N616FE

Service difficulty reports · 267

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 = 'N616FE' 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 FDEA201409242753Skin · damagedCENTER CARGO DOOR AFT JAMB STA 1781 LONGERON 41R, REPAIR CARRIED OUT AT CENTER CARGO DOOR AFT JAMB STATION 1781 LONGERON 41R AREA AS PER EA 1-5330-T0305743A PART 3. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI 53301210 FOR DETAILS.Sep 24, 2014 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201409232729Skin · damagedAGEING ACFT EXISTING REPAIR FOUND AT FWD CARGO DOOR JAMB CUT OUT AFT LOWER AT STATION 1002 BETWEEN LONGERON 40R TO 41R. EXISTING REPAIR FOUND DAMAGED. REPAIRED PER SRM 53-00-15 FIGURE 202 REPAIR 8 EO 1-5100-7-5001B5 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMSep 23, 2014 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201409232731Doubler · crackedRIGHT WING LE BEADED DOUBLER AT STATION XOS 861 - XOS 867 FOUND CRACKED. CRACKED REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Sep 23, 2014 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201409232730Former · crackedRIGHT WING LE FORMER AT STATION XOS 559 FOUND CRACKED. FORMER REMOVED AND FABRICATED NEW FORMER AS PER DRAWING ARC1162 REVISION S INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE STATION XOS 559 AS PER SRM 51-33-01 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-1Sep 23, 2014 · N616FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201409232728Frame · dentedCABIN MAIN DECK CARGO COMPARTMENT LT STATION 1721 LONGERON 12L FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 23, 2014 · N616FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201409232727Door Frame · crackedCABIN MAIN DECK CARGO COMPARTMENT LT STATION 1256 LONGERON 26L FWD L3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Sep 23, 2014 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201409232726Door Frame · crackedCABIN MAIN DECK CARGO COMPARTMENT RT STATION 1310 LONGERON 26R AFT R3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Sep 23, 2014 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201409232725Door Frame · crackedCABIN MAIN DECK CARGO COMPARTMENT RT STATION 1256 LONGERON 26R. FWD R3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201. REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201409232724Cargo Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 755 X=27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 745 TO STATION 785, X= 27.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232723Cargo Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 47.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 47.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232721Cargo Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X=27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 27.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232720Cargo Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 8.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232719Seat Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= -8.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 625 TO STATION 665, X=-8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232718Cargo Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X=-27.5 AS PER SRM 53- 00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232717Seat Track · crackedMAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635, X= -47.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X=-47.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Sep 23, 2014 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201303210636Hinge · wornUPPER CARGO DOOR ATTACHED FORWARD HINGE LOWER LOBES WORN. REAMED AS PER CMM 52-34-04 REVISION 75. REPAIR ACCOMPLISHED AS PER EA 1-5230-167401 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Mar 21, 2013 · N616FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201303180591Skin · chafedLT WING FIXED L/E UPPER SURFACE STATION XIS 247 FOUND WITH CHAFING. REPAIRED AS PER SRM 57-40-02 REPAIR 8 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 REVISION 116.Mar 18, 2013 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201303150575Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD, RT SPOILER MIXER CONTROL ROD FEED THROUGH CUTOUT DOUBLER FOUND CRACKED. FABRICATED DOUBLER INSTALLED AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Mar 15, 2013 · N616FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201303130561Doubler · crackedLEFT WING FIXED L/E XOS 690 BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Mar 13, 2013 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201303130560Doubler · scratchedFORWARD CARGO DOOR CUTOUT AFT JAMB LOWER DOUBLER FOUND SCRATCHED. REPAIRED IAW SRM 53-00-15 REPAIR 8 FIGURE 202 REVISION 51.Mar 13, 2013 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201303130559Skin · dentedLEFT WING INBD FLAP ASSY, INBD LOWER SEGMENT LOWER SURFACE FOUND DENTED. REPAIRED AS PER SRM 57-50-01 FIGURE 201 REPAIR 1 REVISION 52 AND E.A. 1-5750-166104.Mar 13, 2013 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201303130558Skin · corrodedLT WING T/E PANEL NR 541JB CUTOUT FORWARD CAP FOUND CORROSION AT XW 338. REPAIRED IAW SRM 51-31-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Mar 13, 2013 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201301310234Control Unit · failedAFTER TAKEOFF CLIMBING OUT OF 3000 FT LOST ALL GENERATORS, APPEARED TO BE PRODUCING POWER BUT COULD NOT CONNECT TO THE SYSTEM. DEPLOYED ADG AND RETURNED TO AIRPORT. REMOVED AND REPLACED EPCU REF AMM. RAN ALL ENGINES PER JRH. ALL INDICATIONS NORMAL NO FAULJan 31, 2013 · N616FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201301220156Tire · failedNR 10 TIRE BLOWN ON LANDING. R & R RED CENTER WHEEL NR 9 AND NR 10 IAW MM 32-41-01-4. DURING WHEEL REPLACEMENT ON NR 10 FOUND WHEEL AIR TRANSDUCER AND HUBCAP BROKEN, R & R RED TRANSDUCER AS MM 32-46-03-4, REPLACED HUBCAP IAW MM 32-46-11-4, ADJUSTED TIRE PRESJan 22, 2013 · N616FE · Doug MD11F · TireSDR FDEA201209140353Fire Detector · failedAFTER DEPARTURE, CLIMBING THROUGH FL300 FOR FL330. RECEIVED FIRE DET 3 FAIL ALERT. DUMPED APPROX 17,000 LBS FUEL AND RETURNED TO DEPARTURE. AFTER BLOCK IN WITH EXTERNAL POWER ON EXTERNAL POWER DROPPED OFF. AFTER STARTING APU POWER, RECEIVED ENG 3 FIRE WARNISep 14, 2012 · N616FE · Doug MD11F · Fire DetectionSDR FDEA201111184976Tee Fitting · crackedRUNNING TANK TO ENGINE ON ALL 3 ENGINES. ALL FILL VALVES WERE CLOSED BUT FUEL LEVEL IN TANK 1 WAS NOT DECREASING. VERIFIED ON GROUND WITH TANK 2 AND 3 TRANSFER PUMPS ON THE NR1 TANK QUANTITY INCREASED WITH THE FILL VALVE SELECTED (AND INDICATED) CLOSED. UNCNov 18, 2011 · N616FE · Doug MD11F · Aircraft Fuel Distribution SystemSDR FDEA201104061345Longeron Splice · crackedLOWER CTR CARGO COMPARTMENT BILGE, STA 5-123 LONGERON 46RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7116 REVISION D. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS Apr 6, 2011 · N616FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201104061343Skin · crackedLT WING - 15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER BOEING DRAWING : SG11570004 REVISION B. QUANTITY 01 EACH CRACKEDApr 6, 2011 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201104061342Longeron Splice · corrodedLONGERON SPLICE L-52 AT APPROX STA 6-10 FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. LONGERON SPLICE FABRICATED AS PER DRAWING AAA7088 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 6, 2011 · N616FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201104061341Panel · crackedVERTICAL STABILIZER LT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. OPS TEST OF THE ENG IGNITION/FADEC MODE SWITCH AND ADVISORY LIGHTS CARRIED OUT AS PER AMMApr 6, 2011 · N616FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201104061340Panel · crackedVERTICAL STABILIZER RT CTR SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 6, 2011 · N616FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201104061344Skin · crackedRT WING - 13 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER DRAWING : SG11570004 REVISION B. REPAIR CLASSIFIED AS MINOR AS PER Apr 6, 2011 · N616FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201104041314Frame · dentedCABIN RIGHT HAND STATION 1701 L-11 FRAME FOUND DENT. CABIN RIGHT HAND STATION 1701 L-11 DENTED FRAME REPAIRED AS PER SRM 53-00-07 FIG 201 REPAIR 2 REVISION 46. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AApr 4, 2011 · N616FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201104041312Seat Track · corrodedCABIN RIGHT HAND STATION 470 TO 495 X=-27.5 SEAT TRACK FOUND CORROSION. CABIN RIGHT HAND STATION 470 TO 495 X=-27.5, CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 455 TO STATION 525 X=-27.5 AS PER SRM 53-00-52 FIG 201 REPAIR Apr 4, 2011 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104041313Stiffener · crackedEMPENNAGE FORWARD TAIL CONE RIGHT HAND LOWER ALIGNING PIN SUPPORT CHANNEL FOUND CRACKED AT BULKHEAD STATION 2164 AFT FACE. EMPENNAGE LOWER BULKHEAD STATION 2164 RIGHT HAND LOWER ALIGNING PIN SUPPORT STIFFENER REPAIR CARRIED OUT AS PER SRM 53-80-02 FIG 201 RApr 4, 2011 · N616FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201011094288Skin · crackedWHILE CARRYING OUT WALKAROUND CHECK, FOUND LOWER CTR CARGO DOOR WITH 01 EACH EDGE CRACK AT FWD LOWER CORNER. REPAIRED AS PER SRM 52-30-16 FIGURE 201 REVISION 44.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.Nov 9, 2010 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200907212681Structure · crackedCENTER LANDING GEAR - RT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER CRACKED. CTR LANDING GEAR - RT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER IAW SRM 51-31-01 VOL. II REV. 40. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6Jul 21, 2009 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200907212680Structure · crackedCENTER LANDING GEAR- LT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER CRACKED. CTR LANDING GEAR- LT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER IAW SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100Jul 21, 2009 · N616FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200907132591Skin · corrodedAFT BODY FAIRING ENCLOSED AREA AT APPROX 2164 LONGERON, 33RH TO LONGERON 35RT FOUND WITH CORROSION ADJACENT TO SCREW HOLES. REPAIR IAW SRM 53-20-00 VOL1, FIG18, REV40 (MAJOR REPAIR).Jul 13, 2009 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200907132597Hinge Bracket · corrodedLT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.Jul 13, 2009 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907132596Hinge Bracket · corrodedRT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132149.Jul 13, 2009 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907132595Hinge Bracket · corrodedRT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIR IAW EA 1-5750-132149.Jul 13, 2009 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907132593Hinge Bracket · corrodedLT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.Jul 13, 2009 · N616FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200907132592Skin · crackedSKIN CRACK FOUND AT APPROX STA 2140 LONGERON 36 RT JUST ABOVE APU EXHAUST AREA. REPAIR IAW SRM 53-20-00 VOL1, FIG4, REV40 (MAJOR REPAIR).Jul 13, 2009 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200907132590Hinge Bracket · corrodedLT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT LWR BORE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132147.Jul 13, 2009 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907132589Hinge Bracket · corrodedLT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT UPPER BORE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132147.Jul 13, 2009 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907132588Hinge · corrodedRT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132146.Jul 13, 2009 · N616FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200907102566Seat Track · corrodedCABIN - SEAT TRACK FLANGE AT STA 1655 X= -107 FOUND EXFOLIATION CORROSION. CABIN - SEAT TRACK FLANGE AT STA 1655 X= -107 REPAIRED IAW SRM 53-70-00 FIG 6, VOL I, REV. 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.Jul 10, 2009 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907102565Seat Track · corrodedCABIN - RT STA 1259 TO STA 1301 X= -107 SEAT TRACK FOUND CORROSION. CABIN CORRODED SEAT TRACK AT RT STA 1259 TO STA 1301 X= -107, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1229 TO STA 1331 X= -107 IAW SRM 53-70-00 FIG. 1, VOL I, REV. 40. REPAIRJul 10, 2009 · N616FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907092548Door Frame · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NO. 7 LOWER JAMB FITTING AT HOLE B. REPAIRED IAW EA 1-5310-132150.Jul 9, 2009 · N616FE · Doug MD11F · Fuselage Main, Structure
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