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 = 'CF680A' 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 = 'CF680A' 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 IXXA20160429018Shear Tie · crackedDURING MX VISIT ACCOMPLISHED PERMANENT REPAIR FOR THE SHEAR TIE ATTACHED TO THE LT LONGERON LOCATED AT STATION 1746.25 & WL 258.44. WORK WAS ACCOMPLISHED IAW ENGINEERING DOCUMENT 53-767-5445 DATED 04 08 16 REV 3, NR0001, APPROVED REPAIR ON 8110-3.SDR UIEA2016032200215Wire · brokenRIGHT ENG NR 1 IGNITION INOPERATIVE. FOUND BROKEN WIRE AT RELAY K607 PIN A1 IN P11 NR 1 IGN SYS. RE-TERMINATED WIRE W040-714-22 IAW SWPM 20-81-12 & WDM 74-31-21. OPERATIONS CHECKED RT NR 1 IGN IAW AMM 74-00-00. OPERATIONS CHECKED GOOD.SDR 2016F00059Mechanism · miswiredTHE LATERAL TRIM ACTUATOR,(PART OF THE ELEVATOR FEEL MECHANISM ASSEMBLY) RUNS THE OPPOSITE OF THE DIRECTION COMMANDED WHEN OPERATED. SDR WAS FILED PER THE REQUEST OF THE FAA.SDR CA160126011Control Valve · cracked(CAN) DURING PRE-DEPARTURE CHECK A HYDRAULIC LEAK WAS NOTED COMING FROM THE RT MLG ANTI-SKID VALVE MODULE ASSY, CLOSER INVESTIGATION FOUND THE NR 3 ANTI-SKID CONTROL VALVE ON THE MODULE HAD A CRACKED HOUSING. THE NR 3 ANTI-SKID CONTROL VALVE WAS REPLACED IAW SDR CA151104008Bearing · overheated(CAN) INITIAL INDICATION WAS A STATUS MESSAGE, C HYD SYS MAINT. A CHECK OF THE HYDRAULIC PRESSURES REVEALED THE CENTER HYD SYS WAS BELOW NORMAL PRESSURE, 2010 PSI. QUANTITIES ALL OK. WITHIN A FEW MINUTES THERE WAS AN EICAS MESSAGE OF, C1 HYD PRESSURE, FOLLOWSDR UIEA2015072900380Fuel Filter · defectiveAFTER TAKEOFF CAUTION MESSAGE, LEFT ENGINE FUEL FILTER. MESSAGE CHANGED TO STATUS MESSAGE, LEFT ENGINE FUEL FILTER. R & R LEFT ENGINE FUEL FILTER IAW FIM 73-11 FT 804 & 73-11-02. OPERATIONS CHECKED, NO LEAKS NOTED.SDR ABXA20150502068Mec · faultyADVANCED THRUST LEVER APPROX HALF WAY FOR TAKEOFF ON LT ENG & ENG WOULD NOT ACCELERATE. REPLACED LT ENG MAIN ENG CONTROL.SDR UIEA2014112800616Monitor · malfunctionedMAINTENANCE MSG EEC MONITOR. R & R EEC MONITOR IAW AMM 77-35-01.SDR UIEA2014110600563Seal · bentNUMBER 2 ENG INBD SIDE INNER T/R COWL FAN AIR VLV INLET DUCT FLANGE IS BENT. R & R NR 2 ENG INBD SIDE INNER T/R COWL FAN AIR VLV INLET DUCT FLANGE SEAL IAW MM 70-50-00.SDR ABXA20140910291Engine · bird ingestionON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. RESDR ABXA2014022729Intercostal · crackedNR 1 ENG OTBD CORE COWL HAS CRACK INSIDE ON LOWER STIFFENER BETWEEN STATION 291 & STATION 304. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PN 314T1210-259 IAW SRM 51-40-02. SDR INFO PN 314T1210-259, SN NSN, PART NAME INTERCOSTAL, LOCATION NAC STATSDR CA140116001Static Inverter · overheated(CAN) WHILE TOWING ACFT INTO THE HANGAR, A BURNING ODOR WAS DETECTED, THE SOURCE WAS DETERMINED TO BE COMING FROM THE AVIONICS COMPARTMENT. FURTHER INVESTIGATION IDENTIFIED THE STATIC INVERTER AS THE SOURCE OF THE PROBLEM. THE STATIC INVERTER EXHIBITED SIGNSSDR CA140106003Module · failed(CAN) UPON TOUCHDOWN, C SYSTEM HYD QTY AND PRESSURE WAS LOST. MAINTENANCE FOUND THE FILTER BOWL TO BE SEPARATED FROM THE MAIN HYD MODULE ASSY. THE MODULE ASSY WAS REPLACED WITH A SERVICEABLE UNIT AND THE ACFT WAS RETURNED TO SERVICE.SDR UIEA2013121100596Thrust Reverser · malfunctionedRIGHT REVERSER DID NOT DEPLOY ON ROLLOUT KBNA. RAN REVERSERS IAW AMM 78-31-00, BOTH REVERSERS OPERATION CHECKED NORMAL. PERFORMED VISUAL INSPECTION OF BOTH REVERSERS, NO FAULTS NOTED.SDR UIEA2013101200518Blade · damagedDURING WALK AROUND FOUND DAMAGED TO NR 18 FAN BLADE RT ENGINE .6250" FROM BLADE TIP .5 WIDE AND .210 DEEP ON BLADE L/E. ACCOMPLISHED FAN BLADE BLEND OUT REPAIR IAW AMM 72-31-02, ACCOMPLISHED VISUAL INSPECTION OF ENG IAW 05-51-42 AMM.SDR ABXA20131008576Gpu · malfunctionedLEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLESDR CA130920013Check Valve · malfunctioned(CAN) AFTER TAKE-OFF AND DURING THE CLIMB OUT, FLIGHT CREW NOTIFIED MAINTENANCE CONTROL THAT AT 1000 FT THEY HAD AUTO-THROTTLE DISCONNECT AND RT ENGINE OVERHEAT EICAS MESSAGE APPEARED. THE FLIGHT CREW PERFORMED THE RUN CHECKLIST, AND THE RT ENGINE OVERHEAT MESDR ABXA2013081750045Circuit Board · malfunctionedEICAS STATUS MESSAGES LT ENG OH LP2 AND LT ENG OH LP 1. EICAS MESSAGE FIRE/OVHT SYS ILLUMINATED ON DESCENT. CONTINUITY CHECK AND RESTANCE CHECK D2834, D2840, PIN 19, 20 READ1.50K, PIN 18 TO PIN 19, 20. OPEN IAW FIM 26-11 FIG 104.LEAKS TEST C/W. NO LEAK AT SDR AALA20130720004Turbine · damagedNR 1 ENGINE EXHAUST GAS TEMPERATURE WENT TO 941. UPON INSPECTION AT GATE FOUND METAL IN TAILPIPE. ACCOMPLISHED BOROSCOPE OF NR 1 ENGINE LPT & HPT FOUND BLADES DAMAGED & MISSING. REPLACED NR 1 ENGINE ON 7/20/2013. SYSTEM GROUND CHECKED NORMAL.SDR IXXA20130709025J-Box · failedLEFT ENGINE EGT FLUXUATES FROM NORMAL TO 70C ON EICAS AND ALTERNATE SYS. ACFT RETURNED TO STATION. ACCOMPLISHED FIM PROCEDURE 77-21 FAULT TREE 103, BLK 1,2,21. R & R LT ENGINE EGT JUNCTION BOX IAW AMM 77-21-02. OPS CHECKS NORMAL ON ENGINE RUN UP IAW ERH B7SDR CA130530010Line · ruptured(CAN) DURING ENGINE START-UP THE LT HYDRAULIC SYS QTY INDICATION DROPPED TO ZERO. ACFT ENGINES WHERE SHUTDOWN AND UPON INSPECTION MAINTENANCE FOUND A FLEXIBLE LINE RUPTURED AT THE RUDDER RATIO CHANGER. THE FLEXIBLE LINE WAS REPLACED AND LEAK CHECKED. ACFT WASSDR CA130417005Duct · fractured(CAN) LT AIR CONDITIONING PACK SYSTEM PRESSURE WENT TO ZERO PSI ON THE GROUND DURING TAXI. MAINTENANCE FOUND LT ACFT PACK DUCTING RUPTURED. ASSOCIATED ADDITIONAL CLAMPS, ROD ENDS AND HANGARS DAMAGED AT BS 785.90-1065.0. ALL DAMAGED PARTS REPLACED WITH NEW.SDR IXXA20120910024OFuel Cell · leakingDURING TAKEOFF ROLL, WITH AIR CONDITIONING PACKS TURNED OFF, THERE WAS A STRONG JET FUEL ODOR IN FLIGHT DECK. ODOR DISSIPATED WHEN PACKS WERE SWITCHED ON. FOUND CENTER FUEL TANK RIB "O" CENTER MEMBER AND LT MAIN TANK RIB 4 AFT SKIN JOINT LEAKING. ALL WORK PESDR IXXA20120816022OMec · inoperativeFAULT CODE 71-05-XG-01, LT ENGINE WOULD NOT SPOOL TO N1 COMMAND AT 70 PERCENT, AFTER ENGAGING N1, LARGE THROTTLE SPLIT. REJECTED TAKEOFF AT LOW SPEED, LESS THAN 40 KNOTS. NO BRAKING REQUIRED. COMPLIED WITH BORESCOPE INSPECTION IAW AMM 72-00-00/601 AND JOB SDR IXXA20120730018SSkin · damagedON POST FLIGHT WALK AROUND FOUND EVIDENCE OF A TAIL STRIKE. SKIN DAMAGE WAS FOUND TO THE APU DOORS AND AFT FROM BS 1898.4 TO 1923. FRAME DAMAGE WAS FOUND FROM BS 1898.45 TO 1923.5.SDR AALA20120717007Engine · failedJFK - CREW REPORTED RIGHT ENGINE OIL LOSS AND UNCOMMANDED ENGINE SHUTDOWN. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT JFK ON 07/17/2012. SYSTEM GROUND CHECK NORMAL OPERATION.SDR ABXA20120608357Mount · corrodedNR 2 ENGINE AFT MOUNT CORRODED. NR 2 ENGINE REMOVED IAW JC 7010 AFT MOUNT REMOVED, INSTALLED SERVICEABLE AFT MOUNT IAW B767 AMM 71-21-02-4. REINSTALL NR 2 ENG IAW J/C 7010. NR 2 ENG NAC STA 298. AFT MOUNT CORROSION, NO CRACK.SDR AALA20120527007Engine · failedMCO - INFLIGHT JFK-MIA. CREW REPORTED RIGHT "OIL FILTER" EICAS MESSAGE WHICH DID NOT EXTINGUISH WITH POWER REDUCTION. CREW SHUT DOWN RIGHT ENGINE (SINGLE ENGINE TIME 25 MINS). EMERGENCY DECLARED FLIGHT DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVEDSDR CA120402002Blade · damaged(CAN) POST FLIGHT WALK AROUND INSPECTION BY MAINTENANCE PERSONNEL IDENTIFIED MISSING PIECE FROM T3/T4 BLADES, ENGINE NR 2. MAINTENANCE DETERMINED DAMAGE WAS BEYOND LIMITS. ACFT REMOVED FROM SERVICE FOR ENGINE REPLACEMENT. AWAITING ENGINE SHOP TEAR-DOWN TO SDR IXXA110075OGround Wire · damagedDURING CRUISE THE LT ENGINE OIL TEMP STEADILY CLIMB OUT OF LIMITS, OIL TEMP 190, AND OIL PRESSURE 58. THE CREW SHUTDOWN THE LT ENGINE AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT THE OIL TEMP WIRING CIRCUIT AND FOUND PROTECTIVE COATING SDR ABXA20111027122Engine · failedLEFT ENGINE FAILURE DURING CLIMB, LOUD BANG FOLLOWED BY ENGINE SHUTDOWN. N1 EXCEEDANCE OBSERVED. NO ENGINE RESTART ATTEMPTED. REMOVE AND REPLACE ENGINE, AWG.SDR ABXA2011042837Gasket · damagedFUEL LEAK RIGHT ENGINE. FOUND DAMAGED GASKET ON FUEL TUBE AT ENGINE DRIVEN FUEL PUMP. REPLACED GASKET IAW AMM 73-11-06-6 AND PERFORMED ENGINE T/O POWER AND LEAK CHECK IAW AMM 71-00-00-5 TEST 4. FOUND NO LEAKS AT THIS TIME. AIRCRAFT WAS GROUNDED.SDR CA101104006Line · cracked(CAN) ON ARRIVAL, OIL FOUND UNDER NR 1 ENGINE MAINTENANCE INSPECTION FOUND LINE CRACKED TO THE OIL DIFFERENTIAL PRESS SWITCH LINE REPLACED, CHECKED SERVICEABLE.SDR HALA2010091200410Modulating Valve · malfunctionedETOPS SIGNIFICANT SYS - AIR SUPPLY MODULE FAULTS FAN AIR MODULATION VALVE. R & R FAN AIR MODULATING VALVE IAW AMM 36-11-16-004-001-001 AND AMM 36-11-16-404-016-001 AND HAL105 NR 598111. BITE CK OF ASM, OK.SDR CA100702009Insert · looseAPPROXIMATELY 50 MINUTES AFTER DEPARTURE THE CREW HAD DECLARED AN EMERGENCY DUE TO NR 1 ENGINE OIL LOSS, HAD DONE AN IFSD, AND WAS RETURNING TO THE DEPARTURE AIRPORT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING WITH NO ADDITIONAL ISSUES. THE INITIAL INVESTIGATIOSDR AALA20100528TUL15Engine · making metalDTW - INFLIGHT JFK-LAX. CREW REPORTED LEFT ENGINE OIL FILTER CLOG EICAS MESSAGE. CAPTAIN SHUTDOWN LEFT ENGINE (SINGLE ENGINE TIME 30 MINUTES). EMERGENCY DECLARED DIVERTED DTW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ON VISUAL INSPECTION OF SDR ABXA201005200082Structure · cracked#1 ENG I/B THRUST REVERSER #13 CASCADE HAS 3 CRACKS. REMOVED AND REPLACED #13 CASCADE IAW B767 AMM 78-31-16-4SDR ABXR2010072000025Mount · corrodedDURING A MX INSP EVENT, FOUND NR 1 AFT ENGINE MOUNT HAD AREAS OF CORROSION WHERE MOUNT ATTACHED TO THE ENGINE. R & R NR1 ENGINE AFT MOUNT AND MOUNT BOLTS IAW MM.SDR ABXA2010032615Thrust Reverser · crackedRT ENGINE OUTBOARD T/R 2ND CASCADE SECTION FROM BOTTOM CRACKED TOWARD FORWARD SECTION. REMOVED AND REPLACED RT OUTBOARD T/R.SDR ABXR0210072000024Panel · broken(ABXR) DURING A MX INSP EVENT, FOUND PANEL 621ZB , RT L/E HAD (2) DOUBLERS BROKEN AND MISSING. REMOVED (2) DOUBLERS ON PANEL 621ZB IAW DWG 114T2400.SDR IXXA10WSAP036SPanel · damagedDURING ROUTINE C-CHECK INSP FOUND LT FUSELAGE BODY FAIRING PANEL NR 193PL EDGE DAMAGED. APPLIED GLASS CLOTH AND RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.SDR IXXA10WSAP034SPanel · erodedDURING ROUTINE C CHECK INSP FOUND LT HORIZ STABILIZER EXTERIOR UPPER SURFACE AFT STRIP PANEL NR 335UT ERODED. APPLIED RESIN FOR PROTECTION. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.SDR IXXA10WSAP009SFloor Panel · puncturedDURING ROUTINE C-CHECK INSP, FOUND FLOOR PANEL PUNCTURED IN AFT CARGO COMPARTMENT AT STA 1227, RT BOTTOM LINE 12. ACCOMPLISHED REPAIR IAW SRM 53-00-50 REV 101 AND MM 51-21-10 REV 97.SDR IXXA10WSAP010SStructure · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER DRAIN VALVE SURROUNDING STRUCTURE AT STATION 1542. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 53-00-01 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.SDR IXXA10WSAP011SSkin · scratchedDURING ROUTINE C-CHECK INSP FOUND SCRATCH MARKS ON FUSELAGE SKIN BETWEEN STATIONS 1241, 1263 AND STRINGER 25-26. REMOVED SCRATCH MARK’S. FOUND TO BE WITHIN LIMIT’S. PERFORMED NDT INSP. NO CRACK’S OR CORROSION. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRSDR IXXA10WSAP012SPanel · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING T/E PANEL NR 651WB CRACKED. ACCOMPLISHED REPAIR IAW MM 20-11-00 REV 79, AND SRM 51-70-06 REV 101, 51-21-10 REV 97, 51-40-05 REV 101.SDR IXXA10WSAP013SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP OTBD AFT FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND MM 51-20-10 REV 97.SDR IXXA10WSAP014SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD T/E FLAP OTBD FLAP SUPPORT FAIRING FWD FAIRING ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-20-10 REV 97.SDR IXXA10WSAP015SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1070. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA.SDR IXXA10WSAP016SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1076. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA.
Back to GE CF6-80A