N574FE
Service difficulty reports · 611
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 = 'N574FE' 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 = 'N574FE' 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 FDEA201401180135Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE OTBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3.SDR FDEA201401180134Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE INBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. . BUSHING & WASHER FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2, 2B, 3, 4 & 5.SDR FDEA201401180133Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE OTBD ACTUATOR HOLE. WORN BUSHING ON OTBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED IAW EA 1-5750-87638C PART 2 TITLE, WINGS - TE & TE DEVICESSDR FDEA201401180132Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE INBD ACTUATOR HOLE. WORN BUSHING ON INBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED & INSTALLED IAW 1-5750-87638C PART 2 TITLE, WINGS - TE & TSDR FDEA201401100081Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401100080Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-08 REV 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.SDR FDEA201401060041Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2,2B, 3, 4 & 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201401060040Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2, 3, & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISDR FDEA201401060039Hinge Fitting · damagedRIGHT WING OTBD FLAP OTBD FWD HINGE PIVOT HOLE DIAMETER FOUND OUT OF LIMITS AFTER REPAIR BUSHING REMOVAL. HINGE PIVOT BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060031Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060030Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2,2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060027Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING BARREL NUT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C P2 STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060026Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060025Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C PART 2 STEP 2,3 &4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060043Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. BUSHING AND WASHER FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2,2B1,SDR FDEA201401060037Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.SDR FDEA201401060036Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.SDR FDEA201401060035Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIRED IAW CMM 57-44-08 REV 78 AND EA 1-5750-87638C PART 2 FIGURE 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.SDR FDEA201401060029Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060028Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT & AFT SPOT FACE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV. 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION SDR FDEA201401060046Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE OTBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2, 3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060045Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060044Hinge Fitting · corrodedLEFT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87633A P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401060042Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2. REPAIR CLASSIFIEDSDR FDEA201401060038Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE PIVOT FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2, STEP 2 AND STEP 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201401060047Floor Panel · damagedL1 DOOR AREA, FOUND FLOOR PANEL 227AF SPONGY. FLOOR PANEL REMOVED IAW AMM 53-21-04 REVISION 78. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION K AND INSTALLED IAW AMM 53-21-04 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401030011Skin · crackedCRACK INDICATION FOUND APPROXIMATELY 0.3 INCHES IN LENGTH ON FUSELAGE SKIN DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT BS 695 LONGERON 50L. REPAIRED IAW SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 53 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119SDR FDEA201401030013Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT SPOT FACES FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.SDR FDEA201401030012Longeron Splice · crackedCENTER CARGO BAY BETWEEN BS 1661 & 1681, LONGERON SPLICE 29 RT CRACKED. NEW SPLICE FABRICATED IAW DRAWING AFA7830. DAMAGED LONGERON SPLICE REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401030014Skin · crackedRIGHT WING FIXED LE LOWER, FOUND CRACKED AT SLAT TRACK NR 11, CUTOUT AREA SKIN. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.SDR FDEA201401020002Support Fitting · crackedMAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING DAMAGED. NR 1 HOLE REAMED TO 0.562 INCHES. HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED FOUND CRACK INDICATION STILL EXIST, APPROXIMATELY 0.040 INCH. SUPPORT FITTING REMOVED AND REPLACED IAW SSDR FDEA201312313073Wedge · delaminatedLEFT WING OTBD FLAP, INBD TE WEDGE FOUND DELAMINATED AT XOFH 458.74 TO XOFH 465.24. REPAIRED IAW EA 1-5750-T0305303 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119SDR FDEA201310182555Seal · unsecurePASSING FL 220, HEARD A LOUD BANG AND AIR OUT FLOW IN AVIONICS BAY. CABIN PRESSURE CONTINUED A SLOW CLIMB. AIR TURN BACK. ACFT UNABLE TO HOLD PRESSURE. LANDED WITHOUT INCIDENT. FOUND AVIONICS DOOR SEAL HANGING OUT. SEATED DOOR SEAL AND OPS CHECKED DOORSDR FDEA201307281674Power Supply · failedDURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS TEST WILL NOT PASS. REPLACED EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-01-4 , TESTED NORMAL.SDR FDEA201307251663Warning Light · false activationDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.SDR FDEA201307241672Power Supply · inoperativeDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.SDR FDEA201304020701Duct · tornAFTER TAKE OFF "ICE DET SINGLE" LEVEL 1 ALERT FOLLOWED BY "AIR SYS 1 OFF" LVL 1 AND LVL 3 MANIFOLD FAIL FOR SYS 1. NO ANTI ICE WING OR ENG WAS ON. LEVEL 3 MANIFOLD FAIL WENT OUT AS AS THROTTLE WAS RETARDED. REPLACED DUCT.SDR FDEA201209273478Static Wick · missingDURING CLIMBOUT, WE WERE INSTRUCTED TO RETURN TO DEPARTURE DUE TO POSSIBLE DAMAGE DURING PUSHBACK. LEFT UPPER WINGLET MISSING STATIC WICKS. REPAIRED L/H UPPER WINGLET CAP PER PART 2 OF EA 1-5720-162680. INSTALLED UPPER WINGLET CAP IAW MM 57-31-01-4 A/C OSDR FDEA201202030443Angle · corrodedAFT CARGO DOOR AFT CUTOUT ANGLE FOUND WITH SURFACE CORROSIONS. ANGLE REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. INITIAL INSPECTION AT 18300 FC AND REPEAT INSPECTION AT 1250 FC PER ALI 53-10-06 REVISION 15. REPAIR CLASSIFIED AS MAJOR ASSDR FDEA201202030444Skin · corrodedUPON REMOVAL OF R3 DOOR SILL PLATE FOR REPAIR ACCESS FORWARD LOWER DOOR CUTOUT INTERIOR SKIN FOUND CORRODED.SDR FDEA201201300379Skin · corrodedAFTER REMOVAL OF APU EXHAUST DOOR RT FUSELAGE SKIN AT STA 2120 BENEATH APU EXHAUST DOOR FOUND CORROSION.SDR FDEA201201270352Door Frame · misrepairedFORWARD CARGO DOOR FRAME, BS 897 BETWEEN LONGERON 38 AND LONGERON 40R MISREPAIRED. CARRIED OUT REPAIR AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.SDR FDEA201201270350Floor Support · corrodedLEFT STA 421, X= 28 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT FABRICATED AS PER DRAWING ABA8303 REVISION A. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.SDR FDEA201201270349Seat Track · corrodedREMOVAL OF FLOOR PANEL LT STATION 5-103, X= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.SDR FDEA201201270348Hinge · crackedRT MLG DOOR CENTER HINGE CRACKED. HINGE REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. R/H MAIN GEARWELL DOOR REMOVED AND REINSTALLED AS PER AMM 32-14-20-4 REVION 70.1. OPERATION CHECK CARRIED OUT SATISFACTOTY AS PER AMM 32- 14-20-220-801 REVISIONSDR FDEA201201270353Skin · damagedAFT LOWER RUDDER SKIN FORWARD LOWER CORNER FOUND DAMAGED. REPAIRED IAW SRM 55-40-01, FIGURE 201, REV 48. EA 1-5540-156837. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201201260341Skin · misrepairedLT WING FIX L/E LOWER SKIN AT XW 344 MISREPAIRED. REPAIRED IAW DWG ARB1230, REV CEO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201201260343Skin Splice · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT TRANSVERSE SKIN SPLICE, STATION 5-0, LONGERON 4LT ON THE CENTER ROW FASTENER NR 4 TOWARD NR 5 FASTENER APPROX .5" LONG COUNT FROM FORWARD. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. SSDR FDEA201201260342Longeron · crackedRIGHT BS 1299, LONGERON 27, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.SDR FDEA201201260340Seat Track · corrodedRIGHT STA 1541 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.
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