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 RRXA001821Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE CAPT''''S LT AFT SEAT TRACK LOCK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SEAT TRACK IAW DC-8 SRM 51-3-0, 53-2-0 AMar 30, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001820Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE CAPT''S RT AFT SEAT TRACK LOCK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRACK IAW DC-8 SRM 51-3-0, 53-2-0 AND 51-1Mar 30, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001819Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE F/O RT AFT SEAT TRACK LOCK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 53-Mar 30, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001799Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN 3 PLACES TO THE LT I/B AILERON O/B END, 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 SRM 51-1-21 AND EO NR 00-055 Mar 30, 2000 · N961R · Doug DC873F · AileronsSDR DHL2000804137Harness · looseF/O PITOT TUBE ELECTRIC WIRING HARNESS LOOSE. SECURED F/O PITOT TUBE ELECTRIC WIRING HARNESS PER M/M 20-50-1.Mar 30, 2000 · N804DH · Doug DC873F · Pitot/Static Anti-Ice SystemSDR DHL2000804136Angle · crackedAFT ACCY COMPT ANGLE CRACKED 3 INCHES AT STA 680.00 LONGERON 22 LT. REMOVED FASTENERS PER SRM 51-3-0. REMOVED DAMAGED ANGLE PER SRM 51 1-20. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED NEW ANGLE PER SRM 51-1-20.Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080488CBulkhead · damagedAFT BAGGAGE COMPT BULKHEAD SHOWS FILLET BROKEN AT STA 980.000 LT & RT. REMOVED FASTENERS PER SRM 51-1-21. FABRICATED LINING SUPPORT ANGLE PER SRM 53-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED ANGLE WITH NEW FASTENERS PER SRM 51-1-21.Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL200080487CAngle · brokenAFT BAGGAGE COMPT LINING SUPPORT ANGLE RT LOWER PART BROKEN AT STA 1300.0. REMOVED FASTENERS PER SRM 51-1-21. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-21.Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080486CAngle · crackedAFT BAGGAGE COMP FLOOR SUPPORT ANGLE FRAME CRACKED .5 INCH AT STA 1400.00. REMOVED FASTENERS PER SRM 53-2-0. STOP DRILLED CRACK PER SRM 53-2-0. FABRICATED DOUBLER PER SRM 53-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER WITH NEW FASTEMar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080485CAngle · crackedRT WING TO FUSELAGE FAIRING LOWER PART SUPPORT ANGLE CRACKED 1 INCH AT STA 760.00. REMOVED FASTENERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER WITH NEW FAMar 30, 2000 · N804DH · Doug DC873F · Aerodynamic FairingsSDR DHL200080482CSkin · deformedLEFT WING O/B TRAILING EDGE DEFORMED FROM XE 309.00 TO 333.00. REMOVED TRAILING EDGE FROM XE 309.00 TO XE 333.00 PER SRM 51-1-21. FABRICATED TRAILING EDGE PER SRM 51-2-3. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED TRAILING EDGE WITH NEW FASTENERMar 30, 2000 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080490CAccess Door · crackedLEFT WING L/E NR 583F ACCESS DOOR CRACKED 4 INCHES. STOP DRILLED PER SRM 57-2-1. FABRICATED DOUBLER PER SRM 57-21-1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-2-1.Mar 30, 2000 · N804DH · Doug DC873F · Service DoorsSDR DHL200080489CAngle · crackedAFT BAGGAGE COMPT FLOOR SUPPORT ANGLE FRAME CRACKED .5 INCH AT STA 1480.0. REMOVED FASTENERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-0. FABRICATED DOUBLER PER SRM 53-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER WITH NEW FASTENERS Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080439CAngle · crackedRT WING TO FUSELAGE FAIRING ANGLE CRACKED .5 INCH AT STA 630. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 53-2-5.Mar 30, 2000 · N804DH · Doug DC873F · Aerodynamic FairingsSDR DHL200080437CAngle · crackedAFT BAGGAGE COMPT FLOOR SUPPORT ANGLE FRAME CRACKED 1.52 INCH AT STA 1420.0. REMOVED FASTENERS PER SRM 51-1-21 PAGE 1. STOP DRILLED PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER PER SRM 53-2-0. CLEANED, TREATED AND PAINTED PER SRM 51-1-8 PG 1 & 2. INSTALLED DMar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080436CAngle · crackedAFT BAGGAGE COMPT FLOOR SUPPORT ANGLE FRAME CRACKED .5 INCH AT STA 1460.0. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED PER SRM 53-2-0 FIG 1B. FABRICATED ANGLE PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B PG 1 & 2. INSTALLED Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080435CAngle · crackedAFT BAGGAGE COMPT FLOOR SUPPORT ANGLE FRAME CRACKED .5 INCH AT STA 1340.0. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED PER SRM 53-2-0 FIG 18. FABRICATED DOUBLER PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B PG 1 & 2. INSTALLEMar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000804127Skin · crackedNR 2 ENGINE LT THRUST REVERSER INTERNAL SKIN CRACKED .5 INCH AT YN 223.00 11 O'CLOCK POSITION. STOP DRILLED PER SRM 78-2-1. FABRICATED DOUBLER PER SRM 78-2-1A. CLEANED, TREATED AND PRIMED PER SRM 58-1-8. INSTALLED DOUBLER PER SRM 78-2-1A.Mar 30, 2000 · N804DH · Doug DC873F · Engine Thrust ReverserSDR DHL2000804126Angle · brokenRT WING 4 EACH INTERIOR PNUEMATIC TUBING SUPPORT ANGLE BROKEN 2 INCHES AT UPPER PART BETWEEN XW 398.00 AND XW 408.00 ACCESS DOOR. REMOVED BROKEN SUPPORT ANGLE PER SRM 51-1-21. FABRICATED NEW ANGLE PER SRM 57-2-0. CLEANED, TREATED AND PRIMED AREA PER SRM 51-Mar 30, 2000 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2000804116Skin · deformedLEFT WING OUTBOARD FLAP TRAILING EDGE DEFORMED FROM XE 309.00 TO 333.00. REMOVED TRAILING EDGE FROM XE 309.00 TO 333.00 PER SRM 51-1-21. FABRICATED TRAILING EDGE PER SRM 57-2-3. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED TRAILING EDGE PER SRM 51Mar 30, 2000 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080432CSupport Bracket · brokenMAIN CARGO INTERIOR LINING SUPPORT BROKEN AT STA 280.000 9 RT & 8 RT. REMOVED BROKEN SUPPORT PER SRM 51-1-21 PG 1. FABRICATED NEW SUPPORT PER SRM 53-2-0 FIG 1 B. CLEANED AND TREATED AND PAINTED PER SRM 51-1-8 PG 18 & 19. INSTALLED NEW SUPPORT PER SRM 51-1-Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080431CSupport Bracket · crackedFWD BAGGAGE COMPARTMENT RT LINING SUPPORT FILLET CRACKED 1 INCH AT STA 220.00. REMOVED CRACKED FILLET PER SRM 51-1-21 FIG 1B. FABRICATED FILLET PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-6 PG 17-18. INSTALLED FILLET PER SRM 53-2-0 FIG Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080404CAngle · crackedFWD BAGGAGE COMPARTMENT LINING SUPPORT ANGLE STA 100 LONGERON 30 RT CRACKED .5 INCH. REMOVED FASTENERS IAW SRM 51-1-20 PAGE 3. FABRICATED DOUBLER WITH 301 72 H 0.040 IAW SRM 53-2-5 FIG 8. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PAGE 3.Mar 30, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080420CSkin · damagedLEFT WING INBOARD FLAP TRAILING EDGE DEFORMED FROM XW 104 TO XW 115. REMOVED REPAIRED AND REINSTALLED TRAILING EDGE FLAP IAW SRM 51-1-21A AND 57-2-1.Mar 30, 2000 · N804DH · Doug DC873F · Trailing Edge FlapsSDR UPS00832311Fitting · crackedINSPECTION TYPE:C1 STA 280 A PIT DOOR ANGLE SUPPORT FITTING IS BROKEN BETWEEN LONG 26R AND 27R INSIDE LIGHTENING HOLE. REMOVED AND REPLACED FITTING IAW DWG 3754025, AND SRM 51-1-21.Mar 30, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832289Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XW 454. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 30, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS00832288Fitting · crackedINSPECTION TYPE:C1 STA 208 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755211 AND SRM 51-1-20D.Mar 30, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832285Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 30, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS00832279Skin · crackedINSPECTION TYPE:C1 LT CABIN AFT ENTRY DOOR INNER SKIN IS CRACKED AT CENTER CUTOUT AREA STA 1440 LONG 12L. REPAIRED IAW SRM 52-2-0 FIG 2.Mar 30, 2000 · N812UP · Doug DC873F · Passenger/Crew DoorsSDR UPS00832268Fitting · crackedINSPECTION TYPE:C1 STA 320 LONG 27L FRAME DOOR STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW 4897274, AND SRM 51-3-0.Mar 30, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832264Fitting · crackedINSPECTION TYPE:C1 CROSS SLIDE DOOR FITTING CRACKED FS 320 AT LONG 27L. REMOVED, FAB & REPLACED SPLICE FITTING IAW DWG 9751879 & SRM 51-1-20D.Mar 30, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832263Intercostal · crackedINSPECTION TYPE:C1 FRAME IN RT NOSE TUNNEL CRACKED FS 12. REMOVED, FAB & REPLACED INTERCOSTAL IAW SRM 53-3-3 FIG 2.Mar 30, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000716Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO A CABIN SPLICE FITTING AT STA'S 300 TO 320 AND LONGERON 6L, 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 51-1-20D AND DAC DWG #47Mar 29, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002000Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 1 SEAT TRACK AT STA 319 LT AND LBL 59 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3.Mar 29, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001999Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 1 SEAT TRACK AT STA 294 LT AND LBL 59 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3.Mar 29, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001985Frame · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START IN RADIUS AT FRAME 1460, 3 INCHES UP FROM CUSP L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-055 WITH APPMar 29, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001984Shear Tie · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START IN RADIUS OF SHEAR FOOT AT STA 1280, 3 INCHES UP FROM L21R CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-Mar 29, 2000 · N961R · Doug DC873F · Fuselage Main, StructureSDR RRXA001962Skin · crackedDURING A MAINTENANCE VISIT FOUND A HOLE, CRACKS AND RIVETS LOOSE AT THE RIGHT I/B FLAP I/B FLAP WELL AT FUSELAGE ABOVE RIGHT ADF ANT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALMar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001939Skin · gougedDURING A MAINTENANCE VISIT FOUND A SEVERE GOUGE TO THE LEFT I/B FLAP RECESS WELL AREA, 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 SRM 51-1-21 AND 51-1-4.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001929Skin · dentedDURING A MAINTENANCE VISIT FOUND A DENT TO THE LEFT I/B FLAP I/B OF STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO ORIGINAL IAW DC-8 SRM 57-1-0.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001906Panel · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH PANEL AT LT TOP T/E AT STA XRS 75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-1.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001865Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 1 SEAT TRACK AT STA 319 LT AND LBL 59, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PLUG IAW DC-8 SRM 53-2-3.Mar 29, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001864Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 1 SEAT TRACK AT STA 294 LT AND LBL 59, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PLUG IAW DC-8 SRM 53-2-3.Mar 29, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001850Frame · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START IN RADIUS OF FRAME 1460 3 INCHES UP FROM CUSP AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DRILL START AND RETURNED TO SERVICE IAW EO Mar 29, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001849Shear Tie · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START IN RADIUS OF SHEAR FOOT AT STA 1280, 3 INCHES UP FROM L21R CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DRILL START SMOOTH IAW EO NR 00-05Mar 29, 2000 · N961R · Doug DC873F · Fuselage Main, StructureSDR RRXA001827Skin · crackedDURING A MAINTENANCE VISIT FOUND A HOLE, CRACKS AND RIVETS LOOSE IN THE RT I/B FLAP I/B FLAP WELL AT FUSELAGE ABOVE RT ADF ANT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEMar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001804Skin · gougedDURING A MAINTENANCE VISIT FOUND SEVER GOUGE IN THE LEFT I/B FLAP RECESS WELL AREA, 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 51-1-21 AND 51-1-4.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001794Skin · dentedDURING A MAINTENANCE VISIT FOUND A DENT TO THE LT I/B FLAP I/B OF STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO ORIGINAL IAW DC-8 SRM 57-1-0.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001770Panel · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE PANEL ON THE LT TOP TE AT STA XRS 75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-1.Mar 29, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR DHL2000804130Flange · crackedRT ELEVATOR LOWER FLANGE CRACKED .25 INCH AT XE 221.00. REMOVED CRACKED FLANGE PER SRM 51-1-21. FABRICATED NEW FLANGE PER SRM 55-20-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED NEW FLANGE PER SRM 51-1-21.Mar 29, 2000 · N804DH · Doug DC873F · Elevator Structure
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