N416MC
Service difficulty reports · 173
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 = 'N416MC' AND registry_match = 'registration' 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.
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 = 'N416MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2026092200907Display · failedFO INBOARD IDU SHOWED GARBLED INFO. R & R FO NAV DISPLAY IAW AMM 31-61-02 AND IPC 31-61-01A. OPS CHECK GOOD.</P>)SDR UIEA2026081000719Fitting · crackedFOUND LUG FITTING CRACK AT FWD CARGO, BS 1000, LBL 11.33. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0, REV 107. INSTALLED NEW PART IAW SRM 51-40-02-0G-0, REV 107 AND REF EO 4453C024, PART 3, REV 4. CONDITION CHKD NORMAL.SDR UIEA2026081000721Shear Tie · crackedFOUND SHEAR TIE CRACK AT STA 1000 RBL 33, FWD CGO. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 107. PERFORMED EI T2026A53M-1419, REV 0, AND REF EO 4453C024, PART 8, REV 4. ACCOMPLISHED EI T2026A53M-1419, REV 1. CONDITION CHKD NORMAL.SDR UIEA2026081000722Seat Track · crackedFOUND SUBSTITUTE SEAT TRACK SURFACE CRACKED AT M/D BS 1000, LBL 75.92. REMOVED DAMAGED TRACK IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 64525, SRM 53-00-52-2R-13, REV 107. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B82SDR UIEA2026081000723Cargo Track · brokenFOUND FWD CARGO TRACK BROKEN BS 560, LBL 24.75. REMOVED DAMAGED IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60524, SRM 53-00-52-2R-10 REV 107, & EI T2026A53M-1614, REV 0. INSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B12300SDR UIEA2026081000724Spar Web · noneFOUND EXISTING REPAIR ON VERTICLE STAB REAR SPAR WEB BETWEEN VSS 205 - VSS 220. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60564 SRM 55-30-10-2R-2 REV 107. CHKD NORMAL.SDR UIEA2026081000734Bulkhead · modificationPERFORMED BS 2598 BULKHEAD MODIFICATION, FOUND DEVIATION AT DOUBLER. ACCOMPLISHED EI T2026A53M-1528, REV 1, AND EI T2026A53M-1439, REV 1. CHECKED NORMAL.SDR UIEA2026081000735Repair · noneEXISTING REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE. PERFORMED PERMANENT REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE, WBL 563 IAW SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0, REV 107. CONDITION CHECK IS SATISFACTORY. REPAIR PROCESS REFER TO J/C ATTACHING SHSDR UIEA2026081000736Splice Angle · crackedCRACK, PERFORMED SB 4453B761, PART 1-2. FOUND A CRACK AT BS 2598, S11R, RT FWD LWR FITTING AREA. ACCOMPLISHED EI 2026A53M-1510, REV 2, AND DWG 65B02706, SH 24, REV A, AND DWG 65B02597, SH 2 REV H, AND DWG 65B02509, SHT 3, REV R. CHECKED NORMAL.SDR UIEA2026081000737Angle · corrodedFOUND CORROSION ON THE UPPER ANGLE BS 1030, LBL 11.33. ACCOMPLISHED W/S 60551 IAW SRM 53-40-52-2R-3, REV 107. & EI T2026A53M-1522, REV 1. CHECKED NORMAL.SDR UIEA2026081000738Repair · nonePERFORMED UPGRADE TIME-LIMITED REPAIR ON SEC 48 FUSELAGE SKIN AT BS 2600, S51R. ACCOMPLISHED EI T2026A53M-1409, REV 1, AND DWG 65B02509, SH 9, REV C, AND DWG 65B02700, SH 2, REV G, SH 6, REV -. CHECKED NORMAL.SDR UIEA2026050500295Signal Cond Unit · faultedHIGH SPEED RTO AT 140KTS INDICATED DUE TO ENG NR 1 NOT MAKING T/O THRUST. R & R N1 FAN SHAFT SPEED SENSOR & ENG IDLE RUN CHKD OK IAW AMM 77-12-01/401, AMM 71-00-00/501 & IPC 77-12-01-01. NEED THE ENG HIGH PWR CHK. R & R AVM SIGNAL CONDITIONER THEN OPS CHKD OSDR UIEA2025061400773Tire · failed#10 MLG TIRE FAILURE ON LANDING. R/R #9 & #10 MLG WHEEL ASSY PER AMM 32-45-01/401 & AIPC 32-45-03-02. FOUND DAMAGE ON RIGHT BODY GEAR DOOR (OUTBOARD). REPLACED DOOR PER AMM 32-14-02. RIGHT BODY GEAR STRUT DOOR DAMAGED. REPLACED PER AMM 32-14-06. DAMAGE AT R/HSDR UIEA2025052300679Switch · inoperativeBLEED 2 OVHT / PRV EICAS MSG. QRH PROCEDURE IND NO NAI AVAILABLE FOR ENG #2.(<P>REMOVED AND REPLACED BLEED 2 OVHT SWITCH REF AMM 36-22-01 & AIPC 36-22-01-01, OPS CHECK GOOD. NO LEAKS DETECTED. PERFORMED MPA RUN AS REQUESTED, NO FAULTS FOUND REF AMM 71-00-00-71SDR UIEA2024092300930Switch · no discrepancyBLD 4 OVHT/PRV EICAS MSG. REPEAT ISSUE SEE LG PAGE 1858928.(<P>MSG 36044. PERFORMED WIRING CHECK BTWN ASCTU & OVERTEMP SW, RESULT GOOD. R/R ASCTU & GND TEST / OPS CHECK GOOD PER AMM 36-11-30 & IPC 36-11-30-01A. ENG RUN UP PERFORMED AND NO DEFECTS NOTED PER AMMSDR UIEA2024092300915Switch · faultedBLD 4 OVHT/PRV EICAS MSG. QRH C/W(<P>R/R OVERTEMP SW IAW AMM 36-22-01 & IPC 36-22-01-01. LEAK & OPS CHECK GOOD.</P>)SDR UIEA2024081400827Pin · corrodedATB, HYD SYS 4 QTY INDICATION LOW #4. A/C ARRIVED WITH 0.75 ON THE #4 HYD SYS. PLACED LOAD ON SYS WITH NO VISUAL HYD LEAKS ANYWHERE AND A STEADY QTY IND SYS 1 & 2 ARE AT 1.20 AND 3 AT 0.97.(<P>R/R THE CORRODED PIN, CLEAN & RECONNECT. C/W FLUID TRANSFER PER AMMSDR UIEA2024061400520Stringer · cracked#3 PYLON - I/B LOWER STRINGER CRACK FOUND AT MOST AFT END AREA (APPROX NAC STA 374) AS MARKED(<P>3 PYLON - I/B LOWER STRINGER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 REV 101 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024061400521Structure · corrodedCENTER SECTION AFT FACE FOUND CORROSION ( NEAR LH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED. REMAIN 0.783" ORG 0.806" WIDTH 1.4, LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWASDR UIEA2024061400522Structure · corrodedCENTER SECTION AFT FACE CORROSION ( NEAR RH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED : REMAIN 0.755" ORG 0806, WIDTH 1.4" LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DASDR UIEA2024061700526Structure · crackedBS 2598 LH LOWER INNER CHORD 1EA CRACK FOUND ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) AT 2 O'CLOCK POSITION WITH THROUGH THICKNESS CRACK(<P>BS 2598 LH LOWER INNER CHORD 1EA CRACK ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) REPAIRED IAW RI-53-00-16937 RESDR UIEA2024061800535Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800536Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800538Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024061800548Frame · unknownMAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 INSPECTION THE SCREW CANNOT BE INSTALLED AFTER MOVED DUE TO BRACKET BLOCKED(<P>MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 SCREW CANNOT BE INSTALLED. CASE REPAIRED IAW RI-53-60-16951 REV A AND SB 747-53SDR UIEA2024061800549Support Rod · damagedLH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) FOUND HOLE ELONGATED(<P>LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) ROD FITTING FABRICATED IAW RI-57-22-16946 REV A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 101 DATE 20SDR UIEA2024061900556Skin · chafedLHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SEVERAL CHAFING MARKS(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16950 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024062000558Panel · corrodedM/D BELOW FSK STOWAGE PNL FOUND CORROSION(<P>M/D - BELOW FSK STOWAGE PNL REPAIR IAW FVCI EO - 24090-1, 2A, 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024022400126Socket · shortedVIA SATCOM, CREW REPORTED INFLIGHT ELECTRICAL ODOR CORRESPONDING TO AN UN-COMMANED ILLUMINATION OF CEILING LIGHT IN THE GALLEY / LAV AREA. CREW REPORTED STRONG ODOR, BUT NOTED NO C/B OPENED.(<P>REMOVED UPPER DECK CEILING LIGHT COVER IAW AMM 33-28-01 AND FOUND SDR UIEA2024012100020Floor Panel · damagedM/D STA 1850-1920 LBL 78-99 BALL MAT FLOOR PNL FOUND DAMAGE(<P>THE DAMAGED CASTER PANEL TOP SKIN REPAIR HAS BEEN CARRIED OUT PER EO.4425A500 REV.1</P>)SDR UIEA2023061600647Shutoff Valve · unknownITEM 1: AIR TURNBACK DUE TO COCKPIT AND UPPER DECK TEMPERATURES CONTINUALLY DROPPING. FLT DECK SET AT 29C, FWD DECK SET AT 15C, UPPER DECK 8C & CREW REST AT 3C.(<P>REMOVED AND REPLACED FWD TRIM AIR SHUTOFF VALVE PER AMM 21-28-04, TEST PASSED.</P>)SDR UIEA2022120701206Engine · stalledNR 2 ENGINE N2 VIBRATION 5.0 AND NR 2 COMPRESSOR STALLED ON CLIMB OUT. R & R NR 2 ENGINE IAW WORD CARD 71-099-02-01. OPS CHECK GOOD</P>)SDR UIEA2022060200568Indicator · fault messageENGINE #2 OIL QUANTITY INDICATED 19 PRIOR TO START, 14 AFTER START, 10 AT THE TOP OF THE CLIMB, AND DECREASED TO 7 BY LANDING AFTER 2:51 FLIGHT TIME. RETURNED TO RKSI WITH ENGINE #2 AT IDLE POWER. REMOVED AND REPLACED WITH NO.2 ENG AND THEN LEAK CHECK NORMAL SDR UIEA2022051700486Plate · migratedR/H W/W STA 1350 WING LANDING GEAR SUPPORT BEAM SPLICE LOWER PLATE AFT I/B CORNER SHIM MIGRATED. SHIM MIGRATION INSPECTION PER SRM 51-20-08, MOUNT BOLT TORQUE CHECK PERFORMED PER SRM 51-40-04-0G-0, EDGE SEALEANT APPLIED PER AMM 51-31-01.SDR UIEA2022052200493Attach Plate · corrodedR/H WLG W/W STA 1241 R/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITSSDR UIEA2022052200494Attach Plate · corrodedL/H WLG W/W STA 1241 L/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS.SDR UIEA2022052200495Attach Angle · crackedM/D RHS STA 960 S-7 FRAME FWD / CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED ANGLE P/N: 65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02 REV 94 DATE 20FEB2022</P>)SDR UIEA2022052200496Skin · cracked#4 ENG R/H CORE COWL LWR AREA OF AIR EXHAUST FOUND 2EA BOLT HOLE CRACKED SKIN 2EA BOLT HOLE CRACK AREA REPAIRED AS PER SRM 54-45-01-2R-4 REPAIR 4 FIG 201</P>)SDR UIEA2022052200497Skin · crackedL/H BLG I/B STRUT DOOR SKIN FOUND CRACK. SKIN CRACK AREA REPAIRED AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201 REV 94 DATE 20FEB 2022SDR UIEA2022052200498Attach Angle · crackedM/D LHS STA 960 S-7 FRAME FWD/ CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED AND P/N NO.65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02</P>)SDR UIEA2022052300499Beam · elongatedAFT CGO STA 1820-1840 MOST RH HORIZ TORQUE TUBE R/H SUPPORT BEARING ATTACHED BEAM FOUND HOLE ELONGATED. HOLE ELONGATED INTERCOSTAL LOCAL FABRICATED AS PER BOEING DWG: 65B06061 & RPL AND INSTALLED AS PER SRM 51-40-02SDR UIEA2022052300500Panel · crackedLHW TE CAVITY LWR FIXED PANEL CHORD FOUND CRACKED AT WS 1470 CHORD LOCAL FABRICATED AS PER BOEING DWG : 65B08175 AND PART LIST AND CHORD INSTALLED AS PER SRM 51-40-02SDR UIEA2022052300501Curtain · tornBULK CARGO STA 2160 CURTAIN FOUND LWR AREA TORN. PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-15628 REV.A</P>)SDR UIEA2022052300502Frame · chipped#3 ENG R/H CORE COWL NO.5 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED. FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG. 201 REV 94, DATE: 20 FEB 2022</P>)SDR UIEA2022052300503Cowling · gouged#3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022</P>)SDR UIEA2022052300504Frame · chipped#4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022SDR UIEA2022052300528Flap · chafedLHW O/B FORE FLAP T/E UPR SURFACE O/B AREA FOUND CHAFING AS MARKED (3" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB 20/2022</P>)SDR UIEA2022052400529Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (125" TO I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)SDR UIEA2022052400530Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (22" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)SDR UIEA2022052400531Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (145" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)
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