Airbus A310

Service difficulty reports · 606

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A310'
  ORDER BY difficulty_date DESC"

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SDR 04FDEA02364Sensor · failed429 77-15 0006235 30JUL04 IAH CLOSE R THREE TIMES DURING CLIMB NR2 ENG, SURGED A/C YAWED TO LT N1 CLIMB LIMIT EXCEEDED (ECAM) CL N' 100 PERCENT SURGE TO 115 PERCENT A/THR TRIPPED OFF LEVEL AT FL 290 CRUISE. ENG. N1 SURGE CR N1 91 PERCENT SURGED TO 1Jul 30, 2004 · N429FE · Airbus A310 · Engine RPM Indicating SystemSDR 04FDEA00783Iru · failedAFTER T/O 1 IRU FAILED, 2 IRU WAS ALREADY MEL'D INOP. RETURN TO DFW. REMOVED AND REPLACED THE 1 IRU PER MM 34-25-00 -05-1, PERFORMED IRS SYS ADJ/TEST IN CONJUNCTION WITH WRI 34-43-6941 (IRU 3) AND WRI 34-43-6937 (IRU 2). ALL IRU'S TESTED NORMAL. PERFORMEMar 31, 2004 · N410FE · Airbus A310 · Doppler SystemSDR 04FDEA00673Connector · damagedON CLIMBOUT (APPROX 10,000 FT) ECAM WARNING OF FWD CARGO DOOR NOT CLOSED, RT ECAM DOOR PAGE ALL GREEN, PRESSURIZATION NORMAL. MEL 17MAR04 02:33 RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 27MAR04. MEL 52-71-01: (IDENTIFY) LWR FWD CARMar 17, 2004 · N454FE · Airbus A310 · Door Warning SystemSDR 04FDEA00674Coalescer Bag · dirtyON CLIMBOUT PASSING 17,000 FT RECEIVED AVIONICS SMOKE WARNING ALERT, JUST PRIOR SMELLED A MUSKY BURNING ODOR. THE ODOR SEEMED TO INCREASE AND DECREASE IN INTENSITY. THEN RECEIVED AVIONICS SMOKE ALERT. DECLARED EMERGENCY, RETURNED TO MEM. UNABLE TO COMPLY. Mar 16, 2004 · N409FE · Airbus A310 · Humidity Control SystemSDR 04FDEA00627Spar · corrodedRT HORIZONTAL STAB I/B END AT RIB 3 TO RIB 4 UPPER T/E EDGE OF SPAR FOR LENGTH OF 16 INCHES HAS SEVERE CORROSION WITH EXFOLIATION. RIGHT HORIZ STAB UPPER REAR SPAR CHORD FOR RIB 3 TO RIB 4 REMOVED CORROSION BY CUTTING OUT TEE CHORD AND INSTALLING NEW TEE CHORMar 11, 2004 · N450FE · Airbus A310 · Horizontal Stabilizer, Spar/RibSDR 04FDEA00603Thrust Reverser · inoperativeNR 1 ENG REVERSER OPERATING LIGHT CAME ON (AMBER) AS TAKEOFF POWER WAS APPLIED AT ATL. THE LIGHT WENT OUT AFTER THE THROTTLE WAS BROUGHT BACK TO IDLE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 16MAR04 MEL 78-30-01-C: ENGINE (IDENMar 6, 2004 · N447FE · Airbus A310 · Engine Thrust ReverserSDR 04FDEA00565Coalescer Bag · odorWHEN T/O POWER WAS APPLIED BOTH PILOTS NOTICED A VERY STRONG OIL BURNING ODOR. REJECTED T/O AT 90 KTS, COMPLETED QRH CHECK LIST AND TAXIED TO GATE. WHEN TAXIING IN POWER ODOR RETURNED. REMOVED AND REPLACED BOTH LT AND RT A/C PACK WATER SEPARATOR COALESCER BMar 4, 2004 · N411FE · Airbus A310 · Humidity Control SystemSDR 04FDEA00390Thrust Reverser · out of rigON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT ECAM SCREEN. ABORTED T/O COMPLIED WITH QRH, RETURNED TO GATE. MAINTENANCE PROCEDURE PERFORMED IAW MEL 78-30-01-C. MANUALLY CLOSED PRSV ANDFeb 10, 2004 · N418FE · Airbus A310 · Engine Thrust ReverserSDR 04FDEA00389Coalescer Bag · dirtyON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMOFeb 10, 2004 · N412FE · Airbus A310 · Humidity Control SystemSDR 04FDEA00244Proximity Sensor · malfunctionedON TAKEOFF FROM IAD GEAR WOULD NOT RETRACT, BOTH SYSTEMS TRIED. FOLLOWED ECAMS. RETURNED TO IAD. REMOVED AND REPLACED PROX BOX PER MM 32-31-71, OP'S GOOD. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-371-01A. SERVICED LT LANDING GEAR BOGIE BEAM DAMPER PER MMJan 29, 2004 · N428FE · Airbus A310 · Landing Gear Position and WarningSDR 04FDEA00231Damper · malfunctionedAFTER T/O LANDING GEAR WOULD NOT RETRACT- TRIED BOTH SYSTEMS, FOLLOWED ECAM (270 SPEED WAS NOT EXCEEDED), FOLLOWED QRM, RETURNED. REMOVED LT GEAR PITCH DAMPER PER MM 32-11-15-4-01. INSTALLED NEW DAMPER THROUGH STEP 4 (B) (4).Jan 27, 2004 · N428FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 03FDEA02299Engine · inoperativeHEARD LOUD BANG, NOSE MOVED TO RT SHARPLY. FOLLOWED REJECTED TAKEOFF PROCEDURE. ALL ENGINE INSTRUMENTS NORMAL AT 105 KTS. IAW TROUBLESHOOTING MANUAL AND POWERPLANT ENGINEERING CONCURRENCE, ENGINE WILL BE CHANGED. SHIPPING INFO TENATIVE FOR REPLACEMENT ENGIDec 29, 2003 · N801FD · Airbus A310 · Engine (Turbine/Turboprop)SDR 03FDEA02240Control Lever · faultyDURING TAKEOFF ROLL, GOT TAKEOFF CONFIGURATION WARNING WITH ECAM PARKING BRAKE ON WARNING. REJECTED TAKEOFF PRIOR TO TAKEOFF. TAKEOFF CONFIG CHECK SHOWED NORM FOR T/O. NOTE ACARS FLIGHT LOG PAGE NEVER SHOWED BLOCK OUT. REMOVED AND REPLACED 7GG PARKING BRADec 23, 2003 · N405FE · Airbus A310 · Landing Gear Brake SystemSDR 03FDEA02236Computer · faultyLEFT INNER TANK QUANTITY WENT TO ZERO READING IN LESS THAN A MINUTE. AFTER THE FQI CHAN SUPPLY 1 AND 2 C/B'S WERE RESET IAW QRH FUEL LEAK PROCEDURE ECAM SHOWED XX'S IN LT INNER AND TOTAL. FUEL QUANTITY READING RETURNED PASSING 12,700 FT. ON THE DESCENT. REDec 23, 2003 · N415FE · Airbus A310 · Fuel Indicating SystemSDR 03FDEA02235Iru · malfunctionedON TAKEOFF ROLL CAPT'S PFD, NAV DISPLAY, NR 1 YAW DAMPER, NR 1 IRU FAILED. REMOVED, REPLACED AND THEN OPS CHECKED NR 3 IRU AS PER A-310 M/M 34-25-00-5 AND 34-25-14 OKAY FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 461600-0800-0801, POSDec 23, 2003 · N450FE · Airbus A310 · Inertial Guidance SystemSDR 03FDEA02234Iru · malfunctionedNR 1 ATT ON PFD FROZEN, NR 1 FD FAILED, NR 1 A/P & NR 1 YAW DAMPER TRIPPED. SUSPECT NR 1 ADC FAILED. ON SHUTDOWN IRS MONITOR SHOWED NR 1 IRU, FOR DRIFT & GS. REMOVED AND REPLACED NR 1 ADC IAW MM 34-11-34-4. TESTED PER 34-10-00 P BLOCK 501. REMOVED AND REDec 23, 2003 · N451FE · Airbus A310 · Inertial Guidance SystemSDR 03FDEA02233Isolation Valve · malfunctionedON DEPARTURE OUT OF MEM AT 3,000 VERY STRONG ODOR IN COCKPIT / TURNED BACK TO MEM. ON DESCENT TO 3,000 ODOR CAME BACK. AVIONICS FLOW LIGHT CAME ON DURING DEPT. FOLLOWED ECAM SELECTED, OVERBOARD. REMOVED AND REPLACED ISOLATION VALVE PER AIR BUS MM 21-23-12Dec 23, 2003 · N443FE · Airbus A310 · Air Distribution SystemSDR 03FDEA02053Generator · inoperativeREJECTED T/O IN CDG DUE TO NR 1 IDG HIGH OIL TEMP ALERT. DISCONNECTED PER MAINT & DEFERRED PER MEL. GEN NR 1 INOP. APU GEN MUST BE USED TO POWER AFFECTED BUSS THROUGHOUT FLT. VERIFY & RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPEDec 4, 2003 · N801FD · Airbus A310 · AC Generation SystemSDR 03FDEA02044Flap Track · crackedLT WING TE, MIDPOINT BETWEEN NR 1 O/B PYLON AND I/B NR 3 FLAP TRACK EVIDENCE OF CRACK AT RIVET HEAD TO EDGE LWR SKIN. REQUEST NDT TO CONFIRM. REMOVED FASTENER IAW A310 SRM 51-40-21, ROTO TESTED HOLE IAW NTM 51-10-00-01 NO CRACKS FOUND, FABRICATED REPAIR PARDec 4, 2003 · N430FE · Airbus A310 · Trailing Edge FlapsSDR 03FDEA02008Thrust Reverser · malfunctioned1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANGE ABOUT 890, RETARDED THROTTLES AT THAT TIME ECAM WARNING HP VALVE FAULT -OFF, 1 HP VALVE SELECTDec 2, 2003 · N412FE · Airbus A310 · Engine Thrust ReverserSDR 03FDEA01892Limit Switch · faultyON TAKEOFF OUT OF DTW LOWER ACCESS DOOR AMBER LIGHT- FOLLOWED ECAM RETURNED TO LAND DTW NO EMERGENCY DECLARED. AT BLOCK IN FOUND ACCESS DOORS CLOSED AND LOCKED. RELEASED LOCKS ON BOTH DOORS FOUND PRESSURE HOLDING DOORS IN CLOSED POSITION. CREW REPORT NO PRENov 7, 2003 · N401FE · Airbus A310 · Door Warning SystemSDR 03FDEA01900Engine · inoperativeTAKEOFF WAS ABORTED AT 70 KTS DURING TAXI NR 2 ENG HAD TO BE VWD OF NR 1 ENG BY 1 1/2 THROTTLE WIDTHS TO MAKE 40 PERCENT N1. DURING TAKEOFF NR 2 ENG WOULD ONLY MAKE 75 PERCENT PWR WITH THROTTLE ALL THE WAY FWD. NO ENG PARAMETERS WERE CLOSE TO THE LIMITS. PONov 6, 2003 · N455FE · Airbus A310 · Engine (Turbine/Turboprop)SDR 03FDEA01884Damper · lowLANDING GEAR LEVER WOULD NOT RETRACT ON SYS 2 SWITCHED TO SYS 1, STILL WOULD NOT RETRACT. THREE GREEN DOWN WITH 3 RED UNLK. FOUND RIGHT SIDE PITCH DAMPER INDICATION, RESET PIN & RESERVICED PITCH DAMPER WITH NITROGEN TO 1700 PSI. FOUND THE SYSTEM AT 1000 PNov 6, 2003 · N423FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 03FDEA01883Damper · malfunctionedREPEAT WRITE-UP, GEAR WOULD NOT RETRACT. AFTER BLOCK IN, LOOKED AT GEAR TRIM CYLINDERS AGAIN AND THE RIGHT GEAR TRIM CYLINDER WAS POPPED AGAIN. PARTS ORDERED, ADDED MPN D22127000-5 CPN 3212339 QTY 1 DAMPER MSN 862119. REMOVED AND REPLACED RIGHT MLG BOGIE Nov 6, 2003 · N423FE · Airbus A310 · Landing Gear Retraction/Extension SystemSDR 03FDEA02345Filter · cloggedON CLIMBOUT HAD ENG 1 FUEL FILTER CLOG LIGHT ON APPROXIMATELY 100 N1 OUT AT AROUND 90 N1. REPLACED FUEL FILTER PER A310-200 MM 73-12-03 PG 2. LEAK CHECKED NORMAL. RAN ENGINE AT 100 PERCENT N1, NO CLOG LIGHT AT THIS TIME, OK TO CONTINUE.Oct 22, 2003 · N423FE · Airbus A310 · Aircraft Fuel Filter/StrainerSDR 03FDEA01519Window · crackedAFT EDGE OF CAPT'S SIDE VIEW WINDOW GLOWED WHITE HOT IN TWO SPOTS. THERE WAS A NOTICABLE BURNING ODOR AND A SMALL AMOUNT OF SMOKE. TURNED OFF WINDOW HEAT AND BURNING STOPPED. RETURNEDTO MEMPHIS. FOUND CRACK IN WINDOW. REMOVED AND REPLACED LEFT FIXED SIDE WISep 11, 2003 · N447FE · Airbus A310 · Flight Compartment WindowsSDR 03FDEA01392Slide · deployedDOOR L1 OPENED PROPERLY, HOWEVER "EMERGENCY SLIDE" AT LEFT FRONT ENTRANCE DOOR (L1) DID NOT DEPLOY UPON ACTIVATION. MANUAL HANDLE WAS LIKEWISE UNSUCCESSFUL. FACT 06AUG03 16:47 ABQ R REMOVED OLD SLIDE AND INSTALLED SERVICABLE SLIDE ASSY IAW M/M 25-61-21-Aug 26, 2003 · N414FE · Airbus A310 · Escape SlideSDR 03FDEA01353Wire Harness · fireEN ROUTE RIGHT SIDE SLIDING WINDOW HEAT POWER CORD CAUGHT FIRE. SWITCH WAS TURNED OFF AND FIRE WAS EXTINGUISHED. LANDED KLCK, INSP HEAT HARNESS WIRE, FOUND BURNED AREA. REMOVED FROM TERMINAL STRIP AND COMPLIED WITH PART 1 OF EA-6-3040-72501. PER MOCC REQUEAug 21, 2003 · N446FE · Airbus A310 · Ice/Rain Protection System WiringSDR 03FDEA01230Structure · vibrationAIRFRAME VIBRATION STARTED CLIMBING OUT AT FL22.5 2CD A330 KIAS. ENGINE DATA N1-104.1 2C104.23A EGT 832 2C 841 3A VIBES 0.62C+0.2 3A N2 VIBES 2.0 2C0.4. VIBRATION REMAINED THROUGHOUT FLIGHT UNTIL DESCENDING PAST FT.VIBRATION WOULD DECREASE AS POWER WAS REMOAug 9, 2003 · N415FE · Airbus A310 · Fuselage Main, StructureSDR 03FDEA01228Smoke Detector · activatedCRUISE ALTITUDE 2C ENROUTE MEM 2 FLAS 22 CARGO COMPD SMOKE DETECT 22 AFT SMOKE LIGHT ILLUMINATED WITH ECAM DEPICTION. DECLARED EMER 7 DIVERTED TO DISCHARGED AGENT 1 PER CHECKLIST 2C FOLLOWED BY AGENT 2 PER CHECKLIST. A CAPT AND FO REPORTED SMOKE INDICATION Aug 8, 2003 · N414FE · Airbus A310 · Smoke DetectionSDR 03FDEA01203Coalescer Bag · dirtyGTF-RNO SMELLED STRONG ODOR IN THE COCKPIT, WORSE AS FLT PROGRESSED. SMELL NOT NOTICEABLE IN CUR OR LAV AREA. NO SMOKE WARN OR ECAM. FACT 03AUG03 07:39 BOI R INSP MDC & CAB & AVIS COMPT NO SMOKE, DETECTED A SLIGHT JET EXHAUST TYPE ODOR IN MDC AREA. REMAug 3, 2003 · N414FE · Airbus A310 · Humidity Control SystemSDR 03FDEA01202Indicator · false indicationIN CRUISE NR 1 ENGINE LOW OIL PRESS (32) ON ECAM. NO CONFIRMING LOW OIL PRESS LIGHT. ENGINE OPERATED AT IDLE. A/C DIVERTED TO EDDF. NR 1 OIL QUANTITY DROPPED 3 QTS OIL, TEMP WAS 30 DEGREES HIGH. MOMENTARY DC ELEC ADVISORY NR 1 AMPS FLUCTUATING. REMOVED AAug 3, 2003 · N452FE · Airbus A310 · Engine Oil PressureSDR CA030807001B-Nut · cracked(CAN) DURING FLT, THE AIRCRAFT LOST THE B-HYDRAULIC FLUID SYSTEM. DURING INVESTIGATION THE B-NUT WAS FOUND CRACKED ON THE NR 1 ENGINE DRIVEN PUMP CASE DRAIN LINE. THE LINE ASSEMBLY WAS REPLACED, THE HYDRAULIC PUMP WAS REPLACED AS PRECAUTIONARY MEASURE AND THJul 19, 2003 · Airbus A310 · Hydraulic Pump (Electric/Engine), MainSDR 03FDEA00986Circuit Breaker · poppedPDIS 446 24-50 0006790 27JUN03 RDU CLOSE R LOST AC BUS 2 DURING TAKE OFF ROLL AT ABOUT 40 KTS. FACT 27JUN03 11:53 RDU R FOUND 202XP BUS BAR BREAKER POPPED AND NR 2 GE HYD PUMP C/B POPPED , RESET SAME BOTH GREEN PUMPS OPERATE NORMAL, NR 2 AC BUSJun 27, 2003 · N446FE · Airbus A310 · AC Power Distribution SystemSDR 03FDEA00842Indicator · inoperativeON TAKEOFF, N1 ON NR 1 ENG WENT TO 0, TAKEOFF WAS REJECTED AT 95KTS. AFTER REJECT ALL BRAKES WERE HOT AFTER REJECT TO 365DEG, N1 ON #1 MAY HAVE BEEN COMPRESSOR STALL FROM WATER ON RUNWAY. R & R NR 1 N1 INDICATOR PER MM 77-11-21-4. CLEANED AND PROPERLYJun 2, 2003 · N422FE · Airbus A310 · Engine RPM Indicating SystemSDR 03FDEA00843Seat Track · damagedFLOOR DAMAGED ON UPPER DECK AT POSITION 6R.DAMAGE CAUSED BY BALLAST PALLET HITTING LOCK DAMAGING FLOOR. NO RESTRICTION FLOOR DAMAGE ON UPPER DECK..REF E.A 6-5321-71244, OK FOR SCV TEMPORARY REPAIR ACCOMPLISHED PER E.A. 6-5321-71244. 0FACT 02JUN03 18:06 Jun 2, 2003 · N410FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00824Adc · inoperativeAFTER T/O F/O PFD AIRSPEED WAS SLOW TO RESPOND 80 ON CAPT SIDE 50 ON F/O'S SWITCHED TO ADC NR 1 ON F/O SIDE, AT 1000AGL GOT FLAP HIGH SPEED WARNING OVER- SPEED WARNING, SPEED OF A/C WAS 160 KTS IND. FACT 28MAY03 22:03 MEM R REMOVED AND REPLACED NR 2 ADC May 29, 2003 · N413FE · Airbus A310 · Altimeter, Barometric/EncoderSDR 03FDEA00813Line · leakingDURING CRUISE, ECAM SIGNALED GREEN HYD RSVR LO LEVEL. GREEN HYD QUANTITY GAUGE AT RED DOT. FOLLOWED ECAM AND QRH PROCEDURES FOR HYD RSVR LO LEVEL, HYD SYS LO PR, AND L/G EXTENDED USING ALTERNATE GEAR EXTENSION. PERFORMED LEAK CHECK FOUND HYD FLUID LEAKINMay 26, 2003 · N422FE · Airbus A310 · Hydraulic System, MainSDR 03FDEA00725Wire · looseAFTER LEVEL OFF AT CRUISE AT FL350, CABIN RATE ECAM WARNING ILLUMINATED. FOLLOWED ECAM STEPS AND QRH PROCEDURES. WAS UNABLE TO CONTROL CABIN ALTITUDE. WHILE LEVEL AND IN MANUAL PRESSURIZATION, CABIN ALT STABILIZED AT 14,900 FT. WITH ALL OUTFLOW VALVES CLOSMay 10, 2003 · N419FE · Airbus A310 · Air Conditioning System WiringSDR 03FDEA00678Hinge · crackedON GEAR RETRACTION AFTER T/O NOSE GEAR DOOR AMBER LIGHT ON, WITH VIBRATION IN THE AREA BEHIND COCKPIT DOOR. WHEN GEAR EXTENDED FOR LANDING THE NOSE GEAR WAS ON. DID MANUAL GEAR EXTENSION. ALL GEAR GREEN LIGHTS ON. REMOVED AND REPLACED R/H NOSE GEAR DOOR ACMay 4, 2003 · N429FE · Airbus A310 · Landing Gear DoorsSDR 03FDEA00657Vane · gougedRT INBOARD FLAP VANE TOP SURFACE 6 INCHES INBOARD FROM OUTBOARD HOIST POINT IS AN AREA GOUGED AND WORN 2 X 2.5 X .012 INCH (BEEN CHAFING ON NR 2 SPOILER ACTUATOR DRIP PAN). BLENDED OUT DAMAGE IAW SRM 51-73-10. NDT BLENDOUT IAW NTM 51-10-08. FILLED REWORK ARApr 30, 2003 · N423FE · Airbus A310 · Trailing Edge FlapsSDR 03FDEA00653Pylon · damagedNR 1 ENGINE PYLON HAS I/B CENTER SECTION AT CENTER T/R HINGE POINT BOWED INWARD APPROX 17 INCHES HIGH AND 20 INCHES LONG WITH 1 INCH DEPTH. SUBSEQUENT DISASSEMBLY AND INSPECTION REVEALED, I/B SIDE OF SKIN AT RIB 7 HAD DEFORMED GUSSET, PYLON PLANK FROM RIB 1 TApr 29, 2003 · N424FE · Airbus A310 · Nacelle/Pylon, Main FrameSDR 03FDEA00607Wire Harness · damagedON LANDING STBY PROBE HEAT, PILOTS RIGHT ECAM DISPLAY, PITCH TRIM NR 2, YAW DAMP NR 2, & ATS NR 2 ALL FAILED AT ONCE. ALSO IRU'S WENT TO INDEPENDENT OPS. ENG NR 2 N2 CB POPPED. FACT 25APR03 19:09 RNO U C/W E.A. 6-2400-70271 THE R/H ECAM WIRE WAS CAPPApr 23, 2003 · N429FE · Airbus A310 · Instrument System WiringSDR 03FDEA00545Indicator · inoperativeON 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 77Apr 18, 2003 · N420FE · Airbus A310 · Engine EGT/TIT Indicating SystemSDR 03FDEA00437Indicator · inoperativeON TAKEOFF ROLL AS TOGA WAS SELECTED ON AUTO THROTTLE SYSTEM (FOR FLEX POWER) NR 2 N1 ANALOG POINTER HUNG AT 40 PERCENT, ALSO NR 2 ENGINE SLOW TO ACCELERATE WITHIN 3-5 SECONDS. REJECTED TAKEOFF AT 95 KNOTS. FACT 11APR03 06:34 LAX, REMOVED AND REPLACED NR 2Apr 11, 2003 · N403FE · Airbus A310 · Engine RPM Indicating SystemSDR 03FDEA00378Panel · delaminatedNR 1 ENGINE O/B T/R TRANSLATING COWL, LWR AFT LINER DELAMINATED. REMOVED AND REPLACED NR 2 ENGINE T/R TRANS COWL IAW MM 78-32-11-4-B.Apr 3, 2003 · N443FE · Airbus A310 · Engine Thrust ReverserSDR 03FDEA00384Fmc · inoperativeAFTER ROTATION, GOT IRU AND GPS DO NOT AGREE ON ECAM POSITION UPDATE ACCOMPLISHED O/HEAD. ECAM WARNING STILL PRESENT AFTER UPDATE. ECAM WARNING CLEARED AND POSITIONS CAME INTO AGREEMENT O/HEAD SUBIC VOR DURING RETURN TO SFS. AFTER LANDING, IRU NR 1 DISApr 3, 2003 · N456FE · Airbus A310 · Doppler SystemSDR 03FDEA00381Brush Holder · detachedN 517 RT WING ALL SPEED AILERON LWR BRUSH ASSY HAS BECOME DETACHED FROM STRUCTURE. REMOVED AND REPLACED BRUSH ASSY. IAW/SRM 51-40-21 PG.7 UNDER W/O NO. 13350 FEDEX 04/04/2003.Apr 3, 2003 · N443FE · Airbus A310 · Aileron Control SystemSDR 03FDEA00379Fillet · tornNR 2 ENG I/B THRUST REVERSER CORE UPPER AFT FILLET PANEL TORN. R/R FILLET PANEL PER IAW SRM 51-40- 2.Apr 3, 2003 · N443FE · Airbus A310 · Engine Thrust ReverserSDR 03FDEA00380Rib · damagedNR 1 ENG PYLON HYD CASE DRAIN LINE HAS ELONGATED HOLE THRU FRAME AT RIB 20 AND HAS CHAFED THRU ADJACENT ANGLE. R & R STRAP, RIB AND DOUBLER PER IAW SRM 51-40-21Apr 3, 2003 · N443FE · Airbus A310 · Nacelle/Pylon Miscellaneous Structure
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