# Service difficulty reports: N102CK, cancelled Nov 2, 2004 A list on [N102CK, cancelled Nov 2, 2004](https://openairdocs.org/deregistered/N102CK-2004-11-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR K4HA99105](https://openairdocs.org/sdr/K4HA99105.md): Engine · vibration · Jan 28, 2000 · N102CK · Lkheed 1011385115 · Engine (Turbine/Turboprop) > RME - FLT 15019 - DURING 2 ENGINE FERRY (NR 2 ENGINE WINDMILLING/INOPERATIVE DUE HIGH VIB AT TAKEOFF POWER). NR 2 ENGINE STARTED TO PROVIDE ADDITIONAL AIR FOR LANDING GEAR EXTENSION. AFTER ENGINE WAS STARTED, CREW REPORTED SMOKE IN CABIN. CORRECTIVE ACTION - [SDR CKSA9970](https://openairdocs.org/sdr/CKSA9970.md): Floorbeam · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 12INCHES AT ZONE 100, STA 709, RBL 68 TO RBL 80. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 53-21-00, - [SDR CKSA99069](https://openairdocs.org/sdr/CKSA99069.md): Floorbeam · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED STA 1443, C-2 CARGO COMPT. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-21-00 FIG 802, INSTALLED AS PER SRM 51-40-01. REPAIR CARRIED OUT IAW SRM - [SDR CKSA99068](https://openairdocs.org/sdr/CKSA99068.md): Floorbeam · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED AT ZONE 100, STA 689, RBL 60 TO RBL 77. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-21-02. REPAIR CARRIED OUT IAW SRM 53-21-00, FLOORBEAM REPAIR - [SDR CKSA99067](https://openairdocs.org/sdr/CKSA99067.md): Floorbeam · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 23 INCHES LONG AT ZONE 100, STA 789, LBL 34.5 TO LBL 46.5. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-50-02. REPAIR CARRIED OUT IAW SRM - [SDR CKSA99066](https://openairdocs.org/sdr/CKSA99066.md): Stringer · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 865 TO STA 883. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. FABRICATED AND TREATED REPAIR PARTS IAW L1011 SRM 51-21-02. REPAIR CARR - [SDR CKSA99065](https://openairdocs.org/sdr/CKSA99065.md): Skin · disbonded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND SKIN CORRODED AT ZONE 120, STA 709, STR 32 TO 33. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 825, DETAIL A VEIW B (REF NON ROU - [SDR CKSA99064](https://openairdocs.org/sdr/CKSA99064.md): Floorbeam · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 2.5 INCHES LONG AT ZONE 100, STA 769, RBL 57 TO RBL 59. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 53- - [SDR CKSA99063](https://openairdocs.org/sdr/CKSA99063.md): Doubler · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 2.5 INCHES LONG AT ZONE 100, STA 729, RBL 70.5 TO RBL 73. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 5 - [SDR CKSA99062](https://openairdocs.org/sdr/CKSA99062.md): Bulkhead Fitting · cracked · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Bulkhead > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND AFT PRESSURE BLKHD TO FUSELAGE ATTACHMENT FITTING CRACKED AT STA 1792, WL 329, RBL.20. REMOVED CRACKED FITTING IAW SRM 53-40-01. REPAIR CARRIED OUT IAW SRM 53-21-02. INSTALLED RE - [SDR CKSA99061](https://openairdocs.org/sdr/CKSA99061.md): Skin · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND SKIN CORRODED AT ZONE 160, STA 1792, STR 36 TO 37. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. SEALED AND INSTALLED REPAI - [SDR CKSA99060](https://openairdocs.org/sdr/CKSA99060.md): Longeron · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND LONGERON CORRODED AT ZONE 110, STA 270. DETERMINED TO BE OUT OF LIMITS IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-50-02 AND 51-40-01/02. FOUND AT GAMCO MAINTENANCE FACILITY ( - [SDR CKSA99059](https://openairdocs.org/sdr/CKSA99059.md): Stringer · corroded · May 24, 1999 · N102CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer > DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 649 TO STA 749. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. FOUND AT GAMCO MAINTENANCE - [SDR CKSA98745](https://openairdocs.org/sdr/CKSA98745.md): Coalescer Bags · dirty · Dec 11, 1998 · N102CK · Lkheed 1011385115 · Humidity Control System > THE CREW NOTICED DE-ICING FLUID SMELL FROM COCKPIT AIR VENTS AND DUCTS. REMOVED AND CLEANED ALL COALESCER BAGS ON NR 1, 2, 3 PACKS IAW MM 21-51-22. OPS AND LEAK CHECK GOOD. - [SDR CKSA98353](https://openairdocs.org/sdr/CKSA98353.md): Clamp · loose · Jun 27, 1998 · N102CK · Lkheed 1011385115 · Pneumatic Distribution System > AFTER TAKEOFF, NR 3 ENGINE FIRE DET LOOP B ILLUMINATED, SWITCHED TO A LOOP AND FULL FIRE WARNING EXPERIENCED. WHEN PULLING THROTTLE BACK ALL INDICATIONS EXTINGUISHED. FHB EMERGENCY PROCEDURES C/W, ENGINE SHUTDOWN. FOUND NR 3 ENGINE HIGH PRESSURE VALVE CLAMP - [SDR CKSA97544](https://openairdocs.org/sdr/CKSA97544.md): Support · corroded · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure > DURING ROUTINE C-CHECK INSPECTION, FOUND FLOOR SUPPORT AFT OF FS 609 RBL 51 FOUND TO BE OUT OF LIMITS AFTER REMOVAL OF CORROSION. REPAIRED FLOOR SUPPORT AFT OF FS 609 RBL 51 IAW AIA/E/2630 AND EA L1-53-007, 8110-3 REV ORIG, SEPT 08, 1997. C-CHECK WORK CARD N - [SDR CKSA97543](https://openairdocs.org/sdr/CKSA97543.md): Skin · corroded · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, FOUND R-3 DOOR LOWER SILL GUARD HAS LARGE BULGE. REMOVED SILL GUARD IAW L1011 SRM 51-40-01. FURTHER INSPECTION FOUND CORROSION ON SKIN SURFACE. REMOVED CORROSION IAW L1011 SRM 51-20-01. FOUND AREA TO BE OUT OF LIMITS IAW - [SDR CKSA97542](https://openairdocs.org/sdr/CKSA97542.md): Floorbeam · corroded · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Floor Beam > DURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION ON LOWER SURFACE OF UPPER CARGO COMP, FLOORBEAM FS 1665. REMOVED CORROSION IAW L1011 SRM 51-21-01, FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM FS 1665 LWR FLANGE IAW L1011 SRM 53-21-00 FIG 804. C-CHECK WO - [SDR CKSA97541](https://openairdocs.org/sdr/CKSA97541.md): Skin · punctured · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, FOUND COCKPIT ESCAPE HATCH FUSELAGE STRUCTURE HAS HOLE DRILLED THROUGH SKIN, AFT RT HAND CORNER. REPAIRED COCKPIT ESCAPE HATCH FUSELAGE STRUCTURE AFT RT CORNER IAW AIA/E/2620 AND EA L1-53-004, 8110-3 REV ORIG, SEPT 06, 1997. - [SDR CKSA97540](https://openairdocs.org/sdr/CKSA97540.md): Skin · punctured · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, FOUND COCKPIT ESCAPE HATCH FUSELAGE STRUCTURE HAS A HOLE DRILLED THROUGH SKIN AND SKIN BROKEN OUT, FWD LEFT HAND CORNER. REPAIRED COCKPIT ESCAPE HATCH FUSELAGE STRUCTURE FWD LT CORNER IAW AIA/E/2621, AND EA L1-53-005 REV ORI - [SDR CKSA97539](https://openairdocs.org/sdr/CKSA97539.md): Bulkhead Frame · corroded · Sep 21, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Bulkhead > DURING ROUTINE C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD FWD SIDE FROM L24RH TO L12L HAS AREAS OF SPOT CORROSION LOWER SIDE. REMOVED CORRODED FRAME SECTION IAW L1011 SRM 51-21-01. REPAIRED IAW LOCKHEED L1011 SRM 53-11-0 FIG 848. FRAME REPAIR AT S25 AN - [SDR CKSA97316](https://openairdocs.org/sdr/CKSA97316.md): Fire Light · illuminated · Jul 5, 1997 · N102CK · Lkheed 1011385115 · Fire Detection > NR 1 ENGINE B-FIRE DETECTOR LOOP LIGHT ILLUMINATED STEADY IN FLIGHT. A-LOOP TESTED GOOD. SELECTED A-LOOP AND CONTINUED OK, 26-71-10-01. - [SDR CKSA97201](https://openairdocs.org/sdr/CKSA97201.md): Uplock Sensor · out of adjust · May 14, 1997 · N102CK · Lkheed 1011385115 · Landing Gear Position and Warning > WHILE IN CRUISE, FLIGHT GEAR LEVER IN NEUTRAL DOOR LIGHT AND IN TRANSIT LIGHT ILLUMINATED. WHEN LEVER MOVED TO UP LIGHTS EXTINGUISHED FIRM NR 32-12-01-00. NOTE: LEFT GEAR ON DOOR LIGHT ANNUNCIATOR ON FLIGHT ENGINEER'S PANEL ILLUMINATED. ADJUSTED DOOR UPLOCK - [SDR CKSA97191](https://openairdocs.org/sdr/CKSA97191.md): Fitting · cracked · May 8, 1997 · N102CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure > DURING CPCP CHECK INSPECTION, FOUND MESC STA 983 STRINGER 31R STRINGER SPLICE CRACKED AT FASTENER HOLES. REMOVED CRACKED END FITTING, INSTALLED NEW FITTING IAW SRM 51-10-01 AND 51-40-01. CORROSION TASK CARD NUMBER C-53-130-06-00. NON-ROUTINE TASK CARD NUMBE - [SDR CKSA97190](https://openairdocs.org/sdr/CKSA97190.md): Doubler · corroded · May 8, 1997 · N102CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION MESC STA 967 BETWEEN STRINGER 32 AND 33 SKIN AT AND AROUND SHEAR-STRAP HAS CORROSION. CUT OUT CORRODED AREA, INSTALLED REPAIR IAW SRM 53-31-00 FIGURE 827 REV DEC 15, 1989. CORROSION TASK CARD NUMBER C-53- - [SDR CKSA97189](https://openairdocs.org/sdr/CKSA97189.md): Stringer · corroded · May 8, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION MESC STA 963 TO STA 983 STRINGER 32R HAS CORROSION ON LOWER LEG. REMOVED CORRODED STRINGER FROM FS 983 TO FS 953 EXISTING SPLICE. INSTALLED NEW STRINGER 32R IAW SRM 51-10-1, 51-40-01. CORROSION TASK CARD - [SDR CKSA97188](https://openairdocs.org/sdr/CKSA97188.md): Doubler · corroded · May 8, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION MESC STA 970 STRINGER 31R SKIN HAS CORROSION UNDER SHEAR STRAP. CUT OUT CORRODED SKIN, INSTALLED REPAIR IAW SRM 53-31-00 FIGURE 827 REV DEC 15, 1989. CORROSION TASK CARD NUMBER C-53-130-06-00. NON-ROUTIN - [SDR CKSA97187](https://openairdocs.org/sdr/CKSA97187.md): Frame · corroded · May 8, 1997 · N102CK · Lkheed 1011385115 · Fuselage Main, Frame > DURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION MESC STA983: BOTH SIDES OF STRINGER 31R HAS CORROSION ON FRAME LOWER LEG. INSTALLED REPAIR IAW EA 97-126 DRAWING NUMBER AIA/E/2561. CORROSION TASK CARD NUMBER C-53-130-06-00. NON ROUTINE TASK CARD NUMBER - [SDR CKSA95164](https://openairdocs.org/sdr/CKSA95164.md): Indication · malfunctioned · Dec 18, 1995 · N102CK · Lkheed 1011385115 · Trailing Flap Position Indicating System > KSEA/KBYH - FLT 70083 - AFTER TAKEOFF ON FLAP RETRACT, 'FLAP/SLAT' LIGHT ON F/E ANNUNCIATOR PANEL ILLUMINATED AND SLATS REMAINED FULL EXTENDED. FLAPS CAME UP NORMAL. SLAT MONITOR SHOWED SLAT FULL 30 DEGREES AND 14 DEGREES GREEN. FORM 27-28-23-00. RESET SLA - [SDR CKSA95143](https://openairdocs.org/sdr/CKSA95143.md): Control Unit · malfunctioned · Dec 7, 1995 · N102CK · Lkheed 1011385115 · Fire Detection > KHUF - FLT 69407 - ON TOP OF DESCENT 'A' FIRE DETECTOR LOOP ILLUMINATED, 'B' WOULD NOT TEST. SECURED NR 2 ENGINE IAW SHUT DOWN PROCEDURES. RESET FAULT ISOLATION CONTROL UNIT TO BOTH POSITIONS. SYSTEM TESTS GOOD. (X) ## 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 = 'N102CK' AND deregistration_id = 'N102CK-2004-11-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N102CK-2004-11-02/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.