N719FD

Service difficulty reports · 159

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 = 'N719FD' 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 FDEA201709182608Web · crackedFWD PIT FR37 TO 38 RT O/B WEB BELOW ROLLER TRAY CRACKED. REMOVED DAMAGE WEB (SHEAR PLATE) IAW SRM 51-40-21. FABRICATED NEW SHEAR PLATE ON T17/1296691, INSTALLED NEW SHEAR PLATE IAW SRM 51-40-21 AND DWG A 533778338.Sep 18, 2017 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201709162580Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132JG DELAMINATED. FABRICATED FLOOR PANEL 132JG ON T17/1296307 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162579Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132RF DELAMINATED / PUNCTURED. FABRICATED FLOOR PANEL 132RF ON T17/1296700 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162578Floor Panel · crackedMAIN CARGO FLOOR PANEL 241MF HAS CRACK. FABRICATED FLOOR PANEL 241MF ON T17/1296065 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162577Floor Panel · crackedMAIN CARGO FLOOR PANEL 231EF HAS CRACK. FABRICATED FLOOR PANEL 231EF ON T17/1296092 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162576Floor Panel · crackedMAIN CARGO FLOOR PANEL 231HG HAS CRACK. FABRICATED FLOOR PANEL 231HG ON T17/1296692 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162575Floor Panel · crackedMAIN CARGO FLOOR PANEL 231LG HAS CRACK. FABRICATED FLOOR PANEL 231LG ON T17/1295998 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162574Floor Panel · crackedMAIN CARGO FLOOR PANEL 231AH HAS CRACK. FABRICATED FLOOR PANEL 231AH ON T17/1296095 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709162573Floor Panel · crackedMAIN CARGO FLOOR PANEL 231FG HAS A CRACK. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 CLASSIFIED AS A MAJOR REPAIR.Sep 16, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709152572Shear Plate · crackedSUPPORT WEB UNDER FWD CARGO COMPT FLOOR HAS CRACK FR21 Y1456 APPROX. REMOVED SHEAR PLATE IAW SRM 51-40-21. FABRICATED NEW SHEAR PLATE ON T17/1296683. INSTALLED NEW SHEAR PLATE P/N FX-531418-50 IAW A300 SRM 51-40-21. MAJOR REPAIR.Sep 15, 2017 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201709142550Floor Panel · delaminatedCOURIER FLOOR PANEL 221HF HAS MULTIPLE PUNCTURES AND DELAMINATION’S FABRICATED COURIER FLOOR PANEL 221HF ON T17/1295931 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142549Floor Panel · delaminatedCOURIER FLOOR PANEL 221GF HAS MULTIPLE PUNCTURES AND DELAMINATION’S FABRICATED COURIER FLOOR PANEL 221GF ON T17/1295936 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142548Floor Panel · delaminatedCOURIER FLOOR PANEL 221RF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221RF ON T17/1295937 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142547Floor Panel · delaminatedCOURIER FLOOR PANEL 221MF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221MF ON T17/1295993 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142546Floor Panel · delaminatedCOURIER FLOOR PANEL 222HF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222HF ON T17/1295880 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142545Floor Panel · delaminatedCOURIER FLOOR PANEL 221QF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221QF ON T17/1295938 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142544Floor Panel · delaminatedCOURIER FLOOR PANEL 221PF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221PF ON T17/1295933 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142543Floor Panel · delaminatedCOURIER FLOOR PANEL 222NF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222NF ON T17/1295994 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142542Floor Panel · delaminatedCOURIER FLOOR PANEL222RF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222RF ON T17/1295877 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142541Floor Panel · delaminatedCOURIER FLOOR PANEL 221LF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 221LF ON T17/1295935 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201709142540Floor Panel · delaminatedCOURIER FLOOR PANEL 222QF HAS MULTIPLE PUNCTURES AND DELAMINATION’S. FABRICATED COURIER FLOOR PANEL 222QF ON T17/1295876 IAW SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.Sep 14, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201612084357Damper · underservicedON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. COMPLIED WITH ECAM QRH AND RETURNED TO DEPARTURE. THE GEAR HANDLE WOULD ONLY GO UP TO THE NEUTRAL MIDDLE POSITION ON BOTH SYSTEMS. REMOVED AND REPLACED PITCH DAMPER ON THE RT GEAR IAW AMM 32-11-15-04-0. SERVICDec 8, 2016 · N719FD · Airbus A300B4622 · Landing Gear Retraction/Extension SystemSDR FDEA201607282648Pump · leakingRECEIVED GREEN HYD RESERVOIR OVERHEAT DURING CRUISE. TURNED GREEN PUMPS OFF. IAW QRH, TURNED ONE PUMP ON TO DETERMINE AFFECTED PUMP. FOLLOWED BY GREEN HYD RESERVOIR LOW LEVEL WITH ASSOCIATED ECAM WARNING. GRAVITY EXTENDED GEAR, TOWED TO GATE. ALSO NR 1 ENJul 28, 2016 · N719FD · Airbus A300B4622 · Hydraulic Pump (Electric/Engine), MainSDR FDEA201508212670Warning System · false activationTAKEOFF CONFIG TESTED NORMAL FOR TAKEOFF ON INITIAL TAKEOFF. PASSING APPROX 25 KNOTS WITH POWER ADVANCING, RED ECAM ALERTED FOR PARKING BRAKE SET, TAKEOFF REJECTED. WARNING EXTINGUISHED WHEN FIRST OFFICER TOUCHED THE PARKING BRAKE HANDLE WHICH WAS DOWN. NOAug 21, 2015 · N719FD · Airbus A300B4622 · Landing Gear Brake SystemSDR FDEA201507212284Warning System · false activationBOTH PITCH TRIM LEVERS FAULTED OFF JUST AFTER TAKEOFF, NO RESET. PERFORMED AUTO PILOT LAND IAW AMM 22-40-00-05, CAT III. TEST CHECKED OK. ACFT OK FOR SERVICE.Jul 21, 2015 · N719FD · Airbus A300B4622 · Speed-Attitude Correction SystemSDR FDEA201506151803Check Valve · failedFLIGHT TEST SHORTLY AFTER TAKEOFF AT 1000 FEET COCKPIT & COURIER AREA FILLED WITH MODERATE TO HEAVY SMOKE & FUMES WITH AN ACRID OIL ODOR. IAW NORMAL TEST FLIGHT PROCEDURE APU AIR USED AS BLEED SOURCE FOR AIR CONDITIONING SEVERAL LEVEL 3 ECAM CARGO COMPARTMENTJun 15, 2015 · N719FD · Airbus A300B4622 · Hydraulic System, MainSDR FDEA201506151801Unknown · odorFLIGHT TEST, SHORTLY AFTER TAKEOFF AT 1000 FEET COCKPIT & COURIER AREA FILLED WITH MODERATE TO HEAVY SMOKE, FUMES WITH AN ACRID OIL SMELL. IAW NORMAL TEST FLIGHT PROCEDURE, APU AIR USED AS BLEED SOURCE FOR AIR CONDITIONING. SEVERAL LEVEL 3 ECAM CARGO COMPARTJun 15, 2015 · N719FD · Airbus A300B4622 · Air Distribution SystemSDR FDEA201504291324Frame Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24R & 26R HOLE N & ONE EACH ADJACENT HOLE WITH CRACK SIGNAL.Apr 29, 2015 · N719FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201504281310Skin · crackedHFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44R LATERAL PANEL.Apr 28, 2015 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201504281309Skin · crackedHFEC OPEN HOLE INSPECTION FOUND TWO HOLES WITH CRACK INDICATION ON FUSELAGE CTR SECTION FRAME 54, STRINGER 44L LATERAL PANEL.Apr 28, 2015 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201504241291Bolt · missingCTR WING JOINT AT FRAME 40. FOUND LT & RT SIDE HAS SIX BOLTS MISSING. REPAIRED IAW EA 6-5710-T0317008 P1. MAJOR REPAIR IAW GMM6-2-100.Apr 24, 2015 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201504211271Beam · crackedHFEC FOUND CTR FUSELAGE LONGITUDINAL BEAM 4 WITH CRACK INDICATION AT FRAME 49LT.Apr 21, 2015 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201504211270Spar · crackedFUSELAGE CTR WING BOX. INSPECTION OF REAR SPAR & BOTTOM PANEL FASTENER HOLE H WITH CRACK SIGNAL, LT SIDE. COMPLIED WITH EA6-5710-T0317395 PT 1. MINOR REPAIR IAW GMM 6-2-100.Apr 21, 2015 · N719FD · Airbus A300B4622 · Wing SparSDR FDEA201504211269Spar · crackedFUSELAGE CTR WING BOX. INSPECTION OF REAR SPAR & BOTTOM PANEL FASTENER HOLE L WITH CRACK SIGNAL, LT SIDE. COMPLIED WITH EA6-5710-T0317395 PT 1. MINOR REPAIR IAW GMM6-2-100.Apr 21, 2015 · N719FD · Airbus A300B4622R · Wing SparSDR FDEA201408292356Flex Line · looseIN CRUISE FLIGHT ENG 2 WOULD NOT RETARD BELOW 1.30 EPR, CREW RAN THE LACK OF THROTTLE RESPONSE INFLIGHT CHECKLIST. THIS RESULTED IN ENG 2 EPR NO LOWER THAN 1.22. THIS WAS ACCEPTABLE FOR CRUISE FLIGHT, BUT TOO MUCH THRUST FOR THE APPROACH ENVIRONMENT. IAW THAug 29, 2014 · N719FD · Airbus A300B4622 · Power LeverSDR FDEA201408282341Fmu · faultyON DESCENT, NR 2 ENG REMAINED STUCK AT CRUISE POWER & COULD NOT BE CONTROLLED IN AUTO THROTTLE OR MANUAL THROTTLE. ENG HAD TO BE SHUT DOWN FOR LANDING. HAD POSITIVE OIL PRESS BEFORE & AFTER SHUTDOWN. ENG WAS SHUT DOWN FOR APPROX 10 MINUTES. R&R NR 2 ENGINAug 28, 2014 · N719FD · Airbus A300B4622 · Fuel Control/Turbine EnginesSDR FDEA201309242299Pitot Tube · damagedREJECTED TAKEOFF AT 70 KTS FOR NO AIRSPEED ON CAPTAIN`S TAPE. REMOVED AND REPLACED PITOT PROBE IAW MM 34-11-15-04. LEAK AND OPS CHECKED GOOD. ACFT OK FOR SERVICE.Sep 24, 2013 · N719FD · Airbus A300B4622 · Pitot/Static SystemSDR FDEA201309242297Indicator · malfunctionedREJECTED TAKEOFF AT 90 KTS, AT 80 KTS CROSS CHECK CAPTAIN`S AIRSPEED TAPE HAD NOT MOVED. NO FLAGS. STANDBY AIRSPEED NORMAL. FLUSHED CAPTAIN'S TOTAL PRESSURE LINES IAW AMM 34-10-00-03 NO BLOCKAGE NOTED. PERFORMED SYSTEM LEAK TEST PER AMM 34-10-00 P BLOCK 501 Sep 24, 2013 · N719FD · Airbus A300B4622 · Airspeed/Mach IndicatorSDR FDEA201307121546O-Ring · failedGREEN HYD SYS FAILURE IN FLIGHT, DIVERTED. NORMAL APPROACH AND LANDING. ALL EMERGENCY CHECKLIST COMPLIED. GREEN SYS QTY DROPPED TO LOWER END OF GREEN RANGE & ENGINE DRIVEN HYD PUMPS WERE SELECTED OFF AS SOON AS HYD QTY STARTED TO DROP, QTY NEVER CAME CLOSEJul 12, 2013 · N719FD · Airbus A300B4622 · Hydraulic System, MainSDR FDEA201302060275Longeron · crackedFOUND THREE CRACKS IN AREA"C" OF INNER FLANGE OF THE LONGERON AT STRINGER 11 B/W, FR75 AND FR75A ON LT SIDE CUT OUT THE CRACK FLANGE AND SPLICE REPAIR IAW SRM53-18-18/201, FIG 205C.Feb 6, 2013 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR FDEA201301300222Lug · corrodedRT MLG SUPPORT RIB FWD LUG BORE AND FACES FOUND CORROSION COMPLY WITH EA 6-5710-163177.Jan 30, 2013 · N719FD · Airbus A300B4622 · Wing, Landing Gear Attach FittingsSDR FDEA201301300221Lug · corrodedLT MLG SUPPORT RIB FWD LUG BORE AND FACES FOUND CORROSION COMPLY WITH EA 6-5710-163175.Jan 30, 2013 · N719FD · Airbus A300B4622 · Wing, Landing Gear Attach FittingsSDR FDEA201301290214Skin · delaminatedLEFT AILERON T/E INBD CORNER FOUND DELAMINATION ON UPPER & LOWER SKIN. REPAIRED THE DELAMINATED AREA PER EA#6-5750-163173.Jan 29, 2013 · N719FD · Airbus A300B4622 · AileronsSDR FDEA201301120085Structure · damagedFOUND TRAPPED WATER IN RUDDER LT SIDE PANEL TRAILING SCREW LINE. REMOVED OUTER SKIN AND CORE IN THE DAMAGED AREA MADE HONEYCOMB CORE PLUG PER SRM 55-41-12/201 FIG 222. DRIED THE REPAIR AREA AT 60 DEGREE FOR AT LEAST 20 HOURS PER SRM 51-77-10. INSTALLED Jan 12, 2013 · N719FD · Airbus A300B4622R · Rudder StructureSDR FDEA201210183660Rib · crackedRIGHT MLG RIB 5, CRACKED 22MM LENGTH. COMPLIED WITH EA 6-5710-163140.Oct 18, 2012 · N719FD · Airbus A300F4622R · Wing, Rib/BulkheadSDR FDEA201110064346Skin · crackedCRACK RT CENTER FLAP UPPER SKIN BETWEEN RIBS 11 AND 12 REPAIRED IAW SRM 57-50-00 FIG 205, EA 6-5750-153027.Oct 6, 2011 · N719FD · Airbus A300F4622R · Trailing Edge FlapsSDR FDEA201009043273Skin · gougedLT WING OTBD FLAP INBD L/E GOUGED APPROX 0.500 IN LENGTH X 0.250IN WIDTH BLENDED AREA ON LT OTBD FLAP INBD L/E REF SRM 51-73-00 NDT FOUND NO CRACK REF NTM 51-10-08 BEFORE BLEND 0.053 MAT LOSS 0.017 IN MAT REMAINING 0.036 IN OUT OF LIMITS REF SRM 57-50-00 REMSep 4, 2010 · N719FD · Airbus A300B4622 · Trailing Edge FlapsSDR FDEA201007072400Smoke Detector · false activationON CLIMBOUT, RECEIVED AN AVIONICS SMOKE ECAM, WITH NO SMOKE DETECTED IN COCKPIT. RETURNED TO DEPARTURE. PERFORMED OPS CHECK IAW 26-15-00-05. ALL OPS NORMAL. R & R DETECTORS 11WA, 12WA,13WA AS PRECAUTION, OPS CHECKED NORMAL IAW MM 26-15-00-05. OK TO CONTINUEJul 7, 2010 · N719FD · Airbus A300B4622 · Smoke DetectionSDR FDEA200912294543Roller · wornRIGHT AFTER T/O, GOT AN ECAM WARNING FWD AVIONICS DOOR NOT CLOSED. BOTH PILOTS HAD ABNORMAL PRESSURE IN THE CABIN. IAW QRH. MX FOUND DOOR CLOSED, INSP OF LOCKING ROLLER ON DOOR FOUND WORN REPLACED SAME & CHECKED IAW IPC 52-71-00-01B, ABMM 52-41-14-5, ABMM Dec 29, 2009 · N719FD · Airbus A300B4622 · Electrical/Electronic Compartment DoorsSDR 08FDEA02905Frame · corrodedAIR COND BAY HAS CORROSION ON UPPER SURFACE OF "T" ON FR 39 BETWEEN STR 50 AND STR 51 RT SIDE. REMOVED AND REPLACED "T" SECTION FROM STRINGER 53 RHS TO STRINGER 49 RHS. THE NEW "T" SECTION HAS BEEN SPLICED WITH ANGLE ON AFT FACE AND PLATE ON FORWARD FACE. IJul 15, 2008 · N719FD · Airbus A300B4622 · Fuselage Main, Frame
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