# N716CK: Boeing 747-122, registration cancelled 2012-04-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 30, 2012
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 747-122](https://openairdocs.org/model/boeing-747-122) (registry code 1384872)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 19753
- Type of aircraft: Fixed wing multi engine
- Certificate issued: November 13, 2002
- Last registry action: November 18, 2008
- Mode S code: A99293
- Owner when cancelled: [Kelsey Investments LLC](https://openairdocs.org/faa-owner/KELSEY%20INVESTMENTS%20LLC)
- Location: [Ann Arbor, MI](https://openairdocs.org/faa-place/MI/Ann%20Arbor)
- Owner type: Corporation
- Owner's area on the map: 42.2620° N, 83.7167° W: Placed by OpenAirDocs at the center of ZIP code 48104, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N716CK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=716CK
- Page: https://openairdocs.org/deregistered/N716CK-2012-04-30

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 747-122: https://openairdocs.org/model/boeing-747-122.md

## Service difficulty reports (156, newest 50)

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

- [SDR KCSA081415](https://openairdocs.org/sdr/KCSA081415), Aug 20, 2008: SKIN. CORRODED. LT WING LOWER SKIN HAS CORROSION ON UPPER SURFACE AT LES 884. (S)
- [SDR KCSA081407](https://openairdocs.org/sdr/KCSA081407), Aug 18, 2008: BRACKET. CORRODED. CORROSION ON ATTACH ANGLES ON INBOARD AND OUTBOARD SIDE OF BRACKET AT BS 1350, LBL 78, WL 139. (S)
- [SDR KCSA081408](https://openairdocs.org/sdr/KCSA081408), Aug 18, 2008: BULKHEAD. CORRODED. CORROSION ON CANTED BULKHEAD LOWER AFT CORD AT BS 1241, LBL 95. (S)
- [SDR KCSA081403](https://openairdocs.org/sdr/KCSA081403), Aug 16, 2008: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN IS DAMAGED AT AFT SIDE OF BULK CARGO DOOR CUTOUT AREA AT STA 2030, STR 34R. (S)
- [SDR KCSA081397](https://openairdocs.org/sdr/KCSA081397), Aug 16, 2008: ANGLE. CORRODED. RT BODY WHEEL WELL LONGERON BOX ANGLE IS CORRODED AT STA 1446, RBL 120, WL 113. (S)
- [SDR KCSA081383](https://openairdocs.org/sdr/KCSA081383), Aug 13, 2008: ATTACH ANGLE. CORRODED. CORROSION FOUND ON ATTACH ANGLE OF LANDING GEAR SUPPORT BEAM AT STA 1350, RBL 35. (S)
- [SDR KCSA081382](https://openairdocs.org/sdr/KCSA081382), Aug 13, 2008: SKIN. DENTED. FWD E&E DOOR HAS SMALL DENT AT L/E ON SKIN. (S)
- [SDR KCSA081381](https://openairdocs.org/sdr/KCSA081381), Aug 13, 2008: ANGLE. CORRODED. INSIDE LONGERON BOX TEE ANGLE AT WL 113, STA 1379, RBL 115 CORRODED. (S)
- [SDR KCSA081380](https://openairdocs.org/sdr/KCSA081380), Aug 13, 2008: FRAME. CORRODED. CORROSION ON DOUBLER ON TOP OF RT OVERWING LONGERON AT BS 1315, RBL 123, WL 158. (S)
- [SDR KCSA081379](https://openairdocs.org/sdr/KCSA081379), Aug 13, 2008: FRAME. CORRODED. CORROSION ON FRAME ABOVE RT OVERWING LONGERON AT BS 1297, RBL 121, WL 160. (S)
- [SDR KCSA081378](https://openairdocs.org/sdr/KCSA081378), Aug 13, 2008: STIFFENER. CORRODED. CORROSION ON LT OVERWING LONGERON BOX FRAME STIFFENER. (S)
- [SDR KCSA081331](https://openairdocs.org/sdr/KCSA081331), Jul 18, 2008: SKIN. CORRODED. LT WING SKIN AT WS 993 TO WS 995 HAS CORROSION. (A)
- [SDR KCSA081319](https://openairdocs.org/sdr/KCSA081319), Jul 15, 2008: SKIN. CORRODED. LT WING LOWER SKIN CORRODED AT APPROX 1300. (A)
- [SDR KCSA081217](https://openairdocs.org/sdr/KCSA081217), Mar 29, 2008: BULKHEAD. CHAFED. NR 2 PYLON HYDRAULIC PRESSURE LINE FITTING CHAFED ON AFT SIDE OF NAC STA 221.9 BULKHEAD.
- [SDR KCSA081209](https://openairdocs.org/sdr/KCSA081209), Mar 26, 2008: WEB. CRACKED. NOSE WHEEL WELL RT SIDE STA-285 WL-160 WEB CRACKED .75 INCH UNDER BONDED STRAP.
- [SDR KCSA081005](https://openairdocs.org/sdr/KCSA081005), Jan 8, 2008: SEAT TRACK. CRACKED. FORWARD BILGE SEAT TRACK IS CRACKED BETWEEN STA 540 & 560, RBL 45.
- [SDR KCSA081004](https://openairdocs.org/sdr/KCSA081004), Jan 8, 2008: BULKHEAD. GOUGED. NR 4 PYLON UPPER FORWARD ENGINE MOUNT BULKHEAD CHORD NAC STA 128.95 HAS A DEEP GOUGE ON INBOARD SIDE JUST AFT OF CHORD BEND RADIUS AT NOSE COWL FORWARD FAIRING 
- [SDR KCSA071329](https://openairdocs.org/sdr/KCSA071329), Aug 31, 2007: LIGHT. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE UPPER DECK RIGHT ESCAPE DOOR INOP.
- [SDR KCSA071200](https://openairdocs.org/sdr/KCSA071200), Jul 3, 2007: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE UPPER DECK EXIT DOOR INOP.
- [SDR KCSA07041](https://openairdocs.org/sdr/KCSA07041), Apr 24, 2007: FILTER. CONTAMINATED. AT 8000', IDLE THRUST EGT NR 4 AT 874 DEGREES CELSIUS AND N2 AT 43 PERCENT. ALL OTHER INSTRUMENTS NORMAL. ACCOMPLISHED ENGINE STALL IN FLT (ABNORMAL EGT) CHECKL
- [SDR KCSA07011](https://openairdocs.org/sdr/KCSA07011), Feb 1, 2007: ENGINE. FLAMED OUT. FLT LEVEL 34.0 NR 4 ENG FLAMED OUT, DESCENDED TO F.L 280. RESTARTED ENG - ALL PARAMETERS NORMAL. ENG RESTARTED ON FIRST ATTEMPT. CLIMBED TO FL 340 ENG OPERATES 
- [SDR KCSA061490](https://openairdocs.org/sdr/KCSA061490), Nov 2, 2006: LIGHT. INOPERATIVE. UPPER DECK EMERGENCY LIGHT INOP AT UPPER DECK SERVICE DOOR.
- [SDR KCSA061328](https://openairdocs.org/sdr/KCSA061328), Sep 18, 2006: SIGN. NO TEST. FOUND UPPER DECK EXIT SIGN AND SLIDE LIGHT X325 WILL NOT TEST.
- [SDR KCSA06082](https://openairdocs.org/sdr/KCSA06082), Sep 10, 2006: LINE. LEAKING. NR 1 HYD LOW LIGHT FOR SYS NR 1 ILLUMINATED. NR 1 HYD SYS QTY WAS 2 GALS WHEN ADP TURNED OFF AND ADP DEPRESSURIZED. ON POST FLT, FOUND NR 1 ADP BLOWOUT DOOR OPE
- [SDR KCSA061255](https://openairdocs.org/sdr/KCSA061255), Aug 6, 2006: FRAME. CRACKED. NR 2 PYLON NAC STA 221.9 FRAME CRACKED AT FWD I/B UPPER CORNER.
- [SDR KCSA061254](https://openairdocs.org/sdr/KCSA061254), Aug 5, 2006: BULKHEAD. CHAFED. NR 2 PYLON STA NAC 221.9 BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION.
- [SDR 061159](https://openairdocs.org/sdr/061159), May 2, 2006: STIFFENER. CRACKED. BS 2658 BULKHEAD STIFFENER CRACKED AT LBL 30, WL 277.
- [SDR 061157](https://openairdocs.org/sdr/061157), May 2, 2006: RIB. CHAFED. RIGHT WING L/E RIB AT FSSI 1022 IS CHAFED.
- [SDR 061156](https://openairdocs.org/sdr/061156), May 2, 2006: RIB. CHAFED. RIGHT WING L/E RIB AT FSSI 887 IS CHAFED.
- [SDR 061158](https://openairdocs.org/sdr/061158), May 1, 2006: BOLT. LOOSE. EXTERNAL FUSELAGE RT SIDE OVERWING FITTING HAS A BOLT LOOSE AT STA 1346, WL 156.
- [SDR 061154](https://openairdocs.org/sdr/061154), Apr 29, 2006: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION AROUND LT OUTFLOW VALVE CUTOUT AREA AT STA 2210, STR 43L.
- [SDR 061153](https://openairdocs.org/sdr/061153), Apr 27, 2006: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK HAS CORROSION AT STA 910, RBL 11.33.
- [SDR 061152](https://openairdocs.org/sdr/061152), Apr 24, 2006: STIFFENER. CORRODED. CORROSION ON TOP OF BS 1480 BULKHEAD HORIZONTAL STIFFENER WEB AT LBL 48, WL 118.
- [SDR KCSA061149](https://openairdocs.org/sdr/KCSA061149), Apr 20, 2006: FRAME. CRACKED. BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, LBL 18.
- [SDR KCSA061148](https://openairdocs.org/sdr/KCSA061148), Apr 20, 2006: FRAME. CRACKED. BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, RBL 18.
- [SDR KCSA061147](https://openairdocs.org/sdr/KCSA061147), Apr 17, 2006: BULKHEAD. GOUGED. MAIN CABIN STA 2360 PRESSURE BULKHEAD WEB FORWARD SIDE IS GOUGED AROUND FASTENER ADJACENT TO STR 24R.
- [SDR KCSA061143](https://openairdocs.org/sdr/KCSA061143), Apr 17, 2006: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 2484, BETWEEN STR 22L & 23L.
- [SDR KCSA061146](https://openairdocs.org/sdr/KCSA061146), Apr 16, 2006: FRAME. CRACKED. NR 4 PYLON INTERNAL RT SIDE LOWER FRAME IS CRACKED AT NAC STA 236.
- [SDR KCSA061145](https://openairdocs.org/sdr/KCSA061145), Apr 16, 2006: FITTING. CORRODED. FUSELAGE STRINGER END FITTING IS CORRODED AT AFT SIDE OF STA 2360 BULKHEAD, STR 48L.
- [SDR KCSA061144](https://openairdocs.org/sdr/KCSA061144), Apr 16, 2006: BULKHEAD. CORRODED. MAIN CABIN STA 2360 BULKHEAD LOWER FORWARD CHORD IS CORRODED IN HOLES AT STRINGER END FITTING STR 48L.
- [SDR 061141](https://openairdocs.org/sdr/061141), Apr 13, 2006: SKIN. CORRODED. EXTERNAL FUSELAGE SKIN HAS CORROSION AT STA 600, ABOVE STR 6R.
- [SDR 061140](https://openairdocs.org/sdr/061140), Apr 13, 2006: FRAME. CRACKED. BULK PIT BS 2140 FUSELAGE FRAME WEB CRACKED AT RBL 18.
- [SDR 061139](https://openairdocs.org/sdr/061139), Apr 13, 2006: DOUBLER. DAMAGED. NR 3 PYLON I/B EXTERNAL SKIN DOUBLER AT NAC STA 221 ABOVE REAR ENGINE MOUNT HAS DAMAGE.
- [SDR 061137](https://openairdocs.org/sdr/061137), Apr 12, 2006: STRINGER. CRACKED. LEFT HORIZONTAL STAB UPPER STR 4 CRACKED AT STAB STA 260.
- [SDR 061136](https://openairdocs.org/sdr/061136), Apr 12, 2006: BULKHEAD. DENTED. BS 2360 BULKHEAD HAS DENTS AT LBL 7.5, WL 347.
- [SDR 061135](https://openairdocs.org/sdr/061135), Apr 12, 2006: BULKHEAD. DENTED. BS 2360 BULKHEAD HAS DENTS AT RBL 54, WL 313.
- [SDR 061134](https://openairdocs.org/sdr/061134), Apr 12, 2006: STIFFENER. CRACKED. NR 4 PYLON MID SPAR WEB LOWER SIDE STIFFENER CRACKED AT O/B END IN RADIUS AT NAC STA 231.
- [SDR 061133](https://openairdocs.org/sdr/061133), Apr 12, 2006: STRINGER. BENT. FUSELAGE STRINGER IS BENT AT STA 1930, STR 1R.
- [SDR 061132](https://openairdocs.org/sdr/061132), Apr 11, 2006: FITTING. CORRODED. FUSELAGE STRINGER END FITTING IS CORRODED AT STA 1480, STR 47R.
- [SDR 061131](https://openairdocs.org/sdr/061131), Apr 11, 2006: STRAP. CORRODED. AFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.

All 156: https://openairdocs.org/deregistered/N716CK-2012-04-30/reports.md

## Other aircraft with N716CK

- [Registered now](https://openairdocs.org/aircraft/N716CK): Boeing 747-4B5F, S/N 26408, built 1998

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