNED BOTH GREEN PUMPS BACK ON IAW QRH. GREEN SYSTEM RECOVERED AND CLEARED THE RUNWAY. GREEN HYD SYSTEM PRESSURE ON NR 5 SPOILER WORK NORMAL NO FAULT INDICATED. T/S ON TANK AIR PRESSURE SYSTEM IN PROGRESS. LEAK CHECK ON GREEN TANK AIR PRESSURE SYSTEM, FOUND SMALL AIR LEAK ON LINE FROM TANK TO DEPRESSURIZATION AND OVERFLOW VALVE. POSSIBLE TO TIGHT NUT. TANK PRESSURE FILLED FROM GROUND CONNECT CHECKED AFTER SEVERAL HOURS, NO CHANGE. A/C OK TO CONTINUE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,675 hrs · 13,644 cycles

ACCOMPLISH MAINTENANCE C-CHECK, DURING AGING AIRCRAFT INSPECTION AN EXISTING REPAIR DOUBLER WAS FOUND ON THE LOWER FWD CARGO DOOR. DOUBLER WAS REMOVED DURING C4 CHECK AT LIS SCRATCH MARK BLENDED. HFEC INSPECTION OF THE AREA. NEW FASTENERS PAINTED.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 37,670 hrs · 13,641 cycles

NR 2 ENG REV GREEN LIGHT WITH ECAM WARNING AFTER T/O. NO BUFFETING. AIR TURNBACK TO LIM. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C. ENGINE 2, THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. T/R VISUALLY INSPECTED, NO DAMAGE FOUND, NO MANUAL STOW ACTION REQUIRED. SUSPECT INDICATION PROBLEM. MOCC NOTIFIED, CONFERENCE CALL DONE IAW GMM. A/C OK TO CONTINUE.

Part: FITTING — CORRODED (ZONE 300) · airframe 37,076 hrs · 13,226 cycles

A/C 420 WAS IN FOR B-CHECK, FOUND VERT STAB FITTING HAD CORROSION. REMOVED AND REPLACED VERT STAB FITTING.

Part: INDICATOR — INOPERATIVE (NR 1 EGT ECAM) · airframe 36,053 hrs · 12,560 cycles

ON ROTATION ECAM WARNING ACTIVATED AND NR 1 ENGINE EGT SPIKES TO OVER 900 DEG AND NR 1 ENG N2 SPIKES TO NEAR 119 PERCENT. RETURN FOR LANDING WITH NR 1 ENG AT IDLE. REMOVED AND REPLACED NR 1 EGT INDICATOR AND NR 1 N2 INDICATOR PER A310 MM 77-21-21-4 AND MM 77-12-21-4, AND PERF ENGINE IDLE AND HIGH POWER RUN PER A310 JRH, ALL PARAMETERS NORMAL. PROBLEM ON NR 1 EGT AND NR 1N2 INDICATION DUPLICATED ON GROUND. DURING MX ENG RUN PRIOR BOTH INDICATOR CHANGE.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 35,449 hrs · 12,259 cycles

RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, FAULTED PASSING 170KIAS. REPLACED NR 2 ADC PER A310 MM34-11-34. OPERATIONAL CHECK AND PITOT/STATIC LEAK TEST GOOD. R&R RUDDER VARIABLE STOP ACTUATOR AS PER A-310, MM 27-23-23-4. R&R NR 1 FEEL LIMITATION COMPUTER IAW A310 MM 27-23-26. ACCOMPLISHED TESTS PER A310 MM 27-23-00-5. NO FAULT ON BOTH SYSTEM OF PITCH FEEL AND RUDDER TRAVEL.

Part: RELAY — FAILED (RUDDER TRAVEL) · airframe 35,436 hrs · 12,253 cycles

RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, WOULD NOT RESET. RUDDER TRAVEL SYSTEM ONE ALREADY DEFERRED. CHECKED FAULT AT FLC NR 2 RUDDER TRAVEL POWER LOOP. PERFORMED T/S PER TSM 27-23-03 REPLACED 309 CY2 RELAY, BITE TEST FLC NR 2 PER MM 27-23-00. OK, NO FAULT NOTED.

Part: TORQUE BOX — CORRODED (FUSELAGE) · airframe 35,154 hrs · 12,120 cycles

CORROSION AROUND FASTENER HEADS IN AVIONICS COMPT NOSE GEAR WHEEL WELL TOP TORQUE BOX (FROM FRAME 13 TO 15A).

Part: ACTUATOR — DAMAGED (HORIZ STAB) · airframe 35,154 hrs · 12,120 cycles

THS ACTUATOR LWR CLAW STOP RUBBER BUFFER BETWEEN INNER & OUTER RACE SHOWS AXIAL MIGRATION OF 5 MM. THS ACTUATOR SCREW THREAD HAS SCRATCH MARK ON UPPER FACE 27.5 CM ABOVE LWR CLAW STOP. REMOVED AND REPLACED ACTUATOR PER AMM 27-44-11-4.

Part: CONTROL CABLE — CORRODED (ELEVATOR) · airframe 35,154 hrs · 12,120 cycles

CAPT SIDE & COPILOT SIDE ELEVATOR CONTROL CABLES CORRODED AT PULLEYS IN STAB COMPARTMENT. REMOVED AND REPLACED CABLES PER AMM 27-30-00-4.

Part: PIN — ROTATED (VERTICAL STAB) · airframe 35,154 hrs · 12,120 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACHMENT TAPERED PIN & SLEEVE ASSEMBLIES RED INDICATOR MARKS SHOW PIN ROTATION AT ALL SIX LOCATIONS. REMOVED AND REPLACED PINS PER AMM 55-30-11 & EA 6-5530-64304.

Part: GEARBOX — LACK OF LUBE (T/E FLAP) · airframe 35,154 hrs · 12,120 cycles

LEFT WING FLAP SYS RT ANGLE GEARBOX FOUND NO OIL IN GEARBOX. R & R LT WING FLAP SYS RT ANGLE GEARBOX PER MM 27-54-13. REF N00509 FOR FLAP SYS ADJ.

Part: FITTING — CHAFED (LT PYLON) · airframe 35,154 hrs · 12,120 cycles

LT WING PYLON THRUST & SIDE LOAD FITTING OUTBD TOP CORNER OF FITTING FOUND CHAFING.

Part: FITTING — CORRODED (RT PYLON) · airframe 35,154 hrs · 12,120 cycles

RIGHT PYLON THRUST AND SIDE LOAD FITTING FOUND BROWN STAIN ON TOP AND BOTTOM AREA.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 34,593 hrs · 11,858 cycles

ON CLIMBOUT NR 2 BLEED FAULTED. REMOVED AND REPLACED PSC 2.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 33,557 hrs · 11,349 cycles

NR 1 ENG BEGAN COMPRESSOR STALLING. ACCOMPANIED BY LARGE FLUCTUATION IN ALL NR 1 ENG INSTRUMENTS.

Part: DOOR — NOT CLOSED (MAIN PAX) · airframe 33,150 hrs · 11,133 cycles

DURING CLIMBOUT, THE ECAM WARNING ON CABIN DOOR NOT CLOSED.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR)

00-82 52-10-4771, ON CLIMB-OUT, LEFT ECAM ALERT DOOR LR UNSAFE. REMOVED AND REPLACED SERRATED ASSY AND OPS CK NORMAL IAW A310 AMM 52 -10-20-5.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER)

AFT SETTING T/O PWR REVERSER UNLOCKED NR 1 LIGHT CAME ON. ABORTED TAKEOFF. THIS IS A REPEAT.

Part: LINK — DAMAGED (THRUST REVERSER)

NR 1 ENGINE THRUST REVERSER COWLINGS BLOCKER DOOR LINKS FOUND BOWED AFT LATCHING. ADJUSTED PER MM 78-32-14 AND T/R OPER CK SAT PER MM 78-32-11.

Part: STRUT — BROKEN (NLG)

BROKEN NOSE LANDING GEAR GROUND LOCK PIN. REMOVED AND REPLACED TELESCOPIC STRUT, TEST SAISFACTORY. GROUND LOCK WAS INSERTED AND REMOVED EASILY WITH A/C ON GROUND.

Part: RT UNIT — FAILED (NR 1 RADAR)

SMOKE SMELL BY FLT CREW, AVIONICS SMOKE LT ILLUM. REMOVED AND REPLACED BOTH A/C PACKS WATER SEP BAGS, NO HELP. CHECKED COCKPIT, ALL PANELS OK. REMOVED AND REPLACED NR 1 WX RADAR TRANCEIVER PER MM 34-41-33-4. TEST SAT PER MM 34-41-00-5.

Part: RETRACT MECH — MALFUNCTIONED (NR 1 SPOILER)

NR 1 SPOILER DEPLOY DURING TAKEOFF ROLL, SPEED 90 KTS. TAKEOFF REJECTED. FOUND NORM OPS TEST OF GROUND SPOILERS AND SPEED BRAKES, CARRIED OUT IAW MM 27-61-00 PG 511, PARA 2 FOUND NORMAL.

Part: INDICATOR — INOPERATIVE (NR 1 ENGINE)

98-201 - DURING CLIMB-OUT PASS 17000 MSL, NR 1 EGT PEG OUT HIGH FOR 5-10 SEC. ALL OTHER PARAMETERS NORM AND WITHIN RANGE. REDUCE PWR AND EGT CONT PLUS/MINUS 10 DEG OF NEEDLE TRAVEL. EGT INOP RETURN TO SIN. VISUAL CK EXHAUST DUCT. REAR OF FRONT COMPRESS DRIVE TURBINE FOR BURN DISTORT METAL PART. REMOVED AND REPLACED EGT IND C/OUT ENG RUN PER JRH. ALL PARAMETER NML.

Part: THERMOCOUPLE — FAILED (NR 1 ENGINE)

98-195 - ON CLIMB-OUT THROUGH 140 NR 1 EGT FLUCTUATED PLUS/MINUS 20 DEG AT LEVEL OFF EGT CLIMB TO 1025 DEG MAX. CKLIST RAN NOTED ENG SHUTDOWN PROC EGT, THEN STAB BELOW MAX, THEN WENT TO ZERO RETURN TO BASE. WITH NR 1 ENG SHUTDOWN EGT IND NORM. PERFORM RESISTANCE AND MV TEST WHILE SHAKING EGT HARNESS, NO PROBLEM NOTED AND INSPECTED EGT HARNESS AND PROBES. VISUALLY CKS NORM. FOUND SEV LOOSE TERM AND NR 4 PROBE HAD 1/2 BROKEN STUD AND 2 LOOSE TERM. REMOVED AND REPLACED NR 1 ENG THERMOCOUPLE NR 4 PER M/M 77-21-04. RUN UP NR 1 ENG PER A310 JRH, ALL IND NORM.

Part: WARNING SYST — MALFUNCTIONED (CARGO DOOR)

BULK DOOR NOT CLOSED ECAM WARNING DURING TAKEOFF ROLL AT KNOTS. TAKEOFF ROLL DISCONTINUED AND RETURNED TO BLOCKS FOR DOOR INSPECTION. CLEANED AND RESECURED 36WS SWITCH AND INSPECTED ALL DOOR OPERATING MECHANISM FOUND NORMAL. CYCLED DOOR SEVERAL TIMES INDICATION ON ECAM NORMAL.

Part: FAN CASE — WORN (NR 1 ENGINE)

AFTER T/O, A/F VIB DEVELOPED AT 250 KTS/5000 FT STRAIGHT AND LEVEL. SLOWED TO 220 KTS VIB STOPPED, CLIMBED TO 23,000 FT A/S 250 VIB AGAIN AND SLOWING THROUGH 235 KTS VIB STOPPED. NO VIB BELOW 235 KTS, NO VIB THROUGH YOKE OR RUDDER PEDALS. ECAM STS NOT CAT 3/INCRS LDG DIST BY 1.1. FOUND FRONT NR 1 FAN CASE ASSY WORN, REMOVED AND REPLACED PER MM 72-23-01. RAN NR 1 ENG AND NO VIB, OK FOR SERVICE AND LEAK CHECK GOOD. REMOVED AND REPLACED FLEX LINE FOR HYD, PRESS CHECK GOOD. PERFORMED A/FLT SYS AND A/SELF TEST, NO FAULTS.

Part: TIRE TREAD — FAILED (NR 2 MLG)

NR 2 MLG TIRE MISSING A LITTLE TREAD AND FLAT. RUBBER WENT INTO THE NR 1 ENG INLET. NR 1 ENG HAS 8 FAN BLADES BENT NEAR L/E TIRE AREA. NR 1 ENG INLET HAS HOLE IN SOUND ABSORBING MATERIAL APPROX 1.5 BY 1.5 BY 2.5 INCH DEEP AT 11:30 POS 3 INCHES FWD OF FAN. NR 1 ENG LINER SEG DAMAGED BET 11 AND 12 O'CLOCK POS BETWEEN FAN AND EXIT VANES. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL ASSYS. C/W FOD BORESCOPE INSP OF NR 1 ENG HP COMP STAGES 4, 5, 14 AND 15, NO DISC. BLENDED FAN BLADES PER PRATT AND WHITNEY MM 72-21-02 PG 601 TO 617. REMOVED AND REPLACED NOSE COWL PER MM 71-11-00 AND ALL SOUND ABSORBING LINERS PER MM 72-23-05. C/W INSP AFTER TIRE BURST PER MM 05-51-15.