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 99T64R501EWAFitting · crackedFOUND DURING D-CHECK, RIGHT WING FLAP STATION 410 STOP FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0. (M)Nov 22, 1999 · N605AL · Doug DC873F · Trailing Edge FlapsSDR 99T64R524EWALongeron · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1150-1160 L35R CORROSION ON TOP OF LONGERON. BLENDED 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 11/18/99. Nov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR 99T64R527EWAFrame · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1220 L36 TO L35R STATION FRAME HAS CORROSION TOP FORWARD SIDE. BLENDED OUT CORROSION USING MECHANICAL METHOD. FABRICATED REPAIR ANGLES. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 99-186 WITH APPROVED Nov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR 99T64R487EWADuct · damagedFOUND DURING D-CHECK, HOT AIR DUCTS DAMAGED THROUGH OUT MAIN CABIN. REPAIRED HOT AIR DUCTS PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/14/99. (M)Nov 22, 1999 · N605AL · Doug DC873F · Air Distribution SystemSDR 99T64R450EWARib · crackedFOUND DURING D-CHECK, CRACK IN RIB AT STATION XRS 178 MIDDLE AFT EDGE IN FLAP WELL LEFT WING. ROUTED OUT CRACK. FABRICATED REPAIR ANGLE AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 1/27/99. (M)Nov 22, 1999 · N605AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000256Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 70 AND LONGERON 31 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 53-4-1.Nov 21, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000522AP006Fitting · corrodedFOUND DURING D-CHECK, FORWARD ACCESSORY COMPT LONGERON 31R BOTH END FITTINGS CORRODED STATION 70. REMOVED FITTINGS. REMOVED CORROSION IAW DC-8 SRM 51-1-8, 51-1-21. TREATED, PRIMED AND INSTALLED FITTINGS IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21D. (M)Nov 21, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000257Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35 RIGHT BETWEEN STA 55 TO STA 70, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 SRM 51-1-20D.Nov 20, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000255Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER FORWARD CARGO DOOR JAMB FITTING AT STA 280 AND LONGERON 33 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 DCNov 20, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R498EWAFitting · corrodedFOUND DURING D-CHECK, A PIT AT STATION 280 AT L33R CORROSION INSIDE LIGHTING HOLE FORWARD DOOR FRAME. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-8 AND 51-1-20. (M)Nov 20, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R466EWALongeron · corrodedFOUND DURNIG D-CHECK, FORWARD ACCESSORY COMPT LONGERON 35 RIGHT HAS CORROSION AT PREVIOUS REPAIR DOUBLER STATION 55 TO 70. REMOVED CORROSION AND PREVIOUS REPAIR IAW DC-8 SRM 51-1-8 AND 51-1-2. FABRICATED NEW SECTION OF LONGERON. TREATED AND PRIMED IAW DC-8 Nov 20, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000269Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL CENTER TANK ATTACHMENT ANGLE BETWEEN STA 710 TO STA 720 AND BL 47R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAWNov 19, 1999 · N605AL · Doug DC873F · Wing, Center BoxSDR RRXA000233Door Frame · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR JAM TORQUE BOX FROM STA. 280 TO STA. 360.DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED AIRCRAFT TO SERVICE IAW FAA APPROVED DER ENGINEERING SKENov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, StructureSDR 20000613AP004Fitting · crackedFOUND DURING D-CHECK, C PIT DOOR UPPER AFT CUTOUT CORNER STATION 1220 L23R CRACKED FITTING. REMOVED FITTING IAW DC-8 SRM 51-1-20D. LOCATED AND DRILLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-20D. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-120D, 51-1-21, 51Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000609AP014Web · crackedFOUND DURING D-CHECK, CABIN WEB UNDER SEAT TRACK NR 1 BETWEEN STATION 140-160 CRACKED AROUND 1 INCH IN DIAMETER. REMOVED CRACKED AREA IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER IAW DC-8 SRM 51-1-4. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R682EWASkin · dentedFOUND DURING D-CHECK, DENT IN FUSELAGE AT STATION 25 L32-33L. BLENDED OUT DENT. FINISHED THE TITANIUM PER FACTORY SPECS IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/16/99. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 20000522AP020Web · damagedFOUND DURING D-CHECK, CABIN STATION 1630-1660 WEB HAS SEVERAL BROKEN OUT HOLES. REMOVED CRACKED AREA IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000522AP015Fitting · crackedFOUND DURING D-CHECK, CABIN RT SIDE STATION 781.500 XCW 47.5 CRACK ON VERTICAL FITTING ABOVE CENTER FUEL TANK. REMOVED FITTING IAW DC-8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000489Fitting · crackedDURING A MAINTENANCE VISIT FOUND LOWER CARGO DOOR JAMB FITTING CRACKED AT STA 1220 AND LONGERON 23 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-3-0.Nov 19, 1999 · N605AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000320Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND VERTICAL STABILIZER ATTACHMENT FITTING CRACKED AT STA 1781 AND 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 19, 1999 · N605AL · Doug DC873F · Empennage StructureSDR RRXA000305Frame · crackedDURING A MAINTENANCE VISIT FOUND TAIL CONE FRAME CRACKED RIGHT SIDE AT STA 1923. 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 51-1-4.Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000302Shear Tie · crackedDURING A MAINTENANCE VISIT FOUND SHEAR TIE CRACKED AT STA 660 BETWEEN LONGERONS 21 RIGHT TO 22 RIGHT. 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 ENGINEERING SKETCH Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR 99T64R494EWAFrame · corrodedFOUND DURING D-CHECK, FORWARD ACCY COMPARTMENT FRAME 70 HAS CORROSION AROUND FASTENERS FROM L30L TO L31L. REMOVED CORROSION. FABRICATED STRAP AND EXTERNAL DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/05/99. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR 99T64R499EWASkin · corrodedFOUND DURING D-CHECK, FOUND CORROSION ON FUSELAGE FROM AROUND TAIL SKID FAIRING AND AROUND DOOR 60. REMOVED CORROSION. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/18/99. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 99T64R520EWASkin · corrodedFOUND DURING D-CHECK, RIGHT WING NR 3 STUB WING TRAILING EDGE UPPER SCREW HOLES CORRODED AND ELONGATED, XFS 233-245. REAMED HOLES TO .375 COUNTER SINK TO .65. FABRICATED PLUGS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/15/99. (M)Nov 19, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 99T64R530EWAShear Tie · crackedFOUND DURING D-CHECK, SHEAR TIE CRACKED AT FRAME STATION 660 L21-22R. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/15/99. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000424AP031Rib · damagedFOUND DURING D-CHECK, THROUGH ACCESS PANEL 602 IN TAILCONE ON RIGHT SIDE STATION 1923 1ST RIB PASSED PANEL AFT WORN AREA IN RIB. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-21. (M)Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000219Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1540 XCW 53 RT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT CORROSION BY MECHANICAL METHOD. ORIGINAL THICKNESS .132 FINAL THICKNNov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000204Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON NR 3 RIGHT HAND STUB-WING TRAILING EDGE UPPER SCREWS HOLES XFS 233 TO XFS 245. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REAMED HOLES AND FABRICATED PLUGS ANov 19, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000200Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FUSELAGE SKIN UNDER TAIL SKID FAIRING. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.Nov 19, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000258Floor Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT AT STA 1680, 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 51-1-21.Nov 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R681EWADuct · crackedFOUND DURING D-CHECK, CABIN AIR DISTRIBUTION DUCT HAS TWO CRACKS ON TOP AT APPROX STATION 1345/1348. STOP DRILLED CRACKS. NDT CONFIRMED CRACKS HAD BEEN STOPPED. WELDED CRACKS. NDT WELDS NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/14/99. (Nov 18, 1999 · N605AL · Doug DC873F · Air Distribution SystemSDR 20000522AP022Seat Track · brokenFOUND DURING D-CHECK, FUSELAGE SEAT TRACK BROKEN AND WORN FROM STATION 1550-1585 TRACK 2-3. REMOVED SEAT TRACK IAW DC-8 SRM 53-2-3. FABRICATED TRACK SPLICE. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-3, 51-1-8 AND 53-1-0. (M)Nov 18, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000522AP021Brace · corrodedFOUND DURING D-CHECK, CABIN SCREW HOLE HAS CORROSION AT FLOOR BRACE AT STATION 1680. REMOVED CORROSION IAW DC-8 SRM 51-1-8. REMOVED FLOOR BRACE. FABRICATED FLOOR BRACE TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-21. (M)Nov 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000493Frame · crackedDURING A MAINTENANCE VISIT FOUND L1 DOOR FRAME CRACKED. 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 99-168.Nov 18, 1999 · N605AL · Doug DC873F · Passenger/Crew DoorsSDR RRXA000492Frame · crackedDURING A MAINTENANCE VISIT FOUND R2 PASSENGER DOOR FRAME CRACKED. 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 99-186.Nov 18, 1999 · N605AL · Doug DC873F · Passenger/Crew DoorsSDR RRXA000491Frame · crackedDURING A MAINTENANCE VISIT FOUND R1 PASSENGER DOOR FRAME CRACKED. 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 99-186.Nov 18, 1999 · N605AL · Doug DC873F · Passenger/Crew DoorsSDR RRXA000478Seat Track · damagedDURING A MAINTENANCE VISIT FOUND SEAT TRACK BETWEEN STA 1550 TO STA 1585 AND BL 0. 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.Nov 18, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 99T64R541EWAThreshold · crackedFOUND DURING D-CHECK, R1 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/17/99. (M)Nov 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R542EWAThreshold · crackedFOUND DURING D-CHECK, R2 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219, NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/17/99. (M)Nov 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR T64R543EWAThreshold · crackedFOUND DURING D-CHECK, L1 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK AND WELDED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/17/99. (M)Nov 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000522AP029Seat Track · wornFOUND DURING D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATION 1300 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. INSTALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M)Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000522AP028Seat Track · wornFOUND DURING D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATIN 1560 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 51-1-21. INSTALLED TRACK REPAIR IAW DC-8 SRM 51-1-21. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M)Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000522AP027Seat Track · wornFOUND DURING D-CHECK, CABIN SEAT TRACK NR 3 STATION 1580-1610 XCW 55 LEFT WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 51-1-21. INSTALLED TRACK REPAIR IAW DC-8 SRM 51-1-21. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M)Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000330Seat Track · damagedDURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 240 AND BL 0. 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.Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000329Seat Track · damagedDURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 600 AND BL 60 RIGHT. 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.Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000327Seat Track · damagedDURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK BETWEEN STA 1580 TO STA 1610 AND BL 55 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DC-8 SRM 51-1-21.Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000326Seat Track · damagedDURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK DAMAGE AT 1560 AND BL 69 RIGHT. 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 51-1-21.Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000325Seat Track · damagedDURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK AT STA 1300 AND BL 69 RIGHT. 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.Nov 17, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 99T64R495EWASplice · crackedFOUND DURING D-CHECK, B PIT BETWEEN STATION 200-220 AT L31L CRACK IN DOUBLER IN FACTORY SPLICE. REMOVED FITTING. FABRICATED NEW SPLICE FITTING AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20. (M)Nov 17, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous Structure
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