N718FD, cancelled Mar 2, 2024
Service difficulty reports · 130
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 = 'N718FD' AND deregistration_id = 'N718FD-2024-03-02' 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.
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 = 'N718FD' AND deregistration_id = 'N718FD-2024-03-02' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201305150999Spring · failedACCESS PANEL 572CB INBD SPRING ROD ASSY DAMAGED. SPRING ASSY FOUND TO HAVE FAILED INSIDE FLAP SHROUD BOX, THIS HAD CAUSED STRUCTURAL DAMAGE TO THE FWD WEB AND FLAP DRIVE TORQUE SHAFT. REPAIRED IAW EA 6-5751-167417.SDR FDEA201210033548Spar · damagedRT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE, SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.SDR FDEA201210033547Spar · damagedRT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE WITH SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.SDR FDEA201210013525Structure · damagedRT WING NR 2 SPOILER FWD POINT OF OTBD EDGE WORN. REPAIRED ON EA6-5771-157943, CAT B.SDR FDEA201210013522Skin · dentedSHALLOW DENT EVIDENT BETWEEN AFT CARGO DOOR AND BULK CARGO DOOR FR 66, STR 38R-39R, FRAME 66 RT BETWEEN STR 38-39 DENT REPAIRED IAW SRM 53-10-12, FIG 228 MAJOR REPAIR WITH SMR REQUIRMENTS CAT B IAW SRI 53-10-12-2-009-00.SDR FDEA201209283504Skin · damagedRT WING LOWER SKIN HOLE 'S' BUSHINGS TO BE FABRICATED IAW ORIGINAL RAS INSTRUCTION. RT HOLE 'S' REWORKED IAW JPF STEP 2 IAW SRM 51-40-21. 3 BUSHINGS INSTALLED AT 19.1MM DIA IAW RDAS 70566845-003-2012 INSTRUCTION FOR RT SIDE HOLE NR1.SDR FDEA201209283501Skin · crackedLEFT WING LOWER SKIN HOLE G SHOWS EVIDENCE OF A CRACK INDICATION AND MECHANICAL DAMAGE IN THE MAIN BORE. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE G REWORKED UNTIL MECHANICAL DAMAGE REMOVED AND NO CRACK INDICATION STARTING AT A BORE DIAMETER OF 0.530"/13.462MSDR FDEA201209283500Skin · damagedLEFT WING LOWER SKIN HOLE 'S' SHOWS EVIDENCE OF MECHANICAL DAMAGE FROM STEEL BUSHES THROUGH THE FULL BORE DEPTH. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE 'S' REWORKED UNTIL MECHANICAL DAMAGE REMOVED STARTING AT A BORE DIAMETER OF 0.751"/19.075MM TO FINAL DSDR FDEA201209283499Spar · damagedLEFT WING FRM 47 HOLE C, MECHANICAL DAMAGE FOUND IN INTERNAL BORE OF FASTENER HOLE. MECHANICAL DAMAGE REMOVED IAW SRM 51-40-30 FINAL HOLE C DIAMETER IS 0.561"/14.249MM. REWORKED IAW EA 6-5710-162973, PAGE 2.SDR FDEA201209283497Skin · crackedLEFT WING LOWER SKIN HOLE F SHOWS EVIDENCE OF A CRACK INDICATION. THIS HOLE IS A PREVIOUSLY DIA 0.529 HOLE F REWORKED UNTIL CRACK REMOVED IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 3. HOLE F FINAL DIAMETER IS 0.561"/14.249MM.SDR FDEA201209283496Spar · damagedRT WING FR47 REAR SPAR HOLE V POSSIBLE BUSH WITH X4 IMPACT DAMAGE MARKS IN REAR FITTING. NO BUSH WAS FOUND AND HOLE V REMOVED. MECHANICAL DAMAGE IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 11. FINAL DIAMETER IS 0.584"/14.834 MM.SDR FDEA201209283495Spar · crackedRIGHT WING HOLE L CRACK INDICATED BY NDT INSP CRACK IS ASSESSED AS A CORNER CRACK IN THE FRM AT THE INTERFACE WITH REAR ANGLE FITTING AT 1 O'CLOCK POSITION HOLE L REWORKED UNTIL NO CRACK INDICATION IAW SRM 51-40-30. FINAL HOLE DIAMETER 0.624"/15.849 AS DESDR FDEA201209283494Frame · damagedRIGHT FRAME 47 REAR SPAR HOLE H SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 9 O'CLOCK THROUGH REAR SPAR DEPTH. MECHANICAL DAMAGE REMOVED FROM HOLE IAW SRM 51-40-30 FINAL BORE DIAMETER -0.499" AND THE MAXIMUM ALLOWED IN EO 6-5710-7-3305, PT 2 IS 0.499" REFER TO RSDR FDEA201209283493Frame · damagedRIGHT FRAME 47 REAR SPAR HOLE 'G' SHOWS EVIDENCE OF A CRACK INDICATION . THIS IS A PREVIOSULY REWORKED HOLE. MATERIAL REMOVED UNTIL CRACK INDICATION REMOVED STARTING AT BORE DIAMETER 0.259" TO FINAL BORE DIAMETER 0.560" IAW SRM 51-40-30 AND EA 6-5710-16297SDR FDEA201209283491Frame · damagedLEFT FRAME 47 REAR SPAR HOLE 'I' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 12 O'CLOCK THROUGH THE FULL BORE DEPTH. HOLE "I" REWORKED MECHANICAL DAMAGE REMOVED STARTING AT A BORE DIAMETER OF 0.531"/13.487MM TO 0.561"14.249MM IAW SRM 51-40-30 AND EA 6-5710-162SDR FDEA201209283490Frame · damagedLEFT FRAME 47 REAR SPAR HOLE 'N' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 5 O'CLOCK THROUGH THE FORWARD FITTING AND MAIN SPAR DEPTHS. MECHANICAL DAMAGE REMOVED FROM HOLE "N" IAW SRM 51-40-30 AND THE FINAL BORE DIAMETER IS 0.5605". THE MAXIMUM ALLOWED IN EO 6-SDR FDEA201209283489Frame · damagedLEFT FRAME 47 REAR SPAR HOLE 'M' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 11 O'CLOCK THROUGH THE FULL BORE DEPTH. MECHANICAL DAMAGE REMOVED FROM HOLE M STARTING AT A BORE DIAMETER OF 0.5295"/13.449MM TO FINAL DIAMETER OF 0.561"/14.249 MM IAW SRM 51-40-30 AND SDR FDEA201209283488Frame · damagedLEFT FRAME 47 REAR SPAR HOLE 'H' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 6 O'CLOCK AND 12 O'CLOCK THROUGH THE FULL BORE DEPTH. MECHANICAL DAMAGE REMOVED IAW SRM 51-40-30. DAMAGE REMOVAL IN LIMITS WITH EO 6-5710-7-3305 P1 CARD 11 OF 42 ITEM 10.SDR FDEA201209273480Angle · crackedLEFT MLG BAY FWD CUTOUT ANGLE CRACKED, REF SRM 53-15-13 FIG 4 ITEM 40. REPLACED ANGLE WITH NEW ANGLE FABRICATED IAW DWG A538122522 AND FITTED IAW SRM 51-40-21.SDR FDEA201209233413Frame · crackedFR 51 RT BODY FRAME FOUND CRACKED AT S26R BOLT HOLE. FRAME REPLACED IAW SRM 51-40-21 AND EA 6-5315-162967.SDR FDEA201209223395Frame · crackedFRAME 49 FOUND CRACKED, REWORKED AND SHOULDERED BUSHING FITTED IAW EA 6-5315-162967 AND SRM 51-40-21.SDR FDEA201209223394Frame · crackedFRAME 48 FOUND CRACKED AT S26R. UPPER FRAME SECTION REPLACED IAW EA 6-5315-162967 AND SRM 51-40-21.SDR FDEA201209223393Frame · damagedRIGHT FRAME 48, BOLT HOLE 2 FOUND EXCEED STANDARD SIZE. REWORKED IAW EA 6-5315-162967.SDR FDEA201209223392Frame · damagedRT FRAME 51, BOLT HOLE 2 FOUND EXCEED STANDARD SIZE. BOLT HOLE REWORKED IAW EA 6-5315-162967.SDR FDEA201209223391Frame · damagedRT FRAME 53, BOLT HOLE 3 FOUND EXCEED STANDARD SIZE. HOLE REWORKED IAW EA 6-5315-162967, STAGES 35-40 REF.SDR FDEA201209223390Frame · crackedFR 51 BOLT HOLE 4 FOUND CRACKED AND BOLT HOLE 1-3. FOUND EXCEED STANDARD LT FRAME 51 HOLE 4 FOUND CRACKED AND HOLES 1,2 AND 3 FOUND TO EXCEED STANDARD SIZE HOLES. REWORKED IAW EA 6-5315-162967, STAGES 10 TO 34 REF.SDR FDEA201209193356Frame · damagedFRAME 79 S44R FOUND DAMAGED AT FASTENER HOLE, REPAIRED IAW SRM 53-10-13, FIG 202. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201209183350Skin · delaminatedRT ELEVATOR TOP AND BOTTOM SKIN INBD AFT CORNER, DELAMINATING & PAINT CRACKING. REPAIRED IAW AE 6-5520-162959 , RAS 70566197/003/2012. MAJOR REPAIR CAT A.SDR FDEA201209183351Crossbeam · damagedAFT CARGO HOLD, ROLLER TRACK REPLACEMENT RT -Y1470 AT FR57 CROSSBEAM AND FRAME SUPPORT FITTING FOUND WITH EXTRA X2 HOLES AND CLOSE TO EXISTING STRUCTUAL FASTENERS DUE TO UNAUTHORIZED TRACK REPAIR. INVESTIGATE AND RECTIFY IAW RELEVANT MANUAL SRM. AFT CARGO HSDR FDEA201209173340Intercostal · crackedINTERCOSTAL AT FR46-47, STR 42L CRACKED. REMOVED, REPLACED AND FITTED IAW SRM 51-40-21, MINOR REPAIR TO SECONDARY STRUCTURE.SDR FDEA201209173338Skin · dentedIMPACT DAMAGE OBSERVED IN THE LOWER FUSELAGE SKIN POCKET FWD OF TAIL STEADY LOCATION FR 85 REPAIR C/OUT IAW SRM 53-10-12, FIG 225.SDR FDEA201209163334Skin · misrepairedSKIN AFT OF FR 80/82 MISREPAIRED. REMOVED REMAINING DAMAGE. REPAIRED IAW EA 6-5319-162972 CLASSIFIED AS MAJORSDR FDEA201209153329Skin · misrepairedSKIN BETWEEN FRAMES 30-31, STRINGERS 41- 42, MISREPAIRED. REPAIRED IAW SRM 53-10-12 FIG 225, SH1.SDR FDEA201209143325Stringer · misrepairedAFT CARGO BAY STRINGER 52L MISREPAIRED FR 59-61. REPAIRED IAW SRM 53-10-14, FIG 201. REPAIR CLASSIFED AS A MAJORSDR FDEA201209113289Frame · dentedDENT FOUND ON FRAME AT FR 20A RT AFT FACE AND BETWEEN STR 40 TO 41, LOWER SECTION, DENT AT FR 20A RT AFT FACE BETWEEN STR 40 TO STR 41 FOUND ACCEPTABLE IAW EA 6-5300-157946 AND RAS 70566040/003/2012. JPF ATTACHED, SHEET 1, STAGES 1-3.SDR FDEA201209103347Skin · misrepairedSKIN AT FR 77, STR 53-56, MISREPAIRED. REPAIRED IAW SRM 53-10-12, FIG 228, SH3.SDR FDEA201209063242Door · crackedSTABILIZER BAY DOOR 313AL CRACKED REPAIR IAW EA6-5241-157940 AND SRM 51-71-11, PARA 4D.SDR FDEA201209043222Floor Support · corrodedAFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR 64 LT FROM CENTER FOUND CORRODED. REPLACED IAW SRM 51-40-21.SDR FDEA201209043218Floor Support · corrodedAFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR64 SECOND FROM LT SIDE FOUND CORRODED AT ANCHOR NUT LOCATIONS. AFT HOLD SUPPORT BEAM AT FR63 AND FR64 SECOND FROM LT SIDE, REPLACED IAW SRM 51-40-21.SDR FDEA201208253163Floor Support · corrodedUPPER DECK FLOOR SUPPORT AT Y730 AND BETWEEN FRAMES 11 TO 14 FOUND CORRODED. REPLACED IAW SRM 51-40-01 AND DWG A53612214.SDR FDEA201208163032Roller Track · misrepairedCARGO BAY FLOOR ROLLER TRACK NR 2 LT SPLICE MISREPAIRED. REPLACED IAW SRM 51-40-21, SRM 51-72-10 AND AMM 25-52-21-04-01 CLASSIFIED AS MAJOR.SDR FDEA201208153015Bulkhead · corrodedREAR PRESSURE BULKHEAD FOUND CORRODED. ANGLE REPLACED ON EA 6-5300-157937 AND IAW DWG R53970640.SDR FDEA201208072875Skin · misrepairedSKIN FR 57.1-57.2 S35-37R MISREPAIRED. REPAIRED IAW SRM 53-10-12, PARA 9, FIG 228. REPAIR CLASSED AS MAJOR WITH CAT BSDR FDEA201106272456Rib · crackedLT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 47, 5 MM IN LENGTH WITHIN SPOT FACE. REPAIR CARRIED OUT IAW EA 6-5710-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED.SDR FDEA201106272455Rib · crackedLT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 54 12MM IN LENGTH WITHIN SPOT FACE REPAIR CARRIED OUT IAW EA 6-5710-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED BY 42500 FC.SDR FDEA201106272454Rib · crackedRT WING RIB 5 LOWER FLANGE CRACK EVIDENT AT HOLE LOCATION 47 10 MM IN LENGTH WITHIN SPOT FACE REPAIR CARRIED OUT IAW EA 6-57-10-150903. INTERIM REPAIR INSTALLED, RIB 5 TO BE REPLACED.SDR FDEA201003200949Panel · delaminatedRT WING T/E NR 2 DEFECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. REMOVED T/E NR 2 DEFLECTOR TO FOM. REMOVED DAMAGED FOIL. APPLIED NEW ALUMINUM FOIL. INSTALLED HARDWARE IAW EA 6-5720-136631, N/R N00389 FOR ORIGINAL EA N/R N01255SDR FDEA201003200948Deflector · delaminatedRT WING T/E COVE PANEL NR 4 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED PANEL TO FOM. REMOVED ALUMINUM FOIL AND HARDWARE. APPLIED NEW ALUMINUM FOIL AND INSTALLED HARDWARE IAW EA 6-5720-136631,"WINGS - WING FLAP HINGE DESDR FDEA201003200947Deflector · delaminatedRT WING T/E COVE PANEL NR 3 LOWER SURFACE METAL TAPE PEELING/MISSING REPAIRED IAW EA 6-5720-136631. REMOVED AND REINSTALLED HARDWARE IAW SRM 51-40-00. N/R N00389 FOR ORIGINAL EA. N/R N01255 FOR THE APPLICATION OF THE WITNESS MARK.SDR FDEA201003200946Panel · delaminatedRT WING T/E NR1 DEFLECTOR PANEL RUBBED TAPE LOOSE AND PEELING REPAIRED IAW EA 6-5720-136631. R & R WS HARDWARE IAW SRM 51-40-00. REMOVED AND INSTALLED OF RT WING T/E NR 1 DEFLECTOR PANEL ACCOPMPLISHED IAW AMM 27-54-41-4. NR N01255 FOR THE APPLICATION OF THE
Back to N718FD, cancelled Mar 2, 2024