Douglas DC-8-73F

Service difficulty reports · 15,471

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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 RRXA000549Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN DECK SEAT TRACK AT STA 55 TO 310 AND LBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED SEAT TRACK SECTION IAW DC-8 SRM 53-2-3 FIG 8A. (CORROFeb 28, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000546Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 AT STA 35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPLACED PART AND INSTALLED IAW DC-8 SRM 53-1-21 DAC DWG 3702969 -501, ALSO 5Feb 28, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000544Shear Tie · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 35, AND IN BETWEEN LONGERON 35 LEFT TO 34 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHEAR TIE IAW DC-8 SRFeb 28, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR UPS00832121Frame · corrodedINSPECTION TYPE:C123, FLOORBEAM UNDER FLOOR LT STA 1700 LBL 30 HAS CORROSION AT C TRACK ATTACHMENT DOT P142. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLES AND FILLER IAW REO-G07178. ALODINED AND PRIMED IAW DC8 SRMFeb 28, 2000 · N804UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832099Bracket · corrodedINSPECTION TYPE:C123, FLOOR ANGLE ATTACH BRACKET CORRODED OUT AT FS 1750 BL 0. REMOVED OLD BRACKET AT FS 1750 BL 0 AND REPLACED WITH NEW BRACKET (P/N 5773846-59) UPS TAG 786954.Feb 28, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080383CFitting · crackedAT C-CHECK, RT MLG TRAPEZOIDAL PANEL FITTING SHOWS CRACK OF 4.124 LENGTH AT STA 868, REF N/R 2034. STOP DRILLED CRACK, REMOVED FITTING AND FABRICATED NEW FITTING AND DOUBLER IAW SRM 57-2-7, INSTALLED IAW SRM 57-2-7 PG 9 &10. N/R 2035Feb 28, 2000 · N803DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR DHL200080371CVane · delaminatedAT C-CHECK, RT WING NR 1 FLAP VANE DELAMINATED. REMOVED AND REPLACED NR 1 FLAP VANE IAW MM 27-31-14 PG 201, PERFORMED CLEARANCE CHECK IAW MM 27-51-14 PG 302. N/R 1011Feb 28, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR RRXA003402Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN DECK FLOOR BOARD AT STA 1690 AND X=0 Z=0, 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 51-3-0 AND DWG 5754Feb 27, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000672Attach Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTING AT STA 1280 AND LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTACH FITTING AND INSTALLED IAW DC-8 SRM 51-1-Feb 27, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000568Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT HORIZONTAL STAB I/B LEADING EDGE AT BL-R 177, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DAMAGE IAW DC-8 SRM 55-2-1 FIFeb 27, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR RRXA000548Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN DECK SEAT TRACK BETWEEN STA'S 70 TO 310 LONGERON LBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION OF SEAT TRACK AT STA'S 70 TO 310 LONGERON LBL 45 IAW DC-8 SRM 51-1-8 FABRIFeb 26, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000347StrutFOUND DURING C-CHECK. COMPLY WITH MA A1 3210-01:03 MAIN LANDING GEAR SHOCK STRUT ASSY. RETRACT PIN RIGHT GEAR. (DER APPROVED). REMOVED AND REPLACED RT MAIN LANDING GEAR SHOCK STRUT RETRACT PIN IAW MA-A1 3210-01:03Feb 26, 2000 · N792FT · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR RRXA000671Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E UPPER RIB AT XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED FASTENER, FABRICATED ANGLE AND INSTALLED IAW DC-8 SRM 51-1-20D,Feb 26, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000552Structure · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LT WING LEADING EDGE STUB AT STA 520 TO XW 856, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 57-1-21 DAC DWG 5754701. (CORROSION DAFeb 26, 2000 · N831AL · Doug DC873F · Leading Edge DevicesSDR RRXA000543Seat Track · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN DECK SEAT AT STA 80 AND LONGERON LBL 45. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM 51-1-8. REMOVED DAMAGED SECTION OF SEAT TRACK AT STA 80 TO 310 LONGERON LBL 45. FABRICATED SEAT TRACK SECTION AND INSTAFeb 26, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000346Boss · corrodedDURING MAINTENANCE VISIT COMPLIED WITH MA A13210-01:03 MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN LEFT GEAR (EO). REMOVED AND REPLACED LT MAIN LANDING GEAR SHOCK STRUT PIN IAW MA A13210-01:03 AND EO 00-016 (DER APPROVED).Feb 26, 2000 · N792FT · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR RRXA000187Line · brokenHYD FAILURE BOTH SYSTEMS. FOUND RUDDER RETURN HYDRAULIC LINE BROKEN AT WALL RESTRAINT. REMOVED 12 INCHES AND REPLACED LINE IAW M/M CHAPTER 20-12-1. RESERVICED HYD SYSTEM, RAN ENGINES. GROUND OP'S CHECKS NORMAL, LEAK CHECKS GOOD IAW M/M CHAPTER 29-00.Feb 26, 2000 · N795FT · Doug DC873F · Hydraulic System, MainSDR RRXA003401Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXISTING DOUBLER INSIDE TAIL CONE ON SUPPORT WEB AT FS 1985 AND BL-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 Feb 25, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000553Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING LEADING EDGE LOWER SKIN AT STA XW760 TO XW761 AT ATTACH FASTENER HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW DC-8 SRM 5Feb 25, 2000 · N831AL · Doug DC873F · Leading Edge DevicesSDR RRXA000679Skin · wornDURING A MAINTENANCE VISIT, FOUND A SCREW HOLE WORN AT THE RIGHT WING L/E LWR SKIN AT XFS 663, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW DC-8 SRM 57-2-0 FIG 2A.Feb 25, 2000 · N831AL · Doug DC873F · Leading Edge DevicesSDR RRXA000556Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN DECK SEAT TRACK BETWEEN STA 410 TO 530 RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SECTION OF SEAT TRACK BETWEEN STA 410 TO 530 LONGFeb 25, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000555Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN DECK SEAT TRACK BETWEEN STA 270 TO 450 RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC-8 SRM 53-Feb 25, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000550Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN DECK SEAT BETWEEN STA 1010 TO 1090 LONGERON LBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM 51-1-8. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SEAT TRACK SECTION AND INSTALLED IAW Feb 25, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000547Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND MODERATE CORROSION DAMAGE TO LEFT AFT T1 DOOR FITTING AT LONGERON 1 TO 6 LEFT AND AFT END OF DOOR, DAMAGE WAS WITHIN LIMITS IAW DC-8 SRM. REMOVED DAMAGED FASTENERS, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED FASTENERS IAW DFeb 25, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000542Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT HAND WING SKIN AT STA XWO TO XRS 9 FROM STRINGER 2 TO REAR SPAR. DAMAGE LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, FAST AS REQUIRED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED AND REFeb 25, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000541Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT LONGERON 24 RIGHT FITTING AND STA 960. 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. CFeb 25, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000358Skin · crackedDURING A MAINTENANCE VISIT FOUND SKIN CRACK NEAR TOP EXCITER RT FAN REV (1.5 INCH CRACK AND RIVET MISSING). REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK IAW DC-8 SRM 51-1-21 AND DER APPROVED EO 00-016.Feb 25, 2000 · N792FT · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR RRXA000357Angle · crackedDURING A MAINTENANCE VISIT FOUND 4 INCH CRACK IN ANGLE AFT PRESSURE BULKHEAD STA 1766 L19L TO L19R AT CENTER LINE OF HORZ BEAM. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW SRM 53-2Feb 25, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832120Angle · corrodedINSPECTION TYPE:C123 AFT PIT SMOKE BARRIER ATTACH ANGLES CORRODED AND MISSING NUT PLATES. REMOVED CORROSION, FOUND ANGLE TO BE OUT OF LIMITS. FABBED NEW ANGLES IAW DC-8 DAC DWG 9893785. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, AND INSTALLED NUT PLATES IAW 51Feb 25, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080387CWeb · crackedAT C-CHECK, MAIN CARGO COMPARTMENT CUSP WEB CAP CRACKED 1 INCH STA 100 TO STA 120. STOP DRILLED CRACK IAW SRM 53-2-0 PG 2K, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 PG 2K. N/R 5667Feb 25, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080386CFitting · scratchedAT C-CHECK, NR 3 CARGO DOOR HINGE FITTING CRACKED 2.5 INCHES BETWEEN FS 1215 AND FS 1225. REMOVED FITTING, CLEANED AND INSPECTED IAW SRM 52-2-0 PG 22, FOUND TO BE A SCRATCH. REINSTALLED HINGE FITTING IAW SRM 51-1-21. N/R 5352Feb 25, 2000 · N803DH · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003793Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA. 680 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#00-016 WITH APPROVED 811Feb 24, 2000 · N792FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA003400Access Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING BOX TOP ACCESS PANEL 505G, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DC-8 SRM 51-3-0, 51-1-21 AND DWG 57Feb 24, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000670Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT RIGHT WING L/E RIB AT AFT UPPER END AT XFS 810, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000669Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT RT WING L/E RIB AT XFS 785.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000668Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LEFT O/B LEADING EDGE UPPER SKIN AT XFS 697, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-1 FIG 38, 5Feb 24, 2000 · N831AL · Doug DC873F · Leading Edge DevicesSDR RRXA000667Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RT WING L/E RIB AT XFS 753.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIRED DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000666Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE LEFT WING L/E RIB AT STA XFS 397.79, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AFeb 24, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000665Frame · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT STA XFS 760.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-00 FIG 1BFeb 24, 2000 · N831AL · Doug DC873F · Leading Edge DevicesSDR RRXA000567Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE FUSELAGE INTERNAL SKIN (DOUBLER) BETWEEN STA 660 TO 680 AND BETWEEN LONGERON 35 LEFT AND 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Feb 24, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000565Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ''D'' PIT DOOR LOWER AFT CORNER, 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 52-2-3 FIG 10A. (CORROSION DAMAGEFeb 24, 2000 · N831AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000539Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK OF OUTBOARD LOWER ATTACH FLANGE AND ROUND ATTACH FAST. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8Feb 24, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000538Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING OUTBOARD LEADING EDGE SKIN BETWEEN XW761 TO XW-736.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW DCFeb 24, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000537Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN SEAT TRACK AT STA 570 AND BL 63 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC-8 SRM 5Feb 24, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000536Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FORWARD SERVICE DOOR FITTING. 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. CORROSION RECORDED IN EFeb 24, 2000 · N831AL · Doug DC873F · Service DoorsSDR RRXA000535Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 190 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEVIED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D. CORROSION RFeb 24, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000334Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON FUSELAGE SKIN BETWEEN FS 1717R AND 1734R LONGERON L28R. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER APPROVED EO NR Feb 24, 2000 · N792FT · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000803114Fitting · crackedAT C-CHECK, AFT FUSELAGE SECTION 36 LONGERON SPLICE AFT FITTING CRACKED 2 INCHES BETWEEN STA 1690 AND STA 1702. REMOVED AND REPLACED FITTING IAW SRM 51-1-8 PG 12B. REF: N/R 5483.Feb 24, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803113Panel · delaminatedAT C-CHECK, RT WING TRAILING EDGE UPPER SKIN DELAMINATED FROM STA 454 TO STA 463. REMOVED AND REPLACED PANEL IAW SRM 51-1-21 PG 7. REF: N/R 1024.Feb 24, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL200080384CSkin · dentedAT C-CHECK, AFT FUSELAGE SECTION LOWER SKIN SHOWS DENT DAMAGE AT FS 1400 AROUND L-34, 35R. FABRICATED AND INSTALLED DOUBLER IAW EO NR DHL012701. N/R 5517Feb 24, 2000 · N803DH · Doug DC873F · Fuselage Main, Plate/Skin
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