N601FE
Service difficulty reports · 546
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 = 'N601FE' 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 = 'N601FE' 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 FDEA201202210632Support · corrodedMLG RT W/W T/E ADJACENT AREA OF TRAPEZOIDAL FITTING STRUCTURE SUPPORT FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA 1-5710-154300. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202170602Bushing · corrodedRT WING, FLAP SIDE INBD FLAP HINGE INBD PIVOT HOLE BUSHING WORN. REPAIRED AS PER EA#1-5750-159802. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.SDR FDEA201202170600Hinge Bracket · corrodedRT WING - ACFT SIDE OTBD FLAP HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REMOVED CORROSION IAW EA 1-5750-76663B PART 3.SDR FDEA201202170601Hinge Fitting · wornLEFT WING FLAP SIDE INBD FLAP HINGE INBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159801, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202160592Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 595 X=-47 TO -75. REPAIRED IAW EA 1-5310-154298. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202140571Vane · corrodedRT WING OTBD FLAP VANE FITTING C ECCENTRIC BOLT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-150432, PART 1. EXISTING HOLE SIZE: 0.880" X 0.625" FINAL HOLE SIZE 0.956" X 0.658" . BUSHING INSTALLED IAW EA1-5750-150432. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100,SDR FDEA201202140570Vane · corrodedRT WING OTBD FLAP VANE FITTING E ECCENTRIC BOLT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-150432, PART 1. EXISTING HOLE SIZE: 0.923" X 0.606" FINAL HOLE SIZE 0.973" X 0.668" MAX ALLOWABLE LIMIT 0.940" X 0.670". BUSHING INSTALLED IAW EA. REPAIR CLASSIFISDR FDEA201202130566Hinge · corrodedDURING FPI INSPECTION ON LEFT WING INBD FLAP, FLAP SIDE INBD PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-159801. EXISTING HOLE DIA 1.253" FINAL HOLE DIA 1.255'. MAXIMUM HOLE DIA 1.220' . BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-159801, PART 1. RSDR FDEA201202130565Hinge Fitting · corrodedDURING FPI INSPECTION ON RT WING INBD FLAP, FLAP SIDE INBD PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-157802 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202120557Bushing · corrodedLEFT WING - WING SIDE FLAP OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORROSION. REWORKED IAW EA 1-5750-76015A. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76015A . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. EXISTING HOLE DIA 1.222" FINAL HOLE DIA SDR FDEA201202120560Floorbeam · corrodedCABIN FLOORBEAM FOUND CORRODED AT STA 460 X= 48 TO X =53. REMOVED IAW SRM 51-31-01, REV 48 AND INSTALLED NEW FLOORBEAM IAW AMM 20-50-02, REV 70.2. NEW FLOORBEAM REPLACED IAW DWG ACA7364-1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114SDR FDEA201202120559Bushing · wornLEFT WING, FLAP SIDE INBD FLAP HINGE OTBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159801, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202120558Bushing · wornRIGHT WING, FLAP SIDE, INBD FLAP HINGE, OTBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159802, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202120556Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.253", MAX HOLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76015A PART 2, SSDR FDEA201202120555Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. UPPER EXISTING THICKNESS;0.401" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.399" LOWER EXISTING THICKNESS : 0.417" MATERIAL REMOVED: 0.00SDR FDEA201202120554Hinge Fitting · corrodedLEFT WING, WING SIDE, OTBD FLAP, OTBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.416" INBD FWD MATERIAL REMOVED :0.002" REMAINING THICKNESS:0.414" OTBD EXISTING THICKNSDR FDEA201202120553Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP OTBD HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. INBD AFT EXISTING THICKNESS;0.414" MATERIAL REMOVED : 0.008" REMAINING THICKNESS : 0.406" OTBD AFT EXISTING THICKNESS : 0.399" MATERIAL REMOVED:SDR FDEA201202120552Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE OTBD HOLE BUSHING WORN OUT. REPAIRED IAW EA 1-5750-76665A, PART 2, STEP 6. EXISTING HOLE DIA 1.221" MAX. ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A. REPAIR SDR FDEA201202120551Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE INBD HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A, PART 2, STEP 6. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A, PART 2, STEP 6. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202120550Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-76665A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.447" INBD FWD MATERIAL REMOVED:0.008" REMAINING THICKNESS: 0.439" OTBD EXISTING THICKNESDR FDEA201202120549Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT AFT SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5750-76665A PART 2, STEP 3 AND 4. OTBD AFT EXISTING THICKNESS :0.439", MATERIAL REMOVED 0.015", REMAINING THICKNESS 0.424". INBD AFT EXISTING THICKNESS :0.4SDR FDEA201202120548Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE PIVOT HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A PART 2. NEW BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76665A PART 2, STEP 6 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090531Hinge Fitting · corrodedRT WING, WING SIDE OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02, REV 72. EXISTING THICKNESS :0.434" MATERIAL REMOVED :0.002" REMAINING THICKNESS : 0.432". FOUND WITHIN LIMITS IAW DWG ARC0502 SHEET 4, SDR FDEA201202090530Bushing · wornRT WING WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BUSHING WORN OUT. R & R WITH NEW BUSHING IAW EA 1-5750-76664A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201202090529Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD HINGE SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. CORROSION REMOVED IAW EA 1-5750-76663B, PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090528Hinge Fitting · corrodedRT WING OTBD FLAP OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. RT WING - ACFT SIDE OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORROSION. CORROSION REMOVED IAW EA 1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV SDR FDEA201202090527Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. CORROSION REMOVED IAW EA 1-5750-76663B, PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090526Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. CORROSION REMOVAL ACCOMPLISHED IAW EA1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090525Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. CORROSION REMOVAL ACCOMPLISHED IAW EA 1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090524Bushing · wornRIGHT WING OTBD FLAP, OTBD HINGE PIVOT HOLE BUSHING WORN OUT. BUSHING REPAIRED IAW EA 1-5750-76663B, PART 3. EXISTING HOLE DIA 2.331" MAX ALLOWABLE DIA 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76663B, PART 3, STEP 6 AND 11. REPAIR CLASSISDR FDEA201202060499Access Panel · crackedRT WING L/E LOWER SURFACE ACCESS PANEL 619CB CUTOUT FWD INBD CORNER FOUND SUSPECTED CRACK. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202060498Skin · crackedSKIN AROUND FOUR FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND 713.6. REPAIR CARRIED OUT IAW EA 1-5710-154293, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100,SDR FDEA201202060497Skin · crackedSKIN AROUND SIX FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS =683.4 AND 713.6. REPAIR CARRIED OUT IAW EA 1-5710-154294, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10SDR FDEA201202060496Seat Track · wornSEAT TRACK LOPE AT BS 635 RBL 8 WORN. REMOVED AND REPLACED WITH A NEW REWORKED SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202060495Seat Track · wornSEAT TRACK LOPE AT STA 635 X=-47 WORN. TRIMMED OUT AND CARRIED OUT REPAIR IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202060494Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT BS 675 - 695 X= -27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52 FIG 201 REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202060493Longeron Splice · corrodedFWD CARGO COMPT STA 6-50-STA 6-73. DURING REPAIR OF LONGERON 52 FOR CORROSION FOUND SPLICE FITTING REPAIR WITH CORROSION. REMOVED AND CARRIED OUT REPAIR IAW SRM 53-00-05, FIG 202, REPAIR 1, REV 48. NEW REPAIR LONGERON SPLICE FABRICATED IAW SRM 53-00-05, FIGSDR FDEA201202040472Floor Support · crackedBS 405 , X 44 LT UPPER CABIN FLOOR SUPPORT FOUND CRACKED . FLOOR SUPPPORT R & R IAW SRM 51-31-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030463Seat Track · corrodedSEAT TRACK FLANGE CORRODED AT STA 645-655 X= -75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030462Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 625-675 X =-27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030461Seat Track · wornSEAT TRACK LOPE FOUND WORN AT STA 635 X=27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030460Seat Track · wornSEAT TRACK LOPE FOUND WORN AY STA 635 X=47. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030459Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT BS 615-625 X=-27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030458Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT BS 635-675 X=-47. TRIMMED OUT AND CARRIED OUT REPAIR IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030457Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA. 595-605 X=-75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030456Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 505-515 X=-75. SEAT TRACK REPAIRED IAW EA 1-5310-159803 AND SRM 53-00-52, FIG 201. REPAIR 1, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030455Longeron · crackedLONGERON 27 LT FOUND CRACKED AT BS 1219 - 1239. LONGERON R & R IAW SRM 51-31-01, REV 48, NEW LONGERON FABRICATED IAW EA 1-5310-154296. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202030454Skin · chafedRIGHT WING TELESCOPIC DUCT CUTOUT FOUND CHAFED. REPAIRED AREA IAW SRM 51-31-01, REV 48. DOUBLER FABRICATED SRM 57-40-01, REPAIR 10 FIG 201, REV 48. FABRICATED DOUBLER INSTALLED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6SDR FDEA201202030453Skin · chafedLEFT WING FIXED L/E ANTI-ICE DUCT CUTOUT FOUND CHAFED. CUTOUT AREA IAW SRM 51-31-01, REV 48. DOUBLER FABRICATED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. FABRICATED DOUBLER INSTALLED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. REPAIR CLASSIFIED MASDR FDEA201202030452Skin · chafedRIGHT WING INBD AILERON L/E EXTERIOR SURFACE FOUND CHAFING. REPAIR CARRIED OUT IAW EA 1-5750-154291. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
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