N599FE

Service difficulty reports · 318

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 = 'N599FE' 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.

SDR FDEA201509272996Skin · damagedDURING POST FLIGHT, FOUND DAMAGE, DENT & 4" LONG CRACK, TO RT WING, FIXED LE SKIN. DAMAGE IS ON UNDERSIDE OF WING LE, BEHIND INBD END OF NR 5 SLAT. REPAIRED IAW EA 1-5730-T0320545 P1.Sep 27, 2015 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201411073541Skin · crackedR3 PLUG DOOR CUT OUT SURROUNDING FOUND ONE CRACK, INSPECTION ACCESS, FWD MOST LOWER ACCESS. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 7, 2014 · N599FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201411063532Hinge · crackedMAIN LANDING GEAR LT DOOR SIDE, AFT DOOR HINGE FITTING FOUND WITH CRACKED. REMOVED AND REPLACED IAW SRM 51-35-01 REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100Nov 6, 2014 · N599FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201411053518Doubler · crackedRIGHT WING LE RIB DOUBLER FOUND CRACKED AT XOS 667. DOUBLER FABRICATED IAW DRAWING ARB3954 REVISION K. RIB DOUBLER REMOVED AND REPLACED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201411053517Former · crackedRIGHT WING LE SUPPORT FORMER FOUND CRACKED AT XOS 559. FORMER FABRICATED IAW DRAWING ARB1162 REVISION S. FORMER REMOVED AND REPLACED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing SparSDR FDEA201411053516Former · crackedRIGHT WING FIXED LE SUPPORT FORMER FOUND CRACKED AT XOS 584. FORMER REMOVED AND REPLACED IAW SRM 51-33-01. FORMER FABRICATED IAW DRAWING ARB2931 REVISION H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201411053515Skin · crackedRIGHT WING FIXED LE NR 15 SLAT TRACK CUT OUT FOUND CRACKED XOS 944. REPAIRED IAW SRM 57-40- 02 FIGURE 201, REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201411053520Seat Track · crackedSEAT TRACK BS 1561 X -8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411053519Seat Track · corrodedSEAT TRACK BS 1561 X=8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411053514Skin · crackedLEFT WING FIXED LE PANEL 519CB FWD CORNER CUT OUT FOUND CRACKED XOS 610. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201411053513Panel · crackedLEFT WING LE PANEL 518FB FWD CORNER CUT OUT FOUND CRACKED XOS 500. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 5, 2014 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201405291226Bolt · pulledDURING CONTROL CHECK, NO GREEN BOX ON RT AILERON. RETURNED TO GATE. FOUND RT INBD AILERON DROPPED WITH HYD POWER ON, FURTHER INSPECTION FOUND RT INBD ACTUATOR DETACHED FROM WING STRUCTURE, ALL FOUR BOLTS PULLED OUT FROM ACTUATOR. REMOVED AND REPLACED RT IMay 29, 2014 · N599FE · Doug MD11F · AileronsSDR FDEA201312193018Liner · damagedAFTER ADDING POWER FOR TAKEOFF & ACCELERATING THROUGH 60 KTS, HEARD A LOUD HISSING NOISE & FELT SWERVE TO THE LEFT. ABORTED TAKEOFF & RETURNED TO THE GATE. NO ABNORMAL ENGINE INDICATIONS, BUT AFTER RETURN TO GATE, DISCOVERED HONEYCOMB MATERIAL IN THE FAN BLDec 19, 2013 · N599FE · Doug MD11F · Engine Air Intake SystemSDR FDEA201304180802Mechanism · dirtyAFTER TAKEOFF, RECEIVED RED PRIMARY & SECONDARY LIGHTS WITH THE GEAR HANDLE UP. RAN QRH AND RED LIGHT WENT OUT. TRIED TO WIGGLE AND PUSH GEAR HANDLE PRIOR TO CYCLING GEAR. ALL LIGHTS STAYED ON. PUT GEAR HANDLE DOWN, HANDLE WAS STUCK OUT AND NEEDED TO BE Apr 18, 2013 · N599FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201212074261Access Panel · crackedSEVEN FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIR CLASDec 7, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201212074260Access Panel · crackedTWELVE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND STA XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIRDec 7, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201212064251Beam · crackedUPON REMOVAL OF MAIN DECK R3 DOOR FOUND UPPER BEAM AFT END CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 6, 2012 · N599FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201212044239Beam · crackedCENTER CARGO DOOR ROTARY ACTUATOR BEAM FOUND CRACKED. REPAIRED IAW E.A. 1-5310-165173. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201212044238Skin · crackedRT WING SLAT TRACK NR 12 LOWER OTBD CUT-OUT CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201212044237Seat Track · corrodedMAIN DECK COMPARTMENT -FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1390 TO 1530, RBL 75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212044236Seat Track · corrodedMAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1250 TO 1390 X=-75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212044235Seat Track · corrodedMAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1220 TO 1250 X= -75. CARRIED OUT SEAT TRACK SEGMENT REPLACEMENT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212044234Slat Track · crackedLEFT WING NR 8 SLAT TRACK UPPER DOOR CUT-OUT CRACKED. REPAIRED AS PER E.A. 1-5730-163557. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201212034228Skin · crackedLEFT AIR CON COMPARTMENT NR 2 DOOR EXTERIOR UPPER SKIN EDGE CRACKED. REPAIRED AS PER SRM 52-40-01 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.Dec 3, 2012 · N599FE · Doug MD11F · Air Conditioning DoorsSDR FDEA201211304219Skin · corrodedLT WING T/E PANEL 541JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211304218Skin · puncturedRIGHT WING NR 2 SLAT LOWER SURFACE SKIN PUNCTURED. REPAIRED IAW EA 1-5750- 163560. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211304217Skin · corrodedRT WING T/E PANEL 641JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211304209Duct · crackedLT WING TELESCOPIC DUCT UPPER DOOR CUT-OUT CRACKED. REPAIRED IAW SRM 57-40- 01 REPAIR 10 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201105292024Cover · dislodgedL1 EMERGENCY EXIT LIGHT COVER DROPPED OFF. R & R EMERG EXIT LIGHT COVER ALIGNMENT PINS, OPS CKS GOOD. OK FOR SERVICE. FINAL CLOSED.May 29, 2011 · N599FE · Doug MD11F · Emergency LightingSDR FDEA201102030466Blades · damagedDURING INITIAL CLIMBOUT, FELT MODERATE VIBRATION (FELT LIKE NOSE GEAR SPINNING). AFTER INITIAL LEVEL OFF AT 9000 FT, VIBRATION LESSENED. DURING CLIMB TO 15000 FT, VIBRATION CONTINUED TO REVERSE WITH HIGH EVM READING. RAN QRH & WITH HIGH EVM & VIBRATION AFeb 3, 2011 · N599FE · Doug MD11F · Turbine Engine Compressor SectionSDR FDEA201101170196Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 60.5 FOUND CORROED. CORROSION REMOVED IAW SRM 51-21-01, REV 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.137 INCH. MATERIAL REMOVED = 0.030 INCH AND FOUND. ACCEPTABLE IAWJan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170200Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 99.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.151 INCH. MATERIAL REMOVED = 0.016 INCH AND FOUND ACCEPTAJan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170199Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 88 TO X= 84 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.150 INCH. MATERIAL REMOVED = 0.017 INCH AND FOUNDJan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170198Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 95.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.153 INCH. MATERIAL REMOVED = 0.014 INCH AND FOUND ACCEPTAJan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170197Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STA 1227, X= 99.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.151 INCH. MATERIAL REMOVED = 0.016 INCH AND FOUND ACCEPTAJan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170195Skin · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= -60 TO X= -8 FOUND SEVERAL AREAS OF CORROSION. CORRODED AREA REPAIRED IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.Jan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101170194Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= -80 TO X= -101 FOUND SEVERAL AREAS OF CORROSION. CORROSION REPAIRED IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Jan 17, 2011 · N599FE · Doug MD11F · Fuel StorageSDR FDEA201101110103Seat Track · crackedMAIN DECK STA 650, X =75.25, FOUND SEAT TRACK CRACKED. MAIN DECK-CRACKED SEAT TRACK AT STA 650, X =75.25 REPAIRED FROM STA 643 TO STA 685 IAW EA NR1-5310-143827 PART 1, TITLE: FUSELAGE - MAIN FRAME - CURVED SEAT TRACK REPAIR AT X = 75.25 AND STA 643. REPAIJan 11, 2011 · N599FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101100095Frame · dentedMAIN DECK CABIN, FRAME AT STA 1561, LONGERON 12 RT FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-00-07, FIGURE 201, REPAIR 2, REV 45. REPETIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201Jan 10, 2011 · N599FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201101100094Frame · dentedMAIN DECK CABIN, FRAME AT STA 1661, LONGERON 12 RT, FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 45. REPETIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, RJan 10, 2011 · N599FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201101090090Longeron · corrodedLOWER CTR CARGO COMPARTMENT - BILGE AREA STA 5-123 LONGERON 44R FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-00-05 REPAIR 1 FIGURE 202 REVISION 45 AND E.A. 1-5310-143504, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REVISION 111.Jan 9, 2011 · N599FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101080077Longeron Splice · crackedLWR CTR CARGO COMPARTMENT BILGE AREA STA 5-123, LONGERON 49 LT SPLICE FITTING FOUND CRACKED. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 45. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7114 REVISION F. THIS REPAIR CLASSIFIED AS MAJOJan 8, 2011 · N599FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201101070068Rib · crackedRT WING L/E RIB 16 FOUND CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. NEW RIB FABRICATED AS PER DRAWING ARB2850, REVISION G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Jan 7, 2011 · N599FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201101070066Vane · delaminatedLT WING INBD FLAP VANE LOWER SURFACE MID AREA 05 EACH LOCATION DELAMINATED. LT WING INBD FLAP VANE ASSY R & E IAW AMM27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5. REV 69.0.Jan 7, 2011 · N599FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201101070065Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE DELAMINATED. RT WING INBD FLAP VANE ASSY R & R IAW AMM27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV 69.0.Jan 7, 2011 · N599FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201005231618Relay · inoperativeIN LEVEL FLIGHT AT FL330, RECEIVED A LEVEL 1 BAT DISCHARGING ALERT. IT STAYED ON FOR ABOUT 3 MIN, WENT OUT FOR ABOUT 1 MIN, THEN REMAINED ON FOR THE REMAINDER OF THE FLIGHT. R & R R2-17 RELAY IAW SWP 24-31-00, OPS CHECK OF ELECTRICAL BATTERY IAW AMM 24-32-May 23, 2010 · N599FE · Doug MD11F · Battery/Charger SystemSDR FDEA201005161550Connector · corrodedAFTER T/O OAK GEAR SHOWED RED LT MAIN PRIMARY SECONDARY. COMPLED WITH CHECK LIST, RECKED GEAR PRIMARY SECONDARY BOTH SHOW GREEN LANDED MEM WITHOUT INCIDENT. INTERROGATED PSEU AND FOUND NO FAULTS ON SYS. TEST IAW AMM ATA 31-71-01-2. CHECKED D1-81 AND FOUNDMay 16, 2010 · N599FE · Doug MD11F · Landing Gear System WiringSDR FDEA201005151541Pseu · failedAFTER TAKEOFF HAD AN UNSAFE GEAR INDICATION FOR LT MAIN ON BOTH PRIMARY AND SYNOPTIC DISPLAY WHEN GEAR RETRACTED. COMPLETED WITH QRH, RECYCLED GEAR AND GOT A NORMAL UP INDICATION ON BOTH PRIMARY AND SYNOPTIC. LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LT May 15, 2010 · N599FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201003070671Display · failedENG NR1 OIL TEMP HI ALERT APPEARED, ALL OTHER INDICATIONS NORMAL. OIL TEMP MAXED AT 220 DEGREES C. SHUTDOWN NR1 ENG IAW QRH. OIL TEMP RETURNED TO 80 DEGREE C IMMEDIATLY AFTER SHUTDOWN. VIA SATCOM CONSULTED WITH GOC, MOCC, POWERPLANT DUTY OFFICER AND TECH PILMar 7, 2010 · N599FE · Doug MD11F · Engine Temperature Indicating SystemSDR FDEA200903311116Support · crackedLEFT MAIN LANDING GEAR WHEEL WELL, CUT-OUT ON GEAR DOOR CYLINDER SUPPORT CRACKED AT STA 1441. LEFT MAIN LANDING GEAR WHEEL WELL, CUT-OUT ON GEAR DOOR CYLINDER SUPPORT AT STA 1441 REPAIRED AS PER FEDEX EA NR 1-5310-127493 TITLE: FUSELAGE, MAIN FRAME, LEFT MAINMar 31, 2009 · N599FE · Doug MD11F · Fuselage Miscellaneous Structure
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