N574FE

Service difficulty reports · 611

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 = 'N574FE' 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 FDEA201401180135Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE OTBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3.Jan 18, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401180134Hinge Fitting · wornRIGHT WING OTBD FLAP, OTBD FWD HINGE INBD ACTUATOR BUSHING WORN. DAMAGE REMOVED IAW CMM 20-20-07 REV 78. . BUSHING & WASHER FABRICATED & INSTALLED IAW EA 1-5750-87641C PT2 STEP 2, 2B, 3, 4 & 5.Jan 18, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401180133Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE OTBD ACTUATOR HOLE. WORN BUSHING ON OTBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED IAW EA 1-5750-87638C PART 2 TITLE, WINGS - TE & TE DEVICESJan 18, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401180132Hinge Fitting · wornRIGHT WING OTBD FLAP, INBD FWD HINGE INBD ACTUATOR HOLE. WORN BUSHING ON INBD ACTUATOR HOLE AT RT WING OTBD FLAP INBD FWD HINGE. REMOVED IAW MD11 CMM 20-20-07 REV 78. NEW BUSHING & WASHER FABRICATED & INSTALLED IAW 1-5750-87638C PART 2 TITLE, WINGS - TE & TJan 18, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401100081Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-09 REVISION 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 10, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401100080Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING SPOT FACE FOUND CORRODED. REWORKED IAW CMM 57-44-08 REV 78. NEW SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.Jan 10, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060041Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2,2B, 3, 4 & 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060040Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP OTBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. REPAIRED IAW EA 1-5750-87641C PT2 STEP 2, 3, & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVIJan 6, 2014 · N574FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201401060039Hinge Fitting · damagedRIGHT WING OTBD FLAP OTBD FWD HINGE PIVOT HOLE DIAMETER FOUND OUT OF LIMITS AFTER REPAIR BUSHING REMOVAL. HINGE PIVOT BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87641C PT2 STEP 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060031Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201401060030Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2,2A, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060027Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING BARREL NUT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C P2 STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060026Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C STEP 2, 3 AND 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201401060025Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW EA 1-5750-87641 REV C PART 2 STEP 2,3 &4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060043Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE INBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. BUSHING AND WASHER FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2,2B1,Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060037Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060036Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2 STEPS 2 & 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060035Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIRED IAW CMM 57-44-08 REV 78 AND EA 1-5750-87638C PART 2 FIGURE 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060029Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060028Hinge Fitting · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT & AFT SPOT FACE FOUND CORRODED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-09 REVISION 77. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV. 77. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060046Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE OTBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2, 3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060045Hinge Fitting · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87634B P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060044Hinge Fitting · corrodedLEFT WING INBD FLAP OTBD AFT HINGE INBD PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REV 78. REPAIRED IAW EA 1-5750-87633A P2 STEP 2,3 & 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060042Hinge Fitting · corrodedDURING FPI ACCOMPLISHMENT, RT WING OTBD FLAP INBD FWD HINGE OTBD ACTUATOR MOUNT FOUND CORRODED IN BORE. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2. REPAIR CLASSIFIEDJan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060038Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE PIVOT FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REV 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-87638C PART 2, STEP 2 AND STEP 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100Jan 6, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401060047Floor Panel · damagedL1 DOOR AREA, FOUND FLOOR PANEL 227AF SPONGY. FLOOR PANEL REMOVED IAW AMM 53-21-04 REVISION 78. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION K AND INSTALLED IAW AMM 53-21-04 REVISION 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 6, 2014 · N574FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201401030011Skin · crackedCRACK INDICATION FOUND APPROXIMATELY 0.3 INCHES IN LENGTH ON FUSELAGE SKIN DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT BS 695 LONGERON 50L. REPAIRED IAW SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 53 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119Jan 3, 2014 · N574FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201401030013Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT SPOT FACES FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REV 78. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 78. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 119.Jan 3, 2014 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201401030012Longeron Splice · crackedCENTER CARGO BAY BETWEEN BS 1661 & 1681, LONGERON SPLICE 29 RT CRACKED. NEW SPLICE FABRICATED IAW DRAWING AFA7830. DAMAGED LONGERON SPLICE REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 3, 2014 · N574FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201401030014Skin · crackedRIGHT WING FIXED LE LOWER, FOUND CRACKED AT SLAT TRACK NR 11, CUTOUT AREA SKIN. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.Jan 3, 2014 · N574FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201401020002Support Fitting · crackedMAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING DAMAGED. NR 1 HOLE REAMED TO 0.562 INCHES. HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED FOUND CRACK INDICATION STILL EXIST, APPROXIMATELY 0.040 INCH. SUPPORT FITTING REMOVED AND REPLACED IAW SJan 2, 2014 · N574FE · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA201312313073Wedge · delaminatedLEFT WING OTBD FLAP, INBD TE WEDGE FOUND DELAMINATED AT XOFH 458.74 TO XOFH 465.24. REPAIRED IAW EA 1-5750-T0305303 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119Dec 31, 2013 · N574FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201310182555Seal · unsecurePASSING FL 220, HEARD A LOUD BANG AND AIR OUT FLOW IN AVIONICS BAY. CABIN PRESSURE CONTINUED A SLOW CLIMB. AIR TURN BACK. ACFT UNABLE TO HOLD PRESSURE. LANDED WITHOUT INCIDENT. FOUND AVIONICS DOOR SEAL HANGING OUT. SEATED DOOR SEAL AND OPS CHECKED DOOROct 18, 2013 · N574FE · Doug MD11F · Electrical/Electronic Compartment DoorsSDR FDEA201307281674Power Supply · failedDURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS TEST WILL NOT PASS. REPLACED EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-01-4 , TESTED NORMAL.Jul 28, 2013 · N574FE · Doug MD11F · Emergency LightingSDR FDEA201307251663Warning Light · false activationDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.Jul 25, 2013 · N574FE · Doug MD11F · Emergency LightingSDR FDEA201307241672Power Supply · inoperativeDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.Jul 24, 2013 · N574FE · Doug MD11F · Emergency LightingSDR FDEA201304020701Duct · tornAFTER TAKE OFF "ICE DET SINGLE" LEVEL 1 ALERT FOLLOWED BY "AIR SYS 1 OFF" LVL 1 AND LVL 3 MANIFOLD FAIL FOR SYS 1. NO ANTI ICE WING OR ENG WAS ON. LEVEL 3 MANIFOLD FAIL WENT OUT AS AS THROTTLE WAS RETARDED. REPLACED DUCT.Apr 2, 2013 · N574FE · Doug MD11F · Ice/Rain Protection SystemSDR FDEA201209273478Static Wick · missingDURING CLIMBOUT, WE WERE INSTRUCTED TO RETURN TO DEPARTURE DUE TO POSSIBLE DAMAGE DURING PUSHBACK. LEFT UPPER WINGLET MISSING STATIC WICKS. REPAIRED L/H UPPER WINGLET CAP PER PART 2 OF EA 1-5720-162680. INSTALLED UPPER WINGLET CAP IAW MM 57-31-01-4 A/C OSep 27, 2012 · N574FE · Doug MD11F · Pitot/Static SystemSDR FDEA201202030443Angle · corrodedAFT CARGO DOOR AFT CUTOUT ANGLE FOUND WITH SURFACE CORROSIONS. ANGLE REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. INITIAL INSPECTION AT 18300 FC AND REPEAT INSPECTION AT 1250 FC PER ALI 53-10-06 REVISION 15. REPAIR CLASSIFIED AS MAJOR ASFeb 3, 2012 · N574FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201202030444Skin · corrodedUPON REMOVAL OF R3 DOOR SILL PLATE FOR REPAIR ACCESS FORWARD LOWER DOOR CUTOUT INTERIOR SKIN FOUND CORRODED.Feb 3, 2012 · N574FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201201300379Skin · corrodedAFTER REMOVAL OF APU EXHAUST DOOR RT FUSELAGE SKIN AT STA 2120 BENEATH APU EXHAUST DOOR FOUND CORROSION.Jan 30, 2012 · N574FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201201270352Door Frame · misrepairedFORWARD CARGO DOOR FRAME, BS 897 BETWEEN LONGERON 38 AND LONGERON 40R MISREPAIRED. CARRIED OUT REPAIR AS PER SRM 53-00-15 FIGURE 202 REPAIR 1 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Jan 27, 2012 · N574FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201201270350Floor Support · corrodedLEFT STA 421, X= 28 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT FABRICATED AS PER DRAWING ABA8303 REVISION A. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Jan 27, 2012 · N574FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201201270349Seat Track · corrodedREMOVAL OF FLOOR PANEL LT STATION 5-103, X= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Jan 27, 2012 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201270348Hinge · crackedRT MLG DOOR CENTER HINGE CRACKED. HINGE REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. R/H MAIN GEARWELL DOOR REMOVED AND REINSTALLED AS PER AMM 32-14-20-4 REVION 70.1. OPERATION CHECK CARRIED OUT SATISFACTOTY AS PER AMM 32- 14-20-220-801 REVISIONJan 27, 2012 · N574FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201201270353Skin · damagedAFT LOWER RUDDER SKIN FORWARD LOWER CORNER FOUND DAMAGED. REPAIRED IAW SRM 55-40-01, FIGURE 201, REV 48. EA 1-5540-156837. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 27, 2012 · N574FE · Doug MD11F · Rudder, Plate/SkinSDR FDEA201201260341Skin · misrepairedLT WING FIX L/E LOWER SKIN AT XW 344 MISREPAIRED. REPAIRED IAW DWG ARB1230, REV CEO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 26, 2012 · N574FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201201260343Skin Splice · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT TRANSVERSE SKIN SPLICE, STATION 5-0, LONGERON 4LT ON THE CENTER ROW FASTENER NR 4 TOWARD NR 5 FASTENER APPROX .5" LONG COUNT FROM FORWARD. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. SJan 26, 2012 · N574FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201201260342Longeron · crackedRIGHT BS 1299, LONGERON 27, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Jan 26, 2012 · N574FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201201260340Seat Track · corrodedRIGHT STA 1541 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 48. SEAT TRACK REWORKED AS PER DRAWING SP11530506 REVISION NEW. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Jan 26, 2012 · N574FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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