Douglas DC-8-73F

Service difficulty reports · 15,471

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'DC873F'
  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 RRXA991523Bogie Trim Cyl · failedAFTER TAKEOFF, ON GEAR RETRACTION, GEAR NOT LATCHED LIGHT AND DOOR NOT LATCHED LIGHT CAME ON WITH GEAR RETRACTED. FOUND RIGHT BOGIE TRIM CYLINDER AFT BOLT BROKEN CAUSING GEAR NOT TO BE ALL THE WAY IN THE WELL. REMOVED AND REPLACED BOGIE TRIM CYLINDER OPS ANDNov 6, 1999 · N831AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA000307Skin · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING LEADING EDGE WITH 6 INCH CRACK AT XW 257.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99Nov 5, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000301Skin · damagedDURING A MAINTENANCE VISIT REMOVED TEMPORARY REPAIR FROM LEFT WING LEADING EDGE AT XFS 250. REMOVED TEMPORARY REPAIR, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186.Nov 5, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 99T64R464EWASkin · crackedFOUND DURING D-CHECK, RIHT WING L/E NR 3 STUB WING UPPER INBOARD EDGE HAS 6 INCH CRACK STATION EX 257.50. COMBINED REPAIR, ALSO TASK 1B178. CUT OUT DAMAGED AREA. FABRICATED REPLACEMENT SECTION FOR SECTION REMOVED. FABRICATED SPLICE PLATES. TREATED, PRIMEDNov 5, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 99T64R481EWASkin · damagedFOUND DURING D-CHECK, NR 2 ENGINE STUB WING SCREWS PULLING THROUGH COUNTER SINKS FR XS 250. REMOVED TEMPORARY REPAIR, TREATED, PRIMED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/27/99. (M)Nov 5, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 99T64R482EWAFitting · chafedFOUND DURING D-CHECK, NR 2 FLAP CANOE XW 98 T/E CHAFFED. REMOVED GOUGES BY BLENDING. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M)Nov 5, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR 99T64R490EWASkin · looseFOUND DURING D-CHECK, NR 2 ENGINE STUB WING TEMP REPAIR FR XS 246 - XS 233 PULLING LOOSE BOTTOM SIDE. REMOVED TEMPORARY REPAIR. TREATED AND PRIMED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/27/99. (M)Nov 5, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 20000522AP017Fitting · crackedFOUND DURING D-CHECK, CABIN CRACKED HORIZONTAL FITTING STATION 798 XCW 47.5 LEFT. REMOVED FITTING IAW DC-8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 51-1-20D. (M)Nov 4, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000318Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND HORIZONTAL STABILIZER LEFT SIDE ATTACHMENT FITTING CRACKED AT XCW 47.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW ATTACHMENT FITTING IAW DC-8 SRM 51-1-20D.Nov 4, 1999 · N605AL · Doug DC873F · Horizontal Stabilizer StructureSDR 99T64R478EWAFitting · gougedFOUND DURING D-CHECK, NR 3 CANOE FITTING INBOARD AFT SIDE IS GOUGED. REMOVED GOUGES BY BLENDING SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/02/99. (M)Nov 3, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000310Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND UPPER CARGO DOOR JAMB FRAME ATTACHMENT FITTING CRACKED AT STA 120 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FRAME ATTACHMENT FITTING IAW Nov 2, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR 99T64R447EWAFitting · crackedFOUND DURING D-CHECK, CRACK IN UPPER CUSP CARGO DOOR FRAME ATTACH FITTING FRAME STATION 120 FORWARD ATTACH FITTING. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-8, 51-3-0 AND 51-1-20D. (M)Nov 2, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99831050Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY IAW MM 33-50-00, OPS CHECK NORMAL.Nov 2, 1999 · N802UP · Doug DC873F · Emergency LightingSDR 20000522AP019Floorbeam · corrodedFOUND DURING D-CHECK, CABIN CORROSION ON FLOORBEAM AT STATION 1320 BETWEEN 5-6 TRACK. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Nov 1, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR 20000424AP034Frame · corrodedFOUND DURING D-CHECK, CORROSION ON FRAME 1793 IN CHANNEL L32L TO L32R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND 51-1-20D. (M)Nov 1, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000222Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1320 BETWEEN SEAT TRACK NR 5 AND 6. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC-8 SRM 51-1Nov 1, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99831051Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50-01 PAGE 202.Nov 1, 1999 · N802UP · Doug DC873F · Emergency LightingSDR 99T64R485EWAWeb · corrodedFOUND DURING D-CHECK, FORWARD RIGHT TYPE 1 DOOR BELOW ON FLOOR WEB UNDERNEATH DOOR MOUNTING BRACKET HAS CORROSION. REMOVED CORROSION BY MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED Oct 29, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R486EWAWeb · corrodedFOUND DURING D-CHECK, FORWARD LT TYPE 1 DOOR BELOW ON FLOORWEB UNDERNEATH DOOR MOUNTING BRACKET HAS CORROSION. REMOVED CORROSION BY MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/2Oct 29, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000218Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1500 XCW 40 AND XCW 53 RT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 51-1-8, 51-1-20 AOct 29, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000202Web · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FLOOR WEB BELOW R1 ENTRY DOOR. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROOct 29, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000316Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND CUSP ATTACHMENT FITTING CRACKED AT STA 1160 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW CUSP ATTACHMENT FITTING IAW DC-8 SRM 51-1-20D.Oct 28, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR T64R675EWASkin · corrodedFOUND DURING D-CHECK, NR 3 RIGHT STUB WING UPPER FASTENER HOLES L/E ATTACH POINT HAVE CORROSION. BLEND OUT CORROSION USING MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/26/99. (MOct 28, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000203Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON NR 3 RIGHT HAND STUB-WING UPPER FASTENER ATTACH HOLES. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW FAA APPROVED DER ENGINEERING SKETCHOct 28, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 20000609AP005Longeron · crackedFOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1240 L35R TOP OF LONGERON METAL STRIP CRACKED. REMOVED BRACKET IAW DC-8 SRM 51-3-20. FABRICATED METAL STRIP IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M)Oct 27, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR 99T64R489EWAPipe · gougedFOUND DURING D-CHECK, FUEL PIPE ASSY P/N 7751562590 HAS 3 DEEP GOUGES AND COUPLING THREADS HAVE DAMAGE. DRILLED NR 30 HOLE IN CENTER OF 3 GOUGES. FABRICATED PATCH AND WELDED IN PLACE. NDT WELD, NO FLAWS FOUND. PRESSURE TESTED TO 90 PSI, NO LEAKS FOUND. DROct 27, 1999 · N605AL · Doug DC873F · Engine Fuel DistributionSDR 99T64R492EWAFloorbeam · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPARTMENT STATION 822 LEFT XCW 51 FLOORBEAM HAS AREA OF EXFOLIATION. (M)Oct 27, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR 99T64R479EWASkin · damagedFOUND DURING D-CHECK, LEFT INBOARD WING LE 9 TOP MOUNT HOLE COUNTER SINKS ELONGATED. (M)Oct 26, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000266Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 80 TO STA 100 AND LONGERON 13 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-2Oct 25, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR 20000522AP018Floorbeam · corrodedFOUND DURING D-CHECK, CABIN STATION 1140 XCW 60 LEFT FLOORBEAM AREA EXFOLIATED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. (M)Oct 25, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000315Frame · crackedDURING A MAINTENANCE VISIT FOUND FRAME CRACKED AT STA 1580 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Oct 25, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR 99T64R468EWAFrame · crackedFOUND DURING D-CHECK, UPPER CARGO COMPT STATION 1580 UPPER CUSP LINE FRAME CRACKED AND BENT LONGERON 21 LEFT. CUTOUT DAMAGED SECTION IAW DC-8 SRM 53-2-0. FABRICATED REPAIR FILLER AND DOUBLER IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTOct 25, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000217Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1140 XCW 60 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D. (CORROct 25, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000252Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING BETWEEN STA 1160 TO STA 1180 AND LONGERON 26 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 5Oct 24, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000522AP014Floorboard · crackedFOUND DURING D-CHECK, FOUND CABIN STATION 1380 FLOOR MEMBRANE CRACKED AT FLOORBEAM. REMOVED MEMBRANE IAW DC-8 SRM 51-1-21. FABRICATED MEMBRANE, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-4, 51-1-8, 51-1-21. (M)Oct 24, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR 20000522AP024Fitting · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1160-1180 L26R END OF LONGERON HAS CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FITTING IAW DC-8 SRM 51-1-4, 51-1-21. TREATED AND PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. Oct 24, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000321Floorboard · crackedDURING A MAINTENANCE VISIT FOUND FLOOR PANEL MEMBRANE AT STA 1380 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED MEMBRANE IAW DC-8 SRM 51-1-21.Oct 24, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR DHL99802003Mec · unservicableNR 3 ENGINE N1 OCCILATION AND MODERATE VIBRATIONS CONCURRENT WITH OCCILATIONS. PRECAUTIONARY SHUTDOWN. CHANGED NR 3 MEC AND CIT SENSOR. OPS AND LEAK CHECK OK PER MM 73-20-1 AND 73-20-2.Oct 23, 1999 · N802DH · Doug DC873F · Fuel Control/Turbine EnginesSDR UPS99830986Wire · brokenINSPECTION TYPE:N/A, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE ON LANDING IN ONT. AFTER CHECKLIST COMPLETE, A NORMAL LANDING WAS MADE. GEAR PINNED. REPLACED BROKEN WIRE BETWEEN TERMINAL BOARD S3-5 AND L/G DOWN LIMIT SWITCH. WIRE G322E24. LEFT LANDINOct 22, 1999 · N880UP · Doug DC873F · Landing Gear System WiringSDR UPS99830978Battery · dischargedINSPECTION TYPE:N/A, DURING MX INSPECTION EMERGENCY LIGHT FAILED TO TEST. *S/D* REMOVED AND REPLACED BATTERY PACK.Oct 22, 1999 · N880UP · Doug DC873F · Emergency LightingSDR UPS99830968Light · inopON APPROACH TO ONT, RIGHT WING LANDING LIGHT FAILED TO ILLUMINATE WITH SWITH ON. PERFORMED T/S PER FIM 33-42-00 FIG 107, RELAMPED PER MM 33-42-03.Oct 22, 1999 · N880UP · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS99830967Battery Pack · dischargedEMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.Oct 21, 1999 · N880UP · Doug DC873F · Emergency LightingSDR 99T64R493EWASkin · corrodedFOUND DURING D-CHECK, FORWARD ACCY COMPT CORROSION UNDER DOME NUT AIR CONDITION FRAME JUST ABOVE LONGERON 31 RT STATION 42. BLENDED CORROSION USING MECHANICAL METHOD NOT TO EXCEED .128 REMAINING THICKNESS. TREAT AND PRIME PER EO NR 99-186 WITH APPROVED 8110-Oct 20, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000231Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD ACCESSORY COMPARTMENT SKIN ABOVE LONGERON 31 RT AT FUSELAGE STA 42.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER Oct 20, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000313Floorboard · crackedDURING A MAINTENANCE VISIT FOUND FLOOR PANEL CRACKED BETWEEN STA 760 TO 1100. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3.Oct 19, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR 99T64R473EWASeat Track · corrodedFOUND DURING D-CHECK, UPPER CARGO CARGO COMPT SEAT TRACK XCW.0 STATION 1540 EXFOLIATED.Oct 19, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000424AP024Floorboard · crackedFOUND DURING D-CHECK, UPPER CARGO COMPT FLOOR PANEL 760-1100, 5-6 INCH CRACK ON FLOOR PANEL. CUT OUT DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND 53-2-3 AND 51-1-21. (M)Oct 19, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR UPS99830963Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK ASSY PER MM 33-50-01.Oct 19, 1999 · N809UP · Doug DC873F · Emergency LightingSDR UPS99830950Battery Pack · dischargedINSPECTION TYPE:N/A, DURING MECHANICS PRE-DEPARTURE EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK, SYS OPS NORMAL PER 33-50-01.Oct 19, 1999 · N868UP · Doug DC873F · Emergency LightingSDR 99T64R470EWAFloorbeam · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT CORROSION ON FLOORBEAM SEAT TRACK ATTACH POINT XCW 40 RIGHT STATION 1440. (M)Oct 18, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor Beam
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