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 RRXA10902Support Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD SUPPORT BRACKET FWD NR 7 LATCH SPOOL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Mar 28, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806611Spoiler · delaminatedC-CHECK - RT WING REMOVAL AND INSTALLATION OF NR 1 GROUND SPOILER DUE TO UPPER SKIN DELAMINATED BETWEEN XW 5.000 AND XW 47.000. REMOVED NR 1 GROUND SPOILER (DELAMINATED) IAW MM 27-61-1 PAGE 201 TO 204. INSTALLED NR 1 GROUND SPOILER AFTER ITS REPAIR MADE IN UMar 28, 2001 · N806DH · Doug DC873F · SpoilersSDR DHL2001806602Fitting · crackedC-CHECK - FWD CARGO COMPART FITTING CRACKED 1/2 INCH, STA 300 L-27 LT. REMOVED CRACKED FITTING (STA 300 L-27L) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED.Mar 28, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806591Rib · crackedC-CHECK - LT WING AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME CRACKED 4 INCHES, STA XA 425. REMOVED LATERAL RIB ACCESS DOOR FRAME IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME AT STA XA 425 IAW SRM 51-1Mar 28, 2001 · N806DH · Doug DC873F · AileronsSDR RRXA010030Indicator · faultyIN FLIGHT, SAI SHOWS A 20 DEG RIGHT BANK AND 5 DEG TO 6 DEG NOSE UP IN LEVEL FLIGHT. SAI WILL THEN RETURN TO A 3 DEG RIGHT BANK AND 5 DEG''''S TO 6 DEG''''S NOSE UP. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR. OPS CHECKS NORMAL IAW MM CH 34-00-00.Mar 28, 2001 · N2674U · Doug DC873F · Attitude and Direction Data SystemSDR RRXA11032Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT STA XFS 710 ON LT WING OB LE, 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 57-2-1 FIG2H.Mar 27, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR DHL2001806529Floor Support · crackedC-CHECK - MAIN CARGO COMPARTMENT. FLOOR SUPPORT U ANGLE CRACKED 1 INCH BL 0 STA 1734-1760. REMOVED CRACKED U ANGLE IAW SRM 51-1-20 PAGE 21. FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 53-2-Mar 27, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835457Coalescer Bag · contaminatedAFTER TAKEOFF AND LEFT PACK TURNED ON, CAUSTIC FUMES FILLED COCKPIT. DECLARED EMERGENCY. RAN FUMES EVAC CHECKLIST WHILE RETURNING TO LAND . AIR TURN BACK. R & R LEFT WATER SEPARATOR SOCK, INSPECTED R-SOCK FOUND NO DEFECTS. LEFT SOCK FUEL FUME SOAKED.Mar 27, 2001 · N810UP · Doug DC873F · Humidity Control SystemSDR UPS01835458Line · blownATB FOR HYD LOST IN FLT, FOUND NR 2 EDP FLEX LINE BLOWN. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE. RAN ENGINES, LEAK CHECKED. OPS CHECK GOOD.Mar 27, 2001 · N851UP · Doug DC873F · Hydraulic System, MainSDR DHL2001806601Skin · misrepairedC-CHECK - RT WING O/B FLAP T/E AT STA XW 454.000 SHOWS REPAIR IMPROPER. REMOVED T/E WITH REPAIR IMPROPER IAW SRM 51-1-21 PAGE 1. FABRICATED NEW T/E IAW SRM 52-2-0 FIG 2D. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM 51-1-21 PAGE 1. STATUSMar 26, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001806588Angle · crackedC-CHECK - LT OUTBD FLAP SLIDING COVER HOUSING ANGLE CRACKED AT STA XRS 247.REMOVED ANGLE CRACKED IAW SRM 51-1-21 PAGE 1. FABRICATED NEW ANGLE WITH EXTRUSION 7075 T6 IAW SRM 57-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-2Mar 26, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR RRXA10896Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 L29L TO L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-Mar 25, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10895Seat Track · wornDURING A MAINTENANCE VISIT FOUND THE SEAT TRACK WORN BEYOND LIMITS AT STA 590 TO 980 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-1, FIG 4.Mar 25, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10894Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TORQUE BOX BANANA FITTING AT STA 1150 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0.Mar 25, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10890Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING AT LONGERON 35R AT STA 1050, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-1-0 AND DWG 370545.Mar 25, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA010891Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND A DRILLED END FITTING AT RADIUS AT STA 1687 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 4773155.Mar 25, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2001806619Fitting · crackedC-CHECK - AFT FUSELAGE INTERIOR RT UPPER PART FITTING CRACKED 1-1/2 INCH AT STA 1766 L-9R. REMOVED CRACKED FITTING FROM AFT FUSELAGE INTERIOR RT UPPER PART IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-88. INSTALLED NEW FITTING (P/NMar 25, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA10889Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LH AUX TANK UPPER SPAR CAP BETWEEN STA XFS 1.25 TO XFS 113.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAMar 24, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10887Fitting · crackedDURING A MAINTENANCE VISIT FOUND A LARGE GAP BETWEEN O/B END FITTING AND BATHTUB FITTING AT FS 1220 AND L33L TO L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755Mar 24, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10886Fitting · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START TO THE BATHTUB FITTING AT STA 1228 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845.Mar 24, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA10885Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E AT STA XFS 291-500 AND 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2, 51-1-21 AND 51-1-20D.Mar 24, 2001 · N602AL · Doug DC873F · Wing StructureSDR DHL2001806604Fitting · crackedC-CHECK - FWD CARGO COMPT. FITTING CRACKED 1 INCH AT STA 200 L-25 RT. REMOVED CRACKED FITTING AT STA 200 L-25 RT (FWD CARGO COMPT) IAW SRM 51-3-0 PAGE 1, 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PAGE 1, 2. STATUSMar 24, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806528Support · crackedC-CHECK - RH WING OUTBOARD FLAP. SUPPORT ARM PROTECTOR SHOWS 1 INCH CRACK AT STA XRS 230. REMOVED PROTECTOR FROM SUPPORT ARM IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PROTECTOR IAW SRM 53-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW PROTECTOMar 24, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR RRXA11029Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT L33L AND STA 1168-1270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-2Mar 23, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806594Fitting · crackedC-CHECK - AFT CARGO COMPARTMENT. FITTING CRACKED 1 INCH BETWEEN L-25L AND L-23L. STA 1180.000. REMOVED FITTING CRACKED FROM AFT CARGO COMPARTMENT BETWEEN L-25L AND L-27L IAW SRM 51-1-21 PAGE 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSPECTED NEW Mar 23, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835539Web · corrodedINSPECTION TYPE:C2 AT STA -67 SUB FLOOR RT SIDE CORROSION AT CUSP IN FLT DECK REPAIRED SUBFLOOR AT STA -67 AT CUSP AREA DAC DWG SRO 8530026Mar 23, 2001 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835448Stop Fitting · missingINSPECTION TYPE:PFLT BOTH OVERWING EXIT DOORS MISSING STOP FITTING ASSY/WILL NOT LATCH RESEATED IN SILL AND LATCHED INTO PLACE. M/M 52-20-00Mar 23, 2001 · N809UP · Doug DC873F · Emergency ExitsSDR RRXA10901Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1220 BETWEEN L34R TO L35R AND L35R TO L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAWMar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10900Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT WING L/E RIB (UPPER) AT STA XFS 816.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10899Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FINGER DOUBLER AT FS 1350 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21 AND DWG 5779915.Mar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA10898Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE LT CENTER L/E AT STA XFS 341.500, 354.800 & 360.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10897Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP LT WING L/E AT STA XFS 385-250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10892Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE L/H L/E WING CENTER AT STA XFS 422.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAAW DC-8 SRM 57-2-0, FIG AND 51-1-20D.Mar 22, 2001 · N602AL · Doug DC873F · Wing StructureSDR RRXA10884Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FWD DRAIN HOLE ON THE LT WING O/B L/E LWR SKIN AT STA XFS 597.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-21D AND SH SK 602-627.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10883Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 2 LATCH BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1Mar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10882Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 5 LATCH BACKUP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND Mar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10881Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME LOWER NR 4 LATCH BACKUP FITTING , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0Mar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10880Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 AT STA 140-160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-4-1, FIG 28 AND DWG 5758874Mar 22, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10879Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10878Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB LEFT WING L/E AT STA XFS 616.25 AND 622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10877Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XF 5660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10876Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 578375, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10875Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING L/E UPPER RIB AT STA X5497-401, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Mar 22, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001806634Channel · crackedC-CHECK - MAIN CARGO JOINT ANGLE FROM CROSSBEAM - INTERCOSTAL AT STA 680.000 LBL 46.5 CRACKED 2 INCHES. REMOVED CRACKED ANGLE (CHANNEL) IAW SRM 51-3-0 PAGE 1, 2. FABRICATED NEW ANGLE (CHANNEL) IAW ATM 044340A, EA 2001131, DWG 573275. CLEANED, TREATED, AND PMar 22, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001802003Switch · faultyUNABLE TO MAINTAIN CABIN PRESS WITH FLOWS AT MAX MANUAL CONTROL FULL CLOSED. FOUND FAULTY SCOOP ANTI-ICE SWITCH CAUSING LT SCOOP VALVE TO INTERMITTINGLY STICK IN THE OPEN POSITION. REPLACED SWITCH PER MM 20-50-1. ALSO REPLACED LT SCOOP VALVE AS PRECAUTION PMar 22, 2001 · N802DH · Doug DC873F · Ice/Rain Protection SystemSDR RRXA10893Skin · crackedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LEFT I/B FLAP T/E OTBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG 3652279.Mar 21, 2001 · N602AL · Doug DC873F · Trailing Edge FlapsSDR DHL2001806606Fitting · corrodedC-CHECK - FWD CARGO COMPARTMENT - FITTING BETWEEN FRAME AND BEAM SHOWS CORROSION AT STA 822.000, L-21R. R/R FITTING CORRODED IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED MAIN CARGO COMPARTMENT FITTING BETWEEN FRAME AND BEAM AT STA 827.000 L-21R IAWMar 21, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806605Fitting · crackedC-CHECK - FWD CARGO COMPARTMENT FITTING CRACKED 4 INCH BETWEEN STA 600.000 AND STA 620.000 L-32R. R/R FITTING CRACKED IAW SRM 51-1-200 PAGE 21. CLEANED TREATED AND PRIMED FWD CARGO COMPT FITTING BETWEEN STA 600.000 AND STA 620.000 L-32R IAW SRM 51-1-8B. IMar 21, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001805004Connector · dirtyCOMPASS SYSTEM NR 1 AND NR 2 ARE NOT SLAVING TO MAGNETIC HEADING, DG FUNCTION APPEARS NORMAL. CLEANED CONNECTOR AT COMPASS COMPARATOR SYSTEM SLAVING NORMAL, SWUNG TO KNOWN HEADING, SYSTEM CHECKED OK IAW MM 34-24-0.Mar 21, 2001 · N805DH · Doug DC873F · Attitude and Direction Data SystemSDR RRXA11046Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA1050-1270 AND L36, 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 DC-8 SRM 51-1-20D, Mar 20, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/Skin
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