N690FE
Service difficulty reports · 127
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 = 'N690FE' 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 = 'N690FE' 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 FDEA201112155281Fuel Cell · contaminatedIN CRUISE, BOTH CTR TANK PUMPS FAULTED FOLLOWED BY LT OUTER TANK QTY WINDING DOWN TO ZERO. SUMPED ALL TANKS AND FOUND SOME WATER IN LT OUTER TANK ONLY. ENTIRE TIME TRANSFERING FUEL OUT OF LT OUTER TANK AND QTY INDICATION WER STABLE. SUMPED LT OUTER TANK AGAISDR FDEA201110244628Skin · chafedLT WING FIXED L/E RIB 18 HAS 2EA CHAFE MARKS FROM SLAT UP STOP ASSY'S DEFECT MEASURES .25 X .18 X .002 AND .18 X .12 X .002. R & R FIXED L/E NOSE SKIN IAW FSRM 57-41-12, PG 217 L/E.SDR FDEA201110214608Support Bracket · crackedNR 2 ENG PYLON AFT END AT WING REAR SPAR INTERFACE HYD LINES SUPPORT BRACKET HAS 3 EA. CRACKS AT FASTENERS 2 EA 1" AND 1 EA 3" LONG R & R NR2 ENG PYLON AFT END REAR SPAR SUPPORT BRACKET IAW SRM 51-72-10.SDR FDEA201110214607Support Bracket · crackedNR1 ENG PYLON AFT END REAR SPAR INTERFACE HYD LINES SUPPORT BRACKET HAS 4 EA CRACKS AT FASTENERS 3 EA 1" AND 1 EA .3" LONG R & R NR 1 ENG PYLON AFT END AT WING REAR SPAR SUPPORT BRACKET IAW SRM 51-72-10.SDR FDEA201110204604Skin · dentedRT WING AILERON, LWR T/E SURFACE HAS A 1.64 X 1.26 X .031" DENT AT CENTER POSITION. REPAIRED 1EA DENT ON RT AILERON LWR T/E SURFACE AND APPILIED PROTECTIVE COATING IAW SRM 57-61-11, SRM 51-77-12 (4C), AND SRM 51-75-10 (3C) REF EA 6-5750-15609 FOR RSC TRACKINGSDR FDEA201110204603Skin · damagedRT WING ALL SPEED AILERON BOTTOM SURFACE T/E PUNCTERED 1EA DIMENSION APPROX L=0.5 X W=0.3. REPAIRED 1EA PUNCTURE ON RT ALL SPEED AILERON BOTTOM SURFACE T/E AND APPILIED PROTECTIVE COATING IAW SRM 57-61-11, SRM 51-77-12 (4C) AND SRM 51-75-10 (3C). REF EA 6-57SDR FDEA201110184570Support · crackedFWD CARGO DOOR CUTOUT, LOWER FWD CORNER TEE SUPPORT AT FR 20 CRACKED. R & R ANGLE PROFILE AT FR20A IAW FRSM 51-40-21, PARA 6 & 7.SDR FDEA201110134459Torque Box · crackedNR1 ENGINE INBD THRUST REVERSER FWD UPPER TOP CORNER CRACK 4 INCHES. REPAIRED NR1 ENGINE INBD THRUST REVERSER TORQUE BOX UPPER CORNER IAW SRM 51-40-21 AND DWG SRZ 78-002. PERFORMED NTD IAW SRM 70-32-03 TO VERIFY CRACK DOES NOT EXTEND AFTER STOP DRILL. LOCATSDR FDEA201110134478Support · crackedLT WING T/E PANEL AT RIB 15 INTERNAL WEB SUPPORT HAS A CRACK AT THE ATTACH LEG FWD BOTTOM SKIN STOP DRILLED CRACK ON LT WING T/E AT RIB 15 INTERNAL WEB SUPPORT ATTACH LEG FWD BOTTOM SKIN IAW SRM 51-73-10 AND SRM 57-51-00. NDT FOUND NO CRACK IAW NTM 51-10-08.SDR FDEA201110134475Support · crackedRT WING T/E PANEL AT RIB 10 BOTTOM SKIN INTERNAL WEB SUPPORT HAS A CRACK. STOP DRILLED CRACK IAW SRM 51-73-10 AND SRM 57-51-10. NDT IAW NTM 51-10-08 SHOWS NO CRACK INDICATION PAST STOP DRILLED HOLE. FABRICATED REPAIR DOUBLER IAW SRM 51-71-30. ALODINED, PRISDR FDEA201110124455Door Frame · dentedFWD CARGO DOOR CUT-OUT FWD EDGE INTERIOR SIDE HAS A DENT APPROX 6.0L X .40W. REMOVED AND REPLACED PARTIAL FRAME BETWEEN S34 AND 45R IAW EA 6-5310-156035.SDR FDEA201110084384Shear Plate · crackedMAIN CABIN COMPARTMENT RT SIDE AT FR 79 AND FR 80 HAS A CRACKED WEB SUPPORT 1.5" LONG. R & R MAIN CABIN COMPARTMENT RT SIDE WEB SHEAR SUPPORT AT FR 79 AND FR 80 IAW SRM 51-72-10.SDR FDEA201110074377Frame · crackedNR1 ENGINE OTBD THRUST REVERSER UPPER UPPER TOP CORNER CRACKED 4". REPAIRED NR1 ENGINE OTBD THRUST REVERSER TORQUE BOX UPPER CORNER IAW SRM 51-40-21 AND DWG SRZ 78-002. PERFORMED NTD IAW SPM 70-32-03 TO VERIFY CRACK DOES NOT EXTEND AFTER STOP DRILL. LOCATEDSDR FDEA201110074375Channel · chafedNR 2 ENG INBD T/R C-DUCT REAR FAIRING 6 O`CLOCK POSITION HAS A CHAFE MARK AT OTBD SIDE. R & R NR 2 ENGINE T/R C-DUCT FAIRING AT 6:00 POSITION IAW SRM 54-04-01, REPROTECTED FAIRING IAW SRM 54-02-03.SDR FDEA201110074374Channel · chafedNR2 ENG INBD T/R C-DUCT 6'OCLOCK FAIRING REAR SIDE HAS A CHAFE MARK AT OTBD SIDE. R & R NR 2 ENGINE INBD T/R C-DUCT REAR CHANNEL FAIRING IAW SRM 54-04-01 AND REPROTECTED IAW SRM 54-02-03.SDR FDEA201110074372Channel · chafedNR2 ENG LT THRUST REVERSER C-DUCT 6 O'CLOCK FAIRING FWD EDGE CHAFE MARK 1 SQ INCH. R & R FWD SUPPORT CHANNEL ON NR 2 ENGINE LT T/R C-DUCT IAW SRM 54-04-01, AND REPROTECTED SUPPORT CHANNEL IAW SRM 54-02-03.SDR FDEA201110074380Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 242BF HAS 2 EA BROKEN CORNERS. INSPECTION REF AMM 53-10-20-06 FABRICATED REPLACEMENT FLOOR PANEL 242BF IAW DWG SRZ-25-005, REV J . MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201110074379Floor Panel · crackedFLOOR PANEL 242EF HAS 3 EA 2" CRACKS, 1EA 5" CRACK, 1EA DAMAGE FASTENER HOLE FABRICATED REPLACEMENT FLOOR PANEL 242EF IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201110064350Floorboard · damagedFLOOR PANEL 262 ZF IS BROKEN COMPLETELY ACROSS ON THE LOWER PLY APPROX 16" FROM AFT EDGE FABRICATED FLOOR PANEL 262 ZF DWG SRZ 25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201110064349Floorboard · tornFLOORBOARD 261QF HAS 2 EA FASTENER INSERTS TORN OUT. FABRICATED FLOORBOARD 261QF IAW DWG SRZ 25-005 FEV J MAJOR REPAIR GMM 6-2-100.SDR FDEA201110064332Profile · wornTAILCONE ACCESS DOOR 317AL HOLD OPEN ROD VERTICAL ATTACH FTG ON TAILCONE INBD T/E WORN. R & R VERTICAL PROFILE ATTACH FITTING IAW SRM 51-72-10 AND 51-40-21. REPROTECTED PROFILE AT FRAME 103 BETWEEN STR 7L - STR 15L IAW SRM 51-75-10.SDR FDEA201110054317Bracket · brokenRT WING CENTER FLAP OTBD CLOSING RIB 16 HAS A BROKEN ANGLE BRACKET. R & R 1 EA ANGLE BRACKET ON RT WING CENTER FLAP OTBD CLOSING RIB 16 IAW SRM 51-40-21 PG 7 A (1).SDR FDEA201110044292Seat Track · gougedSEAT TRACK 1 CTR INBD SIDE CLEVIS ADAPTER SCALLOP HAS A SMALL GOUGE. REMOVED CLS ADAPTER IAW SRM 51-40-21, CLEANED CLS ADAPTER AND PAINTED SCRATCHES IAW SRM 51-13-10, SMOOTHED/BLENDED SCRATCHES IAW FSRM 51-73-10 PARA 5 FIG 201, NO MEASURABLE MATERIAL LOSS ANDSDR FDEA201110024268Support · crackedMAIN CABIN LT SIDE AT FR 79 AND FR 80 HAS A CRACKED WEB SUPPORT 1 INCH LONG. R & R WEB SUPPORT IAW SRM 51-72-10. REPROTECTED AREA IAW SRM 51-75-10.SDR FDEA201109294206Floor Panel · delaminatedACFT BAY FLOOR PANEL 143DF HAS 30 SQ IN OF DELAM ON BOTTOM SIDE REF AMM 53-10-20-06. FABBED FLOOR PANEL 143DF IAW DWG SRZ 25-005 REV J, MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA200912104397Landing Gear · malfunctionedRECEIVED LANDING GEAR RETRACT FAULT--UNABLE TO RETRACT LANDING GEAR N T/O FROM RWY 28 KORD. TRIED BOTH SYS 1 AND SYS 2 WITH NO LUCK. REF TO AMM 32-31-71-4, TESTED PROXIMITY PROCESSING UNIT AND FOUND FAULT "BL", LT BOOGIE SENSOR. FOUND LT PITCH DAMPER AT SDR FDEA200904291464Skin · dentedDURING WALKAROUND AT KMCO SMALL DEPRESSION DISCOVERED IN LEADING EDGE OF RIGHT WING, FIRST PORTION OF SLATS TOWARD ACFT FUSELAGE DENT ON RT WING NR 1 SLAT FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED FLUSH DOUBLER REPAIR IAW FEDEX EA 6-5750-124265.
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