N320FE
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 = 'N320FE' 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 = 'N320FE' 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 03FDEA00571Angle · corrodedNR 995 AFT CARGO AFT WALL LWR SUPPORT ANGLE IS CORRODED LBL 25 TO LBL 60 STA 1967. CLOSING ACTION ON 04/16/03 ON N/R 00995. REMOVED CORROSION, FOUND ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED ANGLE IAW SRM 51-35-01. FAB ANGLE ON TRAVELER T2/326614SDR 03FDEA00537Channel · crackedFWD CARGO PIT CEILING PANEL HAT TRACK CRACKED AT FS 970 RBL 48. CLOSING ACTION ON 04/14/03. HAT TRACK REMOVED IAW SRM 53-31-01. NEW HAT TRACK FAB ON TRAVELER T2/325808. NEW HAT INSTALLED IAW SRM 51-31-01.SDR 03FDEA00536Pulley · brokenRT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. CLOSING ACTION ON 04/18/03. REPLACED RT INBOARD FLAP FOLLOW-UP CABLE O/B PULLEY BRACKET, PULLEY AND SHAFT IAW M/M 20-20-07-2 AT M/M 20-50-02-2.SDR 03FDEA00535Pulley · brokenRT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN.SDR 03FDEA00534Pulley · brokenRT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. R/R PULLEY BRACKET & PULLEY.SDR 03FDEA00447Structure · crackedCOMPLY WITH EA 8-7832-68786 NR 1 ENGINE RM T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION. CLOSING ACTION ON 04/15/03. COMPLIED WITH EA 8-7830-68786. NR 1 ENGINE RT T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION.SDR 03FDEA00448Manifold · dentedNR 1 ENGINE SIDE LONGITUDINAL CDP AIR 14TH STAGE MANIFOLD FWD END 90 DEG ELBOW PART HAS 2 EA ADJACENT DENTS. CLOSING ACTION ON 04/14/03. ON N/R 00425. REMOVED AND REPLACED CDP AIR TUBE MANIFOLD AT 14TH STAGE IAW M/M 75-00-04-4.SDR 03FDEA00446Slat Track · wornCOMPLY WITH EA 8-2780-68790 FLIGHT CONTROLS-SLATS-REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9. CLOSING ACTION ON 04/14/03. COMPLIED WITH EA 8-2780-68790 FLIGHT CONTROLS-SLAT- REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9.SDR 03FDEA00445Seat Track · corrodedMAIN DECK SEAT TRACK STA 595 TO 675 AND STR FOR FLOORBOARDS BAD. CLIP NUTS HOLES CORRODED TOP AND BOTTOM. BLENDED DAMAGE TRACK IAW SRM 53-10-00 STA 595 TO 620 FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR SECTIONS AND SPLICES IAW SRM 53-70-00.SDR 03FDEA00431Bracket · crackedNR 2 ENGINE FAN CASE ANTI-ICE HOT DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT HAS CRACK. CLOSING ACTION ON 04/10/03. REMOVED AND REPLACED NR 2 ENGINE FAN CASE ANTI-ICE HOT AIR DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT IAW M/SDR 03FDEA00432Seal · tornAFT PIT LOWER CTR DOOR SEAL TORN. CLOSING ACTION ON 04/11/03. NEW SEAL FAB ON TRAVELER T2/324829, LOCATED AND DRILLED IAW SRM 51-31-01, TREATED AND PRIMED IAW SRM 51-21-01, TO BE INSTALLED ON W/C 53SI1516-01.SDR 03FDEA00433Structure · crackedLEFT MLG W/W AFT O/B STRUCTURE HAS CRACKED L-ANGLE. CLOSING ACTION ON 04/11/03. REMOVED ANGLE IAW SRM 51-31-01, FAB ANGLE ON TRAVLER T2/325914. INSTALLED ANGLE IAW SRM 51-31-01.SDR 03FDEA00412Light · failedUPPER AND LOWER BEACON FAILS FLASH RATE CHECK. CLOSING ACTION 04/09/03. REMOVED AND REPLACED UPPER AND LOWER BEACON ASSEMBLIES. OP'S CHECK GOOD IAW M/M 33-45-00-4.SDR 03FDEA00416Flange · gougedNR 3 PYLON FAIRING 487AR MOUNTING FLANG BOTH SIDES GOUGED. REMOVED AT MOUNTING FLANGES IAW SRM 51-31-01, FOUND BOTH FLANGES TO BE OUT OF LIMITS IAW SRM 51-00-00. FAB 2 NEW FLANGES USING MAT 301-1/4 HARD .05056 IAW SRM 54-31-02, INSTALLED FLANGES IAW SRM 51-3SDR 03FDEA00417Bracket · brokenNR 1 PYLON NUT PLATE BRACKET BROKEN FOR 473FL LT SIDE. CLOSING ACTION ON 04/09/03 REMOVED BRACKET IAW SRM 51-35-01. RECEIVED NEW BRACKET FROM FAB SHOP ON TRAVLER T2/324972, DRILLED AND LOCATED PER SRM 51-31-01. TREATED AND PRIMED PER SRM 51-21-01, INSTALLEDSDR 03FDEA00418Hinge · gougedTAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1. CLOSING ACTION ON 04/09/03. COMPLIED WITH EA 8-5240-68763, TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1.SDR 03FDEA00404Sill · gougedCENTER CARGO DOOR JAMBS AFT STRUCTURE 2 EA UPPER CHAFE PLATES ARE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED 2 EA SCUFF PLATES IAW SRM 51-31-01. REMOVED GOUGES FROM AFT SCUFF PLATE. NEG MATERIAL LOSS IAW SRM 53-00-01. ROUTED LWR SCUFF PLATE FAB SHOP. SDR 03FDEA00406Bracket · crackedNR 3 PYLON FLUID LINE SUPPORT BRACKET CRACKED JUST OUTBOARD OF THROTTLE CABLE QUARDANT. CLOSING ACTION ON 04/08/03. REMOVED SUPPORT BRACKET IAW SRM 51-31-01. FAB NEW SUPPORT BRACKET ON TRAVELER T2/325535. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. ISDR 03FDEA00403Angle · chafedNR 3 PYLON ANGLE CHAFED THROUGH AT AFT RIB SUPPORT FOR PANEL 487FL. CLOSING ACTION ON 04/07/03. REMOVED RIB SUPPORT IAW SRM 51-31-01. FAB NEW RIB SUPPORT ON TRAVELER T2/325651. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. TREATED AND PRIMED RIB SUPPORSDR 03FDEA00402Seal · wornTAIL CONE AFT END OF LT PATIO DOOR, 13 INCH METAL CLOSEOUT SEAL IS WORN, UPPER TO LOWER SURFACE. CLOSING ACTION ON 04/07/03. REMOVED CLOSEOUT STRIP SEAL LWR AFT END OF LT PATIO DOOR IAW SRM 51-31-01. FAB NEW CLOSEOUT STRIP SEAL PER TRAVELER T2/325001. INSTSDR 03FDEA00401Strip · wornTAIL CONE AFT END OF RT PATIO DOOR, METAL CLOSEOUT STRIP IS WORN THRU (MARKED) 6 INCH LENGTH. CLOSING ACTION ON 04/07/03. REPLACED CLOSEOUT STRIP IAW SRM 51-31-01. NEW CLOSEOUT, FAB PER MAE TRAVLER T2/324996.SDR 03FDEA00407Seal · gougedNR 3 ENGINE O/B CORE COWL UPPER SEAL AFT OF AFT HINGE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED DAMAGED SEAL IAW SRM 51-35-01. FAB NEW SEAL ON TRAVELER T2/304970. INSTALLED SEAL IAW SRM 51-35-01.SDR 03FDEA00400Intercostal · crackedN 132 TAILCONE LT MAINT PLATFORM WEB IS CRACKED BETWEEN 2EA ACTUATOR ROD/STIFFNERS/ SUPPORT ANGLES PARALLER TO MAINT PLATFORM AT NON-SKID AREA. CLOSING ACTION ON 04/07/03. REMOVED CRACKED DOUBLER AND INTERCOSTAL IAW SRM 51-35-01. FABRICATED REPAIR DOUBSDR 01FDEA00900Landing Gear · malfunctionedAFTER T/O, LANDING GEAR WOULD NOT RETRACT.SDR 00FDEA00722Structure · damagedON POSTFLIGHT FOUND NR 2 SPOILER DAMAGED. REMOVED AND REPLACED NR 2 SPOILER.SDR 99FDEA00297Fuse · cracked99-182 - AFT GEAR RETRACTION, HYD QUAN AND PRESSURE ON NR 3 SYS DROPPED TO 0. REPLACED THE CRACKED LOCK OUT FUSE PER MM 32-31-06-2 ALSO NR 3 HYD SYS CASE DRAIN FILTER CK IS OK PER MM 29-12-02-2 AND MM 29-12-17-2. LEAK CK IS OK CLOSED SECURED AND NR 3 ENG COSDR 99FDEA00092Spar · corrodedLEFT AFT UPPER CORNER OF THE CENTER WING BOX AT BS 118 TO 112 TO INCLUDE THE CLOS RIB AND ATTACH UPPER SKIN PLATES AT BS 1370 TO 1358 WERE FOUND WITH EXFOLIATION CORROSION DURING C-CHECK INSP IN THE LT MLG WHEEL WELL. ALL CORROSION HAS BEEN REMOVED, WAITING FSDR 98FDEA00760Skin · damagedON WALKAROUND FOUND LT NR 1 L/E SLAT INBD FAIRING MISSING. ALSO, DAMAGE TO L/E SLAT ASSY. *S/D* REPLACED NR 1 L/E SLAT (LT) ASSY WITH FAIRING PER MM 27-80-01-4.SDR 98FDEA00364Fire Loop · malfunctionedNR 1 ENG FIRE DETECT SYS LOOP-B LT ON IN FLT, RED TABS ACCOMPLISHED, CHECKED OK. APPROX 2 HRS LATER NR 1 ENG FIRE LIGHTS ON. ACCOMPLISHED RED TABS, EMERGENCY LANDING ABQ. LANDED OVERWEIGHT.SDR 97FDEA00841Cadc · malfunctionedDURING T/O ROLL, F/O AIRSPEED INDICATOR REMAINED AT ZERO. ON CLIMBOUT, IT BEHAVED AS AN ALTIMETER. RETURNED AND LANDED AT LAX. REMOVED AND REPLACED NR 2 CADC. FOUND FLEX LINE LOOSE ON FRONT OF NR 2 DIGITAL AIR DATA COMPUTER NR 2 CADC, OPS CK OK IAW MM 34-1SDR 96FDEA00375Skin · crackedRT HORIZ STAB UPPER AFT SKIN PANEL HAS .5625 INCH CRACK AT K/B AFT CORNER APPROX 1 INCH FROM PANEL AFT EDGE, ADJACENT TO WORKING BULKHEAD.SDR 96FDEA00343Skin · crackLT WING O/B FLAP, I/B UPPER SURFACE T/E SKIN HAS 5 INCH CRACK. REPAIRED PER SRM 57-10-00 PG 10 FIG 7.SDR 96FDEA00326Bracket · crackedLEFT O/B SLAT DRIVE OUTER BRACKET CRACKED .187 LONG IN FILLET RADIUS OF FWD FLANGE.
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