N79750, cancelled Jan 24, 2018
Service difficulty reports · 60
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N79750' AND deregistration_id = 'N79750-2018-01-24' 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 n_number = 'N79750' AND deregistration_id = 'N79750-2018-01-24' 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 2004F00174Line · crackedDURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUPPLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M)SDR 2004F00301Actuator · inoperativeDURING THE AFTER T/O CHECKLIST, NR 2 LEADING EDGE SLAT EXTENDED INDICATION REMAINED ON BOTH FORWARD AND AFT ANNUNCIATOR LIGHTS DUMPED FUEL AND RETURNED TO KCVG WITHOUT INCIDENT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR PER MM 27-81-32. AIRCRAFT RETURNED TO SSDR 2004F00219Steering Sys · out of adjustDISCONTINUED TAKEOFF ROLL, DUE TO LACK OF STEERING CONTROL TO THE RIGHT. RETURNED TO RAMP WITHOUT INCIDENT. ADJUSTED RUDDER PEDAL STEERING MECHANISM PER MM 32-51-0. OPS CHECK GOOD. (M)SDR 2002F01029Ballast · malfunctionedDURING CLIMB, SMOKE ALARMS IN BOTH AFT LAVATORIES WENT ON, SMOKE WAS NOTICED. AFTER 20 OR 3 MINUTES IT WAS CLEAR, AFT GALLEY POWER WAS SWITCHED OFF AS PRECAUTIONARY A/C CONTINUED TO MIAMI. ON THE GROUND, FOUND AFT CABIN CEILING LIGHTS DUAL FILTER BALLAST BURSDR 2002F00402Switch · wornON TAXI-OUT WITH FLAPS 15 F/E AUX PANEL SHOWED NR 4 LE DEVICE NOT DOWN AND LOCKED A/C RETURNED TO GATE. REMOVED AND REPLACED NR 4 L/E DEVICE SWITCH PER MM 27-82-31. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2001F00643Hydraulic Line · leakingFLT 523 - ARRIVING FROM SVMI, AFTER LANDING INTO MIA, HYDRAULIC SYSTEM 'A' PRESSURE AND QUANTITY INDICATION DROPPED TO 0. AIRCRAFT CONTINUED TO GATE WITHOUT INCIDENT. MAINTENANCE T/S AND FOUND THE HYDRAULIC SYSTEM 'A' RETURN LINE FROM THE ENGINE NR 2 HYDRAULSDR FX72001F00003Heat Exchanger · crackedAFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. BOTH AIRCRAFT PACKS DID NOT WORK AND AFTER RESETTING BOTH PACKS TO (ON) AIRCRAFT WILL NOT PRESSURIZE. RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLESHOT AIRCRAFT PRESSURE SYSTEM, FOUND CRACKED PRIMARY HEAT EXCHANGESDR 20010320SG001Indicator · malfunctionedABORTED TAKEOFF DUE TO A LOW EPR INDICATION AT REDUCED POWER ON ENGINE NR 2. INSPECTED AND CREW RAN ENGINE UP TO MAX POWER. NR 2 ENGINE OPS PROPERLY ON GROUND ENGINE RUN AND ALL ENGINE INDICATIONS READ NORMAL AS PER TRIM CHART 71-00-87. AIRCRAFT RETURNED TOSDR 20000614AP003Switch · out of adjON FAE FLIGHT NR 153, DBWI TO KIAD, DURING CLIMB AND GEAR RETRACTION, THE TAIL SKID LIGHT REMAINED ILLUMINATED. AIRCRAFT PERFORMED AN AIR RETURN TO KBWI. ON GROUND MAINTENANCE ADJUSTED THE TAILS SKID SWITCH AND GROUND OPS CHECKED OK IAW 32-71-01. AIRCRAFT WSDR 20000614AP004Seal · misalignedON FAE FERRY FLIGHT 981 - KMIA-KFLL - DURING CLIMB, CREW HEARD LOUD NOISE FROM L1 DOOR. AIRCRAFT RETURNED TO KMIA. ON GROUND MAINTENANCE, FOUND DOOR SEAL LOWER HINGE MISALIGNED. SEAL WAS REPOSITIONED IAW MM 52-11-71. AIRCRAFT WAS PRESSURIZED IAW MM 21-31-0SDR 99ZZZM732Pdu · bindingFLT 201 - KMIA-SDQ - DURING CLIMB AND WHILE RETRACTING FLAPS, OUTBOARD FLAPS STAYED AT 5 DEGREES. RECYCLING BY NORMAL MEANS DID NOT WORK. A/C AIR RETURNED BACK TO KMIA. NO FUEL WAS DUMPED, A/C ACCOMPLISHED NORMAL OVERWEIGHT LANDING. WHILE EXTENDING FLAPS FOSDR CALA9901168Megaphone · inopINSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED.SDR 2000ZZZM204B-Nut · looseON FAE - FLT 945 - KMEM TO NBJ, DURING CLIMB, THROUGH FL260 NR 3 ENGINE STARTED FLUCTUATING INTERMITTENT AT FIRST THEN STEADY. AFTER LEVEL OFF AT FL290, NR 3 ENGINE CONTINUED TO FLUCTUATE. AIRCRAFT RETURNED TO KMEM. ON GROUND MAINTENANCE INSPECTED NR 3 ENGISDR 99ZZZX1758Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1060 - STA 1110, LBL 45.SDR 99ZZZX1757Stringer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950F - STA 990.SDR 99ZZZX1756Channel · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON A SECTION OF HAT CHANNEL LEFT AFT LAVATORY STA 1137 - STA 1176.SDR 99ZZZX1755Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON R-1 DOOR'S LOWER HINGE.SDR 99ZZZX1754Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON NR 1 NOSE FLAP OF NR 1 KREUGER FLAP AT BUSHING FLANGE ATTACH POINT.SDR 99ZZZX1753Beam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM.SDR 99ZZZX1752Strap · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STRAP IN C-1 PIT FLOOR AREA JUST FORWARD OF STA 540 THAT CROSSES FLOORBEAM.SDR 99ZZZX1751Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED AT STA 720L, STR 27.SDR CALA9801961Battery · dischargedAFT GALLEY OVERHEAD EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY.SDR CALA9801051Fitting · crackedINSPECTION FOUND A 2 INCH CRACK ON L-1 DOOR UPPER HINGE FITTING. THE CRACKED AREA WAS CUT OUT, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-5.SDR CALA9801050Fitting · corrodedINSPECTION FOUND LT MLG TRUNNION FITTING CORRODED. THE TRUNNION FITTING WAS REPAIRED IAW ECRA 5340-01320.SDR CALA9800995Skin · delaminatedINSPECTION FOUND A 4 X 2 AREA OF RT WING TRAILING EDGE INBOARD FOREFLAP LOWER SURFACE DELAMINATED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-12.SDR CALA9800948Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 27R-28R. THE CORRODED AREA WAS CUT OUT, A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-4, FIGURE 15, REPAIR 3.SDR CALA9800930Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD BAGGAGE BIN AT STA 500, RBL 9. THE INTERCOSTAL WAS REMOVED AND CORRODED STRINGER WAS CUT OUT IAW SRM 53-10-3. NEW STRINGER AND SPLICES WERE FABRICATED IAW SRM 53-10-5 AND 51-10-2. THE STRINGER, SPLICES AND INSDR CALA9800929Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.SDR CALA9800928Wire · brokenINSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 22 AND AFT. BROKEN WIRING WAS REPAIRED AND A FUSE WAS REPLACED IAW MM 33-50-00 AND OPERATION OF THE LIGHTS CHECKED GOOD.SDR CALA9800927Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AND 51-10-2.SDR CALA9800926Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT LOWER INBOARD AND OUTBOARD CORNERS OF LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9800925Cowling · corrodedINSPECTION FOUND NR 2 ENGINE INLET COWLING RING CORRODED. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, 51-10-2, 51-40-5 AND 51-30-2.SDR CALA9800586Battery Pack · dischargedINSPECTION FOUND CEILING EMERGENCY EXIT LIGHT BETWEEN R-2 DOOR AND L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR CALA9800099Structure · damagedTHE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, STRINGER, AND FRAMES AT STA 440-480, STRINGERS 14-19L. THE FUSELAGE SKIN AND STRINGER WERE REPAIRED IAW ECRA 5330-02621. THE FRAMES WERE REPAIRED IAW ECRA 5310-03656, SRM 51-40-3, AND 53-10-3.SDR CALA9701513Power Supply · inoperativeINSPECTION FOUND RIGHT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED.SDR CALA9701431Fuse · blownEMERGENCY TRACK LIGHTS INOP ROW 10 FORWARD. REMOVED AND REPLACED FUSES.SDR CALA9700423Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1033, RBL 26. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9700422Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1067, RBL 26. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700418Stiffener · crackedINSPECTION FOUND A .75 INCH CRACK IN STIFFENER AT BS 348, STRINGER 10R. THE STIFFENER WAS REPAIRED IAW SRM 51-30-2.SDR CALA9700417Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 10 AND RBL 10. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED USING REPAIR ANGLES AND FILLERS IAW SRM 53-10-8, FIGURE 9.SDR CALA9700416Circumferential · crackedINSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 930, STRINGER 14R. THE CRACKED AREA WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW EC 5310-01397, PAGE 5.SDR CALA9700415Circumferential · crackedINSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 804, STRINGER 14L. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3.SDR CALA9700414Support · brokenINSPECTION FOUND FLOOR SUPPORT BROKEN AT STA 758, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1.SDR CALA9700413Support · corrodedINSPECTION FOUND INBOARD END OF FLOOR SUPPORT CORRODED AT STA 342, RBL 17. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA9700412Stringer · deformedINSPECTION FOUND SKIN BULGED IN STRINGER 2-3L AREA AT STA 420 WITH STRINGER DEFORMED. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3.SDR CALA9700421Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1070 TO 1140, RBL 66. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9700420Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 1050, RBL 26 TO 66. THE CORRODED AREA WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-40-5, 51-10-2, AND 51-30-2.SDR CALA9700419Floor Pan · corrodedINSPECTION FOUND LEFT AFT LAV FLOOR PAN CORRODED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6.SDR CALA9700344Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 300, RBL 12 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700340Floor Support · brokenINSPECTION FOUND FLOOR SUPPORT BROKEN AT STA 758, BL ZERO. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
Back to N79750, cancelled Jan 24, 2018