# Service difficulty reports: N801CK, cancelled Feb 27, 2013 A list on [N801CK, cancelled Feb 27, 2013](https://openairdocs.org/deregistered/N801CK-2013-02-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 98ZZZX2026](https://openairdocs.org/sdr/98ZZZX2026.md): Diaphragm · torn · May 13, 1998 · N801CK · Doug DC8F55 · Hydraulic Accumulator, Auxiliary > AUXILIARY HYDRAULIC POWER SURGE DAMPER ACCUMULATOR TANK HAD NEW DIAPHRAGM INSTALLED AT REPAIR. DIAPHRAGM FAILED (TORN) AFTER 3 MONTHS TIME IN SERVICE. DIAPHRAGM MANUFACTURED BY KAPCO. THIS IS THE 5TH IDENTIFIED FAILURE BY THIS REPAIR STATION. - [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 CKSA97074](https://openairdocs.org/sdr/CKSA97074.md): Oil Cooler · failed · Mar 18, 1997 · N801CK · Doug DC855 · Engine Oil Cooler > ON CLIMBOUT, NR 1 ENGINE OIL TEMPERATURE RAPIDLY ROSE TO 150 DEGREES CELSIUS. PERFORMED ENGINE SHUTDOWN AT 1940Z. OIL PRESSURE DROPPED TO ZERO WITH WINDMILLING N2 AT 36 PERCENT AND N1 AT 18 PERCENT UNTIL 2012Z. NOTE: DUMPED 45,000 POUNDS OF FUEL. DUMPING S - [SDR CKSA96158](https://openairdocs.org/sdr/CKSA96158.md): Air Distr · odor · Sep 29, 1996 · N801CK · Doug DC855 · Air Distribution System > NASI SYSTEM PLACES NAUSEATING ODOR INTO AIRCRAFT, OILY SMELL AND TASTE. TROUBLESHOT SYSTEM, PERFORMED OPS CHECK OF NASI FLOW CONTROL SYSTEM AND NO DISCREPANCIES NOTED. OPS GOOD IAW NASI OPERATIONS MANUAL 21-7-0 PAGE 1. - [SDR CKSA96073](https://openairdocs.org/sdr/CKSA96073.md): Bleed Air · odor · Jul 11, 1996 · N801CK · Doug DC855 · Compressor Bleed Control > OPERATING ALL 4 BLEEDS ON CLIMBOUT DETECTED AN ODOR. EYES BURNED COULD TASTE OILY SUBSTANCE IN MOUTH. PROBLEM REDUCED WITH NR 2 BLEED TURNED OFF. PERFORMED ENGINE RUN AND OPS CHECK AND ALL ENGINE BLEEDS NOTICED ODOR ONLY WITH NR 2 BLEED ON, CLOSED NR 2 BLEE - [SDR CKSA96055R1](https://openairdocs.org/sdr/CKSA96055R1.md): Doubler · corroded · Jun 3, 1996 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > DURING B-D CHECK INSPECTION, FOUND CARD NR 4640-0551 AREA, FLT COMPARTMENT MID AREA FS 220 LEFT OUTBOARD FINGER DOUBLER, HAS CORROSION, LEVEL 2 TASK NR 76881. REPAIRED IAW SKETCH, AIA/E/2316 DATED 5/14/96 AS REQUIRED. (M) - [SDR CKSA95160](https://openairdocs.org/sdr/CKSA95160.md): Spar Cap · corroded · Dec 17, 1995 · N801CK · Doug DC855 · Wing Spar > DURING C-CHECK INSPECTION, FOUND OUTBOARD FLAP TOP SPAR CAP AT STATION 410 CORRODED. REPAIRED SPAR CAP IAW DC-8 SRM 57-2-0 FIGURE 2. ALODINED AND PRIMED IAW DC-8 SRM 51-1-21. INSTALLED HI-LOCKS IAW DC-8 SRM 51-1-20. REPAIRED LOWER FLAP SKIN IAW DRAWING SKA - [SDR CKSA95159](https://openairdocs.org/sdr/CKSA95159.md): Longeron · corrosion · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Main, Longeron/Stringer > KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT LONGERON 24 AT AFT END CORROSION EXCEEDS 20 PERCENT MATERIAL THICKNESS, APPROXIMATE 2 INCH CRACK COMING OUT OF CORRODED AREA ON HORIZONTAL WEB FORWARD AND AFT DIRECTION. REPAIRED RIGHT LONGERON 24 IAW DC-8 SRM 53- - [SDR CKSA95158](https://openairdocs.org/sdr/CKSA95158.md): Spar Cap · crack · Dec 17, 1995 · N801CK · Doug DC855 · Wing Spar > KOSC - DURING C-CHECK INSPECTION, FOUND LEADING EDGE STATION XFS 86 (APPROX) TOP SPAR CAP CRACKED AND CORRODED. INSTALLED REPAIR AS IT REQUIRED IAW AIA/E2119 AND DC-8 SRM 51-1-20D. (M) - [SDR CKSA95157](https://openairdocs.org/sdr/CKSA95157.md): Blkhd Angle · corroded · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Main, Bulkhead > KOSC - DURING C-CHECK INSPECTION, FOUND APB LEFT SIDE FLOOR TO BULKHEAD ANGLE CORRODED. REMOVED AND INSTALLED NEW ANGLE AS IT REQUIRED AS PER IAW DC-8 SRM 53-2-0. (M) - [SDR CKSA95156](https://openairdocs.org/sdr/CKSA95156.md): Panel · cracked · Dec 17, 1995 · N801CK · Doug DC855 · Horizontal Stabilizer, Plate/Skin > KOSC - DURING C-CHECK INSPECTION, FOUND REF R/O 801-363 CRACK INDICATION HORIZONTAL STABILIZER CONSTANT SECTION UPPER FORWARD PANEL RIGHT SIDE BOLT HOLE NR 4 TO NEXT HOLE FORWARD TO FORWARD END OF PANEL. REMOVED AND REPLACED FORWARD UPPER PANEL IAW REFERENCE - [SDR CKSA95155](https://openairdocs.org/sdr/CKSA95155.md): Longeron · cracked · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Main, Longeron/Stringer > KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT WHEEL WELL LONGERON 24 CRACKED AT FORWARD VERTICAL FITTING STATION 879.325. REPAIRED RIGHT WHEEL WELL LONGERON 24 IAW DC-8 SRM 53-2-2 FIGURE 9, SHEET 1 AND 53-2-2 FIGURE 9, SHEET 2. (M) - [SDR CKSA95154](https://openairdocs.org/sdr/CKSA95154.md): Longeron · cracked · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Main, Longeron/Stringer > KOSC - DURING C-CHECK INSPECTION, FOUND LEFT LONGERON 24 CRACKED IN FORWARD BOLT CUTOUT. REPAIRED CRACK PER DC-8 SRM 53-2-2 FIGURE 6, SHEET 1. INSTALLED HI-LOCK FASTENERS PER 51-1-20D. (M) - [SDR CKSA95153](https://openairdocs.org/sdr/CKSA95153.md): Fitting · cracked · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KOSC - DURING C-CHECK INSPECTION, FOUND AFT PIT STATION 1320 CABIN FLOOR SUPPORT AT CENTER SEAT TRACK CRACKED. REMOVED AND INSTALLED NEW FLOOR SUPPORT FITTING AS REQUIRED AS PER 53-2-0. (M) - [SDR CKSA95152](https://openairdocs.org/sdr/CKSA95152.md): Flange · corroded · Dec 17, 1995 · N801CK · Doug DC855 · Wing Miscellaneous Structure > KOSC - DURING C-CHECK INSPECTION, FOUND UPPER TRAILING EDGE PANEL PULLING LOOSE AND POPPED RIVETS JUST OUTBOARD OF MAIN LANDING GEAR TRUNNION. FOUND LOWER FLANGE CORRODED BEYOND LIMITS. INSTALLED NEW FLANGE IAW DC-8 SRM 57-2-0. ALODINED AND PRIMED IAW DC-8 - [SDR CKSA95151](https://openairdocs.org/sdr/CKSA95151.md): Angle · corroded · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KOSC - DURING C-CHECK INSPECTION, FOUND LEFT WHEEL WELL DOGHOUSE FORWARD LOWER CORRODED. REMOVED ANGLE AND INSTALLED NEW ANGLE PER 51-1-20D. (M) - [SDR CKSA95150](https://openairdocs.org/sdr/CKSA95150.md): Angle · corroded · Dec 17, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT WHEEL WELL DOGHOUSE FORWARD LOWER CORRODED. REMOVED AND REPLACED LOWER ANGLE, INSTALLED FASTENERS IAW 51-1-20D. (M) - [SDR CKSA95149](https://openairdocs.org/sdr/CKSA95149.md): Panel · corrosion · Dec 17, 1995 · N801CK · Doug DC855 · Leading Edge Devices > KOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT INBOARD PANEL CORRODED AT LEADING EDGE. INSTALLED NEW OUTBOARD SLOT INBOARD PANEL IAW DC-8 SRM 57-2-0, 51-3-0 AND MM 27-41-2. (M) - [SDR CKSA95148](https://openairdocs.org/sdr/CKSA95148.md): Panel · corrosion · Dec 17, 1995 · N801CK · Doug DC855 · Leading Edge Devices > KOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT OUTBOARD PANEL 1 SPOT CORROSION, 1 SCREW MISSING. INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND MM 27-41-2. (M) - [SDR CKSA95057](https://openairdocs.org/sdr/CKSA95057.md): Fitting · cracked · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 28 RIGHT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) - [SDR CKSA95056](https://openairdocs.org/sdr/CKSA95056.md): Fitting · cracked · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 32 RIGHT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) - [SDR CKSA95055](https://openairdocs.org/sdr/CKSA95055.md): Fitting · cracked · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 34 RIGHT END, FITTING CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) - [SDR CKSA95054](https://openairdocs.org/sdr/CKSA95054.md): Fitting · cracked · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 30 LEFT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) - [SDR CKSA95053](https://openairdocs.org/sdr/CKSA95053.md): Fitting · cracked · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING C-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 34 LEFT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) - [SDR CKSA95052](https://openairdocs.org/sdr/CKSA95052.md): Stiffener · corroded · Jun 15, 1995 · N801CK · Doug DC855 · Fuselage Miscellaneous Structure > KMIA - DURING B-CHECK INSPECTION, FOUND FS 1340 - FS 1360 AT LONGERON 26 LEFT STIFFENER, CORRODED. REPLACED DAMAGED STIFFENER IAW SRM 51-1-0. FASTENERS INSTALLED IAW SRM 51-3-0. (X) - [SDR CKSA95013](https://openairdocs.org/sdr/CKSA95013.md): Defuser Case · cracked · Mar 16, 1995 · N801CK · Doug DC855 · Turbine Engine Combustion Section > MSLP-KMIA - NR 1 ENGINE SHUTDOWN AT 1742Z DUE TO FIRE WARNING. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED NR 1 ENGINE IAW DC-8 MIP-1, CHAPTER 9 DO TO DIFFUSER CASE CRACK. OPS AND LEAKS CHECK GOOD IAW AIA DC-8 MIP-1 CHAPTER 10. (W) ## 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 = 'N801CK' AND deregistration_id = 'N801CK-2013-02-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N801CK-2013-02-27/reports --- 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.