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 RRXA003372Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE DOOR NR 11 DOUBLER ON EXT SKIN AT FS 35 TO 55 AND L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FOUND MATERIAL TO BE IN LIMITS IAW DC-8 SJan 6, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000006Frame · tool damageDURING A MAINTENANCE VISIT FOUND TOOLING DAMAGE, FUSELAGE, FRAME AT STA 879, BETWEEN LONGERON 21 RIGHT AND LONGERON 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 00-Jan 6, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR RRXA000005Frame · tool damageDURING A MAINTENANCE VISIT FOUND FOOLING DAMAGE TO FRAME AT STA 680, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 00-016 WITH APPROVED 8110-3 DATED 01/20/0Jan 6, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002956Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON AT STA 1320, 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 51-1-20D. (CORROSION DAMAGE RECORDED IN EJan 6, 2000 · N792FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000643Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO LONGERON SPLICE FITTING AT STA 1266 AND LONGERON 31L, 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 AND DAC DWJan 6, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000003Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, FLAP CANOE FITTING ON I/B SIDE FROM ICE BRAKER ROD BOLT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA ORIGINAL THICKNESS .300, AFTER BLEND OUT .227. ACCEPTJan 5, 2000 · N792FT · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000002Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, ON FWD FLANGE ABOVE LONGERON 29 LEFT. DAMAGE EXCEEDED LIMITS 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 & 51-1-4.Jan 5, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002952Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE FRAME AT STA 600, 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 IN EWA CORRJan 5, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR UPS00831259Switch · failedWHEN GEAR HANDLE SELECTED TO DOWN POSITION LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE. GEAR NOT LATCHED RED LIGHT ILLUMINATED. CYCLED GEAR WITHOUT IMPROVMENT, AFTER THIRD CYCLE 3 GEAR INDICATION, AND GEAR UNLATCHED LIGHT OUT. CYCLED GEAR, COULD NOT DUPLICATE PJan 5, 2000 · N809UP · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA003385Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING OTBD L/E UPPER SKIN AT STA XW 761 TO XFS 878, DAMAGE EXCEEDED LIMITATIONS IAW DC-8S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1, FIJan 4, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA003370Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING SMALL L/E TO SMALL WING FRONT SPART FWD 2 INCHES AT STA XW-761 TO XW 736.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSJan 4, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA001039Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WHEEL WELL ATTACHMENT CLIP AT STA 902, BL59R AND WL 12. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT CLJan 4, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001026Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1480 TO STA 1490 AND LONGERON 33 RIGHT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG Jan 4, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001022Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 21 RIGHT AT STA 1190. CORROSION DAMAGE BEYOND 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 53-2-0 FIGURE 23.Jan 4, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA002951Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT STA 1400, 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 51-1-20D. (CORROSION DAMAGE RECORDED IN EWJan 4, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002950Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT STA 1360, 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 51-1-20D. (CORROSION DAMAGE RECORDED IN EWJan 4, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000616Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT MLG AT STA 857 RBL 45, 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. (CORROSION DAMAGE RECORDED INJan 4, 2000 · N831AL · Doug DC873F · Main Landing Gear Attach SectionSDR DHL2000803127Fairing · delaminatedAT C-CHECK, LT WING TO FUESLAGE FAIRING NR 704 DELAMINATED AT UPPER SKIN. REMOVED FASTENERS AND DELAMINATED PANEL IAW SRM 51-1-2A PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED OVERHAULED PANEL AND SECURED WITH SOLID RIVETS IAW SJan 4, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR RRXA001037Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. 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 Jan 3, 2000 · N832AL · Doug DC873F · Leading Edge DevicesSDR RRXA001034Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, UPPER SKIN AT XFS 390 AND STRINGER 11. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED Jan 3, 2000 · N832AL · Doug DC873F · Wing, Plate/SkinSDR RRXA001032Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DJan 3, 2000 · N832AL · Doug DC873F · Leading Edge DevicesSDR RRXA001024Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1020 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND 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-Jan 3, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001023Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1040 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING P/N:4640162-501N AND INSTALLEDJan 3, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002949Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT STA 380, 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 51-1-20D. (CORROSION DAMAGE RECORDED IN EWAJan 3, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001031Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 260, BL 65R AND WL-1. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM Jan 2, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001029Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33 LEFT SPLICE, BETWEEN STA 380 TO STA 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SPLICE AND INSTALLED IAW DC-8 SRM 51-Jan 2, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00831247Indicator · failedAT CRUISE ALTITUDE, SMOKE IN THE COCKPIT:F/O EADI WENT BLANK, FOLLOWED BY SMOKE FROM UNDER THE GLARESHIELD. PULLED THE ATT REF Z(F/O)CB AND RT EFIS MASTER. SMOKE PERSISTED INTERMITTENTLY. EMERGENCY DESCENT TO AIA. FOUND THE F/O EADI SHORTED OUT. REMOVED AJan 1, 2000 · N811UP · Doug DC873F · Directional Gyro and Indicating SystemSDR RRXA000287Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FE'S FORWARD SEAT TRACK. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0.Dec 30, 1999 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 99T64R737EWABushing · misalignedFOUND DURING D-CHECK, RIGHT INBOARD FLAP OUTBOARD FITTING FORWARD BUSHING NOT. ALIGNED WITH INBOARD BUSHING. REAMED INBOARD FITTING. FABRICATED BUSHING AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/29/99. (M)Dec 30, 1999 · N605AL · Doug DC873F · Trailing Edge FlapsSDR UPS00831248Terminal · brokenNR 3 ENG FIRE WARNING NO TEST. REPAIRED TERMINAL UNDER CORE COWL.Dec 30, 1999 · N851UP · Doug DC873F · Detection SystemSDR RRXA002953Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR SPLICE BETWEEN STA 280 - 340 AT X-48 AND Z-50, 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. (CDec 29, 1999 · N792FT · Doug DC873F · Fuselage Floor PanelSDR UPS99831237Fitting · corrodedINSPECTION TYPE:N/A, 9G NET ATTACH FITTINGS CORRODED BEYOND REPAIR.Dec 27, 1999 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99831230Slide · looseLOAD SUPERVISOR OPENED MAIN ENTERANCE DOOR AND SLIDE FELL OUT. REINSTALLED EVAC SLIDE IAW MM 25-60-01 PG 202-204.Dec 23, 1999 · N836UP · Doug DC873F · Escape SlideSDR 99T64R528EWABoss · corrodedDURING D-CHECK, C/W MAIN LANDING GEAR SHOCK STRUT ASSEMBLY RETRACT PIN BOSS AND RETRACT IN INSPECTION PER S/B 32-102 AND MA AI-3210-01:03. C/W MA-A1-3210-01:03, AFTER BLENDING REBORE EXCEEDED LIMITS OF MA. REPAIRED PER EO NR 99-186 WITH APPROVED 8110-3 DATEDDec 20, 1999 · N605AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR 99T64R529EWABoss · corrodedDURING D-CHECK, C/W MAIN LANDING GEAR SHOCK STRUT ASSEMBLY RETRACT PIN BOSS AND RETRACT PIN INSPECTION PER S/B 32-102 AND MA AI-3210-01:03. COMPLIED WITH MA AI-3210-01:03, AFTER BLENDING REBORE EXCEEDED LIMITS OF MIA. REPAIRED PER EO NR 99-186 WITH APPROVED Dec 20, 1999 · N605AL · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR RRXA991593Engine · failedNR 4 ENG FLAMED OUT AT FL 39.0 TIME 19:14-Z , OIL PRESS AND TEMP NORMAL, FUEL PRESS 38 PSI PRIOR TO FLAME OUT TANK BOOST PUMP ON. UNABLE RELIGHT AS PER QRH. AFTER INFLT SHUT DOWN CHECK, WINDMILL PARAMETERS WERE OIL PRESS 7 PSI FUEL PRESS 5 PSI, NO RELIGHT ONDec 20, 1999 · N831AL · Doug DC873F · Engine (Turbine/Turboprop)SDR 20000609AP007Angle · crackedFOUND DURING D-CHECK, FORWARD LOWER CARGO BILGE STATION 520 L31R INSIDE DOOR JAM ANGLE CRACKED AND BENT UP. REMOVED ANGLE, FABRICATED DOUBLER IAW DC-8 SRM 51-1-21, 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Dec 18, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000486Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND LOWER CARGO DOOR JAMB ATTACHMENT FITTING CRACKED AT STA 520 AND LONGERON 31 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 51-1Dec 18, 1999 · N605AL · Doug DC873F · Cargo/Baggage DoorsSDR 99T64R449EWAVane · damagedFOUND DURING D-CHECK, LEFT INBOARD FLAP NR 2 VANE INBOARD END SLIDING HINGE COVER TRACK MOUNT HOLES ELONGATED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M)Dec 17, 1999 · N605AL · Doug DC873F · Trailing Edge FlapsSDR RRXA000297Vane · damagedDURING A MAINTENANCE VISIT FOUND LEFT WING INBOARD FLAP NR 2 VANE HAS MOUNT HOLE ENLONGATED. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED ENGINEERINGDec 17, 1999 · N605AL · Doug DC873F · Trailing Edge FlapsSDR UPS99831228Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. CHARGED BATTERY, OPS OK.Dec 16, 1999 · N811UP · Doug DC873F · Emergency LightingSDR 99T64R491EWABellcrank · crackedFOUND DURING D-CHECK, MID WING FLAP CRANK HAS CRACK APPROX .1875 INCH IN LENGTH AT STATION 219 LEFT. REPLACED MIDWING FLAP CRANK IAW DC-8 O/H/M 27-28-8. (M)Dec 15, 1999 · N605AL · Doug DC873F · Trailing Edge Flap ActuatorSDR 99T64R550EWADuct · crackedFOUND DURING D-CHECK, LOWER RIGHT AIR CONDITIONING DUCT AND BULKHEAD FEED THROUGH WORN AND CRACKED STATION 8 L32R. STOP DRILLED CRACK AND WELDED. WELDED WORN AREA'S PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/02/99. (M)Dec 15, 1999 · N605AL · Doug DC873F · Air Distribution SystemSDR 99T64R469EWAFloorbeam · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPARTMENT, FLOORBEAM EXFOLIATED STATION 1540 XCW 69 LEFT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21 AND 53-2-0. (M)Dec 15, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000214Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1540 XCW 69 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21 AND 53-2-0 . (Dec 15, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR 99T64R516EWALongeron · crackedFOUND DURING D-CHECK, LEFT W/W LONGERON 24 STATION 857 HAS CRACK 1.5 INCHES LONG. REMOVED AND REPLACED LEFT L24 IAW DC-8 REPLACEMENT GUIDE AND SRM 51-1-21, 51-1-20D AND 53-2-2. (M)Dec 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR 99T64R476EWABellcrank · crackedFOUND DURING D-CHECK, INBOARD FLAP ACTUATOR ASSY CRANK HAS TWO CRACKS, ONE IS .5 INCH IN LENGTH AND THE OTHER IS .375 INCH LENGTH. REPLACED CRANK IAW DC-8 O/H/M 27-28-9. (M)Dec 14, 1999 · N605AL · Doug DC873F · Trailing Edge Flap ActuatorSDR 99T64R446EWALongeron · corrodedFOUND DURING D-CHECK, RIGHT LONGERON 24 AND FUSELAGE STATION 879 TO STATION 940, CORROSION ON UPPER SURFACE ON FITTING AND 2 PREVIOUS REPAIR DOUBLERS ALSO RUNNING UNDER REPAIR DOUBLERS. REPLACED RIGHT L24 FITTING IAW DOUGLAS L24 REPLACEMENT GUIDE SRM 51-1-20DDec 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000480Longeron · crackedDURING A MAINTENANCE VISIT FOUND LONGERON 24 LEFT CRACKED AT STA 857. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW LONGERON 24 LEFT IAW DC-8 SRM 51-1-20D.Dec 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000234Longeron · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT LONGERON 24 FROM STA 879 TO STA 960. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.Dec 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
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