# Service difficulty reports: N516MC, cancelled Jun 6, 2011

A list on [N516MC, cancelled Jun 6, 2011](https://openairdocs.org/deregistered/N516MC-2011-06-06.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 3 · 104 reports

- [SDR P5CA0801556](https://openairdocs.org/sdr/P5CA0801556.md): Duct · leaking · Apr 10, 2008 · N516MC · Boeing 747243B · Pneumatic System
  > WITH NR 2 ENGINE FIRE LOOP "B" ON DEFERRAL AND APPROXIMATELY 140NM OUT OF ICN AT FL29 LOOP "A" FIRE DETECTOR LIGHT AND FAULT LIGHT ILLUMINATED FOLLOWED BY FIRE WARNING BELLS. THE ENGINE WAS SHUTDOWN AND FIRE HANDLE PULLED WITH OUT DISCHARGING BOTTLES. OIL PR
- [SDR P5CA0801555](https://openairdocs.org/sdr/P5CA0801555.md): Seat Belt · missing · Apr 10, 2008 · N516MC · Boeing 747243B · Flight Compartment Equipment
  > AFTER PUSHBACK FLIGHT ENGINEER FOUND THE CROTCH SEATBELT MISSING FROM FIRST OBSERVER'S SEAT. AIRCRAFT CAME BACK TO GATE AND MAINTENANCE DEFERRED THE FIRST OBSERVER'S SEAT IAW MEL 25-23-1.
- [SDR P5CA0701523](https://openairdocs.org/sdr/P5CA0701523.md): Filter · clogged · May 17, 2007 · N516MC · Boeing 747243B · Fuel Controlling System
  > ON TAKEOFF, NR 2 ENGINE FLAMED OUT. ENGINE HAD SUCCESSFUL RESTART. INLET AND EXHAUST FEELING AND COMPRESSOR CHECKED SATIS NR 2 FUEL TANK WAS SUMPED THEN REPLACED NR 2 ENGINE FUEL FILTER. NO FURTHER PROBLEMS.
- [SDR UIEA200700180](https://openairdocs.org/sdr/UIEA200700180.md): Frame · cracked · Apr 12, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > M/D BS 1740 S-13R-S14R FRAME FOUND CRACKED AND DEFORMED. M/D BS 1740 S13R-S14R DAMAGE FRAME REPAIRED FROM S11R TO S15R/16R AS PER BOEING MSG 1-309862807-8.
- [SDR UIEA200700175](https://openairdocs.org/sdr/UIEA200700175.md): Panel · cracked · Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Structure
  > KEEL BEAM PANEL NR 191KK CRACKED AT RT FWD HINGE CUT-OUT AS MARK. CRACKED HINGE CUT-OUT SKIN REPAIRED AS PER SRM 51-40-02.
- [SDR UIEA200700167](https://openairdocs.org/sdr/UIEA200700167.md): Bear Strap · delaminated · Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/Skin
  > M/DECK R3 DOOR AFT UPPER CORNER AREA BEAR STRAP DELAMINATED. DELAMINATED BEAR STRAP CORROSION REMOVED, OUT OF LIMIT, REPAIRED AS PER BOEING MSG 1-30886570-4.
- [SDR UIEA200700168](https://openairdocs.org/sdr/UIEA200700168.md): Bear Strap · cracked · Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/Skin
  > M/DECK LT MED NR 3 CUT-OUT AFT UPPER CORNER SMALL STEEL DOUBLER 1 HOLE CRACK AT BEAR STRAP APPROX 0.030" LONG (AFTER CORNER REMOVED). CRACKED HOLE REPAIRED AS PER BOEING MSG 1-309886570-4, WORK DETAILS REF N.R C51491.
- [SDR UIEA200700169](https://openairdocs.org/sdr/UIEA200700169.md): Spar · cracked · Apr 11, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer, Spar/Rib
  > EMP LT HORIZ STAB HINGE FTG AREA FOUND NR 25 HOLE CRACK AT REAR SPAR UPPER CHORD APPROX 3/16" RUNNING O/B LOWER DIRECTION. REPAIRED AS PER BOEING MSG 1-305519321-7.
- [SDR UIEA200700166](https://openairdocs.org/sdr/UIEA200700166.md): Bear Strap · delaminated · Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/Skin
  > M/DECK L3 DOOR AFT UPPER CORNER AREA DELAMINATED BEAR STRAP. OUT OF LIMIT DELAMINATION BEAR STRAP REPAIRED AS PER BOEING MSG 1-309886570-4.
- [SDR UIEA200700200](https://openairdocs.org/sdr/UIEA200700200.md): Keelbeam · corroded · Apr 11, 2007 · N516MC · Boeing 747243B · Aerodynamic Fairings
  > KEEL BEAM PNL NR 191KK EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191KK OUT OF LIMIT HINGE AREA REPAIRED AS PER SRM 51-40-03 FIG 1 AND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UIEA200700199](https://openairdocs.org/sdr/UIEA200700199.md): Keelbeam · corroded · Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Keel
  > KEEL BEAM PNL NR 191HH EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191HH HINGE ATTACHMENT AREA OUT OF LIMIT, REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700181](https://openairdocs.org/sdr/UIEA200700181.md): Frame · cracked · Apr 10, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > LT S14 AREA FRAME CRACKED. CRACKED FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700151](https://openairdocs.org/sdr/UIEA200700151.md): Support Channel · cracked · Apr 10, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer Structure
  > LT STAB 344QBL PANEL AFT SUPPORT AREA FOUND CRACKED. REPLACED SUPPORT CHANNEL PER BOEING MESSAGE 1-307217093-2.
- [SDR UIEA200700149](https://openairdocs.org/sdr/UIEA200700149.md): Channel · cracked · Apr 10, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer Structure
  > RT STAB ACCESS PANEL 344 QBR OUTBOARD AFT CORNER PANEL SUPPORT FOUND CRACKED. REPLACED OUTBOARD AFT CORNER SUPPORT CHANNEL PER BOEING MESSAGE 1-307272180-2.
- [SDR UIEA200700174](https://openairdocs.org/sdr/UIEA200700174.md): Support · corroded · Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > FAIRING SUPPORT FRAME AT STA 880 LWR SIDE LBL 2 AND RBL 2 FOUND CORRODED. OUT OF LIMIT LWR CHORD REPAIRED AS PER SRM 53-50-04.
- [SDR UIEA200700173](https://openairdocs.org/sdr/UIEA200700173.md): Support · corroded · Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > FX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1160, LBL58-LBL68. CORROSION OUT OF LIMIT, FAIRING SUPPORT CHORD REPLACED AS PER SRM 51-10-01 PP AND INSTALL AS PER SRM 81-30-02.
- [SDR UIEA200700170](https://openairdocs.org/sdr/UIEA200700170.md): Panel · cracked · Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > M/DECK BS 1241-1250 LBL 75-97 CLOSE-OUT PANEL NEAR TRIM AIR DUCT FOUND CRACK. TRIM AIR DUCT CLOSE-OUT PANEL. REPLACED AS PER SRM 53-23-29 PART IV.
- [SDR UIEA200700172](https://openairdocs.org/sdr/UIEA200700172.md): Stringer · corroded · Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Main, Longeron/Stringer
  > FX - STRINGER FOUND CORROSION CRACKED AT STA2260-S-51L. CORROSION CRACKED STRINGER, REPAIRED AS PER SRM 53-10-02.
- [SDR UIEA200700202](https://openairdocs.org/sdr/UIEA200700202.md): Keelbeam · corroded · Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Main, Keel
  > KEEL BEAM PNL NR 191JJ INTERIOR SURFACE CORROSION REVEALED AT SEVERAL LOCATIONS. KEEL BEAM PANEL NR 191JJ INTERIOR SUPPORT REPLACED AS PER SRM 51-10-01 PP AND INSTALLED AS PER SRM 51-30-02.
- [SDR UIEA200700186](https://openairdocs.org/sdr/UIEA200700186.md): Plate · damaged · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Structure
  > M/D BS 940 LT TENSION TIE STEEL PLATE FASTENER HOLE 1 FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE STEEL PLATE REPAIRED AS PER BOEING MSG 1-30-3983211-2-1 AND 4 FIG 3.
- [SDR UIEA200700178](https://openairdocs.org/sdr/UIEA200700178.md): Doubler · cracked · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > RT BS 900 TENSION TIE AREA HOLE NR 5 FOUND CRACKED AT FRAME DOUBLER, INSULATION BLANKET HOLE FOUND CRACKED AT FRAME DOUBLER BETWEEN S-8R TO S-9R AND S-10R TO S-10AR. FRAME DOUBLER REPAIRED AS PER BOEING MSG 1-306586780-2.
- [SDR UIEA200700176](https://openairdocs.org/sdr/UIEA200700176.md): Plate · damaged · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Structure
  > M/DECK BS940 RT TENSION TIE STEEL PLATE FASTENER HOLE 2 FOUND SHORT EDGE MARGIN AT UPPER ROW MOST O/B. REPAIRED AS PER BOEING MSG 1-303983211-1-2, FIG 3.
- [SDR UIEA200700160](https://openairdocs.org/sdr/UIEA200700160.md): Support · corroded · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > FX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1050 LBL 12, LBL 28 (191AL FRG ATTACH AREA). OUT OF LIMIT FAIRING SUPPORT LWR CHORD LWR FLANGE REPAIRED AS PER SRM 53-50-06 FIG 2.
- [SDR UIEA200700155](https://openairdocs.org/sdr/UIEA200700155.md): Seat Track · corroded · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage, Seat/Cargo Attach Fittings
  > UPPER DECK STATION 685 RBL 27 SEAT TRACK CORRODED AS MARKED. REMOVED CORROSION PER SRM 53-10-05
- [SDR UIEA200700152](https://openairdocs.org/sdr/UIEA200700152.md): Frame · cracked · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > UPPER DECK STATION 740 STRINGER 6R FRAME CUTOUT CRACKED. REPAIRED STRINGER CUTOUT PER SRM 53-10-04 FIG 54.
- [SDR UIEA200700191](https://openairdocs.org/sdr/UIEA200700191.md): Frame · cracked · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > BS 360 LT S24A STRINGER CUT-OUT CRACKED. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307193755-1-2.
- [SDR UIEA200700194](https://openairdocs.org/sdr/UIEA200700194.md): Spar · damaged · Apr 6, 2007 · N516MC · Boeing 747243B · Nacelle/Pylon, Frame/Spar/Rib
  > NR 4 ENG LT LOWER SPAR CHORDS (SIDE COWL HINGE AREA) AFT AREA FOUND DAMAGED. DAMAGED WEB REPAIRED AS PER BOEING MSG 1-308420578-2.
- [SDR UIEA200700196](https://openairdocs.org/sdr/UIEA200700196.md): Frame · cracked · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > RT BS 900 TENSION TIE AREA NR 5 HOLE FOUND CRACK AT FRAME WEB THRU THICKNESS RUNNING I/B AND NR 10 HOLE FOUND CRACK AT FRAME WEB APPROX 0.060" IN LENGTH RUNNING DOWNWARD. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-306586780-2.
- [SDR UIEA200700193](https://openairdocs.org/sdr/UIEA200700193.md): Stringer · corroded · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Longeron/Stringer
  > CABIN FLR SUPPORT BS 1283 RBL 117 CORROSION. OUT OF LIMIT, SUPPORT REPAIRED AS PER BOEING 1-310385513-2.
- [SDR UIEA200700189](https://openairdocs.org/sdr/UIEA200700189.md): Frame · cracked · Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > M/D STA 360 S-23R FRAME STRINGER CUT-OUT CRACK. CRACKED FRAME REPAIRED AS PER BOEING MSG 1-307825515-2-1.
- [SDR UIEA200700154](https://openairdocs.org/sdr/UIEA200700154.md): Frame · deformed · Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > MAIN DECK STATION 2000 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED FLANGE PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700156](https://openairdocs.org/sdr/UIEA200700156.md): Bracket · cracked · Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, Attach Fittings
  > AFTER REMOVAL OF PAX DECK SPLICE FITTING AT STATION 1416 LBL 2 IN THE BLG WHEEL WELL IS FOUND CRACKED. REPLACED FITTING PER SRM 51-10-01 PAGE 9.
- [SDR UIEA200700153](https://openairdocs.org/sdr/UIEA200700153.md): Frame · deformed · Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > MAIN DECK STATION 1960 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700190](https://openairdocs.org/sdr/UIEA200700190.md): Shear Tie · cracked · Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting Structure
  > RT BS 940 TENSION TIE AREA HOLE NR 16 FOUND CRACKED AT AFT CHANNEL APPROX 0.060" RUNNING INBOARD LWR. CRACKED AFT CHANNEL REPAIRED AS PER BOEING MSG 1-303983211-2-2-4.
- [SDR UIEA200700197](https://openairdocs.org/sdr/UIEA200700197.md): Rib · cracked · Apr 5, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer, Spar/Rib
  > EMP LT STAB T/E RIB AT STAB BL421.5 WEB FOUND CRACKED. CRACKED WEB REPAIRED AS PER SRM 55-10-06 FIG 4.
- [SDR UIEA200700187](https://openairdocs.org/sdr/UIEA200700187.md): Rib · cracked · Apr 5, 2007 · N516MC · Boeing 747243B · Wing, Rib/Bulkhead
  > RHW NR 23 VC FLAP I/B ARM ROTARY ATT RIB AT OLES 1278 I/B FACE FOUND CRACKED AT "D" HOLE FWD STIFFENER AREA. CRACKED RIB "D" HOLE REPAIRED AS PER BOEING MSG 1-308409234-2.
- [SDR UIEA200700192](https://openairdocs.org/sdr/UIEA200700192.md): Frame · cracked · Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > M/D STA270 S-R13A AREA FRAME CRACK. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307196918-1-2.
- [SDR UIEA200700177](https://openairdocs.org/sdr/UIEA200700177.md): Shear Tie · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting Structure
  > RT BS 860 TENSION TIE AREA HOLE NR 6 FOUND CRACKED AT AFT CHANNEL APPROX 0.060" IN LENGTH RUNNING UPWARD. RT BS 860 TENSION TIE CRACKED AFT CHANNEL, REPAIRED AS PER BOEING MSG 1-306486452-2.
- [SDR UIEA200700179](https://openairdocs.org/sdr/UIEA200700179.md): Frame · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > LT BS 200 FRAME IS FOUND CRACKED AT 11EA FASTENER HOLES BETWEEN S13L AND S14L. CRACKED FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700163](https://openairdocs.org/sdr/UIEA200700163.md): Vertical Beam · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, Structure
  > NWW RT VERTICAL BEAM WEB AT BS 280 WL 170-180 LOWER STAND OFF HOLE FOUND CRACK APPROX 1/8" LONG. CRACK WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UIEA200700165](https://openairdocs.org/sdr/UIEA200700165.md): Hinge Fitting · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer Structure
  > EMP LT HORIZ STAB C/S STAB HINGE NR 28 HOLE FOUND CRACK AT HINGE FTG 11 O/C POSITION APPROX 1/8" LONG. REPAIRED AS PER BOEING MSG 1-305519321-7.
- [SDR UIEA200700164](https://openairdocs.org/sdr/UIEA200700164.md): Door Frame · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, Structure
  > RT NR 1 MED NR 9 DOOR STOP FTG AREA FOUND CRACK AT BS 488 FRAME WEB TOOLING HOLE APPROX 1/16" AND 1/8" LONG. RT NR 1 MED NR 9 DOORS STOP FTG AREA CRACK WEB REPAIRED AS PER SRM 53-10-04 FIG 121.
- [SDR UIEA200700198](https://openairdocs.org/sdr/UIEA200700198.md): Frame · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, Frame
  > M/D LT BS 200 FRAME INNER CHORD IS FOUND CRACKED AT 1 FASTENER HOLE BETWEEN S13L AND S14L. CRACKED INNER CHORD REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UIEA200700161](https://openairdocs.org/sdr/UIEA200700161.md): Seat Track · corroded · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage, Seat/Cargo Attach Fittings
  > CABIN TIE DOWN TRACK FLANGE CORRODED AT BS 1440-1480 RBL33. CORROSION SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 25.
- [SDR UIEA200700195](https://openairdocs.org/sdr/UIEA200700195.md): Shear Tie · cracked · Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting Structure
  > RT BS 860 TENSION TIE AREA HOLE NR 5 FOUND CRACKED AT FWD CHANNEL APPROX 0.030" ON LENGTH RUNNING UPWARD. CRACKED TENSION TIE FWD CHANNEL REPAIRED AS PER BOEING MSG 1-306484452-2.
- [SDR UIEA200700162](https://openairdocs.org/sdr/UIEA200700162.md): Web · cracked · Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > M/D STA 360-380 S26R FLOOR WEB CRACK AT SKIN ATT AREA. CRACKED FLOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.
- [SDR UIEA200700158](https://openairdocs.org/sdr/UIEA200700158.md): Attach Angle · cracked · Apr 3, 2007 · N516MC · Boeing 747243B · Nacelle/Pylon, Attach Fittings
  > NR 2 PYLON CAP SKIN OUTBOARD LOWER ATTACH ANGLE FOUND CRACKED AS MARKED. REPAIRED AS PER SRM 54-11-02 FIG 7.
- [SDR UIEA200700157](https://openairdocs.org/sdr/UIEA200700157.md): Support · cracked · Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > LEFT FUSE TO WING LOWER PANEL 191KL FAIRING SUPPORT FRAME AT STA 1241 FOUND CRACKED. FAIRING SUPPORT FRAME REPAIRED IAW SRM 51-40-03.
- [SDR UIEA200700159](https://openairdocs.org/sdr/UIEA200700159.md): Support · corroded · Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > AIR-CONDITIONING BAY FAIRING SUPPORT FOUND CORRODED AS MARKED AT STA 1110 LBL 12 (191EL FAIRING ATTACH AREA). REMOVED CORROSION AND REPAIRED PER SRM 53-50-04 FIG 2.
- [SDR UIEA200700188](https://openairdocs.org/sdr/UIEA200700188.md): Web · cracked · Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
  > M/D STA 340-360 S-26R FLR WEB CRACK AT SKIN ATT AREA. CRACKED FLOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.

Next page: https://openairdocs.org/deregistered/N516MC-2011-06-06/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 = 'N516MC' AND deregistration_id = 'N516MC-2011-06-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N516MC-2011-06-06/reports

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