N615FE

Service difficulty reports · 469

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 = 'N615FE' 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 FDEA201605161599Doubler · crackedLEFT WING FIXED LE INTERIOR AT APPROX STATION XOS 862, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605161597Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635, X=-8.5, FOUND CRACKED. CRACKED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161596Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1802, X= 8.5, FOUND CORRODED SEAT TRACK. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1771 - 1831, X =8.5 IAW 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161595Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1802, X=-8.5, FOUND CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1771 - 1831, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161594Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 6-80, X=47.5, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 6-60 - 6-100, X=47.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605161593Door Frame · crackedMAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STATION 1250.75 - 1256.75, LONGERON 26R - 27R, FOUND CRACKED. MAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201605161592Door Frame · crackedMAIN DECK L3 DOOR FWD JAMB, LOWER WEB BOX AT STATION 1250.75 - 1256.75, LONGERON 26L - 27L, FOUND CRACKED. MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED IAW MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201605161591Door Frame · crackedMAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 - 1315.42, LONGERON 26R - 27R, FOUND CRACKED. MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R. FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201605161590Door Frame · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 - 1315.42, LONGERON 26L - 27L, FOUND CRACKED. MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2016 · N615FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201512274099Computer · inoperativeDURING CLIMB OUT, FCC 2 B DATA FAULT, LEVEL TWO ALERT DISPLAYED. QRH PROCEDURE APPLIED. CURRENT FAULT ON SENSOR READ OUT SHOWS FCC 2 FAULTED. FCC 2 CURRENT FAULT SHOWS FCC 2 FAULTED. CARRIED OUT INSPECTION AT FCC 2 AVIONICS RACK BACK SHELL SOCKET PINS & WIDec 27, 2015 · N615FE · Doug MD11F · Autopilot ComputerSDR FDEA201504171253Stick Shaker · activatedMOMENTARY STICK SHAKER ACTIVATION AT FL 360, 242KIASDUE TO MODERATE TURBULENCE. AUTOPILOT WAS ENGAGED & AUTO THROTTLES WERE ENGAGED. CLEAN CONFIGURATION. COMPLIED WITH TURBULENCE INSPECTION IAW AMM 05-51-01-6, NO DEFECTS NOTED.Apr 17, 2015 · N615FE · Doug MD11F · Stall Warning SystemSDR FDEA201405291224Skin · delaminatedRIGHT OTBD FLAP INBD TE UPPER SURFACE FOUND DELAMINATED AT XOFH 477.69 - 497. REPAIRED IAW SRM 57-50-80 PARAGRAPH 4A 1B. REPAIR 1 REVISION 55 & EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.May 29, 2014 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201405201089Structure · wornMAIN DECK CARGO DOOR FOUR FWD HINGE PIN LOBE HOLES FOUND ELONGATED. REWORKED AND FOUND WITHIN LIMITS IAW CMM 52-34-04 PARAGRAPH 2Y REVISION 78 AND EA1-5230-T0308187 PART1 STEP 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 121.May 20, 2014 · N615FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201405191070Longeron · crackedBS 1315, LONGERON 28R FOUND CRACKED. REMOVED AND REPLACED LONGERON IAW SRM 51-33-01 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 19, 2014 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201405171059Skin · crackedSKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 May 17, 2014 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201405171058Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 273HF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 17, 2014 · N615FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201405171057Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 293DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 17, 2014 · N615FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201405171056Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 233DF FOUND DELAMINATED. FABRICATED IAW DRAWING SRZ 25-005 REVISION K. REMOVED AND REPLACED IAW AMM 53-21-04-4 REVISION 79. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 17, 2014 · N615FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201405141018Skin · delaminatedRIGHT OTBD FLAP INBD LOWER TE FOUND DELAMINATED. REPAIRED IAW SRM 57-50-80 PARA 4 1B REPAIR 1 REVISION 55 AND EA 1-5750-T0308362 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 14, 2014 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201405141004Skin · crackedLEFT WING, SLAT TRACK NR 12 LOWER CUT OUT SKIN AT XOS 776 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.May 14, 2014 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201402200375Engine · failedAFTER TAKEOFF NR 1 ENGINE FAILED & OVER TEMPED. MAX POWER TAKEOFF COMPLETED CHECKLIST. CREW FIRED ONE EACH FIRE BOTTLE. R & R NR 1 ENGINE. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.Feb 20, 2014 · N615FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201302070294Skin · missingFOUND NR 8 LT SLAT SKIN MISSING TOP SIDE MIDDLE TO T/E AREA ABOUT CENTER OF SLAT. INSTALLED LT NR 8 SLAT IAW AMM 27-80-30-4.Feb 7, 2013 · N615FE · Doug MD11F · Leading Edge DevicesSDR FDEA201301100167Duct · crackedSHORTLY AFTER T/O WITH ALL ENG A/I SELECTED ON, GOT "ENG 2 A-ICE OFF" ALERT. CONSULTED QRH AND DIVERTED IAW GOC. FOUND DUCT CRACKED AT FLANGE NEAR FWD END. R & R DUCTING 2, ENGINE 2 ANTI-ICE. OPS CHECK GOOD, NO LEAK NOTED AND MESSAGE CLEARED.Jan 10, 2013 · N615FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201212294399Warning Light · illuminatedRECEIVED LEVEL 1 "BUSS R EMER AC OFF" ALERT, 2 HOURS INTO FLIGHT. SELECT FADEC ALT,TANK 2 AFT PUMP LO, SINGLE LAND, FO PITOT HEAT, GPWS FAULT, SEL ALT CADC. FAILURE WENT AWAY AND ALL SYS NORMAL AFTER APPROX 20 MIN, DIVERTED AND LANDED WITHOUT INCIDENT. Dec 29, 2012 · N615FE · Doug MD11F · AC InverterSDR FDEA201211154023Union · leakingAT 118 INTO FLIGHT AT FL 320 GOT LVL 1 "HYD 3 ELEV OFF" ALERT. FLUID LEVEL IN NR 3 WAS 4.3 GALS AND STARTED DECREASING AT A RATE OF .1 GAL EVERY 3 MINUTES. WHEN 3.5 WAS REACHED;, TURNED HYD SYSTEM TO MANUAL AND TURNED OFF HYD 3 LT AND RT PUMPS AND ALSO THENov 15, 2012 · N615FE · Doug MD11F · Hydraulic System, MainSDR FDEA201211103935Idg · inoperativeRAN NR 3 ENG FOR IDG DISCONNECT IDG CAME APART DURING RUN. ENGINE NR 3 FIRE INDICATION IN FLIGHTDECK AND 1EA FIRE BOTTLE DISCHARGED, AFTER FURTHER INSPECTION IDG FOUND CRACKED AND INSPECTION ON WIRING AND GEARBOX INWORK. R & R IDG, AIR/OIL HEAT EXCHANGER FLUNov 10, 2012 · N615FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201210253744Relay · failedAT 5000' 200 KNOTS "BUS RT EMERG AC" ILLUMINATED, RT EMERGENCY AC BUSS FAILED. SELECTED "FADEC ALT", F/O CADC ON 1, TRANSPONDER 1, RAN LEVEL 1 ALERT DUE TO NO APPLICABLE CHECKLIST. TROUBLESHOT IAW FIM: 25-25-01-00 AND WDM: 24-61-51 FOUND RELAY (R2-5157)ATOct 25, 2012 · N615FE · Doug MD11F · AC Power Distribution SystemSDR FDEA201207132562Fitting · misrepairedDURING ACCOMPLISHMENT OF VERTICAL STABILIZER NR 4 BANJO FITTING REPAIR AT RT SIDE FORWARD FLANGE LOWER FITTING EXISTING FASTENER AREA FOUND SHORT WITH 1 EA FASTENER AT REPAIR FITTING IAW REPAIR DWG: SR10550013. REPAIRED AS PER E.A. 1-5530-159861 PART 1. REJul 13, 2012 · N615FE · Doug MD11F · Vertical StabilizerSDR FDEA201207012433Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER, NR4 BANJO FITTING, RT SIDE FWD FLANGE. CARRIED OUT REPAIR AS PER DRAWING SR10550013 SHEET 7, 8, AND 9 REVISION P.Jul 1, 2012 · N615FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201207012431Frame · dentedFRAME AT BS 1661, LONGERON 11L, FOUND DENTED. REPAIRED IAW SRM SRM 51-33-01 REVISION 49. AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 1, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207012430Frame · dentedFRAME AT BS 1721, LONGERON 11R FOUND DENTED. REPAIRED IAW SRM 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 1, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207012429Frame · dentedFRAME AT BS 1661, LONGERON 11R FOUND DENTED. REPAIRED IAW 51-33-01 REVISION 49 AND SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 1, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207012428Frame · dentedFRAME AT BS 1641, LONGERON 11, FOUND DENTED. CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 49. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 1, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201207012432Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LOWER VERTICAL STABILIZER NR 4, BANJO FITTING, LT SIDE, FORWARD FLANGE. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIGURE 201 REPAIR 3 REVISION 49.Jul 1, 2012 · N615FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201206292408Skin · cracked03 EA FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162348. REPAIR CLASSIFIED AS MINOR Jun 29, 2012 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201206292407Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGITUDINAL SPLICE FOUND CRACKED AT STATION 5-113 TO STA 1551, LONGERON 47RT. LONGERON REMOVED AS PER SRM 51-31-01 REVISION 49 AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING A5A7116 REVISION D AND INSTALLED AS PER SRM 51-33-0Jun 29, 2012 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201206292401Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2865", REWORKED HOLE DIAMETER 1.313", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISJun 29, 2012 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201206292400Hinge Fitting · damagedRT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.228", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHED AJun 29, 2012 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201206292399Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.2215", REWORKED HOLE DIAMETER 1.250", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISJun 29, 2012 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201206292398Hinge Fitting · damagedLT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-52-03 REVISION 73. EXISTING HOLE DIAMETER 1.255", REWORKED HOLE DIAMETER 1.2834", MAXIMUM LIMIT DIAMETER 1.220". REPAIR ACCOMPLISHJun 29, 2012 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201206292409Skin · crackedTHREE FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. CARRIED OUT REPAIR AS PER EA 1-5710-162349. REPAIR CLASSIFIED AS MINOR AS PJun 29, 2012 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201206292406Seat Track · dentedBS 765, X= 8.5 SEAT TRACK FOUND DAMAGED. SEAT TRACK REMOVED AS PER SRM 51-33- 01 REVISION 49. NEW REPAIR SEAT TRACK AND SPLICE REWORKED AS PER SRM 53-00-52 REVISION 49 AND INSTALLED AS PER SRM 51-33-01 REVISION 49. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2Jun 29, 2012 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206292405Frame · chafedFRAME BS 535, 9G NET LOWER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.Jun 29, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201206292404Frame · chafedFRAME BS 535, 9G NET UPPER SUPPORT YOKE FOUND CHAFED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49.Jun 29, 2012 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201206292403Splice · crackedCENTER CARGO COMPARTMENT LONGERON 42L SPLICE FOUND CRACKED AT STATION 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7115 REVISION D. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVIJun 29, 2012 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201206292402Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON 40R SPLICE FOUND CRACKED AT STA 5-113 TO 1541. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 49. SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Jun 29, 2012 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201111194980Wire Harness · damagedRECEIVED LEVEL 1 ALERT REV 3 PRESS FAULT PRIOR TO 80 KTS ON TAKEOFF ROLL. WIRE HARNESS FOUND DAMAGED AND REPLACED.Nov 19, 2011 · N615FE · Doug MD11F · Engine Exhaust System WiringSDR FDEA201106012081Check Valve · stuckNR 1 N1 ROLLED BACK TO 25-35 % JUST PRIOR TO DECENT. A NOTICABLE AND AUDIBLE BUMP IN AIRFRAME, LT YAW, & CONFIRM ENGINE OUT ON MCDU'S. SHUTDOWN ENGINE IAW QRH. ELECTED TO LEAVE ENGINE SHUTDOWN DUE TO POSSIBLE DAMAGE. EGT & N2 SLIGHTLY LOWER THAN NR 2, 3. Jun 1, 2011 · N615FE · Doug MD11F · Engine Bleed Air SystemSDR FDEA201008112927Skin · cracked(10EA) FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132468. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 110.Aug 11, 2010 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201008112925Skin · cracked8 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132467. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 110.Aug 11, 2010 · N615FE · Doug MD11F · Wing, Plate/Skin
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