N602FE
Service difficulty reports · 506
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 = 'N602FE' 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 = 'N602FE' 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 FDEA201607032238Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607032237Bushing · corrodedLT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OSDR FDEA201607032236Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSISDR FDEA201607032235Bushing · corrodedLT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZSDR FDEA201607032234Beam · corrodedCABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR PLUG NR 7 LOWER DOOR BEAM DAMAGED.SDR FDEA201607032233Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 -STA 2007, X=-57 FOUND CORROSION AS MARKED.SDR FDEA201607032232Hinge Bracket · corrodedLEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1SDR FDEA201607012220Skin · crackedTWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.SDR FDEA201607012219Hinge · corrodedLEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABSDR FDEA201607012218Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATEDSDR FDEA201607012217Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICASDR FDEA201607012216Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944", REPAIR BUSHING FABRICATEDSDR FDEA201607012215Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201607012214Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED SDR FDEA201607012213Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW SDR FDEA201607012212Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED ANDSDR FDEA201607012211Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATEDSDR FDEA201607012210Bracket · corrodedLEFT HAND WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE ACTUATOR OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.219", FINAL HOLE DIA: 1.235" MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATSDR FDEA201606302203Seat Track · corrodedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 492, X=-27.5, FOUND CORROSION AS MARKED.SDR FDEA201606302202Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1801, X= 47.5. FOUND CROWN DAMAGED AS MARKED.SDR FDEA201606302201Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 5-27, X= 47.5. FOUND CROWN DAMAGED AS MARKED.SDR FDEA201606302200Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1259, X= 47.5, FOUND CROWN DAMAGED AS MARKED.SDR FDEA201606302199Seat Track · damagedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 5-53, X=-47.5. FOUND CROWN DAMAGED AS MARKED.SDR FDEA201606302198Floorbeam · corrodedCENTER CARGO FLOORBEAM UPPER SURFACE FOUND WITH CORROSION AT STA 1701, X=-18 TO X=-24.SDR FDEA201606292189Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDSDR FDEA201606292188Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE D: 0.420", FINAL HOLE D: 0.423", MAXIMUM ALLOWABLE HOLE D: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201606292187Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.420", FINAL HOLE: DIA 0.423", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INSDR FDEA201606292186Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUSDR FDEA201606292185Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.419", MATERIAL REMOVED: 0.006", FWD FACE; 0.006", AFT FACE, REMAINING THICKNESS: 0.389". MINIMUM SDR FDEA201606292184Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1SDR FDEA201606292183Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EASDR FDEA201606292182Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201606292181Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED BY MACHSDR FDEA201606292180Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE PIVOT HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311". FINAL HOLE DIA: 2.316". MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAWSDR FDEA201606282177Screw · defectiveCABIN DOOR WOULD NOT ARM AT PUSHBACK. FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD AND ARMS. REF AMM 52-11-02-6, FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD & ARMS, REF AMM 52-1SDR FDEA201606141999Cover · unsecureLEFT ENTRANCE DOOR, L1 WILL NOT ARM, JAMMED LEVER. RESECURED SLIDE COVER IAW MM 25-61-15-4. OPS CHECK GOOD, ACFT OK FOR SERVICE.SDR FDEA201606041827Block · wornINTERMITTENT SLAT DISAGREE ON APPROACH, WENT AROUND. FOLLOWED QRH, NO SLAT & FLAPS 28 DEGREE LANDING. 194 WAS APPROACH SPEED. R & R FWD ATTACH NR 12 BOLT & ATTACHING HARDWARE IAW AMM. R & R L4B SLAT POSITION SENSOR IAW AMM 27-84-03-4. SENSOR STILL REQUIRESDR FDEA201604061146Girt Bar · out of adjustLEFT CABIN DOOR SLIDE WILL NOT ARM WHEN CLOSED. READJUSTED GIRT BAR IAW MM 52-10-01-2. PERFORMED TEST IAW RMM 52-10-01-2.SDR FDEA201603090875Pump · leakingAPPROXIMATELY 50 MINUTES INTO FLIGHT, ANNUNCIATION, HYD 3 OFF. HYD 3 SYS SHOWED 2.0 AT THAT TIME. LEVEL CONTINUED TO DECREASE UNTIL 0.0. RECEIVED ANNUNCIATION, HYD 3 FAIL. USED ALTERNATE GEAR EXTENSION. TROUBLE SHOT ITEM & FOUND LEAK COMING FROM INBD STSDR FDEA201601270362Girt Bar · out of adjustL1 DOOR EMER SLIDE GIRT BAR WOULD NOT ENGAGE IN DOOR JAMB. UPON INSPECTION, FOUND GIRT BAR DISENGAGED FROM ITS LOCATOR PIN ON SLIDE PACK. RE-CENTERED GIRT BAR, PERFORMED OPERATIONAL TEST OF L1 DOOR SLIDE IAW AMM 52-10-01-2. TESTED OK ACFT OK FOR SERVICE.SDR FDEA201601030010Packing · deterioratedHYD 1 OFF, LEVEL 1 ALERT 2, 30 HOURS INTO FLIGHT AT FL 380, HYD SYS 1 INDICATING 2.8 GALS. FOUND HYD LEAK AT SYS 1 PRESS TRANSDUCER. FURTHER TROUBLESHOOTING FOUND PACKING DETERIORATED AT FITTING SIDE, REMOVED SYS 1 PRESS TRANSDUCER. R & R PACKING ON FITTINGSDR FDEA201511063504Girt Bar · out of positionUNABLE TO ARM L1 DOOR. REPOSITIONED L1 GIRT BAR IAW AMM 52-10-01-2. ACFT OK FOR SERVICE.SDR FDEA201501030013Power Supply · failedDURING EMER LIGHT TEST, GOT A LEVEL 1 EMER LIGHT BATTERY 1 LOW ALERT. REPLACED EMER EXIT LIGHT POWER SUPPLY IAW MM 33-51-01-4 & TESTED OK PER AMM 33-51-01-5.SDR FDEA201409232734Arming Lever · obstructedL1 DOOR SLIDE ARM LEVER IS DIFFICULT TO MOVE TO THE ARM POSITION AMM SMP. FOUND CORN NUT DEBRIS IN GIRT BAR TO DOOR FRAME AREA, REMOVED DEBRIS & GND TESTED NORMAL IAW MM.SDR FDEA201408062086Skin · damagedTO COMPLY WITH WORK CARD T1-5750-T0302286 PART 2 TITLE WINGS, FLIGHT SURFACES, RT INBD FLAP SKIN DAMAGE. INSTALL PERMANENT REPAIR. EA 1-5750-T0302286 PART 2 TITLE: "WINGS-FLIGHT SURFACES - RT INBD FLAP SKIN DAMAGE" HAS BEEN COMPLIED WITH. REPAIR CLASSFIED SDR FDEA201407291995Skin · dentedRIGHT WING INBD FLAP UPPER SURFACE FOUND NUMEROUS DENTS. REPAIRED IAW EA 1-5750-T0309945B PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407231926Doubler · crackedRIGHT WING LE LOWER ACCESS COMPARTMENT BEADED DOUBLER FOUND CRACKED XORS 695 DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR FDEA201407201872Skin · crackedLEFT FUSELAGE NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT UPPER AFT CORNER SKIN FOUND CRACK ABOUT 1 INCH IN LENGTH. DOOR CUTOUT UPPER AFT CORNER SKIN CARRIED OUT REPAIR AS PER SRM 53-20-15 REPAIR 3 FIGURE 201 REV 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2SDR FDEA201401110084Seal · leakingFUEL STREAMING FROM BOTTOM OF NR 1 ENGINE. LEAK COMING FROM BETWEEN NR 1 ENG FUEL PUMP & HEAT EXCHANGER. R & R SEAL BETWEEN FUEL PUMP & FUEL OIL HEAT EXCHANGER. WET MOTOR, NO LEAKS NOTED. RAN NR 1 ENGINE NO LEAKS NOTED IAW MM 73-12-01-4-1 & JRH. DURING SDR FDEA201401050021Light · inoperativeR1 DOOR PRESS TO TEST LAMP INOPERATIVE. R & R BULBS IAW AMM CHAPTER 25-61-04-4. OPERATIONS CHECKED GOOD.
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