N587FE

Service difficulty reports · 399

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 = 'N587FE' 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 FDEA201202230658Bushing · wornRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REPAIRED IAW EA 1-5750-156844 PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMFeb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202230655Hinge Bracket · damagedRIGHT WING INBD FLAP OTBD HINGE BRACKET PIVOT OTBD BORE FOUND SCRATCHED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.256", FINAL DIAMETER 1.2825", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA.1-5750-156846, STEFeb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202230653Hinge Bracket · damagedRT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.3275", FINAL DIAMETER 1.3355", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA 1-5750-156846, STEPFeb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202230652Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CONTACT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841 PART 1, REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Feb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202230651Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1-5750-156844, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-Feb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202230649Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Feb 23, 2012 · N587FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201202220640Spar · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02 FIGURE 201 REVISION 48 AND SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Feb 22, 2012 · N587FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201202220636Tee Fitting · crackedCENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT CHORD CRACKED NEAR DETRIM ACTUATOR AREA. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.Feb 22, 2012 · N587FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201202220639Longeron Splice · crackedDUTING X-RAY INSPECTION ON TRANSVERSE SKIN, FOUND CRACKED AT STA 5-0, LONGERON 7L FWD SIDE OF CENTER SPLICE 3RD TO 4TH FASTENER. R & R IAW SRM 51-33-01, REV 48. NEW LONGERON SPLICE FABRICATED IAW DWG AEA7633 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1Feb 22, 2012 · N587FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201202220638Longeron Splice · crackedBS 5-123 LONGERON 24LT SPLICE FITTING FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7112 REV D. SPLICE R & R IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Feb 22, 2012 · N587FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201202220637Access Panel · corrodedLEFT WING INBD T/E ACCESS PANEL 541JB ATTACHMENT SUPPORT TEE FOUND SURFACE CORROSION ON SEVERAL LOCATION. R & R IAW EA 1-5710-157949, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.Feb 22, 2012 · N587FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201201110079Fastener · looseNR 2 ENGINE NOSE COWL HAS NUMEROUS RIVETS LOOSE IN NOSE LIP SKIN. NOSE COWL REPLACED.Jan 11, 2012 · N587FE · Doug MD11F · Nacelle/Pylon, Main FrameSDR FDEA201201100076Skin · crackedRIGHT INBD UPPER SKIN CRACKED. REPAIRED IAW EA 1-5750-157590, PART 1.Jan 10, 2012 · N587FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201110054304Handle · unsecureL1 DOOR MANUAL LIFTING HANDLE IS NOT SECURELY ATTACHED ON THE FORWARD SIDE ADJUSTED SPRING AT L1 DOOR FWD LIFTING HANDLE FWD SIDE IAW IN REF OF 52-11-00-0-0. SYS CK NML. FINAL CLOSED.Oct 5, 2011 · N587FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201108303577Battery · inoperativeTRANSIT CHK FOUND LT ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS INOPERATIVE. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD IAW AMM 25-23-07-4-1 AND 25-61-15-4-0. OK FOR SERVICE.Aug 30, 2011 · N587FE · Doug MD11F · Escape SlideSDR FDEA201105191883Engine · malfunctionedTAKING OFF ON 30R AT APPROXIMATELY 1000FT EXPERIENCED A NR 2 ENGINE EGT OVERHEAT 966 DEGREES AND LARGE BANGING SOUND (COMPRESSOR STALL). PULLED NR 2 THROTTLE TO IDLE IMMEDIATELY. EGT CAMEBACK TO NORMAL (740-760 ) AND COMPRESSOR STALL STOPPED. AFTER THROMay 19, 2011 · N587FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201011244484Battery Pack · inoperativeLEVEL 1 'EMER LT BAT 6 LO' ALERT DISPLAYED DURING EMERGENCY LIGHT TEST. R & R AFT EMERGENCY LIGHT BATTERY PACK (U1-2070) REF AMM 33-51-01-4-0. OPS CHECKS NORMAL.Nov 24, 2010 · N587FE · Doug MD11F · Emergency LightingSDR FDEA201011154375Fan Blade · bentDURING TAKEOFF GOT "ICE DETECTED" FOLLOWED BY EVM COMP NR 3 ENG 5.6 WITH AMBER BOX. CREW FELT THE EXCESSIVE VIBRATION. ON ARRIVAL INSPECT FAN AREA AND FOUND 2 FAN BLADE BENT. FOUND ALSO SLIGHT REMAIN OF BLOOD AROUND THE ICE DECTECTOR AND NEAR THE OUTER FAN ANov 15, 2010 · N587FE · Doug MD11F · Turbine Engine Compressor SectionSDR FDEA201003040635Door Frame · corrodedMAIN DECK CARGO - L3 DOOR CUTOUT AFT JAMB MID SECTION FOUND CORROSION. MAIN DECK CARGO - L3 DOOR CUTOUT AFT JAMB MID SECTION REPAIRED AS PER SRM 53-40- 15 FIGURE 201 REPAIR 4, REVISION 42. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100 REVISION 109.Mar 4, 2010 · N587FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201002250520Fuel Tank · corrodedCENTER TANK AFT UPPER SURFACE APPROX STA 1229, X = 17 FOUND WITH SURFACE CORROSION. MAIN DECK CARGO -CTR TANK AFT UPPER SURFACE APPROX STA 1229, X =17, SURFACE CORROSION REPAIRED IAW EA 1-5710-132348. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 109.Feb 25, 2010 · N587FE · Doug MD11F · Fuel StorageSDR FDEA201002250519Fuel Tank · corrodedCENTER TANK AFT UPPER SURFACE APPROX STA 1229, X = -45. FOUND SEVERAL LOCATIONS WITH SURFACE CORROSION. MAIN DECK CARGO - CTR TANK AFT UPPER SURFACE APPROX STA 1229, X = -45, SURFACE CORROSION REPAIRED IAW EA 1-5710-132348. REPAIR CLASSIFIED MINOR IAW GMFeb 25, 2010 · N587FE · Doug MD11F · Fuel StorageSDR FDEA201002250518Fuel Tank · corrodedCENTER TANK UPPER SURFACE APPROX STA 1341, X =107, FOUND SURFACE CORROSION. MAIN DECK CARGO - CTR TANK UPPER SURFACE APPROX STA 1341, X =107, SURFACE CORROSION REPAIRED IAW EA NR 1-5710-132364. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.Feb 25, 2010 · N587FE · Doug MD11F · Fuel StorageSDR FDEA201002240508Skin · damagedVERTICAL STABILIZER AFT RUDDER LOWER EDGE FWD SKIN FOUND PEELED. REPAIRED IAW EA NR 1-5540-132347. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.Feb 24, 2010 · N587FE · Doug MD11F · Rudder, Plate/SkinSDR FDEA201002230493Skin · corrodedRT WING, UPPER WING SURFACE AT XORS258 FOUND CORROSION. RT WING, UPPER WING SURFACE AT XORS258 REPAIRED IAW EA NR 1-5710-132362. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.Feb 23, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002220481Skin · crackedCRACK INDICATION DURING HFEC OPEN HOLE INSP AT ONE HOLE (XORS696.730, STR36) ON LT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT. REPAIRED IAW EA NR 1-5710-132354. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.Feb 22, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190474Frame · misrepairedEXISTING REPAIR ON FRAME AT LT AIRCON BAY STA 485, LONGERON 36 LT TO LONGERON 38 LT. EXISTING REPAIR AT LT STA 485 FRAME, BETWEEN LONGERON 36 LT AND LONGERON 38 LT, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUTFeb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201002190473Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT Feb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190472Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT Feb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190471Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256. EXISTING REPAIR AT LT WING INBD FLAP, OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OFeb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190470Skin · noneEXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT UPPER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIGURE 201, REPAIR 1 REVISIONFeb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190469Skin · noneEXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 193. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT UPPER SKIN APPROX STA XIFH 193, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 201, REPAIR 1, REVFeb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190468Skin · noneEXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217. EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 205, REPAIR GENERAL REVIFeb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190467Skin · misrepairedEXISTING REPAIR AT LT WING FIXED L/E STA XORS 433 (BEHIND NR 3 SLAT). EXISTING REPAIR AT L/E WING FIXED L/E STA XORS 433 (BEHIND NR3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR Feb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190466Skin · misrepairedEXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT). EXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NRFeb 19, 2010 · N587FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201002190465Slat · misrepairedEXISTING REPAIR AT LT WING NR 3 SLAT INNER SKIN (04 EACH DOUBLER). EXISTING REPAIR AT LT WING NR 3 SLAT INNER SKIN (04 EACH DOUBLER), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5740Feb 19, 2010 · N587FE · Doug MD11F · Leading Edge DevicesSDR FDEA201002190464Skin · misrepairedEXISTING REPAIR AT LT FUSELAGE SKIN, STA 705, LONGERON 27 LT (BELOW MAIN CARGO DOOR CUTOUT). EXISTING REPAIR AT LT FUSELAGE SKIN, STA 705, LONGERON 27 LT (BELOW MAIN CARGO DOOR CUTOUT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. RFeb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190462Skin · noneEXISTING REPAIR AT RT FUSELAGE SKIN, STA 1781, LONGERON 38 RT TO LONGERON 42 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1781, LONGERON 38 RT TO LONGERON 42, RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53- 00-15, FIGURE 202, REPAIR 8, REVISION Feb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190461Skin · misrepairedEXISTING REPAIR AT LT FUSELAGE SKIN, STA 630 TO STA 635, LONGERON 25 LT TO LONGERON 26 LT. EXISTING REPAIR AT LT FUSELAGE SKIN, STA 630 TO STA 635, LONGERON 25 LT TO LONGERON 26 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTFeb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190459Doubler · noneEXISTING REPAIR AT RT FUSELAGE SKIN, APPROX STA 2010, LONGERON 45 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, APPROX STA 2010, LONGERON 45 RT. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA NR 1-5310-78002, TITLE: FUSELAGE - AFTER FUSELAGE COMPARTMENT ENTRY Feb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190458Skin · misrepairedEXISTING REPAIR AT RT FUSELAGE SKIN, STA 1002 TO STA 1009, LONGERON 37, RT TO LONGERON 39 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1002 TO STA 1009, LONGERON 37, RT TO LONGERON 39 RT EVALUATED AND FOUND NOT CORRELATE WITH ANY SRM. EXISTING REPAIR DOUBLEFeb 19, 2010 · N587FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA201002190457Skin · misrepairedEXISTING REPAIR AT LT FUSELAGE SKIN, STA 605 TO STA 615, LONGERON 34 LT TO LONGERON 35 LT. EXISTING REPAIR AT LT FUSELAGE SKIN, STA 605 TO STA 615, LONGERON 34 LT TO LONGERON 35 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTFeb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190456Skin · misrepairedEXISTING REPAIR AT LT FUSELAGE SKIN, STA 480 TO STA 490, LONGERON 35 LT TO LONGERON 38 LT. EXISTING REPAIR AT LT FUSELAGE SKIN STA 480 TO STA 490, LONGERON 35 LT TO LONGERON 38 LT EVALUATED AND FOUND DOES NOT CORRELATE TO ANY SRM. EXISTING REPAIR, REPAIREDFeb 19, 2010 · N587FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201002190463Wedge · delaminatedLT WING OTBD FLAP INBOARD T/E WEDGE UPPER SURFACE. FOUND DELAMINATION. LT WING OTBD FLAP INBD T/E WEDGE. R & R IAW CMM 57-52-04 REVISION 66.Feb 19, 2010 · N587FE · Doug MD11F · Wing, Control SurfacesSDR FDEA201002190455Strap · crackedRT WING OTBD FLAP INBD HINGE TENSION STRAP FOUND CRACKED. RT WING OTBD FLAP INBD HINGE CRACKED TENSION STRAP. R & R WITH A NEW TENSION STRAP IAW EO NR 1-5750-7-5004, REV 3, PART 2. REPAIR CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REVISION 109.Feb 19, 2010 · N587FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200910163597Position Switch · malfunctionedGEAR HORN WHEN LANDING GEAR SELECTED ON FINAL. UNSAFE GEAR INDICATIONS IN LANDING GEAR LIGHTS AND ON CONFIG PAGE. DURING GO AROUND THE LIGHTS TURNED GREEN AS GEAR HANDLE WAS PULLED OUT TO RAISE THE GEAR. PUSHED HANDLE BACK IN AND LEFT THE GEAR DOWN AND CAMEOct 16, 2009 · N587FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA200909033255Computer · failedON DEPARTURE, ATS FAILED, BOTH AUTOPILOTS FAILES AND BOTH FLIGHT DIRECTORS FAILED AND WINDSHEAR DET FAIL LIGHT ILLUMINATED. UNABLE TO GET ANY OR ALL BACK. RETURNED TO DEPARTURE. MCDU SCRATCHED MESSAGE 'THRUST LIMIT MISMATCH' ALSO ILLUMINATED. PERFORMED BOTSep 3, 2009 · N587FE · Doug MD11F · Autopilot SystemSDR 08FDEA03531Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 AS PER SRM 53-50-00 FIGUREAug 21, 2008 · N587FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03530Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING HOLES A, B, C AND D CARRIED OUT BUSHING REPAIR AAug 21, 2008 · N587FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA03371Skin · cracked05 EACH FASTENER HOLES FOUND CRACK INDICATION AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT RT WING FUEL TANK LOWER SKIN CUTOUT AT STA XORS Aug 10, 2008 · N587FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA03370Skin · cracked8 FASTENERS HOLES FOUND CRACK INDICATIONS AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT LEFT WING FUEL TANK LOWER SKIN CUTOUT AS PER EA NRAug 10, 2008 · N587FE · Doug MD11F · Wing, Plate/Skin
Back to N587FE