Allison AE-3007C
Service difficulty reports · 793
Newest first. General aviation reporting is voluntary.
Query with SQL
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 engine_model_key = 'AE3007C' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 engine_model_key = 'AE3007C' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA060906026Windshield · failed(CAN) IN CRUISE AT 41000 FEET A SOUND LIKE A SHOTGUN WAS HEARD AND THE RT WINDSHIELD OUTER PANE SHATTERED. AFTER AN UNSCHEDULED LANDING AND INSPECTION BY AN AME IT WAS DETERMINED TO BE EITHER A LIGHTNING STRIKE OR A SHORT OF THE HEATING ELEMENT. THE WINDOW WSDR DJFA2006300Engine · malfunctionedTRIP ID NR 1057985 DURING TAKEOFF ROLL THE LT ENGINE ITT SPIKED TO 894 DEGREES C. CFR RESPONSE WAS GIVEN AFTER THE TAKEOFF WAS ABORTED. MAINTENANCE PERFORMED A DATA DOWNLOAD OF THE FADEC COMPUTERS AND HAVE DETERMINED THAT THE ENGINE DID NOT EXCEED ITT LIMITSDR DXTA200601435Fadec · failedAMBER (ENGINE O SPEED SHUTDOWN L) ILLUMINATED AFTER TO. AT APPROXIMATELY 400 FT. ALL ENGINE INDICATIONS WERE NORMAL EXCEPT (L) ITT WAS ERRATIC IN TO THROTTLE POSITION. TROUBLESHOT TO BAD LT (B) FADEC, REMOVED AND REPLACED FADEC, OPERATIONAL CHECKS GOOD. PSDR DXT2006F00000Hose · rupturedAC TOOK OFF AND ATTEMPTED TO RETRACT THE LANDING GEAR. THE CREW THEN NOTICED THAT THE NOSE GEAR DID NOT RETRACT AND THE AIRCRAFT LOST HYDRAULIC FLUID FROM THE (A) RESERVOIR. THE FLIGHT CREW THEN DECLARED AN EMERGENCY. AT THIS TIME THEY PNEUMATICALLY (BLEW) SDR DXTA200601388Engine · failedDURING TAXI, RIGHT ENGINE SHUT DOWN, HAD JUST ADVANCED TLA TO CROSS A RUNWAY AND RIGHT ENGINE FAILED. CHECKED THE RIGHT ENGINE FADECS FOR FAULTS, NO FAULTS INDICATED. RAN THE RIGHT ENGINE NUMEROUS TIMES WITH NORMAL STARTS AND ACCELERATION EACH TIME. INSPECTSDR DXTA200601290Warning Light · illuminatedIN CRUISE, LEFT ENGINE ITT QUICKLY ROSE TO 860 AND SHARPLY DROPPED TO APPROX 820-830 SEVERAL TIMES. APPROX 10-15 BOUNCES IN A 10-15 SEC TIME. FL410, RAT -18, .90M. INSPECTED ALL THERMOCOUPLE CONNECTORS PER A23007C MM 77-21-10. APPLIED STABILANT 22 CONTACT ESDR DXTA200601190Connector · unknownLEFT ENGINE ITT FLUCTUATED APPROX 650-800 DEGREES IN TAKEOFF DETENT AT BEGINNING OF TAKEOFF ROLL. TAKEOFF WAS ABORTED. RAN ENGINES AT T/O POWER. BOTH ENGINES OPERATED NORMALLY. NO FLUCTUATION ON BOTH FADEC NOTED. GAINED ACCESS TO LEFT ENGINE FADEC REPOSITSDR DJFA2006186Unknown · unknownWHILE IN CRUISE FLIGHT FOR 15 MINUTES AT FL 430, THE BAGGAGE DOOR SEAL LIGHT ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. CABIN ALTITUDE WAS BEING MAINTAINED FOR APPROX 15 MINUTES, AND THEN THE CABIN ALTITUDE BEGAN TO RISE RAPIDLY. AN EMERGENCY DESCENT SDR SIMA200600904Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND CORRODED AT FRAME 25. BLENDED THE CORRODED AREA TO REMOVE THE DAMAGE. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)SDR DJFA2005184Check Valve · failedCREW REPORTED, DURING CRUISE FLT, RECEIVED BAGGAGE DOOR SEAL, BAGGAGE ALTITUDE MESSAGES FROM CREW ALERTING SYS. AFTER 10 - 15 MIN, CABIN BEGAN TO CLIMB IN ALTITUDE AT APPROX 2,000 TO 2,500 FT/MIN. EMERGENCY WAS DECLARED, AN EMERGENCY DESCENT WAS INITIATED. SDR SIMA200600505Beam · corrodedTHE CENTER BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200600507Floorbeam · corrodedTHE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING CUT OUT. FABRICATED A DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200600506Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED SERVICEABLE CENTER SILL IAW SRM. (K)SDR DXTA200501175Fadec · inoperativeFADEC FAULT CODE CAME ON DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO BLOCK. PERFORMED CHECKLIST AND CLEARED FAULT CODE. AIRCRAFT OPS CHECKED GOOD.SDR DXTA200501071Igniter · inoperativeDURING ENGINE START, LEFT ENGINE HUNG AT 33 PERCENT AND DID NOT START. FUEL HAD BLOWN OUT THE BACK. COMPLETED STEPS 1 THRU 8 OF TASK 72-00-00-810 IAW RR AE3007C FIM. REMOVED & REPLACED CHANNEL B IGNITER IAW RR AE3007C MM 74-21-10-000-802.SDR DXTA200501057Line · undertorquedDURING THE T/R CHECK, WHILE TAXIING THE RIGHT ENGINE FAILED. CHECKED CABLE FOR SHIM, NONE FOUND. CHECKED ALL BLEED CONTROL LINES FOR PROPER TORQUE. REPLACED A+B FADECS IAW RR AE3007C M/M 76-12-00. REPLACED FPMU IAW AE3007C M/M 73-21-00. FOUND TWO FUEL NOZSDR O2G2005F00013Pdu · failedDURING CLIMBOUT OF SDL, WHILE RETRACTING FLAPS THEY FAILED AT 13 PERCENT AND WOULD NOT RESET. REPLACED FLAP PDU AND SOFT START RELAY. (K)SDR 2005FA0001522Hinge Bracket · corrodedDURING RECENT INSPECTION CORRODED HARDWARE WAS FOUND ON AILERON. AFTER AILERON WAS REMOVED HEAVY GALLING WAS FOUND ON OUTBOARD HINGE SUPPORT AND AILERON FITTING. SEVERAL OTHER AIRCRAFT WERE INSPECTED AND 3 OTHERS AND IDENTICAL GALLING. MFG WAS NOTIFIED AND SDR DXTA200501036Link · crackedDURING REMOVAL OF MLG ASSY, EXCESS MOISTURE CAME OUT OF RT OB AXLE WHEN REMOVING HUBCAP ASSY. TRAILING LINK ASSY HAS VISIBLE CRACK APPROX 10 INCHES IN LENGTH, ON TOP SIDE OF TRAILING LINK, CTRD BETWEEN MLG RETRACT ACTUATOR ATTACH LUGS. BORESCOPE INSP FOUND CSDR DXTA200501047Strut · dirtyDURING FLIGHT GEAR RETRACTS HEARD AND FELT BUMP IN THE NIGHT FOUR (4) TIMES DURING FLIGHT. MEASURED EXTENSION OF NOSE STRUT, MEASURED 9.80 INCHES DISASSEMBLED AND CLEANED LOWER BARREL ASSEMBLY. RESEALED AND REASSEMBLED. MEASUREMENT NOW 9.75 INCHES IAW MM. SDR SIMA200529312Control Unit · inoperativeDURING GEAR EXTENTION OBSERVED MOMENTARY EICAS MESSAGE MAIN PITCH TRIM FAIL AND BACKUP PITCH TRIM FAIL. WARNING WENT OUT AFTER GEAR EXTENDED. TROUBLESHOT SYSTEM REPLACED HORIZONTAL STABILIZER UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200529303Floor Support · damagedDAMAGED FASTENER HOLE WAS DISCOVERED ON THE LT OMEGA BEAM FLOOR SUPPORT TOWER AT FRAME 20. PERFORMED A CUT OUT OF THE SUPPORT TOWER TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200529305Floor Support · corrodedA PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER, REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K)SDR SIMA200529302Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS ON THE SILL TO REMOVED THE CORROSION. FABRICATED 3 REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW2120060542) (K)SDR SIMA200529008Floor Support · corrodedA PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K)SDR SIMA200529304Floor Support · corrodedA PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. FABRICATED REPAIR DOUBLER, FILLER AND SHIMS. REPAIR DOEN IAW SRM. (SW21200600542) (K)SDR CNQ2005F00000Line · chafedFLEXIBLE HYDRAULIC HOSE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST IN THE (B-SYSTEM). HOSE WAS CONTACTING LT ELEVATOR POWER CONTROL UNIT. REPLACED HOSE AND VERIFIED ROUTING UNIT. REPLACED HOSE AND VERIFIED ROUTING TO PREVENT CHAFING. MFG IS ISSUINGSDR DXTA200500994Bleed Valve · failedON INITIAL POWER UP FOR TAXI, RIGHT ENGINE MADE A LARGE THUMP AND SHUT ITSELF DOWN. REMOVED UPPER, LOWER BLEED AIR VALVES & ACCELERATION BLEED VALVE. INSTALLED NEW VALVES. OPS CKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CH 75-31-10 & 75-31-15.SDR FDK2005F00000Odor · detected(REF NR F05002) THE CREW REPORTED A SMOKE LIKE SMELL IN GALLEY DURING FLIGHT. MAINTENANCE PERFORMED A GVI TO GALLEY AREA AND WIRING. MAINTENANCE CHANGED TRASH OUT AND CLEANED COFFEE POTS. NO SMOKE SMELL DETECTED. (K)SDR FDK2005F00001Escape Rope · unsecure(REF NR F05004) THE CREW HAD A F/O EMERGENCY ESCAPE ROPE THAT WAS NOT SECURE IN ITS CONTAINER. MAINTENANCE SECURED ESCAPE ROPE. (K)SDR FDK2005F00002Pump · leaking(REF NR F05005)THE CREW NOTED A STRONG ODOR OF FUEL IN THE CABIN (ACTUAL). MAINTENANCE HAS TROUBLESHOT FAULT TO LEAKING PACKINGS AT THE APR ACCELLERATION UNIT. MAINTENANCE REMOVED AND REPLACED APU FUEL PUMP. (K)SDR UG82005F00007Sensor · intermittentHYDRAULIC SYSTEM, A TEMPERATURE FLUCTUATED BETWEEN 80-130 DEGREES C WITH SMALL VARIATION IN PRESSURE. UNLOADED A HYDRAULIC SYSTEM AND TEMPERATURE DECREASED TO 90 DEGREES C BUT CLIMBED TO 119 DEGREES AT SHUTDOWN ON THE RAMP. REPLACED DEFECTIVE TEMPERATURE SENSDR DXTA200500915Pdu · inoperativeFLAPS FAIL IN FLIGHT, SLATS EXTENDED / FLAPS AT ZERO. ATTEMPTED RESET TO NO AVAIL, DIVERTED. TROUBLESHOT FLAPS WITH TEAM X. TO PDU. REMOVED AND REPLACED PDU WITH OVERHAULED PDU ASSY. RIGGED FLAPS, GOOD. OPS CHECK FLAPS GOOD IAW MM.SDR DXTA200500881Wire Harness · inoperativeFUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS. REMOVED AND REPLACED RT ENGINE HARNESS IAW RR 30007 MM 73-13-10. REMOVED PN 23051442 S/N OFF NX0466.SDR DXTA200500875Filter · bypassingFUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS.SDR 2005FA0001097Union · looseHYD UNION WAS FOUND TO BE LOOSE ALLOWING O-RING TO FAIL OVER TIME. O-RING WAS REPLACED AND FITTING TORQUED. (K)SDR 2005FA0001257O-Ring · failedNAS1612-6, O-RING LOCATED ON AN814-6K, PLUG INSTALLED IN (A) HYDRAULIC SYSTEM MANIFOLD, PN 6717277-3 FAILED, CAUSING LOSS OF SYSTEM (A) HYDRAULIC FLUID AND SUBSEQUENT PILOT SHUTDOWN OF (A) HYDRAULIC SYSTEM. FOUND TORQUE ON PLUG TO BE LESS THAN 30 INCH POUNDS SDR RAIA00506033Relay · failedNR 2 BLEED VALVE CLOSED ADVISORY MESSAGE CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE C7 RELAY IN THE RT RELAY SUPPORT. OPS CHECKED GOOD.SDR SIMA200518101Light · failedDISC - EMERGENCY EXIT SIGN LIGHT AT THE COCKPIT DOOR STEP INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT. OPERATIONAL CHECK GOOD. RETURNED TO SERVICE. (K)SDR SIMA200517801Battery · dischargedCREW DISCOVERED ON PREFLIGHT THAT EMERGENCY STRIP LITES IN FLOOR FROM ROW 11 AFT WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY POWER SUPPLY IAW MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR 2005FA0000633Screw · looseSCREW WAS FOUND LOOSE ON BOTH PILOT AND CO-PILOT SEATS ON 2 SEPARATE OCCASIONS, 6 MONTHS APART. THE SCREWS WERE RE-TIGHTENED ON BOTH OCCASIONS THIS PROBLEM IS SIGNIFICANT DUE TO THE FACT THAT THE POSSIBLE FAILURE MODE COULD BE LOSS OF SEAT LOCKING CAPABILITY SDR 2005FA0000495Switch · intermittentLT THRUST REVERSER (TR) PERFORMED UNCOMMANDED STOW DURING THRUST REVERSER USE AFTER LANDING. AFTER ACCESSING THE THROTTLE QUADRANT, IT WAS NOTICED THAT THE WIRES CONNECTED TO THE LT DEPLOY SWITCH WERE STRETCHED VERY TIGHT WHEN THE T/R (PIGGYBACK) LEVERS WERE SDR DXTA200500647Filter · obstructedAMBER FUEL FILTER BYPASS RT CAME ON DURING TAKEOFF JUST AFTER MAXIMUM POWER. ABORTED TAKEOFF. CAS MESSAGE REMAINED ILLUMINATED DURING TAXI TO RAMP. REPLACED RT ENG FUEL FILTER WITH A NEW FILTER KIT. LEAK CHECK SATISFATORY. NO FURTHER DEFECTS NOTED.SDR DXTA200500632Engine · failedRT ENGINE FAIL IN FLIGHT DURING CRUISE AT FL340. RUN CHECKLIST ATTEMPTED RESTART, RESTART FAIL. FADEC FAIL RT A, FADEC FAULT RT A-B CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR DXTA200500611Isolation Valve · openAFTER STARTING THE LEFT ENGINE, ON FIRST START OF THE DAY, A STRONG ODOR OF RAW FUEL COMES INTO THE COCKPIT. PACK ISOLATION VALVE WAS OPEN. AIR COMING FROM WEMAC SMELLED CLEAN.SDR CA050216001Pin · corroded(CAN) WHEN THE MLG TRAILING LINK WAS REMOVED TO DEAL WITH A MINOR CORROSION ISSUE THE LINK PIN ASSY WAS FOUND CORRODED INSIDE AT THE LOCKING NUT END. THE LINK PIN IN QUESTION IS OPEN AT THE IB END WHEN INSTALLED AND IT HAD ACCUMULATED SAND, OTHER DEBRIS AND WSDR CA050216003Pin · corroded(CAN) WHEN MLG TRAILING LINK WAS REMOVED FOR TREATING MINOR CORROSION THE LINK PIN WAS FOUND CORRODED INSIDE AT THE LOCK NUT END. THE LINK PIN IS OPEN AT THE IB END WHEN INSTALLED AND HAD ACCUMULATED SAND AND OTHER DEBRIS AND WATER CAUSING THE CORROSION. THE SDR DXTA200500562Fuel Filter · bypassingON TAKEOFF ROLL, FUEL FILTER BYPASS L CAS MESSAGE DISPLAYED. REMOVED & REPLACED LT ENGINE FUEL FILTER, RESET BYPASS INDICATOR. PERFORMED ENGINE RUN FOR LEAK CHECK AND HIGH POWER FOR ANY CAS MESSAGE. LEAK CHECK GOOD, NO BYPASS MESSAGE. OPERATIONAL CHECK SATSDR UG8AGM0418Switch · stickingTAKEOFF ABORTED, DURING TAKEOFF ROLL DUE TO HP DUCT O PRESSURE CAS (AMBER) MESSAGE ILLUMINATING. CREW COULD NOT DETERMINE WHICH ENGINE PROBLEM OCCURRED ON. THROTTLE WAS PULLED BACK IMMEDIATELY. TRIP WAS PUT ON ANOTHER AIRCRAFT. SB COMPLIED WITH. MAINT GROSDR DXTA200400456Fuel Filter · cloggedFUEL FILTER BYPASS-R CAS MESSAGE CAME ON DURING THE T/O ROLL. INSPECTED PER ROLLS ROYCE MM 73-30-00200-801 AND FOUND THAT FUEL FILTER NEEDED TO BE REPLACED. REMOVED & INSTALLED NEW FUEL FILTER AND O-RINGS WITH KIT P/N 23061826 RESET BYPASS INDICATOR PERFORME
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