N831US
Service difficulty reports · 73
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 = 'N831US' 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 = 'N831US' 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 Y2PA2025061825006Skin Splice · corrodedDISCREPANCY: WHILE AT C-CHECK IN KBQK, STAMBAUGH AVIATION FOUND CORROSION ON THE L/H WING LOWER SURFACE AT STR. 17 (SKIN SPLICE) AND AT XCW 85. BLENDED OUT THE DAMAGED AREA, PERFORMED HFEC OPEN HOLE INSPECTION AND FABRICATED A REPAIR DOUBLER USING 2024T3 .12SDR Y2PA2022090622047Skin · corrodedDISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, CORROSION FOUND ON FUSELAGE SKIN INTERNAL DOUBLER AT DRAIN VALVE MOUNTING SURFACE AT STATION 157 SDR Y2PA2022090622046Flap · corrodedDISCREPANCY: : DURING C-CHECK AT COMMERCIAL JET IN KDHN, EXFOLIATION CORROSION FOUND ON RH WING INBOARD FLAP AT APPROXIMATELY XRS 69 INNER SURFACE EMANATING FROM UNDER RIB JUST BELOW 3RD FROM INBOARD FLAP VANE MOUNT SDR Y2PA2022090622045Latch · crackedDISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, THE MAIN CARGO DOOR LATCH BASE LUG FITTINGS 3,4,5,6 AND 7 WERE FOUND TO BE CRACKED AT FASTENER HOLES DURING THE ACCOMPLISHMENT OF AD 2004-11-07 (PSE 52.80.FC3) HFEC INSPECTION OF THE MAIN CARGO DOOR LATCH SDR Y2PA2018070900024Duct Clamp · brokenCREW REPORTED, AT 29,000 TAIL COMPARTMENT HIGH ANNUNCIATOR ILLUMINATED. RAN RED BOARDER CHECKLIST. WHEN CREW CONTINUED THE COM PROCEDURE AND GOT TO THE REDUCE THRUST” DECLARED THE EMERGENCY AND RETURNED TO KLRD. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ATSDR Y2PA2016083100022Motor · failedCREW REPORTED PASSING THROUGH 4000 FT DURING CLIMB AND ACCELERATING FROM 200 TO 250 KTS. HAD TO PUSH HARDER ON THE YOKE TO KEEP THE NOSE FROM RISING. TRIED YOKE TRIM CONTROL WAS INOPERATIVE. TRIED SUITCASE HANDLES, THEY WERE INOPERATIVE. REACHED 5000 FT, RESDR Y2PA20160304009Longeron · crackedDURING C-CHECK, FOUND A CRACK AND CORROSION FOUND ON LONGERON 30 BETWEEN STA 237 AND 232. A REPAIR WAS DONE IAW SRM 51-10-4. PAGES 1-11, 51-30-2 AND 51-30-5 PAGES 1-22, REV 116, 8/15/15.SDR Y2PA20160304008Longeron · corrodedDURING C-CHECK FOUND CORROSION ON LONGERON 30C BETWEEN BS 1231 AND 1250. A REPAIR WAS DONE IAW SRM 53-02, PARA 13, PAGES 57-58E, REV 116.SDR Y2PA20160304007Door Frame · corrodedDURING C-CHECK, FOUND CORROSION AT ELECTRONIC EQUIPMENT BAY DOOR JAMB AND FORWARD AND AFT FS 134 AND 160, STR 27L AND 27R. A REPAIR WAS DONE IAW J2 ENGINEERING, INC. DOCUMENT J2R-0024 REV. IR DATED 22 FEB 2016, FAA APPROVAL IAW 8110-3.SDR Y2PA20160304006Cusp Web · corrodedDURING C-CHECK FOUND THE LOWER CUSP OF THE R1 DOOR HAD MINOR CORROSION NEAR THE FORWARD EDGE AT FLOOR LEVEL THAT WAS BLENDED TO REMOVE CORROSION. A REPAIR WAS DONE IAW J2 ENGINEERING, INC. DOCUMENT J2R-0023,
REV IR DATED 22 FEB 2016, FAA APPROVAL.SDR Y2PA20141212048Ground Wire · looseSMOKE AFT CABIN AREA & TEMP HOT. UPON TAKEOFF CREW NOTICED AN ODD SMELL. UNSURE IF THEY SMELLED DE-ICING FLUID OR NOT. TEMP IN BOTH CABIN & SUPERNUMERARY AREA STARTED TO NOTICEABLY INCREASE. SHORTLY AFTER PHYSICALLY SAW SMOKE IN SUPERNUMERARY AREA. DECLARSDR Y2PA20140312004Limit Switch · unstableMAIN CARGO DOOR ANNUNCIATOR ILLUMINATED AT 330. ENROUTE AT FL330, LEVEL FLIGHT, THE RED MAIN CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED TO ATC AND DESCENT/DIVERSION WAS INITIATED. EMERGENCY COM PROCEDURES WERE PERFORMED, ACFT GAVE NSDR Y2PA20140312003Limit Switch · unstableCARGO DOOR WARNING LIGHT AND LATCH LOCK PINS NOT ENGAGE LIGHT ILLUMINATED ENROUTE. CREW REPORTED DURING CRUISE , 350 LEVEL, MASTER CAUTION FOR MAIN CARGO DOOR ILLUMINATED WITH DOOR LATCH LOCK PINS NOT ENGAGED, AMBER LIGHTS. PERFORMED EMERGENCY DESCENT IAW COSDR Y2PA20131201055Battery Pack · inoperativeDURING SERVICE CHECK, COCKPIT/ENTRY EMERGENCY LIGHTS FOUND INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHTING BATTERY PACK IAW AMM 33-52-0. SYSTEM OPS CHECKED GOOD IAW AMM 33-52-0.SDR Y2PA20131107054Proximity Switch · failedCREW REPORTED MAIN CARGO DOOR ANNUNCIATOR ILLUMINATED WHILE BEING VECTORED AND DURING DESCENT. PERFORMED EMERGENCY PROCEDURE AND DECLARED AN EMERGENCY. APPROACH AND LANDING WERE CONDUCTED WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED A BAD AFT LATCH LOCK PSDR Y2PA20130808050Pin · shortCREW REPORTED THAT THE MAIN CARGO DOOR WARNING ILLUMINATED ON ARRIVAL INTO DESTINATION. PERFORMED COM PROCEDURE AND DECLARED AN EMERGENCY. PERFORMED A NORMAL APPROACH AND LANDING WITHOUT FURTHER INCIDENT. R & R THE CARGO DOOR FORWARD LOCK PIN WITH A NEW PSDR Y2PA20130803049Switch · out of adjustCREW REPORTED THAT MAIN CARGO DOOR WARNING LIGHT ILLUMINATED DURING LEVEL FLIGHT AT FL350. PERFORMED EMERGENCY PROCEDURE, DECLARED AN EMERGENCY AND DIVERTED. PERFORMED A NORMAL APPROACH AND LANDING WITHOUT FURTHER INCIDENT. MX FOUND THE LATCH LOCK PIN NOT SDR Y2PA20130802048Throttle Switch · stuckCREW REPORTED THAT ACFT WAS LEVEL AT 16,000 FEET, MAINTAINING 250 KNOTS. WHEN CLEARED TO CLIMB, LT ENGINE THROTTLE WOULD NOT ADVANCE. MAXIMUM THRUST WAS APPROX 63 PERCENT N1. CREW DECLARED EMERGENCY, RETURNED TO DEPARTURE AND REQUESTED FIRE AND RESCUE STANDSDR Y2PA20130801045Skin · corrodedDISCOVERED CORROSION AT LT WINDOW FRAME BETWEEN BS 767 AND 788. MX BLENDED CORROSION AND VERIFIED REMAINING MATERIAL THICKNESS, PRIMED AND TREATED IAW DWG 53-13188, 8110-3.SDR 7AHR20130218001Skin · crackedCRACK IN WING SKIN AT NR 8 SLAT TRACK HINGED DOOR ACCESS PANEL 1289C AT WING STATION 286.6. REPAIR REQUIRED WAS OUTSIDE OF THE STANDARD SRM REPAIR SCHEME. ENGINEERING FIRM, FLIGHT VEHICLES CONSULTING PROVIDED A REPAIR SCHEME. FABRICATED, LAYED OUT NEW FASTESDR 7AHR201308002Skin · corrodedRIGHT AFT WING TO BODY FAIRING ACFT SKIN HAS EIGHT FASTNER HOLES WITH CORROSION. AFTER BLEND OUTS FOUND NUMEROUS FASTENER HOLES TO HAVE IN EXCESS OF 20 PERCENT MATERIAL LOSS. REMOVED PRE-EXISTING DOUBLER. FABRICATED A REPLACEMENT DOUBLER IAW SRM 53-04, FIG 57SDR 7AHR20130108001Seat Track · corrodedCORROSION ON SEAT TRACK BETWEEN BS 1174 AND 1200 AT LT LBL 24. DETERMIND TO BE OUT OF LIMITS. SEAT TRACK R & R IAW SRM 53-05, FIG 4F.SDR Y2PA20120624036Power Supply · inoperativeDURING MX, FOUND AFT RT OVERWING EXIT LIGHTS INOPERATIVE. R & R POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW 33-50-0.SDR Y2PA20120624035Power Supply · inoperativeDURING MX, FOUND FWD RIGHT OVERWING EXIT LIGHTS INOPERATIVE. R & R POWER SUPPLY. SYS OPS CHECKED GOOD IAW MM 33-50-0.SDR Y2PA20120618033Bulb · inoperativeDURING INSPECTION, MX DISCOVERED THE AFT EMERGENCY LIGHTS INOPERATIVE. MX R & R TWO OVERHEAD EMERGENCY LIGHT BULBS AND PERFORMED OPS CHECK IAW AMM 33-53-0. OPS CHECKED GOOD.SDR Y2PA20120510025Power Supply · inoperativeON SERVICE CHECK, FOUND EMERGENCY LIGHTS OVER L1 & R1 DOORS AND IN COCKPIT INOPERATIVE. MX R & R POWER SUPPLY. SYS OPS CHECKED GOOD IAW MM 33-50-0.SDR Y2PA20120418016Power Supply · inoperativeDURING SERVICE CHECK, FOUND EMERGENCY LIGHT POWER SUPPLY B5-100 INOPERATIVE. MX R & R THE EMERGENCY LIGHT POWER SUPPLY B5-100. SYSTEM OPS CHECKED GOOD IAW MM 33-50-0.SDR Y2PA20120418015Power Supply · inoperativeDURING SERVICE CHECK, FOUND FORWARD LT AND RT OVER WING EXIT LIGHTS INOPERATIVE. MX R & R THE EMERGENCY LIGHT POWER SUPPLY B5-103. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-50-0.SDR Y2PA20120418014Power Supply · inoperativeDURING SERVICE CHECK, FOUND L1 AND R1 EMERGENCY EXIT LIGHTS INOP. MX R & R THE EMERGENCY LIGHT POWER SUPPLY B5-205. SYSTEM OPS CHECKS GOOD IAW MM 33-50-0.SDR Y2PA2011092000022Reservoir · underservicedON LANDING ROLLOUT, THRUST REVERSER ACCUMULATOR LOW LIGHT CAME ON AROUND 100KTS. STOWED REVERSERS BY 60KTS, AND EXITED THE RUNWAY ON THE HIGH SPEED. WHEN EXITING THE HIGH SPEED ONTO THE REGULAR TAXI-WAY, LOST COMPLETE HYD PRESSURE FOR 45 SECONDS. ADVISED GROUSDR FOTR2016911104Floor Support · corrodedAFT CARGO LEFT FLOOR SUPPORT AT LBL 18 FROM BS. 1174- 1231. REPAIRED NR11104 FASI W/O 20169.SDR FOTR2016911107Floorbeam · corrodedAFT CARGO BAY FLOORBEAM BS 1183 IS CORRODED AT LBL 16- RBL 3. REPAIRED ON NR 11107 FASI W/O 20169.SDR FOTR2016910975Door Frame · corrodedAFT LOWER CARGO COMPARTMENT DOOR JAMB HAS CORROSION. REPAIRED ON NR 10975 FASI W/O 20169.SDR FOTR2016911083Door Frame · corrodedCENTER CARGO DOOR LOWER FRAMES AT STA. 621- 658. REPAIRED ON NR# 11083 FASI W/O# 20169.SDR FOTR2016911134Floorbeam · corrodedAFT CARGO CABIN FLOORBEAM AT STA. 1309 IS CORRODED AT RBL 20. REPAIRED ON NR 11134 FASI WO 20169.SDR FOTR2016911132Floorbeam · corrodedAFT CARGO COMPARTMENT, BS. 1309 CABIN FLOORBEAM IS CORRODED ON BOTTOM SURFACE LBL.16 TO RBL.16. REPAIRED ON NR 11132 FASI W/O 20169.SDR FOTR2016910976Door Frame · corrodedFWD LOWER CARGO DOOR JAMB HAS CORROSION, STA. 408- 427. REPAIRED ON NR 10976 FASI W/O 20169.SDR FOTR2016911059Floorbeam · corrodedFLOORBEAM SUPPORT ANGLES CORRODED STA 148- 200 BETWEEN LBL 60 AND RBL 60. REPAIRED ON NR 11059 FASI W/O 20169.SDR FOTR2016911140Seat Track · corrodedSEAT TRACK STA 1098 LBL 45 CORRODED. REPAIRED ON NR 11140 FASI W/O 20169.SDR FOTR2016911019Frame · corrodedFRAME STA. 1485 RT VERTICAL STIFFNER CORRODED. REPAIRED NR 11019 FASI W/0 20169.SDR FOTR2016911300Seat Track · corrodedSEAT TRACK FROM STA. 1036-1309 RBL. 55 IS CORRODRD. REPAIRED ON NR 11300 FASI W/O 20169.SDR FOTR2016911299Seat Track · corrodedSEAT TRACK FROM STA. 790-1036 RBL.55 IS CORRODED. REPAIRED ON NR 11299 FASI W/O 20169.SDR FOTR2016911293Cusp Web · crackedMAIN CABIN RIGHT CUSP WEB STA. 1265 RBL58. REPAIRED ON NR 11293 FASI W/O 20169.SDR FOTR2016910867Skin · corrodedLEFT WING O/B FLAP UPPER SURFACE XW 138-342 IS CORRODED. REPAIRED ON NR 10867 FASI W/O 20169.SDR FOTR1016911209Crease Beam · corrodedCREASE WEB STA 1140-1174 LBL 58 IS CORRODED. REPAIRED ON NR 11209 FASI W/O 20169.SDR FOTR2016911216Cusp Web · corrodedCUSP WEB STA 351- 411 CORRODED RBL 57. REPAIRED ON NR 11216 FASI W/O 20169.SDR FOTR2016911251Cusp Web · damagedRIGHT CUSP WEB STA 1079-1098 HOLES DRILLED IN WEB. REPAIRED ON NR 11251 FASI W/O 20169.SDR FOTR2016911285Attach Angle · crackedSEAT TRACK CLIP CRACKED AT STA. 905 RBL.54. REPAIRED ON NR 11285 FASI W/O 20169.SDR FOTR2016911284Seat Track · crackedSEAT TRACK CLIP CRACKED AT STA.886 RBL 54. REPAIRED ON NR 11284 FASI W/O 20169.SDR FOTR2016910869Skin · corrodedLEFT WING OUTBOARD FORE FLAP LOWER SURFACE HAS SURFACE CORROSION IN SEVERAL SPOTS XW 138-342.
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