N840FD
Service difficulty reports · 31
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 = 'N840FD' 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 = 'N840FD' 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 FDEA202608281245Skin · dentedFOUND LT WING, T/E, OTBD FLAP LOWER SURFACE, HAD ONE DENT AT CROSS OTEF, 315 INCHES AND T/E 5 INCHES. REPAIRED LH WING T/E O/B FLAP LOWER SURFACE 01 EA DENT AT CROSS OTEF 315 INCHES AND T/E 5 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70SDR FDEA202608261229Skin · crackedDURING PERFORM W/O: E G-5710-E0376285 H P14 STEP 5.A.(2) THEN FOUND TWO CRACKS AT NR 5 HOLE OF RT UPPER WING SKIN AT WBL 262. RHW UPPER SKIN OF NO.5 HOLE CRACKS REPAIRED AS PER B777 SRM 51-50-02-0G FIG 1, SRM 51- 40-02-0G FIG 12, SRM 51-10-01-0G FIG 1, SRSDR FDEA202509011585Bulb · failedDOOR 1 L/H EXTERIOR EMERGENCY LIGHT INOP. FILAMENT REPLACED AND OPS CHECKED IAW AMM 33-51-04-02-0.SDR FDEA202408301198Window · crackedPOST-FLT INSP, L1 DOOR ESCAPE SLIDE BUSTLE PRESSURE GAUGE VIEWPORT WINDOW CRACKED. THE PART FINALLY SHOWED UP. REMOVED AND REPLACED L1 DOOR EMERGENCY ESCAPE SLIDE BUSTLE PRESSURE VIEWPORT LENS ASSY, REF AMM: 25-66-06-4.SDR FDEA202408031080Window · overheatedRIGHT SIDE AFT WINDOW IS VERY HOT TO THE TOUCH AND APPEARS TO HAVE SOME CHARRING AND DELAMINATION IN THE MIDDLE OF THE WINDOW ALONG THE BOTTOM EDGE. COMPLIED WITH PART 3 OF E.A. # : G-5610-T0380167 REMOVED AND REPLACED R3 WINDOW, OPS CHECKS GOOD.SDR FDEA202403270381Module · inoperativeRECEIVED MULTIPLE EICAS ALERTS CLIMBING TO FL330. NO AUTOLAND, WNDSHEAR SYS, EEC MODE L, EEC MODE R. RAN ECL CHECKLISTS FOR EEC MODE LT & RT. ACFT CONTINUED TO CLIMB THRU MCP SELECTED ALT ON ATTEMPING LEVEL OFF. ATC SHOWED 200 FT LOW WHEN MCP SELECTED ALTITUSDR FDEA202403260372Pitot Head · failedAUTO PILOT DISCONNECTED AFTER LEVELING FL340. ALTIMETERS LEFT AND RIGHT INDICATED 400' HIGH. MULTIPLE EICAS : "AIRSPEED UNRELIABLE" " ENG EEC MODE R" "ENG EEC MODE L" " GND PROX WARN". ATC READOUT SHOWED 300' LOW WHEN WE RETURNED TO FL 340'. EICAS BUTTON DESDR FDEA202402210205Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 57, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 57, SHEET 2 OF 5 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210204Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 53, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE GAP 0.60 MIN IS TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURESDR FDEA202402210203Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 51, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SHOWN SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 51, SSDR FDEA202402210202Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 49, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 49, SHEET 2 OF 3 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210201Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 47, SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 47, SHEET 2 OF 4 SECTION CUT D-D ARROW ORIENTATION IS CLARISDR FDEA202402210200Longeron · misoverhauledWHILE ACCOMPLISHING EO E G-5710-E0366409 D PART7,(LEFT HAND LONGERON MODIFICATION) FOUND FIGURE 44, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QUANTITY 48 LOCATIONS IS NOT IN ACCORDANCE WITH THE FIGURE AND AIRCRAFT QUANTITY. DISCREPANCY IN EO E G-5SDR FDEA202402210199Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 120, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 120, SHEET 2 OF 5, SECTION CUT B-B ARROW ORIENTATION IS CLSDR FDEA202402210198Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 116, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE 0.60 MIN GAP TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 1SDR FDEA202402210197Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 114, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 114, SHEETSDR FDEA202402210196Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 112, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 112, SHEET 2 OF 3, SECTION CUT B-B ARROW ORIENTATION IS CLSDR FDEA202402210195Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 110 SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 110 SHEET 2 OF 4, SECTION CUT D-D ARROW ORIENTATION IS CLASDR FDEA202402210194Longeron · misoverhauledWHILE ACCOMPLISHING EO E G-5710-E0366409D PART8 (RIGHT LONGERON MODIFICATION), FOUND FIGURE 107, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QTY 48 LOCATIONS IS NOT IAW FIGURE AND AIRCRAFTQUANTITY. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 107SDR FDEA202402180184Structure · unknownWHILE ACCOMPLISHING EO # EG-5710-E0366409D-PART8, FOUND RIGHT HAND RING CHORD MODIFICATION KIT PART NUMBER 005W0129-4 SHORTAGE REPAIR ANGLE PART NUMBER 691W0017-2. EO # EG-5710-E0366409D PART8 WORK ACCOMPLISHED WITH THE RIGHT HAND RING CHORD REPAIR ANGLESDR FDEA202307261305Light · inoperativePOST-FLT INSP, SUPRNMRY DIRECT CTR OVRHD EMERGENCY LT INOP. REPLACED LIGHT ASSEMBLY PER AMM 33-51-03-2 OPS CHECKES OK FOR SVCSDR FDEA202212303044Cooling Fan · failedAIRCRAFT SMELLS OF ELECTRICAL SMOKE. DURING TROUBLESHOOTING IT WAS NOTICED THAT WHEN THE L EQUIPMENT COOLING FAN WAS ISOLATED THERE WAS AN IMPROVEMENT OF THE ODOR. FOR PRECAUTION THE L EQUIPMENT COOLING FAN IS RELEASED MEL AND DEACTIVATED. REMOVED ASDR FDEA202203290751None · nonePDIS 840 33-50 1107 03FEB22 CDG EMER LIGHT ARM SWITCH WIRE GUARD DOES NOT PROTECT THE SWITCH R/R THE EMERGENCY LIGHT SWITCH GUARD PER SMP.SDR FDEA202202060236None · leakingPDIS 840 29-11 1118 06FEB22 MEM FACT U GOT THE HYD PRESS PRI L CHECKLIST AND THE HYD QTY LOW L EICAS APPROXIMATELY 3 HOURS INTO FLIGHT FROM EGSS TO KMEM. FL340/ M84/ 480 KTS TAS. COMPLIED WITH ECL. NO FURTHER PROBLEMS. FACT 06FEB22 18:57 MSDR FDEA202111082794None · noneREPEAT WRITE UP HIGH PITCH CONTINUOUS TONE, FROM CAPTAIN SIDE BELOW LEFT FOOT. CAB ALT 5800 FT DP 8.5. WENT TO MANUAL ON OUTFLOW VALVES, REDUCED CAB ALT TO 5000 FT TONE DP 8.3, THE TONE WAS NOTICEABLY QUIETER. AFTER APPROXIMATELY 10 MINUTES WE RESELECTSDR FDEA202104261044Skin · damagedWHILE ACCOMPLISHING LEFT HAND E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER : 143W2314Y405) EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0361452 P1. TITLE:FUSELAGE-MAINFRAME-LH AND SDR FDEA202104261043Skin · damagedWHILE ACCOMPLISHING RIGHT HAND E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER : 143W2314Y406) EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0361452 P2. TITLE:FUSELAGE-MAINFRAME-LH ANDSDR FDEA202104230985Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 RIGHT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:GSDR FDEA202104230984Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1028 STRINGER 37 RIGHT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:GSDR FDEA202104230983Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1028 STRINGER 37 LEFT, APPROXIMATELY 1 INCH IN LENGTH. COMPLIED WITH E.O.#:G-531SDR FDEA202104230982Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 LEFT, APPROXIMATELY 1.5 INCHES IN LENGTH. COMPLIED WITH E.O.#:
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