N390FE, cancelled Mar 2, 2024
Service difficulty reports · 143
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 = 'N390FE' AND deregistration_id = 'N390FE-2024-03-02' 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 = 'N390FE' AND deregistration_id = 'N390FE-2024-03-02' 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 FDEA202001100107Unknown · malfunctionedEMERGENCY LIGHT TEST FAIL ON POST FLIGHT. PERFORMED ADJUSTMENT/TEST OF EMERGENCY LIGHTING. EMERGENCY LIGHTING PASSED MULTIPLE TIMES(3) WITH NO FAULTS. REF AMM 33-50-00-5. OK FOR SERVICE.SDR FDEA2019120433162Warning Message · false activationPDIS 390 29-02 9785 03DEC19 DEN FACT U LOGPAGES:3149673 AT FL 340, RECEIVED LEVEL 1 "HYD 3 ELEV OFF". SWITCHED FROM AUTOPILOT 2 TO AUTOPILOT 1. RECEIVED SUBSEQUENT "HYD 3 QTY LO", ACCOMPANIED BY " HYD 3 FAIL". FACT 03DEC19 04:39 DEN U SERSDR FDEA201906181344Proximity Sensor · out of alignmentON FINAL APP. WITH FLAPS 22*, EXTENDED GEAR AND GOT SLAT DISAG ALERT. PREFORMED GO-AROUND AND RETRACTED GEAR & FLAPS ONLY TO 15*. WENT TO QRH FOR SLAT DISAG. DID FLAP 22* LANDING AND LEFT FLAPS & SLATS IN 22* POSITION ALL THE WAY TO SHUTDOWN. ALERT DID GOSDR FDEA201809252679Pseu · malfunctionedPDIS 390 27-80 8566 25SEP18 MEM OPEN U "SLAT DISAG" LEVEL 2 ON APPROACH WHEN SELECTING FLAPS 35. NO ROLL NOTED. COMPLIED W/QRH LANDED WITH FLAPS 22/EXT. FACT 25SEP18 18:37 MEM REMOVED SDR FDEA20180829005Shear Tie · corrodedAFT CARGO BAY, BS 1987, JUST AFT OF THE SERVICE PANEL BETWEEN LONGERONS 51L & 51R CORRODED ON THE AFT SIDE OF FRAME ANGLE. REPAIRED THE SHEAR TIE IAW EA 8-5310-T0341752.SDR FDEA2018080311881Tee Fitting · corrodedCENTER WHEEL WELL AT STA 1521, RT SIDE CORROSION FOUND ON THE UPPER TEE ANGLE. REPAIRED "T" ANGLE PER EA 8-5310-T0341578.SDR FDEA201807301857Floor Support · corrodedFWD CARGO COMPT DOOR SILL FWD FLOORBOARD SUPPORT CORRODED UNDER NUTPLATE AT STA 876. CLEANED CORROSION PER SRM 51-21-01 VOL 2.SDR FDEA2018081492012Floor Panel · corrodedMAIN DECK, BS 495 LEFT SIDE FLOOR PANEL UNDER RCB HAD EXTENSIVE EXFOLIATION CORROSON ON THE SURFACE. FABRICATED A NEW FLOOR PANEL IAW DWG WSP0791-1.SDR FDEA2018080751928Shear Tie · corrodedAFT CARGO BAY BILGE SHEAR TIE WAS FOUND CORRODED UNDER THE FRAME BS 1967, LONGERON 50R. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA0021-65.SDR FDEA2018073021820Web · crackedCENTER WHEEL WELL, HAS A CRACK ON RT UPPER SIDE WEB AT APROX STA 1501. INSTALLED REPAIR DOUBLER PER EA 8-5310-T0341389.SDR FDEA2018080711927Floor Support · crackedFLOOR SUPPORT BRACKET WAS CRACKED, BS 1501, LONGERON 50R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01, VOL 2.SDR FDEA201803210746Fitting · corrodedRIGHT MLG TRUNNION FWD FITTING FWD BEARING INNER DIAMETER SURFACE HAS PITTED CORROSION. COMPLIED WITH EA 8-5740-T0338917 WINGS - ATTACH FITTINGS RT MLG FWD TRUNNION FITTING HOLE CORRODED STEPS 1-8 DATED MAR 20, 2018 MAJOR REPAIR.SDR FDEA201701260259Switch · malfunctionedUNCOMMANDED GROUND SPOILER DEPLOYMENT DURING TAKEOFF. CHECKED BOTH FCC 1&2 FOR CURRENT OR PREVIOUS FAULTS, NONE FOUND. PERFORMED AGS RTS IN BOTH FCC'S, CHECKED GOOD. INSPECTED AGS ARM SWITCH S1-845 IT APPEARS TO MOVE FREELY AND HAS GOOD AUDIBLE CLICKS. RANSDR FDEA201608052821Bulkhead · crackedRIGHT STA 595 BULKHEAD WEB LOWER FASTENER HOLE AT LONGERON 43R HAS A CRACK INDICATION. OPENED CRACK HOLE ON THE LOWER WEB TO .247 FOR NDT. PERFORMED OPEN HOLE HFEC. NO INDICATION FOUND IAW NDTSPM 93K0393. EA 8-5310-T0326599 FOR MORE INFORMATION.SDR FDEA201608052820Skin · crackedRIGHT STA 595 FUSELAGE SKIN COMMON TO THE TEE CAP AT LONGERON 38R HAVE 2 EA. FASTENER HOLES WITH CRACK INDICATIONS. SAME HOLE LOCATIONS AS TEE CAP CRACK, OPENED FWD HOLE TO .247 AND AFT HOLE .262 AT LONGERON 38R ON THE FUSELAGE SKIN FOR NDT. PEFORMED OPEN HSDR FDEA201608032791Frame · corrodedFWD AVIONICS AREA THROUGH OPENING IN NLG WHEEL WELL UNDER SYSTEM NR 1 RAM AIR DUCT, FRAME AT BS 449, LBL 30 HAS DAMAGE AND SIGNS OF CORROSION. REMOVED LIGHT CORROSION IAW SRM 51-21-01VOL 2.SDR FDEA201607302682Bulkhead · corrodedCENTER CARGO COMPARTMENT, FWD BULKHEAD LOWER WEB HAS EXFOLIATION CORROSION AT 42R, STA 1521, FOUND UNDER ROLLER TRAY. MARKED, 2016-07-30. R & R SMALL SECTION OF ANGLE WITH PN S2929469, S2933839 & S4931827 IN REF TO SRM 53-00-01, FIG 9, VOL 1.SDR FDEA201607292659Skin · crackedNR 3 AIR CONDITIONING DOOR AFT UPPER CUT OUT CORNER HAS A .100 INCH CRACK. REPAIRED IAW SRM 53-50-00 FIG 3A VOL I.SDR FDEA201607212588Angle · corrodedCENTER CARGO COMPARTMENT, AFT BULKHEAD LOWER WEB CORRODED. FOUND AT BS 1781, UNDER THE AFT END OF THE ENTRY WAY OMNI ROLLER TRAY. REMOVED AND REPLACED CORRODED ANGULAR SUPPORT BRACKET IAW SRM VOLUME 2 51-31-01,V2.SDR FDEA201607132437Tee Fitting · crackedRIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.SDR FDEA201607132436Tee Fitting · crackedRIGHT STA 595, BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.SDR FDEA201607132435Tee Fitting · crackedRIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.5" CRACK AT LONGERON 43R, MARKED.SDR FDEA201607132434Tee Fitting · crackedRT STA 595 BULKHEAD TEE CAP HAS A CRACK BETWEEN LONGERON 37R AND 38R ON THE VERTICAL AND FORWARD HORIZONTAL LEG EXTENDING THROUGH THE RADIUS, MARKED.SDR FDEA201511013434Switch · malfunctionedON CLIMB OUT, SELECT ENG & WING ANTI-ICE ON, AS SOON AS WING ANTI-ICE SELECTED, GOT AIR SYS 3 OFF WITH BLEED AIR 3 VLV & PACK 3 BEING TURNED OFF AUTOMATICALLY. R & R NR 3 SYS MANIFOLD FAILURE DETECTION SWITCH IAW AMM.SDR FDEA201509202904Seat Track · damagedSEAT TRACK LUG BROKEN, BETWEEN POS 2L & 3L LOCK ID IS Q758. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-70-00 & SR 10-53-002. THIS IS A MAJOR REPAIR. REPLACED SEAT TRACK SEGMENT ONLY, PN 4929150-12000N. INSTALLED FLOORBOARDS & ROLLER SYS.SDR FDEA201505131505Coalescer Bag · dirtyIN CRUISE AT FLIGHT 350, AIR SYS SMELLS LIKE A GYM ROOM OR DIRTY SOCKS. PERFORMED REPLACEMENT OF PACK SYS 1, 2, & 3 CONICAL COALESCER BAGS. ODOR CLEARED UP & PACKS OPERATIONS CHECK GOOD. ACFT GOOD FOR SERVICE.SDR FDEA201502010407Cable · frayedDURING SERVICE CHECK, FOUND L1 DOOR AFT UPPER DRIVE CABLE FRAYED. R & R L1 DOOR AFT UPPER DRIVE CABLE. RIG & OPS CHECKED OK.SDR FDEA201409112615Dump Valve · failedRIGHT WING DUMP VLV FAILED TO CLOSE AFTER DUMP TERMINATION. RIGHT FUEL DUMP VLV SYS WIRING CHECKED FROM RT FUEL DUMP VLV M1-89 TO FUEL SYS CONTROLLER. RT FUEL DUMP VLV TO FUEL SYS CONTROLLER, RT FUEL DUMP VLV TO 1, 2, 3 VIA CONTINUITY & INSULATION CHECKED NOSDR FDEA201409092547Duct · crackedNR 2 NOSE COWL INLET DUCT, CRACKED THROUGHOUT CIRCUMFERENCE. R & R WITH NEW NOSE COWL ASSEMBLY IAW AMM 54-22-01-2.SDR FDEA201409092545Skin · crackedLEFT OTBD FLAP UPPER SURFACE 2 CRACKS ON THE SKIN .120 TO .250 INCHES IN LENGTH APPROX XOF 560. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.SDR FDEA201409082536Floorbeam · mechanic errorAFT CARGO COMPARTMENT STATION 1868 LT X=36.00 FLOOR LINE, FLOORBEAM HAS MULTIPLE HOLES WITH UNACCEPTABLE SPACING BETWEEN HOLES. FABRICATED & INSTALLED REPAIR ANGLE IAW SRM 53-00-01 FIG 9 SHT 7.SDR FDEA201409082535Seat Track · damagedMAIN DECK STATION 1390 LT 75.5 SEAT TRACK IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.SDR FDEA201409082534Seat Track · damagedMAIN DECK SEAT TRACK AT STATION 1381 LT 75.5 IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.SDR FDEA201409012398Door · crackedLEFT MLG DOOR, CRACK EXISTS AT THE UPPER CTR HINGE PORTION OF THE DOOR. REMOVED DOOR AND REPLACED WITH NEW MLG DOOR IAW MM 32-14-01-2SDR FDEA201311112747Bulkhead · crackedTWO INCH CRACK LT MLG WW INBD BULKHEAD 30 INCHES FWD OF AFT BULKHEAD AND THREE INCHES DOWN FROM UPPER BULKHEAD. MARKED CRACK END HFEC. REPAIRED DAMAGED AREA, CRACK, REF SRM 53-00-01.SDR FDEA201212154310O-Ring · failedRECEIVED LEVEL 1 "HYD 3 ELEV OFF" ALERT. NR 3 SYS INDICATED 4.4 GALLONS AND OVER A 10 MIN PERIOD DECREASED TO 4.0, DIVERTED. DURING GEAR EXTENSION, NR 3 QTY DECREASED TO 1.7 GALLONS WITH "HYD 3 QTY LO". AFTER LT TURN OFF RUNWAY, MX TOW IN. FOUND O-RING TO SDR FDEA201102220674Panel · corrodedLT WHEEL WELL SLANT PANEL HAS SURFACE CORROSION ALONG THE LOWER EDGE IN SEVERAL AREAS. R & R LOWER SECTION OF SEAL RETAINER, REF SRM 51-35-01 AND 51-33-01.SDR FDEA201102220673Angle · corrodedLT WHEEL WELL SLANT PANEL INBD VERTICAL "L" ANGLE IS CORRODED AT LWR EDGE. R & R "L" ANGLE, REF SRM 51-35-01.SDR FDEA201102220672Angle · corrodedLT MAIN WHEEL WELL, FWD BULKHEAD, CORROSION LOCATED AT OTBD LOWER CORNER OF SLANT PANEL. R & R ANGLE. REF DWG NPB6072 AND DPS 4.708.SDR FDEA201102220680Web · crackedSEVERAL CRACKS FOUND AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING BARREL KEEL STRUCTURE. REPAIRED WEB AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING KEEL STRUCTURE IAW EA 8-5310-148486.SDR FDEA201102220671Structure · corrodedLT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR END. R & R VERTICAL TEE SECTION.SDR FDEA201102180623Angle · corrodedRT MAIN WHEEL WELL REAR SPAR CAP ANGLE (APB7080-2) HAS 2 CRACKS (2' CRACK INDICATION AFTER BLEND OUT) REMOVED AND INSTALLED REPAIR ANGLE. SRM 53-40-00, FIG 11.SDR FDEA201102180622Tee Fitting · corrodedRT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR CORNER. REMOVED CORROSION. REF EA 8-5340-148481.SDR FDEA201010204119Floor Support · corrodedAFT CARGO COMPARTMENT BILGE STA 1801 BETWEEN LONGERON 51 RIGHT AND LONGERON 52 FLOOR SUPPORT FRAME CLIP FOUND CORROSION. NEW SHEAR CLIP FABRICATED AS PER DOUGLAS DRAWING AFA0053, REVISION N. CORRODED SHEAR CLIP AT AFT CARGO COMPARTMENT BILGE STA 1801 BETSDR FDEA201010113985Door Frame · damagedFORWARD DOOR CUTOUT FUSELAGE JAMB AFT BETWEEN LONGERON 39 AND LONGERON 42 DOUBLER REPAIR FOUND WITH EDGE DAMAGED. R & R IAW SRM 53-50-00, FIG 26, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053930Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 51. FOUND WITHIN DAC DWG ARC0503, SHEET 2, REV BG LIMIT AND CMM 57-44-09, REV 51, TABLE 601 IN-SERVICE REWORK LIMIT. SHIM FABRICATED SDR FDEA201010053929Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053928Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053927Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053926Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT BEARING HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143446, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
Back to N390FE, cancelled Mar 2, 2024