N445MC
Service difficulty reports · 73
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 = 'N445MC' 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 = 'N445MC' 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 UIEA2026053000371Fmu · faultedENG 2 DUE TO ABNORMAL INDICATIONS AND UNRESPONSIVE THRUST LEVER. (ENG 2 WAS SHUT DOWN IN FLIGHT) R & R NR 2 ENG FMU PER AMM 73-21-01-401 AND IPC 73-21-01-05. OPS CHECK GOOD. NO LEAK NOTED. FOLLOWED FIM 71-00-00-104B)SDR UIEA2025091801240Windshield · failedRIGHT FORWARD OUTER WINDSHIELD BROKE. R & R RIGHT FORWARD WINDSHIELD ASSY IAW AMM 56-11-00. OPS CHK OK.SDR UIEA2025071300946B-Nut · looseDURING FLIGHT, #2 OIL QUANTITY FELL TO 0, NO OTHER ABNORMAL INDICATIONS WERE NOTED AT THE TIME. ABOUT 2 HRS LATER, OIL PRESS BEGAN TO DECREASE, #2 ENG SHUTDOWN DUE TO "ENG 2 OIL PRESS" EICAS MSG WHEN THROTTLES WENT TO IDLE AT DESCENT. OIL PRESS DROPPED TO NEARSDR UIEA2025070600836Skin · delaminatedRHW I/B FORE FLAP L/E MID AND O/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600837Skin · delaminatedLHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600838Skin · delaminatedLHW I/B FORE FLAP O/B OF MID FORE FLAP TRACK APPROX 9" L/E AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600839Skin · delaminatedLHW I/B FORE FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600840Skin · delaminatedLHW I/B FORE FLAP I/B OF FORE FLAP TRACK CUTOUT FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600843Brace · chafedNO.1 PYLON DIAGONAL BRACE RH BELOW HYD DEPRESSURIZATION MODULE FOUND CHAFING.(<P>#1 PYLON DIAGONAL BRACE CHAFING AREA SMOOTHED AS PER RI-54-50-17750 REV.A. (AFTER SMOOTH OUT AREA MEASURED: L=2", W=1.25" & D=0.125"). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070700853Fairing · delaminatedDORSAL FAIRING FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW RI-55-30-17752 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070900876Channel · crackedLH HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT U CHANNEL FOUND CRACKED.(<P>LH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL REPLACED AS PER RI-55-10-17767 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070900877Door · chafed#2 PYLON LH AFT FAIRING DOOR FOUND CHAFFING.(<P>PERFORMED REPAIR AT CHAFFING AREA IAW <SPAN>RI-54-50-17761, REV. A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025070900882Skin · dentedFX STA 520-540 R/H S43R - S44R SKIN FOUND DENT.(<P>FX STA 520-540 R/H S43R-S44R SKIN DENT AREA REPAIRED AS PER SRM 53-00-01-2R-1 REQ 104. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000889Stiffener · crackedLHW L/E LOWER CENTER ZEE STIFFENER FOUND CRACKED.(<P>LHW L/E LOWER CENTER ZEE STIFFENER REPLACED AS PER RI-57-26-17755 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000890Panel · crackedNO.4 PYLON O/B #482KR PANEL FOUND CRACKED.(<P>NO.4 PYLON O/B #482KR PANEL REPLACED AS PER RI-54-50-17765 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000891Beam · damagedNO.4 PYLON AFT FAIRING AREA APPROX WAC STA 415 UPPER BEAM RH FASTENER HOLE FOUND ELONGATED(<P>OVERSIZE FASTENER HOLE AND INSTALL FREEZE PLUG PER RI-54-50-17760 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000892Rib · crackedLHW L/E #581HB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581HB PANEL RIB REPLACED AS PER RI-57-51-17762 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000894Rib · crackedLHW L/E #581JB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581JB PANEL RIB REPLACED AS PER RI-57-51-17769 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071200937Fuel Tank · corrodedLWLG W/W CENTER TANK AFT B/H FUEL BONDING ATTACH AREA SURFACE CORROSION.(<P><SPAN>LWLG W/W CENTER TANK AFT B/H FUEL BONDING AREA </SPAN>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10 ASDR UIEA2025032500388Wire · damagedHYD CONTROL 4 ADVISORY MSG IN FLIGHT. CHECKLIST C/W. AIR TURNBACK TO KMIA.(<P>REPLACED WIRE W4261-434-24R AND 24B PER WDM 29-30-11 AND SWPM 20-10-13. TEST GOOD PER AMM 29-31-00.</P>)SDR UIEA2025021600149Pcu · faultedRT INBOARD AILERON INDICATION MISSING. FLT CONTROL HYD POWER WING SHUTOFF SWITCHES SELECTED TO CLOSED ON P61 PANEL.(<P>1.PARTIALLY REMOVED INBD ALERON POWER CONT PACKAGE PER AMM 27-11-12-002-001 STEP F(1)(I). ACCOMPLISHED REMOVAL OF INBD AILERON AS PER AMM 2SDR UIEA2024041000268Roller Cam · unknownAFTER TAKE OFF AT 2500 FT, DOOR ENTRY L1 EICAS MESSAGE. ACFT PRESSURIZING NORMALLY. 2 VERY LOUD BANGS, SHOOK FLIGHT DECK DOOR. FOUND L1 DOOR UPPER FWD & AFT CRANK ROLLER CAM ASSY BROKEN. CRANK ROLLER CAM ASSY REPLACED. L1 DOOR FUNCTION CHK GOOD IAW AMM 52-1SDR UIEA2023071000735Unknown · unknownCRACK DAMAGE ON THE WEB OF STA 2231 FRAME AT S-21L AND S-22L(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-06-0. REV 97. 2. REPAIRED DAMAGE AREA IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203 PARAGRAPH 5 REV 97. 3. INSTALLED FASTENERS IAW SRM 57-40-0SDR UIEA2023071000736Unknown · unknownREPAIR - SKIN MODIFICATION FOR STATION 1640 TO 1740 LEFT SIDE AT STRINGER 34 PER SB 747-53A2487(<P>1. ACCOMPLISHED JOB IAW EI T2023A53M-1374 REV 1. 2. ACCOMPLISHED EI 72023A53M-1374 REV 2. 3. JOB ACCOMPLISHED AND COND CHK NORMAL.</P>)SDR UIEA2023071000737Unknown · unknownCRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL AT STA 740 RH SIDE(<P>1. REMOVED AFFECTED FASTENER TO GET ACCESS IAW 51-40-02-0G-0. REV 97. 2. PERFORM EI T2023A53M-1451 REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0. REV 97 AND DWG 14241023 SSDR UIEA2023071000738Unknown · unknownCRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL STA 760 RH SIDE(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0, REV 97. 2. PERFORM EI T2023A53M-1450, REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 97 AND DWG 1424102SDR UIEA2023071000739Unknown · unknownFWD FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 LBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV97. 2. REPAIR SUBSTITUTE TRACK IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97 AND DSDR UIEA2023071000740Unknown · unknownDUE TO EO INSP WASHERS WERE NOT FOUND UNDER EACH FASTENER HEAD. REQUEST ADD EO PART 2 AND PART 5. PERFORMED NOSE WW FWD CORNER DOUBLER MODIFICATION NEAR STA 240, S-39 TO S-45(<P>1. PERFORM EI T2023A53M-1504 SEQUENCE A REV 0. 2. ACCOMPLISHED REPAIR AREA IAW EI SDR UIEA2023071000741Unknown · unknownFOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1540 RBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98 AND DWG 65B382SDR UIEA2023071000742Unknown · unknownFOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA1641 LBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98 AND DWG 65B3825SDR UIEA2023071000743Unknown · unknownGOUGE DAMAGE ON RH WING LOWER SKIN PANEL NO.2 BETWEEN STRINGER L-8 AND L-9 AT WBL 743.828(<P>1. ACCOMPLISHED EI T2023A57M-1479. SEQUENCE B REV 1. 2. ACCOMPLISHED EI T2023A57M-1479, REV 2. 3. JOB COMPLETED AND COND CHK NORMAL.</P>)SDR UIEA2023071000744Shear Tie · unknownCRACK ON THE SHEAR TIE AT 1000 LBL 33.99 SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 8 & 9 REV 0 AND IAW EO 4453C024 PART 4 REV 3. 3. ACCOMPLISHED EI NO T2023A53M.1550 RESDR UIEA2023071000745Shear Tie · unknownCRACK ON THE SHEAR TIE AT STA 1000 RBL 33.99 SB 747 53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51.40.02.0G.0 REV 97. ACCOMPLISHED EI T2023A53M-1550 REV 0, SB 747-53A2924 FIG 21, 22 REV0 AND EI ATTACHED TO W/O 8402500 (319) AND IAW EO 4453C024 PART 8 REV 3. 3. JSDR UIEA2023071000746Fitting · unknownCRACK ON THE INTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33, SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI NO T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 17 & 18 REV 0 AND EI ATTACHED TO W/O 8402504 (319) AND EO 4453CSDR UIEA2023071000747Cap · unknownCORROSION - FOUND MAIN DECK CGO FLOOR BEAM CAP CORROSION STA 2360 RBL 3.(<P>1. REMOVED DAMAGE PARTS IAW 51-40-02-0G-0 REV98. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV98 AND BOEING DWG NO. 65B02634 SH 22 REV 4 AND DNG NO 65B06161 SH2 REV E, DWG NO. 65B3875SDR UIEA2023071000748Fitting · unknownCORROSION - 2EA CGO TRACK CORROSION AT R/H STA 2360 MAIN DECK FLOOR(<P>1. IAW AMM SUBTASK 53-44-00-212-001, REV107 REMOVE CGO TRACK 2. IAW AMM SUBTASK 53-44-00-020-001 REV 107 AND REFRENCE EI T2023A53M-1566, REV 0. INSTALL CGO TRACK. 3. JOB COMPLETED AND COND SDR UIEA2023071000749Unknown · unknownFOUND #1 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008, REV 107 R/R #1 FLAP TRACK INBD SIDE LOAD FIG. 2. REFRENCE EI NO. T2023A57M-1497 REV 1 SEQUENCE A REPAIR #1 FLAP TRACK. 3. CONDITION CHECKSDR UIEA2023071000750Unknown · unknownFOUND #8 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #8 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFRENCE EI. NO: T2023A57M-1501 REV1 SEQUENCE A REPAIR #8 FLAP TRACK. 3. CONDITION CHECKSDR UIEA2023071000751Unknown · unknownFOUND #3Â FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #3 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFRENCE EI NO. T2023A57M-1498 REV1 SEQUENCE A REPAIR #3 FLAP TRACK. 3. CONDITION CHK NORMSDR UIEA2023071000752Unknown · unknownFOUND #6 FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008, REV107 R/R #6 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFERENCE EI NO. T2023A57M-1499 REV1 SEQUENCE A REPAIR #6 FLAP TRACK. 3. CONDITION CHECK NOSDR UIEA2023071000753Unknown · unknownFOUND #7 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #7 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFERENCE EI NO. T2023A57M-1500 REV1 SEQUENCE A REPAIR NO.7 FLAP TRACK. 3. CONDITION CHESDR UIEA2023071000754Charger · unknownFOUND EMERGENCY LIGHT BATTERY PACK (MJ120) FUNCTION FAIL.(<P>1. IAW AMM 33-51-04-002-009-001 & 33-51-04-402-012-001 REV.107. REPLACED POWER SUPPLY (MJ170). 2. IAW AMM 33-51-04-402-012-001 REV 107. PERFORMED EMERGENCY LIGHT POWER. SUPPLY INSTALLATION TEST AND TSDR UIEA2023081500777Window · unknownCAPT SIDE REAR MOST WINDOW SQUEALING AND VIBRATING(<P>R/R WINDOW PER AMM 56-11-02. OPS CHK GOOD.</P>)SDR UIEA2022053000559Fmu · failedREJECTED TAKEOFF. AIRCRAFT DID NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED FMU, FUEL BOOST PUMP AND VSV ACTUATOR.SDR UIEA2022041700309None · noneON DESCENT, LOUD ELECTRICAL BUZZ BEHIND CAPTAIN LEFT SIDE FOLLOWED BY STRONG ELECTRICAL SMELL. POWER 2L WINDOW HEAT CIRCUIT BREAKER POPPED.(<P ><SPAN>REMOVED #2L WINDOW LINING. NO BURNING WIRES FOUND. FOUND MAINTENANCE MESSAGE 30120. FOLLOWED FIM 30-41 T818. RSDR UIEA2022040700264Skin · damagedR/H UPPER AFT FUSELAGE ABOVE RH ELEVATOR SECTION 48 APROXIMATE B.S. 258/ HAS HOLE IN SKIN WITH CRACKS.(<P><SPAN>REMOVED DAMAGED SKIN SECTION FROM STRINGER 11 RIGHT FROM FWD END AT STA 2638 FROM AFT END AT STA 2658 AND CUT SKIN BETWEEN STRINGSDR UIEA2022021700146Module · noneAIRCRAFT COMPLETED AIR TURN BACK AND RETURNED TO THE FIELD DUE TO GEAR MONITOR WARNING(<P ><SPAN>REPLACED PSEU MODULE IAW AMM 32-09-03. OPS CHECK GOOD.</SPAN></P> / <P> </P>)SDR UIEA2021082301835Access Door · puncturedFUS - ACCESS DOOR 192AR INT. SURFACE FOUND PUNCTURE(<P>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </P>)SDR UIEA2021082301836Access Door · delaminatedFUS - ACCESS DOOR 191EL EXT SURFACE DELAM(<P><SPAN>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </SPAN></P>)SDR UIEA2021082301837Access Door · delaminatedFUS - ACCESS DOOR 192ER EXT SURFACE DELAM(<P><SPAN>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </SPAN></P>)
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