# Service difficulty reports: N815CK, cancelled May 2, 2002

A list on [N815CK, cancelled May 2, 2002](https://openairdocs.org/deregistered/N815CK-2002-05-02.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 68 reports

- [SDR CKSA98493](https://openairdocs.org/sdr/CKSA98493.md): Fire Loop · out of adjust · Jul 30, 1998 · N815CK · Doug DC863F · Fire Detection
  > ENGINE FIRE INDICATION NR 1, BOTTLE NR 1 DISCHARGED, HANDLE LIGHT REMAINED ILLUMINATED, BOTTLE NR 2 DISCHARGED, LIGHT REMAINED ILLUMINATED, ON POST FLIGHT, NO VISABLE INDICATION OF FIRE. REMOVED AND REPLACED NR 1 ENGINE FIRE LOOP AS PER MM 26-10-1 GROUND GOOD
- [SDR CKSA98341](https://openairdocs.org/sdr/CKSA98341.md): Seat Track · damaged · May 13, 1998 · N815CK · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > FOUND TWO SECTIONS OF SEAT TRACK DAMAGED AT STA 380 ON NR 1 AND NR 2 TRACKS AFTER REMOVAL OF CARGO. REPAIRED DAMAGED AREAS OF SEAT TRACK IAW DOUGLAS DC-8 SRM CH 53-2-3. NON-ROUTINE M-7 ITEM 1 LOG PAGE 815-0860.
- [SDR CKSA98301](https://openairdocs.org/sdr/CKSA98301.md): Skin · damaged · Apr 27, 1998 · N815CK · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE B CHECK INSPECTION, FOUND RIVET PULLED FS 70 STRINGER 23R. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLASS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS (INITIAL INSPECTION OF 12,000 LANDINGS) AND REPLACED WITH CLASS I R
- [SDR CKSA98300](https://openairdocs.org/sdr/CKSA98300.md): Skin · cracked · Apr 27, 1998 · N815CK · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE B CHECK INSPECTION, FOUND FS 100 AT STR 33L SKIN HAS CRACK. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLASS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS AND REPLACED WITHIN 24,000 LANDINGS IAW DC8 SRM 53-2-1 PARAGRAPH 16
- [SDR CKSA98299](https://openairdocs.org/sdr/CKSA98299.md): Seat Track · corroded · Apr 27, 1998 · N815CK · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE B CHECK INSPECTION, FOUND SEAT TRACK STA 490 RBL25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER DC-8 SRM 53-02-3. NON ROUTINE TASK CARD NUMBER 23625.
- [SDR CKSA97572](https://openairdocs.org/sdr/CKSA97572.md): Engine · flamed out · Nov 18, 1997 · N815CK · Doug DC863F · Engine (Turbine/Turboprop)
  > AT 4,000 FT NR 4 ENG FLAMEOUT SUCCESSFULLY RESTARTED. ON GROUND DURING TAXI IN ENG WOULD NOT ACCELERATE NORMALLY. FUEL TEMP WAS READING 34 DEGREES. SUSPECT FUEL ICING, ENGINE IDLES AT 55 PERCNET N2. REPLACED NR 4 ENG FUEL PUMP IAW 73-10-2 LEAK CHECKS GOOD
- [SDR CKSA96403](https://openairdocs.org/sdr/CKSA96403.md): Frame · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Frame
  > DURING C-1 CHECK INSPECTION, FOUND LOWER AREA OF FRAME STA 1600 CORRODED FROM LONGERON 35L TO LONGERON 34R. REMOVED CORRODED AREA AND INSTALLED ZEE FRAME REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. INSTALLED FASTENER IAW DC8 SRM 51-1-20D AND 51-1-21 ALODINED AND PRI
- [SDR CKSA96402](https://openairdocs.org/sdr/CKSA96402.md): Seat Track · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-1 CHECK INSPECTION, FOUND FS 980 TO 1140 LONGERON -3RT SEAT TRACK AND MOUNT CORRODED MARKED L-177. REMOVED AND REPLACED SEAT TRACK AND REPAIRED IAW DC8 SRM 53-2-3 FIGURE 14. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. CORROSION CARD NR 5590-0551. NON-
- [SDR CKSA96401](https://openairdocs.org/sdr/CKSA96401.md): Angle · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Wing Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND LOWER WING CENTER SECTION STA 781.5 RBL 64 HAS CRACKED SUPPORT ANGLE MARKED M6. REPLACED SUPPORT ANGLE IAW DC8 SRM 53-2-0. CORROSION CARD NR 2000 TO 0551. NON-ROUTINE TASK CARD NR 90982.
- [SDR CKSA96400](https://openairdocs.org/sdr/CKSA96400.md): Fitting · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FS 1160 LONGERON 31 LT THROUGH LONGERON 32 LT BATHTUB FITTING CORRODED. REMOVED CORROSION, TREATED, PRIMED IAW SRM DC8 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD
- [SDR CKSA96399](https://openairdocs.org/sdr/CKSA96399.md): Fitting · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FS 1230 LONGERON 35R THROUGH LONGERON 36 BATHTUB FITTING CRACKED. INSTALLED FITTING AND INSTALLED HI-LOCK IAW SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90967.
- [SDR CKSA96398](https://openairdocs.org/sdr/CKSA96398.md): Web · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND INNER GRANULAR CORROSION ON FORMER WEB, FORWARD SIDE, BETWEEN STRINGER 32 AND STRINGER 33R AT STA 120 MARKED H36. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. PART FAB
- [SDR CKSA96397](https://openairdocs.org/sdr/CKSA96397.md): Shear Tie · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTIO, FOUND SHEAR TIE AT STA 1700 BETWEEN STRINGER 22L AND STRINGER 23L IS CORRODED. REMOVED CORRODED SHEAR TIE FABRICATED SHEAR TIE IAW SRM 51-1-4. INSTALLED NEW SHEAR TIE IAW SRM 51-1-20D AND SRM 51-1-21. CORROSION CARD NR 5590-0551.
- [SDR CKSA96396](https://openairdocs.org/sdr/CKSA96396.md): Blkhd Stiffener · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Bulkhead
  > DURING C-1 CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD, WEB AND VERTICAL STIFFENER HAS INNER GRANULAR CORROSION AT RBL 22 AT FLOOR LINE. REPAIRED VERTICAL STIFENER IN ACCORDANCE WITH AIA DRAWING AIA/E/2443 AND REPORT NR 96 AIA 197 DATED 12-12-96 EA 96-348.
- [SDR CKSA96395](https://openairdocs.org/sdr/CKSA96395.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND CORROSION AT FS 680 BETWEEN STRINGER 33 AND 32R. CUT OUT CORRODED AREA, INSTALLED REPAIR IAW AIA/E/2430 AND EA 96-348 REPORT 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91681, LEVEL 2.
- [SDR CKSA96394](https://openairdocs.org/sdr/CKSA96394.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LEADING EDGE UPPER SURFACE FROM STA XFS302 TO XFS424 CORROSION EXCEEDED ALLOWABLE LIMITS. REFERENCE M-40 NR 88619. REPAIRED LEFT HAND WING LEADING EDGE UPPER SURFACE IAW AIA/EA SKETCH NR 2418 AND DC-8 SRM REP
- [SDR CKSA96393](https://openairdocs.org/sdr/CKSA96393.md): Longeron · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-1 CHECK INSPECTION, FOUND LONGERON 36 CRACKED AND CORRODED STA 240 TO STA 300. REPAIRED LONGERON 36 AT STA 240 THROUGH STA 300 IAW AIA SKETCH AIA/E/2438 DATED 12-09-96 EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-
- [SDR CKSA96392](https://openairdocs.org/sdr/CKSA96392.md): Shear Tie · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FS 1040 LONGERON 34R THROUGH 35 LT FRAME SHEAR TIES CORRODED BEYOND ALLOWABLE LIMITS. REPAIRED FRAME SHEAR TIES FS 1040 IAW AIA DRAWING NR AIA/E/2431, EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-05
- [SDR CKSA96391](https://openairdocs.org/sdr/CKSA96391.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND UPPER LEFT WING SKIN CORRODED AT XRS 250 AT WING STRINGER NR 7 AND 8. INSTALLED DOUBLER IAW AIA/E/DRAWING 2426 AND EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 117L-0551. NON-ROUTINE TASK CARD NR 91640
- [SDR CKSA96390](https://openairdocs.org/sdr/CKSA96390.md): Fitting · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND LONGERON END FITTING CORRODED STA 1560 LONGERON 33R. REMOVED AND REPLACED LONGERON END FITTING STA 1560 IAW AIA SKETCH NR AIA/E/2432, EA 96-348 REPORT NR 96-AIA 197 DATED 12-12-96. CORROSION CARD NR 5600-0551. NON-ROUTINE
- [SDR CKSA96389](https://openairdocs.org/sdr/CKSA96389.md): Spar Web · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing Spar
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT WING AFT UPPER SPAR WEB CORRODED AT STA XRS -6.0. REMOVED PARTS AND CORROSION IAW DRAWING AIA/E/2424, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 124R-0551. NON-ROUTINE TASK CARD NR 91051, LEVEL 2.
- [SDR CKSA96388](https://openairdocs.org/sdr/CKSA96388.md): Bulkhead · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Bulkhead
  > DURING C-1 CHECK INSPECTION, FOUND FORWARD BULKHEAD STA 8 IS CORRODED BOTH SIDES OF STRINGER TIE AT STRINGER 35R AND STRINGER TIE FITTING ALSO CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2427 EA 96-348 REPOR
- [SDR CKSA96387](https://openairdocs.org/sdr/CKSA96387.md): Angle · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND L-ANGLE AT LONGERON 27L IN A CARGO BIN IS CORRODED BETWEEN STA 280 AND STA 340 MARKED. REMOVED CORROSION, OUT OF LIMITS, INSTALLED REPAIR IAW AIA SKETCH AIA/E/2437 AND EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSIO
- [SDR CKSA96386](https://openairdocs.org/sdr/CKSA96386.md): Web · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FORWARD DOOR TRACK WEB HAS INNER GRANULAR CORROSION ABOVE STRINGER 31 TO 33R. REMOVED CORROSION, FOUND OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2414 DATED 11-21-96 EA 96-348 AND REPORT 96 AIA 197 DATED 12-12-96
- [SDR CKSA96385](https://openairdocs.org/sdr/CKSA96385.md): Frame · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Frame
  > DURING C-1 CHECK INSPECTION, FOUND FS 1000 LONGERON 36 FRAME FORWARD SIDE LOWER LEG CORRODED. REPAIRED FRAME AS PER SKETCH AIA/E/2435, EA 96-348, REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90885, LEVEL 2.
- [SDR CKSA96384](https://openairdocs.org/sdr/CKSA96384.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LEADING EDGE UPPER SURFACE STA XFS100 TO XFS141. CORROSION REMOVAL EXCEEDED LIMITS. REPAIRED LEADING EDGE UPPER SURFACE STA XFS100 TO XFS141 IAW AIA SKETCH AIA/E/2419 REFERENCE M-40 NR 90811. CORROSION CARD
- [SDR CKSA96383](https://openairdocs.org/sdr/CKSA96383.md): Apron · worn · Dec 15, 1996 · N815CK · Doug DC863F · Nacelle/Pylon Structure
  > DURING C-1 CHECK INSPECTION, FOUND COWLING APRON WORN THROUGH ON RIGHT HAND SIDE MARKED. REPAIRED APRON, RIGHT HAND SIDE IAW SKETCH AIA/E/2436, EA 96-348 REPORT NR 96 AIA 197. C-1 CHECK WORK CARD NR 1006. NON-ROUTINE TASK CARD NR 89228.
- [SDR CKSA96382](https://openairdocs.org/sdr/CKSA96382.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Rudder, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND RUDDER 4TH STATIC WICK FROM TOP CORRODED RIGHT SIDE. REPAIRED STATIC WICKS AT ZR293 AND ZR284 IAW AIA DRAWING AIA/E/2434 REV ORIG AND DC-8 SRM 51-1-21, AND 51-1-21A, EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION
- [SDR CKSA96381](https://openairdocs.org/sdr/CKSA96381.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Rudder, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND RUDDER LEFT SIDE SURFACE CORROSION AROUND STATIC WICK AT STA ZR293 AND TRAILING EDGE AT STA ZR284 AND ZR330. REPAIRED STATIC WICKS ON RUDDER LEFT HAND IAW AIA DRAWING AIA/E/2433 AND DC-8 SRM 51-1-21, 51-1-21A AND EA 96-348 R
- [SDR CKSA96380](https://openairdocs.org/sdr/CKSA96380.md): Tip · damaged · Dec 15, 1996 · N815CK · Doug DC863F · Rudder Structure
  > DURING C-1 CHECK INSPECTION, FOUND TOP OF RUDDER TIP HAS HOLE IN IT. REPAIRED HOLE AT THE TOP OF RUDDER TIP IAW AIA DRAWING NR AIA/E/2439 REV ORIG AND DC-8 SRM 51-21-1A, EA 96-348, REPORT 96 AIA-197 DATED 12-12-96. C-1 CHECK WORK CARD NR 4001 1OF1. NON-ROUT
- [SDR CKSA96379](https://openairdocs.org/sdr/CKSA96379.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE CORROSION AT UPPER LEADING EDGE FASTENERS, APPROXIMATELY XFS697 TO XFS 841.5. INSTALLED REPAIR IAW AIA ENGINEERING SKETCH NR 2420, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD
- [SDR CKSA96378](https://openairdocs.org/sdr/CKSA96378.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE FROM XFS 11.25 TO XFS 182.5 HAVE CORROSION AROUND ATTACH FASTENERS AS MARKED. INSTALLED DOUBLER REPAIR IAW AIA SKETCH NR 2425, EA 96-348 REPORT NR 96-197 DATED 12-12-96. CORROSION CARD NR 121R-0552.
- [SDR CKSA96377](https://openairdocs.org/sdr/CKSA96377.md): Web · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FS 1220 TO 1230 TORQUE BOX UPPER WEB CRACKED RIGHT SIDE. REPAIRED TORQUE BOX UPPER WEB IAW AIA SKETCH NR AIA/E/2421/2421815C DRAWING, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TAS
- [SDR CKSA96376](https://openairdocs.org/sdr/CKSA96376.md): Longeron · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-1 CHECK INSPECTION, FOUND LONGERON 24L CORRODED THROUGH SEVERAL AREA'S BETWEEN STA 1610 THROUGH STA 1660. REPAIRED LONGERON 24L BETWEEN STA 1610 THROUGH STA 1660 IAW DC-8 SRM 53-2-2. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91560, LEVE
- [SDR CKSA96375](https://openairdocs.org/sdr/CKSA96375.md): Fitting · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Cargo/Baggage Doors
  > DURING C-1 CHECK INSPECTION, FOUND CARGO DOOR SPOOL BACK-UP FITTINGS CORRODED STA 158 TO 260. REMOVED AND REPLACED BACK-UP FITTINGS IAW DC8 SRM 51-1-21 AND 51-3-1. C-1 CHECK WORK CARD NR 0049. NON-ROUTINE TASK CARD NR 89537, LEVEL 2.
- [SDR CKSA96374](https://openairdocs.org/sdr/CKSA96374.md): Fitting · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-1 CHECK INSPECTION, FOUND RIGHT HAND SKIN STRINGER 29R FITTING CORRODED AT STA 8. REMOVED AND REPLACED STRINGER 29R END FITTING IAW DC-8 SRM 51-1-0. PART FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 8893, L
- [SDR CKSA96373](https://openairdocs.org/sdr/CKSA96373.md): Stringer · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-1 CHECK INSPECTION, FOUND STRINGER TIE FITTING CRACKED AFT SIDE OF PRODUCTION SPLICE AT STA 1690, STRINGER 25R MARKED H52. REMOVED AND REPLACED STRINGER IAW DOUGLAS SRM 51-01-20. PART FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5600-0551. NO
- [SDR CKSA96372](https://openairdocs.org/sdr/CKSA96372.md): Fitting · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND CRACK IN LOWER END OF FITTING STA 320 STRINGER 27L. REMOVED AND REPLACED LOWER END FITTING IAW DC8 SRM 51-1-0 AND 51-1-20D. PARTS FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 89616
- [SDR CKSA96371](https://openairdocs.org/sdr/CKSA96371.md): Fitting · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND CRACK IN LOWER END OF FITTING STA 300 STRINGER 37L. REMOVED AND REPLACED LOWER END FITTING IAW DC-8 SRM 51-1-0 AND 51-1-20D. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 89615.
- [SDR CKSA96370](https://openairdocs.org/sdr/CKSA96370.md): Casting · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND C-PIT CASTING CRACKED STA 1140 LONGERON 35R. REMOVED AND REPLACED CASTING IAW DC-8 SRM 51-1-20D AND 51-1-10, M-59 ATTACHED. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91658.
- [SDR CKSA96369](https://openairdocs.org/sdr/CKSA96369.md): Doubler · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND STA 80 AT STRINGER 22R PRESSURE FLOOR PANEL FINGER DOUBLERS SEPARATING AND FASTENERS SHEARED. REMOVED AND REPLACED FINGER DOUBLERS CLEANED CORROSION AND FOUND TO BE WITHIN LIMITS ON PRESSURE FLOOR PANEL. REPLACED DOUBLER AR
- [SDR CKSA96368](https://openairdocs.org/sdr/CKSA96368.md): Skin · gouged · Dec 15, 1996 · N815CK · Doug DC863F · Trailing Edge Flaps
  > DURING C-1 CHECK INSPECTION, FOUND OUTBOARD FLAP HAS BOLT GOUGE, INBOARD SIDE OF INBOARD ICE BREAKER MARKED H6. REPAIR OUTBOARD FLAP IAW DC8 SRM 57-2-5 FIGURE 1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. C-1 CHECK CARD NR 1008. NON-ROUTINE TASK CARD NR 89573
- [SDR CKSA96367](https://openairdocs.org/sdr/CKSA96367.md): Fitting · cracked · Dec 15, 1996 · N815CK · Doug DC863F · Wing Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND UPPER WING CENTER SECTION STA 759 RBL 57 FRAME SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. CORROSION CARD NR 2000-0551. NON-ROUTINE TASK CARD NR 90922, LEVEL 2.
- [SDR CKSA96366](https://openairdocs.org/sdr/CKSA96366.md): Skin · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing, Plate/Skin
  > DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING UPPER SURFACE STA XRS693 CORROSION LIMIT EXCEEDED, REFERENCE M-40 NBR. 88626. INSTALLED DOUBLER REPAIR IAW AIA ENGINEERING SKETCH NR 2423. CORROSION CARD NR 109L-0551. NON-ROUTINE TASK CARD NR 90769, LEVEL 2
- [SDR CKSA96365](https://openairdocs.org/sdr/CKSA96365.md): Fitting · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND C-BAGGAGE COMPARTMENT FS 1200 LONGERON 34 LT TO LONGERON 35 LT, BATHTUB FITTING CORRODED. REMOVED CORROSION AND TREATED IAW SRM 51-1-8 AND INSTALLED FITTING WITH HI-LOCKS IAW SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-
- [SDR CKSA96364](https://openairdocs.org/sdr/CKSA96364.md): Doubler · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-1 CHECK INSPECTION, FOUND FS 1220 LONGERON 30 TO 31 LT INNER DOUBLER CORRODED. REMOVED CORROSION, OUT OF LIMITS. REPAIRED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0 FIGURE 1F AND 53-2-0 FIGURE 1B. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK
- [SDR CKSA96363](https://openairdocs.org/sdr/CKSA96363.md): Longeron · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-1 CHECK INSPECTION, FOUND FS 1160 TO 1180 LONGERON 32 LT LONGERON CORRODED. REMOVED CORROSION, OUT OF LIMITS, FABRICATED DOUBLER REPAIR AS PER AIA/E/2422. TREATED AND PRIMED IAW SRM 51-1-8 AND INSTALLED REPAIR AS PER SRM 51-1-20D. CORROSION CARD NR
- [SDR CKSA96362](https://openairdocs.org/sdr/CKSA96362.md): Spar · corroded · Dec 15, 1996 · N815CK · Doug DC863F · Wing Spar
  > DURING C-1 CHECK INSPECTION, FOUND LEFT WING UPPER REAR SPAR STA XRS295 HAS SEVERE CORROSION, WITH SEPARATION. REPAIRED IAW SKETCH NR AIA/E/2415. CORROSION CARD NR 117L-0551. NON-ROUTINE TASK CARD NR 88649, LEVEL 2.
- [SDR CKSA96190](https://openairdocs.org/sdr/CKSA96190.md): Duct · blown · Oct 28, 1996 · N815CK · Doug DC863F · Pneumatic Distribution System
  > NR 1 ENGINE FIRE WARNING ON SHORT FINAL. NR 1 BOTTLE DUMPED FIRE DID NOT GO OUT, NR 2 BOTTLE DUMPED FIRE DID NOT GO OUT FOR 3 MINUTES. FIRE WARNING WILL NOT TEST ON NR 1 ENGINE. ENGINE FIRE, SEVERE DAMAGE CHECKLIST WAS ACCOMPLISHED IAW AIA PROCEDURES. FOUN
- [SDR CKSA96026](https://openairdocs.org/sdr/CKSA96026.md): Prox Switch · failed · Mar 10, 1996 · N815CK · Doug DC863F · Landing Gear Position and Warning
  > AFTER TAKEOFF, DOORS NOT LATCHED LIGHT AND GEAR NOT LATCHED LIGHT REMAINED ON BRIGHT. ON LANDING BOTH RED LIGHTS WERE ON AND RIGHT MAIN GEAR LIGHT WAS OUT. REMOVED AND REPLACED LANDING GEAR PROXIMITY SWITCH CONTROL BOX. SYSTEM OPS CHECK GOOD IAW DC-8 MM 32-

Next page: https://openairdocs.org/deregistered/N815CK-2002-05-02/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 n_number = 'N815CK' AND deregistration_id = 'N815CK-2002-05-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N815CK-2002-05-02/reports

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