N516MC, cancelled Jun 6, 2011

Service difficulty reports · 104

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P5CA0801556Duct · leakingWITH 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 PRApr 10, 2008 · N516MC · Boeing 747243B · Pneumatic SystemSDR P5CA0801555Seat Belt · missingAFTER 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.Apr 10, 2008 · N516MC · Boeing 747243B · Flight Compartment EquipmentSDR P5CA0701523Filter · cloggedON 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.May 17, 2007 · N516MC · Boeing 747243B · Fuel Controlling SystemSDR UIEA200700180Frame · crackedM/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.Apr 12, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700175Panel · crackedKEEL 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.Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, StructureSDR UIEA200700167Bear Strap · delaminatedM/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.Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR UIEA200700168Bear Strap · crackedM/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.Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR UIEA200700169Spar · crackedEMP 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.Apr 11, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer, Spar/RibSDR UIEA200700166Bear Strap · delaminatedM/DECK L3 DOOR AFT UPPER CORNER AREA DELAMINATED BEAR STRAP. OUT OF LIMIT DELAMINATION BEAR STRAP REPAIRED AS PER BOEING MSG 1-309886570-4.Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR UIEA200700200Keelbeam · corrodedKEEL 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.Apr 11, 2007 · N516MC · Boeing 747243B · Aerodynamic FairingsSDR UIEA200700199Keelbeam · corrodedKEEL 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.Apr 11, 2007 · N516MC · Boeing 747243B · Fuselage Main, KeelSDR UIEA200700181Frame · crackedLT S14 AREA FRAME CRACKED. CRACKED FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.Apr 10, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700151Support Channel · crackedLT STAB 344QBL PANEL AFT SUPPORT AREA FOUND CRACKED. REPLACED SUPPORT CHANNEL PER BOEING MESSAGE 1-307217093-2.Apr 10, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer StructureSDR UIEA200700149Channel · crackedRT STAB ACCESS PANEL 344 QBR OUTBOARD AFT CORNER PANEL SUPPORT FOUND CRACKED. REPLACED OUTBOARD AFT CORNER SUPPORT CHANNEL PER BOEING MESSAGE 1-307272180-2.Apr 10, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer StructureSDR UIEA200700174Support · corrodedFAIRING 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.Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700173Support · corrodedFX - 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.Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700170Panel · crackedM/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.Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700172Stringer · corrodedFX - STRINGER FOUND CORROSION CRACKED AT STA2260-S-51L. CORROSION CRACKED STRINGER, REPAIRED AS PER SRM 53-10-02.Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR UIEA200700202Keelbeam · corrodedKEEL 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.Apr 9, 2007 · N516MC · Boeing 747243B · Fuselage Main, KeelSDR UIEA200700186Plate · damagedM/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.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, StructureSDR UIEA200700178Doubler · crackedRT 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.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700176Plate · damagedM/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.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, StructureSDR UIEA200700160Support · corrodedFX - 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.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700155Seat Track · corrodedUPPER DECK STATION 685 RBL 27 SEAT TRACK CORRODED AS MARKED. REMOVED CORROSION PER SRM 53-10-05Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200700152Frame · crackedUPPER DECK STATION 740 STRINGER 6R FRAME CUTOUT CRACKED. REPAIRED STRINGER CUTOUT PER SRM 53-10-04 FIG 54.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700191Frame · crackedBS 360 LT S24A STRINGER CUT-OUT CRACKED. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307193755-1-2.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700194Spar · damagedNR 4 ENG LT LOWER SPAR CHORDS (SIDE COWL HINGE AREA) AFT AREA FOUND DAMAGED. DAMAGED WEB REPAIRED AS PER BOEING MSG 1-308420578-2.Apr 6, 2007 · N516MC · Boeing 747243B · Nacelle/Pylon, Frame/Spar/RibSDR UIEA200700196Frame · crackedRT 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.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700193Stringer · corrodedCABIN FLR SUPPORT BS 1283 RBL 117 CORROSION. OUT OF LIMIT, SUPPORT REPAIRED AS PER BOEING 1-310385513-2.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR UIEA200700189Frame · crackedM/D STA 360 S-23R FRAME STRINGER CUT-OUT CRACK. CRACKED FRAME REPAIRED AS PER BOEING MSG 1-307825515-2-1.Apr 6, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700154Frame · deformedMAIN DECK STATION 2000 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED FLANGE PER SRM 51-40-03 FIG 1.Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700156Bracket · crackedAFTER 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.Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, Attach FittingsSDR UIEA200700153Frame · deformedMAIN DECK STATION 1960 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED PER SRM 51-40-03 FIG 1.Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700190Shear Tie · crackedRT 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.Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting StructureSDR UIEA200700197Rib · crackedEMP LT STAB T/E RIB AT STAB BL421.5 WEB FOUND CRACKED. CRACKED WEB REPAIRED AS PER SRM 55-10-06 FIG 4.Apr 5, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer, Spar/RibSDR UIEA200700187Rib · crackedRHW 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.Apr 5, 2007 · N516MC · Boeing 747243B · Wing, Rib/BulkheadSDR UIEA200700192Frame · crackedM/D STA270 S-R13A AREA FRAME CRACK. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307196918-1-2.Apr 5, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700177Shear Tie · crackedRT 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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting StructureSDR UIEA200700179Frame · crackedLT 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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700163Vertical Beam · crackedNWW 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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, StructureSDR UIEA200700165Hinge Fitting · crackedEMP 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.Apr 4, 2007 · N516MC · Boeing 747243B · Horizontal Stabilizer StructureSDR UIEA200700164Door Frame · crackedRT 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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, StructureSDR UIEA200700198Frame · crackedM/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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA200700161Seat Track · corrodedCABIN TIE DOWN TRACK FLANGE CORRODED AT BS 1440-1480 RBL33. CORROSION SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 25.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200700195Shear Tie · crackedRT 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.Apr 4, 2007 · N516MC · Boeing 747243B · Fuselage Internal Mounting StructureSDR UIEA200700162Web · crackedM/D STA 360-380 S26R FLOOR WEB CRACK AT SKIN ATT AREA. CRACKED FLOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700158Attach Angle · crackedNR 2 PYLON CAP SKIN OUTBOARD LOWER ATTACH ANGLE FOUND CRACKED AS MARKED. REPAIRED AS PER SRM 54-11-02 FIG 7.Apr 3, 2007 · N516MC · Boeing 747243B · Nacelle/Pylon, Attach FittingsSDR UIEA200700157Support · crackedLEFT FUSE TO WING LOWER PANEL 191KL FAIRING SUPPORT FRAME AT STA 1241 FOUND CRACKED. FAIRING SUPPORT FRAME REPAIRED IAW SRM 51-40-03.Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700159Support · corrodedAIR-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.Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA200700188Web · crackedM/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.Apr 3, 2007 · N516MC · Boeing 747243B · Fuselage Miscellaneous Structure
Back to N516MC, cancelled Jun 6, 2011