N717FD

Service difficulty reports · 155

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 = 'N717FD' 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 FDEA201810162902Rib · crackedX-RAY INSPECTED, LT WING CENTER FLAP RIB 27 POSN FOUND CRACKED. PER SRM 57-50-00-201 PARA 4A FIG 201 REPAIRED THE CRACKED RIB. AND PER SRM 57-50-00-201 PARA 4E FIG 205 MAKE THE SKIN REPAIR DOUBLER & WET INSTALL THE REPAIR DOUBLER. THIS REPAIR IS CAT A MAJOR REOct 16, 2018 · N717FD · Airbus A300B4622 · Trailing Edge FlapsSDR FDEA201810152884Stringer · crackedNDT INSPECTED, RT WING LOWER SKIN RIB18, STRINGER 11 WEB POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/StringerSDR FDEA201810152883Stringer · crackedNDT INSPECTED, RT WING UPPER SKIN RIB18, STRINGER 11 POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/StringerSDR FDEA201810152882Stringer · crackedLT WING FUEL TANK RIB18 STRINGER WEB NDT INSPECT FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5720-T0343001. MINOR REPAIR IAW GMM 6-2-100.Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/StringerSDR FDEA2018102612756Doubler · chafedEXISTING REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 WAS EVALUATED AND FOUND CHAFING DAMAGE ON REPAIR DOUBLER PER EA: 6-5750-124214. REWORK THE REPOct 1, 2018 · N717FD · Airbus A300B4622 · Trailing Edge FlapsSDR FDEA201809252674Fitting · crackedFUSELAGE CENTER WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE "M" FOUND CRACK SIGNAL. PER EA 6-5710-167809 B PT2 REPAIR THE CRACKED "M" HOLE. THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100.Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201809252678Web · crackedTOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201809252677Web · crackedTOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y-450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201809252676Web · crackedTOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. TOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. REPAIR THE CRACKED WEB PER SRM 53-15-15-201 PARA.5.A FIG201. THIS IS BSep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201809252675Web · crackedTOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y-1456 AND Y-953 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201809252673Crossbeam · unknownEXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR35 Y-140 - Y-1470 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAISep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Main, StructureSDR FDEA201809252671Crossbeam · unknownEXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR27 Y-140 - Y-805 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIRSep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Main, StructureSDR FDEA2018092532660Crossbeam · unknownEXISTING REPAIR ON AFT CARGO FLOOR CROSSBEAM AT FR56 LHS REQUIRES EVALUATION FOR CONFORMITY THE REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53-10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATALOG- A300/A31Sep 23, 2018 · N717FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA2018092532659Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER BTW FR60 AND FR62 STGR51 LH REQUIRES EVALUATION FOR CONFORMITY THE REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53-10-14 FIG201 SHT1,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR CATSep 23, 2018 · N717FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA201807101661Limiter · malfunctionedSLATS STUCK LESS THAN 15 DEGREES ON RETRACTION. SLATS SYS 1 AND 2 FAULT LIGHTS ILLUMINATED. FOLLOWED ECAM AND QRH. SFP1 SLAT POSITION REMAINED STUCK. ARRIVED AT THE GATE THE FLAPS AND SLATS WERE FULLY RETRACTED, CREW DEBRIEF STATED THAT THE SLATS RESET AFTER Jul 10, 2018 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA201806301609Computer · failedSLATS SYS 1/2 FAULTS AND SLATS STUCK BETWEEN 0 AND 15 DURING RETRACTION AFTER TAKEOFF. CYCLED SLAT/FLAP HANDLE PER QRH. SLATS WENT BACK TO 15 BUT STUCK AGAIN DURING RETRACTION. RETURNED TO AIRPORT AND SLATS AND FLAPS EXTENDED NORMALLY FOR APPROACH. SLATS RETRAJun 30, 2018 · N717FD · Airbus A300B4622 · Leading Edge Slat Control SystemSDR FDEA201806191541Pitot Tube · failedDURING T/O ROLL, FO'S PFD DID NOT DISPLAY ANY AIRSPEED. REJECTED T/O AT 65 KIAS. REMOVED AND REPLACED F/O'S PITOT TUBE REF 34-11-15-04, OPS CHECK GOOD. INSPECTED OLD PITOT TUBE ASSY AND FOUND INSECT IN TUBE. A/C OK FOR CONTINUED SERVICE.Jun 19, 2018 · N717FD · Airbus A300B4622 · Pitot/Static SystemSDR FDEA201806191540Adc · failedDURING T/O ROLL, NO AIRSPEED WAS INDICATED ON THE F/O'S PFD. REJECTED T/O AT 70 KTS. PERFORMED LEAK TEST, HELD 350 KTS FOR OVER 20 MINUTES. REMOVED AND REPLACED NR 2 ADC, OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE.Jun 19, 2018 · N717FD · Airbus A300B4622 · Air Data ComputerSDR FDEA201803150699Flap System · malfunctionedON APPROACH, SLATS EXTENDED AND INDICATED NORMALLY. AT FLAPS 15 AND FLAPS 20 COULD FEEL A PITCH CHANGE, BUT STILL NO INDICATOR MOVEMENT. CYCLED THE FLAP HANDLE AND COULD FEEL PITCH CHANGE BUT STILL NO INDICATION. PERFORMED A GO AROUND AND INDICATOR BEGAN TOMar 15, 2018 · N717FD · Airbus A300B4622 · Trailing Edge Flap Control SystemSDR FDEA201709282781Rudder · delaminatedRUDDER THERMOGRAPH FAILS STEP 10 EA 6-5540-A0319362 A PT2 PREVIOUS REPAIR. REPAIRED RIGHT HAND PREVOUS REPAIR AREA BETWEEN NR 3 AND NR 4 SCREW ON TRAILING EDGE FROM BOTTOM IAW SRM 55-41-12-201 PARA 31 FIG 222, EA 6-5540-T0335547, AND TD/7037 1608/807/2017A. MSep 28, 2017 · N717FD · Airbus A300B4622 · Elevator StructureSDR FDEA201709282779Skin · dentedRUDDER OUTER LEFT SKIN APPROX 4.5FT FROM BOTTOM OF RUDDER AND APPROX 3 FT FROM THE LEADING EDGE SPAR THERE IS A DENT " BY 0.025". REPAIRED SKIN IAW SRM 55-41-12 PARA 30 FIG 219-220, AND COMPLIED WITH EA 6-5540-T0335649 CLASSIFIED AS A CAT "B" MAJOR REPAIR.Sep 28, 2017 · N717FD · Airbus A300B4622 · Rudder, Plate/SkinSDR FDEA201702270669Transmitter · crackedDURING CRUISE, FL350, ECAM WARNING WITH GREEN HYD SYSTEM LOW QUANTITY LEVEL WHICH WAS ALSO SHOWING ON HYD PAGE OF ECAM. ACCOMPLISHED QRH PROCEDURE TO INCLUDE MANUAL GEAR EXTENSION, QTY INCREASED UPON ENGINE SHUTDOWN. REMOVED AND REPLACED THE GREEN PRESSFeb 27, 2017 · N717FD · Airbus A300B4622 · Hydraulic System, MainSDR FDEA201611113979Control Unit · malfunctionedDURING CLIMBOUT AND TWICE DURING CRUISE, AIRCRAFT YAWED ABRUBTLY AND UNCOMMANDED. ALL FLT CONTROL PARAMETERS CHECKED NORMAL. SET FAULTS FCC NR 1 WITH TRANS FLAG.AND FMC 1 & 2 WITH NCD. R & R NR 1 FAC AS A PRECAUTION IAW MM 22-18-34-04 AND PERFORMED AFS/LNov 11, 2016 · N717FD · Airbus A300B4622 · Autopilot SystemSDR FDEA201607142460Warning System · false activationDURING CLIMBOUT, PASSING 8000 FT LT AMBER ECAM FOR AVIONICS DOOR OPEN. RELEASED FOR SERVICE IAW MEL. VERIFIED FORWARD AVIONICS DOOR CLOSED AND LOCKED. ITEM WAS VERIFIED CLOSED, MEL ADDED, AIRCRAT DEPARTED. MEL ITEM FACT'S PER AMM 52-41-14-05-02 ADJ/TEST, NOJul 14, 2016 · N717FD · Airbus A300B4622 · Door Warning SystemSDR FDEA201605251729Wire · damagedAFTER BLOCK IN, SPARKS COMING FROM THE CEILING PANEL NEXT TO THE GND SERVICE PANEL. AFTER REMOVING THE FWD CEILING PANEL FWD OF THE GND SERVICE PANEL FOUND WIRES BURNT. ALSO FOUND CB`S TR2 SUPPLY & 205XP BUS BAR & 214XP & 215XP GND SERVICE BUS BAR, TERMINAL BMay 25, 2016 · N717FD · Airbus A300B4622 · Light System WiringSDR FDEA201604141215Roller Tray · corrodedUPON REMOVAL OF ROLLER TRAY AT FRAME 32, FOUND HEAVY CORROSION ON TOP OF FLANGE. CHECKED DIMENSIONS L 5.0", W 1.5" NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REPAIRED UPPER FLANGE BY CUTTING & SPLICING IAW SRM 53-10-15 FIG 207. FABRICATED FLANGE ON T16 119851Apr 14, 2016 · N717FD · Airbus A300B4622 · Cargo CompartmentsSDR FDEA201604061154Skin · corrodedFORWARD CARGO PIT, BETWEEN FRAME 36 - 37 & STRINGERS 50 - 51 LT SIDE HAS LIGHT SURFACE CORROSION ON THE INTERNAL SKIN. ACCOMPLISHED SKIN REPAIR ON EA 6-5330-T03244564. CLASSIFIED AS A MAJOR CAT C REPAIR.Apr 6, 2016 · N717FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201603261061Floor Panel · corrodedFORWARD PIT FLOOR PANEL 132QF, HAS CORROSION AROUND FASTENER HOLES. FABRICATED FLOOR PANEL 132QF ON T16 1196402 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261072Fitting · corrodedAFT CARGO BILGE HAS CORROSION ON SHEAR CLIP A FRAME 59, STRINGER L 54. R & R SHEAR CLIP IAW SRM 51-40-21. FABRICATED SHEAR CLIP ON T16 1196435. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201603261071Crossbeam · crackedBULK CARGO COMPARTMENT HAS CRACK ON FLOORBEAM SUPPORT LT CTR AT FRAME 66. BLENDED CORRODED AREA IAW SRM 51-10-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED CROSSBEAM IAW SRM 51-40-22, FABRICATED NEW INTERCOSTAL IAW SRM 51-40-44, INSTALLED NEW CROSMar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201603261070Floor Panel · damagedFORWARD PIT FLOOR PANEL 131QF HAS DELAMINATION AT EDGES & PUNCTURES ON BOTTOM SIDE. FABRICATED FLOOR PANEL 131QF ON T16 1196097 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261069Floor Panel · puncturedFORWARD PIT FLOOR PANEL 132HG HAS PUNCTURES ON BOTTOM SIDE. FABRICATED FLOOR PANEL 132HG ON T16 1196118 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261068Floor Panel · delaminatedFORWARD PIT FLOOR PANEL 132ZF HAS DELAMINATED EDGES, MISSING & TORN INSERTS. FABRICATED FLOOR PANEL 132ZF ON T16 1196407 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261067Floor Panel · delaminatedFORWARD PIT FLOOR PANEL 132JG IS DELAMINATED AROUND THE EDGES & HAS BROKEN INSERTS. FABRICATED FLOOR PANEL 132JG ON T16 1196111 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261066Floor Panel · delaminatedFORWARD PIT FLOOR PANEL 131ZF IS DELAMINATED & BROKEN. FABRICATED FLOOR PANEL 131ZF ON T16 1196409 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261065Floor Panel · damagedAFT PIT FLOOR PANEL 152CF IS DAMAGED. FABRICATED FLOOR PANEL 152CF ON T16 1196410 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261064Floor Panel · damagedBULK PIT FLOOR PANEL 161BF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 161BF ON T16 1196408 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261063Floor Panel · delaminatedBULK PIT FLOOR PANEL 161GF HAS DELAMINATION ON UPPER SKIN. FABRICATED FLOOR PANEL 161GF ON T16 1196098 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261060Floor Panel · crackedAFT PIT FLOOR PANEL 151AF IS CRACKED. FABRICATED FLOOR PANEL 151AF ON T16 1196099 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261059Floor Panel · damagedAFT PIT FLOOR PANEL 151FF IS DAMAGED. FABRICATED FLOOR PANEL 151FF ON T16 1196113 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261058Floor Panel · crackedAFT PIT FLOOR PANEL 151CF IS CRACKED. FABRICATED FLOOR PANEL 151CF ON T16 1196112 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261057Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241KF DELAMINATED. FABRICATED FLOOR PANEL 241KF ON T16 1197922 IAW SRZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603261056Frame · crackedMAIN CABIN RT SIDE FRAME 43 IS CRACKED, BETWEEN STRINGER 24 - 28. REMOVED FRAME 43, BETWEEN STRINGERS 24 - 28 RT IAW SRM 51-40-21. LOCATED & DRILLED NEW FRAME IAW SRM 51-40-44. INSTALLED NEW FRAME IAW SRM 51-40-21. PAINTED AREA IAW SRM 51-75-10. THIS REPAMar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201603261055Floor Panel · brokenFORWARD PIT FLOOR PANEL 131RF HAS BROKEN OUT INSERT. FABRICATED FLOOR PANEL 131RF ON T16 1196100 IAW RZ-25-005. CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Mar 26, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603241046Seat Track · gougedMDC SEAT TRACK GOUGED, 5" FWD OF FRAME 57.1 & Y450. REMOVED DAMAGED AREA, AFTER REWORK L=0.26" & W=0.20, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. FABRICATED NEW SEAT TRACK SECTION FROM PN A53274005- SFS-DAP, FROM FRAME 57.1 - 58, Y450, IAW SRM 53-Mar 24, 2016 · N717FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201603231005Floor Panel · crackedMAIN DECK FLOOR PANEL 232CF IS CRACKED. FABRICATED FLOOR PANEL 232CF ON T16 1195816 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603231004Floor Panel · crackedMAIN DECK FLOOR PANEL 242ZJ IS CRACKED. FABRICATED FLOOR PANEL 242ZJ ON T16 1195835 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603231002Floor Panel · crackedMAIN DECK FLOOR PANEL 242EF IS CRACKED. FABRICATED FLOOR PANEL 242EF ON T16 1195824 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603231001Floor Panel · puncturedMAIN DECK FLOOR PANEL 242WH IS PUNCTURED. FABRICATED FLOOR PANEL 242WH ON T16 1196091 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603231000Floor Panel · crackedMAIN DECK FLOOR PANEL 241QJ IS CRACKED. FABRICATED FLOOR PANEL 241QJ ON T16 1195906 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor Panel
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