N864RW
Service difficulty reports · 183
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 = 'N864RW' 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 = 'N864RW' 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 UHLA2012070800211Girt Bar · out of positionL1 DOOR HARD TO CLOSE AND ARM. FOUND GIRT BAR OUT OF HOLES, RE-INSTALLED PER EMB 170 MM 52-13-41. ARM OPERATION NORMAL, OPS CHECK GOOD IAW EMB 170 MM 52-11-20.SDR UHLA2011122100461Structure · corrodedMAJOR REPAIR - CTR SEAL REST LEVEL 2 CORROSION ON FWD CARGO DOOR LOWER BEAM. REMOVED CORRODED SEAL REST AND INSTALLED NEW SEAL REST IAW EMB 170 SRM 51-40-02, 51-41-01, AND 51-21-00.SDR UHLA2011121400448Skin · dentedMAJOR REPAIR - FOUR DENTS BETWEEN FR9-11 JUST ABOVE STR 17L. REMOVED PAINT FROM AREA IAW EMB 170 SRM 51-23-02, RECONTOURED SKIN AT FR10L, FOUND SKIN OIL CANNING. CUT AND REMOVED DAMAGED AREA IAW EMB 170 SRM 53-10-01 ABD 51-75-12. PERFORMED HFEC, NO CRACKLIKSDR UHLA2011121400445Beam · corrodedLEVEL 2 CORROSION AFT WET AREA RT BEAM, CORRODED 6 INCHES AFT OF FRAM 86. REMOVED AND REPLACED BEAM IAW EMB 170 SRM 51-43-01 AND 51-41-01.SDR UHLA2011121400444Structure · corrodedLEVEL 2 CORROSION LT AFT WET AREA BETWEEN FR85 AND 86. REMOVED AND REPLACED UPPER SHEET IAW EMB 170 SRM 51-41-01 AND 51-43-02.SDR UHLA2011121400443Gusset · corrodedLEVEL 2 CORROSION FR90 IN AFT WET AREA, OUTBOARD LT AND RT AREAS. REMOVED AND REPLACED RT GUSSET AT FR90 AND CLEANED AND RESTORED TOP COAT AT ALL OTHER AREAS ON FR90 IAW SRM 51-41-02 AND 51-23-06.SDR UHLA2011121400441Panel · corrodedLEVEL 2 CORROSION AFT WET AREA WEBBINGS, LEFT, RIGHT, AND CENTER PORTIONS AND AROUND BOLT HOLES. REMOVED AND REPLACED RIGHT AND CENTER SHEAR PANELS, RESTORED TOP COAT ON LEFT SHEAR PANELS IAW EMB 170 SRM 51-41-01, 51-42-01, AND 51-43-03.SDR UHLA2011121300464Shear Web · corrodedLEVEL 2 CORROSION AROUND SEVERAL AREAS OF LT SHEAR WEB. REMOVED AND REPLACED SHEAR WEB IAW EMB 170 SRM 51-43-04, 51-46-02.SDR UHLA2011121300447Floorbeam · corrodedLEVEL 2 CORROSION ON FLOORBEAM AT LT FR17. REMOVED AND REPLACED FLOORBEAM IAW EMB 170 SRM 51-41-01 AND 51-43-01.SDR UHLA2011121300446Shear Web · corrodedLEVEL 2 CORROSION AROUND FASTENER HOLES ON FWD GALLEY RT SHEAR WEB (FWD OF R1 DOOR). REMOVED AND REPLACED SHEAR WEB FWD OF R1 DOOR IAW EMB 170 SRM 51-40-02, 51-41-02, 51-41-02, 51-42-02, 51-43-02, AND 51-43-04.SDR UHLA2011121300442Floorbeam · corrodedLEVEL 2 CORROSION AT RT FLOORBEAM BETWEEN FR12-13. REMOVED AND REPLACED FLOORBEAM IAW EMB 170 SRM 51-41-01, 51-41-02, 51-43-01, AND 51-43-02.SDR UHLA2011081800271Power Unit · inoperativeEMERGENCY LIGHT ABOVE ROW 9 INOP. FOUND EMERGENCY LIGHT POWER UNIT IN RT AFT FUSELAGE INOP. REMOVED AND REPLACED RT AFT EMERGENCY LIGHT POWER UNIT IAW EMB 170 MM 33-50-01. OPS CHECK NORMAL.SDR UHLA2011021200078Shaft · obstructedR2 DOOR DIFFICULT TO ARM/DISARM. F/A STATES IT FEELS LIKE IT'S HANGING UP WHEN MOVING LEVERS. UPON INSPECTION OF LINKS AND RODS, REMOVED DEBRIS AND LUBRICATED CONNECTING ROD CABLE SHAFT ON ARM/DISARM LINK TO GIRT BAR AS REQUIRED. OPS CHECK GOOD.SDR 2010F00104Bushing · crackedPROBLEM FOUND ON AIRCELLE THRUST REVERSER REMOVED FROM ACFT, UPON PRELIMINARY INSPECTION AT APPLIED COMPOSITES ENGINEERING (ACE) IT WAS DISCOVERED THAT THE FWD HINGE BUSHING P/N 14G0311-203 WAS CRACKED ACROSS THE SHOULDER AND AROUND THE TRANSITION FROM THE RADSDR UHLA2010030300030Tripler · damagedMAJOR REPAIR - PREVIOUS REPAIR OF DENT BETWEEN FR24 AND FR25 AND STR 18L AND STR 19L HAS TOOLING MARKS ON TRIPLER AND RII NOT PERFORMED ON ORIGINAL REPAIR. REMOVED ORIGINAL REPAIR DOUBLERS IAW EMB 170 SRM 53-21-01 AND 51-41-02. HFEC OF DAMAGE CUT OUT IAW NDTSDR UHLA2010030300022Skin · dentedDENT ON LT CTR FUSELAGE I APPROX 12 INCHES BELOW 'U' IN 'OPERATED BY SHUTTLE AMERICA' LOGO. DENT IS 1.75L X 1.5W X .085D. DENT IS BETWEEN FR24 AND FR25 AND BETWEEN STR 18L AND STR 19L. MANUFACTURED NEW TRIPLER FROM 2024-T3 .050 IAW EMB SRM 53-21-01. ALODINSDR UHLA2010022600020Seat Track · corrodedLEVEL 2 CORROSION LEFT FWD SEAT TRACK, 37 IN BACK, 54 IN, 64 IN BACK. PERFORMED REPAIR IAW EMB ETD 2010-170/01383. NDT PERFORMED.SDR UHLA2010022300016Shear Plate · corrodedLEVEL 2 CORROSION ON RT SHEAR PLATE BETWEEN FR 87 AND FR 88. REMOVED AND REPLACED RT SHEAR PLATE IAW EMB SRM 51-42-01 AND 51-43-01.SDR UHLA2010022600015Seat Track · corrodedLEVEL 2 CORROSION RIGHT FWD SEAT TRACK BEAM, 23, 33, 41, 47, AND 54 INCHES AFT ON BEAM. REMOVED AND REPLACED RIGHT FWD SEAT TRACK IAW EMB SRM 51-41-02.SDR UHLA2010022300019Shear Plate · corrodedLEVEL 2 CORROSION LT SIDE OF LT SHEAR PLATE CORRODED BETWEEN FR 87 AND FR 88. REMOVED AND REPLACED SPLICE IAW EMB 170 SRM 51-40-02 AND 51-42-01.SDR UHLA2010022300018Seat Track · corrodedLEVEL 2 CORROSION LT SEAT TRACK BEAM CORROSION AT FR 90 GUSSET. REMOVED AND REPLACED GUSSET IAW EMB 170 SRM 51-40-02 AND 51-41-02.SDR UHLA2010022300017Shear Plate · corrodedLEVEL 2 CORROSION LT SHEAR PLATE BETWEEN FR 87 AND FR 88 IN AFT LAV/GALLEY AREA. REMOVED AND REPLACED LT SHEAR PLATE IAW EMB 170 SRM 51-31-00, 51-40-02, 51-43-01 AND 51-42-01.SDR UHLA2010022300014Gusset · corrodedLEVEL 2 CORROSION WASTE TANK HOLD DOWN GUSSET AT FR 90. REMOVED AND FABRICATED NEW GUSSET PER EMB 170 SRM 51-31-00 AND EMB 170 SRM 51-41-01.SDR UHLA2010022300013Seat Track · corrodedLEVEL 2 CORROSION RT SEAT TRACK BEAM, BETWEEN FR 84 AND 87. REMOVED AND REPLACED UPPER SHEET OF SEAT TRACK BEAM PER EMB 170 SRM 51-40-02 AND INSTALLED PER EMB 170 SRM 51-41-01.SDR UHLA2010022300012Gusset · corrodedLEVEL 2 CORROSION RT FLOORBEAM GUSSET, FWD OF AFT AVIONICS RACKS AT FR 90. REMOVED AND REPLACED GUSSET PER EMB 170 SRM 51-41-01.SDR UHLA2010022200029Beam · crackedMAJOR REPAIR - CRACK FOUND ON NLG I-BEAM ON FWD SIDE OF I-BEAM. REMOVED DAMAGED I-BEAM AND INSTALLED SERVICEABLE UNIT PER EMB IC2008-170/08207 AND SB 170-53-0055.SDR UHLA2010022200021Beam · crackedCRACK FOUND ON NLG I-BEAM, ON FWD SIDE OF I-BEAM, SHOWN IN FIG 2 OF SE531012. REMOVED DAMAGED I-BEAM ASSY PER EMB SRM 51-43-03. INSTALLED I-BEAM PER EMB SRM 51-43-03.SDR UHLA2009101100068Actuator · failedDURING APPROACH SELECTED FLAPS 1 AND RECEIVED `FLAP FAIL` EICAS MESSAGE. RAN QRH FOR NO FLAPS AND SLATS 3. DECLARED EMERGENCY. LANDED WITH 0 FLAPS. MAINTENANCE RELEASED ELECTRONIC BRAKE, CLEARED INHIBITS, AND OPS CHECKED GOOD. SI275042 WAS COMPLIED WITH 10SDR UHLA2009082400055Autopilot Sys · malfunctionedAT CRUISE FL370, THE AUTO PILOT FAILED WITH THE ASSOCIATED A/P FAIL CAUTION EICAS MESSAGE. ABOUT 3-4 SECONDS LATER THE SHAKER ANTICIPATED EICAS CAUTION APPEARED AND THE SHAKER BEGAN TO ENGAGE. ATC WAS NOTIFIED OF THE FAILURE, DESCENDED TO FL280. RAN QRH PROSDR UHLA2009080400054Light · malfunctionedAFTER FLIGHT ATTENDANT TESTED EMERGENCY LIGHTS, LIGHTS WOULD NOT TURN OFF. RECEIVED EMER LT BATT FAULT ON EICAS. UPON MAINTENANCE ARRIVAL TO AIRCRAFT, FOUND EMERGENCY LIGHTS IN CHARGING CYCLE. FAULTS CLEARED AND SYSTEM CHECKED NORMAL IAW EMB 170 MM 33-50-00SDR UHLA2008110700003Engine · malfunctionedFLIGHT 5952 ATL-HPN ON FINAL APPROACH WITH GEAR DOWN AND FLAPS AT NR 5 POS, NR 2 ENG SPOOLED UP TO 80% UN-COMMANDED. CREW SHOT MISSED APPROACH. ON SECOND APPROACH AND SAME THING HAPPENED. CREW SHUT DOWN ENGINE. CREW DID NOT RECEIVE ANY MESSAGES IN AIR OR ON GRSDR 200607311Warning Light · illuminatedFLIGHT 6453 LGA TO DFW ON CLIMB OUT CREW RECEIVED "BLEED 1 OVERPRESSURE" EICAS AMBER MESSAGE FOLLOWED BY "BLEED 1 LEAK" MESSAGE AND BLEED 1 BUTTON AMBER ILLUMINATION. CREW FOLLOWED QRH, AND DIVERT TO IAD. MTX VERIFIED NO ACTUAL LEAK THROUGH CMC. ONLY INDICSDR 200606162Sensor · faultyFLIGHT 6445 AUS TO SLC CREW RECEIVED A MASTER WARNING OF AFT CARGO DOOR OPEN, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE DOOR, DETERMINED DOOR SENSOR TO BE FAULTY. MEL THE DOOR INDICATION AND DEPARTED WITH NO FURTHER INCIDENT. NO PARTS
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