# Service difficulty reports: Douglas DC-8-55

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

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 126 reports

- [SDR K4HA99099](https://openairdocs.org/sdr/K4HA99099.md): Ballast · failed · Dec 18, 1999 · N807CK · Doug DC855 · Instrument Panel
  > SJS - FLT 14949 - SMOKE COMING FROM F/O RAIN REMOVAL HANDLE AREA. INSPECTED AND FOUND BURNED BALLAST FOR MAIN INSTRUMENT LIGHTS. REMOVED CANNON PLUG AND STOWED PLUG, PLACED ON DMI. INSTALLED PLACARDS. (M)
- [SDR CKSA98012](https://openairdocs.org/sdr/CKSA98012.md): Fire Loop · chaffing · Feb 12, 1998 · N807CK · Doug DC855 · Fire Detection
  > NR 2 ENG FIRE LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT ACCOMPANIED BY BELL, SYSTEM CHECKS OK. FOUND FIRE LOOP CHAFING. REPOSITIONED RUBBER GROMMET, CLEANED CANNON PLUG AND LEAK CHECKED BLEED SYSTEM. OPS CHECKS GOOD IAW DC8 MM 26-2-0.
- [SDR CKSA98013](https://openairdocs.org/sdr/CKSA98013.md): Switch · failed · Jan 6, 1998 · N801CK · Doug DC855 · Landing Gear Position and Warning
  > THIRTY MINS AFTER T/O, RIGHT LANDING GEAR LIGHT ILLUMINATED (GOOD UPLATCH CHECK PRIOR TO THIS). FOUND PUSH PIN AT RIGHT GEAR DOWN AND LOCK SWITCH. REPAIRED AND SYSTEM OPS CHECKS GOOD IAW MM CHAPTER 32-7-0.
- [SDR CKSA97177](https://openairdocs.org/sdr/CKSA97177.md): O-Ring · failed · Apr 4, 1997 · N807CK · Doug DC855 · Hydraulic Pump (Electric/Engine), Main
  > ON BASE LEG DURING FLAP EXTENSION AILERON REVERSION LIGHT INTERMITTENT AND YOKE WENT INTO MANUAL REVERSION. CHECKLIST ACCOMPLISHED AND EMERGENCY DECLARED FOR PRECAUTIONARY REASONS. ABNORMAL HYDRAULIC OPERATION LANDING. QUANTITY MAINTAINED AT AUXILIARY LEVEL
- [SDR CKSA97171](https://openairdocs.org/sdr/CKSA97171.md): Doubler · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION. HEAVY CORROSION ON FINGER DOUBLER OUTBOARD OF STRINGER 31 LT FS 1260. CUT OUT AREA AND INSTALLED REPAIR IAW AIA SKETCH AIA/E/2475 EA 97-013A. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUTINE TASK CARD
- [SDR CKSA97170](https://openairdocs.org/sdr/CKSA97170.md): Skin · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION INNER SKIN CORRODED AT FS 840 BELOW LONGERON 22L. REPAIRED CORRODED AREA IAW AIA SKETCH AIA/E/2487 EA 97-013 A AND AIA 8110-3 DATED 1-19-97. C-1 CHECK INSPECTION WORK CARD NUMBER 3010. NON-ROUTINE TASK CA
- [SDR CKSA97169](https://openairdocs.org/sdr/CKSA97169.md): Frame · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Frame
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 1140 FRAME AT STRINGER 36. REPAIRED IAW AIA/E/2517 AND DC8 SRM 51-1-20D EA 97-013A. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUTINE TASK CARD NUMBER 93040.
- [SDR CKSA97168](https://openairdocs.org/sdr/CKSA97168.md): Flange · damaged · Mar 24, 1997 · N809CK · Doug DC855 · Wing Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LOWER ACCESS PANEL FLANGE DAMAGED OUTBOARD MAIN LANDING GEAR DOOR. REPAIRED LEFT HAND WING LOWER ACCESS PANEL FLANGE IAW SKETCH AIA/E/2509 EA 97-013A. C-1 CHECK INSPECTION WORK CARD NUMBER 1002. NON-ROUTINE
- [SDR CKSA97167](https://openairdocs.org/sdr/CKSA97167.md): Access Door · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon, Bulkhead/Firewall
  > DURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON ACCESS DOOR 411 CRACKED AT SEVERAL FASTENER HOLES. REPAIRED IAW AIA SKETCH AIA/E/2505 SRM 51-1-8, 51-1-20D EA 97-013A. CORROSION TASK CARD NUMBER 84-1-0551. NON-ROUTINE TASK CARD NUMBER 93384.
- [SDR CKSA97166](https://openairdocs.org/sdr/CKSA97166.md): Web · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION LEFT HAND WHEEL WELL OVERHEAD WEB ABOVE LONGERON 24 BETWEEN 1ST AND 2ND FITTINGS. REPAIRED WEB IAW AIA SKETCH AIA/E/2500 EA 97-013A. CORROSION TASK CARD NUMBER 574L-0551. NON-ROUTINE TASK CARD NUMBER 928
- [SDR CKSA97165](https://openairdocs.org/sdr/CKSA97165.md): Doubler · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON ACCESS DOOR 407 DOUBLER CRACKED AT UPPER FASTENER HOLE. REPAIRED DAMAGE TO ACCESS DOOR DOUBLER IAW SKETCH AIA/E/2504, SRM 51-1-8, 51-1-20 EA 97-013A. CORROSION TASK CARD NUMBER 84-1-0551. NON-ROUTINE TASK CARD
- [SDR CKSA97164](https://openairdocs.org/sdr/CKSA97164.md): Doubler · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION. HEAVY CORROSION ON FINGER DOUBLER OUTBOARD OF STRINGER 31LT FS 1280. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 51-1-8, AIA SKETCH AIA/E/2475 EA 97-013A. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUT
- [SDR CKSA97163](https://openairdocs.org/sdr/CKSA97163.md): Spar Web · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON UPPER SPAR WEB CRACKED UNDER DOUBLER OUTBOARD SIDE APPROXIMATELY STA YOP244. INSTALLED REPAIR AS PER AIA/E/2491 EA 97-013A. CORROSION TASK CARD NUMBER 81-1-0551. NON-ROUTINE TASK CARD NUMBER 93408.
- [SDR CKSA97162](https://openairdocs.org/sdr/CKSA97162.md): Fitting · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEFT HAND WHEEL WELL ABOVE FORWARD END OF LONGERON 24 FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-01-20 AND 51-1-0. CORROSION TASK CARD NUMBER 574L-0551. NON-ROUTINE TASK CARD NUMBER 92831.
- [SDR CKSA97161](https://openairdocs.org/sdr/CKSA97161.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION FLOORBEAM UPPER FORWARD FLANGE STA 822 RIGHT SIDE. REMOVED CORROSION OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2493 REV ORIG EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 0060. NON-ROUTINE
- [SDR CKSA97160](https://openairdocs.org/sdr/CKSA97160.md): Skin · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Wing, Plate/Skin
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION LEFT HAND WING UPPER SURFACE SKIN THICKNESS EXCEEDS LIMITS AT XRS535.00. REMOVED MINOR EXISTING CORROSION AROUND FASTENERS AND REPAIRED AS REQUIRED. REPAIRED IAW AIA SKETCH AIA/E/2520 EA 97-013. CORROSIO
- [SDR CKSA97159](https://openairdocs.org/sdr/CKSA97159.md): Spar Cap · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION NR 3 PYLON UPPER OUTBOARD SPAR CAP CRACKED AT STA YIP230. INSTALLED REPAIR TO UPPER OUTBOARD SPAR CAP IAW AIA SKETCH AIA/E/2519 EA 97-013. CORROSION TASK CARD NUMBER 83-1-0551. NON-ROUTINE TASK CARD NUMB
- [SDR CKSA97158](https://openairdocs.org/sdr/CKSA97158.md): Angle · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 857 LBL 25 TO RBL 60 SHEAR WEB TO FLOORBEAM ATTACH ANGLE CORRODED. CLEANED AND TREATED CORROSION IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW AIA SKETCH AIA/E/2518 DATED 2-4-97 EA 97-013. CORROSION TASK C
- [SDR CKSA97157](https://openairdocs.org/sdr/CKSA97157.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION FOUND LEVEL 2 CORROSION FS 1200 RBL 40 FLOORBEAM. REPAIRED IAW AIA SKETCH AIA/E/2516 EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 0060. NON-ROUTINE TASK CARD NUMBER 95033.
- [SDR CKSA97156](https://openairdocs.org/sdr/CKSA97156.md): Skin · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION NR 3 TC DOOR OUTER SKIN SEVERAL AREAS. REPAIRED TC DOOR PER ENGINEERING DRAWING NUMBER 25128090, AIA SKETCH AIA/E/2512 EA 97-012. C-1 CHECK INSPECTION WORK CARD NUMBER 3005. NON-ROUTINE TASK CARD NUMBER 9
- [SDR CKSA97155](https://openairdocs.org/sdr/CKSA97155.md): Skin · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION NR 4 TC DOOR OUTER SKIN SEVERAL AREAS. REPAIRED TC DOOR PER ENGINEERING DRAWING NUMBER 25128090, AIA SKETCH AIA/E/2512 EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 3005. NON-ROUTINE TASK NUMBER 92242.
- [SDR CKSA97154](https://openairdocs.org/sdr/CKSA97154.md): Cusp · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 879 TO 800 RIGHT CUSP. REMOVED AND REPLACED RIGHT CUSP AND REPAIRED IAW DC8 SRM 51-1-0 AND AIA SKETCH AIA/E/2502 DATED 1-22-97 EA 97-013. CORROSION TASK CARD NUMBER 5700-0552. NON-ROUTINE TASK CARD NU
- [SDR CKSA97153](https://openairdocs.org/sdr/CKSA97153.md): Shear Web · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 879 RBL 60 SHEAR WEB. REMOVED AND REPLACED FS 879 RBL 60 SHEAR WEB IAW DC8 SRM 51-1-0 AND 51-1-21, 51-1-21D AND AIA SKETCH AIA/E/2502 EA 97-013. CORROSION TASK CARD NUMBER 5700-0552. NON-ROUTINE TASK
- [SDR CKSA97152](https://openairdocs.org/sdr/CKSA97152.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 879 RBL 60 ON LOWER LEG OF FLOORBEAM. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND REPAIRED IAW AIA SKETCH AIA/E/2502 EA 97-013. CORROSION TASK CARD NUMBER 5700-0552. NON-ROUTIN
- [SDR CKSA97151](https://openairdocs.org/sdr/CKSA97151.md): Angle · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 980 LONGERON 34-35RT LOWER ANGLE. REPAIRED ANGLE IAW AIA/E/2510 AND DC8 SRM 51-1-20D AND EA 97-013. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUTINE TASK CARD NUMBER 93051.
- [SDR CKSA97150](https://openairdocs.org/sdr/CKSA97150.md): Rib · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Wing, Rib/Bulkhead
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT HAND WING TRAILING EDGE (FLAPWELL) HAS A CRACKED RIB FRAME AT XRS303. REPAIRED FRAME AT XRS303 TRAILING EDGE RIGHT HAND WING AS PER AIA SKETCH AIA/E/2501 EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 2002. NON-ROU
- [SDR CKSA97149](https://openairdocs.org/sdr/CKSA97149.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 879 RBL 60 FLOORBEAM CORRODED. REMOVED CORROSION OUT OF LIMITS IAW 53-2-0. INSTALLED REPAIR DOUBLER IAW AIA SKETCH AIA/E/2495 REV A EA 97-013. CORROSION TASK CARD NUMBER 5700-0552. NON-ROUTINE TASK C
- [SDR CKSA97148](https://openairdocs.org/sdr/CKSA97148.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 834 LBL 50 ON FLOORBEAM FORWARD SIDE. REPAIRED IAW AIA SKETCH AIA/E/2493 EA 97-013. CORROSION TASK CARD NUMBER 5700-0553. NON-ROUTINE TASK CARD NUMBER 93632.
- [SDR CKSA97147](https://openairdocs.org/sdr/CKSA97147.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 834 LBL 45 FLOORBEAM CORRODED. REPAIRED FLOORBEAM IAW AIA SKETCH AIA/E/2493 EA 97-013. CORROSION TASK CARD NUMBER 5700-0553. NON-ROUTINE TASK CARD NUMBER 93578.
- [SDR CKSA97146](https://openairdocs.org/sdr/CKSA97146.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 798 LBL 45 AND 50 ON FLOORBEAM AFT SIDE. REPAIRED FLOORBEAM IAW AIA SKETCH AIA/E/2493 EA 97-013. CORROSION TASK CARD NUMBER 5700-0553. NON-ROUTINE TASK CARD NUMBER 93633.
- [SDR CKSA97145](https://openairdocs.org/sdr/CKSA97145.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 759 LBL 25 AT SEAT TRACK BOLTS. REPAIRED FLOORBEAM IAW AIA SKETCH AIA/E/2492 EA 97-013. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE TASK CARD NUMBER 93335.
- [SDR CKSA97144](https://openairdocs.org/sdr/CKSA97144.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 742 LBL 25 AT SEAT TRACK. REPAIRED FLOORBEAM IAW AIA SKETCH AIA/E/2492 EA 97-013. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE TASK CARD NUMBER 93336.
- [SDR CKSA97143](https://openairdocs.org/sdr/CKSA97143.md): Floorbeam · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Floor Beam
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 702 LBL 25 AT SEAT TRACK BOLTS ON FLOORBEAM. REPAIRED FLOORBEAM AS PER AIA SKETCH AIA/E/2492 EA 97-013. REMOVED AND REPLACED SPLICE PLATE AS PER SRM 53-2-0. CORROSION TASK CARD NUMBER 2000-0551. NON-
- [SDR CKSA97142](https://openairdocs.org/sdr/CKSA97142.md): A Frame · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Ailerons
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT HAND AILERON A-FRAME IS CRACKED (3RD A FRAME FROM INBOARD). INSTALLED REPAIR PER AIA SKETCH AIA/E/2481 EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 2003. NON-ROUTINE TASK CARD NUMBER 92981.
- [SDR CKSA97141](https://openairdocs.org/sdr/CKSA97141.md): Seat Track · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 834 RBL 45 SEAT TRACK. REMOVED SEAT TRACK, FOUND FLOORBEAM CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW 53-2-0. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2483 REV A. REMOVED AND REPLACED SEAT TRA
- [SDR CKSA97140](https://openairdocs.org/sdr/CKSA97140.md): Skin · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Wing, Plate/Skin
  > DURING CPCP CHECK INSPECTION, FOUND RIGHT HAND LOWER WING AT CENTER SPAR XRS74.849 WING SURFACE IS CRACKED. REPAIRED CRACK XRS 74.849 RIGHT HAND LOWER WING IAW AIA SKETCH AIA/E/2470 EA 97-013. CORROSION TASK CARD NUMBER 123R-0551. NON-ROUTINE TASK CARD NUMB
- [SDR CKSA97139](https://openairdocs.org/sdr/CKSA97139.md): Angle · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON OUTBOARD UPPER SPAR CAP CRACKED APPROXIMATELY STA YOP223 VIEWED THROUGH PANEL 110. REMOVED AND INSTALLED NEW ANGLE AND HARDWARE PER SRM 51-1-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551. NON-ROUTINE TAS
- [SDR CKSA97138](https://openairdocs.org/sdr/CKSA97138.md): Frame · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Frame
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION. FS 1260 LEFT HAND CUSP AND FRAME CORRODED RIVET HEAD BLOWED OFF. CUT OUT AREA WITH EXFOLIATION CORROSION. REMOVED CORROSION ON AREA WITH MINOR CORROSION IAW DC8 SRM 51-1-8 ALODINED AND PRIMER. INSTALLE
- [SDR CKSA97137](https://openairdocs.org/sdr/CKSA97137.md): Angle · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION FS 1616 LEFT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CORRODED. REPAIRED IAW SKETCH AIA/E/2528 EA 97-017 B. C-1 CHECK INSPECTION WORK CARD NUMBER 3011. NON-ROUTINE TASK CARD NUMBER 95592.
- [SDR CKSA97136](https://openairdocs.org/sdr/CKSA97136.md): Longeron · corroded · Mar 24, 1997 · N809CK · Doug DC855 · Fuselage Main, Longeron/Stringer
  > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, REMOVED LEFT HAND LONGERON 24. REMOVED AND REPLACED LONGERON 24 IAW SRM 51-1-0 DOUGLAS PROCEDURE'S 51-1-20D HI LOC INSTALLATION 51-3-0 AND 51-3-1. INSTALLATION OF BOLT AND TORQUEING SHIMMED ALL AREAS IAW
- [SDR CKSA97135](https://openairdocs.org/sdr/CKSA97135.md): Web · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING C-2 CHECK INSPECTION, FOUND NR 4 PYLON STA YOP244 OUTBOARD SIDE WEB HAS A 3 INCH CRACK. STOP DRILLED CRACK, INSTALLED REPAIR IAW AIA SKETCH AIA/E/2522, SRM 51-1-82, SRM 51-1-20D, EA 97-017.B. C-1 CHECK INSPECTION WORK CARD NUMBER 2007. NON-ROUTINE TA
- [SDR CKSA97134](https://openairdocs.org/sdr/CKSA97134.md): Stiffener · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Wing Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT HAND WING FRONT SPAR HAS A STIFFENER BRACKET CRACKED (AT BOTTOM) AT XFS522 INBOARD NR 4 ENGINE. REMOVED AND REPLACED RIGHT HAND WING FRONT SPAR STIFFENER AT XFS522 INBOARD NR 4 ENGINE IAW DC8 SRM 51-1-0 AND 51-1-20D.
- [SDR CKSA97133](https://openairdocs.org/sdr/CKSA97133.md): Doubler · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON DOOR 412 CUTOUT CRACKED INNER AND OUTER DOUBLER STA YOP208 UPPER SPAR AREA, NR 4 PYLON UPPER OUTBOARD SPAR CAP CRACKED STA YOP206, NR 4 PYLON UPPER OUTBOARD SPAR CAP CRACKED STA YOP224. INSTALLED REPAIR DOUBLER N
- [SDR CKSA97132](https://openairdocs.org/sdr/CKSA97132.md): Spar Cap · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON UPPER INBOARD SPAR CAP CRACKED PAST STOP DRILL AT UPPER AND APPROXIMATELY STA YOP254. INSTALLED REPAIR ON UPPER SPAR CAP IAW DC8 SRM 54-2-1 FIGURE 5. INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. CORROSION TASK CARD
- [SDR CKSA97131](https://openairdocs.org/sdr/CKSA97131.md): Bracket · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND BRACKET INBOARD SIDE OF NR 1 PYLON AT SLOT ATTACH AREA CRACKED. INSTALLED BRACKET INBOARD SIDE NR 1 PYLON, SLOT ATTACH AREA, IAW DC8 SRM 51-1-0, INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551
- [SDR CKSA97130](https://openairdocs.org/sdr/CKSA97130.md): Attach Plate · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON CAP ATTACH PLATE INBOARD SIDE CRACKED TWO PLACES APPROXIMATELY STA YOP270. REMOVED AND REPLACED ATTACH PLATE INBOARD SIDE AS PER SRM 51-1-0. INSTALLED FASTENERS IAW SRM 51-1-20D AND 51-1-21. CORROSION TASK CARD
- [SDR CKSA97129](https://openairdocs.org/sdr/CKSA97129.md): Angle · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON CAP SUPPORT RIB OUTBOARD ATTACH ANGLE CRACKED APPROXIMATELY STA YOP212. REMOVED AND REPLACED OUTBOARD SUPPORT RIB AS PER SRM 51-1-0. INSTALLED FASTENERS IAW SRM 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551. N
- [SDR CKSA97128](https://openairdocs.org/sdr/CKSA97128.md): Skin · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON CRACKED PYLON STUB WING LOWER SKIN DOUBLER AT XFS552.00 AND XFS454.00. REMOVED AND INSTALLED SKIN DOUBLER XFS552.00 AND XFS454.00 IAW DC8 SRM 51-1-0 AND INSTALLED HARDWARE IAW DC8 51-1-20D. C-1 CHECK INSPECTION W
- [SDR CKSA97127](https://openairdocs.org/sdr/CKSA97127.md): Skin · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND CRACKED PYLON STUB WING LOWER SKIN AT XFS552 AND XFS542 NR 1 PYLON. REMOVED AND INSTALLED SKIN DOUBLER IAW SRM 51-1-0 AND INSTALLED FASTENERS AS PER DC8 SRM 51-1-20D AND 51-1-21. C-1 CHECK INSPECTION WORK CARD NUMBER 1007.
- [SDR CKSA97126](https://openairdocs.org/sdr/CKSA97126.md): Bracket · cracked · Mar 24, 1997 · N809CK · Doug DC855 · Nacelle/Pylon Structure
  > DURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON CRACKED PYLON BRACKET AT XFS542.50 AT FORWARD AND AFT END ALONG BENDS (2 EACH CRACKS APPROXIMATELY 1.0 INCHES AT AFT END AND 1 EACH CRACK APPROXIMATELY 2 INCHES FORWARD). REMOVED AND REPLACED PYLON BRACKET AT STA

Next page: https://openairdocs.org/model/douglas-dc-8-55/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 = 'DC855'
ORDER BY difficulty_date DESC
```

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

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.