N652FE

Service difficulty reports · 320

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 = 'N652FE' 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 FDEA201111094848Floorbeam · corrodedFLOORBEAM AT FR47 BETWEEN SEAT TRACKS NR1-2L UP SIDE CORRODED AT BOTH ENDS REF AMM 53-10-15-06, ZONE 240. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-74-10. FLOORBEAM IS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50 PERCENT MATERIAL LOSS. MATERIAL THICKNESSNov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111094851Door · chafedRT NLG SECONDARY DOOR INTERNAL UPPER SURFACE HAS A 2.25 X .5 X .37" GOUGE FROM ACTUATING CYLINDER GREASE ZERT FITTING. BROKE SHARP EDGES ON GOUGE IAW SRM 51-73-10. FABRICATED REPAIR ANGLE IAW SRM 51-26-10. HEAT TREATED ANGLE IAW SRM 51-28-10. COMPLETED CONDNov 9, 2011 · N652FE · Airbus A300F4605R · Landing Gear DoorsSDR FDEA201111094850Angle · missingRT WING OTBD FLAP INBD CLOSING RIB ANGLE BRACKET IS MISSING ADJACENT TO CTR FLAP OTBD CLOSING RIB. INSTALLED ANGLE BRACKET ON RT OTBD FLAP INBD CLOSING RIB IAW SRM 51-40-21.Nov 9, 2011 · N652FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201111094849Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LOWER RT SIDE FUSELAGE SKIN BETWEEN FRAMES 63 TO 65 AND BETWEEN STRINGERS 47 TO 49 RT BELOW LAP SEAM IS INSTALLED AT LAP SEAM LINE AND SHOULD BE COVERING ABOVE AND BELOW LAP SEAM AND THE SKIN HAS NO CUT OUT. REMNov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111094846Seat Track · corrodedSEAT TRACK 4L CORRODED FROM FR42 TO 43 PANEL LANDING AREA REF AMM 53-10-15-06. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 103, FIG 101. R & R SEAT TRACK SECTION IAW SRM 51-72-10.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111094845Skin · misrepairedSKIN BETWEEN FRAMES 19 TO 20 AND BETWEEN STRINGERS 52 AND 54 MISREPAIRED. REPAIRED IAW SRM 51-40-21 PAGE 22 AND SRM 53-10-12 FIG 208, SHEET 2 PAGES 279 TO 286.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111094844Floorboard · crackedFLOORBOARD 151VF CRACKED IN HALF AND MULTIPLE CRACKS. FABRICATED REPLACEMENT FLOORBOARD 151 VF IAW DWG SRZ 25-005, REV J.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094843Floorboard · damagedFLOORBOARD 151SF HAS EDGE DAMAGE 12" X 3" FABRICATED REPLACEMENT FLOORBOARD 151SF IAW DWG SRZ 25-005, REV J.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094842Floorboard · delaminatedFWD PIT FLOORBOARD 132 KG EDGES DELAM 25 SQ IN. FABRICATED REPLACEMENT FLOORBOARD 132 KG IAW DWG SRZ 25-005, REV J.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094841Floorboard · tornFLOORBOARD 152PF TORN IN SEVERAL PLACES FABRICATED REPLACEMENT FLOORBOARD 152PF IAW DWG. SRZ25-005.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111094826Seat Track · gougedMID SEAT TRACK 5L RT EDGE GOUGED AROUND 4EA SCREW HOLES FROM FR 52 THRU FR 54. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 105, FIG 102. FABRICATED NEW SEAT TRACK IAW DWG A53832211. INSTALLED NEW SEAT TRACK IAW SRM 51-72-10 & 51-40-21.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111094825Seat Track · gougedMID SEAT TRACK 4L GOUGED AT 2 LOCATIONS BETWEEN FR 48 AND FR 49. AFTER REMOVAL OF GOUGES ON SEAT TRACK IT WAS FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 PG 105. R & R SEAT TRACK IAW SRM 51-72-10 PG 2, PARA 5.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111094824Seat Track · corrodedMID SEAT TRACK 5L CORRODED AT 7 EA SCREW HOLES BETWEEN FR 43 AND FR 47. REMOVED AND REPLACE SEAT TRACK.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111094823Seat Track · corrodedMID SEAT TRACK 4L CORRODED AT LT FLANGE 9, LOCATIONS FROM FR 43 TO FR 47. SEAT TRACK R & R IAW SRM 51-72-10.Nov 9, 2011 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111084821Skin · misrepairedSKIN AT FRAME 39, BETWEEN STRINGERS 36 & 39 RT MISREPAIRED. REPAIRED IAW EA 6-5330-83906 B AND RDAS/70555478/012/2011 ISSUE A. COMPLIED WITH EA 6-5330-83906 B PT2.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111084816Floor Panel · damagedFLOOR PANEL 151UF HAS SEVERAL PUNCTURES ON BACK AND CORNER DELAMINATED FABRICATED FLOOR PANEL 151UF IAW DWG SRZ 25-005, REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084815Floor Panel · crackedFLOOR PANEL 242UJ HAS 3 EA 9" CRACKS. FABRICATED FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084814Floor Panel · crackedFLOOR PANEL 241DF HAS 3EA 7" CRACKS. FABRICATED FLOOR PANEL 241DF DWG SRZ 25-005, REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084813Floor Panel · damagedFLOOR PANEL 152VF HAS EDGE DAMAGE 2' FABRICATED REPLACEMENT FLOOR PANEL 152VF IAW DWG SRZ 25-005 REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084812Floor Panel · crackedFLOOR PANEL 152TF HAS A 10" CRACKED. FABRICATED REPLACEMENT FLOOR PANEL 152TF IAW DWG SRZ 25-005 REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111084811Floor Panel · damagedFLOOR PANEL 151WF HAS 10" OF DAMAGED AND 20 EA TOOL MARKS. FLOOR PANEL 151WF FABRICATED NEW PANEL IAW DWG SRZ-25-005, REV J.Nov 8, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074784Floor Panel · crackedFLOOR PANEL 151TF HAS A 21" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 151TF IAW DWG SRZ 25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074783Floorboard · damagedFLOORBOARD 152XF HAS DAMAGE AT CORNER 6" X 4". FABRICATED REPLACEMENT FLOORBOARD 152XF IAW DWG SRZ25-005, REV J. IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074782Floorboard · crackedFLOORBOARD 251BH HAS 1 EA 9.5 CRACK AND CRUSHED AROUND CLEVIS ADAPTOR. FABRICATED REPLACEMENT FLOORBOARD 251BT IAW DWG SRZ 25-005.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201111074781Floorboard · crackedFLOORBOARD 242 ZJ HAS 5 EA, 12" CRACKS. FABRICATED REPLACEMENT FLOORBOARD 242ZT IAW DWG SRZ 25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074780Floorboard · damagedFLOORBOARD 151RF HAS SEVERAL PUNCTURES ON BACK OF PANEL. FABRICATED REPLACEMENT FLOORBOARD 151 RF IAW DWG SRZ 25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074779Floorboard · tornFLOORBOARD 151QF TORN IN SEVERAL PLACES FABRICATED REPLACEMENT FLOORBOARD 151QF IAW DWG SRZ25-005, REVJ.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074778Floorboard · damagedFLOORBOARD 151XF HAS 2 EA CRACKS, 6 EA 1" PUNCTURES, 7" EDGE DAMAGE FABRICATED REPLACEMENT FLOORBOARD 151 XF IAW DWG SRZ-25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074777Floorboard · crackedFLOORBOARD 152SF IS CRACKED IN HALF, FABRICATED REPLACEMENT FLOORBOARD 152SF IAW DWG SRZ 25-055, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074776Floorboard · crackedFLOORBOARD 242QJ HAS 2 EA 9.5 CRACKS FABRICATED REPLACEMENT FLOORBOARD 242QJ IAW DWG SRZ 25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111074775Floorboard · crackedFLOORBOARD 242GF HAS 1 EA 9.5 CRACK FABRICATED REPLACEMENT FLOORBOARD 242GF IAW DWG SRZ 25-005, REV J.Nov 7, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054768Floor Panel · crackedFLOOR PANEL 132 QG HAS SEVERAL PUNCTURES ON BACK AND 4 CRACKS. FABRICATED FLOOR PANEL 132 QG IAW DWG SRZ 25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054767Floor Panel · crackedFLOOR PANEL 252UH HAS 1, 10" CRACK. FABRICATED FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054766Floor Panel · crackedFLOOR PANEL 252PH HAS 2 EA, 9" CRACKS. FABRICATED REPLACEMENT FLOOR PANEL 252PH IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054765Floor Panel · crackedFLOOR PANEL 241RJ IS CRACKED IN HALF FABRICATED REPLACEMENT FLOOR PANEL 241RJ IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054764Floor Panel · delaminatedFLOOR PANEL 132LG HAD SEPARATION AT CORNER 6"X2". FABRICATED REPLACEMENT FLOOR PANEL 132 LG IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054763Floor Panel · crackedFLOOR PANEL 252VF HAS 1 EA 10" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 252 VF IAW DWG SRZ-25-005, REV J. MAJOR REPAIR IAW GMM 6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111054762Floor Panel · crackedFLOOR PANEL 131SG HAS A 8" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 131 SG IAW DWG SRZ-25-005, REV J MAJOR. REPAIRED IAW GMM6-2-100.Nov 5, 2011 · N652FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201012164700Gcu · malfunctionedACFT RETURNED TO DEPARTURE WITH NR1 ENGINE GEN FAULTED AND NR 1 AC BUSS FAILURE. INSPECTED AND PERFORMED GPCU BITE. TROUBLE SHOOTING INDICATED NO RESPONSE FROM NR 1 GCU. PULLED NR 1 GCU FROM RACK SMELLED STRONG BURN ODOR. SWAPPED APU GCU INTO NR 1 POSITIODec 16, 2010 · N652FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA200905271813Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 4 LT BETWEEN FR 51 AND FR 53 HAS 2 EA AREAS OF CORROSION REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 4 LT BETWEEN FR 50 AND FR 53 IAW SRM 53-10-16, FIGMay 27, 2009 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271812Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 5 LT BETWEEN FR 47 AND FR 48 HAS CORROSION. REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 5 LT BETWEEN FR 46 AND FR 49 IAW SRM 53-10-16, FIG 205, PAGE May 27, 2009 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271810Floorbeam · crackedBULK CARGO COMPARTMENT FR 66 BETWEEN SEAT TRACKS NR 3 AND 4 RT MAIN DECK CARGO FLOORBEAM CRACK AT VERTICAL STIFFENER. REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FLOORBEAM IAW SRM 53-10-15,FIG 211,PAGE 389/390May 27, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905271809Stiffener · crackedBULK CARGO COMPARTMENT FR 64 BETWEEN SEAT TRACKS NR 4 RT AND 5 RT,MAIN DECK CARGO FLOORBEAM HAS CRACK ON VERTCAL STIFFENER. REMOVED CRACK AND INSTALLED REPAIR IAW SRM 53-10- 15,FIG 211,PAGE 389/390May 27, 2009 · N652FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200905261799Floorbeam · crackedFWD CARGO COMPARTMENT FR 25 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT MAIN DECK CARGO FLOORBEAM CRACKED ON VERTICAL STIFFENER. CUT OUT DAMAGED AREA AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 25 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW A300-600 FREIGMay 26, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905261798Floorbeam · crackedBULK CARGO COMPARTMENT FR 66 BETWEEN SEAT TRACKS NR 3 AND NR 4 LT AT VERTICAL STIFFENER ON MAIN DECK CARGO FLOORBEAM CRACKED. ROUTED OUT CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 66 BETWEEN SEAT TRACKS NR 3 AND NR 4 LT IAW A300-600 FREIGMay 26, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905231774Floorbeam · crackedFWD CARGO COMPARTMENT FR 27 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT AT MAIN DECK CARGO FLOORBEAM HAS CRACK REMOVED CRACK ON FLOORBEAM AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 27 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW A300-600 FREIGHTER SRM 53-1May 23, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905211761Crossbeam · crackedBULK CARGO COMPARTMENT FR 65 BETWEEN SEAT TRACKS NR 3 AND 4 LT AT VERTICAL STIFFENER ON MAIN DECK FLOORBEAM CRACKED. REMOVED CRACK ON FR 65 UPPER DECK CROSSBEAM STIFFENER & INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER IAW SRM 53-10-15,FIG 212,PAGE 397/3May 21, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA200905191743Floorbeam · crackedAFT LOWER CARGO COMPARTMENT R/H SIDE FR 60,MAIN UPPER DECK FLOORBEAM CRACKED,BETWEEN SEAT TRACKS NR 4 & 5,CRACK .250 IN LONG CUT OUT DAMAGED SECTION OF FLOORBEAM AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 60 BETWEEN SEAT TRACKS NR 4 RT & 5 RT May 19, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200905181711Crossbeam · crackedFORWARD LOWER CARGO COMPARTMENT CEILING FR 35 BETWEEN SEAT TRACKS NR 2 AND 3 RT MAIN DECK CARGO FLOORBEAM HAS CRACK,0.250 IN. CUT OUT DAMAGED AREA AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 35 BETWEEN SEAT TRACKS NR 2 RT AND 3 RT IAW FREIGHTERMay 18, 2009 · N652FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA200905181710Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 4 LT FR 34 TO FR 38 HAS 4 EA AREAS OF CORROSION,6 SQ INCHES REMOVED LEVEL 1 CORROSION.REMOVED DAMAGED SECTION OF TRACK NR 4 LT AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 34 AND FR 38 IAW SRM 53-10-16,FIG201,PAMay 18, 2009 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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