N721FD
Service difficulty reports · 231
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 = 'N721FD' 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.
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 = 'N721FD' AND registry_match = 'registration' 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 FDEA201308041763Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "G" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "G" EXISTING DIA= 0.529 IN. FASTENER "G" HOLE REAMED TO REMOVE SCSDR FDEA201308041765Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "Q" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "Q" EXISTING DIA= 0.653 IN. FASTENER "Q" HOLE REAMED TO REMOVESDR FDEA201308041764Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "C" IN CTR WING BOX REAR SPAR, FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "C" EXISTING DIA= 0.529 IN. FASTENER "C" HOLE REAMED TO REMOVE SDR FDEA201308041762Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "F" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "F" EXISTING DIA= 0.529 IN. FASTENER 'F' HOLE REAMED TO REMOVESDR FDEA201308041761Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "E" IN CTR WING BOX, REAR SPAR, FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "E" EXISTING DIA= 0.529 IN. FASTENER "E" HOLE REAMED TO REMOVESDR FDEA201308041760Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT3, WRI: 57101122, POST REMOVAL OF FASTENER "D" IN CTR WING BOX REAR SPAR, FR.47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. "D" HOLE EXISTING DIA= 0.591 IN. FASTENER "D" HOLE REAMED TO REMOVSDR FDEA201308041759Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "A" IN CTR WING BOX REAR SPAR, FR 47, LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. A-HOLE EXISTING DIA= 0.591 IN. FASTENER "A" HOLE REAMED TO REMOVE SDR FDEA201308041758Frame · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT3, WRI: 57101122, POST REMOVAL OF FASTENER "B" IN CTR WING BOX REAR SPAR FR 47 LT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "B" EXISTING DIA= 0.591 IN. REAMED TO REMOVE SCORE AND HOLE NDTSDR FDEA201308041774Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "S" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGED FOUND IN WALL OF HOLE. HOLE "S" EXISTING DIA= 0.653 IN. FASTENER "S" HOLE REAMED TO REMOVESDR FDEA201308041773Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "Q" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGED. FOUND IN WALL OF HOLE. HOLE "Q" EXISTING DIA= 0.653 IN. FASTENER "Q" HOLE REAMED TO REMSDR FDEA201308041772Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "G" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "G" EXISTING DIA= 0.529 IN. FASTENER "G" HOLE REAMED TO REMOVE SDR FDEA201308041771Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305 D3 PT4, WRI: 57101121, POST REMOVAL OF FASTENER "F" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE, HOLE "F" EXISTING DIA= 0.529 IN. HOLE "F" SCORES REMOVED BY REAMING, SDR FDEA201308041770Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "E" IN CTR WING BOX REAR SPAR FR 47, RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "E" EXISTING DIA= 0.529 IN. FASTENER "E" HOLE REAMED TO REMOVSDR FDEA201308041769Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "D" IN CTR WING BOX REAR SPAR FR 47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "D" EXISTING DIA= 0.639 IN. FASTENER "D" HOLE REAMED TO REMOVESDR FDEA201308041768Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "C" IN CTR WING BOX REAR SPAR FR.47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "C" EXISTING DIA= 0.529 IN. FASTENER "C" HOLE REAMED TO REMOVSDR FDEA201308041767Skin · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "B" IN CTR WING BOX REAR SPAR FR 47 RY JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE. HOLE "B" EXISTING DIA= 0.591". FASTENER HOLE B REAMED TO REMOVE SCSDR FDEA201308041766Panel · damagedDURING ACCOMPLISHMENT OF EO: 6-5710-7-3305, D3, PT4, WRI: 57101121, POST REMOVAL OF FASTENER "A" IN CTR WING BOX REAR SPAR FR.47 RT JUNCTION WITH FUSELAGE SCORE DAMAGE FOUND IN WALL OF HOLE AND SCRATCH IN UPPER SURFACE AROUND HOLE. HOLE "A" EXISTING DIA= 0.59SDR FDEA201307171579Elevator · unknownRT ELEVATOR HAS SUSPECT WATER INGRESS. CARRY OUT REQUIREMENTS OF EA 6-5521-197477 REQUIREMENTS OF EA 6-5521-167477 CARRIED OUT.SDR FDEA201307051479Fitting · crackedDURING REPLACMENT OF RT MLG MAIN DOOR FITTING. JOINT FITTING BEHIND RT MLG KEEL BEAM PANEL AT FR 50 RT, FOUND TO HAVE IMPACT DAMAGE CAUSING DENT AND CRACKING IAW SRM 53-15-15-4-150. REPAIRED IAW EA 6-5300-167469.SDR FDEA201307041477Skin · damagedLEFT WING TOP SKIN FWD SPAR AREA APPROX RIB 9-10 HAS INCORRECTLY FITTED FASTENER AND SUSPECT DAMAGE AROUND THE HOLE. REPAIRED IAW EA 6-5700-167463, CAT A REPAIR CLASSED AS MAJOR.SDR FDEA201307021468Skin · damagedBULK CARGO BAY DOOR EXTERNAL SKIN AROUND OPERATING HANDLE HAS VARIOUS DENTS AND DAMAGE. REPAIRED IAW EA6-5230-197462.SDR FDEA201307021469Skin · damagedFWD CARGO BAY RT SIDE AT THE DOOR CUT OUT, DAMAGE ON THE L/E OF THE FRAME 25A BETWEEN STRINGERS 33 AND 35. REPAIRED IAW EA 6-5300-167464. CAT "A" REPAIR.SDR FDEA201306251387Skin · dentedDENT NOTED TO BOTTOM SKIN OF RT AILERON APROX CENTER OF AILERON. FOUNT OUT OF LIMITS AREA REPAIRED IAW SRM 57-61-11 PB201 FIG 206 PARA 4.F CAT A REPAIR CLASSIFIED AS A MAJOR REPAIR. AREA REPROTECTED IAW SRM 51-75-10.SDR FDEA201306251393Skin · dentedLT WING DENT IN AILERON T/E AREA BOTTOM SKIN 1.5" IN/BD OF RIB 1 AND 4.0" FWD OF T/E AFT EDGE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-61-11 PARA 4G & 51-77-12 PARA 4C.SDR FDEA201306251391Skin · dentedLEFT WING DENT IN AILERON T/E AREA BOTTOM SKIN 2.5" INBD OF RIB 1 AND 10.0" FWD OF T/E AFT EDGE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-61-11 PARA 4G & 51-77-12, PARA 4C.SDR FDEA201306231377Skin · damagedDAMAGE FOUND TO BACK SIDE OF NR 2 SLAT, 12 INCHES FROM INBD END OF SLAT ON RT WING. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-43-11 PB201 PARA 4.B, FIG 202.SDR FDEA201306231376Fitting · corrodedCORROSION FOUND ON BORE OF RT MLG RIB 5 FITTING FWD LUG. CORROSION REMOVED, REPLACEMENT BUSHES FABRICATED AND INSTALLED IAW REPAIR DWG R57240425 ISSUE B AND RT MLG INSTALLED IAW INSTRUCTION OF EA 6-5710-167452 AND RDAS 70579091/003/2013 ISSUE A. MAJOR REPAISDR FDEA201306231375Rib · corrodedCORROSION FOUND ON BORE AND AFT FACE OF LT MLG RIB 5, FITTING FWD LUG. RIB REPLACED IAW EA 6-5710-167482.SDR FDEA201306231374Uplock · miswiredLT MLG DOOR UPLOCK FREE FALL INPUT ROD FOUND TO BE WIRED TO UPLOCK IN CLOSED POSITION THROUGH RIGGING PIN HOLE. CARRIED OUT UPLOCK FREEFALL INPUT ROD REMOVED CABLE CONNECTION AND RIG CHECK AND FOUND TO BE CORRECT. MANUAL GROUND DOOR OPENING AND CLOSING TEST CSDR FDEA201306211364Fuel Tank · damagedDURING ACCOMPLISHMENT OF O: 6-5310-7-5013 C 1 PT2, POST REMOVAL OF FASTENER THROUGH CENTER TANK UPPER SKIN AT FR 47 BORE OF HOLE FOUND WITH SEVERAL SCRATCHES IN UPPER SPLICE PLATE. REF FIG 6, SHEET 2 OF 3 ITEM 6. REAMED & FASTENER INSTALLED IAW EA 6-5710-167SDR FDEA201306201356Angle · crackedRIGHT WING KREUGER FLAP CAVITY AT FIXED L/E HAS A SUSPECTED CRACK AT RIB, 8 AT OTBD OF KREUGER ACTUATOR. REPAIRED IAW SRM 51-72-10 REF DWG A57241993.SDR FDEA201306201358Web · crackedNDT INSPECTION OF CENTER WING BOX, CENTER SPAR AT CUTOUT DOUBLER RUNOUT L/H AT FR. 44, CRACK FOUND AT R/H LOWER HOLE 4 , INDICATION 25 PERCENT FSH 10MM FROM AFT FACE AT APPROXIMATE VERTICAL POSITION. REPAIRED OUT IAW EA 6-5710-167465.SDR FDEA201306201357Spar · crackedNDT INSPECTION OF CENTER WING BOX, CENTER SPAR AT CUTOUT DOUBLER RUNOUT RT AT FR 44, CRACK FOUND AT RT UPPER HOLE 7 I, INDICATION 25 PERCENT FSH 10MM FROM AFT FACE AT APPROXIMATE VERTICAL POSITION. REPAIRED IAW EA 6-5710-167466.SDR FDEA201306201355Frame · chafedRT GEAR DOOR ACTUATOR UPPER FITTING AFT FRAME SCOURED & CHAFED ON INNER FWD FACE. REPLACED IAW SRM 51-72-10, REF DWG A53810931 & A53810771.SDR FDEA201306121262Rib · crackedLT WING KREUGER FLAP CUTOUT CAVITY AT FIXED L/E SUPPORT, RIB CRACKED APPROX 8" OTBD OF KREUGER ACTUATOR. REPLACED IAW SRM 51-72-10 AND DWG A57241993.SDR FDEA201304090757Hydraulic System · malfunctionedAFTER DEPARTING, GREEN HYD QTY BEGAN TO SLOWLY DECREASE. ON RETURN, QTY DECREASED TO RED DOT ON QTY GAUGE. ECAM DISPLAY CONFIRMED LOW QTY . FOLLOWED ECAM AND QRH AND PERFORMED GRAVITY EXTENSION OF LANDING GEAR. AFTER GEAR WAS EXTENDED, HYD QTY ROSE BACKSDR FDEA201304090752Hose · leakingAFTER TAKEOFF LOST ALL GREEN HYD FLUID. GAUGES INDICATED ZERO QTY ON OVERHEAD PANEL AND ECAM. COMPLETED QRH AIR TURN BACK, TROUBLESHOOTING FOUND THE RT AILERON ACTUATOR PRESSURE HOSE RUPTURED. R & R THE HOSE . PERFORMED LEAK CHECK, NO LEAKS FOUND, SERVICESDR FDEA201104191586Pitot Head · malfunctionedALTITUDE ALERT ON CONTINUOSLY IN LEVEL FLT. ALTITUDE NEVER OFF BY 50FT AND LIGHT & HORN ACTIVATED & HAD TO BE MANUALLY CORRECTED TO ALTITUDE WITH EITHER AUTOPILOT ON. USED NR 2 REMAINDER OF FLT DUE TO LOSS OF CAPT FD/ADC. REPLACED CAPT'S, F/O'S & STANDBY PISDR FDEA201102110539Slat Track · chafedLT WING NR 8 SLAT TRACK, ON THE TRACK FWD LOWER OTBD RADIUS, THERE IS CHAFING MARKED REPAIRED IAW EA 6-5740-146827, WINGS,ATTACH FITTINGS: LT WING NR 8 SLAT TRACK CHAFING, PERMANANT REPAIRS.SDR FDEA201102100529Web · crackedFWD CARGO DOOR WEB CRACKED .5" INCH AT DOOR ACTUATOR MOUNT. FABRICATED DRILLED AND INSTALLED REPAIR DOUBLER IAW EA 6-5230-145552. ROUTED OUT CRACK. NDT AREA OF REMOVAL, NO CRACKS FOUND, REPROTECTED AREA IAW SRM 51-75-10 FWD CARGO DOOR INNER WEB AT ACTUATORSDR FDEA201102100527Rib · corrodedCORROSION FOUND ON RT MLG RIB 5, FWD LUG. COMPLIED WITH EA 6-5710-145558.SDR FDEA201005131530Jackscrew · bindingSLAT 1 & SLAT 2 FAULT ON ECAM. FOLLOWED QRH SLAT WOULD NOT MOVE. PLEASE WORK IN CONJUNCTION WITH TSI 27-80/7759. R & R NR 3 LT SLAT SCREWJACK IAW MM 27-84-22-4. ACCOMPLISHED OPS TEST OF L/E SLATS IAW MM 27-84-00-5 WITH NO FAULTS NOTED.SDR FDEA201005131529Jackscrew · damagedSLAT 1 & SLAT 2 FAULT ON ECAM. FOLLOWED QRH SLAT WOULD NOT MOVE. PLEASE WORK IN CONJUNCTION WITH TSI 27-80/7759. R & R NR 3 LT SLAT SCREWJACK.SDR FDEA201003040641Slat System · malfunctionedDURING SLAT EXTENSION, SLATS STUCK AT 0 DEGREES. BOTH OVERHEAD SLAT FAULT LIGHTS CAME ON. CYCLED HANDLE AND SLATS STAYED STUCK. DURING TAXI IN CYCLED HANDLE AND SLATS WORKED NORMALLY. BITE TEST OF SFCC 1 SHOWED "MAIN CONT VLV" ON ARRIVAL, SLATS WORKING NORSDR FDEA200902100499Shutoff Valve · malfunctionedGOT REVERSER UNLOCK ON NR 1 ENG AT 60 KTS. ATTEMPTED SECOND T/O SAME RESULTS. R&R PRSOV PER AMM 78-32-11-5SDR FDEA200811014671Smoke Detector · failedAT 8000 AFTER TAKEOFF FROM EGSS GOT SMOKE/FUME ALERT FROM MAIN DECK SMOKE DETECTOR MID 2A. STAYED ON FOR ABOUT 8 MINS, WENT OFF JUST BEFORE LANDING. MID 1B, MID 2B, AND AFT A WERE ALL READY DEFERRED. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-B CATEGORYSDR 08FDEA04671Smoke Detector · malfunctionedAT 8000 AFTER TAKEOFF FROM EGSS GOT SMOKE/FUME ALERT FROM MAIN DECK SMOKE DETECTOR MID 2A. STAYED ON FOR ABOUT 8 MINS, WENT OFF JUST BEFORE LANDING. REACTIVATED ALL MDC LOOPS ALREADY DEFERRED (AFT A, MID 1B AND MID 2B). NO MORE FAULT DISPLAYED ON MDC SMOKESDR 08FDEA02978Fitting · corrodedRT WING, INTERIOR FITTING AT FRONT CARRIAGE NR 3 FLAP TRACK WITH CORROSION, DETECTED ON ACCOMPLISHMENT OF NR 0599. A NEW FITTING WAS FABRICATED SO AS TO REPLACE THE EXISTING ONE.SDR 08FDEA02979Fitting · corrodedLT WING NR 3 TRACK FRONT CARRIAGE INTERIOR FITTING WITH CORROSION, DETECTED WHILE PERFORMING N0800. THE NR 3 TRACK FRONT CARRIAGE WAS REPLACED BY ONE FABRICATED AS PER FEDEX EA 6-5740-120510.SDR 08FDEA02980Frame · gougedFUSELAGE, FR 47 HOLE K REF TO EO 6-5310-7-5017 PT4, FOUND DAMAGED. HOLE K REPAIRED AS PER FEDEX EA 6-5310-121645.
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