N596FE
Service difficulty reports · 417
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 = 'N596FE' 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 = 'N596FE' 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 FDEA201411213841Cargo Track · corrodedMAIN DECK CARGO TRACK BETWEEN BS 1643 - 1738 X -8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201408142170Skin · crackedRIGHT WING HAS 2 POSSIBLE CRACKS AT TOP EDGE OF ANTI-ICE DUCT CUT OUT LOCATED 4 FT OTBD OF NR 3 ENG PYLON. REPAIRED IAW MD 11 SRM 57-40-01 FIG 201SDR FDEA201408142169Skin · crackedLEFT WING HAS CRACK AT LE CUT OUT ON LOWER SIDE OF WING AT 5TH SLAT TRACK FROM OTBD END. REPAIRED IAW SRM 57-40-02 REPAIR 7.SDR FDEA201311132753Warning Light · false indicationON FIRST LANDING ATTEMPT, LANDING GEAR SHOWED ALL UNSAFE, CONFIGUATION DISPLAYED ALSO, CYCLED GEAR AND ALL SHOWED SAFE. TOWER STATED GEAR WAS DOWN ON FIRST ATTEMPT. PERFORMED TEST OF PROXIMITY SWITCH ELECTRONICS UNIT, IAW MM 31-71-01-2. ALL UNITS FUNCTIOSDR FDEA201306191346Uplock · inoperativeAFTER TAKEOFF, LEFT MAIN GEAR DID NOT RETRACT. RED LIGHT ON GEAR HANDLE SPOT AND RED LIGHT ON CONFIG PANEL. SPEED MAX 220. PERFORMED CHECKLIST. CHECKLIST WORKED. NORMAL FLT AND LANDING. REPLACED GEAR UNLOCK CYLINDER. OPS CHECKS NORMAL THROUGH LEAK CHECK SDR FDEA201212264377Skin · crackedRT WING ACCESS PANEL CUTOUT FOUND CRACKED DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS 683.4 AND 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201212264376Skin · crackedLT WING ACCESS PANEL CUTOUT SKIN FOUND CRACKED DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS 683.4 AND 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201212264375Doubler · crackedLEFT WING FIXED L/E COMPARTMENT XOS 745 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02, FIG 203, REPAIR 15, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201212244371Beam · crackedL3 DOOR LOWER BEAM FORWARD FITTING FOUND CRACKED. R & R IAW SRM 51-31-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR FDEA201212244370Access Panel · corrodedLEFT WING T/E LOWER ACCESS PANEL NR 541JB CUTOUT FORWARD EDGE LOWER CAP LOWER SURFACE FOUND CORRODED. R & R WITH NEW CAP AT LT WING T/E LOWER ACCESS PANEL 541JB CUTOUT IAW SRM 51-33-01, REV 51 AND SRM 51-35-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-SDR FDEA201212244369Access Panel · crackedLEFT WING T/E LOWER ACCESS PANEL 3541FB CUTOUT FORWARD EDGE OTBD CORNER SILL FOUND CRACKED. R & R IAW SRM 51-34-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201107072609Power Supply · inoperativePRE-FLIGHT FOUND EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHT POWER SUPPLY ASSY IAW AMM 33-51-01-4 AND TESTED OK IAW AMM 33-51-01-5, ACFT OK FOR SERVICE.SDR FDEA201103231149Skin · gouged2 SCRATCHES ON LT FUSELAGE. FIRST SCRATCH IS AT STA 401.92 WATER LINE 27 SCRATCH IS APPROX .875 LONG AND APPROX. .007 DEPTH SECOND SCRATCH IS AT STA. 40 6.55 WATER LINE 27 SCRATCH IS APPROX .9375 LONG AND APPROX .035 DEPTH. BLENDED SCRATCH AT FS 401.92 WITSDR FDEA201102100528Skin · misrepairedLT INBD T/E INBD LOWER SEGMENT FOUND EXISTING REPAIR ON UPPER SURFACE, OTBD LOWER AREA. FOUND NOT IN ACCORDANCE WITH APPROVED DATA. L/H INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT CARRIED OUT REPAIR AS PER EA 1-5750-143853. REPAIR CLASSIFIED AS MAJORSDR FDEA201102100520Skin · misrepairedEXISTING REPAIR FOUND AT RT LOWER FUSELAGE SKIN AT STA 1811, LONGERON 38. FOUND NOT IN ACCORDANCE WITH SRM 53-00-01 REVISION 45. FUSELAGE - EXTERNAL SKIN CARRIED OUT REPAIR AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 45. EO 1-5100-7-5001 A5 PART 1. SDR FDEA201102070487Panel · crackedEMPENNAGE - NR 2 INTAKE DUCT PANEL NR362PL INTERIOR AREA, ELECTRICAL WIRING CUT-OUT FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIGURE 201 REVISION 45. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101290409Skin · damagedFOUND SKIN DAMAGED. CARGO DOOR AFT CUTOUT SKIN AT STATION 1781 LONGERON 39 CARRIED OUT REPAIR AS PER SRM 53-00-15 REPAIR 8 FIGURE 201 REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101280395Skin · damagedFWD CARGO DOOR CUTOUT AFT JAMB FUSELAGE SKIN FOUND WITH SCRATCHES AT LONGERON 40 TO LONGERON 41. CARRIED OUT REPAIR AS PER SRM 53-00-15 REPAIR 8 FIGURE 201 REVISION 45. INITIAL INSPECTION AT 12,600 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 6,300 FLIGHT SDR FDEA201101280397Skin · cracked13 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PERSDR FDEA201101280396Skin · cracked15 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS= 683.4 AND XORS= 713.6. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-SDR FDEA201101260382Longeron Splice · crackedONE CRACK FOUND DURING HIGH FREQUENCY EDDY CURRENT INSP AT STA 6-100, LONGERON 1L, STRINGER SPLICE CRACK LENGTH APPROX 1". CRACKED LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 45. NEW LONGERON SPLICE FABRICATED AS PER DWG A6A7112-507 RSDR FDEA201101260381Vane · delaminatedRIGHT WING OTBD FLAP INBD VANE, UPPER AND LOWER SURFACE FOUND DELAMINATED BETWEEN NR 1 AND NR 2 VANE TRACK. REMOVED AND REPALCED AS PER AMM 27-50-33-4 REVISION 69.0 FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-32-5 REVISION 69.0. FOUND SATISSDR FDEA201101260380Frame · misrepairedREPAIR, ON CABIN LT AT STATION 535, L22. FOUND REPAIR NOT IN ACCORDANCE WITH APPROVED DATA. CARRIED OUT REPAIR PER DRAWING SG 10530002 REVISION 0. EO 1-5100-7-5001 A5 PART1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.SDR FDEA201101260379Frame · misrepairedREPAIR ON CABIN LT AT STATION 535, L24. FOUND NOT IN ACCORDANCE WITH APPROVED DATA. CARRIED OUT REPAIR AS PER DRAWING SG10530002 REVISION 0. EO 1-5100-7-5001 A5 PART1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101260378Skin · misrepairedLT INBD T/E FLAP OTBD LOWER SEGMENT FOUND A ROUND PATCH REPAIR AT LOWER SURFACE. CARRIED OUT REPAIR AS PER EA 1-5750-143852. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101260377Skin · damagedCTR CARGO DOOR CUTOUT FWD JAMB FUSELAGE SKIN FOUND WITH SCRATCHES AT L-39 TO L-40. REPAIR CARRIED OUT AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 45 AND REPAIR DOUBLER AND FILLER INSTALLED AS PER SRM 51-33-01 REVISION 45. REPAIR CLASSIFIED AS MAJOR PER SDR FDEA201101260363Skin · misrepairedLT WING FIXED L/E FOUND WITH EXISTING REPAIR AT FORWARD OF FUEL PANEL AREA. LT WING FIXED L/E REPAIR AT FWD OF REFUEL PANEL AREA EVALUATED AND FOUND NOT IAW APPROVED DATA. LT WING FIXED L/E FWD OF REFUEL PANEL CARRIED OUT REPAIR IAW EA 1-5730-143848 & EO 1-5SDR FDEA201101260365Skin · misrepairedCARGO - EXISTING REPAIR FOUND CTR CARGO DOOR LOWER MID AFT AT STA 1761. CARGO - EXISTING REPAIR FOUND CTR CARGO DOOR LOWER MID AFT AT STA 1761. FOUND NOT IAW SRM REPAIR. CARGO DOOR LOWER MID AFT AT STA 1761 CARRIED OUT REPAIR IAW EA 1- 5230-143522: DOORS -SDR FDEA201101260362Skin · misrepairedLT WING NR 4 SLAT INTERIOR SKIN FOUND WITH EXISTING REPAIR. LT WING NR 4 SLAT INTERIOR SKIN EXISTING REPAIR FOUND NOT ACCOMPLISHED IAW SRM 57-40-01, FIG 201, REV 45. LT WING NR4 SLAT CARRIED OUT REPAIR IAW EA1-5750-143849: WINGS - FLIGHT SURFACES - LT NR 4 SDR FDEA201101260369Seat Track · corrodedLOWER AFT WASTE TANK COMPARTMENT - STA 2007, X=107.25 CABIN SEAT TRACK FOUND CORRODED. REPAIRED BY SEGMENT SEAT TRACK REPLACEMENT FROM STA 1831 TO STA 2007 X= 107.25 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, RSDR FDEA201101260368Seat Track · corrodedLOWER AFT WASTE TANK COMPARTMENT - STA 2007, X= 107.25 CABIN SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201101260367Seat Track · crackedCABIN - SEAT TRACK AT STATION 5-32, X= 75.25 FOUND CRACK. REPAIRED IAW SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-63 X= -75.25 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201101260366Seat Track · corrodedSEAT TRACK AT STATION 1289, X= 8.50 FOUND CORROSION. REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 45 FROM STA 1269 TO STA 1311, X=8.50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201011014203Warning Light · illuminatedON DEPARTURE RECEIVED LEVEL 1 "ANTI ICE SENSOR FAIL" REMAINED ON UNTIL SHUTDOWN IN CHOCKS.SDR FDEA201001270279Selector Valve · malfunctionedON FINAL EXTENDED LANDING GEAR HANDLE, GOT 4 RED LIGHTS NO OUTSIDE NOISES ASSOCIATED WITH NORMAL EXTENSION, RETRACTED GEAR HANDLE UNTIL ALL LIGHTS EXTINGUISHED. ON SECOND ATTEMPT HAD NORMAL GEAR EXTENSION. R & R LANDING GEAR SELECTOR VALVE IAW REF TO MM 32-SDR FDEA200909083268Skin · damagedRT WING NR 2 SPOILER PANEL WAS FOUND BROKEN. REMOVED AND REPLACED THE RT WING NR 2 SPOILER ASSY IAW AMM 27-60-30-4 AND DID A TEST OF THE SPOLIER LATERAL CONTROL IAW AMM 27-61-00-730-801, CKD OK FOR SERVICE.SDR FDEA200904091257Support Fitting · corrodedCORROSION FOUND ON INBD FLAP INBD TRACK NR 4 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091256Support Fitting · corrodedCORROSION FOUND ON INBD FLAP INBD TRACK NR 4 SUPPORT FITTING LOWER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091255Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 4 SUPPORT FITTING UPPER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091254Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 4 SUPPORT FITTING UPP FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091253Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING LOWER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091252Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091251Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING UPP AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091250Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 3 SUPPORT FITTING UPP FWD HOLE. CORROSION REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091249Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 2 SUPPORT FITTING LOWER FWD HOLE. SUPPORT FITTING LOWER REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091248Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 2 SUPPORT FITTING UPP AFT HOLE. CORROSION AT RIGHT WING INBOARD FLAP INBOARD TRACK NR 2 SUPPORT FITTING UPPER AFT HOLE REPAIRED AS PER EA 1-5750-12781. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091247Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 1 SUPPORT FITTING LOWER AFT HOLE. RT WING INBOARD FLAP INBOARD TRACK NR 1 SUPPORT FITTING LOWER AFT HOLE REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091246Support Fitting · corrodedFOUND CORROSION INBD FLAP INBD TRACK NR 1 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPIAR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091245Fitting · corrodedCORROSION INBD FLAP INBD TRACK NR 1 SUPPORT FITTING UPPER FWD HOLE. RT WING INBOARD FLAP TRACK NR 1 SUPPORT FITTING UPPER FORWARD HOLE REPAIRED AS PER EA 1-5750-127817, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904021166Longeron · crackedCRACKED LONGERON AT 38R STA 5-123 IN CENTER CARGO COMPARTMENT. CARRIED OUT SECTIONAL LONGERON REPLACEMENT FROM STA 5-103 TO STA 5-123 AS PER SRM 53-10-00 FIGURE 2, VOLUME I, REVISION 40. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.
Back to N596FE