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 = 'CT79B' 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 = 'CT79B' 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 29GA2016050400003Pump · malfunctionedHYDRAULIC PUMP STOPS HALFWAY THROUGH GEAR EXTENSION FOR 2 SECONDS AND THEN KICKS BACK ON. INSPECTED AND CYCLED ALL GEAR NUMEROUS TIMES AND NUMEROUS CONFIGURATIONS IAW AMM 32-30-00-05. OPS CHECK NORMAL, COULD NOT DUPLICATE ON GROUND. ACFT OK FOR SERVICE.SDR 29GA2016050400001Brake Sys · malfunctionedBRAKES ARE SOFT, PARKING BRAKE IS VERY HARD TO SET. BLED THE BRAKES IAW AMM 32-42-00-02. OPS CHECK GOOD.SDR 29GA2016050400002Brake · unknownPARKING BRAKE VERY HARD TO SET, BRAKES FEEL MUSHY, PEDALS GO ALL THE WAY TO THE FLOOR. PERFORMED FUNCTIONAL CHECK OF PARKING BRAKE IAW AMM 32-42-00. OPS CHECK SATISFACTORY.SDR 29GA2016043000001Switch · missingEMERGENCY LIGHT SWITCH ON F/A PANEL MISSING. R & R EMERGENCY LIGHT SWITCH COVER ON F/A PANEL IAW AMM 25-25-25. OPS CHECKED NORMAL.SDR 29GA2016042700001Rail · dirtyMCD HAS DIFFICULTY SLIDING CHECK FOR OPERATION. CLEANED INSIDE OF RAIL AND SLIDING UNIT IAW 52-60-05-02 D1.SDR 29GA2016042600001Cover · unsecureEMERGENCY EXIT HANDLE COVER AT ROW 7 IS NOT SECURE. RESECURED ROW 7E-EXIT HANDLE COVER IAW AMM 52-20-10.SDR 29GA2016041300001Engine · shutdownENGINE SHUTDOWN IN FLIGHT. AFTER TAKEOFF, LT ENGINE MAKES A LOUD BANG FOLLOW BY MULTIPLE BANG. ENGINE FAILS AND RE-START AGAIN. WITH NO TORQUE ITT WENT RED LIGHT AFTER ENGINE RE-START ITSELF CAP HAD NO CONTROL OF TORQUE. R & R NR 1 ENGINE IAW TC 71-00-01. SDR 29GA2016041100002Power Supply · inoperativeF/A REPORTS THE FRONT CABIN EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY 21LN. OPS CHECK IS GOOD.SDR 29GA20160404001Brake Sys · weakBRAKES SPONGY. CHECKED HYD QTY, ACCUMULATOR PRESSURE, BRAKES FOR WEAR. BLED BRAKES IAW AMM CHAPTER 32-42-00-02 LOW SPEED MAINTENANCE TAXI GOOD, HIGH SPEED CREW TAXI CHECK GOOD.SDR 29GA2016040400002Safety Wire · brokenTHE SAFETY WIRE IS BROKEN ON THE EMERGENCY EXIT BY 7A. SAFETIED BREAK AWAY WIRE AT EMERGENCY EXIT 7A IAW AMM 52-20-10.SDR 29GA2016032900001Psu · faultyCABIN F/A CALL, EMERGENCY CHIMES GOES OFF IN FLIGHT CONSTATNTLY. R & R PSU PANEL ABOVE SEAT 8A IAW AMM 23-30-35-04-2. OPS CHECKS GOOD.SDR 29GA2016033000001Cover · looseFWD RT EMERGENCY EXIT COVER NOT SECURE. SECURED EMERGENCY EXIT DOOR COVER IAW AMM 20-10-00.SDR 29GA2016032800001Circuit Breaker · trippedCIRCUIT BREAKER, L8, EMERGENCY AND EXTERIOR LIGHTS TRIPPED DURING FLIGHT. RESET THE CIRCUIT BREAKER. PERFORMED EMERGENCY LIGHTING OPS TEST IAW AMM 33-50-00-05-1.SDR 29GA2016032800003Power Supply · faultyEMERGENCY POWER LIGHT ILLUMINATED DURING TAXI. R & R EMERGENCY POWER SUPPLY IAW AMM 24-35-10-04. OPS TEST SATISFACTORY.SDR 29GA2016032800004Brake Sys · weakBRAKES INTERMITTENTLY USE FULL PEDAL TRAVEL WITHOUT BRAKING SUFFICENTLY. BLEEDED ACFT BRAKE SYSTEM IAW AMM 32-42-00-02. NO FAULT NOTED AFTER, OPS CHECK NORMAL.SDR 29GA2016032300001Cover · detachedRIGHT SIDE EMERGENCY EXIT COVER FELL OFF. REINSTALLED COVER IAW AMM 52-20-05-04.SDR 29GA2016032200003Transducer · faultyLOSS OF BRAKING DURING TAXI. ANTI-SKID SWITCH TURNED OFF AND REGAINED BRAKING ON AIRCRAFT. R & R WHEEL SPEED TRANSDUCER IAW MM 32-43-15-01. OPS CHECK OK.SDR 29GA2016032200002Brake Sys · weakDURING TAXI, AFTER LANDING, BRAKES FELT MUSHEY AND LATE TO RESPOND TO PEDAL PRESSURE. BLED THE BRAKE SYS IAW AMM 32-42-00-05, LEAK CHECK AND OPS CHECK NORMAL.SDR 29GA2016032000001Bulb · burned outON F/A LIGHT PANEL EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATE ON ARM WHEN BOTH ENGINES ARE RUNNING. R & R LIGHT BULB TO F\A LIGHT PANEL EMERGENCY LIGHT SWITCH IAW AMM 33-32-10-04, PERFORMED OPS CHECK, OPS CHECK SATISFACTORY,SDR 29GA2016032000003Power Supply · no testEMERGENCY LIGHTING POWER SUPPLY 24LN FAILS TESTING. LIGHT FLASHES IMMEDIATELY UPON STARTING TEST. R & R 24LN EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-10-04-1.
OPS CHECKED GOOD.SDR 29GA2016031200001Panel · unsecureF/A REPORTED HAVING TROUBLE CLOSING THE MAIN DOOR FROM INSIDE. IT CAN ONLY BE CLOSED FROM OUTSIDE. SECURED UPPER PANEL INBD CABIN MAIN DOOR, OPS TEST GOOD IAW AMM 52-10-00-05.SDR 29GA2016031300001Panel · looseF/A REPORTED HAVING TROUBLE CLOSING THE MAIN DOOR FROM INSIDE. IT CAN ONLY BE CLOSED FROM OUTSIDE. SECURED UPPER PANEL INBD CABIN MAIN DOOR, OPS TEST GOOD IAW AMM 52-10-00-05.SDR 29GA2016030700001Power Supply · intermittentEMERGENCY FLOOR LIGHTS ROW 3-6 INTERMITTENT. R & R POWER SUPPLY AT 20LN IAW TASK CARD 35-50-02S. OPS CHECKED GOOD.SDR 29GA2016030600001Handle · looseAFT HANDLE ON AIRSTAIR IS LOOSE. REATTACHED AFT HANDLE ON AIRSTAIR DOOR IAW AMM 20-10-00.SDR 29GA2016022900001Cover · looseEMERGENCY DOOR COVER FELL OFF ON TAKEOFF. REINSTALLED EMERGENCY DOOR COVER IAW AMM 52-20-05SDR 29GA2016022900002Airstair · bindingF/A REPORTS AIR STAIRS DIFFICULT TO FOLD AND STORE. REMOVED DEBRIS FROM ENTRANCE STAIRS TRACK. OPS TEST GOOD IAW AMM 52-60-00-05.SDR 2016FA0000103Warning Message · activatedWHILE MOVING THROTTLES FORWARD FOR TAKEOFF AT ABOUT 30 PERCENT, LT ENGINE ITT RAISED TO 940 DEGREES FOLLOWED BY THE LT CHIP DETECTOR WARNING LIGHT.SDR 29GA2016022300001Seal · unsecureFLIGHT GROUND RUN, F/A REPORTS CABIN DOOR NOT SEALING AND DAYLIGHT VISIBLE THROUGH GAP IN DOOR SEAL. INSPECTED CABIN DOOR AND SEALS, NO DEFECTS NOTED, REF AMM 52-20-20-15.SDR 29GA2016022200001Hinge · lack of lubeF/A REPORT CABIN FORWARD DOOR DIFFICULT UP AND DOWN FUNCTION. INSPECTED AND LUBED HINGE POINTS TO HANDLE AND DOOR FRAME. OPS CHECKED GOOD IAW AMM 52-10-00.SDR 29GA2016022200002Handle · damagedMAIN CABIN DOOR DOES NOT STORE CORRECTLY WHEN PUSHED IN. SUPPORT HANDLE BENT AND STICKS OUT PREVENTING DOOR TO SLIDE IN. INSPECTED AND FOUND FORWARD HAND RAIL UPPER NOT SECURED CORRECT LEFT. RESECURED HAND RAIL UPPER FORWARD AND PERFORMED OPS CHECK OF MAIN SDR 29GA2016021600001Door · stuckLEFT SIDE INBD MLG DOOR WAS FOUND TO BE OPEN DURING FLIGHT. ONCE ON THE GROUND CREW NOTICED A CHUNK OF ICE WAS KEEPING THE DOOR FROM CLOSING. REMOVED ICE FROM L/E OF LT INBD LANDING GEAR DOOR. CHECKED IAW AMM 32-12-10-02. DOOR IS CLOSED AS REQUIRED. NO DESDR 29GA2016021600002Ground Wire · overheatedDURING FIRST START OF NR 1 ENGINE BEFORE FUEL INTRO NR 1 NG WOULD NOT RISE. ABORTED THE START. NR 2 START WAS NORMAL UNTIL AFTER STABILIZING FLAMES WERE SEEN COMING OUT OF NR 1 ENGINE NACELLE. FIRE WAS PULLED AND EXTINGUISHED. STARTER GENERATOR GROUND CABLSDR 29GA20161300001Sign · looseF/A NOTICED FORWARD EMERGENCY EXIT SIGN IN CABIN IS COMING OFF. SECURED EXIT SIGN IAW AMM 20-10-00.SDR 29GA2016021300001Sign · looseF/A NOTICED FORWARD EMERGENCY EXIT SIGN IN CABIN IS COMING OFF. SECURED EXIT SIGN IAW AMM 20-10-00SDR 29GA2016020800001Handle · detachedMAIN CABIN DOOR INNER DOOR HANDLE BROKE. RESECURED MAIN CABIN DOOR INNER HANDLE BY REINSERTING THE RETAINER RING. OPS AND RIG CHECKED GOOD IAW AMM 52-10-00-05.SDR 29GA2016020800002Engine · failedTHE OIL PRESSURE LIGHT CAME ON 50 FT OFF THE GROUND FOLLOWED BY THE CHIP DETECTOR LIGHT. THEN A BUNCH OF LIGHTS CAME ON AND THEN THE ENGINE STARTED PRODUCING A LOUD BANGING NOISE. THE CAPTAIN SAID HE SHUT THE ENGINE DOWN AND DID AN AIR RETURN. R & R NR 2 ESDR 29GA2016012200001Light · inoperativeEMERGENCY LIGHT INOPERATIVE. R & R FORWARD EMERGENCY LIGHT STRIP. OPS CHECKED GOOD IAW AMM 33-50-20-04.SDR 29GA201601260001Warning System · false indicationTOO LOW FLAPS WARNING ALARMED WITH FLAPS AT 20 DEGREES. WENT AROUND AND FLAPS CAUTION LIGHT ILLUMINATED ON RETRACTION. EMERGENCY DECLARED, FLAPS 0 DEGREE LANDING. PERFORMED AN OPS CHECK OF TAWS SYSTEM IAW AMM 34-46-00-05, NO FAULT FOUND PERFORMED AN OPS CHESDR 29GA2016012000001Relay · failedFLIGHT DECK WILL NOT WARM UP ON AUTO TEMP SELECT. UPON DOING IT MANUALLY A SMELL OF BURNED COMES OUT OF ACFT DUCT. AFTER REPLACEMENT OF RELAY 8HD FLIGHT DECK TEMP IS CONTROLLABLE. NO BURNING ODOR NOTED FROM ANY PARTS OF THE ACFT AT THIS TIME.SDR 29GA2016011800001Bulb · burned outRED EMERGENCY LIGHT ON F/A PANEL DOESN'T COME ON WHEN EMERGENCY BUTTON ON PILOT PANEL TURNED ON. R&R RED EMERGENCY LIGHT BULB ON F/A PANEL IAW AMM 20-10-00, OPS CHECKED GOOD.SDR PNSA2015103004Duct · failedLEFT INTAKE LIGHT ON. R & R LOWER INLET DUCT.SDR PNSA2015101201Indicator · failedRIGHT ITT ROLLS DOWN TO ZERO INFLIGHT, BOTH ANALOG AND DIGITAL INTERMITTENT. CLEANED RT ENGINE DECU YELLOW CABLE AND AIRFRAME CONNECTORS. R & R RT ITT INDICATOR.SDR S9BA201508140010Skin · dentedDENT AT RT FUSELAGE UNDER 11TH CABIN WINDOW. EVALUATED DAMAGE AT FUSELAGE BS 580.0, WATERLINE 100. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.SDR S9BA201507220008Blade · damagedLEFT ENGINE STAGE 1 ROTOR BLADE MISSING MATERIAL. DAMAGE DISCOVERED VIA BORESCOPE INSPECTION. PICTURE TAKEN AND FORWARDED TO TECH SUPPORT AND THEY DETERMINE THAT ENGINE NEED TO BE REPLACE.SDR 29GA2015060200001Oil System · underservicedLOST LT ENGINE OIL PRESSURE IN FLIGHT AT CRUISE. INSPECTED AND FOUND NR 1 ENGINE TO BE LOW ON OIL, ADDED 3.5 QUARTS TO NR 1 ENGINE, PERFORMED HIGH POWER RUNS OPS CHECKS GOOD.SDR PNSA2015052105Anti-Ice Valve · dirtyLEFT ANTI-ICE BLEED VALVE LIGHT CAME ON, REMOVED AND CLEANED ANTI-ICE BLEED VALVE.SDR 29GA2015052200001Bulb · inoperativeEMERGENCY LIGHT INDICATOR ON F/A PANEL IS NOT WORKING. REPLACED EMERGENCY LIGHT INDICATOR BULB ON F/A PANEL, OPS CHECKED GOOD.SDR 29GA2015051500002B-Nut · leakingLEFT ENGINE OIL LIGHT ILLUMINATED IN FLIGHT, LT OIL PRESSURE DECREASED BELOW 30 PSI. RETURNED TO DEPARTURE, LANDED SAFELY. TORQUED COUPLING NUT AT PGB BRACKET UNION AT 1300 IN LBS ENGINE RUNS. OPS AND LEAK CHECK GOOD.SDR 29GA2015050600001Engine · failedLEFT ENGINE FAILURE ON BASE TO FINAL APPROACH. REPLACED LT ENGINE TORQUE AND SPEED SENSOR, PERFORMED ENGINE RUNS ALL PARAMETERS, CHECK NORMAL.SDR S9BA2015042700002Compressor · stalledDURING TAKEOFF ROLL JUST AFTER CTOT WAS APPLIED, THE RT ENGINE STARTED DOING A COMPRESSOR STALL PRIOR TO 60 KNOTS.
Back to GE CT7-9B