N712PS
Service difficulty reports · 135
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 = 'N712PS' 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 = 'N712PS' 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 VNAA2024111090016Attach Angle · corrodedCORROSION FOUND ON RH OB ANGLE (ITEM 48) @ F.S. 879.00. (REFERENCE SRM 53-82-55-001-002-A01 SHEET 3 OF 5 ) FOR CLARIFICATION OF LOCATION. REMOVED UNSERVICEABLE R/H OUTBOARD ANGLE AND INSTALLED NEW SERVICEABLE R/H OUTBOARD ANGLE AT F.S. 879.00 P/N SH670-3932SDR VNAA202411090015Strap · corrodedCORROSION FOUND ON LH STRAP (ITEM 112) @ F.S. 847.00. (REFERENCE SRM 53-82-55-001-002-A01 SHEET 2 OF 5 ) FOR CLARIFICATION OF LOCATION. REMOVED AND REPLACED LH STRAP IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01, AND 51-40-11-001-001-A01.SDR VNAA202411090014Strap · corrodedCORROSION FOUND ON LH STRAP (ITEM 109) @ F.S. 847.00. (REFERENCE SRM 53-82-55-001-002-A01 SHEET 2 OF 5 ) FOR CLARIFICATION OF LOCATION. REMOVED AND REPLACED LH STRAP IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01, 51-42-21-001-001-A01, AND 51-40-1SDR VNAA202411090013Support Frame · corrodedFS 629 FWD WING TO BODY SUPPORT FRAME JOINT STRAP IS CORRODED. REMOVED AND REPLACED JOINT STRAP IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.SDR VNAA202411090012Hinge Box · gougedL/H FLAP HINGE BOX WS 264.00 HAS A GOUGE ON UPPER SURFACE JUST AFT OF OUTBOARD AFT ATTACH LUG. REPAIRED L/H FLAP HINGE BOX AT WS 264.00 IN ACCORDANCE WITH MHIRJ REO 670-57-54-067 REV-- DATED: 2024-08-27SDR VNAA202411090011Frame · corrodedFRAME SECTOR 364.00 HAS AREA OF CORROSION ON LOWER FLANGE FWD SIDE AT STR 27. REMOVED DEFECTIVE FRAME SH670-32090-7 AND REPLACED WITH NEW FRAME SH670-32090-9 AT FS364.00 STR27.00 AND COMPLIED WITH MHI RJ REO 670-53-21-687 REV.- B DATED 2023-04-10.SDR VNAA202411090010Intercostal · corrodedFS 349- FS 364 STR 26R OTBD INTERCOSTALCORRODED ON OTBD FWD SURFACE. INSTALLED NEW INTERCOSTAL PN# SH670-32077-4 (DIAPHRAGM) AT STR26R IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.SDR VNAA2024111090009Floorbeam · corrodedFOUND MOST FWD FLOORBOARD SUPPORT FOR FLOORBOARD 141ALF TO BE CORRODED AT FS 280. REMOVED AND REPLACED FWD FLOORBOARD SUPPORT FOR FLOORBOARD 141ALF WITH NEW SERVICEABLE (PN:CC670-34256-3) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR VNAA2024111090008Angle · corrodedFOUND RH CLIP ON FS 280 TO BE CORRODED. INSTALLED NEW SERVICEABLE RH CLIP AT FS. 280 POST IAW CRJ700 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.SDR VNAA2024111090007Angle · corrodedFOUND LH CLIP ON FS 280 TO BE CORRODED. INSTALLED NEW SERVICEABLE LH CLIP AT FS. 280 POST IAW CRJ700 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.SDR VNAA2024111090006Stringer · corrodedCORROSION FOUND ON STGR 20R BETWEEN FS 364.00-379.00. REMOVED AND REPLACED STGR 20R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.SDR VNAA202411090005Stringer · corrodedCORROSION FOUND ON STGR 20R BETWEEN FS 333.00-349.00. REMOVED DAMAGED STRINGER 20R SEGMENT BETWEEN FS 333 & 349 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PART PN SH670-32045-1 IAW CRJ 700 SRMSDR VNAA202411090004Stringer · corrodedCORROSION FOUND ON STGR 22R BETWEEN FS 333.00-349.00. REMOVED DAMAGED STRINGER22R SEGMENT BETWEEN FS 333 & 349 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PART PN SH670-31379-1S IAW CRJ 700 SRMSDR VNAA202411090003Plate · bentNLG DOOR HAS BENT PLATE LANDING ON THE FWD SIDE. REMOVED AND REPLACED PLATE LANDING IAW CRJ-700 SRM 51-42-10-001-001-A01, SRM 51-40-11-001-001-A01, SRM 52-81-02-001-001-A01, SRM 52-81-02-101-001-A01.SDR VNAA2024111090002Skin · scratchedTHE EXTERNAL SIDE OF THE FUSELAGE SKIN IS SCRATCHED AROUND THE PERIMETER OF THE AFT GPS ANTENNA LANDING. (BETWEEN FS 565 AND FS 581, STGR 0). REPAIRED IAW MHIRJ REO 670-53-31-927 REV-- DATED 2024-08-22.SDR VNA2024111000021Skin · scratchedTHE EXTERNAL SIDE OF THE FUSELAGE SKIN IS SCRATCHED AROUND THE PERIMETER OF THE AFT GPS ANTENNA LANDING. (BETWEEN FS 565 AND FS 581, STGR 0) REPAIRED IAW MHIRJ REO 670-53-31-927 REV-- DATED 2024-08-22.SDR VNAA2024111090001Beam · gougedAFT CARGO NET UPPER ATTACHMENT TOP SEAL HAS 2 AREAS THAT HAVE GOUGES. INSTALLED NEW SERVICEABLE PART MM670-35502-014S BEAM IAW CRJ700 SRM 51-42-21-001-001-A01SDR VNAA202205251111Skin · distortedEA22-C7-53-101 (PERM REPAIR - AERODYNAMIC FILLER LOOSE FUSELAGE SKIN FS 220) / FINISHED THE PERM REPAIR OF THE AERODYNAMIC SMOOTHNESS OF THE FUSELAGE SKIN AT FS220 IAW EA 21-C7-53-128 REV B INSTRUCTIONS AND SRM 51-12-00. THIS CLEARS THE PERM REPAIR NO FURTHER SDR VNAA2021040299915Hinge · crackedCRACK INDICATION DETECTED DURING NDT IN AFT INBOARD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING AT WS 128.00 LH WING. CRACK LOCATED .150" FROM SKIN SURFACE, .090" LENGTH, 040" DEEP.
COMPLETED REPAIR IN AFT INBD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING ATSDR VNAA202104029998Seat Track · corroded(NR0291) CENTER L/H SIDE SEAT RAIL BETWEEN STA. 485 TO 581 WITH NICKS, GOUGES AND LIGHT CORROSION. REPLACED L/H SEAT RAIL BETWEEN STA 485-581. IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03/ SRM 53-00-49-201-002-A01SDR VNAA2021040299914Rib · crackedR/H WING LEADING EDGE MACHINED RIB BETWEEN FIXED LEADING EDGE AND NO 1 SLAT HAS A CRACK AT THE UPPER AFT FLANGE. REMOVED & REPLACED MACHINED RIB BETWEEN FIXED LEADING EDGE NO 1 SLAT RH WING LEADING EDGE IAW CRJ-700 SRM 51-42-06 & 51-42-11.SDR VNAA202104029997Seat Track · corroded(NR0290) L/H SEAT RAIL BETWEEN STA 394 - 501 HAS SEVERAL AREAS OF NICKS, GOUGES AND CORROSION. REPLACED L/H SEAT RAIL BETWEEN STA 394-501. IAW CRJ 700 AMM 53-00-49-400-801 CONFIG A03/ SRM 53-00-49-201-002-A01SDR VNAA2021040299913Angle · corrodedANGLE UNDER PASSENGER DOOR THRESHOLD HAS SIGNS OF CORROSION. REMOVED AND REPLACED ANGLES (2 EA.) UNDER PASSENGER DOOR THRESHOLD IAW CRJ-700 SRM 51-41-21 & 51-42-06.SDR VNAA202104029996Seat Track · corrodedNR0289) R/H SEAT RAIL BETWEEN STA. 394 - 485 HAS SEVERAL AREAS OF NICKS, GOUGES AND CORROSION. INSTALLED R/H SEAT RAIL BETWEEN STA 394 - 485 IAW CRJ-700 SRM 53-21-49SDR VNAA2021040299912Floorbeam · corrodedCORROSION AT AFT BAGGAGE BY STA 1031, DOT 601 BLK ABOUT 12 INCHES IN FROM DOOR FRAME. REPAIR AT AFT BAGGAGE BAY STA 1031, ABOUT 12" . LBL9 PERFORMED IAW EA 21-C7-53-194.SDR VNAA202104029995Seat Track · corroded(NR0285) R/H SIDE SEAT RAIL BETWEEN STA. 379 TO 485 WITH SCRATCHES, GOUGES AND LIGHT CORROSION IN SEVERAL AREAS. INSTALLED R/H SIDE SEAT RAIL BETWEEN STA 379 TO 485 IAW CRJ-700 SRM 53-31-49.SDR VNAA2021040299911Floorbeam · corrodedCORROSION AT STA 1031 R.B.L9 DOT 604 BLK. PERFORMED AFT FLOOR BEAM SPLICE REPAIR AT STA 1031 IAW EA 21-C7-53-194 AND SRM 53-00-41.SDR VNAA202104029994Seat Track · corroded(NR0284) L/H SIDE SEAT RAIL BETWEEN STA 581 TO 677 WITH GOUGES, NICKS AND CORROSION IN SEVERAL AREAS. REPLACED L/H SEAT BETWEEN STA 581 TO 677. IAW CRJ-700 AMM 53-00-49-400-801. CONFIG A03 / SRM 53-00-49-201-002-A01.SDR VNAA202104029993Seat Track · corroded(NR0283) L/H SIDE SEAT RAIL BETWEEN STA. 501 TO 565 WITH NICKS GOUGES AND LIGHT CORROSION IN SEVERAL AREAS. INSTALLED L/H SIDE SEAT RAIL BETWEEN STA. 585 TO 581 IAW CRJ 700 SRM 51-41-02.SDR VNAA2021040299910Seat Track · corrodedLEFT SIDE SEAT RAIL FS' 669.40 TO FS977.00 HAS CORROSION, GOUGES AND SCRATCHES. ALONG WITH FASTENER MISSING. STGR15L. INSTALLED LEFT SIDE SEAT RAIL FS 669.40 TO FS 977.00 IAW CRJ700 SRM 51-41-02SDR VNAA202104029992Seat Track · corrodedINSTALLED L/H SIDE SEAT RAIL BETWEEN STA 319 TO 485 IAW CRJ-700 SRM 53-31-49.SDR VNAA202104029999Frame · corrodedBLENDED AND EVALUATED CORROSION AT FS 331 BETWEEN STR 27R AND 26R AND FLANGE WAS FOUND TO OUT OF LIMITS, IAW CRJ 700 SRM 53-00-06-201-005-A01. REMOVED CORRODED FLANGE AND REPLACED WITH FALSE FLANGE IAW CRJ 700 SRM 53-00-06, 51-40-11, 51-21-11, 51-25-01SDR VNAA202104029991Crossbeam · corrodedREMOVED AND REPLACED CROSS BEAN ANGLE SUPPORT AT FS 280 WL 72.50 IAW CRJ 700 SRM 51-42-06 AND 51-42-21SDR VNAA2020041611103Battery Pack · failedL/H MIDDLE EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND MULTIPLE ADDITIONAL LIGHTS OUT IN THE INTERIOR OF THE AIRCRAFT. SUSPECT #2 BATTERY ISSUES. TROUBLESHOT AND FOUND #2 BATTERY TERMINAL WITH POOR INTERNAL CONNECTION DUE TO FLUCTUATING OUTPUT VOLTAGE.SDR VNAA2020010951101Computer · failedWHILE FLIGHT 5277 DCA-RDU WAS EN-ROUTE MULTIPLE STATUS MESSAGES ILLUMINATED FO SIDE ATTITUDE INDICATOR BLANK, YAW DAMP 2 INOP S MSG, PITCH FEEL FAULT S MSG, RUDDER LIMIT FAULT S MSG, LEFT AND RIGHT FADEC FAULT 2. DUE TO THE MULTIPLE MESSAGES CREW DECLARED EMERSDR VNAA2019111911101Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT ILLUMINATE OR TEST WHEN THE FLIGHT ATTENDANT TESTS THEM. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES. (REMOVED PART NUMBER: 2013-1A (FOR ALL 4) / REMOVED SERIAL NUMBERS: POS 1: 495284 / POS 2: 121685 / POS 3: 503167 / POS 4: 79SDR VNAA2019062811101Warning Message · false activationDURING APPROACH TO CLT THE CREW RECEIVED A FLIGHT SPOILER CAUTION MESSAGE AND DECLARED AN EMERGENCY. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. PERFORMED SPOST 1 IAW CRJ 700 AMM TASK 27-61-05-740-802 OPS CK GOOD AT THIS TIME.SDR VNAA2019052811101Sensor · failedON CLIMBOUT CREW RECEIVED RED MASTER WARNING FOR BRAKE OVERHEAT.Ï¿½ CREW DECLARED EMERGENCY AND LEVELED OFF.Ï¿½ CREW BEGAN GOING THROUGH THE PROCEDURES IN THEIR QRH AND THE MESSAGE WENT AWAY, RETURNING 30 SECONDS LATER.Ï¿½ CREW DECIDED TO RETURN TO CAE TO BE SSDR VNAA2019052811102Warning System · false activationDURING APPROACH TO CAE THE CREW RECEIVED AN IB FLT SPLRS/IB SPOILERONS CAUTION MSG.Ï¿½ THE CREW DECLAREDÏ¿½ AN EMERGENCY .Ï¿½ TRUCKS ROLLED. NO BRACE.Ï¿½ AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. RESET SYSTEM, OPS CHECK GOOD.SDR VNAA2019041511101Warning Message · false activationIB FLT SPLRS/IB SPLRNS CAUTION MSGS ILUMINATAED ON DESCENT INTO PHL. RAN QRH, BOTH MSGS REMAINED "ON" IB FLT SPLRS/IBN SPLRNS CAUTION MESSAGES RECEIVED. THE FLIGHT LANDED AND TAXIED TO GATE WITHOUT INCIDENT. AS A PRECAUTION THE CREW DECLARED AN EMERGENCY. C/W SDR VNAA2018041211101Warning System · activatedON ARRIVAL INTO CLT THE CREW RECEIVED OUTBOARD SPOILERONS & OUTBOARD FLIGHT SPOILERONS CAUTIONS MSG AND DECLARED AN EMERGENCY. EMERGENCY VEHICLES DID RESPOND, LANDED ON 18C WITHOUT INCIDENT AND TAXIED TO GATE UNDER THEIR OWN POWER. MX C/W SPOST 2. OPS CHECKS GSDR VNAA2017122911101A/C Pack · failedCREW RETURNED TO GATE DUE TO DUE TO BOTH AIR-CONDITIONING PACKS FAILED AND HAD A LAV SMOKE MESSAGE. THE FLIGHT ATTENDANT REPORTED A STRONG SMOKE SMELL IN LAV AND CABIN AND AN EMERGENCY WAS DECLARED ON THE TAXI WAY AND PEOPLE WERE EVACUATED. MX PERFORMED AN OPSSDR VNAA2017053000013Windshield · crackedLEFT SIDE WINDSHIELD CRACKED IN FLIGHT; REMOVED AND REPLACED LEFT WINDSHIELD.SDR VNAA2017050100001Warning Message · illuminatedBRAKE OVERHEAT WHITE MESSAGE.SDR VNAA2017021300019Drag Angle · crackedVERTICAL STABILIZER TO RIGHT FUSELAGE FORWARD DRAG ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR.SDR VNAA2017021100016Bulkhead Web · corrodedLEFT BULKHEAD LOWER WEB AT BS 280 IS CORRODED BETWEEN RBL 11 TO 17. REPAIRED THE LEFT BULKHEAD WEB.SDR VNAA2017021100015Bulkhead Web · corrodedRIGHT BULKHEAD LOWER WEB AT BS 280 IS CORRODED BETWEEN RBL 11 & 17. REPAIRED THE BULKHEAD WEB.SDR VNAA2016101300014Quick Disconnect · disconnectedDURING FLAP RETRACTION ON CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 1 LOW PRESSURE CAUTION MESSAGE. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FOUND ENGINE DRIVEN PUMP 1 SUPPLY QUICK DISCONNECT AT THE LINE DISCONNECTED. MAINTENANCE RECONNSDR VNAA2016100400006Light · looseEMERGENCY LIGHT STRIP FOUND LOOSE. MAINTENANCE SECURED THE EMERGENCY LIGHT STRIP IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA2016030100004Brake · failedCREW REPORTED RECEIVING A RT OTBD BTMS MASTER WARNING AT FL160. DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE BRAKE ASSY. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERV
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