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 = 'CF66D' 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 = 'CF66D' 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 FDEA201311192829Towershaft · failedFL 350 CRUISE FLIGHT ENG 3 FLAMED OUT DUE TO HIGH OIL PRESS & 0 ZERO N2 COMPLIED WITH QRH DIVERTED TO KMIA. NR 3 ENG R & R DUE TO TOWER SHAFT FAILURE, OPERATIONS CHECKED GOOD.SDR FDEA201307201602Pump · failedREJECTED TAKEOFF DUE TO NR 1 ENGINE ROLL BACK AT 95 KTS. R & R THE MEC AND FUEL PUMP.SDR FDEA201306301422Sensor · failedNR 3 OIL TEMP ALERT, TEMP REACHED 162 DEGREES. RAN QRH, SHUTDOWN ENGINE AFTER 15 MINS IN CAUTION ZONE. TROUBLE SHOT IAW AMM 72-00-00-1/FIM 79-32-01. NO AIU FAULTS; NO FUEL AND/OR OIL CONTAMINATION. CHECKED MASTER CHIP DETECTOR PRECAUTIONARY; NO METAL NOTED.SDR FDEA201306261405Mec · inoperativeCLIMBING OUT AT 15,000 FT NR 2 ENGINE SPOOLED DOWN TO INOPERATIVE. DID ENGINE SHUTDOWN PROCEDURES AND RETURNED FOR LANDING. REPLACED MEC AND FUEL PUMP, ACCOMPLSIHED HIGH POWER RUNS, ALL CHECKED GOOD. COMPLETED INSTALLATION OF MEC AND FUEL PUMP PERFORMED A THSDR FDEA201306191342Mec · failedDURING DESCENT, NR 3 ENGINE FLAMED OUT. NO FIRE OR ABNORMAL INDICATIONS. ATTEMPTED ONE RESTART, RAN ALL APPLICABLE QRH CHECKLIST. FUEL AT FLAME OUT 8K, 7K, 8K. ENGINE WINDMILL 15 MIN AFTER FLAMEOUT. REMOVED NR 3 ENG FUEL PUMP AND MEC IAW MM 73-12-01-2.SDR FDEA201305291138Warning Light · false activationWHEN PM SET TAKEOFF POWER ENG 2 N1 WAS 5 PERCENT ABOVE ENG 1 & 3. REJECTED TAKE OFF DUE TO ENG 2 EXCEEDANCE ALERT AT 189KTS. N2 PEAKED AT 101.1 PERFORMED BORESCOPE INSPECTION OF THE NR 2 ENGINE HIGH PRESSURE COMPRESSOR AND HIGH PRESSURE TURBINE IAW AMM 72-SDR UIEA2013030500114Exhaust Stack · crackedDURING MX WALK AROUND, FOUND A CRACK ON ENGINE NR 3 PRIMARY EXHAUST NOZZLE LOCATED AT 9 O'CLOCK POSITION AFT EDGE. THE CRACK DIMENSION RUNS 4.7500" LONG CIRCUMFERENTIAL AND LOCATED .7500" FROM THE NOZZLE AFT END. THE CRACK IS DETERMINED TO BE OUTSIDE ALLOWASDR FDEA201302120329Unknown · vibrationENGINE VIBRATION NOTED IN CRUISE FLIGHT. CLIMB WAS NORMAL. AS POWER WAS REDUCED AT TOP OF CLIMB, VIBRATION WAS NOTED AND DETERMINED TO BE ENGINE NR1. VIBRATION WAS MOST PROMINENT AT APPROX 95 PERCENT NI. AT LOW POWER SETTINGS VIBRATION WAS LESS AND NO VIBSDR UIEA2013021900096Frame · chafedNR 1 ENGINE LT CORE COWL NR 2 INTERIOR FRAME FOUND CHAFING MARK. (NR 1 ENG LT CORE COWL NR 2 INTERIOR FRAME CHAFING MARK AREA REPAIRED IAW SRM 54-45-02-2R1, REP 1, FIG 201.)SDR UIEA2013021900097Frame · chafedNR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME FOUND CHAFED. (NR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME CHAFING MARK AREA REPAIRED IAW CN13-0428).SDR FDEA201301270199Line · cloggedENGINE FAIL WARNING ILLUMINATED ON GLARESHIELD ON TAKEOFF, NR 1 ENG N1 DID NOT ACCELERATE PAST 87 PERCENT. ENG DID NOT FAIL. DISCONNECTED NR 1 ENG CDP LINE. BLEW LINE CLEAR, FOUND MINOR DEBRIS IN LINE. CAPPED LINE AND PRESSURE CHECKED FOR LEAKS, NONE FOUSDR FDEA201211023815Sensor · failedON CLIMB OUT, NR 3 ENGINE EXCEEDENCE. RAN QRH, OIL PRESSURE MAINTAINED THROUGH OUT WINDMILL. ALL OTHER PERIMETERS WERE NORMAL. REMOVED AND REPLACED N1 FAN SPEED SENSOR IAW AMM 77-11-01.SDR FDEA201209273473Skin · damagedRT OTBD FLAP UPPER SURFACE SKIN IS SEPARATED FROM STRUCTURE DUE TO PULLED THRU FASTENERS 60" FROM OTBD END. REPAIRED IAW SRM 57-10-00, FIG 7, VOL I. MAJOR REPAIR.SDR FDEA201209203366Mount · brokenUNSAFE NOSE GEAR INDICATION ON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE AFTER TAKEOFF. CAPTAIN STATED THEY DID NOT FEEL THE NOSE GEAR EXTEND WHEN SELECTED DOWN. RT PSEU SHOWED NO NOSE GEAR CURRENT OR PREVIOUS FSDR FDEA201209153328Scavenge Pump · leakingDURING CLIMB NR 1 OIL QUANTITY INDICATED '0'. ALL OTHER INDICATIONS NORMAL INITALLY. IN CRUISE NR 1 OIL PRESS DROPPED TO 14 PSI WITH AN AMBER INDICATION. CONFERRED WITH MAINT. THROUGHOUT, QRH COMPLIED WITH. DIVERTED. UPON ARRIVAL CHECKED NR 1 ENG. OIL, CSDR FDEA201208293198Proximity Sensor · out of adjustON GEAR RETRACTION RECEIVED A RED LT MAIN GEAR LIGHT ON THE PRIMARY AND SECONDARY INDICATORS. PERFORMED QHR PROCEDURES AND HAD SAME INDICATIONS. DUMPED FUEL TO MAX LANDING WT AND RETURNED TO DEPARTURE. R & R LT MLG CRANK SENSOR SUPPORT FOR THE UP AND LASDR FDEA201208243184Fuel Cell · leaking"TANK 2 PUMP OFF" FOLLOWED BY " NR 2 CROSSFEED" ABOUT 1 HOUR INTO FLIGHT. NR 2 QTY INDICATED ALMOST 5000 POUNDS LESS THAN 1 AND 3. FOLLOWED QRH AND IN MANUAL ALL QUANTITIES DROPPED AT A CONSISTENT RATE. NR 2 QUANTITY VARIED FROM 1,800 TO 10,000. GROUND CRSDR FDEA201208213092Skin · crackedFUSELAGE SKIN CRACKED AT FWD RT SIDE OF NOSE GEAR W/W CUTOUT REPAIRED USING SRM 53-50-00 AS A REFERENCE.SDR FDEA201208213093Skin · crackedFUSELAGE SKIN CRACKED AT FWD LT SIDE OF NOSE GEAR W/W CUTOUT. COMPLIED WITH EA 8-5350-157364 & REPAIRED AREA USING SRM 53-50-00.SDR FDEA201208112941Skin · crackedLT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00, FIG 68, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201208102952Fuel Cell · contaminatedDEBRIS REMOVED FROM NR2 TANK DURING MX. NEED FFC TO INSPECT NR 2 TANK FOR FURTHER DEBRIS. ALSO NEED TO INSPECT PLUMBING FOR 2L AFT PUMP INLET AND PUMP MANIFOLD FOR DEBRIS DUE TO HISTORY. BASKET ASSY CRACKED AND DEFORMED FROM COMPACTED DEBRIS. R & R PICK UPSDR FDEA201208082888Frame · corrodedAFT CARGO BAY BS 1841 FRAME CORRODED. REMOVED DAMAGED AREA. FABRICATED, DRILLED, DEBURRED, ALODINED & PRIMED REPAIR ANGLE & SPLICE & FILLER IAW SRM53-30-00. FRAME REPAIRED IAW SRM.53-30-00, VOL I AND ER 12-03855.SDR FDEA201208072897Bulkhead Web · crackedCRACK IN LT SIDEWALL 10 INCHES AFT OF BS 1381 AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK EMANATE'S OUT OF LIGHTNING HOLE AND ENDS AT FASTENER. REPAIRED LT WW SIDEWALL IAW SRM 53-00-01, FIG 10.SDR FDEA201208062858Skin · dentedLOWER FUSELAGE SKIN AFT OF CENTER CARGO DOOR SHOWING DENT APPROX 3 INCHES LONG. INSTALLED DOUBLER IAW EA 8-5330-160630 & SRM 53-20-00, FIG 3, SHEET 8.SDR FDEA201207312784O-Ring · failedHYDRAULIC SYSTEM 1 LOST QUANTITY INITIALLY 0 BUT AFTER LANDING RECOVERED TO 2.2 GAL. ACFT STILL HAD 3.7 GAL OF HYDRAULIC FLUID IN NR 1 SYS. TROUBLESHOOTING FOUND NR 1 SYS BRAKE ACCUMILATOR HAS A BLOWN O-RING. REPLACED O-RING IAW SMP, SERVICED ACCUMILATOR ISDR FDEA201207312775Fire Bottle · lowENGINE FIRE AGENT LOW, AT GATE AFTER ENGINE SHUTDOWN. REMOVED AND REPLACED NR 3 ENGINE FIRE DISCHARGE BOTTLES IAW MM 26-21-01-4. PERFORMED ALL ADJ/TEST'S PER MM 26-21-06/ 26-21-01. FOUND BRACKET BROKEN ON PNEUMATIC BLEED DUCT CAUSING UNRESTRAINED FLEX DUCTSDR FDEA201207282723Floorbeam · corrodedAFT CARGO BAY BS 1841 FLOORBEAM CORRODED AT SEVERAL FLOORBOARD NUTPLATE HOLES. REMOVED AND REPLACED CORRODED FLOORBEAM IAW DWG AGA 3874 AND SRM 51-35-01 VOL. 2.SDR FDEA201207262685Angle · crackedAIR CONDITIONING COMPARTMENT NR 3 - BETWEEN BS 575 - 595 AT L30. CAL ANGLE IS CRACKED APPROX 8.00". REPAIRED IAW SRM.SDR FDEA201207232878Bulkhead · crackedLEFT FWD CORNER OF NOSE WW CRACKED. REPAIRED CRACK AND INSTALLED DOUBLERS IAW SRM VOL I 53-50-00, FIG 25.SDR FDEA201207232879Skin · crackedAFT UPPER CORNER OF NR 1 ACM EXHAUST CRACKED. INSTALLED DOUBLER AND TRIPLER ON AFT UPPER COUNER OF NR 1 ACM EXHAUST USING SRM 53-20-00 AS A REF.SDR FDEA201207232880Skin · crackedAFT UPPER CORNER OF NR 2 ACM EXHAUST CRACKED. REPAIRED CORNER ACM EXHAUST AS REQUIRED IAW SRM 53-20-00, FIG 2.SDR FDEA201207232881Bulkhead · crackedLT MLG WW SIDEWALL CRACKED 20 INCHES AFT OF BS 1381 AND 7 INCHES DOWN AND A CRACK 17 INCHES AFT OF 1381 5.5 INCHES DOWN. REPAIRED CRACK REF EA 8-5310-157358, REV B.SDR FDEA201207232882Structure · crackedCRACK ON INBD SIDEWALL 30 INCHES FWD OF BS 1521 AND 20 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-157357.SDR FDEA201207222636Skin · misrepairedCARGO DOOR SKIN MISREPAIRED. REPAIRED AS PER EA 8-5230-159867.SDR FDEA201207192620Angle · crackedAIR CONDITIONING COMPARTMENT NR 3 - BETWEEN BS 555-575 AT L30. ANGLE IS CRACKED APROX 8".SDR FDEA201207142578Support Fitting · crackedRT MLG WHEEL WELL AFT OTBD CORNER, LOWER REINFORCING STRUCTURE HAS A CRACKED SUPPORT FITTING AT BS 1501. R & R CRACKED SUPPORT FITTING IAW SRM 51-31-01, FOUND STIFFENER CRACKED, REMOVED STIFFENER, FABRICATED AND INSTALLED STIFFENER IAW SRM 51-31-01, VO.I, FSDR FDEA201207042479Skin · misrepairedLT WING NR 3 SLAT AFT SKIN INBD OF NR 7 TRACK MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 98. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207042480Rib · misrepairedLT WING AILERON LOWER SKIN RIB MISREPAIRED, REPAIRED IAW EA 8-5750-160989, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207032453Button · inoperativeON WALK AROUND, FOUND LT ENTRY DOOR SLIDE PRESS TO TEST LIGHT INOPERATIVE. REPLACED BATTERIES, NO HELP, REPLACED TEST BUTTON WITH R1 LIGHT BUTTON CHECKED GOOD. REMOVED AND REPLACED L1 DOOR SLIDE PRESSURE PTT ASSEMBLY REF AMM 25-61-03-2. OPS CHECKED GOOD.SDR FDEA201207032472Bolt · corrodedRIGHT MLG FWD UPPER TRUNNION BOLT CORRODED. REPLACED RT MLG FWD TRUNNION BOLT PER EO 8-3210-7-5004B PT2, ACCOMPLISHED CHECK.SDR FDEA201207032466Trunnion · corrodedLEFT MLG STRUT FWD TRUNNION LUG IS CORRODED, MISSING. REMOVED AND REPACED LT MAIN LANDING GEAR.SDR FDEA201207022435Skin · misrepairedLT WING NR 8 SLAT INBD LOWER SKIN MISREPAIRED. LT WING NR 8 SLAT R & R AMM 27-80-01-04, REV 14.3. OPS AND GAP CHECK CARRIED OUT IAW AMM 27-80-01-04, REV 14.3 FOUND SATISFACTORY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207022436Skin · misrepairedRT WING NR 5 SLAT AFT SKIN MISREPAIRED. REPAIRED IAW EA 8-5100-162351. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201207022440Skin · misrepairedRT WING NR 1 SLAT AFT SKIN MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL I, REV 99. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206302418Skin · dentedLOWER FUSELAGE SKIN, APPROX STATION 1964, LONGERON 40 LT, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6 SHEET 3 VOL I, REV 98. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-20-00, FIG 6, SHEET 3, VOL I, REV 98. REPAIR CLASSIFIED AS MAJOR IAW SDR FDEA201206302417Skin · misrepairedHORIZONTAL STABILIZER DETACHABLE ELEVATOR UPPER SKIN AT XE 50 RT MISREPAIRED. REPAIRED IAW SRM 51-35-02, VOLUME II, REV 98 AND EA8-5520-162352. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206282376Skin · misrepairedRT WING L/E INNER SKIN MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-160976, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206252344Skin · misrepairedRT WING, NR 4 SLAT AFT SURFACE STATION XOS 623 MISREPAIRED. REPAIR ACCOMPLISHED IAW SRM 57-10-00, FIG 31, VOLUME I, REV 98. EO 8-5100-7-5001 B2 PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206252345Skin · misrepairedRT WING NR 4 SLAT AFT SURFACE, STATION XOS 633 MISREPAIRED. REPAIR ACCOMPLISHED IAW SRM 57-10-00 FIG 31, VOL I, REV 98. EO 8-5100-7-5001 B2, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100 REV 115.SDR FDEA201206252339Skin · misrepairedRT WING NR 1 SPOILER PANEL LOWER SURFACE MISREPAIRED. SPOILER PANEL REPLACED IAW AMM 27-60-01-4, REV 14.3. CLEARANCE CHECK AND OPS TEST CARRIED OUT IAW AMM 27-60-01, REV 14.3 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.
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