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 OZCA20150305015Seal · leakingLEFT PROPELLER OIL PRESS DECREASED BELOW 25 PSI DURING FLIGHT. INSPECTED LT PROPELLER PRESS INDICATING SYS. FOUND LT AC GEN LEAKING OIL THROUGH BEARING SEAL. R & R LT AC GEN & SHAFT O RING IAW MM. OPERATIONAL & LEAK CHECKED ALL SATISFACTORY.SDR S9BA2015011500001Engine · making metalDURING CRUISE, LT CHIP DETECTOR LIGHT INTERMITTENT, ONE CHIME. LT ENGINE HAD PREVIOUS CHIP DETECTOR LIGHT ON, REPORTS WHICH RESULTED WITH NO PARTICLES PRESENT AT THE CHIP DETECTOR UPON INSPECTION. DURING THE LAST CHIP DETECTOR LIGHT INSPECTION, MINOR METAL SDR OZCA20140101011Connector · looseAUTO COARSEN LIGHT ILLUMINATED ON DESCENT. UPON TROUBLESHOOTING FOUND ELEC CONNECTOR AT SWITCHER COMPUTER LOOSE. SECURED ELEC CONNECTOR. PERFORMED OPERATIONAL CHECK. ALL CHECKED SATISFACTORY. AS PRECAUTION, R & R AUTO COARSEN COMPUTER IAW MM. OPERATIONS SDR OZCA20141231010Pressure Switch · defectiveDURING DESCENT NR 1 ENG AUTO COARSENED. TROUBLE SHOT SYS & PERFORMED GND OPERATIONAL CHECKS OF AUTO COARSEN SYS. ALL CHECKED SATISFACTORY. R & R LT AUTO COARSEN PRESS SWITCH IAW MM. OPERATIONAL CHECKED SATISFACTORY.SDR CA141114007Cable · broken(CAN) DURING ENGINE START-UP IT WAS NOTICED THAT THE NR 1 ENGINE RPM WAS NOT RESPONDING PROPERLY WHEN THE ENGINE POWER LEVER WAS ADVANCED. WITH MINIMAL POWER LEVER INCREASE THE RPM WOULD INCREASE TO NEAR THE MAXIMUM ALLOWABLE RPM. THE ROOT CAUSE WAS A BROKEN PSDR CA141023009Gps · failed(CAN) CLIMBING THROUGH 10,000 FEET, THE GPS REBOOTED & FLAGGED ON THE EFIS, SHORTLY AFTERWARDS & ELECTRICAL BURNING ODOR COULD BE DETECTED. THE AIRCRAFT RETURNED. REMOVED THE GPS FROM THE AIRCRAFT & COULD SMELL AN ELECTRICAL BURNED ODOR. NO PHYSICAL DAMAGE SDR 29GA2014072100002Chip Detector · dirtyLEFT CHIP DETECTOR INDICATOR ILLUMINATED DURING FLIGHT, AT ALL TIMES NO CHANGES TO ENGINE PARAMETERS. REMOVED AND CLEANED SMALL CARBON DEPOSITS FROM CHIP DETECTOR RAN LT ENGINE FOR 30 MINUTES WITH NO LT CHIP DETECT LIGHT ILLUMINATING, OPS CHECKED GOOD.SDR S9BA2014072100007Line · leakingSTRONG ODOR OF OIL & FUEL IN CABIN. LANDED, INSPECTED ALL FUEL LINES AND OIL COMPONENTS THE LT ENGINE FOR ANY POSSIBLE LEAKAGES THAT MAY CAUSE THE ODOR IN THE CABIN. FOUND AGB TO HMU LINE LEAKING AFTER INITIAL ENGINE RUN. TIGHTEN LINE IAW MM 730000, STEP 9ASDR UG8A201302220001Outflow Valve · faultyPRESSURIZATION AT FL200 WENT OUT. OUTFLOW CABIN ALTITUDE CLIMBED. TROUBLESHOT SYSTEM IAW MM 21-30-00 AND FOUND PRIMARY OUTFLOW VALVE DOES NOT CLOSE FULLY. R & R OUTFLOW VALVE. OPS CHECKED GOOD.SDR NSVA20120613554Engine · vibrationDURING EN ROUTE CLIMB, THE CREW FELT SEVERE VIBRATION COMING FROM THE NR 2 ENGINE. THE CREW FOLLOWED UNUSUAL ENGINE VIBRATION PROCEDURES, SHUTDOWN ENGINE, DECLARED AN EMERGENCY. LANDED WITHOUT ADDITIONAL COMPLICATION . THE CREW REPORTED NO OTHER ABNORMAL ISDR NSVA20120407507Control Cable · brokenON LANDING, HAD LEFT ENGINE REDUCE THRUST DOWN TO 20 PERCENT. THE CREW DID SHUT DOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE 9 PASSENGERS ON BOARD WERE NOT BRACED. FOUND LT POWER LEVER CABLE FROM NACELLE TO FUSELAGE IS BROKEN.SDR PNSA111101Engine · shutdownENGINE SHUT DOWN IN FLIGHT, LANDED WITHOUT INCIDENT.SDR NSVA2011189Engine · smokeGRAY SMOKE FROM RT ENGINE TAIL PIPE. MX INSPECTED RT ENGINE, DRAINED EPA CAN AND PERFORMED RUNS COULD NOT DUP.SDR CA110901003Conduit · damaged(CAN) LT FUEL BOOST PUMP CONDUIT FOUND LEAKING AND FOUND TO HAVE A PIN HOLE THROUGH THE CONDUIT ALLOWING FUEL TO RUN INSIDE THE CONDUIT, IPC REF 28-20-00-01 ITEM 15B.SDR PNSA20110823001Hmu · malfunctionedERRATIC TRQ NR 1 ENGINE - TRQ MOTOR LOCKOUT FIXED PROBLEM. RETURNED TO ANC. MAINT REMOVED AND REPLACED THE HMU AND THE DECU.SDR NSVA2011106Oil System · lowCREW RECEIVED RT ENG OIL PRESSURE MASTER WARNING DURING INITIAL CLIMB. ALL RT ENG INDICATIONS WERE NORMAL EXCEPT ENG OIL PRESSURE WHICH WAS FLUCTUATING FROM 50 PSI TO BOTTOM OF GREEN ARC (30 PSI) AND IN SOME CASES INTO YELLOW ARC. THEN MASTER WARNING EXTINGUSDR NSVA2011105Engine · leakingABNORMAL RT ENGINE INDICATION CREW ELECTED TO DO A PRECAUTIONARY ENGINE SHUT DOWN, AND RETURNED TO IAH. ENGINE CHANGE DUE TO OIL IN THE BURNER CAN AND TURBINE SECTION.SDR NSVA2011070Engine · defectiveON CLIMBOUT (ABOUT 400 FT) RIGHT ENGINE OVERTEMP LIGHT CAME ON AND ITT EXCEEDED 980 DEG C WHILE THE TORQUE DROPPED OFF TO ABOUT 60 PERCENT CTOT WAS DIALED BACK AND ENGINE THEN FAILED AND AUTOCOARSENED. OVERTEMP LIGHT STAYED ON APPROX 30 SEC, EVERYTHING ELSE WSDR MALA110040Control Handle · malfunctionedON TAKEOFF, LANDING GEAR WOULD NOT STOW. TRANSIT LIGHT REMAINED ILLUMINATED. EMERGENCY NON NORMAL RAN. PROBLEM REMAINED. AFTER DISCUSSING WITH MX CONTROL AND DISPATCH, THE DECISION WAS MADE TO RETURN TO DEPARTURE. THE FLIGHT LANDED WITHOUT INCIDENT. INSPSDR MALA100212Control Unit · inoperativeGEAR INTRANSIT LIGHT INOP (BOTH WAYS). LIGHT BULBS TESTED OK. GEAR 3 GREEN LIGHT WORKS FINE. R & R LANDING GEAR CONTROL UNIT PN ON/OFF D494-12-001, SN OFF 659/02-98, SN ON 614/09-96. OPS CHECK GOOD IAW AMM 32-31-05-02.SDR MALA100207Uplock · icedAFTER TAKEOFF LANDING GEAR "IN TRANSIT" LIGHT REMAINED ON. RECYCLED GEAR IAW NON-NORMAL CHECKLIST. LIGHT REMAINED ON AFTER GEAR SELECTED UP AGAIN. COMPLETED REMAINDER OF FLIGHT WITH GEAR DOWN IAW CHECKLIST. ALL HYD INDICATIONS NORMAL. UPLOCK PADS WERE CHESDR NSVA2010230Pressure Switch · malfunctionedGEAR TOOK ABOUT 4 MINUTES TO COME UP HYD PUMP RAN CONTINOUSLY. RAN QRH CYCLED GEAR THEN CAME UP NORMALLY. COULD NOT DUPLICATE DISCREPENCY. REPLACED HYDRAULIC AUTO PRESSURE SWITCH. REPLACED HYDRAULIC RESEVOIR, BLED SYS AND SERVICED; PERFORMED NUMEROUS GEAR SDR MALA100200Cdu · malfunctionedSMOKE FROM FMS AREA, ON GROUND PULLED "AREA NAV" CIRCUIT BREAKER TURNED OFF LT AND RT AVIONICS. SMOKE STOPPED. R & R FMS CDU IAW 34-60, ALL CHECKS GOOD PN ON/OFF F1014-21, SN OFF 470, SN ON 417.SDR MALA100196Uplock Switch · out of adjustGEAR UNSAFE INDICATION AFTER DEPARTURE. ALL LDG GEAR LIGHTS EXTINGUISHED. ENNC COMPLETED. GEAR UNSAFE LIGHT EXTINGUISHED. FOUND LT & RT MLG UPLOCKS WERE PREVIOUSLY ADJUSTED TOO TIGHT. READJUSTED WITHIN LIMITS IAW AMM 32-32-00-05. PERFORMED ADJUSTMENT OF LTSDR MALA100195Door · out of rigGEAR UNSAFE LIGHT WITH GEAR IN UP POSITION JUST AFTER TAKEOFF. EMER NON-NORMAL CHECKLIST COMPLETED. PERFORMED RIGGING OF UPLOCK AND RELEASE ON LT LANDING GEAR IAW AMM 32-32-00. PERFORMED FUNCTIONAL TEST OF EXTENSION RETRACTION SYS 32-30-00. FUNCTIONAL TESTSDR MALA100188Control Unit · malfunctionedON DEPARTURE, WE RECEIVED GEAR UNSAFE INDICATIONS WITH GEAR HANDLE IN THE UP POSITION AND HANDLE ILLUMINATED. RAN CHECK LIST ON BOTH OCCASIONS AND RECYCLED GEAR. LIGHT EXTINGUISHED. PERFORMED GEAR SWINGS. UNABLE TO DUPLICATE. R & R LANDING GEAR CONTROL UNSDR MALA100183Control Unit · malfunctionedIN-TRANSIT LIGHT REMAINS ILLUMINATED WHEN GEAR HANDLE SELECTED UP, 3 GEAR LIGHTS OUT. RECYCLED WITH SAME RESULTS. REPLACED LANDING GEAR CONTROL UNIT AND PERFORMED FUNCTIONAL TEST OF EXTENSION & RETRACTION SYS IAW AMM 32-31-05-02. ALL CHECKS GOOD.SDR PNSA101101Line · crackedWHILE ON CLIMBOUT AT 1000FT AGL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL IMMEDIATELY FOLLOWING A POWER REDUCTION FOR CLIMB POWER. THERE WAS 2 "BANGS" AND THE ENGINE WENT INTO AUTO COARSENING AND THE ENGINE WAS SHUT DOWN BY THE FLIGHT CREW AND NO TEMPERSDR 2010F00238Indicator · burnedWHILE IN CRUISE, PILOTS SAY THE CABIN PRESSURE INDICATOR STOP WORKING. CREW THEN SMELLED A FAINT ELECTRICAL BURNING SMELL, NO SMOKE WAS REPORTED. ACFT RETURNED, NO OTHER PROBLEMS WERE NOTED. MX FOUND THAT THE CABIN PRESSURE CONTROLLER HAD FAILED AND WAS THESDR NSVA2010181Engine · malfunctionedTHE APPROACH WAS NOT STABLE AT 500 FEET CAPTAIN INITIALIZED GO-AROUND. CREW APPLIED GO-AROUND POWER AND THAT'S WHEN THE RIGHT ENGINE FAILED (ENGINE AUTOCOARSENED). CREW DECLARED AN EMERGENCY PASSENGER WERE BRIEFED OF THE ENGINE FAILURE. FLIGHT CAME AROUND ASDR MALA100145Power Supply · failedEMERGENCY POWER SUPPLY 23LN & 20LN FAILED CAP CHECK. REPLACED EMERGENCY POWER SUPPLY 23LN IAW SF3 AMM 33-50-10. OPS CHECK GOOD. OPS CHECK GOOD.SDR MALA100147Switch · inoperativeWHILE PERFORMING MX, FOUND EMERGENCY LIGHT SWITCH BAD. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. REF AMM 39-40-15-02. P/N ON&OFF MS27406-1. OPS CHECK GOOD REF AMM 33-50-00.SDR NSVA2010176Engine · failedRIGHT ENGINE ABNORMAL INDICATIONS IN FLIGHT. CREW SHUT DOWN THE ENGINE AFTER FOLLOWING THE CHECKLIST. LANDED NORMAL, TAXIED TO GATE ON IT'S OWN POWER. PASSENGERS AND CREW ARE ALL RIGHT WITH NO KNOWN COMPLICATIONS AT THIS TIME. PERFORMED FDR DOWNLOAD FOUND ESDR MALA100142Seat Track · corrodedRT CTR AISLE SEAT TRACK HAS A SPOT OF CORROSION AT STATION 296. CUT OUT 12 INCH SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION IAW EO S53060. THIS EO PROVIDES INSTRUCTIONS FOR REPAIR OF DAMAGE TO SEAT TRACKS FROM TOP TO BOTTOM IAW SRM CHAPTER 53-70-60, SPECSDR MALA100143Power Supply · failedDURING TC 335003 POWER SUPPLY 21LN FAILED CAPACITY CHECK. REPLACED POWER SUPPLY 21LN IAW AMM 33-50-10, PN 3301-51, SN OFF 2056, SN ON 1355. EMERGENCY LIGHTING SYSTEM OPS CHECKS GOOD IAW AMM 33-50-00.SDR MALA100141Battery Pack · failedDURING TC NR335003 EMERGENCY BATTERY PACK 21LN FAILED CAPACITY CHECK. REPLACED EMERGENCY BATTERY PACK 21LN IAW AMM 33-50-10. EMERGENCY LIGHTING SYS OPS CHECKS GOOD IAW AMM 33-50-00.SDR MALA100139Firewall · chafedRT NACELLE FIREWALL CHAFED .675 X .25 X .039 DEEP. APPROX 1.375" FWD AND INBD OF DEICE LINE/FIREWALL UNION. ACCOMPLISHMENT OF INTERIM REPAIR IAW REPAIR STATEMENT 340SDS021032 DATED 8/21/2010 AND EOS54246 PROVIDES CONTINUED OPERATION UNTIL 10/12/2010 (N4K, 30/SDR MALA100138Acm · seizedDURING TAXI OPERATIONS WITH RT ENGINE FEATHERED AND RT HP ON, NOTED, A SMELL SIMILAR TO MATCHES. NOT LONG AFTER NOTICING THE SMELL, AIR GOT EXTREMELY HOT. F/A DID NOT FEEL HOT AIR IN THE CABIN AT THIS TIME. NO WARNING LIGHTS ILLUMINATED ON CWP OR OVERHEAD PASDR MALA100129Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FOR 21LN FAILED OPS TEST. REPLACED EMER LIGHT POWER SUPPLY 21LN (PN: 3301-51, SN OFF: 1358) IAW AMM 33-50-10. OPS TEST GOOD.SDR MALA100126Lamp · inoperativeF/A EMERGENCY LIGHT IS INDICATING ON AND NOT SHOWING ARMED ON THE EMERGENCY LIGHTS. RELAMPED F/A ARM/ON BUTTON.SDR MALA100135Battery Pack · failedEMERGENCY LIGHTING BATTERY PACK 24LN FAILED OPS TEST. REPLACED EMERG BATTERY PACK 24LN, PN 3301-51, SN OFF 2102, SN ON 1370, IAW AMM 33-50-10-04-1.SDR MALA100136Battery Pack · failedEMERGENCY LIGHTING BATTERY PACK, 23LN FAILED OPS TEST. R & R EMERGENCY POWER SUPPLY AT 23LN PN 330-51 ON/OFF SN ON 2103 OFF 2166 IAW AMM 33-50-10-04-1.SDR NSVA2010161Relay · failedDURING DESCENT, CA'S NAVIGATION DISPLAY FAILED. CREW WAS ABLE TO CONTINUE AND LANDED. REPLACED BATTERIES AND 2 RELAYS. OPS CHECKED GOOD.SDR MALA100125Power Supply · failedEMERGENCY POWER SUPPLY 21LN FAILED CAPACITY CHECK. REPLACED 21LN.SDR NSVA2010159Generator · overtempRT DC GENERATOR OVERTEMP LIGHT ILLUMINATED DURING TAXI. RETURNED TO GATE. REPLACED RT DC GENERATOR.SDR MALA100119Structure · chafedFRAME 630-112 IS CHAFED IN RT SIDE JUST ABOVE SEAT TRACK. BLENDED AND APPLIED DOUBLER IAW EO S53775.SDR MALA100130Seat Track · corrodedCARGO CENTER AISLE SEAT TRACK CORROSION: BL 0, STA 622-686. REPAIRED IAW S53060.SDR MALA100131Seat Track · corrodedCENTER AISLE SEAT TRACK CORROSION: LBL 18.3, STA 297-308. REPAIRED IAW S53060.SDR MALA100132Seat Track · corrodedCTR AISLE SEAT TRACK CORROSION: BL 0, STA 297-307. REPAIRED IAW S53060.SDR MALA100133Frame · unknownLOWER FRAME, UPPER FLANGE, STA 294 LBL 18 TO BL0. REPAIRED IAW S53776.
Back to GE CT7-9B