N597FE
Service difficulty reports · 406
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 = 'N597FE' 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 = 'N597FE' 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 FDEA201910042436Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52SDR FDEA201910042435Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042434Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042433Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA201910032430Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TOE EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PARSDR FDEA201910032429Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032428Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, SDR FDEA201910032427Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CSDR FDEA201910032426Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM SDR FDEA201910032425Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3A, AND SDR FDEA201910032424Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T034988SDR FDEA201910032423Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA201910032422Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED SDR FDEA201910032421Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMSDR FDEA201910032420Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PARTSDR FDEA2019100322399Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750- T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57SDR FDEA2019100312389Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, OUTBOARD BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349884, PART 1, STEP 3A, AND INSTALLSDR FDEA2019100312388Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, INBOARD BORE SURFACE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PARSDR FDEA201910012387Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BRACKET, INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312386Hinge Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE BRACKET, OUTBOARD LUG BORE WAS FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PSDR FDEA2019100312385Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE FITTING OTBD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, SDR FDEA2019100312384Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR, INBOARD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEPSDR FDEA2019100312383Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750- T0349824, PART 1, STEP 3,SDR FDEA2019100312382Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57- 44-09 AND EA 1-5750-T0349824, PART 1, STSDR FDEA2019100312381Hinge Bracket · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0349824, PART 1, STEP 3B, AND SSDR FDEA201908302045Sensor · malfunctionedAFTER LANDING, RECEIVED A BRAKE DIFF TEMP LVL 1 MESSAGE. BRAKE TEMP ON NR 8 WAS ABOUT 200 COOLER THAN ALL OTHER TEMPS. REMOVED AND REPLACED THE NR 8 BRAKE TEMP SENSOR IAW MM 32-46-01-4. PERFORMED A TEST OF THE BRAKE TEMPERATURE MONITOR AND TIRE PRESSURE INSDR FDEA2018120653434Sensor · malfunctionedCRUZ FLT FL320.LEVEL THREE ALERT "AIR MANF #2 FAIL. QRH COMPLIED WITH,AIR SYSTEM REMAINED IN AUTO. AIR SYSTEM #2 27PSI #2 BLEED VALVE OPEN PER TECH PILOT CYCLED "PNEUM PRESS REG VLV ENG #2. PRV CYCLED #2 PNEUMATIC SYST PRESSURE LESS THAN 10PSI, LANDED NSDR FDEA2018082982271Truck · failedON TAXI OUT PVD FELT UNUSUAL VIBRATION WHILE TAXIING. WE SUSPECTED A FLAT TIRE ON THE RIGHT MAIN TRUCK. REMOVED AND REPLACED LT MLG TRUCK ASSEMBLY PER AMM 32-12-20-4.SDR FDEA201806081440Slat Track · crackedNR 12 RT SLAT TRACK (MOST O/B ON THE NR 5 SLAT) APPEARS TO BE CRACKED FROM L/E OF CUT OUT THROUGH 2 FASTENERS GOING AFT. INSTALLED REPAIR IN REF TO SRM 57-40-02-2R AND PRIMED AND PAINTED REPAIR IN REF TO SRM 51-21-01.SDR FDEA201803140686Sensor · failedBRAKE DIFF TEMP, LEVEL ONE ALERT CAME ON DURING CLIMB, TIRE NR 8 WHILE READING QRH IT BECAME A LEVEL TWO BRAKE OVERHEAT WITH A TEMP OF 640 DEGREES AT FL 370. DESCENDED TO FL240, SLOWED AND LOWERED THE GEAR IAW QRH. THE TEMP BEGAN TO DECREASE, BUT THE INSDR FDEA201802200442Warning System · activatedLVL 2 ANTI SKID L FAIL ON APPROACH, COMPLIED WITH QRH. ANTI-SKID CONTROL VALVE INOP. SYSTEM 1 BRAKE 6 DISABLED. ENSURE PENALIES ARE APPLIED. COMPLIED WITH "M" PROCEDURE. BRAKE INOP KIT INSTALLED ON NR 6 BRAKE.SDR FDEA201709192616Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 555 FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709182590Seat Track · damagedMAIN DECK CARGO SEAT TRACK CROWN AREA DAMAGED AT STA 5-5, RBL 8.5. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709172587Intercostal · crackedEMPENNAGE VERTICAL STAB, UPON REMOVAL FOR ACCESS RT CENTER REAR SPAR TO REAR SPAR INTERCOSTAL AT BS 2164 FOUND CRACKED. REPAIRED AS PER EA 1-5530-T0335514, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709172586Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB3954, REVISION K. INSTALLED THE DOUBLER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709172585Rib · crackedDURING BORESCOPE INSPECTION, FOUND THE RT WING NR 8 SLAT INNER RIB, XOS 1092 CRACKED. A NEW RIB WAS FABRICATED IAW DRAWING ARB1928 REVISION G. REMOVED AND REPLACED THE RIB IAW SRM 51-35-01-0G, AND EA 1-5750-T0335496, PART 1. THE REPAIR WAS CLASSIFIED AS MSDR FDEA201709152569Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON THE RIGHT WING FUEL TANK LOWER ACCESS PANEL 636AB, FOUND THREE FASTENER HOLES 10, 28 AND 34 CRACKED. REPAIRED IAW SRM 57-20-02-2R, FIGURE 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709152568Rib · crackedLEFT WING NR 3 SLAT INNER RIB AT XOS 435.446 FOUND CRACKED. REPAIRED THE RIB IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 7, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709152567Skin · dentedLEFT WING NR 3 SLAT FOUND DENTED AT XOS 435.446. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 11, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709142556Doubler · crackedRIGHT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 546, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709142555Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 24L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G. A NEW REPAIR ANGLE WAS FABRICATED IAW SRM 53- 20-07-2R, FIGURE 201, REPAIR 1, AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 2SDR FDEA201709142554Frame · chafedMAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 19L. REMOVED THE REPAIR IAW SRM 51-33-01-0G. A NEW OUTER REPAIR ANGLE, FABRICATED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE NEW REPAIR ANGLE WAS INSTALLED IAW SRM 53-20-07SDR FDEA201709142553Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 907 FOUND CRACKED. REPAIRED THE LEADING EDGE LOWER AREA IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709142552Fitting · crackedDURING HFEC INSPECTION AT RT FWD FLANGE LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER, Y=2164 A CRACK WAS FOUND APPROXIMATELY 0.25 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335558, PART 1. THE REPAIR WAS CLASSISDR FDEA201709132532Frame · dentedMAIN DECK CARGO FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2.SDR FDEA201709132531Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 27.5. REPLACED THE SEAT TRACK FROM BS 625 TO 665, LBL 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132530Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 47. REPLACED THE SEAT TRACK FROM BS 625 TO 665 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132529Cargo Track · crackedMAIN DECK CARGO TRACK FOUND CRACKED AT BS 755, LBL 49. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132528Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM BS 665 TO 705 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709132527Seat Track · crackedMAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 8.5. REPLACED THE SEAT TRACK FROM BS 625 TO 705, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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