N579FE, cancelled Mar 2, 2024
Service difficulty reports · 254
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 = 'N579FE' AND deregistration_id = 'N579FE-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 = 'N579FE' AND deregistration_id = 'N579FE-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 FDEA201311192828Sensor · failedUPON CONFIGURATION AT 15 DEG FLAPS, LEVEL 2 SLAT DISAGREE ILLUMINATED, GO AROUND. RAN CHECKLIST ON EXTENDED DOWNWIND. DURING GO AROUND THERE WAS SOME FEEL THAT CONFIGURATION WAS OFF. LANDED SLAT STOW FLAPS 28 DEGREES AT 185KTS & MAX BRAKES. RAN SLATS VERSDR FDEA201308011738Wheel · failedLEVEL 2 TIRE FAIL ON LANDING ROLL, R & R NR 10 MAIN WHEEL ASSY IAW 32-41-01-4 UP TO STEP 5F(6).SDR FDEA201307201601Switch · failedSLIDE PRESSURE LIGHT IN L1 DOOR WAS INOPERATIVE, REPLACED LIGHT SWITCH ASSY IAW MM 25-61-04-4. OPS CHECKED NORMAL.SDR FDEA201304080743Transmitter · malfunctionedPASSING THRU FL 260 RECEIVED A LEVEL 2 FUEL QTY/USED CHECK. FUEL USED ON ALL THREE ENGINES TOTALED WITH FUEL ONBOARD TOTALED 58.8 VICE FOB OF 56.4 AT TAKEOFF. RAN CHECK LIST AND DECIDED TO LEAVE ALL THREE ENG RUNNING. DURING DESCENT FUEL USED ON ENGINE 1 SDR FDEA201212084268Skin · looseLEFT WING INBD FLAP UPPER SURFACE AT XIFH= 171 RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 4 REVISION 51 AND EA 1-5750-163534 STEP 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074267Bulkhead · misrepairedNLG HORIZONTAL PRESSURE PANEL, LT SIDE, BS 495 TO 515, "X"=30 TO "X"=39 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074266Bulkhead · misrepairedNLG HORIZONTAL PRESSURE PANEL, LT SIDE, AT BS 495 TO 515, "X"=42 TO "X"=47 MISREPAIRED. REPAIRED IAW EA 1-5310-163550. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074265Floorbeam · misrepairedFLOORBEAM LOWER FLANGE AT BS 5-53 MISREPAIRED. REPAIRED IAW EA 1-5310-163551. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201212074264Hinge Bracket · corrodedRT WING, OTBD FLAP, INBD FORWARD HINGE BRACKET, LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER: 0.705", FINAL HOLE DIAMETER: 0.709", MAXIMUM HOLE: 0.709". REPAIR BUSHING FABRSDR FDEA201211304215Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162SDR FDEA201211304216Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162399 PSDR FDEA201211294198Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS XIFH 261 FOUND LOOSE. REMOVED AND REPAIR ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211294201Stop Fitting · crackedON REMOVAL OF R1 MED DUST COVER NR 3 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211294200Stop Fitting · crackedON REMOVAL OF R1 MED DUST COVER NR 2 DOOR BEAM AFT STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51 AND EA 1-5210-163538. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211284192Frame · crackedNR 1 ENGINE THRUST REVERSER AFT CASCADE SUPPORT FRAME AT POSITION 6 FOUND CRACKED AT NUTPLATE AREA. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SUPPORT FRAME AS PER EA 1-7830-163531. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211284189Skin · looseRIGHT WING INBD FLAP UPPER SURFACE AT "XIFH" = 269 FOUND LOOSE RIVETS. REMOVED AND REPAIRED ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211264180Skin · corrodedAFT ACCESSORY COMPARTMENT, FUSELAGE RT SIDE, SKIN AT STATION 2163 TO 2140, BETWEEN LONGERON 33 RIGHT AND 35 RIGHT, FOUND SURFACE CORROSION ON INTERIOR AREA COMMON TO EXISTING EXTERIOR REPAIR DOUBLER. REPAIRED IAW SRM 51-21-01 REVISION 51. FOUND EXCEEDED LSDR FDEA201211264158Seat Track · corrodedBS 1385, "X"= 8.5. SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264157Seat Track · corrodedBS 1451, "X"= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53- 00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264160Seat Track · corrodedBS 1641, "X"=-8.5, SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264159Seat Track · corrodedBS 1884 TO 1887, "X"=-8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211234132Web · canningCENTER LANDING GEAR LT KEEL WEB AT BS 1431 OIL CANNING FOUND EXCEED SRM ALLOWABLE LIMITS. REPAIRED IAW EA 1-5310-163532. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211224122Skin · misrepairedSKIN MISREPAIRED AT BS 1846, LONGEON 42 TO 44 RIGHT. REPAIRED IAW EA 1-5330-163536. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211214115Web · crackedRT OBSERVER SEAT, LOWER FLOOR WEB FOUND EDGE CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-51, REPAIR 1, FIGURE 202, REVISION 51. REPAIR PARTS INSTALLED IAW SRM 51-35-01, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115.SDR FDEA201211214107Frame · crackedFRAME END CAP AT BS 555, NEAR LONGERON 32R, IN AIR CONDITION PACK NR 3 COMPARTMENT, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-35- 01, REVISION 51.. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115.SDR FDEA201211194084Hinge Bracket · damagedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND EXCEEDED LIMITS AFTER BUSHING REMOVED. REPAIRED PER EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194097Skin · looseLEFT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163534, STEP 4, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194096Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REMOVED AND REPAIRED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211194095Hinge Bracket · scratchedLEFT WING INBD FLAP FORWARD HINGE BRACKET PIVOT BORE OTBD SPOT FACE FOUND SCRATCHED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07, REVISION 74. REPAIR ACCOMPLISHED PER EA 1-5750-162397, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 1SDR FDEA201211194094Hinge Bracket · corrodedRIGHT WING INBD FLAP, FORWARD HINGE BRACKET PIVOT LUG BORE INBD AND OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07 REVISION 74. REPAIR ACCOMPLISHED AS PER EA 1-5750-163542, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201211194092Hinge Bracket · corrodedDURING BUSHING REMOVAL, LEFT WING INBD FLAP, AFT OTBD HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED BEYOND LIMITS. ACCOMPLISHED BUSHING REPAIR PER EA 1-5750-162394 PART 1. REPAIR CLASSIFIED A MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194091Skin · chafedSKIN CHAFED AT BS 889, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194090Skin · chafedSKIN CHAFED BS 1009, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. EO 1-5100-7-5001 B2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194085Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND EXCEEDED LIMIT AFTER BUSHING REMOVED. REPAIRED IAW EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194082Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-10-6 REVISION 74. FOUND ACCEPTABLE IAW EA 1-5750-162398 PART 1. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 74. REPAIR CARRIED OUT PER ESDR FDEA201211194089Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS WERE FOUND ON RIB AT STATION XOS =1141.2. R & R IAW DWG ARB1954 REV NC AND EA 1-5750-163529, STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211194088Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1146.8. REMOVED AND REPLACED AS PER DRAWING ARB1954 REVISION NC AND E.A. 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194087Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1135.6. REMOVED AND REPLACED IAW DRAWING ARB1954 REVISION NC AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194086Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1152.4. REMOVED AND REPLACED IAW DRAWING ARB1955 REVISION D AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194083Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER MOUNT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08 REVISION 74. REPAIRED IAW EA 1-5750-162398 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194081Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10. REPAIR CLASSIFIED AS MAJORSDR FDEA201211194080Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10, . WASHER AT OUTBOARD HINSDR FDEA201211194079Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION SDR FDEA201211194078Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVSDR FDEA201211194077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MSDR FDEA201211194076Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITD AS PER CMM 57-44-09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MASDR FDEA201211194075Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44- 09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEPS 1, 2, 3, 4, 5, 8, 9 AND 10. REPAIR CLASSIFIED AS MAJOR PERSDR FDEA201211194093Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING THICKNESS: 0.263", MATERIAL REMOVED: 0.078", REMAINING THICKNESS: 0.185", MINIMUM THICKNESS: 0.SDR FDEA201211174062Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.224 INCH, FINAL HOLE DIAMETER = 1.228 INCH, MAXIMUM HOLE DIAMETER = 1.220 INCH. RSDR FDEA201211174065Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
Back to N579FE, cancelled Mar 2, 2024