N591FE

Service difficulty reports · 394

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 = 'N591FE' 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 FDEA201701030013Web · crackedMAIN DECK CARGO BAY, R3 DOOR FORWARD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255 BETWEEN LONGERON 26 AND 27R. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. MAJOR REPAIR IAW GMM 6-2-100.Jan 3, 2017 · N591FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201701030012Beam · brokenCABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR FORWARD LOWER BEAM DOOR STOP NR 7 BROKEN. REMOVED AND REPLACED IAW SRM 51-31-01-0G AND EA 1-5210-T0330676A.Jan 3, 2017 · N591FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201701030011Seat Track · damagedCABIN, MAIN DECK CABIN COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT RIGHT HAND STATION 1279, X = -8.5. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1229 TO STA 1331, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR Jan 3, 2017 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701030010Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 646 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030009Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 655 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030008Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 669 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030007Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 700 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11 · Wing, Plate/SkinSDR FDEA201701030006Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 712 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030005Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 790 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030004Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 612 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701030003Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 666 FOUND FORWARD STRINGER CRACKED.Jan 3, 2017 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606292197Computer · failedRECEIVED AURAL CAWS ALERT, TIRE FAILURE, ON GEAR EXTENSION. ALL OTHER INDICATIONS NORMAL. PERFORMED GO AROUND, QRH CHECKLIST, LANDED. PREMATURE REMOVAL/INSTALLATION. LAST FLIGHT FAULT SHOWED, BTM/TPI CONTROL UNIT COMPUTER FAIL INTERMITTENT. REPLACED THE TJun 29, 2016 · N591FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201606202067O-Ring · failedLEVEL 1 ALERT, HYD 2 OFF, 40 MIN INTO FLIGHT AT 370. 2.7 GAL LEFT, HYD 2 QTY LO, 1.3 GAL LEFT AFTER CONFIGURING. QRH COMPLIED WITH. LEAK WAS FOUND AT THE NR 2 HYD PRESSURE TRANSDUCER O-RING, REPLACED O-RING, MPN NAS1612-10, IPC 29-12-24-01, ITEM 060, REF MJun 20, 2016 · N591FE · Doug MD11F · Hydraulic System, MainSDR FDEA201509303009Charger · failed30 MIN INTO FLIGHT, AT FL 370 RECEIVED LEVEL ONE BATTERY DISCHARGE FOR 10 - 15 SECONDS, FOLLOWED BY BATTERY CHARGE FOR 5 SECONDS. BATTERY SHOWED 29V & CHARGED TO 31 VOLTS & REMAINED THERE TILL SHUTDOWN. BATTERY DISCHARGE ALERT CLEARED AFTER BATTERY CHARGE TOSep 30, 2015 · N591FE · Doug MD11F · Battery/Charger SystemSDR FDEA201509202901Unknown · malfunctionedDURING CLIMB, LOST DU 1, 2, 3, 4, 6 & HAD NUMEROUS ALERTS, AUTOPILOT & AUTO THROTTLE DISCONNECT & NOT AVAILABLE. EMERGENCY POWER CAME ON. ACFT SEEMED TO BE POWERED BY EMERGENCY POWER ONLY, GEN 2 & 3 OPERATIONAL. GEN 1 DISCONNECTED. STARTED APU WITH NO CHANSep 20, 2015 · N591FE · Doug MD11F · AC Generation SystemSDR FDEA201506231982Cover · unsecureLIGHTED EXIT DOOR COVER OVER 1L ENTRY DOOR FELL OFF DURING TAKEOFF. SECURED COVER IAW SMP. ACFT OK FOR SERVICE.Jun 23, 2015 · N591FE · Doug MD11F · Emergency LightingSDR FDEA201504161249Door · malfunctionedLEFT FWD CABIN DOOR WILL NOT LOWER OR RAISE. L1 DOOR OPERATED NUMEROUS TIMES PER AMM 52-10-01-2. CHECKED TRACKS, RETRACTING CEILING PANEL FOUND NO BINDING. SUSPECT SLIDE DISARM LEVER NOT COMPLETELY SEATED IN D-TENT. DOOR OK FOR SERVICE.Apr 16, 2015 · N591FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201501220259Spar Cap · corrodedLEFT WING TE AFT SPAR UPPER AFT FLANGE SURFACE CORRODED BETWEEN STATION XORS 1020 - 1042. REPAIRED IAW EA T1-5710-T0314790 PT 1.Jan 22, 2015 · N591FE · Doug MD11F · Wing SparSDR FDEA201501210247Keelbeam · canningCENTER LG AREA, RT KEEL WEB, SEE SEQUENCE 472. REFERENCED AREA HAS BEEN REMAPPED, OIL CANNING DIMENSIONS HAVE BEEN CHANGED. ONE ADDITIONAL AREA HAS BEEN NOTED. Y=1394 - 1401 Z=-100.00--110.00 DEPTH .080 & 2 MAPPED AREAS ARE BEYOND MAX DIMENSION OF .190 Y=14Jan 21, 2015 · N591FE · Doug MD11F · Fuselage Main, KeelSDR FDEA201501130157Feeder Cable · failedNR 2 ENGINE POWER FEEDER CABLE SHORTED ON SUPPORT BRACKET INSIDE PYLON PANEL 457BR. REPLACED DAMAGED POWER FEEDER CABLE,Jan 13, 2015 · N591FE · Doug MD11F · Electrical Power System WiringSDR FDEA201501130140Feeder Cable · shortedNR 2 ENGINE POWER FEEDER CABLE SHORTED ON SUPPORT BRACKET INSIDE PYLON PANEL 457BR. REMOVED AND REPLACED THE POWER FEEDER CABLE IAW SWPM 20-00-16.Jan 13, 2015 · N591FE · Doug MD11F · Electrical Power System WiringSDR FDEA201501110118Doubler · crackedLEFT MLG WW INBD WEB LOWER FWD CORNER AT STATION X=31.5 WEB FEED THRU DOUBLER AEA0526-1 IS CRACKED. R & R AEA0526U1 DOUBLER IAW DWG AEA0526.Jan 11, 2015 · N591FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201501100112Skin · corrodedLEFT AC COMPARTMENT BETWEEN STATION 435 & 575 CORROSION ON SKIN BELOW NR 1 ACM DOOR CUT OUT. REMOVED MINOR CORROSION WITHIN LIMITS IAW MM 51-12-00. ALODINE & PRIME IAW MM 51-21-00 & MM 51-22-00.Jan 10, 2015 · N591FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201501090111Fitting · crackedUPPER FUSELAGE RT SIDE, STATION 2164. TAIL CONE GUIDE ROLLER FITTING IS CRACKED. INSTALLED NEW TAIL CONE ROLLER FITTING IAW SRM 51-31-01.Jan 9, 2015 · N591FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201501090106Nut · looseCENTER LG LT PILLOW BLOCK ATTACH LUG NUT LOOSE, AS INDICATED BY ROTATING WASHER & RUST EMANATING FROM ATTACH POINT AREA. REPLACED LT PILLOW BLOCK ATTACH LUG NUT, TRUNNION PIN, IAW CMM 32-15-01. WASHER NO LONGER ROTATES. REMOVE SURFACE CORROSION EXISTING ON Jan 9, 2015 · N591FE · Doug MD11F · Main Landing Gear Attach SectionSDR FDEA201405301233Reservoir · lowDURING SERVICE CHECK FOUND R1 ESCAPE SLIDE PRESS IS LOW, REQUIRES SERVICING, FOUND TO BE WITHIN LIMITS. OBSERVED R1 DOOR PNEUMATIC STORAGE SYS TO BE IN NEED OF SERVICING. SERVICED DOOR.May 30, 2014 · N591FE · Doug MD11F · Service DoorsSDR FDEA201302200378Lamp · inoperativeDOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST BUTTON, INOPERATIVE. REMOVED AND REPLACED R1 DOOR REMOTE DOOR SLIDE PRESSURE INDICATOR LAMPS BY REMOVING LENS AND REPLACING LAMPS PER SMP AND OPS CHECKED IAW MM 25-61-04-5. OPS CHECKED NORMAL.Feb 20, 2013 · N591FE · Doug MD11F · Escape SlideSDR FDEA201301240168Skin · erodedRIGHT WING NR 1 L/E SLAT INBD PERFORMANCE FILLET SURFACE FOUND ERODED. REPAIRED IAW EA 1-5750-163572. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jan 24, 2013 · N591FE · Doug MD11F · Leading Edge DevicesSDR FDEA201301230163Doubler · crackedLEFT WING FIXED L/E BEAD DOUBLER AT XOS 666 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Jan 23, 2013 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201301180131Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT LT SIDE LONGERON SPLICE FOUND CRACKED BETWEEN STATION 5-113 TO STATION 5-123, LONGERON 43L. SPLICE FABRICATED IAW DWG A5A7116, REV D LOWER CENTER CARGO COMPARTMENT LT SIDE LONGERON SPLICE 43L STATION BETWEEN 5-113-TO 5-123. R &Jan 18, 2013 · N591FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201301180130Longeron · corrodedLOWER AFT CARGO COMPARTMENT BILGE AREA LONGERON 44R FOUND WITH CORROSION BETWEEN STATION 1887 TO STATION 1902.160. REPAIR LONGERON FABRICATED IAW DWG AGA7038 REVISION B AND EA 1-5310-165183. REPAIRED IAW SRM 53-00-05, REPAIR 1, REV 51. REPAIR CLASSIFIED AJan 18, 2013 · N591FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201301180129Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT RT SIDE LONGERON SPLICE WITH CRACK BETWEEN STA 5-113 TO 5-123, LONGERON 35R. SPLICE FABRICATED IAW DWG A5A7114, REV J. LOWER CENTER CARGO COMPARTMENT RT SIDE LONGERON SPLICE R& R WITH NEW SPLICE IAW SRM 51-33-01, REV 51. REPJan 18, 2013 · N591FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201301180128Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT LT SIDE LONGERON SPLICE WITH CRACK BETWEEN STATION 5-113 TO 5-123, LONGERON 37L. SPLICE FABRICATED IAW DWG A5A7114, REV J. LONGERON SPLICE R & R WITH NEW SPLICE IAW SRM 51-33-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2Jan 18, 2013 · N591FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201301180127Tee Fitting · crackedCENTER WHEEL WELL FORWARD BULKHEAD LT VERTICAL TEE FITTING CRACKED. TEE FITTING FABRICATED IAW DWG APB 7158 REVISION C. TEE CHORD REMOVED AND REPLACED IAW SRM 51-31-01, REV 51. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100, REV 116.Jan 18, 2013 · N591FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201301160102Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 75.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 75.0. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 116.Jan 16, 2013 · N591FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201301160103Access Panel · corrodedLEFT WING - T/E LOWER ACCESS PANEL 541JB CUT-OUT FORWARD EDGE LOWER CAP, LOWER SURFACE FOUND CORROSION. FOUND WITHIN LIMITS IAW SRM 57-00-00, FIG 202, REV 51. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.Jan 16, 2013 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201301160101Access Panel · corrodedRT WING - T/E LOWER ACCESS PANEL 641JB CUT-OUT FORWARD EDGE LOWER CAP, LOWER SURFACE FOUND CORROSION. CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01, REV 51. ORIGINAL THICKNESS: 0.120", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.0116" AND FOUND WIJan 16, 2013 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201103040843Lug · crackedUPON REMOVAL OF RT WING OTBD HYD SYS NR 3 SLAT ACTUATOR, FOUND OTBD SLAT MECHANISM ASSY OTBD UPPER SUPPORT LUG CRACKED. OUTBOARD LUG BRACKET REMOVED AND REPLACED AS PER CMM 27-83-11 REVISION 69. FUNCTIONAL TEST OF THE SLAT CARRIED OUT AS PER AMM 27-82-02-4 RMar 4, 2011 · N591FE · Doug MD11F · Leading Edge DevicesSDR FDEA201102270792Skin · chafedLEFT WING EXISTING REPAIR DOUBLER CHAFED AT WING ANTI-ICE DUCT CUT-OUT OUTBOARD CORNER. LT WING EXISTING REPAIR DOUBLER AT WING ANTI-ICE DUCT CUT-OUT OUTBOARD CORNER REMOVED AND FABRICATED NEW REPAIR DOUBLER AS PER SRM 57-40-02 FIGURE 201 REVISION 45. INSTALFeb 27, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102250763Skin · crackedLEFT WING LEADING EDGE LOWER SURFACE SKIN FOUND CRACKED AT STATION XORS 616, NR 5 SLAT MAIN TRACK CUTOUT OUTBOARD CORNER. REPAIR CARRIED OUT AT LT WING LOWER LEADING EDGE SKIN AREA AT STATION 616 NR 5 SLAT MAIN TRACK CUTOUT OUTBOARD CORNER AS PER SRM 57-40-Feb 25, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102250762Skin · crackedRIGHT WING LEADING EDGE LOWER SKIN FOUND CRACKED AT STATION XORS 507, REFUELING STATION ACCESS PANEL, INBOARD HINGE CORNER. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER SKIN AT STATION XORS 50. REFUELING STATION ACCESS PANEL INBOARD HINGE CORNER AS PER SFeb 25, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102250761Skin · crackedLEFT WING LEADING EDGE LOWER SURFACE SKIN FOUND CRACKED AT STATION XORS 507, REFUELING STATION ACCESS PANEL, INBOARD HINGE CORNER. REPAIR CARRIED OUT AT LT WING LEADING EDGE LOWER SKIN AT STATION XORS 507 REFUELING STATION ACCESS PANEL INBOARD HINGE CORNER Feb 25, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102170602Skin · cracked07 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.65. ACCESS DOOR CUTOUT REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. REPFeb 17, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102170601Skin · cracked09 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND XORS 713.65. ACCESS DOOR CUTOUT REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. Feb 17, 2011 · N591FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201102170600Fillet · crackedRT WING L/E CRUISE PERFORMANCE FILLET NEAR UPPER JOINT FOUND CRACKED. FILLET DOUBLER REPAIRED AS PER SRM 57-40-71 REPAIR 1 FIGURE 201 REVISION 45. OPERATIONAL TEST OF THE SLAT CARRIED OUT AS PER AMM 27-80-00-860-801 REVISION 69.0 FOUND SATISFACTORY. REPAIFeb 17, 2011 · N591FE · Doug MD11F · Leading Edge DevicesSDR FDEA201102170599Rib · crackedLT WING L/E NR 1 SLAT INBD RIB AREA FOUND CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Feb 17, 2011 · N591FE · Doug MD11F · Leading Edge DevicesSDR FDEA201102170598Rib · crackedRT WING L/E NR 1 SLAT INBD RIB AREA FOUND CRACKED. REPAIRED AS PER DRAWING ARB7128 REVISION L AND SRM 51-31-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 45.Feb 17, 2011 · N591FE · Doug MD11F · Leading Edge DevicesSDR FDEA201102170588Seat Track · corrodedLEFT STA 5-70 X=8.5 SEAT TRACK FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 45 REPAIR 1 FROM STATION 5-0 TO STATION 5-83 X= 8.5. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Feb 17, 2011 · N591FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102170587Frame · dentedRIGHT STA 1701, LONGERON 12R FRAME FOUND DENT. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REVISION 45. MAINTENANCE REQUIREMENT METHOD HIGH FREQUENCY EDDY CURRENT INITIAL INSPECTION 14500 CYCLE SUBSEQUENT REPETITIVE INSPECTION OF 9500 CYCLE AS PER SRM 53-0Feb 17, 2011 · N591FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201102170586Frame · dentedRIGHT STA 1681, LONGERON 12R FRAME FOUND DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REVISION 45. MAINTENANCE REQUIREMENT METHOD HIGH FREQUENCY EDDY CURRENT INITIAL INSPECTION AT 14500 CYCLE AND SUBSEQUENT REPETITIVE INSPECTION AT 9500 CYCLE AS PERFeb 17, 2011 · N591FE · Doug MD11F · Fuselage Main, Frame
Back to N591FE