# Service difficulty reports: Douglas DC-8F-55

A list on [Douglas DC-8F-55](https://openairdocs.org/model/douglas-dc-8f-55.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 238 reports

- [SDR 20001208AP007](https://openairdocs.org/sdr/20001208AP007.md): Longeron · cracked · Aug 28, 2000 · N55FB · Doug DC8F55 · Fuselage Main, Longeron/Stringer
  > DURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CRACKED LONGERON AT STATION 248, RECORDED ON NON-ROUTINE ITEM NR 3222. REPAIRED CRACKED LONGERON IAW SRM 53-2-2. (M)
- [SDR 20001208AP005](https://openairdocs.org/sdr/20001208AP005.md): Fitting · corroded · Aug 28, 2000 · N55FB · Doug DC8F55 · Fuselage Miscellaneous Structure
  > DURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CORRODED LONGERON FITTING AT BS 248, L-33R, RECORDED ON NON-ROUTINE ITEM NR 3257. REPLACED LONGERON SPLICE FITTING IAW SRM 51-1-20D, 51-3-0. (M)
- [SDR 20001208AP004](https://openairdocs.org/sdr/20001208AP004.md): Door · open · Aug 28, 2000 · N55FB · Doug DC8F55 · Landing Gear Retraction/Extension System
  > JUST AFTER TAKEOFF FROM KINGSTON CREW NOTICED THAT THE NLG DOOR STAYED OPEN. RETURNED FLIGHT BACK TO KINGSTON AND LANDED WITH A GROSS WEIGHT OF 190,000 LBS. UPON INSPECTION CONFIRMED OPEN DOOR. OPS CHECK NOSE GEAR DOOR LINKAGE IAW DC8 MM 32-2-6 FOUND OK. (
- [SDR 2000ZZZX690](https://openairdocs.org/sdr/2000ZZZX690.md): Fitting · cracked · Nov 18, 1999 · N812TC · Doug DC8F55 · Trailing Edge Flap Actuator
  > LEFT HAND STA 98 FLAP ACTUATOR ATTACH FITTING (INSIDE PANEL 562L) HAS APPROXIMATELY 1 INCH CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM'S 57-3-0, 51-3-2, AND 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX684](https://openairdocs.org/sdr/2000ZZZX684.md): Door · damaged · Nov 17, 1999 · N812TC · Doug DC8F55 · Fixed Inner Doors
  > REPLACED COCKPIT DOOR. FABRICATED NEW COCKPIT DOOR PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX697](https://openairdocs.org/sdr/2000ZZZX697.md): Floor Panel · corroded · Nov 16, 1999 · N812TC · Doug DC8F55 · Fuselage Floor Panel
  > CORROSION EXISTS ON THE SURFACE OF ALL FLOOR PLANKS FROM STA 280 TO STA 1490 L21L TO L21R. REMOVED CORROSION BY CHEMICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNAT
- [SDR 2000ZZZX708](https://openairdocs.org/sdr/2000ZZZX708.md): Filler · missing · Nov 11, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > DUE TO EXISTING REPAIR, DOUBLER ON LT FRONT SPAR (XRS 69.5) LOWER WING PLANK, TAPER FILLERS NEED TO BE FABRICATED TO COMPLETE SB 57-2OR5. FABRICATED FILLERS AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-22-99. REF: ZANTOP INTERNATIONAL AIRLINES,
- [SDR 2000ZZZX676](https://openairdocs.org/sdr/2000ZZZX676.md): Skin · cracked · Nov 11, 1999 · N812TC · Doug DC8F55 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND.50 INCH LOWER L/E SURFACE AT INBOARD SLOT APPROXIMATELY XFS 213.5 LT WING. NDT TO ASSURE CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-11-99. REF: ZANTOP INTERNATIONAL
- [SDR 2000ZZZX675](https://openairdocs.org/sdr/2000ZZZX675.md): Skin · cracked · Nov 11, 1999 · N812TC · Doug DC8F55 · Wing, Plate/Skin
  > FOUND DURING C-CHECK. CRACK LOCATED AT INBOARD SLOT LOWER L/E, 1.50 INCHES LONG ON RT WING XFS 214.25. NDT CRACK TO ASSURE THAT CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-11-99. REF: ZAN
- [SDR 2000ZZZX694](https://openairdocs.org/sdr/2000ZZZX694.md): Spar · cracked · Nov 8, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > LOWER FRONT SPAR HORIZONTAL LEG 10 INCH CRACK BS 680 - 26.5 INCHES TO 36.50 INCHES RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLER, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30R5. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX671](https://openairdocs.org/sdr/2000ZZZX671.md): Spar · cracked · Nov 8, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > LOWER FRONT SPAR 1.50 INCH CRACK FS 680 LBL 34 INCHES Z AXIS -47 AND.50 INCH CRACK BS 680 LBL XCW 39 INCHES AND XCW 43 INCHES Z AXIS -47 INCH. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30-R5. REF: ZANTOP INTERNATIONAL AI
- [SDR 2000ZZZM213](https://openairdocs.org/sdr/2000ZZZM213.md): Spar · cracked · Nov 8, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > LOWER FRONT SPAR HORIZ LEG 10 INCHES CRACK FS 680 - 26.5 TO 36.5 INCH RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW DC-8 S/B 57-30R5. (M)
- [SDR 2000ZZZX681](https://openairdocs.org/sdr/2000ZZZX681.md): Fairing · damaged · Nov 5, 1999 · N812TC · Doug DC8F55 · Aerodynamic Fairings
  > PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX680](https://openairdocs.org/sdr/2000ZZZX680.md): Fairing · damaged · Nov 5, 1999 · N812TC · Doug DC8F55 · Aerodynamic Fairings
  > PANEL 161V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX679](https://openairdocs.org/sdr/2000ZZZX679.md): Skin · damaged · Nov 5, 1999 · N812TC · Doug DC8F55 · Landing Gear Doors
  > RT MLG DOOR CENTER STRUT/SEVERAL SCREWS STARTING TO PULL THROUGH SKIN. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZM260](https://openairdocs.org/sdr/2000ZZZM260.md): Skin · damaged · Nov 5, 1999 · N812TC · Doug DC8F55 · Wing, Plate/Skin
  > SCREWS PULLING THROUGH SKIN L/E CENTER SECTION LOWER SURFACE XW454 LEFT WING. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 11/05/99. (M)
- [SDR 2000ZZZX670](https://openairdocs.org/sdr/2000ZZZX670.md): Tee · corroded · Nov 4, 1999 · N812TC · Doug DC8F55 · Wing Miscellaneous Structure
  > THROUGH ACCESS HOLE 506C AND THROUGH INBOARD RIB CUT-OUT, INBOARD LOWER WING STR 63-72 AT STA XW.000 IN NR 3 MAIN TANK HAS CORROSION BETWEEN STRINGER. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND T-CHORD OUT OF LIMITS IAW DC-8 SRM 57-2-0. REPLACED T-CHORD I
- [SDR 2000ZZZX711](https://openairdocs.org/sdr/2000ZZZX711.md): Web · cracked · Nov 2, 1999 · N812TC · Doug DC8F55 · Trailing Edge Flaps
  > FOUND DURING C-CHECK. RT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-29-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX688](https://openairdocs.org/sdr/2000ZZZX688.md): Gilliner · damaged · Nov 2, 1999 · N812TC · Doug DC8F55 · Cargo Compartments
  > REPLACED MAIN CABIN GILLINER AND STRAPS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 7-24-99. REF: ZANTOP INTERNAL AIRLINES, INC. ZIAA.
- [SDR 2000ZZZX682](https://openairdocs.org/sdr/2000ZZZX682.md): Fitting · corroded · Nov 2, 1999 · N812TC · Doug DC8F55 · Ailerons
  > PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX677](https://openairdocs.org/sdr/2000ZZZX677.md): Skin · cracked · Nov 2, 1999 · N812TC · Doug DC8F55 · Ailerons
  > INBOARD AILERON L/E PLATING AT STA XA 503.5 HAS A 2.5 INCH CRACK (EO). ROUTED OUT CRACK. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-28-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZM215](https://openairdocs.org/sdr/2000ZZZM215.md): Web · cracked · Nov 2, 1999 · N812TC · Doug DC8F55 · Trailing Edge Flaps
  > FOUND DURING C-CHECK, RIGHT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT CRACKED SECTION. FABRICATED NEW WEB AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3, DATED 10/29/99. (M)
- [SDR 2000ZZZX695](https://openairdocs.org/sdr/2000ZZZX695.md): Spar · cracked · Oct 29, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > FOUND DURING C-CHECK. A 4.75 INCH CORROSION CRACK APPROXIMATE STA XCW 31.0 LT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK, REMOVED. TREATED AND PRIMED. FILLED SEALER, CONTINUED THE INSTALLATION OF LOWER FRONT SPAR
- [SDR 2000ZZZM214](https://openairdocs.org/sdr/2000ZZZM214.md): Spar · cracked · Oct 29, 1999 · N812TC · Doug DC8F55 · Wing Spar
  > FOUND DURING C-CHECK, A 4.75 INCH CORROSION CRACK APPROX STATION XCW 31 LEFT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK. REMOVED, TREATED AND PRIMED. FILLED SEALER CONTINUED THE INSTALLATION OF LOWER FRONG SPAR CA
- [SDR 2000ZZZX703](https://openairdocs.org/sdr/2000ZZZX703.md): Skin · cracked · Oct 28, 1999 · N812TC · Doug DC8F55 · Nacelle/Pylon, Plate/Skin
  > AFT LEFT COWL DOOR HAS 3 INCH CRACK OUTSIDE SKIN AT INLET SCOOP NR 3 ENGINE. STOP DRILLED, NDT CONFIRMED CRACK HAS BEEN STOPPED. WELDED CRACK AND NDT NO FLAWS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-8-99. REF: ZAN
- [SDR 2000ZZZX709](https://openairdocs.org/sdr/2000ZZZX709.md): Gear Tab · dented · Oct 25, 1999 · N812TC · Doug DC8F55 · Elevator, Tab Structure
  > RT ELEVATOR GEAR TAB DAMAGED DENT/CREASE. REPAIRED RT ELEVATOR GEAR TAB PER EO 99-136 WITH APPROVED 8110-3 DATED 10-15-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX669](https://openairdocs.org/sdr/2000ZZZX669.md): Ring · missing · Oct 21, 1999 · N812TC · Doug DC8F55 · Engine Thrust Reverser
  > FOUND DURING C-CHECK. DOUBLER AROUND CIRCUMFERENCE OF FORWARD SIDE OF WIND SOCK HAS SECTION MISSING. NR 4 ENGINE. FABRICATED NEW SECTION, WELDED IN PLACE NDT WELD (NO FLAWS) PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10-19-99. REF: ZANTOP INTERNATIONAL
- [SDR 2000ZZZX704](https://openairdocs.org/sdr/2000ZZZX704.md): Duct · cracked · Oct 19, 1999 · N812TC · Doug DC8F55 · Fire Detection
  > NR 2 ENGINE INBOARD SIDE 1 O'CLOCK POSITION. FIRE EXTINGUISHER DUCT CRACKED AT ATTACH ANGLE. REMOVED DUCT, REPAIRED PER BOEING MEMO 99-00006 H AND EO 99-136 WITH APPROVED 8110-3 DATED 8-23-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZM235](https://openairdocs.org/sdr/2000ZZZM235.md): Drain · cracked · Oct 18, 1999 · N812TC · Doug DC8F55 · Landing Gear Doors
  > FOUND DURING C-CHECK, LEFT MAIN GEAR WELL FORWARD DRAIN SPOUT CRACKED. NDT TO DETERMINE END OF CRACK, STOP DRILLED AND WELDED PER MIL-STD-2219. NDT NO FLAWS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10/01/99. (M)
- [SDR 2000ZZZX696](https://openairdocs.org/sdr/2000ZZZX696.md): Skin · misrepaired · Oct 14, 1999 · N812TC · Doug DC8F55 · Fuselage Main, Plate/Skin
  > LEFT HAND AFT ENTRY DOOR FUSELAGE SKIN CUT-OUT, PREVIOUS REPAIR IMPROPER STA 1400 - L21L. REMOVED EXISTING DOUBLER. FABRICATED NEW DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-4-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX689](https://openairdocs.org/sdr/2000ZZZX689.md): Frame · cracked · Oct 14, 1999 · N812TC · Doug DC8F55 · Fuselage Main, Frame
  > FUSELAGE STATION 460 LONGERON 21R FRAME BENT AND FRAME CAP CRACKED. REMOVED DAMAGED SECTION OF FRAME. FABRICATED FRAME SPLICES IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLI
- [SDR 2000ZZZX702](https://openairdocs.org/sdr/2000ZZZX702.md): Rivet · sheared · Oct 9, 1999 · N812TC · Doug DC8F55 · Engine Air Intake System
  > NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR PNEUMATIC HEAT EXCHANGER. IT IS ACCEPTABLE TO USE AS IS, IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX699](https://openairdocs.org/sdr/2000ZZZX699.md): Heat Shield · cracked · Oct 6, 1999 · N812TC · Doug DC8F55 · Engine Fireseals
  > NR 1 ENGINE HEAT SHIELD FOR MAIN FUEL LINE CRACKED. STOP DRILLED CRACK, NDT TO ASSURE CRACK HAD BEEN STOPPED. WELDED ACCORDING TO MIL-STD-2219. NDT WELD NO FLAWS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-25-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC.,
- [SDR 2000ZZZX687](https://openairdocs.org/sdr/2000ZZZX687.md): Pipe · chafed · Oct 5, 1999 · N812TC · Doug DC8F55 · Engine Cooling System
  > FOUND DURING C-CHECK. NR 3 PYLON VENTILATION PIPE CHAFED. FABRICATED DOUBLERS AND WELDED IN PLACE IAW BOEING MESSAGE M-7200-99-07969 WITH APPROVED 8110-3 DATED 10-22-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX678](https://openairdocs.org/sdr/2000ZZZX678.md): Skin · cracked · Sep 27, 1999 · N812TC · Doug DC8F55 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP SKIN JUST BELOW HINGE FITTING IS CRACKED STA XR 219. STOP DRILLED CRACKS, NDT TO ASSURE CRACKS HAD BEEN STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-15-99. REF: ZANTOP INTERNATIONAL AIRLINES
- [SDR 2000ZZZX672](https://openairdocs.org/sdr/2000ZZZX672.md): Fitting · cracked · Sep 23, 1999 · N812TC · Doug DC8F55 · Elevator Tab, Attach Fittings
  > RIGHT ELEVATOR NR 2 A-FRAME CRACKED. REMOVED AND REPLACED NR 2 POSITION A-FRAME RT ELEVATOR IAW DC-8 OHM 27-30-1. (X)
- [SDR 2000ZZZX691](https://openairdocs.org/sdr/2000ZZZX691.md): Longeron · corroded · Sep 16, 1999 · N812TC · Doug DC8F55 · Fuselage Main, Longeron/Stringer
  > LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIA
- [SDR 2000ZZZM210](https://openairdocs.org/sdr/2000ZZZM210.md): Longeron · corroded · Sep 16, 1999 · N812TC · Doug DC8F55 · Fuselage Main, Longeron/Stringer
  > LONGERON 6R STATION 1490 TO 1600 HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED AND REPAIR PER DC-8 SRM 53-2-2 PAGE 59/60 PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/11/99. (M)
- [SDR 2000ZZZX700](https://openairdocs.org/sdr/2000ZZZX700.md): Spinner · cracked · Sep 15, 1999 · N812TC · Doug DC8F55 · Turbine Engine Air Inlet Section
  > NOSE COWL CRACKED AT 6:00 O'CLOCK POSITION NR 4 ENGINE. CUT OUT PREVIOUS WELD, NDT TO ASSURE ALL CRACKS STOPPED. FABRICATED PLUG AND WELDED IN PLACE. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 8-31-99. REF: ZANTOP INTERNATIONAL AIRL
- [SDR 2000ZZZX692](https://openairdocs.org/sdr/2000ZZZX692.md): Ring · cracked · Sep 15, 1999 · N812TC · Doug DC8F55 · Engine Thrust Reverser
  > LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIA
- [SDR 2000ZZZX683](https://openairdocs.org/sdr/2000ZZZX683.md): Leg · broken · Sep 15, 1999 · N812TC · Doug DC8F55 · Hydraulic Compartment Doors
  > LEFT MAIN W/W SAFETY NET LEG BROKEN OFF. WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 9-10-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZM211](https://openairdocs.org/sdr/2000ZZZM211.md): Ring · cracked · Sep 15, 1999 · N812TC · Doug DC8F55 · Engine Thrust Reverser
  > INBOARD TOP SIDE OF TRANSLATING RING HAS CRACK NR 4 ENGINE. STOP DRILLED CRACK, NDT TO ASSURE CRACK STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3 DATED 9/2/99. (M)
- [SDR 2000ZZZX673](https://openairdocs.org/sdr/2000ZZZX673.md): Longeron · corroded · Sep 14, 1999 · N812TC · Doug DC8F55 · Fuselage Main, Longeron/Stringer
  > LONGERON 30, 31 RIGHT AT STA 320 HAD CORROSION. REMOVED CORROSION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-1-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX686](https://openairdocs.org/sdr/2000ZZZX686.md): Panel · corroded · Sep 10, 1999 · N812TC · Doug DC8F55 · Leading Edge Devices
  > LEFT OUTBOARD MOST UPPER SLOT DOOR BOTTOM INBOARD OF INBOARD ADJ SCREW HAS CORROSION XS 503.789. BLENDED OUT CORROSION, TREATED AND PRIMED. MAXIMUM UNDER CUT IN RIB IS DOWN.078 INCHES. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-
- [SDR 2000ZZZX701](https://openairdocs.org/sdr/2000ZZZX701.md): Rivet · sheared · Sep 9, 1999 · N812TC · Doug DC8F55 · Engine Air Intake System
  > NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR OIL COOLER. IT IS ACCEPTABLE TO USE AS IS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX706](https://openairdocs.org/sdr/2000ZZZX706.md): Outflow Valve · corroded · Sep 8, 1999 · N812TC · Doug DC8F55 · Pressure Regulator/Outflow Valve
  > SUGAR SCOOP CORRODED (OUTFLOW VALVE) STA 1323. REMOVED CORROSION IAW DC-8 SRM 51-1-8. WELDED AREA, NDT TO ASSURE NO FLAWS (NONE FOUND) BLEND SMOOTH AND FINISHED PER FACTORY SPECS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-14-99. REF: ZANTOP INTERNATIONAL A
- [SDR 2000ZZZM229](https://openairdocs.org/sdr/2000ZZZM229.md): Fitting · cracked · Sep 2, 1999 · N55FB · Doug DC8F55 · Wing Miscellaneous Structure
  > DURING B-CHECK INSPECTION, FOUND 20 INCH CRACK AT LEFT INBOARD CANOE FITTING AT STATION 98. REPLACED FITTING AT LEFT CANOE IAW MM 27-27-7. (M)
- [SDR 2000ZZZM245](https://openairdocs.org/sdr/2000ZZZM245.md): Skin · corroded · Aug 31, 1999 · N55FB · Doug DC8F55 · Rudder, Plate/Skin
  > DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE AT LEFT AND RIGHT RUDDER SKIN. REPAIRED CORROSION DAMAGE IAW FINE AIR EO NR 9808131, SRM 51-1-21. (M)
- [SDR 2000ZZZX685](https://openairdocs.org/sdr/2000ZZZX685.md): Panel · corroded · Aug 30, 1999 · N812TC · Doug DC8F55 · Leading Edge Devices
  > OUTBOARD SLOT LEFT WING L/E HAS AREA OF EXFOLIATION XW 454. CUT OUT AREA OF EXFOLIATION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-13-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)
- [SDR 2000ZZZX674](https://openairdocs.org/sdr/2000ZZZX674.md): Skin · cracked · Aug 26, 1999 · N812TC · Doug DC8F55 · Wing, Plate/Skin
  > LEFT WING CENTER L/E OTBD EDGE XFS 291.500 FWD VERTICAL PLATE CRACKED APPROXIMATELY 3 INCHES. REMOVED OUTBOARD END WEB. FABRICATED NEW SECTION AND SPLICE PLATE AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-20-99. REF: ZANTOP INTERNATIONAL AIRL

Next page: https://openairdocs.org/model/douglas-dc-8f-55/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'DC8F55'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8f-55/reports

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