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 RRXA001990Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN RADIUS AT AFT PRESSURE BULKHEAD I BEAM UPPER ATTACH ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC-8 SRM 51-1-21,Mar 19, 2000 · N961R · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA001859Support Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TRACK SUPPORT FITTING AND TRACK NR 5 MAIN CABIN AT STA 700, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FITTING IAW DC-8 SRMar 19, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001855Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD I BEAM UPPER ATTACH ANGLE AT STA 1766, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRMar 19, 2000 · N961R · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA001992Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TRACK SUPPORT AT STA 780 AND NR 3 TRACK MAIN CABIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED FITTING IAW DC-8 SRM 51-1-20D.Mar 18, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001857Support Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TRACK SUPPORT NR 3 TRACK MAIN CABIN AT STA 780, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D.Mar 18, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832137Strap · corrodedINSPECTION TYPE: C123, FWD CARGO BAY FS 520 LONGERON 35 RT STRAP IS CORRODED. REMOVED LONGERON 35 RT STRAP IAW DC8 SRM 51-1-21. FABED STRAP IAW DAC DWG 3758450. ALODINED & PRIMED STRAP IAW DC8 SRM 51-1-8. INSTALLED STRAP IAW DC8 SRM 51-1-21.Mar 18, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832085Hinge · crackedINSPECTION TYPE: C 123 AFT CARGO BAY DOOR RAMP COVER GATE HINGES ARE CRACKED. REMOVED CRACKED HINGE IAW DC8 SRM 51-3-0. RECD NEW HINGE P#5754062-1 . LOCATED & DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED NUT PLATES IAW DC8 SRM 51-1-21. INSTALLED HINGE IMar 18, 2000 · N804UP · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001991Web · crackedDURING A MAINTENANCE VISIT FOUND A 1.25 INCH CRACK TO THE WEB PANEL JUST RIGHT OF SEAT TRACK NR 2 MAIN CABIN AT STA 1000 AND LBL 40 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Mar 17, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001856Web · crackedDURING A MAINTENANCE VISIT FOUND A 1.25 INCH CRACK TO THE WEB PANEL JUST RIGHT OF SEAT TRACK NR 2 MAIN CABIN AT STA 1000 AND LBL 40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLMar 17, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002130Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 4 TRACK AT STA 740 AND BL 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3.Mar 16, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002116Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN #6 SEAT TRACK AT STA 1408 & 1411 RT. AND RBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3.Mar 16, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000715Skin · damagedDURING A MAINTENANCE VISIT FOUND 3 TEMPERARY REPAIRS AT THE C-PIT DOOR FLOOR COVER HINGED SECTION SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SKIN IAW DC-8 SRM 51-1-2Mar 16, 2000 · N831AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000714Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO C-PIT DOOR FLOOR COVER HINGED SECTION FRAME, EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED FRAME, REINSTALLED NEW FRAME IAW DC-8 SRM 51-1-21.Mar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA001961Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE KEEL FILLER PANEL ATTACH WEB AT STA 945, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-1-20, 51-1-4 ANMar 16, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001960Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE KEEL FILLET PANEL ATTACH WEB AT STA 955, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-4, 51-1-20 AND 51-Mar 16, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001826Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE KEEL FILLER PANEL ATTACH WEB AT STA 945, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-1-20D, 51-1-20 Mar 16, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001825Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE KEEL FILLET PANEL ATTACH WEB AT STA 955, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D.Mar 16, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000598Keelbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO KEEL BEAM AT STA 660 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED PER DEE HOWARD AIRCRAFT MAINTENANCE SK 831-363. (CORROSION DAMAMar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, KeelSDR RRXA000597Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT FUSE FRAME AT STA 1793 AND LONGERON 30L AND 30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RE-INSTALLED FASTENERS AND BRACKETS IAW DC-8 SRMMar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR UPS00832170Floor Support · corrodedINSPECTION TYPE: C123, CORRODED FLOOR SUPPORT FS 1715 BLR 28, UNDERNEATH, AFT, ACCESSORY COMP. FABED ANGLE IAW DAC DWG 575032.ALODINED & PRIMED IAW DC8 SRM 51 -1-8. INSTALLED IAW DC8 SRM 51-1-20D & 51-1-21.Mar 16, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832129Floor Support · corrodedINSPECTION TYPE: C123, CORRODED FLOOR SUPPORT FS 1700, RBL20, UNDERSIDE, AFT ACCESSORY BAY. FABBED FLOOR SUPPORT IAW DAC DWG 575032. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED FLOOR SUPPORT IAW2 DC8 SRM 51-1-20D.Mar 16, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000191O Ring · leakingIN CRUISE, HYD QTY IND DROPPED TO STAND PIPE COMPLYED WITH QRH PROCEDURES EM AIRBRAKE HANDLE WIRE BROKEN. FOUND O-RING BETWEEN SLOT CONTROL VALVE AND C/H HYD MANIFOLD BLOWN. REMOVED AND REPLACED SAME PER M/M 27-80-4. SYSTEM OPS AND LEAK CHECKS GOODMar 16, 2000 · N870TV · Doug DC873F · Hydraulic Quantity IndicatorSDR RRXA000712Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE WEB AT STA 1160 LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER AND FILLER IAW Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR RRXA001908Panel · chafedDURING A MAINTENANCE VISIT FOUND A CHAFED UPPER REAR SPAR PANEL LT WING BY NR 1 SPOILER O/B HINGE AT STA XW 90, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SMar 15, 2000 · N961R · Doug DC873F · SpoilersSDR RRXA001772Panel · chafedDURING A MAINTENANCE VISIT, FOUND A CHAFED PANEL BY NR 1 SPOILER OB HINGE AT THE LT WING UPPER REAR SPAR AT STA XW 90, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLEMar 15, 2000 · N961R · Doug DC873F · SpoilersSDR RRXA000600Attach Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1220 BETWEEN LONGERONS 33R AND 34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2G AND DAC Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000599Attach Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1220 BETWEEN LONGERONS 33R TO 32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND DAC DMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000595Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER NUT PLATES AT STA 1000 AND LONGERON L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPAIRED AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 2 AND DACMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000592Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT UPPER WING SKIN AT STA 354 TO 366 STR 5 TO 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 57-2-1 FIG 29 AND SRMMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000591Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO 21 WASHERS AND NUTS AT STA 680 TO 660 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED WASHERS AND NUTS IAW DC-8 SRM Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA002034Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLE EDGE ON THE RT L/E AUX TANK AT STA XFS 63, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 5Mar 14, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000713Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE ATTACH FITTING AT STA 1160 AND LONGERON 33R, 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.Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Structure (General)SDR RRXA001968Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR SEAL RETAINER AT STA 890 AT KEEL BEAM, 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 SMar 14, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA001833Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MAIN LANDING GEAR DOOR SEAL RETAINER AT STA 890 AT KEEL BEAM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 Mar 14, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA000593Attach Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND DAMAGE TO BULKHEAD FITTING ON O/B SIDE AT STA 8 AND LONGERON 33 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DMar 14, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000590Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUB FLOOR SUPPORT ANGLE AT STA 80 TO 100 AND BL-R 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUB FLOOR SUPPORT ANGLE IAW DC-8 Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000589Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUB FLOOR WEB AT STA 80 TO 100 AND LONGERON BL-R 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUB FLOOR WEB IAW DC-8 SRM 51-1-20Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002161Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT AFT EDGE OF SKIN IN "D" BAG BIN DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1-20D.Mar 13, 2000 · N2674U · Doug DC873F · Cargo/Baggage DoorsSDR RRXA002160Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RIGHT WING LEADING EDGE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, Mar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002159Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LEADING EDGE SKIN AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IMar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002158Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LIGHTNING HOLE BELOW THE LEFT HINGE ON THE RADOME BULKHEAD AT FS 156, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA002157Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK 5 INCHES FWD OF THE WING SPAR ON THE LEFT WING LEADING EDGE SKIN LOWER SURFACE AT XFS 335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAWMar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002156Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE ON THE AFT END OF THE CENTER WING BOX LOWER SKIN EXTERIOR AT FS 855 AND XCW 68 RT., DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLMar 13, 2000 · N2674U · Doug DC873F · Wing Miscellaneous StructureSDR RRXA002151Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN COURIER AREA FLOOR WEB AT FS 25-45 AND RBL 48-75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-4.Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA002055Web · crackedDURING A MAINTENANCE VISIT FOUND A 4 INCH CRACK TO THE FILLER WEB AT LT WING I/B FLAP AT ST A980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20DMar 13, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA000711Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT FWD JAMB FITTING AT STA 1150 AND LONGERON 32R, 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 53-1-0 AND 51-1-2Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000710Bracket · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET ON THE A/C COMPARTMENT DOOR #12 DOOR SWITCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BRACKET IAWMar 13, 2000 · N831AL · Doug DC873F · Air Conditioning DoorsSDR RRXA000709Splice · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT A SPLICE FITTING AT STA 390 AND LONGERON 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT AND REINSTALLED FITTING.Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001743Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LIGHTNING HOLE BELOW THE LEFT HINGE ON THE RADOME BULKHEAD AT FS 156, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA000585Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1152 AND LONGERON L33 RIGHT TO L34 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SPLICES AND FITTINGS AND INSTALLED Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure
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