N930EV
Service difficulty reports · 151
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 = 'N930EV' 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 = 'N930EV' 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 SWIA202157111Handle · gougedAFT CARGO DOOR OUTER HANDLE IS GOUGED AT (4EA) LOCATIONS. (C-CHECK RO 4/1/2021) REMOVED DAMAGED DOOR HANDLE ASSEMBLY AND INSTALLED A NEW ASSEMBLY IAW CRJ 200 SRM 51-42-21. OPERATIONAL CHECKS AND PRESSURE CHECKS ARE GOOD. TASK CARD 51-900-1003-SKY AND M-33SDR SWIA202157109Retainer · damagedAFT CARGO DOOR SEAL RETAINER IS DAMAGED AT THE LOWER AFT CORNER. (C-CHECK RO 4/1/2021) REMOVED DAMAGED SEAL RETAINER AND INSTALLED ANEW SERVICABLE SEAL RETAINER IAW CRJ 200 SRM 51-42-06. NO CHANGE TO WEIGHT. PRESSURE CHECK AND OPERATIONAL CHECKS GOOD. TASSDR SWIA202157115Beam · corrodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA47138-601R-52-41-244 N930EV -PR - BLENDED CORROSION ON LWR AFT PAN OF SERVICE DOOR REF REO 601R-52-41-244 REV -- DATED 2016-12-27. PERFORM PERM REPAIR WITHIN 14000 FH FROM TIME OF INCORPORATION OF REV --, PART NUMBER: SDR SWIA202057142Bushing · not reportedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 4/1/2021) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 & REO_601R-57-51-941 REV.--SDR SWIA2019101146459Bracket · damagedGEAR DISAGREE. NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF. RAN QRH AND RETURNED TO ORD. NOSE WHEEL STEERING DID DISENGAGE MOMENTARILY DURING TAXI IN TO THE GATE. (FLT#5071) CLOSED REPLACED OLEO/CENTERING SENSOR BRACKET.SDR SWIA2019082746228Seal · failedON CLIMBOUT, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. RAN QRH PROCEDURES AND RETURNED TO ORD. REMOVED AND REPLACED NLG SLIDING MEMBER ASSY AND NLG FLOATING PISTON SEALS IAW AMM.SDR SWIA2019072546096Proximity Switch · faultyNOSE GEAR DID NOT COME UP AFTER TAKEOFF. FL 5270 CLOSED. REMOVED AND REPLACED NOSE LANDING GEAR WOW NR 2 AND CENTERED HARNESS ASSEMBLY AND CENTERED BRACKET.SDR SWIA2018121245310Skin · dentedDENT ON RH WING LEADING EDGE. (FLT#3110) FO: 11/30/2018. CLOSED C/W REO.SDR SWIA2018113045310Skin · dentedDENT ON RT WING LEADING EDGE. FLIGHT 3110. FO: 11/30/2018. CARRIED FORWARD FOR RESCHEDULING, TIME REMAINING UNTIL NEXT RE-INSPECTION IS DUE OR UNTIL PERMANENT REPAIR IS REQUIRED.SDR SWIA2018052444714Skin · crackedCRACK IN RIGHT AILERON. CRACK IS LOCATED ABOUT 1/4" IN FROM THE OUTBOARD END OF THE AILERON AND EXTENDS FROM THE TRAILING EDGE FORWARD ABOUT 2" ON THE UPPER SURFACE AND ABOUT 1 1/2" ON THE LOWER SURFACE. (FLT 3130) CLOSED COMPLIED WITH TEMP REPAIR IAW REO. AIRSDR SWIA2017101743870Proximity Sensor · bentGEAR DISAGREE NOSE GEAR WOULD NOT COME UP. ADJUSTED THE PROXIMITY SENSORS.SDR SWIA201743643Signal Cond Unit · failedRT ENGINE OIL PRESSURE FLUCTUATED DURING CRUISE, FLAGGING LOWER RED LIMIT. RT OIL PRESSURE WARNING ACTIVATED ONCE MOMENTARILY AT CRUISE. OIL TEMP LOWER THAN OTHER SIDE, DIVERTED. REMOVED AND REPLACED THE SIGNAL CONDITIONING UNIT & ENGINE OIL TEST PANEL IAWSDR SWIA201642852Target · out of rigGEAR DISAGREE ON RT MLG. GEAR WAS RETRACTED THEN MANUALLY EXTENDED. DECLARED AN EMERGENCY. ACFT LANDED SAFELY. FOUND THE RT UPLOCK MLG TARGET OUT OF RIG, RERIGGED AND OPS CHECKED GOOD.SDR SWIA201641807Warning Message · false activationLEFT 14TH DUCT MESSAGE OVERTEMP ON CLIMBOUT. CREW FOLLOWED QRH AND TOOK ENGINE TO IDLE. CREW DECLARED EMERGENCY. R & R BLEED DUCT INSIDE PYLON, OPS CHECKED GOOD. R & R LT PYLON SENSING ELEMENT IAW AMM. OPS CHECK GOOD.SDR SWIA201540733Mount · chafedLEFT THRUST REVERSER MAIN TRACK AFT MOUNT LUG AT 5 O'CLOCK IS CHAFED,C-CHECK RO 2/19/15. MEASURED DEPTH OF CHAFE DAMAGE. DAMAGE IS .046" AND FOUND TO BE BEYOND ALLOWABLE LIMITS, REF REO. R & R LT THRUST REVERSER MAIN TRACK AT 5 O`CLOCK POSITION REF AMM. WOSDR SWIA201540731Lug · chafedRIGHT THRUST REVERSER MAIN TRACK SUPPORT LUGS AT 7 O'CLOCK ARE CHAFED. C-CHECK, RO 2/19/15, EVALUATED RT T/R MAIN TRACK SUPPORT LUGS AT 7 O`CLOCK. CHAFE DAMAGE MEASURES .051. DAMAGE EXCEEDS LIMITS. REF REO. NEW THRUST REVERSER INSTALLED ON JOB 2801435, SDR SWIA201540740Bulkhead · crackedFS 621, BULKHEAD HAS 2 CRACKS AT LINTEL FITTING. C-CHECK, RO 2/19/15, REPAIRED FS 621 BULKHEAD LINTEL FITTING REF REO. NO LEAKS NOTED, COMPLIED WITH ST.SDR SWIA201540739Skin · dentedLOWER FUSELAGE SKIN HAS DENT AT FS 605.00 BETWEEN STR 25L AND 26L. PERFORMED PERMANENT REPAIR ON LOWER SKIN AT FS 605.00 IAW STS EA WORK DONE IN REF TO STS EA.SDR SWIA201540738Bulkhead Web · crackedFS 621, BULKHEAD WEB AT LBL 27.50 HAS CRACK AT TOP OF CARGO DOOR TRACK. C-CHECK, RO 2/19/15. REPAIRED CRACK AT FS 621, BULKHEAD WEB AT LBL 27.50, AT TOP OF CARGO DOOR TRACK REF REO.SDR SWIA201540735Structure · failedPAX DOOR CUTOUT HAS A BENT EXTRUSION NEAR THE FWD UPPER LOCKPIN HOLE, ON AIRCRAFT SIDE. C-CHECK, RO 2/19/15, COMPLIED WITH REO. TYPE I PERMANENT REPAIR.SDR SWIA201540734Structure · corrodedAFT CARGO HAS CORROSION AROUND NUT-PLATE HOLES AT FLOOR EDGE MEMBER LT SIDE AT FS 574.00 TO FS 621.0, C-CHECK, RO 2/19/15. BLENDED CORROSION ON AFT CARGO SILL AROUND NUT-PLATES HOLES AT FS574.00 TO FS621.0 REF AMM. ORIGINAL MATERIAL THICKNESS ON CARGO FLOORSDR SWIA201540732Track · chafedLEFT THRUST REVERSER HAS BOTTOM OTBD MAIN TRACK AFT END CHAFING MARK AGAINST BLOCKER DOOR. C-CHECK RO 2/19/15, REPAIRED LT THRUST REVERSER REF REO & SB CF-34-NEEDS PERFORMED, SB ACCOMPLISHED ON JOB 2801435, OP 101, CAMP11845915. DUE TO REO BEING TEMPORARY LTSDR SWIA201540737Skin · dentedRIGHT WING UPPER SURFACE HAS SMALL DENT IN BETWEEN THE SPOILERON AND FLIGHT SPOILER. C-CHECK, REPAIRED RT WING UPPER SURFACE SMALL DENT BETWEEN THE SPOILERON AND FLIGHT SPOILER, REF STS, EA STS EA. WORK DONE IN REFERENCE TO STS EA.SDR SWIA201540736Skin · dentedDENT AT FUSELAGE STA 606.0 BETWEEN STRINGERS L18 AND L19. FOUND DENT TO WITHIN LIMITS IAW REO. PERMANENT REPAIR DUE AT NEXT C-CHECK, COMPLETED PERMANENT REPAIR FOR DENT AT FUSELAGE STA 606.0 BETWEEN STRINGER L18 AND L19 IAW STS EA.SDR SWIA201439232Control Panel · failedAIRCRAFT THOUGHT IT WAS ABOUT 15,000 FT AT THE GATE AND DROPPED THE PAX OXYGEN MASKS. REMOVED AND REPLACED CPAM IAW AMM.SDR SWIA201439289Flap System · failedFLAPS FAILED AT 20, RETURN TO FIELD. RAN QRH. RESET FLAPS IAW FIM. RAN FLAPS FIVE FULL CYCLES. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES IAW AD.SDR SWIA201438595Battery Pack · inoperativeAFT EMERGENCY CEILING EXIT LIGHT INOPERATIVE. R & R NR 2 BATTERY PACK IAW AMM.SDR ASOA2014050710469Battery Pack · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES IAW AMM 25-60-00, NO FURTHER DEFECT NOTED.SDR ASOA2014040110260Battery · dischargedF/A FLASHLIGHT INTERMITTENTLY WORKING. REPLACED BATTERY IAW AMM 25-60-00. OK FOR SERVICE.SDR ASOA2013082608911Selector Valve · failedLOWERED GEAR HANDLE FOR LANDING, RECEIVED GEAR DISAGREE WARNING. BOTH MAIN GEAR FAILED TO EXTEND. RAN QRH. MANUAL EXTENSION SUCCESSFUL, EMERGENCY ACTIONS, R & R MLG EXTENTION AND RETRACTION SELECTOR VLAVE IAW AMM 32-32-10 AND IPC 32-32-10, FIG 1 ITEM 30. SDR ASOA2013060603774Skin · burnedFOUND ONE BURN BETWEEN FS 295 AND 280 BETWEEN STRG 26L AND 27L. DRILLED OUT DAMAGE TO A NR 40 IAW REO 601R-53-115. INSTALLED 1 EA FASTENER BETWEEN FS 295 AND FS 280, BETWEEN STGR 26L AND STGR 27 IAW REO 601R-53-00-115, REV C. MAJOR REPAIR,SDR ASOA2013060603773Skin · burnedLEFT WING LOWER WING PLANK HAS LIGHTNING BURN AT OTBD AFT SKIN EDGE OF FUEL TANK ACCESS PANEL 610AB CUTOUT. BLENDED BURN ON LT WING LOWER WING PLANK REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (LIGHTNING STRIKE NOT ALLOWED TO WING PLANK). ROTO-PEENEDSDR ASOA2013060603772Skin · burnedBURN MARK AT BS 473.15 AT STRINGER 26L. BLENDED BURN IN SKIN REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING BURNS ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01.SDR ASOA2013060603771Skin · burnedBURN ON FUEL ACCESS PANEL AT FS 461 AT STRINGER 26L. BLENDED TWO BURNS IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS. ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-25-01. MAJOR REPAIR IAW GMM 5-3.SDR ASOA2013060603770Skin · burned2 BURN MARKS AT FS 449.85 AT STRINGER 26L. BLENDED 2 BURNS IN SKIN REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING BURNS ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24-11. RESTORED SURFACE FINISH TO RE-WORKED AREA SRM 51-SDR ASOA2013060603769Skin · burnedBURN MARK BETWEEN FS 424 AND 439, BETWEEN STRINGER 27 AND 26L. BLENDED BURN IN SKIN SRM 51-12-00. BLEND MEASURES .013" D, .450"L, .500"W. DETERMINED TO BE OUT OF LIMITS (NO LIGHTNING DAMAGE ALLOWED TO WING SKINS). ROTO-PEENED, RE-WORKED AREA IAW SRM 51-24SDR ASOA2013060603768Skin · burnedTWO BURN MARKS BETWEEN FS 409+128 AND FS 424, BETWEEN STRINGER 27L AND 26L. BLENDED BURNS, REF SRM 51-12-00. BLEND A MEASURES .021" D, .450"L, .600"W. BLEND B MEASURES .015" D, .500"L, .500"W. DAMAGE FOUND TO BE OUT OF LIMITS (NO LIGHTNING STRIKE ALLOWESDR ASOA2013060603767Skin · burnedONE BURN MARK BETWEEN FS 409.00 AND 409+16, AT STRINGER 26L. REMOVED BURNED FASTENER FOUND COUNTERSINK DAMAGED STEPPED UP HOLE TO A NR 6 FASTENER HOLE AND ALL DAMAGE IS GONE AFTER CONTER SINK IAW REO 601R-53-00-115, REV C. INSTALLED NEW FASTENER BETWEEN FS 4SDR ASOA2013060603766Skin · burnedONE BURN MARK BETWEEN FS 310.00 AND 319.70, BETWEEN STRINGERS 27 AND 26L. DRILLED OUT DAMAGE TO A NR 30 IAW REO 601R-53-00-115, REV C. INSTALLED ONE FASTENER BETWEEN FS 310 AND FS 319, BETWEEN STGR 27 AND STGR 26L IAW REO 601R-53-00-115, REV C. CLASSIFIED ASDR ASOA2013060603765Skin · burnedONE BURN MARK BETWEEN FS 295 AND 310, BETWEEN STRINGERS 27 AND 26L. DRILLED OUT DAMAGE TO A NR 30 IAW REO 601R-53-00-115, REV C. INSTALLED 1 FASTENER BETWEEN FS 295 AND FS 310, BETWEEN STGR 27 AND STGR 26L IAW REO 601R-53-00-115, REV C. CLASSIFIED AS A MAJSDR ASOA2013060603764Skin · burnedTWO BURN MARKS BETWEEN FS 280 AND 295, BETWEEN STRINGERS 26 AND 27L. DRILLED OUT DAMAGE, 1 DAMAGE TO A NR 30 AND 1 TO NR 40 IAW REO 601R-53-00-115, REV C. INSTALLED FASTENERS IAW REO 601R-53-00-115, REV C. MAJOR REPAIR.SDR ASOA2013060603763Skin · burnedTWO BURN MARKS AT FS 169.00 ON BOTTOM, 1 IS 3" TO THE LEFT OF CENTERLINE AND 1 IS 4" TO THE RT OF CENTERLINE. REPAIRED IAW REO 601R-53-00-115, REV C, STS EA 12-2013-293, SRM 51-25-01. MAJOR REPAIR.SDR ASOA2013050903485Lock · lack of lubePAX DOOR HARD TO OPEN FROM INSIDE CABIN. INSPECTED AND LUBED LOCK MECHANISM IAW AMM 52-11-00, OPS CHECKS NORMAL, ACFT OK FOR SVC.SDR ASOA2013021503017Light · inoperativeEMERGENCY LIGHT, INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.SDR ASOA2013011702824Bulkhead · crackedREAR PRESSURE BULKHEAD WEB AFT SIDE AT ABOUT 8:45 O`CLOCK POSITION HAS A CRACKED CLIP. R & R REAR PRESSURE BULKHEAD WEB AFT SIDE AT ABOUT 8:45 0'CLOCK POSITION CLIP IAW SRM 51-42-20.SDR ASOA2013011702823Angle · crackedPRESSURE BULKHEAD WEB CAP ANGLE CRACKED AT FS 559 LBL 18.00. RECEIVED AND COMPLIED WITH REO 601R-53-41-1650.SDR ASOA2013011702822Floor Support · corrodedMINOR CORROSION AROUND SCREW HOLES ON LBL 27, JUST INBD OF CARGO DOOR. REMOVED CORROISON MATERIAL LOSS MORE THAN 50 PERCENT FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43+ 53-00-00. REMOVED AFT LT FUSELAGE FLOOR CAP. LOCATED AND DRILLED NEW TRACK IAW SRM 51-40-SDR ASOA2013011602820Sill · corrodedCARGO DOOR SILL PLATE HAS MINOR CORROSION. REMOVED CORROSION IAW SRM 51-21-06.SDR ASOA2013011602819Angle · corrodedPAX DOOR LOWER SILL ANGLE CORRODED AT FWD SECTION. REMOVED CORROSION IAW 51-21-06. COMPLIED WITH REO 601R-53-21-2390.SDR ASOA2013011602818Seat Track · corrodedSEAT TRACK CORRODED FS 484 - 487 RBL 9. R & R CORRODED SEAT TRACK WITH NEW IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
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