N588FE

Service difficulty reports · 346

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 = 'N588FE' 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 FDEA201608022746Seat Track · damagedCABIN LEFT, STA 1410, X=8.5, SEAT TRACK CROWN FOUND DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1310 TO STA 1410. X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 2, 2016 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606081872Stick Shaker · false activationSTICK SHAKER: AFTER TAKEOFF AND BEFORE FLAP RETRACTION, THE STICK SHAKER ACTIVATED FOR ABOUT 2 SECONDS. THE PDF SHOWED BOXED, SLATS, IN AMBER. ALTITUDE WAS ABOUT 300 FEET. NO CURRENT OR PREVIOUS LEG FAULTS IN FCC'S. PERFORMED OPERATION TEST OF SLAT POSITJun 8, 2016 · N588FE · Doug MD11F · Stall Warning SystemSDR FDEA201511143606Panel · abnormalON ARRIVAL FOUND NR 1 ENG PYLON MISSING PANEL 438EL. INSTALLED REPAIRED ATTACH BRACKET IAW SRM 51-35-01. INSTALLED NEW 438EL PANEL ON NR 1 ENG IAW MM 54-81-01-4-0. ACFT OK FOR SERVICE.Nov 14, 2015 · N588FE · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR FDEA201509232929Skin Panel · corrodedMINOR CORROSION ON UPPER SURFACE OF RT WING SKIN PANEL JUST INBD OF XRDS345, STRINGER 2, AFT THE NR 3 ENG. REPAIRED IAW SRM 57-00-01-1A, WITHIN LIMITS AS FAR AS MATERIAL REMOVED.Sep 23, 2015 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201507092187Sign · unsecureL1 SLIDING DOOR OVERHEAD EXIT SIGN IS HANGING DOWN. L1 DOOR SLIDING PANEL INOPERATIVE DUE TO EMER EXIT LIGHT REMOVED. REFERENCED & COMPLIED WITH AMM 25-23-23-2. RELEASED TO OPEN ITEM LIST EMER LIGHT WIRES CAPPED & STOWED. R & R L1 DOOR SLIDING CEILING PANELJul 9, 2015 · N588FE · Doug MD11F · Emergency EquipmentSDR FDEA201410213321Longeron Splice · crackedCRACK INDICATION FOUND DURING X-RAY INSPECTION AT BS 5-0, LONGERON SPLICE 1R FROM TWO EACH FASTENER HOLE. CRACK LENGTH APPROX 0.3 INCHES. AREA REMOVED IAW SRM 51-33- 01. NEW LONGERON SPLICE FABRICATED IAW DRAWING AEA7634 REVISION B. NEW LONGERON SPLICE INOct 21, 2014 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201410163197Longeron Splice · crackedCENTER ACCESSORY COMPARTMENT BS 6-87 LBL 51 LONGERON SPLICE FOUND CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 16, 2014 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201410133139Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER CRACKED XOS 608 - 703. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2014 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201410133137Skin · crackedLEFT WING FIXED EDGE BEADED DOUBLER CRACKED AT XOS 673 - 679. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 14. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Oct 13, 2014 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201410133136Skin · crackedLEFT WING FIXED LE BEADED DOUBLER CRACKED AT XOS 626 - 629. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Oct 13, 2014 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201410133132Cargo Track · corrodedCABIN MAIN DECK CARGO TRACK BS 1581 X -8.5 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2014 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410133131Seat Track · crackedCABIN MAIN DECK CARGO TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2014 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410123121Skin · crackedRIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUT OUT XOS 464 - 470 FOUND CRACKED AT OTBD CORNER. REPAIRED IAW SRM 57-40-01, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Oct 12, 2014 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201405060953Smoke Detector · failedGOT INTERMITTENT CABIN SMOKE LEVEL 3 ALERT WITH TRITONE ALERT WAS ON 2 TIMES FOR ABOUT 2 SECONDS. LANDED UNEVENTFULLY & FIRE DEPT SAID NO INDICATION OF FIRE OR HEAT. FOUND NR 9 SMOKE DETECTOR FAILED. R & R NR 9 SMOKE DETECTOR & TESTED GOOD IAW AMM 26-15-01May 6, 2014 · N588FE · Doug MD11F · Smoke DetectionSDR FDEA201311202831Panel · missingFOUND A PANEL MISSING ON NR 3 ENG INBD, PANEL MPN AUB7726-501. SS OIL 20NOV13 09:05 SYD U NO RESTRICTION IAW1-5480-T0304174 NR 3 ENG PYLON PANEL 488EL MISSING FROM INBD SIDE. OK TO CONTINUE IAW EA 1-5480-T0304174. COMPLIED WITH PT1 OF EA 1-5480-T0304174 C0Nov 20, 2013 · N588FE · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201305261092Bracket · tornAFTER TAKEOFF HAD UNSAFE LT GEAR UP INDICATION. COMPLIED WITH CHECKLIST AND RECYCLED THE GEAR. HAD A SECOND UNSAFE GEAR UP INDICATION ON BOTH INDICATORS. NO FUEL WAS DUMPED. FOUND AFT MLG TRUCK HOSE SUPPORT BRACKET BROKEN. HOSE/HARNESS SUPPORT AND ANTI-SKMay 26, 2013 · N588FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201301280208Relay · failedAFTER TAKEOFF RECEIVED ACFT TIE 1 OFF ALERT. WITH NR 1 IDG DISCONNECTED, LOST LT BUSS AND MOST DISPLAYS ON CAPTS SIDE, EMERGENCY POWER CAME ON. ADG WAS DEPLOYED TO CHARGE BATTERY. FOUND BTR-1/INTFC FAULT CODE. PERFORMED TROUBLESHOOTING IAW FIM 24-20-37, Jan 28, 2013 · N588FE · Doug MD11F · AC Power Distribution SystemSDR FDEA201211154037Support Fitting · damagedLEFT WING NR 8 L/E SLAT INBD SUPPORT FITTING FWD HOLE OTBD SIDE SURFACE FOUND STEPPED. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GENERAL MM 6-2-100, REV 115.Nov 15, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211144006Support Fitting · chafedLEFT WING NR 8 L/E SLAT, INBD SUPPORT FITTING, AFT HOLE, BOTH SIDES SURFACES FOUND CHAFED. FOUND DURING LT OTBD SLAT DRIVE CABLES TENSION CHECK. SUPPORT FITTING REMOVED IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50. HOLES PICKED UP ON NEW SUPPORT FITTING IAW SNov 14, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211093918Skin · crackedLEFT WING INBD FLAP UPPER SKIN PANEL ASSY CRACKED AT XIFH 171.3. REPAIRED IAW SRM 57-00-01 REPAIR 1 FIGURE 201 REVISION 50 AND EA 1-5750-163526Nov 9, 2012 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211093915Seat Track · corrodedMAIN DECK SEAT TRACK CLIP NUT HOLE AT BS 5-55, "X" = -107.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR Nov 9, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211083909Splice · crackedCENTER LANDING GEAR WHEEL WELL RT UPPER FORWARD SPLICE JOINT FOUND CRACKED. SPLICE REMOVED AND REPLACED WITH WITH NEW SPLICE IAW SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211083908Slat Track · crackedRT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Leading Edge DevicesSDR FDEA201211083907Doubler · crackedLEFT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 203, REPAIR 15, TYPE A, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM REVISION 115.Nov 8, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211073896Seat Track · corrodedMAIN DECK SEAT TRACK BS 1372, "X" = -8.5 FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 50. NEW SEAT TRACK SEGMENT REWORKED IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. NEW SEAT TRACK SEGMENT INSTALLED IAW SRM 53-00-52, FIG 201, RENov 7, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211073895Seat Track · corrodedMAIN DECK SEAT TRACK BS 1861, "X" = -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201 REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR CLANov 7, 2012 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211073892Frame · dentedDENT FOUND FRAME AT BS 1741, L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211073891Frame · dentedDENT FOUND AT RT SIDE FRAME AT BS 1761, NEAR L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211073890Frame · dentedDENT FOUND ON RT SIDE OF CABIN FUSELAGE FRAME AT BS 1641, NEAR L11R. REPAIR CARRIED OUT IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 7, 2012 · N588FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201211063867Door Frame · crackedUPPER CENTER CARGO DOOR FRAME, BS 1743 BETWEEN LONGERON 28 - 29R, "X" = 106 FOUND CRACKED. APPROX 1.25" IN LENGTH. REPAIRED IAW EA 1-5310-163524. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211063863Spar Cap · crackedRT WING T/E REAR SPAR LOWER CAP XORS 433 FOUND CRACKED. REMOVED AND REPLACED WITH NEW SILL AS PER SRM 51-34-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Wing SparSDR FDEA201211063865Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211063878Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L44L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RENov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063877Longeron Splice · crackedCENTER CARGO BAY BS 5-123 L45R LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RENov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063876Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND CRACK INDICATIONS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MANov 6, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211063874Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND 713.6. FOUND CRACKED INDICATION AT FASTENER HOLES. FASTENER HOLES CRACKED AT RIGHT WING LOWER SKIN ACCESS DOOR COUTOUT REPAIRED IAW SRM 5Nov 6, 2012 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211063872Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L46L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPANov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063871Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L41L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7115 REVISION D. RNov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063870Longeron Splice · crackedCENTER CARGO BS BS 5-123, LONGERON 40L LONGEORN SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISIONNov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063869Longeron Fitting · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 44 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063868Longeron Splice · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 37 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 50. SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J.Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211063866Web · crackedLEFT WING INBD FLAP OTBD EDGE CENTER WEB FOUND CRACKED. CRACKED WEB REMOVED AS PER SRM 51-35-01 REVISION 50. NEW WEB FABRICATED IAW DRAWING ARC2305 REVISION C. NEW FABRICATED WEB INSTALLED IAW SRM 51-35-01 REVISION 50 AND EA 1-5750-163519. FLAP OPS TEST Nov 6, 2012 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201211063858Beam · brokenR3 DOOR NR 7 BEAM FOUND BROKEN. BEAM REMOVED IAW SRM 51-31-01 REVISION 50. HOLES PICKED UP ON NEW BEAM IAW SRM 51-31-01 REVISION 50. NEW BEAM INSTALLED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.Nov 6, 2012 · N588FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201206082170Tie Rod · brokenON GEAR RETRACTION AFTER T/O, THE ACFT HAD SEVERE VIBRATION. VIBRATION DIMINISHED AFTER ACFT WAS SLOWED AND GEAR EXTENDED. LANDING WAS NORMAL. NO FUEL DUMP. NO UNSAFE GEAR INDICATIONS. FOUND RT NLG DOOR TIE ROD END BROKE, REMOVED, REPLACED AND ADJUSTEDJun 8, 2012 · N588FE · Doug MD11F · Landing Gear Door Retract SectionSDR FDEA201205272003Control Valve · inoperativeTOUCHDOWN FELT NORMAL, NO HARD PULL, BUT AS LANDING ROLL PROGRESSED IT SEEMED TO TAKE AN INCREASING AMOUNT OF RUDDER IN ORDER TO STAY ON RUNNWAY CENTERLINE W/ WINDS 40 DEG LT OF CENTERLINE AT 12 KNOTS. WHEN I DID GET ON THE BRAKES THEY GRABBED SIGNIFICANTLMay 27, 2012 · N588FE · Doug MD11F · Brake Anti-Skid SectionSDR FDEA201201040013Oil System · leakingCRUISE FLIGHT NR 1 OIL QTY DECREASING, NOTICED AT 8 QTS REMAINING. AT 5 QTS REMAINING PLACED NR1 ENG AT IDLE THIS SIGNIFICANTLY SLOWED THE RATE OF DEPLETION 2 HRS LATER OIL QTY DECREASED TO 0 WITH A CORESPONDING DROP IN PRESSURE TO 15 PSI. SHUTDOWN NR 1 ENJan 4, 2012 · N588FE · Doug MD11F · Turbine Engine Oil SystemSDR FDEA201111255025Power Supply · dischargedDURING EMERGENCY LIGHT TEST RECEIVED A LEVEL 1, EMERGENCY LIGHT BATTERY 1 LOW ALERT. R & R POWER SUPPLY PER AMM 33-51-01-4-0. TESTED OK.Nov 25, 2011 · N588FE · Doug MD11F · Emergency LightingSDR FDEA201109213993Oven · odorOVEN EMITTED A STRONG BURNING ODOR. LOOSE PARTS (METAL GRATE AND SCREWS) FOUND STACKED ASIDE THE OVEN. CLEANED OVEN IAW SMP, RAN OVEN; OVEN WORKED NORMALLY AND DID NOT SMELL. ACFT OK FOR SERVICE. FINAL CLOSED.Sep 21, 2011 · N588FE · Doug MD11F · Buffet/GalleysSDR FDEA201105181869Bulb · failedDURING PREFLIGHT CHECK FOUND LH DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOP. REPLACED PRESS TO TEST SW BULB AND REMOTE PRESS INDICATION OPS TEST PASSED PER MM25-61-04-4-0May 18, 2011 · N588FE · Doug MD11F · Escape SlideSDR FDEA201104251619Structure · departedAFTER DEPARTURE, WEST OF THE AIRPORT BY APPROX 20NM OVER THE WATER, FELT A SHARP BUMP THAT FELT LIKE WAKE TURBULENCE CLIMBING THROUGH APPROX 14000 FT AND 320 KTS UPON LANDING, COWLING ON NR 2 ENGINE JUST BEHIND WHERE THE REVERSER SEPARATES IS COMPLETELY MISSApr 25, 2011 · N588FE · Doug MD11F · Nacelle/Pylon, Main Frame
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