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 FDEA201805231278Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1285, LBL 47.5, FOUND TO CROWN DAMAGED. REPLACED THE SEAT TRACK FROM BS 1248 TO 1312, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231293Web · crackedCOCKPIT RT OBSERVER`S SEAT FLOOR SUPPORT CUTOUT WEB FOUND CRACKED AT BS 365, RBL 3.5. THE WEB WAS REPAIRED IAW SRM 53-10-51-2R, FIG 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231292Frame · damagedFRAME AT BS 535, LONGERON 23L FOUND WITH A REPAIR ANGLE DAMAGED. REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231291Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 47.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 665 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231290Seat Track · crackedMAIN DECK FLOOR SEAT TRACK CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 745 IAW SRM 53-00- 52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231285Seat Track · gougedMAIN DECK SEAT TRACK CROWN AT BS 5-113, RBL 47.5 FOUND GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 5-83 TO EXISTING SPLICE AT BS 5-123 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPASDR FDEA201805231284Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 5-43, RBL 8.5 WAS FOUND CORRODED. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM EXISTING SPLICE BS 5-0 TO 5-83 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSDR FDEA201805231283Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1471, LBL 8.5 WAS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1411 TO EXISTING SPLICE AT BS 5-0 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLSDR FDEA201805231275Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 701 FOUND CRACKED. REPAIRED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201805231274Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201805231273Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201805231272Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201805231268Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. REPLACED FROM EXISTING SPLICES BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201805231303Skin · damagedLEFT WING, LOWER FUEL TANK ACCESS PANEL 538AB CUTOUT FOUND DAMAGED. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231289Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231288Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 8.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES AT BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231277Seat Track · damagedMAIN DECK SEAT TRACK AT BS 775, X= 75.25, FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 765 TO 816, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201805231269Seat Track · gougedMAIN DECK SEAT TRACK AT BS 880, RBL 8.5, FOUND THE CROWN DAMAGED. REPLACED FROM BS 869 TO 909, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201712183406Warning Message · illuminatedDURING A PREFLIGHT CHECK OF EMERGENCY LIGHTS, EMERGENCY LIGHT BATTERY 1 LOW MESSAGE DISPLAYED.SDR FDEA201701270270Sensor · malfunctionedAFTER DEPARTURE, RECEIVED SLAT DISAGREE AND STICK SHAKER AT 200 FT. AIRCRAFT DID NOT ROLL, MAINTAINED LEVEL FLIGHT AND CONTINURED DEPARTURE. RETRACTED FLAPS AND SLATS WITH NO ISSUES. WENT INTO HOLDING FOR ATC WITH SLATS EXTENDED SPEED 210. NO ISSUE IN HOLDINSDR FDEA201701140162Light · inoperativeL1 PRESS TO TEST DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMBLY IAW AMM 25-61-04-4-0. OPS CHECKED OK. GOOD FOR SERVICE.SDR FDEA201612224521Apu · failedON PRE-FLIGHT WITH APU RUNNING SMOKE ENTERED FLIGHT DECK AND ALL AIR CONDITIONING DUCTS. SPARKS WERE SEEN EXITING APU EXHAUST AREA. APU FIRE HANDLE WAS PULLED AND BOTH FIRE BOTTLES WERE DISCHARGED. INSTALLED APU PER W/C 49T1901, APU OPS CHECKED GOOD WITH NO DESDR FDEA201606141993Fitting · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING-D, FWD HOLE CORROSION. CORROSION FOUND TO EXCEED LIMIT IAW SRM 57-50-02, REPAIR 5, FIGURE 201. EXISTING SLOT: 0.890", LENGTH, 0.625", WIDTH. FINAL SLOT: 0.965", LENGTH, 0.662", WIDTH. MAXIMUM ALLOWABLE: 0.940", LENGTHSDR FDEA201606141991Hinge · corrodedLT WING OTBD FLAP, INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.162", MAXIMUM ALLOWABLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750SDR FDEA201606131981Hinge · corrodedLEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE SURFACE CORROSION. CORROSION FOUND EXCEEDED LIMIT AS CMM 57-52-03, EXISTING THICKNESS: 0.260", MATERIAL REMOVED: 0.074", REMAINING THICKNESS: 0.186", MINIMUM ALLOWABLE THICKNESS: 0.205". STRAP RESDR FDEA201606121957Skin · cracked1EA FASTENER HOLE FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN BS XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT RT WING LOWER SKIN ACCESS DOOR CUTOUT IAW SRM 57-20-02-2R, FIG 201, REPSDR FDEA201606121960Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1601- BS 1621, X= 8.0, OTBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121959Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE FOUND CORRODED AT BS 1621- BS 1641, X= 75, INBD. SEAT TRACK REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606121956Skin · cracked6 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA, XORS =683.4 AND XORS =713.6. REPAIR BUSHING CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XSDR FDEA201606101934Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT DENTED FRAME AT RT BS 5-53, LONGERON 12R. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14500 FLT CYCLES AND REPETITIVE INSPECTION AT 9500 FLT CYCLES TO BE CARSDR FDEA201606101931Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.286", FINAL HOLE DIA 1.290", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783C, PASDR FDEA201606101930Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.253", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783, CSDR FDEA201606101929Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.375", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PSDR FDEA201606101928Hinge · corrodedLT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PT5,SDR FDEA201606101927Hinge · corrodedRT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA 0.644", FINAL HOLE DIA 0.713", MAXIMUM ALLOWABLE DIA 0.709". REPAIR BUSHING FABRICATED AND INSTALLED IAW EASDR FDEA201606101926Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA 0.594", FINAL HOLE DIA 0.705", MAXIMUM ALLOWABLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-SDR FDEA201606101925Hinge · corrodedLT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA 1.214", FINAL DIA 1.224", MAX ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892SDR FDEA201606101924Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.643", FINAL HOLE DIA: 0.716", MAXIMUM ALLOWABLE DIA: 0.709". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201606101923Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDING LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.306", FINAL HOLE DIA: 2.3290", MAXIMUM ALLOWABLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201606101922Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.325" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED ANDSDR FDEA201606101921Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.324" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201606101920Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.582" FINAL HOLE, DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INSSDR FDEA201606101919Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.579" FINAL HOLE DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INSDR FDEA201606091906Frame · damagedAGING AIRCRAFT, EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT, STA 1661, LONGERON L12R. EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1661, LONGERON L12R EVALUATED AND FOUND DAMAGED. REPAIR CARRIED OUT AT FRAME AT MAIN CARGO COMPARTMENT, SSDR FDEA201606081879Skin · crackedAGING AIRCRAFT, EXISTING SKIN REPAIR DOUBLER FOUND AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, LONGERON L39R-L41R EXISTING REPAIR AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, L39R-L41R EVALUATED AND FOUND CRACK. REPAIR CARRIED OUT AT FWD CARGO DOOR CUTOUT SDR FDEA201606081888Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1310 BETWEEN LONGERON 26L-27L. WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606081887Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR FWD LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1256 BETWEEN LONGERON 26L-27L. CRACKED WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606081881Frame · chafedCABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 19R. DAMAGED FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606081880Frame · chafedCABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 24R. FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606071865Skin · damagedLEFT WING FIXED LE ANTI-ICE TELESCOPIC DUCT INNER SKIN BEADED AT STATION XOS 464, SURFACE FOUND DAMAGED. REPAIR CARRIED OUT PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
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