N674FE

Service difficulty reports · 345

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 = 'N674FE' 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 FDEA201505031372Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242BJ PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005, CAT A REPAIR MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505031371Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242UJ HAS DENTS & DELAMINATION ON EXTERIOR SURFACE & MISSING INSERTS. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005, CAT A REPAIR MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505031370Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241ZH PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. CAT A REPAIR MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505031369Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241RH HAS SEVERAL SPOTS PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. CAT A REPAIR MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505031368Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241TH PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. CAT A REPAIR MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505031367Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242JG HAS EDGE DAMAGED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005, CAT A MAJOR.May 3, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011357Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242 HK HAS TWO EACH CRACKS. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. CAT A REPAIR MAJOR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011356Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242BK PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR, CAT A.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011353Floor Panel · crackedMAIN DECK FLOOR PANEL 242 QJ EXT SURFACE HAS CRACK. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011352Floor Panel · crackedMAIN DECK CARGO BAY FLOOR PANEL 241UJ HAVE CRACKS ON CUT OUTS. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011351Floor Panel · damagedFORWARD CARGO BAY FLOOR PANEL 131QG HAS DAMAGE. PUNCTURED & BROKEN PARTS ALONG THE EDGE. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011350Floor Panel · damagedFORWARD CARGO BAY FLOOR PANEL 132SG HAS DAMAGE. DENTS & BROKEN PARTS ALONG THE EDGE, INTERIOR SURFACE. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011349Floor Panel · damagedAFT PIT FLOORBOARD 151 QF MISSING INSERTS. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011348Floor Panel · damagedMAIN DECK FLOOR PANEL 232 BH BROKEN. FABRICATED FLOOR PANEL IAW DWG 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011347Floor Panel · damagedMAIN DECK CARGO BAY FLOOR PANEL 241 BJ PUNCTURED. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011346Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242 UH HAS SEVERAL SPOTS PUNCTURED. FABRICATED FLOOR PANEL 242 UH ON T15 1136804 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011345Floor Panel · damagedAFT PIT FLOORBOARD 151 TF, TWO EACH CORNERS DAMAGED. FABRICATED FLOOR PANEL 151TF ON T15 1136845 IAW SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011344Floor Panel · damagedFORWARD PIT FLOOR PANEL 132 MG HAS DAMAGE. PUNCTURED & DELAMINATED ON INTERIOR SURFACE ALONG THE EDGE. FABRICATED FLOOR PANEL 132 MG ON T15 1136102 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011343Floor Panel · damagedFORWARD PIT FLOOR PANEL 132 KG INTERIOR SURFACE HAS DAMAGE, DENTS & DELAMINATION. FABRICATED FLOOR PANEL 132 KG ON T15 1136100 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011342Floor Panel · damagedFORWARD PIT FLOOR PANEL 132 LG HAS DAMAGE. DENTS & PUNCTURES AROUND THE EDGE, INTERIOR SURFACE. FABRICATED FLOOR PANEL 132 LG ON T15 1136109 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011341Floor Panel · damagedAFT PIT FLOORBOARD 151 VF CORNER DAMAGED. FABRICATED FLOOR PANEL 15 VF ON T15 1136502 IAW DWG 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011340Floor Panel · damagedAFT PIT FLOORBOARD 152 RF PUNCTURE. FABRICATED FLOOR PANEL 152 RF ON T15 1136499 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011339Floor Panel · damagedAFT PIT FLOORBOARD 152 QF MISSING INSERTS. FABRICATED FLOOR PANEL 152 QF ON T15 1136500 IAW DWG 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201505011338Floor Panel · damagedAFT PIT FLOORBOARD 152 UF MISSING INSERTS. FABRICATED FLOOR PANEL 152 UF ON T15 1136501 IAW DWG 25-005 CAT A MAJOR REPAIR.May 1, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201504301337Floor Panel · damagedFORWARD CARGO FLOOR PANEL 131 LG HAS DAMAGE & CRACKS, DENTS & DELAMINATION AROUND THE EDGE, INTERNAL SURFACE. FABRICATED FLOOR PANEL 131 LG ON T15 1136107 IAW DWG 25-005 CAT A MAJOR REPAIR.Apr 30, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201504301336Floor Panel · damagedFORWARD PIT FLOOR PANEL 131 MG HAS DAMAGE. PUNCTURED & DELAMINATED ALONG THE EDGE, INTERNAL SURFACE. FABRICATED FLOOR PANEL 131 MG ON T15 1136106 IAW DWG 25-005 CAT A. MAJOR REPAIRApr 30, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201504301335Floor Panel · damagedFORWARD PIT PANEL 131 NG INTERNAL SURFACE HAS DENTS & DELAMINATION IN SEVERAL SPOTS. FABRICATED FLOOR PANEL 131 NG ON T15 1136099 IAW DWG 25-005 CAT A MAJOR REPAIR.Apr 30, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201504301329Seat Track · corrodedY953 SEAT TRACK CORRODED AT FRAME 72 BLENDED OUT CORROSION IAW SRM 51-74-10. CHECKED LIMITS L=2.00 W=.500 D=.081" FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED SEAT TRACK FROM FRAME 69 - 71.9 IAW SRM 51-40-21. FABRICATED NEW SEAT TRACK MATERIAL USEDApr 30, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201504301328Floor Support · corrodedMDCC FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION AT 4 IN & 8 IN FWD OF FRAME 15 & 6 IN FWD OF FRAME 12, Y953. R & R FLOOR SUPPORT IAW SRM 51-40-21 PN A5361261920001 BATCH 0002785920 CLASS A MAJOR REPAIR.Apr 30, 2015 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201504291323Seat Track · corrodedY1456 SEAT TRACK CORRODED AT FRAME 73. REMOVED CORROSION IAW 53-10-16 FIG 102. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-21 CLASS A MAJOR REPAIR.Apr 29, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201504291322Seat Track · corrodedMAIN DECK RT SEAT TRACK, Y1959 HAS CORROSION SPOTS FROM FRAME 26.5 - 31. REMOVED CORROSION IAW SRM 51-74-10. MAT LOSS .125" FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16-101. FABRICATED NEW SEAT TRACK IAW DWG A53812923. INSTALLED SEAT TRACK IAW SRM 51-40-21 CApr 29, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201504291316Seat Track · corrodedAFT MAIN DECK FRAME 70 - 71, -Y953 SEAT TRACK HAS CORROSION. R & R NEW SEAT ON AFT MAIN DECK IAW SRM 51-40-21. INSTALLED TWO EACH SPLICES & FOUR EACH BRACKETS IAW SRM 51-40-21 CLASS A MAJOR REPAIR.Apr 29, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201504291314Mount · corrodedNUMBER 1 ENG PYLON FWD MOUNT FITTING, PYRAMID, FWD HOLES & ALIGNMENT HOLE UPPER SURFACE AREA LIGHT SURFACE CORROSION. REPAIRED FWD MOUNT FWD HOLE IAW SRM 54-51-81 FIG 202. CLEANED ALIGNMENT HOLE UPPER SURFACE IAW SRM 54-51-81. FOUND TO BE SEALANT & DIRT OApr 29, 2015 · N674FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201504291313Seat Track · corrodedAREAS OF CORROSION & BARE METAL ON Y 1456 SEAT TRACK FRAME 54.2 - 57.2. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REMOVED SEAT TRACK FROM 57/ 5 - 57.2/ 5. FABRICATED NEW SEAT TRACK & SPLICES IAW SRM 53-10-16 FIG 201 BATCH 2764239Apr 29, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201504231279Floor Panel · damagedFORWARD COURIER AREA FLOOR PANEL 221 RF HAS SURFACE DAMAGE. RECEIVED FABRICATED FLOOR PANEL 221 RF FOR FWD COURIER AREA ON T15 1134958. INSTALLED ON WC 220 FL FIT CAT A MAJOR REPAIR.Apr 23, 2015 · N674FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201504171250Seat Track · corrodedCABIN RT FLOOR 11 EACH SIDE TRACKS HAVE CORROSION FROM FRAME 19 - 31 BETWEEN -Y1959 - Y2462. CLEANED SIDE TRACKS, CLEANED LIGHT SURFACE CORROSION OFF SIDE TRACK AT FRAME 21. MATERIAL LOSS .003 FOUND TO BE WITHIN LIMITS IAW SRM 51-10-15.Apr 17, 2015 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408072105Connector · unknownON TAKEOFF NR 2 THRUST REVERSER PRESSURIZED. FOUND LT DPV SOLENOID CONNECTOR NOT PROPERLY REMOVED IAW MEL 78-30-01-A. REMOVED CONNECTOR & CONTINUED ON WITH MX PROCEDURES TO END. OK TO CONTINUE ON MEL.Aug 7, 2014 · N674FE · Airbus A300F4605R · Engine Exhaust System WiringSDR FDEA201401070064Pivot · lack of lubeLANDING GEAR RETRACTION FAULT SYSTEMS 1 & 2. LUBED PIVOT. GEAR SWINGS GOOD.Jan 7, 2014 · N674FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201311062789Switch · malfunctionedCLIMBING THRU FL 280, RECIEVED A MAIN DECK DOOR SWITCH FAULT WARNING AND MAIN DECK DOOR NOT CLOSED WARNING. WENT OUT AT 14,000 ON DESCENT. MAIN CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE, INOPERATIVE MAIN CARGO DOOR VISUALLY CHECKED, CLOSED & Nov 6, 2013 · N674FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201311062705Warning Message · false activationCLIMBING THRU FL 280, RECEIVED A MAIN DECK DOOR SWITCH FAULT WARNING AND MAIN DECK DOOR NOT CLOSED. WARNING WENT OUT AT 14,000 DURING DESCENT. PERFORMED VISUAL INSP, MAIN CARGO DOOR CLOSED AND LOCKED. PERFORMED DOOR WARNING TEST IAW AMM 52-71-00-05-02. OPSNov 6, 2013 · N674FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201212044241Fitting · damagedFOUND LT WING RIB NR 5 HOLE NR 52 ALREADY 2ND OVERSIZE FASTENER HOLE. PERFORMED OVERSIZE THE SUBJECT HOLE TO DIAMETER OF 0.8075" TO 0.8095" IAW EO 6-5710-7-3325. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 4, 2012 · N674FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201212044240Fitting · gougedRT WING RIB 5 SPOTFACE HOLE 43, AFT DRILL PARALLEL HOLE TO SECOND OVERSIZE, FOUND SOME GOUGES. REPAIRED IAW GMM 6-2-100, REPAIR CLASSIFIED MINOR.Dec 4, 2012 · N674FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201211274188Fitting · corrodedCORROSION WAS FOUND ON RT RIB5 FWD LUG BORE AND BOTH SIDE OF THE SPOTFACE OF RIB 5 FWD LUG. 1 IAW EA 6-5740-149078 ACCOMPLISHED THE CORROSION REPAIR. 2 EA 6-5740-149078.Nov 27, 2012 · N674FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201108063118Uplock · inoperativeON TAKEOFF, AFTER GEAR RETACTION, NOSE WHEEL GEAR DOOR STAYED OPEN. INDICATION ON BOTH PANELS. REPLACED NOSE GEAR DOOR LT UPLOCK ASSY IAW MM 32-31-14-04. SYS CHECKS OK.Aug 6, 2011 · N674FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201106012039Battery · failedDURING A-CHECK, FOUND EMERGENCY LIGHTS DO NOT TEST PROPERLY AT LIGHT PANEL IN COURRIER AREA. R & R EMERGENCY LIGHT PWR SUPPLY UNIT AND BATTERY IAW AMM SUPP 33-51-14. LIGHTS OPS TEST GOOD.Jun 1, 2011 · N674FE · Airbus A300F4605R · Emergency LightingSDR FDEA201103120941Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FRAME 75-77 SEAT TRACK 1 CORROSION FOUND TO BE OUT OF LIMITS. LEVEL-1 CORROSION -REMOVED AND REPLACED SEAT TRACK SECTION Y-0 AT FR 75-77 DUE TO OUT OF LIMIT CORROSION REMOVAL IAW SRM 53-10-16 FIG 204.Mar 12, 2011 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103120940Skin · chafedLT MLG DOOR EXTERNAL SKIN HAS CHAFE MARK. REPAIRED LT MLG DOOR EXTERNAL SKIN IAW EA 5200-145567 AND OE-781-02-11-010B USING DOUBLER AND FILLER REPAIR SCHEME.Mar 12, 2011 · N674FE · Airbus A300B4605R · Landing Gear DoorsSDR FDEA201102280795Bracket · corrodedMDCC UNDER FLOOR UNDER NUTPLATES HAVE CORROSION AND 5 EACH NUTPLATES ARE MISSING BETWEEN FRAMES 26 AND 27 AND BETWEEN Y0 TO Y1959. REMOVED LEVEL 1 CORROSION IAW A300-600 SRM 51-74-10. CHECKED LIMITS AND NO CORROSION REMOVAL OR MATERIAL LOSS ALLOWED ON THRUSTFeb 28, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201102270787Transition Panel · corrodedCORROSION ON LT TRANSITION PLATE BULK CARGO FRAMES 64 TO 65 AT FASTENER HOLES. REMOVED AND REPLACED BULK CARGO COMPARTMENT LT PROFILE FR 64 -67 AND WEB FR 64 TO 65 AT STR44L IAW A300-600 SRM 51-72-10 PGS 1-3.Feb 27, 2011 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201102250760Floorbeam · crackedMAIN CABIN FLOORBEAM AT FR 66 BETWEEN 3L AND 4L SEAT TRACKS HAS 2 EACH 0.30 INCH CRACKS, 1 INCH ABOVE ON MILLED GRIP 2 INCH FROM TOP OF FRAME. CUT OUT DAMAGED AREA IAW SRM 53-10-15 FIG 211 PG 389. NDT CHECK COMPLIED WITH FOR INITIAL CRACKS, NO CRACKS FOUND IFeb 25, 2011 · N674FE · Airbus A300F4605R · Fuselage Main, Floor Beam
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