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 RRXA991386Finger Dougler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULGE AND RIVETS POPPED ON FINGER DOUBLER AT STA -82 TO STA -67 RIGHT HAND SIDE BL 60 RIGHT, 10 BELOW COCKPIT FLOOR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jun 8, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829976Fitting · crackedINSPECTION TYPE:C-1, CROSS SLIDE RAMP MOUNT ATTACH FIG CRACKED FS 340 ABOVE L 35L. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8-SRM 53-2-0 & 51-1-20D.Jun 7, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829893Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L-10R FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED, LOCATED AND DRILLED NEW FITTING AT STA 680 AND L-10R IAW DC-8 SRM 51-3-2. INSTALLED FITTING IAW DC- 8 SRM 51-1-20D. TORQUED BOLT IAW DC-8 SRJun 7, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829892Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L6L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING, TORQUED BOLT.Jun 7, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829891Fitting · crackedINSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L4L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED FITTING. INSTALLED NEW FITTING, TORQUED BOLT.Jun 7, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829772Battery Pack · dischargedINSPECTION TYPE:N/A, DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL.Jun 7, 1999 · N836UP · Doug DC873F · Emergency LightingSDR RRXA991413Skin · chafedDURING A MAINTENANCE VISIT, FOUND LEFT WING CENTER L/E HAS SCREWS AND WASHERS WEARING INTO SKIN BY I/B SLOT DOOR AT STA 250.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER FROJun 7, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829894Fitting · crackedINSPECTION TYPE:C1, INTERCOSTAL FITTING FWD SIDE OF FS 1140 FRAME ABOUT I/B HALF OF LONGERON 33 RT IS CRACKED. REMOVED CRACKED FITTING, RECEIVED NEW FITTING (P/N 4758514-521N). LOCATED, DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING.Jun 6, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991595Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BETWEEN STA 50 AND STA 70, AND AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21. Jun 6, 1999 · N604AL · Doug DC873F · Fuselage Main, FrameSDR UPS99829959Fitting · crackedINSPECTION TYPE:C-1, BANANA FITTING FS 1220 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING. RECEIVED NEW FITTING, DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Jun 5, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829958Fitting · crackedINSPECTION TYPE:C-1, BANANA FITTING FS 1228 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING, RECEIVED NEW FITTING. DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Jun 5, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829896Fitting · crackedINSPECTION TYPE:C, INTERCOSTAL FITTING, AT FS 1228 ABOVE O/B HALF OF LONGERON 33 RT IS CRACKED ON UPPER AFT LEG. REMOVED INTERCOSTAL FITTING IAW DC-8 SRM 51-1-20D, RECEIVED FITTING NR 4758514-519N PO NR 294625 AND DRILLED UP IAW DC-8 SRM 51-1-20D, INSTALLED FJun 5, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829895Fitting · crackedINSPECTION TYPE:C1, LONGERON 36 AT FS 1270 SPLICE FITTING IS CRACKED. RECEIVED, LOCATED AND DRILLED NEW LONGERON SPLICE FITTING (P/N 375922 2-1) IAW DC-8 SRM 51-3-2. INSTALLED NEW FITTING IAW DAC DWG NR 5750322.Jun 5, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829971Fitting · crackedINSPECTION TYPE:C-1, LONG 24R FITTING AT STA 920 IS CRACKED ON AFT SIDE DOT L122. REMOVED FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, DC8 SRM 51-3-0, 51-1-20D. INSTALLED SPOILER PULLEY BRACKET AND UPLOCK ASSEMBLY IAW DC8 SRM 51-3-0 AND MM 32-31-Jun 4, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991409Skin · gougedDURING A MAINTENANCE VISIT FOUND SMALL GOUGE IN SKIN FWD OF EXTERNAL POWER RECEPTACLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED GOUGE. FABRICATED AND INSTALLED ANGLE IAW FAA APPROVED TENNESSEE TECHNICAJun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991406Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE SKIN BY AFT CARGO DOOR STA 1445, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESJun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991405Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE SKIN AT STA 1400, AT DOOR LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROED TENNESSEE TECHJun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991402Skin · crackedDURING A MAINTENANCE VISIT, FOUND A-PIT DOOR CUT-OUT BOTTOM SKIN CRACK AND CHIPPED OFF, ALSO GOUGES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNEJun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991393Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LOWER SKIN AT STA 1420, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNIJun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991391Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN UNDER A PIT DOOR CORRODED AND MISSING LAYER AT STA 320, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS Jun 4, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991601Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN, AT STA 1688, FLOOR PANEL A CORRODED AND CRACKED AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOORBOAJun 3, 1999 · N604AL · Doug DC873F · Fuselage Floor PanelSDR RRXA991616Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CUSP FRAME SUPPORT AND WEB AT STA 25 AND LONGERON 25 RIGHT FLOOR LEVEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DCJun 2, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991408Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E I/B EDGE 45 FWD FRONT SPAR AT STA XFS 285.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IJun 2, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991135Pin · damagedDURING A MAINTENANCE VISIT FOUND SPIRALED TOP AND BOTTOM HOLES, LEFT MLG RETRACT PIN BOSS THROUGH BOLT HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. SMOOTHED BORE, FLAP PEENED HOLE IAW FAA APPROVED TENNESSEE TJun 2, 1999 · N606AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA991134Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETRACT CYL. A PIN REPAIR PER CUSTOMER REQUEST IAW MA AI 3210-01:03 S/B 32-102, REF AD 71-25-09. ACCOMPLISHED INSPECTION, FOUND CORROSION, IN PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGEDJun 2, 1999 · N606AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA991133Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT CYL A-PIN REPAIR PER CUSTOMER REQUEST IAW MA A13210-01:03 S/B 32-102 REF. AD 71-25-09. ACCOMPLISHED INSPECTION FOUND CORROSION IN PIN BOSS.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TRJun 2, 1999 · N606AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA991132Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, RIGHT ELEV, RT GEAR TAB ASSY, I/B FITTING GOUGED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. BLENDED GEARED TAB I/B FITTING IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3 DAJun 2, 1999 · N606AL · Doug DC873F · Elevator StructureSDR RRXA991131Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 1 PYLON, I/B TRIPLER (ANGLE) CRACKED 1.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ANGLES IAW DC8 SRM 51-1-6 AND 51-1-7, 51-1-20D.Jun 2, 1999 · N606AL · Doug DC873F · Nacelle/Pylon, Attach FittingsSDR RRXA991130Fastener · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, FASTENER DAMAGED INSIDE NR 4 ALT FUEL TANK BY NR 4 PYLON AT XW 463 STR 58 LOWER SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. FASTENER OK AS IS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETJun 2, 1999 · N606AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991129Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, B-PIT LEFT FWD BETWEEN STA 460 AND STA 480 LEFT AT LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991128Float Box · twistedDURING A MAINTENANCE VISIT FOUND TUBE TWISTED, RIGHT WING, NR 4 A FLOAT BOX WELDED TUBE TWISTED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLOAT BOX, WELDED TUBE IN PLACE IAW FAA APPROVED TENNESSEE TECH Jun 2, 1999 · N606AL · Doug DC873F · Fuel StorageSDR RRXA991126Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, JUST FWD OF TAIL SKID AT STA 1746, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-1, INSTALLED FJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991125Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM UNDER SEAT TRACK 3 ABOVE LONGERON 32 LEFT AT STA 1700. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991124Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, L/E BETWEEN NR 3 AND NR 4 ENG JUST O/B OF STALL WARNING TRANSDUCER BETWEEN XSF 385 AND XFS 388. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991123Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, LOWER ATTACH FITTING IN BOX FRAME AT STA 280, LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8 AND Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991121Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS AT STA 1746 BETWEEN BL 1-1/2 LEFT AND 20-1/2. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DCJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991120Floorbeam · corrosionDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 1726, BL 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CORROSIONJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991119Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS AT STA 1700 BL 29 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (COJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991118Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680 BL 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991117Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 3 STUB WING, UPPER SURFACE EMANATING FROM RIVET 2 FWD OF FRONT SPAR AT STA XS 227.335. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991116Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680, BL 14 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SUPPORT AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991115Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, AROUND SCREW HOLES LEFT WING L/E CENTER SECTION UPPER SURFACE BETWEEN XFS 304.000 TO XFS 397.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991114Frame · crackDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE A PIT FRAME DOOR BETWEEN BOLTS AT STA 280, BETWEEN LONGERONS 26 RIGHT AND LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FRAME PER DWG Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, FrameSDR RRXA991113Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, I/B L/E TANK UPPER SURFACE AROUND SCREW HOLES BETWEEN XFS 151.205 AND XFS 157.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991112Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, TANK UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 95.000 AND XFS 101.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991111Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, C/D PIT DIVIDER AND SUPPORT FORMER CRACKED AND TORN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARTITION IAW FAA APPROVED TENNESSEE Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991110Guard · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, CABIN, LONG SECTION OF MAIN CARGO SEAL GUARD BUMP RAIL AT STA 210 (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. WELDED CRACKED AREA IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROJun 2, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991109Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, IMPROPER REPAIR LEFT WING O/B L/E O/B SECTION LWR SURFACE BETWEEN STA 822.50 TO XFS 841.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INJun 2, 1999 · N606AL · Doug DC873F · Leading Edge DevicesSDR RRXA991108Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, LEFT WING, O/B FLAP LOWER SURFACE SKIN BULGED AND 2 CRACK 3 BELOW L/E, JUST UNDER CENTER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLEJun 2, 1999 · N606AL · Doug DC873F · Trailing Edge FlapsSDR RRXA991107Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, RIGHT WING, O/B FLAP, NR 3 WEDGE I/B LOWER MOUNTING FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NUT PLATE IAW FAA APPROVED TENNESSEE TECH Jun 2, 1999 · N606AL · Doug DC873F · Trailing Edge Flaps
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