N436UP
Service difficulty reports · 217
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 = 'N436UP' AND registry_match = 'registration' 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 = 'N436UP' AND registry_match = 'registration' 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 IPXA09557966Pump · malfunctionedINSPECTION TYPE:N/A DURING APPROACH THE NR 2 CENTER ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON. THE PUMP WAS NOT PRODUCING ANY PRESSURE. MAINTENANCE FOUND THE NR 2 ELECTRIC HYDRAULIC PUMP HAD OVERHEATED AND THERE WAS A STRONG BURNED ELECTRICAL SMELL SDR UPS08552370Skin · damagedINSPECTION TYPE:C LIGHTNING STRIKE AT FUSELAGE EXTERNAL SURFACE APPROX STA 1280, S2R. REMOVED 1EA RIVET IAW SRM 51-40-01 F 2. ENLARGED HOLE 0 UP TO .250 IAW SRM 53-00-01-2R6 SECTION II PARAGRAPH 3 3. HFEC IAW NTM 51-00-00 PT.6 FIG23. FOUND CRACK INDICATIONSDR UPS08552367Frame · dentedDENT IN BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1480 BETWEEN S25R AND S26R. DENT SIZE L:=.085", W=.059", D=.030". DENT LOCATION, FROM PRODUCTION SPLICE 4.5", FROM TRANSITION PANEL 10". REMOVED CLIP AT STA 1480 AND S25R AND LINER SUPPORT IAW SRM 51-40-02. SDR UPS08552369Frame · dentedDENTS IN AFT CARGO FUSELAGE FRAME STA 1340 APPROX BET S25L AND S26L (2EA). DENT SIZE NR 1 L=1.3 INCH, W=.75 INCH, D=.022 INCH. DENT SIZE NR 2 L=1.35 INCH, W=.8 INCH, D=.028 INCH. DENTS LOCATION IS 2.7 INCH FROM PRODUCTION SPLICE, 8.1 FROM TRANS PNL. CUTOUTSDR UPS08552368Frame · dentedDENT IN AFT CARGO FUSELAGE FRAME STA 1320, BETWEEN S25R AND S26R. DENT SIZE L = 1.5", W=.80", D= .030" DENT LOCATION: 6.10" FROM PRODUCTION SPLICES 7.15" FROM TRANS PNL 2. CUT OUT DAMAGE AREA DIMENSIONS L=1.51 INCH, W=1.40 INCH, IAW SRM 53-07-2R5 STEP NR 1 DSDR UPS06548178Engine · stalledAIR TURN BACK, LT ENG. EXPERIENCED APPROX. 5 COMPRESSOR STALLS IN APPROX 5 SECONDS. PASSING 1,300 FT. SHORTLY AFTER SELECTING V-NAV S SWITCHING FROM T/O TO CLB THRUST. EGT OVERTEMPED (RED) WENT TO 907 PEAK TEMP. ENGINE STABILIZED AND OPERATED NORMALLY WITH THRSDR UPS06548170Engine · stalledLEFT ENGINE ON T/O STALLED AND EGT LIMIT WENT TO AROUND 855C FOR 7 SECS. ATB WAS ACCOMPLISHED. ACCOMPLISHED ALL STEPS OF POWERPLANT INSP AFTER A SURGE PER MM 71- 32-00/101 FIG 103. REMOVED AND REPLACED BVCU REF LP 532320, I2 AND TPCU REF LP 542316, I2. ACCSDR UPS06546799Bearing · corrodedL/MLG AFT TRUNNION BEARING IS CORRODED IN THE RACE. REMOVED AND REPLACED L/MLG AFT TRUNNION BEARING IAW MM 57-07-4.SDR UPS06546798Bearing · corrodedR/MLG AFT TRUNNION BEARING IS CORRODED IN THE RACE. REMOVED AND REPLACED R/MLG AFT TRUNNION BEARING IAW MM57-54-07-4 STEP 4 C (1)-(9) AND STEP 5F(1)-(11).SDR UPS06546785Bearing · corrodedFOUND L/MLG AFT TRUNNION BEARING IS CORRODED IN THE RACE. REMOVED AND REPLACED L/MLG AFT TRUNNION BEARING IAW MM 57-07-04.SDR UPS06546784Bearing · corrodedRT MLG AFT TRUNNION BEARING IS CORRIDED IN THE RACE. REMOVED AND REPLACED RT MLG AFT TRUNNION BEARING IAW MM 57-54-07-4 STEP 4.C. (1)-(9) AND STEP 5F (1)-(11).SDR UPS06546245Thrust Reverser · delaminatedRT INBD T/R DELAMINATED.SDR UPS03541632Skin · crackedMAIN CARGO DOOR HAS A DAMAE SKIN AFT UPPER CORNER BEHING AFT ACTUATOR. REPAIRED DAMAGED SKIN ON MCD AFT UPPER PER SRM 52-30-01-2.SDR UPS01535010Gearbox · failedINSPECTION TYPE:N/A, ON TAKEOFF OUT OF 2000 FEET, THE LEFT ENGINE LOST OIL PRESSURE. MAINTENANCE VERIFIED THAT HIGH SPEED GEARBOX DRIVE FOR OIL PUMP FAILED. SUSPECT INTERNAL GEARBOX MALFUNCTION. REMOVED AND REPLACED ENGINE.SDR UPS99528368Seat Track · crackedINSPECTION TYPE:S-1 CRACKED SEAT TRACK FLANGE AT BS 1010, RBL 16, WL 156. REMOVED CRACKED SEAT TRACK SECTION FROM BS 950-BS 1010 RBL 16, WL 156. INSTALLED NEW SEAT TRACK PER SRM 51-10-1.SDR UPS98527486Bulb · failedINSPECTION TYPE-N/A, EN ROUNTE DID A LIGHT TEST AND OBSERVE RIGHT MAIN GEAR LIGHT INOP. CALLED MMOC TO CHANGE LIGHTS AND OBSERVED BOTH MAIN GEAR LIGHTS WERE INOP. DID A FLY-BY IN DSM. AIRCRAFT NEEDS SPARE BULBS (387). BITE PSEU AND FOUND NO FAULTS. REMOVSDR UPS502663Ldg Lever Module · malfunctionedPILOT REPORTED, PUT GEAR DOWN TO LAND IN ONT. NO RT GEAR DOWN INDICATION LIGHT. PRESS TO TEST AT BULB, WOULD NOT WORK. TEST SWITCH ON OVERHEAD PANEL WAS PUSHED. DID GO AROUND. CYCLED GEAR 4 TO 5 TIMES. DID NOT HELP. DID EMER GEAR CHECK LIST. DID NOT HE
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