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 DHL2000803134Angle · crackedAT C-CHECK, AFT FWD LOWER CARGO RT NR 2 AFT DOOR FRAME PROTECTIVE ANGLE CRACKED. REMOVED DAMAGED AREA AND PERFORMED ANTI-CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER IAW SRM 52-2-0 PAGE 13. TREATED AND PRIMED IAW SRM 51-1-8 PG 12. INSTALLJan 11, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803111Seat Track · deterioratedAT C-CHECK, MAIN CARGO NR 3 LT SEAT TRACK FLANGE DETERIORATED BETWEEN FS 780 TO FS 810. REMOVED DAMAGED TRACK FLANGE IAW SRM 53-2-3, FABRICATED AND INSTALLED TRACK FLANGE IAW SRM 51-1-21 PG 7. REF: N/R 5194.Jan 11, 2000 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2000803106Floor Support · crackedAT C-CHECK, AFT FWD LOWER CARGO COMPT LATERAL FLOOR SUPPORT STRAP SHOWS CRACK AT STA 440.00 NEAR L3 RT. REMOVED FLOOR SUPPORT STRAP IAW SRM 51-1-8 PAGE 11, FABRICATED DOUBLER, TREATED AND PRIMED IAW SRM 53-2-0 PAGE 26 FIG 3, INSTALLED DOUBLER WITH SOLID RIVETJan 11, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00831270Switch · inoperativeMASTER FIRE WARNING RESET SWITCH FAILED AFTER TEST OF SECOND ENGINE. REPLACED MASTER FIRE WARNING SWITCH.Jan 11, 2000 · N851UP · Doug DC873F · Detection SystemSDR RRX000008Trim Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK, MAIN CARGO DOOR CUT OUT AFT LWR CORNER, TRIMPLATE CRACKED AND METAL BROKEN OFF. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 11, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003373Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE 'B' PIT GILINER SUPPORT AT STA 560 TO 640 AND X-36 Z-10, 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 51-1-21A Jan 10, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003369Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BOARD AT FS 50 X+50 Z=0, 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, FIG 1F AND 53-2-0.Jan 10, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA001035Vane · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP VANE AT XFS 225 TO XFS 322. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLAP VANE AND INSTALLED NEW VANE IAW DC-8 MM 27-51-Jan 10, 2000 · N832AL · Doug DC873F · Trailing Edge FlapsSDR RRXA001030Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT BETWEEN STA 370 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 SRMJan 10, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000660Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT HORIZONTAL STAB LOWER FWD SUPPORT BRACKET (O/B END) AT STA XFS 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SUPPORT BRACKET AND INSTALLED IAW Jan 10, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA000649Skin · crackedDURING A MAINTENANCE VISIT FOUND A DEEP DENT AND CRACK AT THE RT HORIZONTAL STAB UPPER PLATING JUST FWD OF ACCESS HOLE AT STA XE 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8Jan 10, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR RRXA000530Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 1160 TO STA 1210 AND BL 60 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DC-Jan 10, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2000803101Spar · brokenLEFT WING REAR SPAR UPPER CAP STEEL PLATE BROKEN 1 IN STA 350.00. REMOVED PLATE AND FASTENERS IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11. FABRICATED PLATE IAW SRM 57-2-1 PAGE 6. INSTALLED PLATE AND SECURED WITH SOLID RIVETSJan 10, 2000 · N803DH · Doug DC873F · Wing SparSDR DHL2000803137Stiffener · crackedAT C-CHECK, WING TO FUSELAGE FAIRING HOUSING REINFORCING STRIP CRACKED 1/2 INCH AT XWG 69.500 CLOSE TO FS 970.00. REMOVED DAMAGE AREA AND PERFORMED ANTI-CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER PLATE IAW SRM 53-2-0 PAGE 2E-2F. PRIMED PJan 10, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003367Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD CARGO FWD BULKHEAD LOWER PANEL MOUNTING STRAP AT STA 80 AND L31L TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRJan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003366Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON "B" PIT FLOOR PANEL ATTACH STRAP BETWEEN STA'S 360-460 AND L33L, 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-Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003365Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 480 TO 510 AND L31R, 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 53-4-1, 51-1-20, 51-1Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003364Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AROUND FASTENERS AT FS 120-140 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0.Jan 9, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003363Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR SUPPORT STRAP IN 'B' PIT BETWEEN STA'S 360-460 AND L33R, 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-Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003358Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GILINER SUPPORT AROUND NUT PLATE AT STA 75 X=18 TO 48L AND -24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DOUGLAS DWJan 9, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA003355Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ANGLE DOUBLER AT FS Y1000 AND L35R, 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, FIG 2F, 51-1-20Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000652Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO A LONGERON END FITTING AT STA 680 AND LONGERON 3R, 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, 51-3-0 AND 51-Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000651Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LONGERON END FITTING AT STA 680 AND LONGERON 7R, 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, 51-3-0 AND 5Jan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000650Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LONGERON END FITTING AT STA 680 AND LONGERON 8L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW SRM 53-1-0, 51-3-0, 51-1-23 AJan 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003383Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE FLOOR BEAM AT STA 340 AND RBL -12-48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PART IAW DC-8 SRM 53-2-0.Jan 8, 2000 · N831AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003362Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 6 LATCH BACK-UP FITTING AT STA 330 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED REA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 51-1-21.Jan 8, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003361Rod · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ADJ TENSION ROD FOR "C" PIT DOOR COUNTER BALANCE SPRINGS AT STA 1070, X=-40 AND Z=-30 AND L26R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTJan 8, 2000 · N831AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003360Jackscrew · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H HORIZONTAL STABILIZER JACK SCREW AT STA 1800 AND X=-24, Z=35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW MM 27-Jan 8, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA003359Jackscrew · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H HORIZONTAL STABILIZER JACK SCREW AT STA 1800 X=24 Z=35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-41-1.Jan 8, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA003357Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD CARGO FWD BULKHEAD PANEL MOUNTING LOWER STRAP AT STA 80, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED.Jan 8, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003353Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BEAM AT STA Y900 TO Y920, 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 FIG 1F, 53-1-0 AND DC-8 DJan 8, 2000 · N831AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001025Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 960 TO STA 980 AND BL44R. 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 51-1Jan 8, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000004Frame · tool damageDURING A MAINTENANCE VISIT FOUND TOOLING DAMAGE AT FRAME, STA 940, BETWEEN LONGERON 20 RIGHT AND LONGERON 21 RIGHT. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #00-016 WITH APPROVED 8110-3 DATED 01/20/00.Jan 8, 2000 · N792FT · Doug DC873F · Fuselage Main, FrameSDR RRXA000646Seat Track · wornDURING A MAINTENANCE VISIT, FOUND DAMAGE TO MAIN DECK SEAT TRACK BETWEEN STA 580 TO 600 AND LBL 45, 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 53-2-3.Jan 8, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000560Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SPLICE FITTING IMMEDIATELY AFT AT STA 8 AND LONGERON 29 RIGHT BULKHEAD IN A/C COMPARTMENT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW SRM 51-1-8. REPLACED FITTING AND INSTAJan 8, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000558Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SPLICE FITTING AT STA 70 AND LONGERON 30 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SPLICE FITTING IAW DC-8 SRM 51-1-20 AND 51-3-0. (CJan 8, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803129Frame · crackedAT C-CHECK, AFT ACCESSORIES COMPT FRAME DOUBLER CRACKED 3 INCHES AT 640.000, BETWEEN L20 AND L22 LT. REMOVED DAMAGED AREA AND PERFORMED ANTI CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2C-2E. TREATED AND PRIMED DOUBLERJan 8, 2000 · N803DH · Doug DC873F · Fuselage Main, FrameSDR RRXA003371Vane · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT INBD SLOT VANE INBD LWR CORNER AT XILO.7095, 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 51-1-21, 51-3-0,Jan 7, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA003356Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NUT PLATES ON FRAME UNDER FLANGE AT FS 1100 AND L36L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0.Jan 7, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000703Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE RT WING L/E RIB AFT UPPER END AT STA XFS 741.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIRED PARTS IAW DC-8 Jan 7, 2000 · N831AL · Doug DC873F · Wing Main, Frame StructureSDR RXA000661Strap · damagedDURING A MAINTENANCE VISIT, FOUND OPEN HOLES ON FRAME UPPER STRAP AT STA 1140 AND LONGERON 33R TO 35L, 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 5755Jan 7, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000532Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1660 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 4773146. CORROSION Jan 7, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000803138Skin · delaminatedAT C-CHECK, RT WING TRAILING EDGE LOWER PANEL DELAMINATED FROM XW 5.000 TO 90.0000. REMOVED PANEL AND FASTENERS IAW SRM 51-1-21 PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. REPLACED AND SECURED PANEL WITH SOLID RIVETS IAW SRM 51-1-21 PAGJan 7, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL2000803130Panel · delaminatedAT C-CHECK, RT WING NR 546 ACCESS PANEL LOWER PART DELAMINATED FROM STA XW 5.000 TO XW 20.000. REMOVED NR 546 ACCESS PANEL AND FASTENERS IAW SRM 51-1-21A PG 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED AND SECURED RT WING NR 546 ACCJan 7, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL2000803128Panel · delaminatedAT C-CHECK, LT WING NR 546 ACCSES PANEL DELAMINATED FROM XW 47.000. REMOVED FASTENERS AND PANEL FROM LT WING. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. REPLACED PANEL AND SECURED WITH SOLID RIVETS.Jan 7, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL2000803126Fairing · delaminatedAT C-CHECK, RT WING TO FUSELAGE FAIRING NR 709 DELAMINATED AT UPPER SKIN. REMOVED SCREWS AND DELAMINATED PANEL IAW SRM 51-3-0 PAGE 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. REPLACED AND SECURED COVER WITH SCREWS IAW SRM 51-3-0 PAGE 1 & 2 (Jan 7, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR DHL2000803125Fairing · delaminatedAT C-CHECK, LT WING TO FUESLAGE FAIRING NR 705 UPPER SKIN DELAMINATED. REMOVED SCREWS AND DELAMINATED PANEL IAW SRM 51-3-0 PAGE 3. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11&12. INSTALLED OVERHAULED PANEL (WITH SERVICEABLE TAG) AND SECURED WITH SCREJan 7, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR DHL2000803124Fairing · delaminatedLEFT WING TO FUSELAGE FAIRING DELAMINATED. REMOVED FASTENERS AND PANEL FOR REPAIR IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED OVERHAULED PANEL (WITH SERVICEABLE TAG) AND SECURED CHERRY MAX RIVETS IAW SRM Jan 7, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR DHL2000803122Skin · delaminatedAT C-CHECK, LEFT WING TRAILING EDGE PANEL DELAMINATED FROM STA 693.000. REMOVED FASTENERS AND DELAMINATED PANEL IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11&12. REPLACED WITH SERVICEABLE PANEL AND SECURED WITH SOLID RIVETS IAWJan 7, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR RRXA003390Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 AT FS 8 TO 70 , 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 51-1-21 AND 51-1-11.Jan 6, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer
Back to Douglas DC-8-73F