N625FE

Service difficulty reports · 266

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 = 'N625FE' 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 FDEA201703220971Pump · damagedHOLDING SHORT OF RWY 5R IND RECEIVED LVL 2 HYD 2 QTY LOW. PUT HYD SYS IN MANUAL TURNED HYD PUMPS OFF. TEMP WAS 33C AT HYD PUMP SHUTOFF. HYD QTY WENT TO ZERO. PER CREW DEBRIEF, HYDRAULIC QUANTITY WAS 1.1 WHEN PUMPS WERE SHUTOFF AND PUMPS WERE NOT OPERATING WHEMar 22, 2017 · N625FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA201608212946Longeron Splice · crackedCRACKS, 3EA, FROM FASTENERS HOLE TO NEXT HOLE FOUND ON TRANSVERSE SKIN SPLICE INSPECTION AT STA 5-0, STR 6R DURING X-RAY INSPECTION AT LONGERON SPLICE FITTING. NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING IAW DWG AEA7633, REV B. REPAIR CLASSIFIED AS Aug 21, 2016 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201608202943Skin · cracked05 EA FASTENER HOLES, NR 6, 10, 12, 33, 34, FOUND CRACK INDICATION DURING HFEC OPEN-HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS =713.6. REPAIR CARRIED OUT IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFAug 20, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608192938Doubler · crackedLT WING FIXED L/E LOWER SURFACE AT STA XOS 906 DOUBLER CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 19, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608192937Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 906 DOUBLER CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 19, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608192936Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 605 DOUBLER CRACKED. DOUBLER R & R IAW SRM 51-31-01-0G. THE NEW DOUBLER FABRICATED IAW DWG ARB2933, REV AJ. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 19, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608192935Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 546 DOUBLER CRACKED. CRACKED DOUBLER R & R IAW SRM 51-31-01-0G. THE NEW DOUBLER FABRICATED IAW DWG ARB2933, REV AJ. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 19, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182925Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 669 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182924Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 792 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182923Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 782 BEADED DOUBLER CRACKED. THE BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182922Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 731 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182921Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 639 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182920Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 634 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182919Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 627 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182918Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 613 BEADED DOUBLER CRACKED. BEADED DOUBLER CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 18, 2016 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201608182917Frame · damagedMAIN DECK RIGHT FRAME AT BS 1641 LONGERON 12R FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSP REQUIRED-INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT EVERY 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R, TABLE 201.Aug 18, 2016 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201608182916Frame · damagedMAIN DECK RIGHT FRAME AT BS 1661 LONGERON 12R FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSP REQUIRED-INITIAL AT 14,500 CYCLES AND REPETITIVE. INSP AT EVERY 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R, TABLE 201Aug 18, 2016 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201608182915Frame · damagedMAIN DECK LEFT FRAME AT BS 1661 LONGERON 12L FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R, FIG 201, REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE, INSP AT EVERY 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R, TABLAug 18, 2016 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201608172903Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1422, X 75.25 FOUND CORRODED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1451 TO EXISTING SPLICE AT STA 1391, X= 75.25 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 17, 2016 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201608172901Trunnion · crackedNOSE LANDING GEAR WHEEL WELL - LEFT HAND TRUNNION FITTING SUSPECT CRACKED BASED ON MARKING. NDT TO CONFIRM. REPAIR CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 FIG 202. INITIAL INSPECTION TO BE CARRIED OUT AFTER 1,500 FLT CYCLES AND REPETITIVE INSPECTION TO Aug 17, 2016 · N625FE · Doug MD11F · Nose/Tail Landing Gear Attach SectionSDR FDEA201605071508Solenoid · defectiveL1 DOOR WILL NOT CLOSE. FOUND L1 DOOR LOCK PIN RELEASE SOLENOID NOT RELEASING FULLY. R & R L1 DOOR LOCK RELEASE SOLENOID IAW AMM 52-10-06-4.May 7, 2016 · N625FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201604291429Control Unit · defectiveRAMP REPORTED LONGITUDINAL PDU 3LT & RT & 4LT & RT. A4 & A6 CARD FILES ARE VIOLENTLY BURNING UP & HAS CREATED EXCESSIVE INTERIOR HEAT & SMOKE DAMAGE TO CTR CARGO CTL UNIT. ALSO SLAVED IN KNOWN GOOD A12 CARD FILE TO POS A6, & IT BURNED UP AS WELL. CTR CARGOApr 29, 2016 · N625FE · Doug MD11F · Cargo CompartmentsSDR FDEA201602060474Power Supply · inoperativeEMERGENCY LIGHT BATTERY 1 LOW ALERT ON. RELEASED FOR SERVICE. REPLACED POWER SUPPLY IAW MM 33-51-01-4. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.Feb 6, 2016 · N625FE · Doug MD11F · Emergency LightingSDR FDEA201506272098Light · inoperativeR1 DOOR, DOOR DISARMED LIGHT INOPERATIVE.Jun 27, 2015 · N625FE · Doug MD11F · Door Warning SystemSDR FDEA201506171833Spring · brokenL1 DOOR EMERGENCY LIGHT PANEL DAMAGED. REMOVED THE EMERGENCY LIGHT PANEL & SECURED WIRING IAW AMM 25-23-23-2. REPLACED DAMAGED WIRE HARNESS TIE OFF ONDOOR PANEL & INSTALLED 1-L PANEL IAW AMM 25-23-23-2& WDM 33-52-01. OP'S CHECK NORMAL. OK TO CONTINUE. FOJun 17, 2015 · N625FE · Doug MD11F · Emergency LightingSDR FDEA201501270310Unknown · smokeDURING PREFLIGHT, SMOKE FILLED COCKPIT CABIN CARGO AREA. AMM SMP VISUAL INSPECTION PERFORMED OF APU COMPARTMENT, NO ABNORMALITIES FOUND. ACFT OK FOR SERVICE.Jan 27, 2015 · N625FE · Doug MD11F · Air Distribution SystemSDR FDEA201408202220Longeron · crackedCRACK INDICATION APPROX 0.5 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON 4R FWD SECTION AS MARKED. MAIN DECK CRACKED DAMAGED LONGERON AT STATION 6-100, LONGERON 4R FORWARD SECTION PERMANENT REPAIR ACCOMPLISHED AS PER EA 1-5310-T03Aug 20, 2014 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201408202218Longeron · crackedCRACK INDICATION APPROX 0.7 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STATION 6-00, LONGERON 3R FWD SECTION AS MARKED. MAIN DECK CRACKED DAMAGED LONGERON AT STATION 6-100, LONGERON 3R FORWARD SECTION PERMANENT REPAIR ACCOMPLISHED AS PER EA 1-5310-T031Aug 20, 2014 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201408202215Longeron · crackedCRACK INDICATION APPROX 1.0 INCH IN LENGTH FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON 2R FWD SECTION AS MARKED. MAIN DECK CRACKED DAMAGED LONGERON AT STATION 6-100, LONGERON 2R FORWARD SECTION PERMANENT REPAIR ACCOMPLISHED AS PER EA 1-5310-T0310Aug 20, 2014 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201408202255Stringer · crackedRIGHT WING LE CAVITY AT STATION XOS 664, FIXED FAIRING ATTACH STRINGER FOUND CRACKED DURING SLAT DRIVE CABLE INSPECTION. CRACKED AREA TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-03 REPAIR 2 FIGURE 202 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Aug 20, 2014 · N625FE · Doug MD11F · Wing, Longeron/StringerSDR FDEA201408202254Stringer · crackedLEFT WING LE CAVITY AT STATION XOS 665, INTERIOR SKIN ATTACH STRINGER FOUND CRACKED DURING SLAT CONTROL CABLE INSPECTION. CRACKED AREA TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-03 REPAIR 2 FIGURE 202. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Aug 20, 2014 · N625FE · Doug MD11F · Wing, Longeron/StringerSDR FDEA201408192210Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA STATION 1700 TO 1708 LONGERON 49R FOUND CORRODED. CENTER CARGO COMPARTMENT BILGE AREA STA 1700 TO STA 1708 LONGERON 49R. CORRODED LONGERON FOUND OUT OF LIMIT AS PER SRM 53-00-00 FIGURE 205 AND REPAIR CARRIED OUT AS PER EA Aug 19, 2014 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201408192209Frame · dentedCABIN LT STATION 1721, LONGERON 12L FRAME FOUND DENTED. LEFT HAND STATION 1721, LONGERON 12L FRAME CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY B, INITIAL INSPECTION AT 1Aug 19, 2014 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201408192208Frame · dentedCABIN LT STATION 1681, LONGERON 12L FRAME FOUND DENTED. LEFT HAND STATION 1681, LONGERON 12L FRAME CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY B, INITIAL INSPECTION AT 1Aug 19, 2014 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201408192207Frame · dentedCABIN LT STATION 1701, LONGERON 12L FRAME FOUND DENTED. LEFT HAND STATION 1701, LONGERON 12L FRAME CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY B, INITIAL INSPECTION AT 1Aug 19, 2014 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201408192206Frame · dentedCABIN RT STATION 1701, LONGERON 12R FRAME FOUND DENTED. RIGHT HAND STATION 1701, LONGERON 12R FRAME CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY B, INITIAL INSPECTION AT Aug 19, 2014 · N625FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201407171835Indicator · inoperativeFLIGHT CREW REPORTS R1 DOOR REMOTE PRESS TO TEST FOR DOOR SLIDE INOPERATIVE. R1 DOOR EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY. R & R R1 DOOR REMOTE PRESS. OPERATIONS CHECKJul 17, 2014 · N625FE · Doug MD11F · Emergency EquipmentSDR FDEA201404110726Line · out of positionNEAR TOWER REPORTED SMOKE COMING FROM RT MAIN GEAR AFTER LANDING. NO ABNORMAL INDICATIONS IN THE COCKPIT OR ON THE CONFIG PAGE. PORT AUTHORITY CREWS RESPONDED & NOTED NO SMOKE OR DAMAGE. FOUND BRAKES 9 & 10 FWD HYD BRAKE FLEX LINES CROSSED. REPOSITIONED IApr 11, 2014 · N625FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201401080066Brake · malfunctionedDURING CLIMB OUT PASSING FLT LEVEL 210, BRAKE DIFF TEMP ILLUMINATED. CONFIG PAGE INDICATED NR 7 BRAKE AT 391 DEGREES. OTHER TEMPS ON RT TRUCK INDICATED APROX 60 - 70 DEGREES. PERFORMED QRH. STOPPED CLIMB AT FL 250 TO SLOW & LOWER GEAR IN AN ATTEMPT TO COOJan 8, 2014 · N625FE · Doug MD11F · BrakeSDR FDEA201312052924Wire Harness · out of positionUPON GEAR RETRACTION, THE NOSE GEAR PRIMARY INDICATOR REMAINED RED, SECONDARY INDICATOR SHOWED NORMAL. CYCLED GEAR & ALL INDICATORS RETURNED TO NORMAL. DURING VISUAL INSPECTION & CREW DEBRIEF FOUND THAT WIRE HARNESS NR ACP8600-508 FOR THE NLG LIGHTS WAS HANGIDec 5, 2013 · N625FE · Doug MD11F · Light System WiringSDR FDEA201211294208Warning Light · false activationFLAX PWR, GOT REV-PRESS FAULT(SUSPECT ENG 3).REJECTED T/O AND RETURNED TO LINE DUE FLAGGED I TEM. UNABLE TO DUPLICATE, ACCOMPLISHED HIGH POWER RUNS PERFORMED ENG RUN IAW JRH, NO REV FAULT MESSAGE FOUND, PERFORMED REVERSER FUNTION TEST IAW MM 78-30-00-5.Nov 29, 2012 · N625FE · Doug MD11F · Central WarningSDR FDEA201211234136Dadc · failedFIRST OFFICER LOST AIRSPEED INFORMATION DURING TAKEOFF ROLL, SUSPECT DADC FAILURE. AT 300FT AGL, CAPTAIN LOST FLT DIRECTOR CONTROL OF FCP ALT-SELECTOR AIRSPEED SEEMED OK. WHEN F/O SWITCH TO CAPTAIN'S ADC, CAPTAIN'S SIDE GOT FLT DIRECT, AUTO PILOT, AUTO THROTNov 23, 2012 · N625FE · Doug MD11F · Auto Flight SystemSDR FDEA201211053832Longeron Splice · crackedFORWARD CARGO COMPARTMENT, LONGERON 34R, BS 1119 TO 6-10, LONGERON SPLICE CRACKED. R & R WITH FABRICATED SPLICE IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 5, 2012 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211023810Skin · corrodedCENTER CARGO BILGE SKIN FOUND CORRODED AT STA 5-40, LONGERON 49 - 50R. REPAIRED IAW EA 1-5310-162393. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 2, 2012 · N625FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201211023812Skin · crackedFASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS= 683.4 AND XORS= 713.6. REPAIRED IAW SRM 57-20-02, FIG 201 REPAIR 5, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMMNov 2, 2012 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211023811Skin · crackedFASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS= 683.4 AND XORS=713.6. REPAIRED IAW SRM 57-20-02, FIG 201, REPAIR 5 REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMMNov 2, 2012 · N625FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201211013796Longeron · corrodedBS 1481-1501 LONGERON 18L STRAP FOUND CORRODED. REPAIRED IAW EA 1-5310-163525. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115,Nov 1, 2012 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201211013801Tee Fitting · crackedLEFT UPPER FUSELAGE TEE FITTING FOUND CRACKED BETWEEN BS 1361 TO 1381 BELOW LONGERON 27. R & R IAW SRM 51-31-01, REVISION 50. PNEUMATIC LEAK CHECK CARRIED OUT IAW AMM 36-10-00 REV 74.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 1, 2012 · N625FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201211013800Support · chafedMAIN DECK LT SUPPORT YOKES AT FRAME BS 535 BETWEEN LONGERONS L23 TO L24 FOUND CHAFED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 1, 2012 · N625FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201211013799Support · chafedMAIN DECK LT SUPPORT YOKES AT FRAME BS 535 BETWEEN LONGERONS L20 TO L21. FOUND CHAFED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Nov 1, 2012 · N625FE · Doug MD11F · Fuselage Miscellaneous Structure
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