Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR UPS00832438Floor Support · corrodedINSPECTION TYPE:C2, FWD PIT STA 100 RT FLOORBEAM SUPPORT LOWER END CORRODED. REMOVED STANTION AT STA 100 RT IAW DC8 SRM 51-1-20D, OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW STANTION (P/N 3773077-510N), PO 256499, DRILLED STANTION IAW DAC 3773077. ALODINApr 10, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832437Fitting · crackedINSPECTION TYPE:C2 AFT LWR CARGO PIT AT FS 1270 LONG 31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.Apr 10, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832496Frame · corrodedINSPECTION TYPE:C2, AFT PIT FS 1060 CORROSION ON LWR SURFACE OF UPPER FRAME FLANGE AT L36, L34L & L35L & ALSO ON FRAME CAP AT L36. REMOVED DAMAGED SECTION OF FRAME. FABBED REPAIR PARTS. ALODINED AND PRIMED REPAIR PARTS AND DAMAGED AREA. INSTALLED REPAIR IAApr 9, 2000 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832506Fitting · corrodedINSPECTION TYPE:C2, AFT LOWER CARGO PIT A FS 1195 BETWEEN L33R -L34R CROSS SLIDE DOOR 4TH FROM FWD LATCH FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED FITTING IAW DC8 SRM 51-1-20D & 53-2-0.Apr 9, 2000 · N818UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS00832457Web · corrodedINSPECTION TYPE:C2, AFT LWR PIT AT FS 1180 BETWEEN LONG 33R - 34R DOORWAY WEB IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. GEN AND RECRFTS 818UP-14-20292 W/REO G07302. FAB DOUBLERS IAW REO G07302. ALODINEApr 9, 2000 · N818UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS00832456Fitting · corrodedINSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1190 BETWEEN L33R - 34R 3RD FROM FWD CROSS SLI DE DOOR LATCH FITTING CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC 8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED ANApr 9, 2000 · N818UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS00832445Fitting · corrodedINSPECTION TYPE:C2, FITTING CORRODED AT FS 1200 L31L AFT LOWER CARGO COMPARTMENT. REMOVED CORRODED FITTING, LOCATE NEW FITTING AND DRILL EXISTING FAST ENER HOLES AND INSTALLED NEW FITTING.Apr 9, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002018Cowl Door · damagedDURING A MAINTENANCE VISIT FOUND A LARGE SCRATCH AND CREASE ACROSS RT FWD COWL DOOR LWR SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-055 WITH APPROVED 8110-3 DApr 8, 2000 · N961R · Doug DC873F · Engine Cowling SystemSDR RRXA001884Cowl Door · damagedDURING A MAINTENANCE VISIT FOUND A LARGE SCRATCH AND CREASE ACROSS RT FWD COWL DOOR LWR SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FILLED CREASES AND GOUGES WITH A ERODINAMIC DECON PUTTY AND PAINTED IApr 8, 2000 · N961R · Doug DC873F · Engine Cowl FlapsSDR UPS00832507Frame · crackedINSPECTION TYPE:C2, MAIN CABIN STA 1540 AT L21L (CUSP) FRAME ATTACHMENT. REMOVED AND REPLACED FRAME SECTION IAW DC8 SRM 53-2-0, FIG 2.Apr 8, 2000 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832465Attach Fitting · crackedINSPECTION TYPE:C2, CABIN STA 320 L21L, A FRAME TO CUSP ATTACH FITTING, CRACKED FRAME. REMOVED DAMAGED SECTION OF FRAME, INSTALLED NEW FRAME SECTION AND SPLICES IAW DC8 SRM 53-2-0 FIG AND 51-7-20D.Apr 8, 2000 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00832464Frame · corrodedINSPECTION TYPE:C2, CABIN STA 1040 L21L AT ATTACH FITTING, FRAME, CRACKED AND CORRODED. REMOVED CORRODED FRAME SECTION AT FS 1040 TO L18L-L21L. FABRICATED NEW SECTION IAW DC8 SRM 53-0265. FABRICATED -29, -31, -33 & -35 REP AIR SPLICES IAW DC8 SRM 53-2-0. AApr 8, 2000 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832463Web · corrodedINSPECTION TYPE:C2, CABIN STA 409 L21L CUSP CORRODED AS MARKED. REMOVED CORROSION AND REPAIRED AREA IAW REO-G07299.Apr 8, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080410CAngle · crackedFWD BAGGAGE COMPARTMENT FRAME REINFORCING ANGLE CRACKED 1 INCH AT STA 400 L-34 RT. STOP DRILLED AND INSTALLED DOUBLER IAW SRM 51-1-21 AND 53-2-0.Apr 8, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002028Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 RT AND RBL 25.5 INCHES TO 27 INCHES 34.5 INCHES TO 34.75 INCHES & 35.5 INCHES TO 35.75 INCHES Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED ANApr 6, 2000 · N961R · Doug DC873F · Fuselage Main, BulkheadSDR RRXA002027Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 LT AND LBL 24.25 INCHES TO 27.25 INCHES & 33.5 INCHES TO 36.25 INCHES LBL Z AXIS + 65.5 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREAApr 6, 2000 · N961R · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001916Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER SURFACE OF THE RT I/B AUX TANK FROM STA XFS 13 TO 135, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAWApr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001915Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGED AND A SCREW MISSING ON THE UPPER SURFACE RT LEADING EDGE STUB WING AT STA XFS 550, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLEApr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001898Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING LWR AUX SPAR PANEL AT XW 90 TO XW 138, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0. CORROSIApr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001897Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING LWR AILERON POWER PACK AT PANEL NR 540, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PANEL NR 540 IAW DC-8 SRM, Apr 6, 2000 · N961R · Doug DC873F · AileronsSDR RRXA001894Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 RT AND RBL 25.5 TO 27, 34.5 TO 34.75 AND 35.5 TO 35.75 Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABApr 6, 2000 · N961R · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001893Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 LT AND LBL 24.25 TO 27.25 & 33.5 TO 36.25 LBL Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AApr 6, 2000 · N961R · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001780Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE UPPER SURFACE ON THE RT IB AUX TANK AT STA XFS 13 TO 135, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED IAApr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001779Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE SCREW HOLE ON THE UPPER SURFACE RT LE STUB WING AT STA XFS 550, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED FASTENER PER E.O. 00Apr 6, 2000 · N961R · Doug DC873F · Leading Edge DevicesSDR RRXA001762Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING LWR. AUX SPAR PANEL AT XW 90 TO XW 138, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLEED NEW PANEL IAW DC-8 SRM 51-3-0.Apr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001761Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING LWR. AILERON POWER PACK PANEL NR 540, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0.Apr 6, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR UPS00832508Fitting · corrodedINSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1180 CROSSSLIDE DOOR WAY 2ND FROM FWD LATCH FITTING IS CORRODED AT LONG 33R. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGE IAW DC8 SRM 51-1-20D. LOCATED AND DRApr 6, 2000 · N818UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL200080411CFloor Support · crackedMAIN CARGO COMPARTMENT NR 1D FLOOR CRACKED 1 INCH. STOP DRILLED AND INSTALLED DOUBLER IAW SRM 53-2-3 AND 51-1-8.Apr 6, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832317Angle · corrodedINSPECTION TYPE:C1, STA 270 - 280 LONG 27R INTERCOSTAL ATTACH ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754020 AND SRM 51-1-20D.Apr 6, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832310Fitting · crackedINSPECTION TYPE:C1, WING BOX STA 680 LBL 60 FITTING IS CRACKED, UPPER SPAR CAP TO FRAME FITTING. REMOVED AND REPLACED FITTING IAW DWG 3642974 AND SRM 51-1-20D.Apr 6, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000225Oil Cap · unsecureLOST OIL PRESSURE & QUANTITY ON NR 4 ENGINE AT 1439Z. PERFORMED CHECKLIST FOR ABNORMAL OIL PRESSURE, SHUT ENGINE DOWN, MONITORED ALL OTHER ENGINE FUNCTIONS UNTIL LDG AT MCO. CORRECTIVE ACTION : FOUND OIL CAP OFF, PUT CAP BACK ON. SERVICED WITH OIL, RANApr 6, 2000 · N870TV · Doug DC873F · Turbine Engine Oil SystemSDR RRXA001938Skin · damagedDURING A MAINTENANCE VISIT FOUND THAT THE WING SKIN AT STR 64 LT WING NEEDED TO BE MODIFIED PER MA-AM-5732-03:00, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. COMPLIED WITH LOWER WING SKIN MODIFICATION STRINGER 64 IAW EWA EO AM-5732-04:00.Apr 5, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001917Skin · damagedDURING A MAINTENANCE VISIT FOUND THE LWR WING SKIN AT STR 64 RT WING NEEDED MODIFICATION PER EWA MA-AM-5732-04:00, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. MODIFIED LWR WING SKIN AT STR 64 RT IAW EWA EO AM-5732-04:00.Apr 5, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001803Skin · damagedDURING A MAINTENANCE VISIT FOUND THAT THE LWR WING SKIN AT STR 64 LT WING NEEDED TO BE MODIFIED PER EWA MA-AM-5732-03:00, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. COMPLIED WITH LOWER WING SKIN MODIFICATION STRINGER 64 IAW EWA EO AM-5732-03:0Apr 5, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA000685Door Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO DOOR 62 DOOR JAMB L/H FWD CORNER AND R/H CENTER AREA, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIRED PART AND INSTALLED IAW DC-8 SRM 53-2-0.Apr 5, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR RRXA002023Skin · gougedDURING A MAINTENANCE VISIT FOUND SEVERAL GOUGES AROUND OUTSIDE OF C-PIT DOOR (EXTERNAL), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 52-4-2 AND 51-1-21.Apr 5, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001959Structure · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN TWO PLACES AT SCREW HOLES ON THE LT CHIN SCOOP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0 AND EO NR 00-055.Apr 5, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001950Plate · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE B-PIT KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND EO NR 00-055 WITH APPROVED 8110-3 DATED 4-4-0Apr 5, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001932Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND THE SCREW HOLES AT THE LT WING I/B LEADING EDGE UPPER SURFACE SKIN AT STA XFS 113.750 TO XFS 10.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8Apr 5, 2000 · N961R · Doug DC873F · Wing Miscellaneous StructureSDR RRXA001889Skin · gougedDURING A MAINTENANCE VISIT FOUND SEVERAL GOUGES TO THE C-PIT DOOR AROUND OUTSIDE OF DOOR (EXTERNAL), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 52-4-2 AApr 5, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001824Structure · crackedDURING A MAINTENANCE VISIT FOUND CRACKS TO THE SCREW HOLES IN THE LT CHIN SCOOP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKS AND INSTALLED SCOOP IAW DC-8 SRM 51-3-0.Apr 5, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001815Plate · gougedDURING A MAINTENANCE VISIT FOUND THE B-PIT KICK PLATE GOUGED, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FORMED KICK PLATE BACK TO ORIGINAL CONTOUR, STOP DRILLED CRACK AND INSTALLED IAW DC-8 SRM 51-1-21 AND EOApr 5, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001797Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLES AT LT WING I/B LEADING EDGE UPPER SURFACE AT STA XFS 113.750 TO XFS 10.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATEDApr 5, 2000 · N961R · Doug DC873F · Leading Edge DevicesSDR RRXA001781Skin · damagedDURING A MAINTENANCE VISIT FOUND THAT THE LWR. WING SKIN NEEDED TO BE MODIFIED AT STR. 64 RT. AND XRS 445, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. MODIFIED LWR. WING SKIN AT STR. 64 RT. IAW EWA E.O. AM-5Apr 5, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA002025Skin · bulgedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE SKIN LOWER LOBE AT STA 360 & 380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 ANApr 4, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001997Frame · damagedDURING A MAINTENANCE VISIT FOUND A GIL LINER RIVET HOLE DRILLED IN RADIUS OF FRAME IN MAIN CABIN AT STA 1480, 8 INCHES UP FROM CUSP LINE L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED ANDApr 4, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001986Frame · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START IN RADIUS OF FRAME & SHEAR FOOT AT STA 1480, 3 INCHES UP FROM CUSP L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EApr 4, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001967Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR HINGE BEAM ATTACH CLIP AT STA 898, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW CLIP IAW DC-8 SRM 5Apr 4, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA001891Skin · bulgedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE SKIN LOWER LOBE AT STA 360 AND 380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 Apr 4, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001862Frame · misdrilledDURING A MAINTENANCE VISIT FOUND A HOLE DRILLED IN THE RADIUS OF FRAME MAIN CABIN GILL LINER AT STA 1480, 8 INCHES FROM CUSP LINE AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIApr 4, 2000 · N961R · Doug DC873F · Fuselage Main, Frame
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