N346UP
Service difficulty reports · 23
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 = 'N346UP' 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 = 'N346UP' 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 IPXA2026061094710Handle · inoperativeMAIN ENTRY DOOR LOCK IS LOOSE WHEN LOCKING AND UNLOCKING FROM THE INSIDE. TIGHTEND SECONDARY CAPTURE HANDLE BOLT IAW AMM 52-12-25. PERFORMED OPERATIONAL CHECK OF DOOR IAW AMM 52-12-00. DOOR OPERATED NORMALLY.SDR IPXA2026030497959Aoa · faultedATB, ON CLIMBOUT CAPT SIDE AIRSPEED WAS ABOVE CLEAN MAN BUT EICAS SHOWED AIRSPEED LOW F/O SIDE NORMAL. GOT STICK SHAKER WITH NORMAL AIRSPEED BOTH F/D VERTICAL GUIDANCE WENT AWAY. ONCE LEVELED OFF A/C WAS€¦. REMOVED AND REPLACED LEFT AOA SENSOR IAW AMM 34-12-0SDR IPXA2025062521798Angle · brokenBROKEN - ANGLE, AFTER CARGO DOOR FORWARD LINK AREA (REPLACE) FORMED THE JOGGLES OF THE REPAIR ANGLE I.A.W. EGAT EI NO. F2025A52M-1318 SEQUENCE A STEP 1.C (FORMED THE JOGGLES OF THE REPAIR ANGLE, REFER TO 143T6482-5 DRAWING REQUIREMENTS.) REV.0 REPAIR DAMAGE ASDR IPXA2025070304712Lever · deformedFOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE (REPLACE) INSTALLED DOORWAY LINING I.A.W AMM 52-12-02-404-025 REV. 145.SDR IPXA2025062601105Filler · corrodedFOUND THE PLATE WITH CORROSION DAMAGE AT STA 1601 LBL 59 IN BULK CARGO COMPARTMENT CEILING AREA. (REPLACE) 1. FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH7 REV."-"; PL REV."AA" AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 11 REQUIREMENT 2. INSTSDR IPXA2025061904712Hinge · deformedFOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE (REPLACE)SDR IPXA2025061901689Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-105 PANEL NO : 231AFF STA 412 ~ STA 530 RBL 11 ~ LBL 11 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001, AMM 25-58-01-004-014, AMM 25-58-03-004-001, AMM 25-58-03-404-031 AND AMM 25-57-03-00SDR IPXA2025061901603Floor Panel · crackedFOUND MAIN DECK CARGO FLOOR PANEL WITH CRACK DAMAGE, P/N : 143T5864-89 PANEL NO : 251XFF (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145. REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMALSDR IPXA2025061901749Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-99 PANEL NO : 231FFF STA 530 ~ STA 654+22 LBL 11 ~ RBL 11 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-03-004-001, AMM 25-57-90-024-010, AMM 25-58-01-004-014, AMM 25-58-03-004-001 AND AMM 25-58-03-SDR IPXA2025061901844Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-111 PANEL NO : 232FFF STA 530 ~ STA 654+22 RBL 11 ~ RBL 33 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-03-004-001, AMM 25-57-90-024-010, AMM 25-58-01-004-014, AMM 25-58-05-004-021 AND AMM 25-58-05SDR IPXA2025061901724Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-103 PANEL NO : 232AFF STA 412 ~ STA 530 RBL 11 ~ RBL 33 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-03-004-001, AMM 25-57-05-004-001, AMM 25-57-08-004-015, AMM 25-58-01-004-001 AND AMM 25-58-01-00SDR IPXA2024070873240Lamp · inoperativeDURING PDC, FOUND EXTERIOR EMERGENCY LIGHT INOP RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.SDR IPXA2023052877635Battery · no test*** SUPPLEMENTAL SDR *** FAULT - FOUND EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAIL (REPLACE) 1. I.A.W AMM 33-51-07-022-001 & 33-51-07-422-012 REV.139.01 REPLACED EMERGENCY LIGHT BATTERY PACK & PERFORMED INSTALLATION TEST OF THE BATTERY PACK, THE RESULT WASSDR IPXA2023052277635Unknown · unknown*SDR FILED OPEN* FAULT - FOUND EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAIL (REPLACE)SDR IPXA2022100486839Fan · odorFWD EQ EXH FAN STATUS FAUL ODOR IN COCKPIT. DEFERRED IAW MEL # 21 58 4 2 1 DMP C/W.R/R FWD EQUIP COOLING EXIT FAN PER AMM 21-58-06-004-133 & 21-58-404-146. LEAK CK AND OPS CK GOOD. ORIG SUB DATE: 10/5/2022SDR IPXA2018062030876Fmc · lockedBOTH FMC'S LOCKED UP. AIR TURNBACK. ACCOMPLISHED FIM PROCEDURE 815-854. FAULT CORRECTED.SDR IPXA2016040101497Eec · inoperativeEGT INDICATES BLANK OR ABNORMAL OTHER ENGINE INDICATIONS NORMAL. R & R NR 2 ELECTRONIC ENGINE CONTROL IAW AMM 73-21-15-401. OPS CHECKS GOOD IAW AMM 71-00-00-725-268-H03.SDR IPXA2016031100633Seal · leakingI.T. ISS BY L1 DOOR STARTED AT 8000FT DIFFICULTY IN YELLOW .87 CABIN ALT 6200, DIFFICULTY ALT 6200 DIFF AT FL 210 NOISE STOPPED, DIFFICULTY ALT 4KFOUND PRESSURE SEAL OFF TRACK AT LOWER SECTION OF THE DOOR REPOSITIONED. THE SEAL IAW AMM 52 09 01SDR IPXA2016030800493Skin · damagedLEFT INBD AFT FLAP LOWER SKIN DAMAGED, REPAIRED IAW EP B767-5750-59435-C.SDR IPXA2016020598932Seal · leakingCREW ENTRY DOOR: CREW ENTRY DOOR HAS NOISE FROM AIRLEAK. LEAK SEEMS TO BE IN THE AREA NEAR THE BOTTOM OF THE DOOR. INSTALLED LOOSE SEAL AT BOTTOM OF CREW ENTRY DOOR IAW MM 52-09-00. PRESSURIZED ACFT TO LESS THAN 2 PSI COULD NOT DUPLICATE LEAK.SDR IPXA2014092984467Wedge · damagedNR 9 SLAT T/E WEDGE DAMAGED AT APPROXIMATELY OSS 682.74. REPAIRED IAW EO 5750-55602-A.SDR IPXA2014092984466Skin · damagedNR 10 SLAT T/E WEDGE, UPPER SKIN DAMAGED AT INBD AFT CORNER. REPAIRED IAW EO B767-5750-55629-A.SDR IPXA12671000Warning Light · false activationINSPECTION TYPE:ETOP ATB FORWARD EQUIPMENT OVERHEAT EICAS MESSAGE DISPLAYED AND OVERHEAT LIGHT ILLUMINATED. COMPLETED FIM 21-58-00, FIG 116. NO FAULTS FOUND.
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