N682FE

Service difficulty reports · 299

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 = 'N682FE' 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.

SDR FDEA201201160198Floorboard · crackedMDCC FLOORBOARD 231 ZG CRACKED AT UPPER AND LOWER SURFACES AND 2 EA SCREW HOLES CRUSHED. FABRICATED REPLACEMENT FLOORBOARD 231 ZG IAW DWG SRZ 25-005.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160197Floor Panel · damagedMAIN DECK FLOOR PANEL 241 AJ, 3 SECTIONS WHERE CLEVIS ATTACHES ARE CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL 241 AJ IAW DWG, SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160196Floorboard · damagedMDCC FLOORBOARD 323 TG HAS IMPACT DAMAGE AT UPPER SURFACE TOTAL DEFECT MEASURES 8.5" LONG. FABRICATED REPLACEMENT FLOORBOARD 232TG IAW DWG SRZ 25-005.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160195Floor Panel · crackedMDCC FLOOR PANEL 242 VG HAS 3 EA 8" CRACKS AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL 242 VG IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160194Floor Panel · damagedFLOOR PANEL 242 UJ HAS 5 AREAS THAT ARE CRUSHED WHERE CLEVIS ATTACHES. FABRICATED REPLACEMENT FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160193Floor Panel · damagedMAIN DECK FLOOR PANEL 241QH CENTER SECTION WERE CLEVIS ATTACHES IS CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL 241 QH IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160192Floor Panel · damagedMAIN DECK FLOOR PANEL 241 WH HAS 3 SECTION THAT ARE CRUSHED WHERE CLEVIS ATTACHES. FABRICATED FLOOR PANEL 241 WH IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160191Floor Panel · crackedMDCC FLOOR PANEL 232 NG HAS TWO, ONE INCH CRACKS AROUND CLEVIS ADAPTER CUTOUTS FABRICATED FLOOR PANEL 232 NG IAW DWG SRZ 25-005.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160190Floor Panel · crackedMACC FLOOR PANEL 241 GJ HAS 2 EA, 8" CRACKS CLEVIS ADAPTER CUTOUT FABBED FLOOR PANEL 241 GJ IAW DWG SRZ 25-005, REVJ.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160189Floorboard · crackedAFT CARGO FLOORBOARD 151 X F HAS 2 EA CRACKS ALONG EDGE 2 IN LONG ON BOTTOM SIDE FABRICATED REPLACEMENT FLOORBOARD 151 XF IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201160188Floorboard · damagedAFT CARGO FLOORBOARD 151 VF HAS A SECTION 1 IN BY 10 IN BROKEN OFF AT EDGE FABRICATED REPLACEMENT FLOORBOARD 151 VF IAW DWG SRZ 25-005, REV J.Jan 16, 2012 · N682FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201150184Web · crackedMDCC 260 ZONE WEB ASSY OTBD OF SEAT TRACK 5L BETWEEN FRAMES 79 AND 80/82 HAS A 2" CRACK. R & R WEB ASSY AT FRAME 79 AND 80/82 OTBD OF SEAT TRACK 5L IAW SRM 51-72-10.Jan 15, 2012 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201150183Web · corrodedMDCC 260 ZONE WEB ASSY OTBD OF SEAT TRACK 5R BETWEEN FRAME 79 AND 80/82 HAS A 1.5" CRACK. R & R WEB ASSY IAW SRM 51-72-10.Jan 15, 2012 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201150182Profile · corrodedAFT CARGO COMPARTMENT LT SIDE FRAME 63 TO FRAME 67 LOWER TRANSITION PROFILE HAS 18 SQ INCHES OF CORROSION AROUND FASTENER HOLES. R & R PROFILE AT FRAME 63 T0 FRAME 67 LT SIDE AFT CARGO COMPARTMENT IAW SRM 51-40-21.Jan 15, 2012 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201150181Fitting · crackedRT FUSELAGE FITTING AFT OF FRAME 47 BETWEEN STRINGERS 28 AND 29 RT HAS A 2 INCH LONG CRACK IN LOWER RADIUS. R & R RT FUSELAGE FITTING AFT OF FRAME 47 BETWEEN STRINGERS 28 AND 29 IAW FSRM 51-40-21 AND 51-72-10.Jan 15, 2012 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201150180Shear Plate · crackedFWD FUSELAGE, FR38 4IN., 3IN. OUTBD OF SEAT TRACK 6R, SHEAR PLATE CRACKED 2 INCHES LONG. R & R FWD FUSELAGE SHEAR PLATE SUPPORT IAW FSRM 51-72-10.Jan 15, 2012 · N682FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201201130158Floorboard · damagedFLOORBOARD 241HK CENTER SECTION IS CRUSHED WERE CLEVIS A TTACHES, FABRICATED REPLACEMENT FLOORBOARD 241 HK IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130169Seat Track · damagedMDCC SEAT TRACK 2L BETWEEN FR57 - FR57.1 HAS 2 EA AREAS WITH WORN SCALLOPS, DAMAGE 8 INCHES LONG. FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, FIG 102. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPLACEMENT SEAT TRACK SECTION AND REPAIR SPLICES, AND IJan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201130168Adapter · damagedMDCC FLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R GOUGED AT FR62. CLEVIS ADAPTER LOCATED AT FR62 BETWEEN SEAT TRACK 2R AND 3R HAS SCALLOPS TORN OUT AND IS OUT OF LIMITS IAW SRM 53-10-15, FIG 107. R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201130167Floorboard · damagedMAIN DECK 240, FLOORBOARD 242RJ CLEVIS ATTACHMENT SECTION IS BROKEN OFF. FABRICATED REPLACEMENT FLOORBOARD 242 RJ IAW SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130166Floorboard · crackedMAIN DECK FLOORBOARD 242LK HAS A 9" CRACK, FASTENER HOLE MISSING 1" SECTION OF CORE, AND END SECTION OF FLOORBOARD. FABRICATED REPLACEMENT FLOORBOARD 242 LK IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130165Floorboard · crackedFLOORBOARD 252GF, CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 GF IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130157Floorboard · crackedFLOORBOARD 241PF CRACKED 1.5 INCHES AT CLS ADAPTER CUT-OUT. FABRICATED REPLACEMENT FLOORBOARD 241 PF IAW DWG SRZ 25-005 REV JJan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130155Floorboard · crackedFLOORBOARD 252BF, CRACKED AT UPPER SURFACE 4 EA FABRICATED REPLACEMENT FLOORBOARD 252 BF IAW DWG SRZ 25-005. REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130154Floorboard · crackedFLOORBOARD 242 ZJ HAS 5 AREAS WERE CLEVIS ATTACHES THAT ARE CRUSHED AND ALSO A 9 '. CRACK FABRICATED REPLACEMENT FLOORBOARD 242 ZJ IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130153Floorboard · crackedFLOORBOARD 241 DF CRACKED AT 3 PLACES LOWER SURFACE. FABRICATED FLOORBOARD 241 DF IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130152Floorboard · damagedMAIN DECK FLOORBOARD 241 TH PANEL IS CRUSHED WHERE CLEVIS IS ATTACHED FABRICATED. FLOORBOARD 241TH IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201130151Floorboard · delaminatedFLOORBOARD 251 VF DISBONDED/ DELAMINATED AT UPPER SURFACE FABRICATED. REPLACEMENT PANEL 251VF IAW DWG SRZ 25-005, REV J.Jan 13, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120131Floorboard · delaminatedFLOORBOAR 251YG COMPOSITE MATERIAL SEPARATING, 8 IN LONG, UPP SURFACE. FABRICATED REPLACEMENT PANEL 251 YG IAW DWD SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120130Floorboard · crackedFLOORBOARD 252WH CRACKED AT UPPER SURFACE 1 EA. FABRICATED REPLACEMENT PANEL 252 WH IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120129Floorboard · crackedFLOORBOARD 252 UH CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 UH IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120128Floorboard · crackedFLOORBOARD 252PH CRACKED AT UPPER SURFACE 3 EA. FABRICATED REPLACEMENT PANEL 252 PH IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120127Floorboard · crackedMAIN CABIN FLOOR PANEL 251 BH HAS 3 EA CRACKS AT CLEVIS CUT OUT. FABRICATED REPLACEMENT PANEL 251BH IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120126Floorboard · crackedFLOORBOARD 252YG, CRACKED AT UPPER SURFACE 1 EA. FABRICATED REPLACEMENT PANEL 252YG IAW DWG SRZ 25-005, REJ.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120125Floorboard · crackedFLOORBOARD 252ZF, CRACKED AT UPPER SURFACE 2 EA. FABRICATED REPLACEMENT PANEL 252ZF IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120124Floorboard · delaminatedFLOODBOARD 251UH COMPOSITE MATERIAL SEPARATED AT UPPER SURFACE AROUND CLEVIS CUT-OUT, FABRICATED FLOORBOARD PANEL 251UH IAW DWG NR SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201120123Floorboard · damagedFLOORBOARD 242EK HAS 4 AREAS THAT ARE CRUSHED, WHERE CLEVIS ATTACHES, FABRICATED FLOORBOARD 242EK IAW DWG SRZ 25-005, REV J.Jan 12, 2012 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201201070448Rib · crackedNR 2 ENG PYLON RT RIB 20 HAS A 3" CRACK EXTENDING FROM RIVET TO PRODUCTION HOLE. REMOVED PRODUCTION DOUBLER, FABRICATED REPLACEMENT PRODUCTION DOUBLER AND 2 EA. REPAIR DOUBLERS, AND INSTALLED ALL DOUBLERS IAW SRM 54-54-11, AND DWG 41A54515196, REV A. MINORJan 7, 2012 · N682FE · Airbus A300F4605R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA200907152631Structure · damagedRUDDER TIP ATTACH LAND LT AND RT SIDES ARE DAMAGED. COMPLIED WITH E.O. 6-5540-127975.Jul 15, 2009 · N682FE · Airbus A300F4605R · Rudder StructureSDR FDEA200907132607Bracket · failedLT VERTICAL STAB CLIP NUT BRACKET UNDER FAIRING PANEL 323 AL IS BROKEN. REMOVED ANGLE BRACKET IAW SRM 51-40-21, PARA 6. FABRICATED ANGLE BRACKET IAW DWG F5357011; SHEET 2; REV "A". ALODINED AND PRIMED IAW SRM 51-23- 10; PG 1. APPLIES TOP COAT IAW SRM 51-23Jul 13, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907132604Bracket · corrodedAFT CARGO COMPARTMENT; FWD BULKHEAD PANEL NR 152 DW; ATTACH ANGLE IS CORRODED ON THE END AT STA 3354; FRAME 54 RT. REMOVED PANELS 152 DW AND 151 BW IAW AMM 25-13-31. INSTALLED PANELS 152 DW AND 151 BW IAW AMM 25-13-31. REMOVED BRACKET IAW SRM 51-40-21; PARAJul 13, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907092557Floor Panel · crackedMAIN CABIN FLOOR PANEL 242 TG IS CRACKED. FABRICATED FLOOR PANEL 242 TG USING THE OLD PANEL AS A TEMPLATE; LOCATED PANEL ATTACH HOLES; ROUTED AND POTTED EDGES; INSTALLED INSERTS; APPLIED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25-005, REV "H".Jul 9, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200907082538Support · crackedAVIONICS COMPARTMENT; THE BATTERY RACK INBD RAIL IS CRACKED AT THE FWD SUPPORT. REMOVED AND REPLACED SUPPORT TUBE IAW SRM 51-72-10; REMOVED AND REPLACED 2 EA BATTERIES IAW AMM 24-31-11-4.Jul 8, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907082537Skin · crackedFWD CARGO COMPARTMENT BALL MAT 132 XG IS PUNCTURED/CRACKED ON THE BOTTOM SKIN. REMOVED BOTTOM SKIN IAW SRM 51-72-10; PARA 5A. LOCATED AND DRILLED BOTTOM SKIN IAW SRM 51- 72-10; PARA 6A. ALODINED BOTTOM SKIN IAW SRM 51-21-10; PARA 2B3. PRIMED AND TOPCOATEJul 8, 2009 · N682FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200907082539Rail · crackedAVIONICS COMPARTMENT; THE BATTERY RACK INBD RAIL IS CRACKED AT THE CTR SUPPORT. REMOVED AND REPLACED EXTRUSION HAT IAW SRM 51-72-10.Jul 8, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907062497Frame · damagedFRAME 41; LEFT SIDE AT STRINGER 35; HAS A DOUBLE DRILLED HOLE IN THE FOOT FITTING. COMPLIED WITH E.A. 6-5310-127976.Jul 6, 2009 · N682FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA200907022463Floor Support · crackedMAIN CABIN FLOOR SUPPORT LINK AT FRAME 48 & BL Y 1456 IS CRACKED. REMOVED AND REPLACED DAMAGED TRACK LINK IN REF TO DWG A53812067.Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907022461Bracket · crackedFWD CARGO COMPARTMENT AFT FIRE BOTTLE MOUNT BRACKET BEAM IS CRACKED AT THE MOUNT HOLES. REPLACED BRACKET IAW SRM 51-72-10.Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200907022458Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD DENTED / CRACKED ZONE Z241; PANEL GK AT FRAME 51. FABRICATED NEW FLOORBOARD 241 GK IAW DWG SRZ 25-005; REV "H".Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200907022455Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132 MG HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 132 MG IAW DWG SRZ 25-005, REV "H".Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
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