N572FE

Service difficulty reports · 258

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 = 'N572FE' 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 FDEA201704161210Skin · crackedLEFT WING FIXED LEADING EDGE, NR 14 SLAT TRACK CUTOUT FOUND CRACKED AT XOS 891. REPAIRED THE TRACK CUTOUT IAW SRM 57-40-02-2R, REPAIR 7, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 16, 2017 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201704161209Repair · chafedCABIN, MAIN DECK CARGO COMPT FRAME EXISTING REPAIR CHAFED AT LT STA 535, LONGERON 24L. REPAIR ANGLE REPAIRED AS PER SRM 53-00-07-2R FIG 201 REPAIR 1. CHAFING MARKS ON OUTER REPAIR ANGLE EXCEEDED LIMITS AS PER SRM 53-00-00-2R FIG 202. ORIG THICKNESS: 0.125", MAApr 16, 2017 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201704161208Repair · chafedCABIN, MAIN DECK CARGO COMPT FRAME EXISTING REPAIR CHAFED AT LT STA 535, LONGERON 19L. REPAIR ANGLE REPAIRED AS PER SRM 53-00-07-2R FIG 202 REPAIR 1. CHAFING MARKS FOUND EXCEEDED LIMITS AS PER SRM 53-00-00-2R FIG 202, ORIG THICKNESS: 0.125", MATERIAL REMOVED: Apr 16, 2017 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201704161207Skin · chafedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIR DOUBLER FOUND CHAFED AT XOS 464 TO 470. REPAIRED THE WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT SKIN IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 16, 2017 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201704161206Doubler · chafedLEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIR DOUBLER, FOUND CHAFED AT XOS 464 TO XOS 470. REPAIRED THE LEFT WING TELESCOPIC DUCT CUTOUT IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 16, 2017 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201601150157Hmu · malfunctionedDURING INITIAL DESCENT, BLEED AIR 3 OFF, ALERT CAME ON AROUND FL 340. NOTICED HIGH EGT ON ENG 3 VERSES OTHER 2 ENGS. ENG 3 WAS NOT RESPONSIVE AS THROTTLE PUSHED FWD. CREW PUSHED ENG OUT CLEAR ON FMS & RAN THE ENG SHUTDOWN IN FLIGHT PROCEDURES IN QRH FOR NRJan 15, 2016 · N572FE · Doug MD11F · Fuel Controlling SystemSDR FDEA201512103962Anti-Ice Valve · failedON DESCENT THROUGH 15000 FT, RECEIVED ENG 2 ANTI-ICE LEVEL 3 WITH TRITONE, FOLLOWED QRH & SHUT ENG DOWN FOR LANDING. R & R NR 2 ENG COWL ANTI-ICE MANIFOLD FAILURE SENSING ELEMENTS IAW AMM 30-22-11-4. ALSO R & R NR 2 ENG ANTI-ICE VLV IAW MM 30-22-01-4. ALL Dec 10, 2015 · N572FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201508262705Brake · damagedON PUSH BACK, PUSH CREW NOTICED BRAKE COMING APART ON RT MAIN, RETURNED TO CHOCKS. R & R NR 4 TIRE & BRAKE ASSEMBLY IAW AMM 32-41-01-04 & 32-43-20-04.Aug 26, 2015 · N572FE · Doug MD11F · BrakeSDR FDEA201507102189Contactor · failedL1 DOOR WON’T RAISE WITH ELECTRIC SWITCH. REMOVED AND REPLACED THE LEFT FWD DOOR CONTROL CONTACTOR IAW SWPM 20-20-03. COMPLIED WITH AN OPS TEST IAW MM 52-11-02-2. OPS CHECKED NORMAL. OK TO CONTINUE.Jul 10, 2015 · N572FE · Doug MD11F · Door System WiringSDR FDEA201505281654Actuator · corrodedRIGHT OTBD SLAT DRIVE INBD & OTBD ACTUATORS WILL NOT TAKE GREASE. R & R RT OTBD SLAT DRIVE ASSEMBLY. BOTH INBD & OTBD DRIVE ACTUATORS & ASSOCIATED ATTACH HARDWARE IAW AMM 27-83-30-4.May 28, 2015 · N572FE · Doug MD11F · Leading Edge Slat ActuatorSDR FDEA201505281653Actuator · corrodedLEFT OTBD SLAT DRIVE INBD ACTUATOR WILL NOT TAKE GREASE. R & R LT OTBD SLAT DRIVE ASSEMBLY & BOTH INBD & OTBD DRIVE ACTUATORS & ASSOCIATED ATTACH HARDWARE IAW AMM 27-83-30-4.May 28, 2015 · N572FE · Doug MD11F · Leading Edge Slat ActuatorSDR FDEA201505281652Structure · out of alignmentNUMBER 2 ENG HAS MIS-MATCH BETWEEN NOSE COWL INLET & MATING NACELLE STRUCTURE. REPAIRED MIS-MATCH CONDITION ON NR 2 ENG NOSE COWL IAW EA T 1-5410-T0317737 P1.May 28, 2015 · N572FE · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201505271639Keelbeam · canningCENTER WW KEEL WEB, X 31.5 RT Y=1431 - 1441 Z= -90. OIL CANNING CONDITION IS BEYOND LIMITS, MAX IS .190, CANNING MEASURES .300. REPAIRED OIL CANNING CONDITION IAW EA T1-5310-T0317404 REV A P1.May 27, 2015 · N572FE · Doug MD11F · Fuselage Main, KeelSDR FDEA201505211590Skin · crackedLEFT WING AT NR 8 SLAT TRACK LE CUT OUT HAS CRACK, TEAR IN LE STRUCTURE. REPAIRED LE DAMAGE IAW EA T 1-5710-T0317457 P1.May 21, 2015 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201505201589Skin · delaminatedRIGHT WING, OTBD FLAP TOP SURFACE INBD MID-SECTION TE SHOWS EVIDENCE OF DELAMINATION. REMOVED INBD TE OF OTBD FLAP & ROUTED TO COMP SHOP. CUT OUT DAMAGED AREA, FABRICATED CARBON FIBER CLOTH IAW SRM 57-50-80-2R, OK TO BOND. BONDED RT WING OTBD FLAP SURFACE IMay 20, 2015 · N572FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201505201569Skin · crackedRIGHT WING LOWER FIXED LE HAS A 1" CRACK LOCATED AT A PANEL LAND OF 626DB OTBD END, AFT OF SLAT NR 7. REPAIR IAW SRM 57-40-03 REPAIR 1 FIG 201.May 20, 2015 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201505201564Skin · delaminatedRIGHT WING OTBD FLAP TE WEDGE INBD, TOP SURFACE HAS DELAMINATION ON INBD SIDE 6"X13". REPAIRED RT WING OTBD FLAP TE WEDGE INBD TOP SURFACE 6"X 13" IAW SRM 57-50-80-2R.May 20, 2015 · N572FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201505151518Wedge · delaminatedRIGHT WING OTBD FLAP, TE INBD SECTION HAS DELAMINATION ON BOTTOM SIDE AT CTR OF WEDGE. CUT OUT THE DAMAGED AREA INBD SECTION LOWER SURFACE. FABRICATED FOAM & CARBON FIBER IAW SRM 51-62-01, 436825, 97349. BONDED RT WING OTBD FLAP TE INBD SECTION IAW SRM 51-6May 15, 2015 · N572FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201505131502Skin Panel · corrodedRIGHT WING UPPER SURFACE SKIN PANEL HAS SURFACE CORROSION AT APPROX STATION XORS 826, STRINGER 3. REPAIRED IAW SRM 57-00-01 FIG 101 51-00-10 FIG 7.May 13, 2015 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201505131501Bolt · missingLEFT WING NR 3 SLAT MISSING HARDWARE FOR NR 8 SLAT TRACK FWD LOWER FITTING. REPLACED HARDWARE FOR LT NR 8 SLAT TRACK. ADJUSTED & OPERATIONS CHECKED GOOD IAW AMM 27-80-30-4.May 13, 2015 · N572FE · Doug MD11F · Leading Edge DevicesSDR FDEA201505131498Structure · crackedLEFT WING AT NR 8 SLAT TRACK LE CUT OUT HAS CRACK. TEAR IN LE STRUCTURE.May 13, 2015 · N572FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201505061390Skin · crackedFUSELAGE SKIN AT THE UPPER AFT CORNER OF THE NR 3 ACFT COMPARTMENT DOOR, CUT OUT HAS CRACKS AT TWO EACH FASTENER LOCATIONS. PERFORMED REPAIR FOR TWO CRACKS FOUND ON FUSELAGE SKIN AT UPPER AFT CORNER OF THE NR 3 AC COMPARTMENT DOOR CUT OUT IAW SRM 53-20-15-2R.May 6, 2015 · N572FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201505031366Relay · failedON ARRIVAL, L1 DOOR OPENED ELECTRICALLY INTERMITTENTLY. DOOR CLOSES NORMALLY. R & R RELAY FOR FWD DOOR LOCK PIN RELEASE RELAY & LT FWD DOOR CONT POWER INTERLOCK SWITCH CHECKED GOOD, INSIDE & OUTSIDE. DOOR CONT SWITCH OPERATION CHECKED GOOD. LT FWD DOOR May 3, 2015 · N572FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201503030637Spring · detachedDOOR 1L ENTRY DOOR'S SLIDING DOOR PANEL WITH EXIT SIGN DETACHED. INSTALLED SERVICABLE DOOR 1L OVERHEAD SLIDING PANEL IN REF. AMM 25-23-23-4-0. OPS CHECKED GOOD WITH DOOR IN OPEN AND C LOSED POSITIONS. WORKED IN CONJUNCTION WITH WRI 33-2 0/8284 AND WRI 33Mar 3, 2015 · N572FE · Doug MD11F · Emergency LightingSDR FDEA201412174130Valve · failedAFTER TAKEOFF, LANDING GEAR HANDLE COULD NOT BE RAISED. ABLE TO RAISE THE HANDLE AFTER FOUR ATTEMPTS. ACFT SPEED WAS BELOW 210 KNOTS. R & R RT MLG TRUCK BEAM TRIM INTERLOCK VALVE IAW AMM ATA 32-37-03-4. OPS & LEAK CHECKED GOOD. NORMAL EXTENSION & RETRACTIDec 17, 2014 · N572FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201410163174Check Valve · failedAFTER LANDING, AT IDLE NR 2 ENGINE SHUTDOWN. REMOVED LOW PRESSURE BLEED AIR CHECK VALVE FOR INSPECTION IAW MM 36-11-01-6, FOUND ONE FLAPPER HINGE STIFF AND LOWER BEARING CAP LOOSE. REPLACED NR 2 ENGINE LOW PRESSURE CHECK VALVE.Oct 16, 2014 · N572FE · Doug MD11F · Engine Fuel DistributionSDR FDEA201406011245Skin · crackedON PRE-FLIGHT INSP SUSPECT CRACK RT WING LE PANEL INBD RADIUS OF SLAT DRIVE MECHANISM DOOR CUT OUT. VERIFIED AREA TO BE CRACKED IAW NDT SPM PART 6. CRACK IS MARKED WITH PERMANENT MARKER. CUT OUT DAMAGE IAW SRM 57-40-02. NEED NDT TO INSPECT FOR DAMAGE REMJun 1, 2014 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201402200374Engine · failedDURING CLIMB, HAD A LIGHTNING STRIKE ON RADOME & RECEIVED A NR 2 ENGINE N1 EXCEEDANCE WITH AUTO THROTTLES ON OF 118.1. QRH PROCEDURES FOLLOWED & ALL ENGINE INDICATIONS NORMAL. DURING CLIMB TO ALT RECEIVED A NR 2 ENGINE OIL FILTER BYPASS. QRH PROCEDURES FOFeb 20, 2014 · N572FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201308171920Lamp · failedDOOR PRESS TO TEST SWITCH LAMPS FOUND INOPERATIVE. REPLACED LAMPS IAW REF TO AMM 25-61-04-4. OPS TEST PASSED, SYS OK FOR SERVICE.Aug 17, 2013 · N572FE · Doug MD11F · Emergency EquipmentSDR FDEA201306161310Bracket · corrodedRT WING-OTBD FLAP ASSY INBD AFT HINGE INBD LUG PIVOT BORE CORROSION AFTER REMOVAL OF OTBD FLAP ASSY. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04, REV.76. EXISTING HOLE DIAMETER 1.1525 INCH, FINAL HOLE DIAMETER 1.1605 INCH, MAXIMUM HOLE DIAMETER 1.15 IJun 16, 2013 · N572FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306141285Doubler · crackedLEFT WING FIXED L/E COMPARTMENT STATION XOS 755, BEADED DOUBLER CRACKED. REPAIRED AS PER SRM 57-40-02, FIGURE 203, REPAIR 15, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 14, 2013 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306131270Door Frame · crackedMAIN DECK DOOR NR 3 RT AFT DOOR JAMB LOWEST LIGHTENING HOLE FOUND CRACKED. REPAIRED AS PER SRM 53-40-15, FIGURE 201, REPAIR 3, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 13, 2013 · N572FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306131269Door Frame · crackedMAIN DECK DOOR NR 3 RT FWD DOOR JAMB LOWEST LIGHTENING HOLE FOUND CRACKED. MAIN DECK DOOR 3R BS 1256.75, LONGERON 27 CRACK WEB REPAIRED AS PER SRM 53-40-15, FIGURE 201, REPAIR 3, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 13, 2013 · N572FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306071220Frame · dentedMAIN DECK CARGO BS 1681 FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 7, 2013 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306061207Door Frame · crackedMAIN DECK CARGO, LEFT SIDE L3 DOOR FORWARD FRAME AT LONGERON 21 LIGHTNING HOLE FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 6, 2013 · N572FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306061206Skin · crackedRT WING, L/E REFUELING PANEL 619CB INBD FORWARD CUT-OUT CRACKED. REPAIRED IAW SRM 57-40-02, FIG 202, REPAIR 7, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 6, 2013 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306051197Web · crackedFAC COMPARTMENT CEILING RT OBSERVER SEAT BASE ATTACHMENT CENTER HOLE FOUND CRACKED BS 360 TO 370. REPAIRED IAW SRM 53-10-51, FIG 202, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 5, 2013 · N572FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201306041188Skin · corrodedLT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-T0300678A, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 4, 2013 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201302240423Lamp · inoperativeLT ENTRY DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. REPLACED LAMP IAW SMP. OPS CHECKED IS SATISFACTORY ACFT OK FOR CONTINUE SERVICE.Feb 24, 2013 · N572FE · Doug MD11F · Escape SlideSDR FDEA201204271651Indicator · failedDOOR SLIDE LIGHT WILL NOT GO OUT. REPLACED R1 REMOTE PRESSURE INDICATOR ASSY REF MM 25-61-04-4-0. OP CHECKED GOOD.Apr 27, 2012 · N572FE · Doug MD11F · Escape SlideSDR FDEA201110044278Duct · damagedLEVEL 1 " ENG 2 A-ICE OFF" ALERT DISPLAYED AFTER TAKE-OFF CREW DEBREIF, LEVEL ONE "ENG 2 A/I OFF" ALERT REMAINED ON DURING FLIGHT, EXTINGUISHED UPON LANDING. INSPECTED OVERHEAT ELEMENTS SURROUNDING NR 2 ENGINE A/I DUCT VISUALLY, NO FAULT FOUND. FOUND EVIDEOct 4, 2011 · N572FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201107052575Seat Track · damagedSEAT TRACK FOUND DAMAGED RT STA 735 - STA 999 X=-77.25. R & R IAW SRM 51-31-01, REV 46 FOR WORK DETAILS REFER TO SNRM N00252. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 5, 2011 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107012506Fitting · crackedVERTICAL STABILIZER RT NR 4 FWD BANJO FITTING WITH CRACK APPROX 3" LONG. FITTING AND REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 55-30-02 REPAIR 3 FIGURE 201 REV 46. REPAIR PARTS CARRIED OUT CHROMIC AND ANODIZE AS PER EA 1-5530-143611. REPAIR CLASSJul 1, 2011 · N572FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201106272443Frame · dentedCABIN LT STA 1741, L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201106272439Frame · dentedCABIN RT STATION 1661, L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112. INITIAL INSPECTION AT 14,500 AND REPETITIVE INSPECTION AT 9,500 USING HFEC METHOD.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201106272448Seat Track · damagedCABIN RT STA 795, SEAT TRACK FOUND DAMAGED. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 46. SEAT TRACK FABRICATED AS PER DRAWING AGA7083 REV D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106272442Frame · dentedCABIN LT STA 1721, L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201106272447Seat Track · corrodedCABIN RT STA 1331- 1341 X=-77.25 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 46. SEAT TRACK FABRICATED AS PER DRAWING AGA7083 REV A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106272446Frame · damagedCABIN LT STA 535, FRAME AT UPPER SUPPORT YOKE FOUND DAMAGED. REPAIRED AS PER DRAWING SG10530002 REV NEW. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201106272445Frame · damagedCABIN LT STA 535 FRAME AT LOWER SUPPORT YOKE FOUND DAMAGED. REPAIRED AS PER DRAWING SG10530002 REV NEW. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jun 27, 2011 · N572FE · Doug MD11F · Fuselage Main, Frame
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