N620FE
Service difficulty reports · 352
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 = 'N620FE' 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 = 'N620FE' 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 FDEA201511123574Unknown · leakingIN CRUISE FLIGHT, 3.5 HOURS INTO FLIGHT HAD HYD 3 FAIL ALERT WITH HYD 3 INDICATING 0.0 QTY.SDR FDEA201412114102Warning System · activatedBEGINNING DESCENT, RECEIVED ENG 2 ANTI-ICE OFF, ALERT WHEN ENG ANTI-ICE SELECTED ON.SDR FDEA201407091681Pseu · faultySLAT DISAG ON ROTATION ON TAKEOFF. AT SLAT RETRACTION SPEED DURING CLIMB SLAT DISAG EXTINGUISHED. 30 SECONDS LATER SLAT DISAG LIGHT CAME ON. LIGHT STAYED ON UNTIL SLATS EXTENDED FOR LANDING, THEN LIGHT EXTINGUISHED, NORMAL LANDING. TROUBLE SHOT IAW FIM 31SDR FDEA201406281570Skin · corrodedCABIN RT STATION 1229, XCW = 105 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA 1-5730-T0309294 PART 1, TITLE: WINGS - PLATES AND SKINS - CENTER WING UPPER SKIN CORROSION REMOVAL BEYOND SRM LIMITS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISSDR FDEA201406251545Skin · crackedFIVE EACH FASTENER HOLES 08, 28, 29, 30 & 31 FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS =690 & XORS=700. SKIN ACCESS DOOR CUTOUT REPAIRED AS PER SRM 57-20-02 FSDR FDEA201406251544Skin · crackedSIX EACH FASTENER HOLES 5, 10, 17, 29, 30 & 31 FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS =690 & XORS=700. LOWER SKIN ACCESS DOOR CUTOUT REPAIRED AS PER SRM 57SDR FDEA201406221508Skin · crackedLEFT WING LE SKIN AT OTBD OF SLAT TRACK 10 AT XOS 667 FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 9 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201310072442Satcom · malfunctionedLOST CPDLC CONTACT. HAD CPDLC "NO COMM" ATTEMPTED TO LOGON WITH NO RESULTS. SAW ACARS DISPLAYED "NO COMM" AND SATCOM MENU SHOWED "NOT AVAILABLE". AIRTURN BACK TO DEPARTURE. RESET FMC 1 AND FMC 2 CIRCUIT BREAKERS REF 34-63-09-05 AND CYCLED SATCOM CIRCUITSDR FDEA201301110069Torque Tube · brokenON ROLLOUT F/O RT RUDDER PEDAL WENT FULL FORWARD. CAPT SIDE NORMAL, THEN ON TAXI IN CAPT SIDE WENT FULL FORWARD BUT OPPOSITE OF F/O'S. F/O'S LT SIDE FULL FWD/CAPT RT SIDE FWD. ACCESSED AVIONICS COMPT & INSPECTED RUDDER PEDAL TORQUE TUBE. FOUND BROKEN IN HSDR FDEA201210283764Handle · contaminatedRAISED GEAR HANDLE ALL FOUR GEAR INDICATED UNSAFE "RED" ON ALL PRIMARY AND SECONDARY INDICATIONS. CHECKED GEAR HANDLE AND FOUND TO BE OPERATIONAL BUT SLIDING HANDLE WAS GUMMED UP AND WOULD INTERMITTENTLY SLIDE INTO EITHER UP OR DOWN LOCKING POSITION. REMOVESDR FDEA201209103272Seat Track · corrodedMAIN DECK BS 1877, X= 8.5 , SEAT TRACK FLANGE FOUND WITH CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209103271Seat Track · corrodedMAIN DECK BS 1801 - 1821, X= 8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209103270Flange · corrodedMAIN DECK BS 1761 - 1801, X=8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209103269Seat Track · corrodedMAIN DECK BS 1801- 1821, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201209103268Seat Track · corrodedMAIN DECK BS 1761 - 1801, X=-8.5 , SEAT TRACK FLANGE FOUND CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115SDR FDEA201209073249Seat Track · corrodedMAIN DECK CARGO TRACK AT BS 1880, X=-8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1751 TO STA..1887 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063239Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 1689, X=-8.5 , FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1571 TO 1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REFER TO SNRM N00262 FOR WORK DETAILS. REPAIR CLASSIFIED MAJORSDR FDEA201209063238Rib · crackedRIGHT WING RIB NR 16 AT FIXED L/E AREA (INBD SIDE) FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 REV. 50 AND REPLACED WITH NEW RIB 16 AS PER DWG ARB7565 REV. C REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063237Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 997, X= 75 , FOUND CROWN CHIPPED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 989 TO 1049 , X=75 AS PER SRM 53-00- 52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201209063236Cargo Track · corrodedMAIN DECK CARGO SEAT TRACK AT BS 1581, X=-8.5, FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA.1571 TO STA..1691 , X= -8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6- 2-100 REVISISDR FDEA201206082161Fire Detector · inaccurateFSS DISCHARGE 7L AND 7R TEMP READS 451 ON FSS PANEL BUT NO OTHER FIRE INDICATIONS. FSS PANEL SHOWED TEMP OF 451 DEGREES. EMERGENCY DECLARED, DIVERTED. COMPLIED WITH EA 1-2624-160811A. REACTIVATED MAIN DECK FIRE SUPPRESSION SYS.SDR FDEA201110054305Sign · unsecureL1 "EXIT SIGN" FELL OFF IN FLIGHT. REINSTALLED L1 EXIT SIGN LIGHT COVER IAW SMP.SDR FDEA201010214141Frame · dentedMAIN DECK CARGO, RT INTERIOR FUSELAGE FRAME STA 1661 L-11R FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 44. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.SDR FDEA201010214143Cargo Track · damagedMAIN DECK CARGO COMPARTMENT CARGO TRACK RBL 8.5 AT STATION 755 FOUND WITH DAMAGED CROWN. SPLICE REPAIR CARRIED OUT ON DAMAGED SEAT TRACK BETWEEN STATION 745 AND STATION 800 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV. 44. (MAJOR REPAIR).SDR FDEA201010214140Seat Track · corrodedUPON REMOVAL OF MAIN DECK CARGO FLOOR PANEL NR245BF FOR SEAT TRACK REPAIR ACCESS, SEAT TRACK X=-8 INBD FLANGE AT STA 799 WAS FOUND CORRODED. SPLICE REPAIR CARRIED OUT ON CORRODED SEAT TRACK BETWEEN STATION 745 AND STATION 800 AS PER SRM 53-00-52 FIG 201 REPSDR FDEA200910313749Controller · failedLEVEL 1 A-ICE FAIL AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURES. NO CHANGE. RETURNED TO PEN. RELEASED FOR SERVICE IAW MEL: 36-10-01 CATEGORY: C EXPIRATION: 10NOV09 "MEL 36-10-01: PNEUMATIC SYS CONTROLLER NR 2-INOP. OPERATE AIR SYS CONTROL PANEL IN AUTO. " SDR FDEA200904171327Seat Track · corrodedCABIN, RT STA 5-113 TO STA 5-120 X= -8 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141299Rib · crackedLT WING NR 16 SLAT TRACK INBD RIB SUPPORT FOUND CRACKED. REMOVED AND REPLACED AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141298Frame · dentedCABIN, RT STA 735 LONGERON, 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I REV 40. RSDR FDEA200904141297Seat Track · corrodedCABIN, LT STA 1731 X= 107 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 6 VOL.I REV. 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141296Seat Track · corrodedLT STA 1545 TO STA 1551 X= 8 SEAT TRACK FOUND CORRODED. REPAIRED PER SRM 53-70-00 FIG. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141295Seat Track · corrodedRT STA 1471 X= -8 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIG I VOL I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10 REV 107.SDR FDEA200904141294Seat Track · corrodedRT STA 1531 - STA 1561 X= -8 SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIG. I REV 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141293Shear Tie · crackedAFT FUSELAGE COMPARTMENT CROWN CLIP AT APPROX STA 2046 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904141292Attach Fitting · crackedAFT FUSELAGE COMPARTMENT CROWN CLIP AT STA 2093 FOUND WITH CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 107.SDR FDEA200904131281Skin · dentedLT WING INBD FLAP LOWER SURFACE LOWER OUTBD SEGMENT FOUND SEVERAL DENTS AT XIFH 243 TO XIFH 255 EXCEED LIMIT. REPAIRED AS PER SRM 57-10-00 FIG. 3 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR FDEA200904131280Frame · dentedCABIN, LT STA 1741 LONGERON 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 40SDR FDEA200904131279Frame · dentedCABIN, RT STA 1641 LONGERON 12 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I REV 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I REV. 4SDR FDEA200904131278Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II REV. 40. REPAIR BUSHINGS INSTALLED FOR THE 1ST AND 2ND LAYESDR FDEA200904131277Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-SDR FDEA200904131276Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVSDR FDEA200904131275Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 RESDR FDEA200904131274Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVSDR FDEA200904131273Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.SDR FDEA200904131272Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.SDR 08FDEA04010Unknown · unknownDURING ILS APPROACH TO SFS, IN LIGHT TO MODERATE PRECIP, AT'S AND AP DISCONNECTED, ALSO HAD IAS COMPARATOR WARNING, W/ 5 TO 15 KTS DIFFERENCE. ALSO LEVEL 2 SEL ELEV FEEL MANUAL, LSAS ALL FAIL AND TWO OR MORE MOMENTARY LEVEL 2 ALERTS OCCURRED. ON GO AROUND, SDR 08FDEA03867Skin · dentedNOSE SKIN LOWER PANEL INSTALLATION, REPAIR OF SKIN DENT AT BS.421.5 BETWEEN X=0 AND X=-21. REFERENCE WRI NR 53-30/5861. LOWER FUSELAGE SKIN AT STA 421.5, BETWEEN X = 0 AND X = -21 CARRIED OUT REPAIR AS PER EA NR1-5330-121688. REPAIR OF SKIN DENT AT BS 421.5SDR 08FDEA03866Frame · crackedUPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT FRAME AT STA 421.507, X=-20 CRACKED. FRAME AT STA 421.507, X = -21.25 CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5310-123101 PT1, TITLE: FUSELAGE, MAINFRAME BS 421.5 FRAME, X = -21.25 - FLANGE CRACK REPAIR. THIS REPAISDR 08FDEA03865Intercostal · crackedUPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT INTERCOSTAL AT STA 410 CRACKED. INTERCOSTAL AT STA 410, X = -1.750 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. FABRICATED INTERCOSTAL AS PER DOUGLAS DRAWING ABA8678. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-SDR 08FDEA00691Rccb · failedT/O ROLL NR 4 DU BLANKED, NR 1 FMS DISP "TIMEOUT RESELECT" NR 3 MCDU BLANKED, OCCURRED PRIOR TO V, CONTINUED T/O. AT 180 NM FROM HNL RECEIVED MANY LVL 1 AND LVL 2. ALERTS MOST SIGNIFICANT LVL 1 "BUS AC 1 OFF" AND LVL2 FUEL QTY FAULT", LVL 2 SELECT FADEC ALTN
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