N522FE

Service difficulty reports · 338

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 = 'N522FE' 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 FDEA201308221999Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104703C PART 2 STEPS 1,2, AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.Aug 22, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308222000Hinge Fitting · corrodedLEFT WING INBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE HAS SURFACE CORROSION. REPAIRED IAW EA 1-5750-104702C PART 2 STEPS 1,2 AND 4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REVISION 117.Aug 22, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308221998Hinge · corrodedLEFT WING OTBD FLAP INBD AFT HINGE PIVOT INBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-04 REVISION 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0302073 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 117.Aug 22, 2013 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308191960Hinge Fitting · damagedLT WING INBD FLAP, OTBD AFT (HINGE SIDE) PIVOT INBD BORE FOUND DAMAGED AFTER BUSHING REMOVAL. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA 1-5750-104706D, PART 2, STEPS 1,2,3 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308191959Hinge Fitting · damagedLT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BORE FOUND, EXCEEDED LIMIT AFTER BUSHING REMOVAL. REPAIRED IAW EA 1-5750-104706D, PART 2, STEPS 1, 2, 4 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308191958Hinge Fitting · corrodedLT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104702C, PART 2, STEPS 1, 2 AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308191957Hinge Fitting · corrodedRT WING INBD FLAP OTBD FWD (WING SIDE) HINGE PIVOT CORROSION. FOUND EXCEEDED LIMIT IAW CMM 57-44-07, REV 76. REPAIRED IAW EA 1-5750-104703C, PART 2, STEPS 1, 2, AND 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 19, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181946Skin · crackedFASTENER HOLES FOUND CRACKED DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED IAW EA 1-5710-T0302030 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308181947Skin · crackedFASTENER HOLES FOUND CRACKED DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER EA 1-5710-T0302029 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116Aug 18, 2013 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308181945Bulkhead · canningCENTER LANDING GEAR WHEEL WELL - OIL CANNING FOUND AT RT KEEL BEAM WEB X=31.50, Y=1435 , 43" ABOVE FWD DOOR HINGE LINE. OIL CANNING MEASURED 0.215", MAXIMUM ALLOWABLE 0.19". REPAIRED IAW EA 1-5310-T0301907. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 18, 2013 · N522FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201308181944Hinge Fitting · corrodedRT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA1-5750-104705D, PART 2, STEPS 1, 2, 3 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308181943Hinge Fitting · corrodedRIGHT WING INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BORE HAS CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. REPAIRED IAW EA 1-5750-104705, PART 2, STEPS 1, 2, 4 AND 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308181942Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181941Hinge Fitting · corrodedRT WING OTBD FLAP, INBOD FWD (WING SIDE) HINGE LOWER MOUNT INBD HOLE HAS SURFACE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0302028A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181940Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT HOLES SURFACE CORROSION. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09, REV 76. REPAIR CLASSIFIED MINOR GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181939Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL NUT LOWER BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181938Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT UPPER BORE CORRODED. REPAIRHED IAW EA 1-5750-T0302072, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181937Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. REPAIRED IAW EA 1-5750-T0302026, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181936Structure · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181935Hinge · corrodedLT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORROSION. FOUND EXCEEDED LIMITS IAW CMM 57-44- 09, REV 76. REPAIRED IAW EA 1-5750-T0302070A, PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 117Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181934Hinge · corrodedLT WING OTBD FLAP, INBD FWD( WING SIDE) HINGE PIVOT HOLE BORE CORROSION. FOUND EXCEEDED LIMITS. REPAIRED IAW EA 1-5750-T0302026. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308181933Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. REPAIRED IAW CMM.Aug 18, 2013 · N522FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201308151893Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123 LONGERON 34RT. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 15, 2013 · N522FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308151895Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123, LONGERON 39R. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 15, 2013 · N522FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308151897Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-123, LONGERON 49L. R & R WITH NEW FABRICATED SPLICE IAW SRM 51-33-01, REVISION 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 15, 2013 · N522FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308151896Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-123 LONGERON 49R. R & R WITH NEW FABRICATED SPLICE SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 15, 2013 · N522FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308151894Longeron Splice · crackedCENTER CARGO LONGERON SPLICE CRACKED AT BS 5-123 LONGERON 37R. R & R IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 15, 2013 · N522FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201308141876Strap · crackedRT WING LOWER SURFACE L/E PANEL 626GB CUTOUT FOUND LOWER STRAP CRACKED XOS 993.237. REPAIRED IAW SRM 57-40-03, REPAIR 1, FIG 201, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 14, 2013 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308141874Skin · crackedRT WING LOWER SURFACE L/E NR 6 SLAT INBD COMMON IDLE TRACK CUTOUT FOUND SKIN CRACKED AT XOS 775. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 14, 2013 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308141879Slat Track · crackedLT WING FIXED L/E AT NR 18 SLAT TRACK CUTOUT FOUND CRACKED AT XOS 1116.032. REPAIRED IAW EA NR 1-5730-T0301989 REV A PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 117.Aug 14, 2013 · N522FE · Doug MD11F · Leading Edge DevicesSDR FDEA201308141875Seat Track · corrodedMAIN DECK BS 1600, X=-8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1531 TO 1631 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 53. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 14, 2013 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308141873Access Panel · crackedRT WING LOWER SURFACE L/E REFUEL PANEL CUTOUT FOUND CRACKED AT FWD INBD CORNER AT XOS 602. REPAIRED IAW SRM 57-40-02, FIG. 202, REPAIR 7, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 14, 2013 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308131851Seat Track · corrodedMAIN DECK BS 750, X=8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 745 - 834 IAW SRM 53-00-52, FIG 201. REPAIR 1 REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 13, 2013 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308131849Seat Track · corrodedMAIN DECK BS 1080, X=8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1069 TO 1129 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116Aug 13, 2013 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308131853Door Frame · crackedMAIN DECK R3 DOOR AFT FRAME LOWER CORNER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 116.Aug 13, 2013 · N522FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201308131852Panel · delaminatedRT WING NR 1 SPOILER PANEL UPPER SURFACE FOUND THREE LOCATIONS DELAMINATED. REPAIRED IAW EA 1-5750-T0302163, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Aug 13, 2013 · N522FE · Doug MD11F · SpoilersSDR FDEA201308131850Door Frame · crackedMAIN DECK R3 DOOR FORWARD FRAME LOWER CORNER WEB FOUND ONE CRACK. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 13, 2013 · N522FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201308131848Trunnion · crackedNLG LT TRUNNION FITTING FOUND CRACKED AT STATION Y=595. REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 13, 2013 · N522FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201305151004Coalescer Bag · dirtyIN HIGH HUMIDITY CONDITIONS, APPROACHING GATE, COCKPIT FILLED WITH VISIBLE MOISTURE AND GOT MOMENTARY CABIN AIR SMOKE LIGHT AND WARNINGS. (NR 2 ENG WAS SHUTDOWN). R & R THE NR 1 WATER SEPARATOR COALESCER ASSY IAW AMM 21-54-05-01. OPS TEST NORMAL IAW AMM 21May 15, 2013 · N522FE · Doug MD11F · Humidity Control SystemSDR FDEA201301250184Control Unit · burnedCONTROL UNIT REMOVED FROM ACFT DUE TO THE PUNGENT ELECTRICAL ODOR EMANATING FROM IT. INSTALLED ABSCU. OPS TEST NORMAL, REF MM 32-48-01-4.Jan 25, 2013 · N522FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201212064257Structure · damagedLEFT WINGLET DAMAGED & AFT LIGHT ASSY. WINGLET REPLACED & ACFT RETURNED TO SERVICE.Dec 6, 2012 · N522FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201203231086Battery Pack · inoperativeL1 DOOR PRESS TO TEST SWITCH FOR EVACUATION SLIDE BOTTLE PRESSURE CHECK, INOPERATIVE. FOUND NO POWER BEFORE SWITCH. R & R BATTERIES, PERFORMED TEST, LIGHT COMES ON IAW MM 25-61-15-4. OPS CHECKED OK.Mar 23, 2012 · N522FE · Doug MD11F · Escape SlideSDR FDEA201109073740Spar · crackedVERTICAL STABILIZER LEFT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 7, 2011 · N522FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201109073739Spar · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Sep 7, 2011 · N522FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201109073738Seat Track · corrodedMAIN DECK CARGO COMPARTMENT - WHILE CARRYING INSPECTION AS PER WORKCARD ITEM 1, FOUND SEAT TRACK AT STA.5-0, X=-27.5 WITH CORROSION ON CHANNEL. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA. 5-0 TO STA. 5-43 X= -27.5 AS PER SRM 53-00-52 FIG. 201 RSep 7, 2011 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109023632Seat Track · corrodedMAIN DECK CARGO COMPARTMENT WHILE CARRYING OUT INSPECTION IAW WORKCARD ITEM 2, FOUND SEAT TRACK AT STA 6-10, X= 8.5 WITH CORROSION ON THE CHANNEL SURFACE. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV.47 REPAIR CLASSIFSep 2, 2011 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108313597Vane · delaminatedLEFT INBD VANE LOWER SURFACE FOUND DELAMINATED. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV.70. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV. 70. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV.112.Aug 31, 2011 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201108313596Vane · delaminatedRT INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV 70.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV.70.0. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Aug 31, 2011 · N522FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201108313595Skin · crackedRIGHT WING SLAT NR 14 TRACK CUT OUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02 REV 47 FIG.201 REPAIR 7. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Aug 31, 2011 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201012154688Shoulder Belt · malfunctionedCAPTS LT SHOULDER HARNESS WILL NOT RELEASE. PERFORMED OPS OF CAPT'S SHOULDER HARNESS IAW AMM 25-11-04-4-0. NO DEFECTS NOTED AT THIS TIME. NO HISTORY IN LAST 30 DAYS. (CLOSED)Dec 15, 2010 · N522FE · Doug MD11F · Emergency Equipment
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