N670FE

Service difficulty reports · 205

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 = 'N670FE' 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 FDEA200909193334Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK 2L BETWEEN FR 74 AND FR 76 LT HAS APPROX 3 SQ INS. OF CORROSION ON TRACK BASE. REMOVED CORROSION FROM MAIN DECK SEAT TRACK 2L BETWEEN FR 74 AND FR 76 LT IAW SRM 51-74-10. MATERIAL LOSS OUT OF LIMITS ON SEAT TRACK 2L AT FR 75.3. RESep 19, 2009 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909183331Skin · damagedWHILE PERFORMING FLAP OPERATIONAL TEST, BRACKET FOR RT NR 5 SPOILER ACTUATOR CAUSED A PUNCTURE IN UPPER FWD OTBD AREA OF RT CENTER FLAP. DAMAGED AREA 26MM X 24 MM. REMOVED DAMAGED SECTION AT RT CENTER FLAP RIB 27 FWD AND OTBD. FABRICATED REPAIR SKIN, BUTT STSep 18, 2009 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200909163304Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASep 16, 2009 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200909163303Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASep 16, 2009 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200909163302Skin · chafedRT WING INBD FLAP UPPER SKIN HAS CHAFE MARK APPROX 1 SQUARE INCH AT 10 INCHES FROM INBD SIDE AND 20 INCHES FROM L/E. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 57-50-00, FIG 205.Sep 16, 2009 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200902260738Transmitter · leakingDURING CRUISE GREEN HYDRAULIC SYSTEM QUANTITY DECREASED TO RED DOT. (READABLE INDICATION THROUGH LANDING) TO RED DOT. ECAM LOW LEVEL WARNING ACTUATED. KRUGER FAILED WITH OUT HYD. PRESS. IN FLIGHT AFTER LANDING. GREEN SYSTEM QTY. INCREASED TO NEAR NORMAL LEFeb 26, 2009 · N670FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR 08FDEA01162Transmitter · failedDURING CLIMB-OUT GOT ECAM YELLOW HYD SYS LOW PRESSURE. OVERHEAD QTY GAUGE INDICATED NO QUANTITY. AFTER LANDING QTY APPEARED NORMAL. COMPLIED WITH ECAM AND REFERRED TO QRH PROCEDURE HYD LOW PRESSURE. OPERATED YELLOW SYS WITH PTU, PRESSURE WAS 3000 AND QUANTMar 27, 2008 · N670FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR 08FDEA00259Apu · fireAT TOUCHDOWN, APU FIRE, AGENT AUTO FIRED. APU FIRE HANDLE PULLED. APU MASTER SWITCH OFF, APU NOT ON. UPON FURTHER INVESTIGATION, DISCOVERED EVIDENCE OF FIRE IN APU BAY. CONNECTOR P18 AT MONOPOLE ASSY IS MELTED/BURNED. NUMEROUS WIRE BUNDLES ON APU HARNESS Jan 24, 2008 · N670FE · Airbus A300F4605R · APU Core EngineSDR 08FDEA00262Apu · fireAT TOUCHDOWN, APU FIRE LIGHT, AGENT AUTO FIRED. APU FIRE HANDLE PULLED. APU MASTER SW WAS OFF AND APU WAS NOT ON/RUNNING. UPON FURTHER INVESTIGATION, DISCOVERED EVIDENCE OF A FIRE IN THE APU COMPARTMENT. PLUG P18 FROM THE MONOPOLE ASSY IS MELTED AND BURNEDJan 24, 2008 · N670FE · Airbus A300F4605R · Airborne Auxiliary Power Unit (APU) SystemSDR 07FDEA04608Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM CRACKED FRAME 27 BETWEEN YD AND YE(RBC 37 AND RBL18). FABRICATED AND INSTALLED CROSSBEAM COUPLING IAW SRM 53-10-15.Oct 16, 2007 · N670FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA04580Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM CRACKED FRAME 30 BETWEEN YD TO YE. FABRICATED AND INSTALLED CROSSBEAM COUPLING IAW SRM 53-10-15 .Oct 13, 2007 · N670FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA04576Seat Track · corrodedMCD SEAT TRACK FROM FR 78 TO FR 73, RBL15 HAS 7 AREAS WITH CORROSION. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16- AND 51-50-21.Oct 12, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04562Seat Track · corrodedMAIN CARGO DECK SEAT TRACK FROM FR 76 TO FR 75 RBL 58 HAS 3 AREAS WITH CORROSION. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-10-16 AND SRM 51-40-44.Oct 10, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04556Seat Track · corrodedMAIN CARGO DECK SEAT TRACK FROM FR 73 TO FR 78, LBL 15 HAS CORROSION IN 8 AREAS REMOVED. FABRICATED AND REPLACED SEAT TRACK IAW 53-10-16.Oct 10, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04521Seat Track · corrodedMAIN CARGO DECK SEAT TRACK FROM FR 78 TO FR 73 RBL25 HAS 7 AREAS WITH CORROSION REMOVED AND REPLACED DAMAGED SEAT TRACK IAW 51-40-21.Oct 6, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04520Seat Track · corrodedMAIN CARGO DECK SEAT TRACK FROM FR 76 TO FR 74 LBL42 HAS 2 AREAS WITH CORROSION REMOVED DAMAGED SEAT TRACK. FABRICATED REPLACEMENT FROM PART NR A5324005/84 T7 AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-21 AND 51-10-16.Oct 6, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04519Stringer · bentSTRINGER 49R IS DAMAGED STA 4377 REMOVED DAMAGED STRINGER SECTION, FABRICATED REPAIR COUPLING IAW SRM 53-10-14 FIG 201. TREATED, PRIMED AND TRIMMED STRINGER IAW SRM 51-21-10. SEALED AND INSTALLED REPAIR COUPLING IAW 53-10-14 FIG 201.Oct 6, 2007 · N670FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR 07FDEA04342Seat Track · corrodedMCD SEAT TRACK FROM FR 73 TO FR 65 BL 0 HAS SIX AREAS WITH CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 65 TO FR 78 IAW SRM 51-40-21.Sep 27, 2007 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03919Indicator · incorrectON TAKEOFF ROLL F/O LOST AIRSPEED INDICATIONS ON PFD NEVER HAD ANY CORRECT INDICATIONS ON F/O PFD. ROUND DIAL STBY AIRSPEED WORKED NORMAL. PERFORMED LEAK TEST AND LEAK TEST CHECKS OK, AS PRECAUTION REMOVED AND REPLACED NR 2 ADC AND PER MOCC REQUEST ALSO REMONov 7, 2006 · N670FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR 06FDEA0691Hydraulic System · leakingDURING DESCENT GOT ECAM -HYD RSVR LO LEVEL- ALERT. QTY NORMAL AFTER T/O, UNTIL START OF DESCENT THEN DROPPED TO RED DOT. AFTER LANDING, QTY BACK TO NORMAL GREEN BAND ON OVERHEAD AND ECAM. VERIFIED THAT GREEN SYSTEM RESERVOIR INDICATOR SHOWS 6 GALLONS OF FLUFeb 15, 2006 · N670FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR 06FDEA0264Valve · malfunctionedSHORTLY AFTER TAKEOFF IN SNOW, WING ANTI-ICE VALVE FAULT INDICATED ON ECAM. TEMP 3C QRH PROCEDURES FOLLOWED WITH NO CHANGE IN FAULT LIGHT, PER CREW COMMENT RT WING WAS CAUSING FAULT. TESTED SYSTEM OPS CHECKED OK. DURING FURTHER T/S FOUND THAT EITHER VALVJan 18, 2006 · N670FE · Airbus A300F4605R · Airfoil Anti/De-ice SystemSDR 05FDEA02331Floor Panel · damagedMDC FLOOR PNL 242CF IS DAMAGED.Aug 8, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02330Floor Panel · crackedMDC FLOOR PNL 231EF IS CRACKED.Aug 8, 2005 · N670FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02329Floor Panel · crackedMDC FLOOR PNL 252UF CRACKED.Aug 8, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02328Floor Panel · brokenMDC FLOOR PNL 241LK BROKEN.Aug 8, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02310Web · crackedNR 2 PYLON L/E AREA INSIDE PNL 421CL AFT HORIZONTAL WEB HAS CRACK.Aug 7, 2005 · N670FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR 05FDEA02253Floor Panel · delaminatedMDC FLOOR PNL 231BH DELAMINATED.Aug 4, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02252Floor Panel · crackedMDC FLOOR PNL 252WG CRACKED.Aug 4, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02251Floor Panel · crackedMDC FLOOR PNL 252AH CRACKED.Aug 4, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02250Floor Panel · crackedMDC FLOOR PNL 252BH IS CRACKED.Aug 4, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02143Frame · gougedCOMPLY WITH EA 6-5310-82112, COMPLIED WITH EA 6-5310-82112 FUSELAGE-MAIN FRAME, FRAME 28 GOUGE REPAIR STR 10L THROUGH STR 11L.Jul 30, 2005 · N670FE · Airbus A300F4605R · Fuselage Main, FrameSDR 05FDEA02135Seat Track · corrodedSEAT TRACK AT Y953 FR 17-19 IS CORRODEDJul 28, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02134Seat Track · corrodedSEAT TRACK AT Y953 FR 17-19 IS CORRODED.Jul 28, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02133Gusset · crackedLT WING BELOW NR 5 SPOILER INBD ATTACH POINT HAS A GUSSET CRACKED.Jul 28, 2005 · N670FE · Airbus A300F4605R · Wing, Control Surface Attach FittingsSDR 05FDEA02132Blowout Door · gougedEXHAUST THRUST REVERSE R BLOWOUT DOOR EDGE REPAIR. COMPLIED WITH EA 6-7830-82111, EXHAUST THRUST REVERSER BLOWOUT DOOR EDGE WEAR REPAIR.Jul 28, 2005 · N670FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA02122Floor Panel · crackedMAIN DECK FLOOR PANEL 232CF CRACKED.Jul 27, 2005 · N670FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02121Floor Panel · crackedMAIN DECK FLOOR PANEL 232CF CRACKED.Jul 27, 2005 · N670FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02094Seat Track · corrodedSEAT TRACK AT R-2, -Y953 FR 55 TO 56 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 53-10-16 FIG 201 REF TRAVELER T5/533734.Jul 25, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02093Seat Track · corrodedSEAT TRACK BL-0 FR 72.5 CORRODED OUT OF LIMITS. CUT OUT THE DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED NEW SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16 REF TRAVELER T5/533030.Jul 25, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02092Seat Track · corrodedSEAT TRACK AT BL-0 FR 70.5 IS CORRODED OUT OF LIMITS. CUT OUT THE DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16 REF TRAVELER T5/533029.Jul 25, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02059Web · crackedMAIN CARGO AT FR 38.1 38.2 AT -Y2462 RT SIDE SUPPORT WEB IS CRACKED.Jul 25, 2005 · N670FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 05FDEA02058Seat Track · corrodedSEAT TRACK AT Y450 FR 15 IS CORRODEDJul 25, 2005 · N670FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA02029Skin · dentedRT WING T/E INBD FLAP LOWER SURFACE INBD SECTION HAS DENT (31" FROM INBD END AND 7" FROM T/E). CHECKED ALLOWABLE DENT LIMIT FOUND OT OF LIMIT ACTUAL DENT 0.1405, ALLOWED IS ONLY 0.14" PER SRM 57-50-00 PAGE 105. REMOVED DAMAGE IAW SRM 57-50-00 FIG 205 PAGE 22Jul 23, 2005 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR 05FDEA02028Web · crackedMAIN DECK REAR CARGO COMPT BET FRAME 79 AND 80 AT FLOOR LEVEL LT SIDE FUSELAGE TO FRAME WEB HAS CRACK. REMOVED WEB IAW SRM 51-40-21, FABRICATED NEW WEB ON MAE TRAVELER T5/533479. INSTALLED NEW WEB IAW SRM 51-40-21.Jul 23, 2005 · N670FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 05FDEA02027Floor Panel · crackedMAIN DECK FLOOR PANEL 261AH CRACKED. FABBED FLOOR PANEL 261AH ON MAE TRAVELER T5/532924 REF SRZ-25-005 MAJOR REPAIR.Jul 23, 2005 · N670FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02026Floor Panel · crackedMAIN CABIN FLOOR PANEL 241MF CRACKED. FABBED FLOOR PANEL 241MF ON MAE TRAVELER T5/532595 REF SRZ-25-005 MAJOR REPAIR.Jul 23, 2005 · N670FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02025Floor Panel · crackedMAIN CABIN FLOOR PANEL 242MF CRACKED. FABBED FLOOR PANEL 242MF ON MAE TRAVELER T5/532594 REF SRZ-25-005 MAJOR REPAIR.Jul 23, 2005 · N670FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02007Skin · dentedFUSELAGE BOTTOM SKIN PANEL, FR 1-10 AREA -A- FOUND DENTED SKIN DURING ALI INSPECTION. REMOVED DAMAGED AREA OF SKIN, FAB'D REPAIR DOUBLER AND FILLER FROM 2024-T3 .071 AND .050 INSTALLED THE REPAIR IAW SRM 53-11-12 FIG 201. PAINTED REPAIRED AREA IAW MM 51Jul 21, 2005 · N670FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 03FDEA01092Alternator · failedPDIS 670 34-54 0005194 10JUL03 CWF CLOSER GPWS TERRAIN PULL-UP" OCCURED ON FINAL WITH GEAR AND FLAPS 40 FACT, 11JUL03, 12:46 CWFU REMOVED AND REPLACED RADIO ALT NR 2 IAW A300-600 AMM 34-42-33-4 OPS CHECK GOOD IAW A300-600 AMM 34-71-00-5 AND 34-42-00-5.Jul 11, 2003 · N670FE · Airbus A300F4605R · Visual Omnirange (VOR) SystemSDR 03FDEA01091Controller · failedCWF CLOSER DURING CATIII APPROACH WITH A NORMAL GLIDE SLOPE AND SINK RATE A RAPID COUNTDOWN (50,40,30,ECT) OCCURED AND THE AIRCRAFT FLARED EARLY FOLLOWED BY A PUSHOVER AND SUBSEQUENT FIRM LANDING. REMOVED AND REPLACED TCC IAW AMM 22-36-34-4 AND RADIO ALT. Jul 11, 2003 · N670FE · Airbus A300B4605R · Autopilot System
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