# Service difficulty reports: N707CK, cancelled Dec 11, 2014

A list on [N707CK, cancelled Dec 11, 2014](https://openairdocs.org/deregistered/N707CK-2014-12-11.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 · 100 reports

- [SDR KCSA101111](https://openairdocs.org/sdr/KCSA101111.md): Light · inoperative · Aug 14, 2010 · N707CK · Boeing 747246F · Emergency Lighting
  > COCKPIT STAIRWELL UPPER DECK AND MAIN DECK EMERGENCY LIGHTS INOP.
- [SDR KCSA101060](https://openairdocs.org/sdr/KCSA101060.md): Light · inoperative · May 18, 2010 · N707CK · Boeing 747246F · Emergency Lighting
  > UPPER DECK EMERGENCY LIGHT ABOVE ESCAPE DOOR IS INOP.
- [SDR KCSA091082](https://openairdocs.org/sdr/KCSA091082.md): Light · inoperative · Aug 12, 2009 · N707CK · Boeing 747246F · Emergency Lighting
  > RIGHT EMERGENCY SLIDE LIGHT INOP.
- [SDR KCSA091081](https://openairdocs.org/sdr/KCSA091081.md): Frame · cracked · Aug 12, 2009 · N707CK · Boeing 747246F · Nacelle/Pylon, Frame/Spar/Rib
  > NR 2 PYLON AFT ENGINE MOUNT FRAMES CRACKED APPROX 19 INCHES BELOW MID SPAR AT NAC STA 221.9.
- [SDR KCSA091080](https://openairdocs.org/sdr/KCSA091080.md): Bulkhead · corroded · Aug 11, 2009 · N707CK · Boeing 747246F · Nacelle/Pylon, Bulkhead/Firewall
  > NR 4 PYLON AFT ENGINE MOUNT BULKHEAD I/B FRAME LOWER TWO FASTENER HOLES CORRODED.
- [SDR KCSA081471](https://openairdocs.org/sdr/KCSA081471.md): Light · inoperative · Sep 16, 2008 · N707CK · Boeing 747246F · Emergency Lighting
  > DOOR L1 FWD CEILING EMERGENCY LIGHT INOP.
- [SDR KCSA081173](https://openairdocs.org/sdr/KCSA081173.md): Light · inoperative · Mar 13, 2008 · N707CK · Boeing 747246F · Emergency Lighting
  > UPPER DECK EMERGENCY SLIDE LIGHT IS INOP.
- [SDR KCSA071468](https://openairdocs.org/sdr/KCSA071468.md): Stiffener · cracked · Oct 14, 2007 · N707CK · Boeing 747246F · Nacelle/Pylon Miscellaneous Structure
  > NR 3 PYLON STIFFENER HORIZONTAL FLANGE CRACKED AT NAC STA 132, NAC WL 164.
- [SDR KCSA061184](https://openairdocs.org/sdr/KCSA061184.md): Doubler · gouged · Jun 21, 2006 · N707CK · Boeing 747246F · Nacelle/Pylon, Main Frame
  > NR 3 PYLON INTERNAL DOUBLER (FOR EMERGENCY FUEL DRAIN TUBE) IS GOUGED OR CRACKED AT NAC STA 190, RT SIDE.
- [SDR KCSA061183](https://openairdocs.org/sdr/KCSA061183.md): Shear Web · cracked · Jun 17, 2006 · N707CK · Boeing 747246F · Fuselage Miscellaneous Structure
  > MAIN DECK TENSION TIE SLOPING SHEAR WEB CRACKED BETWEEN BS 820 AND 840, RBL 80.
- [SDR KCSA061182](https://openairdocs.org/sdr/KCSA061182.md): Shear Web · cracked · Jun 17, 2006 · N707CK · Boeing 747246F · Fuselage Miscellaneous Structure
  > MAIN DECK TENSION TIE SLOPING SHEAR WEB IS CRACKED BETWEEN BS 820 AND 840, LBL 80.
- [SDR KCSA061179](https://openairdocs.org/sdr/KCSA061179.md): Strap · cracked · Jun 15, 2006 · N707CK · Boeing 747246F · Fuselage Miscellaneous Structure
  > MAIN DECK STA 780 TENSION TIE REINFORCEMENT STRAP IS CRACKED AT LBL 88.
- [SDR KCSA061178](https://openairdocs.org/sdr/KCSA061178.md): Shear Tie · cracked · Jun 15, 2006 · N707CK · Boeing 747246F · Fuselage Internal Mounting Structure
  > FUSELAGE FRAME SHEAR TIE IS CRACKED AT STA 840, BETWEEN STR 10L & 10AL.
- [SDR KCSA061177](https://openairdocs.org/sdr/KCSA061177.md): Shear Tie · cracked · Jun 15, 2006 · N707CK · Boeing 747246F · Fuselage Internal Mounting Structure
  > FUSELAGE FRAME SHEAR TIE IS CRACKED AT STA 840, BETWEEN STR 10R & 10AR.
- [SDR KCSA061176](https://openairdocs.org/sdr/KCSA061176.md): Frame · cracked · Jun 15, 2006 · N707CK · Boeing 747246F · Fuselage Main, Frame
  > FUSELAGE FRAME AND SHEAR TIES ARE CRACKED AT STA 820, BETWEEN STR 10R & 11R.
- [SDR KCSA061175](https://openairdocs.org/sdr/KCSA061175.md): Stringer · cracked · Jun 15, 2006 · N707CK · Boeing 747246F · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER IS CRACKED AT STA 820, STR 12R.
- [SDR KCSA061174](https://openairdocs.org/sdr/KCSA061174.md): Seat Track · damaged · Jun 11, 2006 · N707CK · Boeing 747246F · Fuselage, Seat/Cargo Attach Fittings
  > FWD PIT SEAT TRACK DAMAGED AT BS 650, RBL 45.
- [SDR KCSA061173](https://openairdocs.org/sdr/KCSA061173.md): Splice · corroded · Jun 6, 2006 · N707CK · Boeing 747246F · Fuselage Miscellaneous Structure
  > A/C BAY, STA 1000 LT SPLICE FITTING HAS EVIDENCE OF CORROSION.
- [SDR KCSA061170](https://openairdocs.org/sdr/KCSA061170.md): Skin · dented · May 25, 2006 · N707CK · Boeing 747246F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT APPROX BS 560, STR 45R.
- [SDR KCSA061169](https://openairdocs.org/sdr/KCSA061169.md): Bulkhead · cracked · May 24, 2006 · N707CK · Boeing 747246F · Nacelle/Pylon, Bulkhead/Firewall
  > NR 3 PYLON INTERNAL UPPER REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED AT NAC STA 221.90, LT SIDE.
- [SDR KCSA061168](https://openairdocs.org/sdr/KCSA061168.md): Bulkhead · cracked · May 24, 2006 · N707CK · Boeing 747246F · Nacelle/Pylon, Bulkhead/Firewall
  > NR 3 PYLON INTERNAL UPPER REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED AT NAC STA 221.90, RT SIDE.
- [SDR KCSA061167](https://openairdocs.org/sdr/KCSA061167.md): Floorbeam · damaged · May 18, 2006 · N707CK · Boeing 747246F · Fuselage Main, Floor Beam
  > UPPER CAP OF FLOORBEAM DAMAGED IN FWD BILGE AT BS 560, LBL 12.
- [SDR KCSA061166](https://openairdocs.org/sdr/KCSA061166.md): Fitting · corroded · May 16, 2006 · N707CK · Boeing 747246F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOORBEAM LOADING SYSTEM FITTING IS CORRODED AT STA 640, LBL 83.
- [SDR 061165](https://openairdocs.org/sdr/061165.md): Seat Track · cracked · May 15, 2006 · N707CK · Boeing 747246F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK CLIP NUT HOLE CRACKED AT BS 1600, RBL 75.
- [SDR 061164](https://openairdocs.org/sdr/061164.md): Seat Track · cracked · May 12, 2006 · N707CK · Boeing 747246F · Fuselage, Seat/Cargo Attach Fittings
  > COCKPIT CAPTAIN SEAT TRACK IS CRACKED AROUND STOP AREA AT FORWARD OUTBOARD LT SIDE.
- [SDR 061163](https://openairdocs.org/sdr/061163.md): Seat Track · cracked · May 12, 2006 · N707CK · Boeing 747246F · Fuselage, Seat/Cargo Attach Fittings
  > COCKPIT FIRST OFFICER SEAT TRACK IS CRACKED AROUND STOP AREA AT FORWARD OUTBOARD RT SIDE.
- [SDR 061162](https://openairdocs.org/sdr/061162.md): Rib · cracked · May 12, 2006 · N707CK · Boeing 747246F · Nacelle/Pylon, Frame/Spar/Rib
  > NR 3 PYLON INTERNAL RT SIDE RIB FRAME IS CRACKED AND GOUGED AT NAC STA 192, 7 INCHES ABOVE LOWER SPAR.
- [SDR K4HA99077](https://openairdocs.org/sdr/K4HA99077.md): Engine · failed · Oct 2, 1999 · N707CK · Boeing 747269B · Engine (Turbine/Turboprop)
  > NUMBER 4 ENGINE ON TAKEOFF LOST POWER, IFSD AND PULLED FIRE HANDLE. ABNORMAL ENGINE IND-EPR, N1, N2, FF, EGT. REMOVED AND REPLACED ENGINE.
- [SDR K4HA99095](https://openairdocs.org/sdr/K4HA99095.md): Skin · corroded · Aug 2, 1999 · N707CK · Boeing 747269B · Wing, Plate/Skin
  > IAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND EXTERIOR OF THE RIGHT WING FROM WING TO BODY FAIRINGS TO TIP, INCLUDING UPPER AND LOWER INSPAR SKINS AND FASTENERS, LEADING AND TRAILING EDGE STRUCTURE BEYOND SRM LIMITS. REMO
- [SDR CKSA99071](https://openairdocs.org/sdr/CKSA99071.md): Engine · malfunctioned · Jul 29, 1999 · N707CK · Boeing 747269B · Engine (Turbine/Turboprop)
  > DURING CLIMB AT ALT 28.0, HEARD LOUD BANG JARRING ACFT. NR 3 ENG FAILURE. TIME 2345Z, 21 MIN INTO CLIMB. CLEAR AIR, NO ICING. AIRSPEED 300 KTS, OIL TEMP 130 DEGREES, EGT NORMAL, ENG IGNITION ON, ANTI-ICE OFF, OIL PRESSURE WENT TO 0 SHORTLY AFTER SHUTDOWN (
- [SDR CKSA99003](https://openairdocs.org/sdr/CKSA99003.md): Slide · deployed · Mar 8, 1999 · N707CK · Boeing 747269B · Escape Slide
  > ON ARRIVING AT AIRCRAFT FOR PREFLIGHT, FOUND UPPER DECK CREW DOOR OPEN, CREW ESCAPE SLIDE PARTIALLY DEPLOYED. THE FOLLOWING WAS DETERMINED: SLIDE WAS IN PROPER POSITION FOR DEPLOYMENT, DOOR WAS FOUND OPEN WITH DOOR HANDLE IN ARMED POSITION, SLIDE BOTTLE TO DE
- [SDR CKSA98757](https://openairdocs.org/sdr/CKSA98757.md): Longeron · bulged · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage Main, Longeron/Stringer
  > LT WLG W/W STA 1241 BULKHEAD UPPER AREA FOUND BULGE UP AT STA 1241 TO STA 1250, LBL 60 TO LBL 70. REPLACED RIVETS, BOLTS AND COLLARS AT AFFECTED AREA IAW SRM 51-10-01. CORROSION REMOVAL IAW SRM 57-10-01, PRIMED AND TREATED IAW SRM 51-10-02, MM 51-20-11 AND 5
- [SDR CKSA98756](https://openairdocs.org/sdr/CKSA98756.md): Seat Track · cracked · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage, Seat/Cargo Attach Fittings
  > LOCATED AT ZONE 250 MAIN DECK, STA 1540, RBL 33, CORROSION CRACK FOUND ON SEAT TRACK SECTION L-1. FOUND TO BE OUT OF LIMITS PER SRM 53-10-01 FIG 1. REPAIRED SEAT TRACK IAW SRM 53-10-05 FIG 1A AND SRM 51-10-02. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CA
- [SDR CKSA98755](https://openairdocs.org/sdr/CKSA98755.md): Seat Track · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage, Seat/Cargo Attach Fittings
  > LOCATED IN ZONE 240 MID DECK, STA 1010, RBL 11, SEAT/TIE DOWN TRACK FOUND CORRODED. CORROSION BLEND OUT BEYOND SRM LIMITS IAW SRM 53-10-01 FIG 1. REPAIRED IAW SRM 53-10-05 FIG 35 AND MM 51-10-00, 12-20-00. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD A
- [SDR CKSA98754](https://openairdocs.org/sdr/CKSA98754.md): Seat Track · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage, Seat/Cargo Attach Fittings
  > AT ZONE 250 MID DECK, STA 2260 TO STA 2280, LBL 34 SEAT TRACK FOUND CORRODED. REMOVED CORROSION IAW SRM 51-10-01, FOUND OUT OF LIMITS IAW SRM 53-10-01 FIG 1. REPAIRED IAW SRM 53-10-05 FIG 1A AND SRM 51-10-02. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD
- [SDR CKSA98753](https://openairdocs.org/sdr/CKSA98753.md): Floorbeam · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage Main, Floor Beam
  > LOCATED AT ZONE 250 MID CABIN, BS 2240, FLOORBEAM HAS AREA OF CORROSION FROM LBL62 TO LBL 82. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FLOORBEAM IAW SRM 51-40-04 FIG 1, TREATED IAW SRM 53-10-02. FOUND DURING S
- [SDR CKSA98752](https://openairdocs.org/sdr/CKSA98752.md): Seat Track · cracked · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT ZONE 220 UPPER DECK CABIN, STA 480, LBL 55, SEAT TRACK/TIE DOWN TRACK HAS CORROSION CRACK 3 INCH LENGTH. REMOVED CORROSION IAW SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPLACED SEAT TRACK IAW SRM 51-10-01 PG 18. CORROSION INHIBITO
- [SDR CKSA98751](https://openairdocs.org/sdr/CKSA98751.md): Intercostal · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage Miscellaneous Structure
  > IN BULK CARGO COMPARTMENT, AFTER FLOOR SUPPORT INTERCOSTAL REMOVED. CORROSION FOUND ON FLOOR SUPPORT HAT SECTION HORIZONTAL FLANGE A AT ZONE 150 AFT, BS 1980, RBL 55. FLOOR SUPPORT HAT SECTION REPLACED AS PER SRM H-4001. FOUND DURING SCHEDULED C-CHECK AND C
- [SDR CKSA98750](https://openairdocs.org/sdr/CKSA98750.md): Skin · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Cargo/Baggage Doors
  > AFT CARGO DOOR INTERNAL SKIN BULGE CORROSION FOUND AT AFT LOWER CORNER OF DOOR UNDER SEAL RETAINER ZONE 141. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NUMBER
- [SDR CKSA98749](https://openairdocs.org/sdr/CKSA98749.md): Intercostal · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Fuselage Miscellaneous Structure
  > FOUND IN BULK CARGO COMPARTMENT, FLOOR SUPPORT INTERCOSTAL BULGED AND CORRODED AROUND ANCHOR NUTS AT ZONE 100, STA 1920 TO STA 1980, RBL 55. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (V
- [SDR CKSA98748](https://openairdocs.org/sdr/CKSA98748.md): Spar · corroded · Dec 12, 1998 · N707CK · Boeing 747269B · Wing Spar
  > LOCATED AT LEFT WING LOWER L/E CAVITY, FRONT SPAR, LOWER CHORD AT OSLE 1440 AND OSLE 1460 FOUND SMALL AREA OF LEVEL 2 LOCAL CORROSION. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG).
- [SDR CKSA98518](https://openairdocs.org/sdr/CKSA98518.md): Engine · defective · Sep 19, 1998 · N707CK · Boeing 747269B · Engine (Turbine/Turboprop)
  > NR 4 ENGINE FIRE INDICATION LIGHT AND BELL WENT OFF AT 2135Z, 24,000 FEET. AIRCRAFT GW 764,998 POUNDS, FUEL 264,000. SECURED ENGINE, DID NOT HAVE TO FIRE BOTTLE, DUMPED 132,000 POUNDS OF FUEL. OIL QUANTITY OBSERVED DECREASING TO HALF INDICATION PRIOR TO BEL
- [SDR CKSA98337](https://openairdocs.org/sdr/CKSA98337.md): Engine · failed · May 25, 1998 · N707CK · Boeing 747269B · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, NR 1 ENGINE HAD A FIRE WARNING SHUTDOWN ENGINE AS PER AOM DISCHARGED ONE FIRE BOTTLE, LIGHT WENT OUT. ON POST FLIGHT, FOUND HEAT DAMAGE TO BOTH COWLS, AFT FIRE LOOP, AND AFT WIRING HARNESS. DETERMINED ACFT WILL DO 3 ENGINE FERRY. NR 1 ENGINE
- [SDR CKSA98019](https://openairdocs.org/sdr/CKSA98019.md): Clamp · misinstalled · Feb 9, 1998 · N707CK · Boeing 747269B · Landing Gear Position and Warning
  > AFTER T/O, MLG LEVER LOCK WOULD NOT RETRACT. ACCOMP ABNORMAL CHECKLIST, FOUND BOTH PRIMARY AND ALT WING GEAR TILT LIGHTS ILLUM. CYCLED PRIM DIS AND CONT L/G CB, MLG LEVER LOCK RETRACTED. WING GEAR PRI TILT LIGHT EXTINGUISHED AND GEAR RETRACTED. APPROX 10 MIN A
- [SDR CKSA97315](https://openairdocs.org/sdr/CKSA97315.md): Fire Loop · malfunctioned · Jul 2, 1997 · N707CK · Boeing 747269B · Fire Detection
  > NR 1 ENGINE A FIRE DETECTION LOOP FLUCTUATING (SPIKING INTO RED ZONE). TRANSFERRED TO DMI NR 257 IAW MEL 26-1 CAT C PLACARD INSTALLED. PERFORMED OPERATIONAL CHECK OF NR 1 ENG A LOOP, OPS CHECKS NORMAL ON GROUND. THIS CLEARS DMI 257, PLACARDS REMOVED.
- [SDR CKSA97313](https://openairdocs.org/sdr/CKSA97313.md): Connector · dirty · Jun 26, 1997 · N707CK · Boeing 747269B · Fire Detection
  > NUMBER ONE ENGINE FIRE WARNING A-LOOP SHOWS INTERMITTENT FAULT. TRANSFERRED TO DMI NUMBER 250 IN ACCORDANCE WITH MEL 26-1 CATAGORY C PLACARDS INSTALLED. CLEANED FIRE LOOP CONNECTORS ON ENGINE, OPS CHECKS GOOD IAW 26-12-00. THIS CLEARS DMI 250 PLACARDS REMOV
- [SDR CKSA97279](https://openairdocs.org/sdr/CKSA97279.md): Wire · broken · Jun 15, 1997 · N707CK · Boeing 747269B · Fire Detection
  > NR 1 ENGINE A FIRE DETECTOR LOOP FLUCTUATING FULL SCALE. TRANSFERRED TO DMI NR 242 IAW MEL 26-2 CAT C, PLACARDS INSTALLED. REPAIRED BROKEN WIRE AT A-SYSTEM LOOP AT CANNON PLUG, OPS CHECK NORMAL IAW B747 26-11-00. THIS CLEARS DMI 242.
- [SDR CKSA97278](https://openairdocs.org/sdr/CKSA97278.md): Fire Loop · shorted · Jun 13, 1997 · N707CK · Boeing 747269B · Fire Detection
  > NR 1 ENGINE A FIRE DETECTOR LOOP INTERMITTENTLY SPIKES HIGH CAUSING FAULT LIGHT, B-LOOP OK. FOUND FIRE LOOP-A SYSTEM LOOSE AND TOUCHING COWL. RESECURED, OPS CHECKED ON GROUND IAW CHAPTER 26-00. NO DEFECTS NOTED AT THIS TIME.
- [SDR CKSA97252](https://openairdocs.org/sdr/CKSA97252.md): Bulkhead · cracked · May 19, 1997 · N707CK · Boeing 747269B · Fuselage Main, Bulkhead
  > DURING HARD LANDING INSPECT, FOUND AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OUTBOARD FASTENER ROW 16TH FROM TOP HOLE EMITS CRACK. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR ON AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OTHER FAS
- [SDR CKSA97251](https://openairdocs.org/sdr/CKSA97251.md): Bulkhead · cracked · May 19, 1997 · N707CK · Boeing 747269B · Nacelle/Pylon, Bulkhead/Firewall
  > DURING C-2 CHECK INSPECTION, FOUND PYLON BULKHEAD, NAC STA 222 FORWARD OUTBOARD DOUBLER CRACKED. REPLACED FORWARD OUTBOARD DOUBLER WITH NEW PART IAW SRM 51-10-01 AND 51-30-02. C-CHECK WORK CARD NUMBER 7TK7197. NON-ROUTINE TASK CARD NUMBER 101932.

Next page: https://openairdocs.org/deregistered/N707CK-2014-12-11/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 = 'N707CK' AND deregistration_id = 'N707CK-2014-12-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N707CK-2014-12-11/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.
