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 DHL2000803133Support Bracket · crackedAT C-CHECK, AFT CARGO COMPT PRESS WALL PANEL SUPPORT FILLET CRACKED AT FS 980.00. REMOVED RIVETS AND PERFORMED ANTI-CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2E & 2F FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12.Jan 16, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080321CSkin · deformedAT C-CHECK, RT WING INBOARD FLAP T/E DEFORMED FROM STA 106.00 TO 120.00. REMOVED TRAILING EDGE DEFORMED, FABRICATED NEW T/E, TREATED AND PRIMED, THEN INSTALLED ON RT WING INBOARD FLAP STA 106.00 TO XW 120.00 IAW SRM 57-2-1 PG 28.Jan 15, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080310CSeat Track · wornAT C-CHECK, LT/RT PILOT FWD TRACKS WORN. REPLACED LT/RT PILOT FWD TRACKS IAW SRM 53-2-3 PG 43-44.Jan 15, 2000 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080305CFloorbeam · brokenAT C-CHECK, AFT FUSELAGE MAIN CARGO FLOOR SUPPORT ANGLE BROKEN 1 AT STA 1746 BY L-26. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-2-0.Jan 15, 2000 · N803DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL200080356CWeb · crackedAT C-CHECK, MAIN CARGO COMPARTMENT, CUSP WEB SKIN LT SIDE CRACKED 2 INCHES BETWEEN FS 1560 AND FS 1580. REMOVED TRACK AS REQUIRED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21 PG 6, REINSTALLED TRACK IAW SRM 51-3-0 PG 1 & 2. N/R 5220Jan 15, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000023Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, RIGHT WING, STA 98 AFT PANEL UNDER FLAP ACTUATOR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 51-1-4 & 51-1-20Jan 14, 2000 · N792FT · Doug DC873F · Wing, Plate/SkinSDR RRXA000022Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, LWR ACCESS PANEL R/H AILERON POWER PACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21Jan 14, 2000 · N792FT · Doug DC873F · Wing, Plate/SkinSDR RRXA000021Longeron · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FWD LWR CARGO BILGE AT STA 280, LONGERON 33 RIGHT, NEXT TO DOOR JAM HAS A CRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-Jan 14, 2000 · N792FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000020Support · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FWD LWR CARGO COMPT AT STA 340, LONGERON 21 RIGHT, BEAM SUPPORT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D & 51-2Jan 14, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000019Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FWD LWR CARGO COMPT AT STA 340, LONGERON 27 RIGHT, FLOOR BEAM STRUT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51Jan 14, 2000 · N792FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000018Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE, UPPER CARGO COMPT AT FS 1220 XCW 45.5 LT SEAT TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3.Jan 14, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000017Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE, UPPER CARGO COMPT AT FS 1215 XCW 44.5 L/H SEAT TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3.Jan 14, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000016Seat Track · wornDURING A MAINTENANCE VISIT FOUND AREA WORN IN SEAT TRACK, UPPER COMPART FS 1584 XCW 44.5 R/H 5" AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 Jan 14, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000015Seat Track · wornDURING A MAINTENANCE VISIT FOUND AREA WORN IN SEAT TRACK, UPPER CARGO COMPT FS 1592 XCW 44.5 T/H 10.5". DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-Jan 14, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000014Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE, UPPER CARGO COMPT AT FS 1660 XCW 44.5 R/H IN SEAT TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3.Jan 14, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000013Duct · damagedDURING A MAINTENANCE VISIT FOUND HOLES, MAIN CABIN OVERHEAD AIR DUCT AT STA 460 AND STA 540. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.Jan 14, 2000 · N792FT · Doug DC873F · Air Distribution SystemSDR RRXA002961Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BRACKET BETWEEN STA 960 - 980 AT X+8 & Z-10, 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. (CORROSIOJan 14, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803119Fillet · deterioratedAT C-CHECK, FUSELAGE FILLET DETERIOATED AT FS 660.00 NEAR L-22 RT. REMOVED DETERIOATED FILLET AND REBUILT FILLET ALCLAD 2024-T3 0.032 IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12. INSTALLED FILLET IAW SRM 53-2-0.Jan 14, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR DHL2000803121Angle · crackedAT C-CHECK, LEFT WING I/B FLAP ANGLE CRACKED 1 INCH BETWEEN FLAPS AT XRS 162. REMOVED AND REPLACED ANGLE PER SRM 57-2-0. N/R 1295.Jan 14, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080317CSupport Bracket · crackedAT C-CHECK, WING TO FUESLAGE FAIRING SUPPORT ANGLE CRACKED 1.5 INCH AT XCW 0.000. REMOVED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ANGLE (2024 T3 0.063) IAW SRM 53-2-0 PG 10 TO TO 12, TREATED AND PRIMED IAW SRM 51-1-6 PG 1. INSTALLED ANGLE IAW SRM 51-Jan 14, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003379Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL AT FS 8 L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-20D, 51-1-21 AND DWG 5615530-54.Jan 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003378Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK HARDWARE AT STA 680 THROUGH 1000 AND LBL 46 THROUGH LBL 49 Z=0 THROUGH Z=-2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND IJan 13, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003377Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LAV FLOOR BOARDS AT FS 25-37 AND LBL18 TO RBL34, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8S RM 53-7-1 AND 51-1-2Jan 13, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA001028Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 34 LEFT BETWEEN STA 390 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIGURE Jan 13, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA001021Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1590 AND BL48R TO WL 0. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW FAA DER APJan 13, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000286Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, EXTERNAL SKIN AT XFS 710. 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 57-2-1.Jan 13, 2000 · N832AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000012Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, BRACKET FOR H.F. ANTENNA CANNON PLUG CRACKED & CORRODED VERT STAB TIP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & Jan 13, 2000 · N792FT · Doug DC873F · Empennage Flight Control Surfaces, Attach FittingsSDR RRXA000011Skin · dentedDURING A MAINTENANCE VISIT FOUND DENT, R/H O/B HORZ STAB L/E DENT FILLER BETWEEN XFS 247 AND XFS 272, RIGHT WING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 55-2-1 &Jan 13, 2000 · N792FT · Doug DC873F · Wing, Plate/SkinSDR RRXA000645Cargo Track · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE TO A CARGO DECK FITTING AT STA 1230 AND LONGERON 21R TO 20R, 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 51-1-20D.Jan 13, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2000803102Skin · damagedLT INBD FLAP LOWER SKIN DEFORMED AT XN 5.000 BETWEEN L/E AND TRAILING EDGE. REMOVED SKIN, FABRICATED NEW SKIN IAW SRM 57-7-1 PAGE 2. REF BOEING FAX SEU-XXX-00-0003 H 31, JAN 2000. PERFORMED ANTI CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. INSTALLED NEW SKIJan 13, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHL2000803103Skin · crackedFUSELAGE RT SURFACE SKIN WEB CRACKED 1 INCH FS 980.00 RBL 56.00 XW 0.00. PERFORMED ANTI CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-5 PAGE 34A-34B FIG 14A. TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12. INSTALLED DOUBLER WTIH SOJan 13, 2000 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000803104Seat Track · wornAT C-CHECK, FLIGHT COMPARTMENT MID F/E SEAT TRACK LT WORN. REMOVED DAMAGED TRACK IAW SRM 53-40-1 PAGE 201-203, CLEANED AND PERFORMED ANTI CORROSIVE TREATMENT AND PRIMED IAW SRM 51-1-8 PAGE 11-12. INSTALLED NEW TRACK IAW SRM 53-40 1 PAGE 202-203.Jan 13, 2000 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080338CSkin · deformedAT C-CHECK, RT WING I/B FLAP T/E SKIN DEFORMED AT XW 90. REMOVED SKIN, FABRICATED AND INSTALLED T/E SKIN ON RT I/B FLAP AT 90 XW IAW SRM 57-2-1, PG 28. N/R 1175Jan 13, 2000 · N803CH · Doug DC873F · Trailing Edge FlapsSDR RRXA003375Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON AT STA 990 AND L21R, 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.Jan 12, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003354Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT STA 1040 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8S RM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2.Jan 12, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA001027Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1040 AND LONGERON 35 RIGHT. CORROSION DAMAGE BEYOND 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 FIGURE 2.Jan 12, 2000 · N832AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000010Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FWD LWR CARGO BILGE AT STA 630, LONGERON 36, KEEL BEAM DOUBLER. DAMAGE WITHIN LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED FASTENERS IAW DC-8 SRM 51-3-0 AND E.O.Jan 12, 2000 · N792FT · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000803105Floor Support · crackedAT C-CHECK, AFT FUSELAGE SECTION MAIN CARGO FLOOR SUPPORT ANGLE CRACKED AT STA 1723.000 RT. REMOVED DAMAGED AREA AND PERFORMED ANTI CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. INSTALLED EXTRUSION IAW SRM 53-2-0 PAGE 2E&F. SECURED EXTRUSION WITH CHERRY MAX RJan 12, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003395Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON INBD 2 DOORS AT THE LT OTBD UPPER SLOT DOORS 12-30 INCHES FWD OF SPAR BETWEEN STA'S XS448 TO 497 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART Jan 11, 2000 · N831AL · Doug DC873F · Wing, Control SurfacesSDR RRXA003376Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN DECK FLOOR BOARD 1688C, 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 AND DWG 5755032.Jan 11, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003374Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WEB UNDER I/B END OF RELAY PANEL AT STA Y-2 X-8 Z=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 53-2-0, FIGJan 11, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000009Duct · damagedDURING A MAINTENANCE VISIT FOUND HOLES, MAIN CARGO CABIN OPEN AIR DUCT AT STA 380. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 51-1-4.Jan 11, 2000 · N792FT · Doug DC873F · Fuselage Structure (General)SDR RRXA000008Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK, MAIN CARGO DOOR CUT OUT AFT LWR CORNER, TRIM PLATE CRACKED AND METAL BROKEN OFF. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51Jan 11, 2000 · N792FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000007Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT STA 540, BETWEEN LONGERON 20 RIGHT AND LONGERON 21 RIGHT. DAMAGE WITHIN LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Jan 11, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002970Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE AT STA 1240, 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 51-1-0. (CORROSION DAMAGE RECORDED INJan 11, 2000 · N792FT · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA002969Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE AT STA 1220, 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. (CORROSION DAMAGE RECORDED INJan 11, 2000 · N792FT · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA002934Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PLANK AT STA 800, 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. (CORROSION DAMAGE RECORDED IN Jan 11, 2000 · N792FT · Doug DC873F · Fuselage Floor PanelSDR RRXA002924Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE FLOOR PANEL BETWEEN STA 580 & 880 AT X-24, 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. (CORROSION DAJan 11, 2000 · N792FT · Doug DC873F · Fuselage Floor PanelSDR RRXA000514Floor Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT BEAM AT STA 1710 AND BL 12 LEFT. 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 Jan 11, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000501Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME FITTING AT STA 560 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING. CORROSION DAMAGE RECORDED IN EWA CORROSION PROJan 11, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure
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