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 FDEA201603230999Floor Panel · crackedMAIN DECK COMPARTMENT FLOOR PANEL 241BF CRACKED. FABRICATED FLOOR PANEL 241BF ON T16 1195955 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230998Floor Panel · brokenMAIN DECK FLOOR PANEL 251SH HAS BROKEN CORNER PIECE. FABRICATED FLOOR PANEL 251SH ON T16 1195959 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230997Floor Panel · brokenMAIN DECK FLOOR PANEL 251ZG HAS BROKEN CORNER PIECE. FABRICATED FLOOR PANEL 251ZG ON T16 1196092 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230994Floor Panel · crackedMAIN DECK FLOOR PANEL 241JF IS CRACKED. FABRICATED FLOOR PANEL 241JF ON T16 1195908 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230993Floor Panel · crackedMAIN DECK FLOOR PANEL 241QF IS CRACKED. FABRICATED FLOOR PANEL 241QF ON T16 1195834 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230992Floor Panel · damagedMAIN DECK FLOOR PANEL 251RG IS DAMAGED. FABRICATED FLOOR PANEL 251RG ON T16 1196095 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603230991Floor Panel · crackedMAIN DECK FLOOR PANEL 232WG IS CRACKED. FABRICATED FLOOR PANEL 232WG ON T16 1195903 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 23, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603221003Floor Panel · crackedMAIN DECK FLOOR PANEL 242ZH IS CRACKED. FABRICATED FLOOR PANEL 242ZH ON T16 1195902 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220990Floor Panel · damagedMAIN DECK FLOOR PANEL 232RG IS PUNCTURED & ELONGATED HOLES. FABRICATED FLOOR PANEL 232RG ON T16 1195821 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220989Floor Panel · damagedMAIN DECK FLOOR PANEL 251WH IS DAMAGED. FABRICATED FLOOR PANEL 251WH ON T16 1196096 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220988Floor Panel · damagedMAIN DECK PANEL 251BF IS DAMAGED. FABRICATED FLOOR PANEL 251BF ON T16 1196094 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220987Floor Panel · brokenMAIN DECK FLOOR PANEL 251NG HAS BROKEN CORNER. FABRICATED FLOOR PANEL 251NG ON T16 1196093 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220986Floor Panel · crackedMAIN DECK FLOOR PANEL 241FK IS CRACKED. FABRICATED FLOOR PANEL 241FK ON T16 1195838 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220985Floor Panel · crackedMAIN DECK FLOOR PANEL 242GK IS CRACKED. FABRICATED FLOOR PANEL 242GK ON T16 1195904 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220984Floor Panel · damagedMAIN DECK FLOOR PANEL 252HH, HAS A DAMAGED CORNER. FABRICATED FLOOR PANEL 252HH ON T16 1195960 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603220983Floor Panel · damagedMAIN DECK FLOOR PANEL 251JF, MIDDLE PANEL HAS BROKEN CORNER. FABRICATED FLOOR PANEL 251JF ON T16 1195858 IAW SRZ-25-005. CLASSIFIED AS MAJOR REPAIR CAT A.Mar 22, 2016 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201603210960Seat Track · gougedMDC SEAT TRACK GOUGED, FRAME 57, -Y1959. REMOVED DAMAGE IAW SRM 51-73-10. CHECKED LIMITS= L=0.140", W= 0.406", D= 0.118", FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, TR 86778 & TR 85721. REMOVED DAMAGED SECTION IAW SRM 53-10-16 FIG 208. REMOVED 6 EACH SPLIMar 21, 2016 · N717FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201603180945Seat Track · corrodedCOURIER AREA AT FRAME 18 & 19, & -Y450 SEAT TRACK HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. TREATED ALODINED, PRIMED & PAINTED IAW SRM 53-10-16 FIG 102. REMOVED CORROSION AT SEAT TRACK FLANGE FRAME 18, FOUND TO BE OUT OF LIMITS. FABRICATEMar 18, 2016 · N717FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201601010005Sensor · failedDURING DESCENT AT 180FL, THE ECAM SHOWED FUEL LOW LEVEL WITH THE LOW LEVEL LIGHT ON THE OVERHEAD FOR THE LT OUTER TANK. FOUND PLUG LOOSE TO THE LOW LEVEL SENSOR UPON TANK ENTRY. R & R THE LT OUTER LOW LEVEL SENSOR 605QJ.Jan 1, 2016 · N717FD · Airbus A300B4622 · Fuel Quantity SensorSDR FDEA201410133154Warning System · malfunctionedL1 DOOR ESCAPE SLIDE BUZZER WILL NOT TEST. RELEASED FOR SERVICE IAW MEL 52- XX. L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYS BUZZERS INOPERATIVE. PERFORMED OPERATIONAL CHECK OF L1 DOOR EMER DOOR WARNING SYS. NO DEFECT NOTED, OPERATED NORMAL SEVERAL TIMES IOct 13, 2014 · N717FD · Airbus A300B4622 · Door Warning SystemSDR FDEA201409192685Fitting · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.Sep 19, 2014 · N717FD · Airbus A300B4622 · Wing Miscellaneous StructureSDR FDEA201409192683Fitting · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P1 WING BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.Sep 19, 2014 · N717FD · Airbus A300B4622 · Wing Miscellaneous StructureSDR FDEA201401250194Angle · crackedAT EMPENNAGE AREA BETWEEN FRAME 86 & FRAME 87, STRINGER 34L UPPER ANGLE CRACKED. REMOVED WEB & UPPER ANGLE IAW SRM 51-40-21, NO DAMAGE ON WEB NOTED. FABRICATED NEW ANGLE IAW DRAWING 53986751, MAT 2024-T3, 032C BATCH 0002526114. LOCATED & DRILLED, TREATED & Jan 25, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401210155Bulkhead · corrodedCOMPARTMENT AFT OF FWD CARGO BAY FRAME 39, FWD CORNER OF PRESSURE BULKHEAD CORRODED. PERFORMED REPAIR IAW DWG R53810795 & R53810796 IAW EA 6-5310-T0304935.Jan 21, 2014 · N717FD · Airbus A300B4622 · Fuselage Main, BulkheadSDR FDEA201401120089Intercostal · bentCOMPARTMENT INTERIOR INTERCOSTAL ANGLE BENT AT STRINGER 33L BETWEEN FRAMES 84 - 85. REMOVED DAMAGED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED NEW ANGLE IAW T13 1039785 & SRM 53-19-18. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.Jan 12, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401120087Intercostal · crackedCOMPARTMENT INTERIOR INTERCOSTAL ANGLE CRACKED & BENT AT STRINGER 33R BETWEEN FRAMES 86 - 87. REMOVED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED INTERCOSTAL ANGLE IAW T13 1039629 & T131039784. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.Jan 12, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401120086Intercostal · bentCOMPARTMENT INTERIOR INTERCOSTAL BENT AT STRINGER 33L BETWEEN FRAMES 85 - 86. REMOVED DAMAGED INTERCOSTAL ANGLE IAW SRM 51-40-21. FABRICATED NEW ANGLE STRAP IAW T13 1039628 IAW SRM 53-19-18. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-40-21.Jan 12, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401120088Intercostal · bentCOMPARTMENT INTERIOR INTERCOSTAL ANGLE BENT AT STRINGER 34R BETWEEN FRAMES 86 - 87. REMOVED DAMAGE ANGLE IAW SRM 51-40-21. FABRICATED PART IAW T13 1040084. INSTALLED ANGLE IAW SRM 51-40-21.Jan 12, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401100079Strap · bentTHIS COMPARTMENT INTERIOR INTERCOSTAL RIB BENT AT STRINGER 33R BETWEEN FRAME 85 - FRAME 86. R & R INTERCOSTAL RIB STRAP, FABRICATED ON T13/1039630 BATCH 0002540969 AT STRINGER 33R BETWEEN FRAME 85 - FRAME 86 IN THIS COMPARTMENT IAW SRM 51-40-21. TOP COATED FAJan 10, 2014 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201401070063Skin · dentedAFT FUSELAGE SKIN BETWEEN FRAMES 96 & 97 FROM STRINGER 3 & 4R DENTED. REPAIRED IAW SRM 53-19-12 FIG 202.Jan 7, 2014 · N717FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201401020006Floor Panel · damagedBULK CARGO COMPARTMENT FLOOR PANEL 161AF HAS NUMEROUS DENTS & PUNCTURED IN 1 LOCATION. FABRICATED NEW FLOOR PANEL 161AF ON T13 1040702 IAW DRAWING SRZ=25-005.Jan 2, 2014 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312313074Stringer Splice · corrodedSTRINGER SPLICE HAS CORROSION FRAME C83, STRINGER 36R. REMOVED CORROSION L 500 INCHES, W .500 INCHES & D .045 INCHES, FOUND TO BE OUT OF LIMITS IAW SRM 53-19-14 PAGE 101. REPLACED SPLICE IAW SRM 51-40-21 & 51-40-44.Dec 31, 2013 · N717FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR FDEA201312303069Skin · dentedFORWARD LOWER SKIN DENTED AT FRAME 16 BETWEEN STRINGERS 33 - 34R. REPAIRED IAW SRM 53-12-12 FIG 202. REPAIR CLASSIFIED AS MAJOR.Dec 30, 2013 · N717FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201312303068Skin · dentedFORWARD LOWER FUSELAGE RT SIDE DENTED BETWEEN FRAMES 6 - 7 & STRINGER 26 - 27R. REPAIRED IAW SRM 53-11-12 FIG 201. REPAIR CLASSIFIED AS MAJOR.Dec 30, 2013 · N717FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR FDEA201312293065Floor Panel · damagedBULK CARGO COMPARTMENT FLOOR PANEL 162HF HAS NUMEROUS DENTS & SEVERAL PUNCTURES. R & R FLOOR PANEL 162HF IAW SRM 51-72-10.Dec 29, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312193020Floorboard · puncturedMAIN CABIN DECK FLOORBOARD BETWEEN FR 26 - FR 29 Y O IS PUNCTURED ON TOP SURFACE. R & R FLOOR PANEL IAW AMM 53-10-25-04-02. FABRICATED FLOOR PANEL IAW SRZ-25-005.Dec 19, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183015Floor Panel · crackedAFT CARGO BAY FLOOR PANEL 152EF EDGE IS CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 106. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183014Floor Panel · crackedMID CABIN FLOOR PANEL 241TH CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183013Floor Panel · crackedMID CABIN FLOOR PANEL 241HK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183012Floor Panel · crackedMID CABIN FLOOR PANEL 241LK CRACKED, FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183011Floor Panel · damagedMID CABIN FLOOR PANEL 241AK EDGE BROKEN, FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183009Floor Panel · crackedMID CABIN FLOOR PANEL 242HK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183008Floor Panel · crackedMID CABIN FLOOR PANEL 241RJ CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183007Floor Panel · crackedMAIN DECK FLOOR PANEL 241JF CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183006Floor Panel · damagedMID CABIN FLOOR PANEL 242EK PUNCTURED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201312183005Floor Panel · crackedMID CABIN FLOOR PANEL 242LK CRACKED. FOUND OUT OF LIMITS IAW SRM 53-10-20 FIG 105. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005.Dec 18, 2013 · N717FD · Airbus A300B4622 · Fuselage Floor PanelSDR FDEA201211214120Mount · corrodedNR 2 ENG PYLON FWD ENGINE MOUNT FITTING INBD AFT TENSILE BOLT HOLE HAS OXIDATION AND PITTING IN ITS BORE. REAMED NR 2 ENG FWD ENG MOUNT FITTING TO CLEAN OXIDATION AND PITTING TO 0.997 IAW SRM 54-51-81. INSP HOLE FOR CRACKS IAW NTM 51-60-00. REPROTECTED BORE IANov 21, 2012 · N717FD · Airbus A300B4622 · Engine Mount SectionSDR FDEA201107262962Frame · dentedMAIN DECK FUSELAGE FRAME DENTED AT STA 1741, LT L12. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV112.Jul 26, 2011 · N717FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201107262953Spar · damagedDURING ACCOMPLISHMENT OF EO6-5710-7-3305, D2, PT3 WORK STEP 6, FOUND HOLE 'A' EXISTING FASTENER HOLE DIAMETER 0.625" IS BIGGER THAN NEW FASTENER SIZE 0.562" AT CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE LT SIDE. INSTALLED NEW FASJul 26, 2011 · N717FD · Airbus A300F4622R · Wing, Center BoxSDR FDEA201107262950Frame · crackedCABIN LT SIDE FRAME 40 TOP MOST TENSION BOLT HOLE 'A'. FOUND DAMAGED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION. FRAME REPAIRED AS PER EA 6-5710-143620 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV112.Jul 26, 2011 · N717FD · Airbus A300F4622R · Fuselage Main, Frame
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