N522FE

Service difficulty reports · 338

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 = 'N522FE' 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 FDEA200909273390Door Frame · chafedNR 2 ENGINE DOOR JAMB AREAS AT APPROX 5 O'CLOCK POSITION CHAFED. REPAIRED PER EA1-5450-133871 (MAJOR REPAIR).Sep 27, 2009 · N522FE · Doug MD11F · Nacelle/Pylon, Main FrameSDR FDEA200909213347Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK FOUND DAMAGED AT STA 1241, X = -47.5. REPAIRED IAW SRM 53-00-52, FIG201. REPAIR 1, REV 41 (MAJOR REPAIR).Sep 21, 2009 · N522FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909173312Shear Tie · corrodedAFT CARGO COMPARTMENT - STA 1953 FROM LONGERON 50 LT TO LONGERON 49 RT FRAME SHEAR CLIP FOUND CORROSION. REPAIRED IAW SRM 51-31-01 REV 41.Sep 17, 2009 · N522FE · Doug MD11F · Fuselage Internal Mounting StructureSDR FDEA200909153300Access Panel · crackedRT WING NR 3 SLAT AREA, STA XOS 464 L/E UPPER ACCESS CUT OUT FOR WING ANTI ICE TELESCOPIC DUCT CRACKED AT 02 CORNERS. REPAIR IAW SRM 57-40-01, FIG 201 REV 41.Sep 15, 2009 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909153299Fitting · crackedLWR VERT STAB, RT SIDE FWD FLANGE OF UPPER REAR SPAR CAP BETWEEN FIRST AND SECOND LOWEST FASTENER FOUND APPROX 1 INCH CRACKED. RT LWR VERTICAL STABILIZER FWD FLANGE UPPER REAR SPAR CAP AREA REPAIRED IAW SRM 55-30-02, FIGURE 201, REPAIR 3, REVISION 41. FABRSep 15, 2009 · N522FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR 08FDEA01118Frame · dentedMAIN DECK LEFT FRAME AT BS 1721 S12L FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFIED AS MAJOR AMar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01117Frame · chafedMAIN DECK LT FRAME AT STATION 535 , BETWEEN L23-24L, 1 CHAFED MARK FOUND. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Mar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01116Frame · chafedMAIN DECK LEFT FRAME AT BS 535, BETWEEN L19-20L, 01 EACH CHAFED MARK FOUND NEAR 9G NET YOKE. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Mar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01115Frame · dentedMAIN DECK LEFT FRAME AT STATION 1661, STRINGER 12 LEFT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFMar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01114Frame · dentedMAIN DECK RIGHT FRAME AT BS 1721 S12R FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFIED AS MAJOR AS PMar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01113Frame · dentedMAIN DECK RIGHT FRAME AT STATION 1681, STRINGER 12 RIGHT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSMar 23, 2008 · N522FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA01087Skin · crackedLEFT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER SKIN CRACKED. REPAIRED AS PER SRM 57-10-00, FIGURE 43, VOLUME 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 20, 2008 · N522FE · Doug MD11F · Wing, Plate/SkinSDR 06FDEA03785Skin · damagedFOUND CTR CARGO DOOR JAMB CUT OUT LOWER AFT EXTERIOR SKIN EDGES FOUND DAMAGED. AREA TRIMMED OUT 0.50"X 6 AS PER SRM 53-50-00 FIG.16 VOL.I AND FOUND WITHIN LIMIT. NEW DOUBLERS FABRICATED AS PER SRM 53-50-00 VOL.I. HOLES PICKED UP AS PER SRM 51-31-01 VOL.IIOct 25, 2006 · N522FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03770Skin · chafedRT WING L/E NR 1 SLAT AFT SKIN FOUND CHAFING MARKS. REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Oct 24, 2006 · N522FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03701Skin · damagedFWD CARGO DOOR JAMB CUT OUT AFT LOWER OUTER SKIN EDGES FOUND WITH SLIGHT DAMAGE. CARGO DOOR JAMB CUT OUT AFT LOWER SKIN EDGES AREA TRIMMED OUT 3 LOCATIONS AS PER SRM 53-50-00 AND FOUND OUT OF LIMITS PER SRM 53-00-01 FIG.1A VOL.I FABRICATED NEW DOUBLER AS Oct 19, 2006 · N522FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03700Frame · crackedSTA 859 LONGERON 6 BETWEEN FRAME AND LONGERON ATTACHMENT HOLE 1, FOUND CRACK. REPAIR CARRIED OUT AS PER E.A.1-5330-103545. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N522FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03377Hinge Bracket · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2006 · N522FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03376Hinge Bracket · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 19, 2006 · N522FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03375Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG.621-622. BUSHING FABRICATED AND INSTALLED AS PER EA1-5750-104709 TEE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1Sep 19, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03356Skin · dentedFOUND UPPER FUSELAGE EXTERIOR, DENT MARK ON EXTERNAL SKIN STA 859 TO STA 875 BETWEEN LONGERON 10R AND 11R. REPAIR DOUBLERS AND 3 PCS. FINGER DOUBLERS INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 18, 2006 · N522FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03354Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMITS AS PER CMM 57-44-08 PG.602-607 AND WITHIN DAC DWG AWRC0502 LIMITS. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND REPAIR CLASSIFIED AS MINORSep 18, 2006 · N522FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03353Hinge · corrodedRT WING I/B FLAP O/B HINGE (WING SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07. REPAIR CARRIED OUT AS PER EA 1-5750-104703. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Sep 18, 2006 · N522FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03352Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 1.1875" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PESep 18, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03351Hinge · corrodedLT WING I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. LT FWD I/B FLAP O/B HINGE PIVOT HOLE SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07 PG.403-404. ORIGINAL THK I/B 0.461" O/B 0.435" REMAINING THK I/B 0.445" Sep 18, 2006 · N522FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 06FDEA03350Hinge · corrodedLEFT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG.442-444. ORIGINAL THK 1.187" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PERSep 18, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03324Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG.402-408 AND FOUND WITHIN DAC DWG ARC0503 LIMITS. ORIGINAL THK I/B 0.408" REMSep 14, 2006 · N522FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03323Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.2695" FINAL 1.314" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSep 14, 2006 · N522FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03321Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.1885" FINAL 1.2155" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSep 14, 2006 · N522FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03320Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE LOWER MOUNT SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 AND WITHIN DAC DWG ARC 0502 LIMITS. SHIMS FABRICATED AND INSTALLED Sep 14, 2006 · N522FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03234Doubler · crackedCTR LANDING GEAR LT BULKHEAD FWD CUTOUT DOUBLER SUSPECT CRACK. CTR LANDING GEAR L/H BULKHEAD FWD CUTOUT DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 AND 51-35-01 VOL.II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 10, 2006 · N522FE · Doug MD11 · Fuselage Main, BulkheadSDR 06FDEA03181Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY UPPER SURFACE O/B SEGMENT.Sep 4, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03180Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY LWR SURFACE, 63" FROM O/B, 31" FROM T/E.Sep 4, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03179Skin · dentedLHW I/B FLAP ASSY O/B SEGMENT LWR SURFACE FOUND MULTIPLE DENTS. LT WING I/B FLAP ASSY O/B SEGMENT LOWER SURFACE MULTIPLE DENTS REPAIRED AS PER SRM 57-10-00 FIG.2 VOL. I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Sep 4, 2006 · N522FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03160Skin · damagedRT HORIZ STAB REMOVABLE L/E NR 341DT FOUND WITH EXISTING EXTERIOR DOUBLER INSTALLED. RT HORIZONTAL STAB REMOVEABLE L/E #341DT EXISTING EXTERIOR DOUBLER REMOVED AS PER SRM 51-31-01 VOL.II. WEB AND RIBS REMOVED AND REWORKED AS PER SRM 55-20-00 VOL.I FIG.5Sep 1, 2006 · N522FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA03158Block · damagedFOUND EXISTING REPAIR AT CENTER LANDING GEAR PILLOW BLOCK. CTR LANDING GEAR PILLOW BLOCK REMOVED AND REPLACED AS PER CMM 32-15-01 AND OPERATIONAL CHECK CARRIED OUT AS PER AMM 32-31-00 FOUND SATISFACTORY. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.Sep 1, 2006 · N522FE · Doug MD11 · Main Landing GearSDR 06FDEA03120Skin · damagedEXISTING DOUBLER REPAIR FOUND AT STA 1937 AND STA 1959 AFT LAV AIR EXHAUST PORT. REPAIR CARRIED OUT AS PER E.A.1-5330-103543 TITLE: SKINS AND PLATES- VACUUM WASTE PORTS DELETION AT BS 1937 AND BS 1959 RESPECTIVELY, BETWEEN LONGERON 39R AND 40R. REPAIR CAug 28, 2006 · N522FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03119Spar Cap · corrodedHORIZONTAL STAB BARREL NUT BORE NR 01 RT FOUND CORROSION. REPAIRED AS PER E.A.1-5510-95657 ATTACHMENT 2 - A.D. 2003-22-08 - STABILIZER- HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 28, 2006 · N522FE · Doug MD11 · Horizontal Stabilizer, Spar/RibSDR 06FDEA03118Seat Track · corrodedAFT CABIN CORROSION ON SEAT TRACK CROWN AT STA 1341 TO STA 1358 X=- 75. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.1 AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLAug 28, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03117Seat Track · corrodedMID-CABIN CORROSION ON SEAT TRACK BASE AND CROWN AT STA 745 TO STA 832 RBL 27.5". REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I AND CARRY OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG.1 VOL.I. Aug 28, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03116Seat Track · corrodedFOUND CABIN SEAT TRACK FLANGE, BASE AND CROWN FOUND CORRODED AT STA 808 TO STA 859 RBL 8.5". CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIGAug 28, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA02994Stringer · crackedCRACK FOUND AT THE END OF STRINGER 7 APPROX 1" OF LT WING TANK AT XORS 952 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 7 CRACK AT XORS 952 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 16, 2006 · N522FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA02995Spar Cap · corrodedHORIZ STAB CONSTANT SECTION BARREL NUT NR 1 LT BORE CORROSION EXCEEDED THE LIMIT PER EO1-5510-7-5000 D1 PT1. HORIZONTAL STABILIZER CONSTANT SECTION BARREL NUT NR 1 LT BORE REPAIRED AS PER EA1-5510-95657 ATTACHMENT 1-A.D 2003-22-08- STABILIZERS, HORIZONTAL STAAug 16, 2006 · N522FE · Doug MD11 · Horizontal Stabilizer, Spar/RibSDR 06FDEA02993Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FLANGE AND CROWN AT STA 859 TO STA 824 RBL 27.5. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I AND CARRIED OUT. REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG VOL.I. CLASSIFIAug 16, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2995Structure · corrodedHORZ STAB CONSTANT SECTION BARREL NUT NR 1 R BORE CORROSION EXCEEDED THE LIMIT IAW EO 1-5510-7-5000 D1 P1.Aug 16, 2006 · N522FE · Doug MD11 · Horizontal Stabilizer StructureSDR 06FDEA2994Stringer · crackedSNRM N00786: CRACK FOUND AT THE END OF STRINGER 7 APPROX. 1 INCH OF LT WING TANK AT XORS 952 DURING HFEC INSPECTION.Aug 16, 2006 · N522FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2993Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FLANGE AND CROWN AT STA 859 TO STA 824 RBL 27.5.Aug 16, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA02970Seat Track · corrodedSEAT TRACK FLANGE AND CROWN FOUND CORRODED ON STA 919 TO STA 1019 LBL 8.5. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL.I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL.I. CLASSIFIED MAAug 14, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA02971Seat Track · corrodedSEAT TRACK BASE AND CROWN FOUND CORRODED ON STA 939 TO STA 1019 RBL 8.5. REMOVED CORROSION AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL.1. CLASSIFIED MAAug 14, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2970Seat Track · corrodedSEAT TRACK FLANGE AND CROWN FOUND CORRODED ON STA 919 TO STA 1019 LBL 8.5.Aug 14, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2971Seat Track · corrodedSEAT TRACK BASE AND CROWN FOUND CORRODED ON STA 939 TO STA 1019 RBL 8.5.Aug 14, 2006 · N522FE · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
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