# Service difficulty reports: N716CK, cancelled Apr 30, 2012

A list on [N716CK, cancelled Apr 30, 2012](https://openairdocs.org/deregistered/N716CK-2012-04-30.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 4 · 156 reports

- [SDR KCSA081415](https://openairdocs.org/sdr/KCSA081415.md): Skin · corroded · Aug 20, 2008 · N716CK · Boeing 747122 · Wing, Plate/Skin
  > LT WING LOWER SKIN HAS CORROSION ON UPPER SURFACE AT LES 884. (S)
- [SDR KCSA081407](https://openairdocs.org/sdr/KCSA081407.md): Bracket · corroded · Aug 18, 2008 · N716CK · Boeing 747122 · Fuselage Main, Attach Fittings
  > 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.md): Bulkhead · corroded · Aug 18, 2008 · N716CK · Boeing 747122 · Fuselage Main, Bulkhead
  > CORROSION ON CANTED BULKHEAD LOWER AFT CORD AT BS 1241, LBL 95. (S)
- [SDR KCSA081403](https://openairdocs.org/sdr/KCSA081403.md): Skin · damaged · Aug 16, 2008 · N716CK · Boeing 747122 · Fuselage Main, Plate/Skin
  > 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.md): Angle · corroded · Aug 16, 2008 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > RT BODY WHEEL WELL LONGERON BOX ANGLE IS CORRODED AT STA 1446, RBL 120, WL 113. (S)
- [SDR KCSA081383](https://openairdocs.org/sdr/KCSA081383.md): Attach Angle · corroded · Aug 13, 2008 · N716CK · Boeing 747122 · Fuselage, Landing Gear Attach Fittings
  > CORROSION FOUND ON ATTACH ANGLE OF LANDING GEAR SUPPORT BEAM AT STA 1350, RBL 35. (S)
- [SDR KCSA081382](https://openairdocs.org/sdr/KCSA081382.md): Skin · dented · Aug 13, 2008 · N716CK · Boeing 747122 · Electrical/Electronic Compartment Doors
  > FWD E&E DOOR HAS SMALL DENT AT L/E ON SKIN. (S)
- [SDR KCSA081381](https://openairdocs.org/sdr/KCSA081381.md): Angle · corroded · Aug 13, 2008 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > INSIDE LONGERON BOX TEE ANGLE AT WL 113, STA 1379, RBL 115 CORRODED. (S)
- [SDR KCSA081380](https://openairdocs.org/sdr/KCSA081380.md): Frame · corroded · Aug 13, 2008 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > CORROSION ON DOUBLER ON TOP OF RT OVERWING LONGERON AT BS 1315, RBL 123, WL 158. (S)
- [SDR KCSA081379](https://openairdocs.org/sdr/KCSA081379.md): Frame · corroded · Aug 13, 2008 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > CORROSION ON FRAME ABOVE RT OVERWING LONGERON AT BS 1297, RBL 121, WL 160. (S)
- [SDR KCSA081378](https://openairdocs.org/sdr/KCSA081378.md): Stiffener · corroded · Aug 13, 2008 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > CORROSION ON LT OVERWING LONGERON BOX FRAME STIFFENER. (S)
- [SDR KCSA081331](https://openairdocs.org/sdr/KCSA081331.md): Skin · corroded · Jul 18, 2008 · N716CK · Boeing 747122 · Wing, Plate/Skin
  > LT WING SKIN AT WS 993 TO WS 995 HAS CORROSION. (A)
- [SDR KCSA081319](https://openairdocs.org/sdr/KCSA081319.md): Skin · corroded · Jul 15, 2008 · N716CK · Boeing 747122 · Wing, Plate/Skin
  > LT WING LOWER SKIN CORRODED AT APPROX 1300. (A)
- [SDR KCSA081217](https://openairdocs.org/sdr/KCSA081217.md): Bulkhead · chafed · Mar 29, 2008 · N716CK · Boeing 747122 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 PYLON HYDRAULIC PRESSURE LINE FITTING CHAFED ON AFT SIDE OF NAC STA 221.9 BULKHEAD.
- [SDR KCSA081209](https://openairdocs.org/sdr/KCSA081209.md): Web · cracked · Mar 26, 2008 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL RT SIDE STA-285 WL-160 WEB CRACKED.75 INCH UNDER BONDED STRAP.
- [SDR KCSA081005](https://openairdocs.org/sdr/KCSA081005.md): Seat Track · cracked · Jan 8, 2008 · N716CK · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD BILGE SEAT TRACK IS CRACKED BETWEEN STA 540 & 560, RBL 45.
- [SDR KCSA081004](https://openairdocs.org/sdr/KCSA081004.md): Bulkhead · gouged · Jan 8, 2008 · N716CK · Boeing 747122 · Nacelle/Pylon, Bulkhead/Firewall
  > 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 LATCH FITTING.
- [SDR KCSA071329](https://openairdocs.org/sdr/KCSA071329.md): Light · inoperative · Aug 31, 2007 · N716CK · Boeing 747122 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE UPPER DECK RIGHT ESCAPE DOOR INOP.
- [SDR KCSA071200](https://openairdocs.org/sdr/KCSA071200.md): Light · inoperative · Jul 3, 2007 · N716CK · Boeing 747122 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE UPPER DECK EXIT DOOR INOP.
- [SDR KCSA07041](https://openairdocs.org/sdr/KCSA07041.md): Filter · contaminated · Apr 24, 2007 · N716CK · Boeing 747122 · Engine (Turbine/Turboprop)
  > 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) CHECKLISTS. ATTEMPTED RESTART WITH RAPID RESTART PROCEDURE QRH-69. RESULTED IN DUPLICATE INDICATIONS.
- [SDR KCSA07011](https://openairdocs.org/sdr/KCSA07011.md): Engine · flamed out · Feb 1, 2007 · N716CK · Boeing 747122 · Engine (Turbine/Turboprop)
  > 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 NORMAL. PERFORMED ENG FLAME OUT INSPECTION IAW MM 71-00-42 P-118. PERFORMED ENG WINDMILL INSPECTION
- [SDR KCSA061490](https://openairdocs.org/sdr/KCSA061490.md): Light · inoperative · Nov 2, 2006 · N716CK · Boeing 747122 · Emergency Lighting
  > UPPER DECK EMERGENCY LIGHT INOP AT UPPER DECK SERVICE DOOR.
- [SDR KCSA061328](https://openairdocs.org/sdr/KCSA061328.md): Sign · no test · Sep 18, 2006 · N716CK · Boeing 747122 · Emergency Lighting
  > FOUND UPPER DECK EXIT SIGN AND SLIDE LIGHT X325 WILL NOT TEST.
- [SDR KCSA06082](https://openairdocs.org/sdr/KCSA06082.md): Line · leaking · Sep 10, 2006 · N716CK · Boeing 747122 · Hydraulic System, Main
  > 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 OPEN AND SKYDROL LEAK FROM ACCESSORY PANEL. REPLACED NR 1 HYD SYSTEM RETURN LINE IAW AMM 29-11-00.
- [SDR KCSA061255](https://openairdocs.org/sdr/KCSA061255.md): Frame · cracked · Aug 6, 2006 · N716CK · Boeing 747122 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 2 PYLON NAC STA 221.9 FRAME CRACKED AT FWD I/B UPPER CORNER.
- [SDR KCSA061254](https://openairdocs.org/sdr/KCSA061254.md): Bulkhead · chafed · Aug 5, 2006 · N716CK · Boeing 747122 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 2 PYLON STA NAC 221.9 BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION.
- [SDR 061159](https://openairdocs.org/sdr/061159.md): Stiffener · cracked · May 2, 2006 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > BS 2658 BULKHEAD STIFFENER CRACKED AT LBL 30, WL 277.
- [SDR 061157](https://openairdocs.org/sdr/061157.md): Rib · chafed · May 2, 2006 · N716CK · Boeing 747122 · Wing, Rib/Bulkhead
  > RIGHT WING L/E RIB AT FSSI 1022 IS CHAFED.
- [SDR 061156](https://openairdocs.org/sdr/061156.md): Rib · chafed · May 2, 2006 · N716CK · Boeing 747122 · Wing, Rib/Bulkhead
  > RIGHT WING L/E RIB AT FSSI 887 IS CHAFED.
- [SDR 061158](https://openairdocs.org/sdr/061158.md): Bolt · loose · May 1, 2006 · N716CK · Boeing 747122 · Fuselage Main, Attach Fittings
  > EXTERNAL FUSELAGE RT SIDE OVERWING FITTING HAS A BOLT LOOSE AT STA 1346, WL 156.
- [SDR 061154](https://openairdocs.org/sdr/061154.md): Skin · corroded · Apr 29, 2006 · N716CK · Boeing 747122 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION AROUND LT OUTFLOW VALVE CUTOUT AREA AT STA 2210, STR 43L.
- [SDR 061153](https://openairdocs.org/sdr/061153.md): Seat Track · corroded · Apr 27, 2006 · N716CK · Boeing 747122 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK HAS CORROSION AT STA 910, RBL 11.33.
- [SDR 061152](https://openairdocs.org/sdr/061152.md): Stiffener · corroded · Apr 24, 2006 · N716CK · Boeing 747122 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP OF BS 1480 BULKHEAD HORIZONTAL STIFFENER WEB AT LBL 48, WL 118.
- [SDR KCSA061149](https://openairdocs.org/sdr/KCSA061149.md): Frame · cracked · Apr 20, 2006 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, LBL 18.
- [SDR KCSA061148](https://openairdocs.org/sdr/KCSA061148.md): Frame · cracked · Apr 20, 2006 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > BULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, RBL 18.
- [SDR KCSA061147](https://openairdocs.org/sdr/KCSA061147.md): Bulkhead · gouged · Apr 17, 2006 · N716CK · Boeing 747122 · Fuselage Main, Bulkhead
  > MAIN CABIN STA 2360 PRESSURE BULKHEAD WEB FORWARD SIDE IS GOUGED AROUND FASTENER ADJACENT TO STR 24R.
- [SDR KCSA061143](https://openairdocs.org/sdr/KCSA061143.md): Skin · damaged · Apr 17, 2006 · N716CK · Boeing 747122 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 2484, BETWEEN STR 22L & 23L.
- [SDR KCSA061146](https://openairdocs.org/sdr/KCSA061146.md): Frame · cracked · Apr 16, 2006 · N716CK · Boeing 747122 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 4 PYLON INTERNAL RT SIDE LOWER FRAME IS CRACKED AT NAC STA 236.
- [SDR KCSA061145](https://openairdocs.org/sdr/KCSA061145.md): Fitting · corroded · Apr 16, 2006 · N716CK · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER END FITTING IS CORRODED AT AFT SIDE OF STA 2360 BULKHEAD, STR 48L.
- [SDR KCSA061144](https://openairdocs.org/sdr/KCSA061144.md): Bulkhead · corroded · Apr 16, 2006 · N716CK · Boeing 747122 · Fuselage Main, Bulkhead
  > 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.md): Skin · corroded · Apr 13, 2006 · N716CK · Boeing 747122 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS CORROSION AT STA 600, ABOVE STR 6R.
- [SDR 061140](https://openairdocs.org/sdr/061140.md): Frame · cracked · Apr 13, 2006 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > BULK PIT BS 2140 FUSELAGE FRAME WEB CRACKED AT RBL 18.
- [SDR 061139](https://openairdocs.org/sdr/061139.md): Doubler · damaged · Apr 13, 2006 · N716CK · Boeing 747122 · Nacelle/Pylon, Plate/Skin
  > 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.md): Stringer · cracked · Apr 12, 2006 · N716CK · Boeing 747122 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB UPPER STR 4 CRACKED AT STAB STA 260.
- [SDR 061136](https://openairdocs.org/sdr/061136.md): Bulkhead · dented · Apr 12, 2006 · N716CK · Boeing 747122 · Fuselage Main, Bulkhead
  > BS 2360 BULKHEAD HAS DENTS AT LBL 7.5, WL 347.
- [SDR 061135](https://openairdocs.org/sdr/061135.md): Bulkhead · dented · Apr 12, 2006 · N716CK · Boeing 747122 · Fuselage Main, Bulkhead
  > BS 2360 BULKHEAD HAS DENTS AT RBL 54, WL 313.
- [SDR 061134](https://openairdocs.org/sdr/061134.md): Stiffener · cracked · Apr 12, 2006 · N716CK · Boeing 747122 · Nacelle/Pylon Miscellaneous Structure
  > 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.md): Stringer · bent · Apr 12, 2006 · N716CK · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER IS BENT AT STA 1930, STR 1R.
- [SDR 061132](https://openairdocs.org/sdr/061132.md): Fitting · corroded · Apr 11, 2006 · N716CK · Boeing 747122 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER END FITTING IS CORRODED AT STA 1480, STR 47R.
- [SDR 061131](https://openairdocs.org/sdr/061131.md): Strap · corroded · Apr 11, 2006 · N716CK · Boeing 747122 · Fuselage Main, Frame
  > AFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.

Next page: https://openairdocs.org/deregistered/N716CK-2012-04-30/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 = 'N716CK' AND deregistration_id = 'N716CK-2012-04-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N716CK-2012-04-30/reports

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