N664FE
Service difficulty reports · 307
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 = 'N664FE' 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 = 'N664FE' 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 FDEA201212144306Floorboard · delaminatedAFT CARGO FLOORBOARD 151QF HAS CORNER DELAMINATED AND .7500" PUNCTURE ON THE BACK. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201212144305Floorboard · delaminatedBULK CARGO COMPT FLOORBOARD 161 CF, HAS 2 EA DENT W/DELAMINATION CORE MEASURING 2.5 X 2" & 1 X .75" AT UPPER SURFACE AND 12 EA AREAS OF CORROSION AT LWR SURFACE, MEASURING APPROX 16 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201212144296Floor Panel · crackedFLOORBOARD 262MF HAS APPROX. 6 INCH CRACK IN CENTER OF BOARD. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201212134294Floorbeam · crackedFWD CARGO BAY AT FR 31 BETWEEN SEAT TRACKS 4L AND 5L FLOORBEAM CRACKED AT STIFFENER. REMOVED DAMAGED AREA FR 31 SEAT TRACK 4L AND 5L FLOORBEAM IAW SRM 53-10-15 PARA 15 FIG 212 SHEET 1&2 NDT FOR CRACKS PER 51-10-08, NO CRACKS FOUND. FABRICATED REPAIR CHANNSDR FDEA201212134293Floorbeam · crackedFWD CARGO AT FR 32 BETWEEN SEAT TRACKS 4L AND 5L FLOORBEAM IS CRACKED AT STIFFENER. REMOVED DAMAGED AREA SEAT TRACK 4L AND 5L FLOORBEAM IAW PARA 15 FIG. 212 SHEED 1&2 NDT FOR CRACKS PER NDT 51-10-08 . NO CRACKS FOUND. FABRICATED REPAIR CHANNEL AND FILLER, MASDR FDEA201211184073Bushing · corrodedCORROSION INSIDE BUSHING OF FWD ECCENTRIC LUG OF RT MLG FWD CROSS BRACE (OTBD END) R & R RT MLG FWD CROSS BRACE ECCENTRIC BUSHING IAW A32140045. ADJUSTED RT MLG FWD CROSS BRACE ECCENTRIC BUSHING IAW DWG A32140045. FOLLOW UP INSTALLATION OF RT MLG CROSS BRACESDR FDEA201211184072Bushing · corrodedCORROSION INSIDE BUSHING OF FWD ECCENTRIC LUG OF LT MLG FWD CROSS BRACE ATTACH (OTBD END) R & R LT MLG FWD CROSS BRACE ECCENTRIC BUSHING IAW DWG A32140045. ADJUSTED LT MLG FWD CROSS BRACE ECCENTRIC BUSHING IAW DWG A32140045. FOLLOW UP INSTALLATION OF LT MLG CRSDR FDEA201111154924Gcu · inoperativeAT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, NR 2 GENERATOR FAILED WITH ASSOCIATED ECAM WARNINGS FOR EQUIPMENT ON NR 2 BUSS. REJECTED TAKEOFF AND RETURNED TO BLOCKS. R & R NR 2 GCU (2XU) WITH APU GCU IAW AMM 24-22-12-04-0. OPS CHECKED NR 2 GENERATOR AT IDLE ONSDR FDEA201110274669Bulb · burned outON GEAR EXTENSION ON APPROACH, NOSE GEAR DOWN INDICTIOR DID NOT SHOW GREEN ON OVERHEAD SYS. LIGHT TEST INDICATED BULBS BURNED OUT. REPLACED 2 BULBS AND THEN GOT 3 GREEN INDICATIONS ON OVEHEAD PANEL.SDR FDEA201101260361Support Angle · crackedNR 2 ENG, LT THRUST REVERSER HINGE COVER SUPPORT ANGLE CRACKED. ACCOMPLISHED REPAIR IAW EA 6-7830-141662.SDR FDEA201101260360Support Angle · crackedNR 1 ENG. LT THRUST REVERSER HINGE COVER SUPPORT ANG L/E CRACK. ACCOMPLISHED REPAIR IAW EA 6-7830-141662.SDR FDEA201101250359Support Angle · crackedNR1 ENG RT THRUST REVERSER HINGE COVER SUPPORT ANGLES CRACKED. ACCOMPLISHED REPAIR IAW EA 6-7830-141662.SDR FDEA201101200320Rib · crackedRT WING INBD FLAP RIB 25A UPPER RAD II OF THE HORIZ UPPER FLANGE CRACKED. REPLACED WITH NEW RIB AND CHECK CONDITION NORMAL. REP AIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201101200319Rib · crackedLT WING INBD FLAP, RIB 25A UPPER RADII OF THE HORIZONTAL UPPER FLANGE CRACKED. REPLACED WITH NEW RIB AND CHECK CONDITION NORMAL. REP AIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201101200317Ring · crackedNR 2 ENG RT THRUST REVERSER TORQUE BOX UPPER SIDE FRAME RING CRACKED LENGTH ABOUT 2". ACCOMPLISHED REPAIR IAW DWG NR:SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201101180223Shim · migratedRT NR6 FLAP TRACK OTBD SHIM MIGRATION FOUND AREA L X W X T 1" X 0.050" X 0.003" 1. IAW EA6-5750-123612 REPAIR ACCOMPLISHED. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR. PAINTER TOUCHED UP IAW AB6F SRM 51-75-10.SDR FDEA201101170201Carriage · misalignedLT WING NR 4 FRONT CARRIAGE UPPER BRIDGE SHIM GOT MIGRATION (INBD AND OTBD) IAW EA6-2750-14659 REPAIR ACCOMPLISHED. IAW GMM:6-2-100 REPAIR CLASSIFIED AS MINOR.SDR FDEA201101170192Carriage · misalignedLT WING NR 3 FRONT CARRIAGE UPPER BRIDGE SHIM GOT MIGRATION (INBD) IAW EA 6-2750-141659, REPAIR ACCOMPLISHED. IAW GMM:6-2-100 REPAIR CLASSIFIED AS MINOR.SDR FDEA201101170189Carriage · misalignedRT WING T/E FLAP NR5 CARRIAGE UPPER BRIDGE OTBD SHIM EXTRUDED. IAW EA6-2750-141659 REPAIR ACCOMPLISHED. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.SDR 08FDEA03583Channel · crackedE/E COMPARTMENT, BATTERY FWD MOUNT CHANNEL IS CRACKED. REMOVED MOUNT CHANNEL IAW SRM 51-40-21. COMPLIED WITH EA 6-5320-117009. RE-INSTALLED REPAIRED MOUNT CHANNEL IAW SRM 51-40-21.SDR 08FDEA03575Panel · crackedLEFT AILERON BOOSTER PANEL IS CRACKED. REPLACED THE LEFT AILERON BOOSTER PANEL IAW A300-600 AMM 27-11-28-4.SDR 08FDEA03574Panel · crackedRIGHT SIDE WING BOX REAR SPAR BOTTOM PANEL HOLE "U" HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION FOUND WITH BHEC. REPAIRED THE RIGHT SIDE WING BOX REAR SPAR BOTTOM PANEL HOLE "U" IAW EA 6-5710-117013 "FUSELAGE - AD 2005 -23 - 08 - S/B A300-57-0649R06 FRAMSDR 08FDEA03573Pan · gougedFWD CARGO COMPART, EMT BALL MAT 131 XG PDU PAN IS GOUGED AT A MOUNT HOLE. REPAIRED BALL MAT 131 XG PDU PAN IAW EA 6-2550-117025.SDR 08FDEA03551Skin · gougedMAIN CARGO DOOR LOWER AFT CORNED OF THE EXTERIOR SKIN IS GOUGED. REPAIRED THE GOUGED AREA IAW EA 6-5230-123389.SDR 08FDEA03550Panel · crackedTHE NR 1 ENGINE PYLON PANEL NR 475 AL HAS A 3/8 INCH CRACK AT THE RADIUS. COMPLIED WITH FEDEX EA 6-5480-123386 "NACELLES/PYLON, NR 1 ENGINE PYLON 475 AL EQUIPMENT ACCESS PANEL ASSY, CRACK WELD REPAIR".SDR 08FDEA03543Panel · chafedRIGHT WING LOWER T/E PANEL NR 675 CB INNER SKIN OF THE PANEL AND PANEL LAND ON THE AIRFRAME SIDE IS CHAFED WITH BARE METAL. REPAIRED AREAS BY BLENDING CHAFFED AREAS AND BONDING A REPAIR DOUBLER IAW EA NR 6-5720-123622. ALODINED, PRIMED AND PAINTED PER A033-6SDR 08FDEA03506Skin · crackedLEFT WING INBD FLAP L/E HAS A DENT APPROXIMATELY 6' FROM THE INBD EDGE OF THE FLAP. REPAIRED THE LEFT WING INBD FLAP L/E SECTION IAW SRM 57-50-00, FIG 208.SDR 08FDEA03404Skin · gougedLEFT WING INBD FLAP T/E UPPER SURFACE EXTERNAL SKIN IS GOUGED IN TWO PLACES. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-73-10. GOUGED INBD FLAP UPPER SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00; PG 108. FABBED REPAIR AND INSTALLED BOTH IAW A300-6SDR 08FDEA03387Floor Panel · damagedMAIN CARGO DECK PANEL 262 AH HAS A CRACK ON THE LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1001.SDR 08FDEA03386Floor Panel · damagedMAIN CARGO DECK PANEL 262 AH HAS AN INSERT PULLING LOOSE ON THE AFT LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1001.SDR 08FDEA03379Floorboard · damagedMAIN CARGO FLOORBOARD 242 ZJ IS CRACKED. FABRICATED NEW FLOORBOARD NR 242 ZJ IAW FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03291Panel · damagedMAIN CARGO DOOR PANEL NR 251 WHM IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03290Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 VH, IS CRUSHED; CRACKED; HAS BROKEN INSERTS AND IS PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03289Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 UM, IS CRUSHED, CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03288Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 TH, LOWER SURFACE IS CRACKED AND PUNCTURED ON THE UPPER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03287Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 UH, IS CRACKED AND CRUSHED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03286Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 WH, IS CRACKED AND HAS A HOLE IN THE LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03285Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 YG, IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03284Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 XG; IS CRACKED; HAS EDGE DAMAGE AND PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03283Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 VF; IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03282Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 VF; FWD END IS CRACKED AND HAS SEVERAL PUNCTURES. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03281Panel · damagedMAIN CARGO DOOR PANEL NR 251 YG; LOWER SURFACE IS CRACKED AND THE UPPER SURFACE IS PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03280Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 BH, CENTER CUT-OUT IS CRACKED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03279Floor Panel · crackedMAIN CARGO DOOR PANEL NR 251 AH; UPPER AND LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03278Floor Panel · puncturedMAIN CARGO DOOR PANEL NR 261 UF, LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".SDR 08FDEA03292Frame · crackedFRAME 44 FROM STRINGER 25L TO STRINGER 26L, FASTENER HOLE "B" AS CALLED OUT IN EO E6-5310-7-5006 PT1 STEP 70 STILL SHOWS A CRACK INDICATION AFTER REAMING IT TO A MAX SIZE OF 0.437. REMOVED FRAME 44 SECTION FROM S22-27L IAW SRM 51-40-21, PARA 'S 6 AND 7. RECESDR 08FDEA03277Floor Panel · puncturedMAIN CARGO DOOR PANEL NR 261 RF, FWD OUTBD LOWER SURFACE IS PUNCTURED. FABRICATED PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".SDR 08FDEA03270Keelbeam · gougedMAIN LANDING GEAR WHEEL WELL AFT OF THE KEEL BEAM BOX AT FRAME 54, THE RIGHT AFT SIDE OF THE BOX MARKED IN RED. THE FITTING IS GOUGED.SDR 08FDEA03239Skin · dentedRIGHT WING INBD FLAP UPPER SKIN IS DENTED 5' FROM THE INBD END. SMOOTHED AREA AROUND THE DENT IAW A300-600 SRM 51-73-10. ORIGINAL MATERIAL 0.031 IAW SRM 57-52-12; ITEM 45. MATERIAL REMOVED 0.002. MATERIAL REMAINING 0.029, FOUND TO BE OUT OF LIMITS IAW ASDR 08FDEA03238Skin · gougedRIGHT WING INBD FLAP UPPER SKIN 1 INCH FROM THE INBD END IS GOUGED. BLENDED GOUGE IAW A300-600 SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 IAW A300-600 SRM 57-52-12; ITEM 45. REMOVED 0.004. REMAINING MATERIAL 0.027 AND FOUND TO BE OUT OF LIMITS IAW A
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