N576FE

Service difficulty reports · 353

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 = 'N576FE' 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 FDEA201402250398Doubler · crackedRIGHT WING FIXED LE RIB DOUBLER FOUND CRACK AT XOS 789 DURING OTBD SLAT DRIVE CONTROL CABLE INSPECTION. RIB DOUBLER REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. DOUBLER FABRICATED IAW DWG ARB 3954 REVISION K. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REFeb 25, 2014 · N576FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201402190363Skin · crackedDURING RADIOGRAPHY INSPECTION ON TRANSVERSE SKIN SPLICE AT BS 1528, FOUND A CRACK INDICATION AT LONGERON 1L. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 19, 2014 · N576FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201402170345Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER FOUND CRACKED AT XOS 732. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 17, 2014 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201402160335Frame · chafedFRAME AT BS 535, LONGERON 24L FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 16, 2014 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201402160334Frame · dentedFRAME AT BS 1681, LONGERON 12R FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 16, 2014 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201402160333Frame · chafedFRAME AT BS 535, LONGERON 19R FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 16, 2014 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201402160332Frame · chafedFRAME BS 535, LONGERON 24R FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.Feb 16, 2014 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201206082168Landing Gear · malfunctionedEXTENDED MLG AT 8000 FT MSL/250KTS DURING CLIMBOUT DUE TO INCREASING BRAKE TEMP ON RT MLG. AFTER BRAKE TEMP STABILIZED, MLG WAS RETRACTED BEFORE SLOWING TO 230 KTS. NOSE GEAR LAST ONE TO STOW/LOCK DID NOT STOW LOCK UNTIL SLOW'G TO 240KTS. PERFORMED OPS TEJun 8, 2012 · N576FE · Doug MD11F · Main Landing GearSDR FDEA201203231075Fitting · corrodedLEFT INBD FLAP DRIVE LINK SUPPORT ATTACH BOLT HOLE AT FLAP SIDE FOUND WITH CORROSION. R & R IAW SRM 51-33-01 REV 49. & EA 1-5750-157164. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.Mar 23, 2012 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203211042Skin · crackedRT WING FIXED L/E NR 12 SLAT TRACK CUT-OUT EDGE CORNER CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 REPAIR 7, FIG 201, REV 48. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Mar 21, 2012 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201203201033Skin · crackedLOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 20, 2012 · N576FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201203191010Hinge Bracket · corrodedRT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. EXISTING DIAMETER 1.2553", FINAL DIA 1.256", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-157161 Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191012Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET PIVOT BORE FOUND CORRODED. REWORKED AS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 2.314", FINAL HOLE DIA METER 2.329", MAXIMUM HOLE DIAMETER 2.3135". REPAIR CARRIED OUT IAW EA 1-5750-157156, PART 1. REMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191009Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. EXISTING DIAMETER 1.217", FINAL DIAMETER 1.253", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191008Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03, REV 72. EXISTING DIAMETER 1.217", FINAL DIAMETER 1.253", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EAMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191007Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 1.226", FINAL DIAMETER 1.231", MAXIMUM ALLOWABLE DIAMETER 1.220", REPAIR ACCOMPLISHED EA 1-5Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191006Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED EA 1-5750-157156, PART 1, STEPS 1, 3, AND 6. EXISTING HOLE DIAMETER 0.590", FINAL DIAMETER 0.631", MAXIMUM ALLOWABLE DIAMETER 0.584", REPAIR BUSHING AND WASHER FAMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191005Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.584", FINAL DIAMETER 0.629", MAXIMUM ALLOWABLE DIAMETER 0.584", REPAIR ACCOMPLISHED IAWMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191004Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 1.222", FINAL DIAMETER 1.224", MAXIMUM ALLOWABLE DIAMETER 1.220", REPAIR ACCOMPLISMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191003Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE SPOTFACE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING THICKNESS 0.415", REMAINING THICKNESS 0.384". MATERIAL REMOVED: FWD 0.002"AND AFT 0.029", MMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191002Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER 0.705", FINAL DIAMETER 0.712", MAXIMUM ALLOWABLE DIAMETER 0.709", REPAIR ACCOMPLISHED IAMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191001Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET, LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER 0.7065", FINAL DIAMETER 0.712", MAXIMUM ALLOWABLE DIAMETER 0.709", REPAIR CARRIED OUT IAW Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191000Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. SURFACE REWORKED IAW REV 72. EXISTING THICKNESS UPPER 0.356", LOWER 0.355", REMAINING THICKNESS UPPER 0.353", LOWER 0.354". MATERIAL REMOVED: UPPER 0.002", LOWERMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203190999Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. SURFACE REWORKED IAW CMM 57-44-09, REV 72. EXISTING THICKNESS UPPER 0.467", LOWER 0.467", REMAINING THICKNESS UPPER 0.465", LOWER 0.464". MATERIAL REMOVED: UMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191011Hinge Bracket · corrodedRIGHT WING-INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. EXISTING DIAMETER 1.2515", FINAL DIAMETER 1.256", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191017Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 1.279", FINAL DIAMETER 1.285", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIMar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191016Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 1.251", FINAL DIAMETER 1.256", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191015Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET PIVOT BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 2.3115", FINAL DIAMETER 2.316", MAXIMUM ALLOWABLE DIAMETER 2.3135". REPAIR ACCOMPLISHED IAW EA 1-575Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191014Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING DIAMETER 0.708", FINAL DIAMETER 0.721", MAXIMUM ALLOWABLE DIAMETER 0.709". REPAIR CARRIED OUT IAW EA 1-5Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203191013Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER 0.393", LOWER 0.392", REMAINING THICKNESS UPPER 0.390", LOWER 0.389. MATERIAL REMOVED: UPPER 0.003"Mar 19, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203170992Skin · crackedSTRUCTURE AROUND FIVE FASTENER HOLES, FOUND TO HAVE CRACK INDICATIONS. FOUND DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS= 683.400 AND STA XORS= 713.600. REPAIR CARRIED OUT IAW EA 1-5710-Mar 17, 2012 · N576FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201203170991Bushing · wornRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 72 AND FOUND EXCEED LIMITS IAW CMM 57-44-09, REV 72. BORE MEASURED DIAMETER 1.222", MAXIMUM ALLOWABLE DIAMETER 1.220". Mar 17, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203170989Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET, LOWER OTBD STUD HOLE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.585", FINAL HOLE DIAMETER 0.610", MAXIMUM ALLOWABLE DIAMETER 0.584". REPAIRED IAW EA 1Mar 17, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203170988Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.592", FINAL HOLE DIAMETER 0.611", MAXIMUM ALLOWABLE DIAMETER 0.584". REPAIRED IAW EA 1-57Mar 17, 2012 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203170987Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET WING SIDE LOAD FITTING ATTACH BARREL NUT HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISTING HOLE DIAMETER 0.660", FINAL HOLE DIAMETER 0.669", ALLOWABLE HOLE DIAMETER 0.667Mar 17, 2012 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201203170986Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. AREA REWORKED IAW CMM 57-44-09, REV 72. EXISTING THICKNESS UPPER 0.406", LOWER 0.406", REMAINING THICKNESS UPPER 0.400", LOWER 0.400". REPAIRED IAW EA 1-5750-157158 Mar 17, 2012 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203160977Seat Track · corrodedRT STA 465, X= -47.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIGURE 201, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.Mar 16, 2012 · N576FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203160976Longeron · crackedLOWER FUSELAGE- CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 LT LONGERON 39 FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01 REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 11Mar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160975Longeron · crackedLOWER FUSELAGE- CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 RT LONGERON 49 FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01 REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 11Mar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160974Longeron · crackedLOWER FUSELAGE- CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 RT LONGERON 46 FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7116, REVISION D AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, Mar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160973Longeron · crackedLOWER FUSELAGE- CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 RT LONGERON 43 FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 114.Mar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160972Longeron · crackedLOWER FUSELAGE CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 RT LONGERON 39 FOUND CRACKED. RT R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7114, REV J AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REMar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160971Longeron · crackedLOWER FUSELAGE- CENTER CARGO COMPARTMENT APPROX BETWEEN STA 5-113 TO 1541 RT LONGERON 31 FOUND CRACKED. R & R WITH NEW FABRICATED LONGERON SPLICE IAW DWG A5A7112 REV D AND INSTALLED IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 11Mar 16, 2012 · N576FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201203160970Seat Track · corrodedRIGHT STA 815, X= -27.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 48 AND SRM 51-31-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 16, 2012 · N576FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203150948Skin · damagedFUSELAGE SKIN DAMAGED FORWARD OF CARGO DOOR CUT-OUT. CARRIED OUT REPAIR IAW SRM 53-00-15 REPAIR 8, FIG 202, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Mar 15, 2012 · N576FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201203150950Frame · dentedFRAME BS 1741 LONGERON 11 LEFT, FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 15, 2012 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201203150949Frame · dentedFRAME BS 1661 LONGERON 11 LEFT, FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIGURE 201, REV 48. REPAIR CLASSIFIED AS MAJOR, GMM 6-2-100, REV 114.Mar 15, 2012 · N576FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201203140930Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION. R & R IAW AMM 27-50-22-4, REV 72.0. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY IAW AMM 27-50-22-5, REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 114.Mar 14, 2012 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201203140929Vane · delaminatedRT WING INBD FLAP VANE UPPER SURFACE FOUND DELAMINATION. R & R IAW AMM 27-50-22 REVISION 72.0. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY IAW AMM 27-50-22-5, REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 114.Mar 14, 2012 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201112115243Warning Light · false activationCABIN DOOR FWD RT LEVEL 1 ALERT ON TAXI IN. SAFE/ARM HANDLE IN ARMED POSITION. PERFORMED DOOR WARNING ADJUSTMENT AND TEST FOR THE R1 DOOR REF AMM 52-70-00-5-0. TESTED GOOD. ACFT OK FOR SERVICE.Dec 11, 2011 · N576FE · Doug MD11F · Door Warning System
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