N546JN
Service difficulty reports · 146
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 = 'N546JN' 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 = 'N546JN' 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 9WGA2025082654644Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWESDR 9WGA2025082654643Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 0.5 AT 5-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSSDR 9WGA2025082654642Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA. 1182, XCW 8.5 AT 5-21. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX. STA. 1182, XCW 8.5 AT S-21 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11 MSDR 9WGA2025082354641Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT L/H APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT L/H CENTER WING USDR 9WGA2025082354640Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1205, XCW 4.0 AT S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WINSDR 9WGA2025082254630Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESDR 9WGA2025082254629Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH AAPROX STA. 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPSDR 9WGA2025082254628Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1229, XCW 34.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING SDR 9WGA2025082254627Panel · corrodedDURING HEAVY CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1226 XCW 80.5 AT S-15. AFTER FURTHER EVALUATION BOING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANELSDR 9WGA2025081854625Angle · crackedDURING HEAVY MAINTENANCE ANGLE BELOW FWD RH PATIO FLOOR HAS A CRACK. FABRICATED AND INSTALLED ANGLE STIFFENER AT PATIO FLOOR BELOW RH FWD IAW MD-11 SRM 51-31-10 AND DRAWING AKC7546. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025091854653Bolt · corrodedDURING HEAVY MAINTENANCE CORROSION FOUND ON LH OB ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.SDR 9WGA2025062054624Bolt · corrodedDURING HEAVY MAINTENANCE CORROSION FOUND ON L/H O/B ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.SDR 9WGA2025081954626Slat Track · corrodedDURING HEAVY MAINTENANCE LH #5 SLAT TRACK OB RIB HAS CORROSION AT STA. XIS 332. REMOVED SURFACE CORROSION FROM INNER DOUBLER AT LH #5 SLAT TRACK OB RIB STA XIS 332. FOUND TO BE WITHIN LIMITS IAW MD-11 SRM 57-00-00-2R -0, FIGURE 206 EXAMPLE A. THE AIRCRAFT WSDR 9WGA2025050354623Housing · crackedAPU DOOR LATCH LOWER HOUSING IS CRACKED.SDR 9WGA2025042854601Ring · corrodedNR# 286 - DURING HEAVY MAINTNENANCE #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVED AND REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O#15700 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPROVSDR 9WGA2025041445614Bracket · corrodedDURING HEAVY MAINTENANCE CHECK HYDRAULIC DRAIN LINE BRACKET ON FWD WALL, BOTTOM, CENTER INSIDE PNL 316AB CORRODED. REMOVED AND REPLACED BRACKET ON HYDRAULIC DRAINN LINE ON FWD WALL BOTTOM CENTER INSIDE PNL 316AB IAW MD-11 SRM 51-31-01. THE AIRCRAFT WAS APPROSDR 9WGA2025041454609Shroud · crackedDURING HEAVY MAINTENANCE PILOTS SLIDING WINDOW FWD SHROUD COVER HAS A CRACK. REPAIRED AND RE-INSTALLED PILOT SLIDING WINDOW FWD SHROUD COVERS IAW MD-11, AMM 20-20-00 AND 20-20-09. (FWD SHROUD COVER REPAIRED). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454604Skin · puncturedDURING HEAVY MAINTENANCE PAC #3 DOOR OUTER UPPER SKIN HAS A HOLE IN IT. ACCOMPLISHED REPAIR ON PAC #3 DOOR OUTER UPPER SKIN IAW MD-11 SRM 52-00-00-20-0, SRM 52-40-01, REPAIR 1, SRM 51-33-01 AND BOEING REPAIR SKETCH: WGN-WGN-25-0020-01C. RECEIVED FINAL APPROSDR 9WGA2025042954622Inlet · corroded#3 INLET HAS PITTING CORROSION AT 11 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 11 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS ATSDR 9WGA2025042954621Inlet · corroded#3 INLET HAS PITTING CORROSION BETWEEN 8 & 9 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 8 AND 9 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL Q AND SRM 51-21-01. NOSDR 9WGA2025042954620Inlet · corroded3# INLET HAS PITTING CORROSION AT 3 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 3 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103, DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS AT SDR 9WGA2025042954619Inlet · corroded#3 INLET HAS PITTING CORROSION BETWEEN 5 & 6 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 5 & 6 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02. NO MATERIAL LOSS AT THIS TIME. O. ARILA D0011. SDR 9WGA2025042854617Ring · corrodedDURING HEAVY MAINTENANCE CHECK NR 1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ 8 O'CLOCK POSITION. ACCOMPLISHED WITH ENGINE REMOVAL AND REPLACEMENT IAW MD-11 T/C: MS-71-00-01-00-00-01-WG, SEQ,1,W/O# 15701 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPRSDR 9WGA2025042854616Ring · corrodedDURING HEAVY MAINTENANCE CHECK NR 2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVAL ANF REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O# 15700 AND AMM 71-00-03-000-801.THE AIRCRAFT WAS APPROVED FOSDR 9WGA20250428017Ring · corroded#1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8' O'CLOCK POSITION.SDR 9WGA20250428016Ring · corroded#2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF.SDR 9WGA2025041454601Bracket · brokenL/H MLG AFT WIRE HARNESS BRACKET BROKEN. REMOVED AND REPLACED BRACKET AT L/H MLG AFT WIRE HARNESS IAW MD-11 AMM 20-20-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454611Shroud · crackedDURING HEAVY MAINTENANCE CHECK COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. ACCOMPLISHED REPAIR OF R/H COPILOTS WINDOW SLIDING COVER IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454614Bracket · corrodedDURING HEAVY MAINTENANCE CHECK HYDRAULIC DRAIN LINE BRACKET ON FWD WALL, BOTTOM, CENTER INSIDE PNL 316AB CORRODED. REMOVED AND REPLACED BRACKET ON HYDRAULIC DRAIN LINE ON FWD WALL BOTTOM CENTER INSIDE PNL316AB IAW SRM 51-31-01. THE AIRCRAFT WAS APPROVED FOR SDR 9WGA2025041454613Bracket · corrodedDURING HEAVY MAINTENANCE CHECK FLEXIBLE HYDRAULIC HOSE BRACKET FOR TRANSFER PUMP ON FWD WALL CORRODED INSIDE PANEL 316AB. REMOVED AND REPLACED BRACKET (CLIP) AT FWD WALL INSIDE PANEL 316AB ON FLEXIBLE HYDRAULIC HOSE FOR TRANSFER PUMP IAW MD-11 SRM 51-35-01 ANSDR 9WGA2025041454612Shroud · crackedDURING HEAVY MAINTENANCE CHECK COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. ACCOMPLISHED REPAIR AT COPILOTS SLIDING WINDOW AFT SHROUD COVER IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WG2025F00000Shroud · crackedCOPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK.SDR 9WGA2025041454610Shroud · crackedPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. REINSTALLED PILOTS SLIDING WINDOW AFT SHROUD COVER IAW MD-11, AFT SHROUD COVER REPAIRED IAW MD-11 AMM 20-20--00 AND 20-20-09. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454602Intercostal · crackedDURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN: ACA3820-14 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA3820-14 ON PAX #3 DOOR AT MIDDLESIDE 2ND FROM TOP IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454608Brace · crackedL/H O/B AILERON O/B PNL BRACE HAS DENTED BRACE, BROKEN RIVETS, & CRACKED UPPER BRACKET. REMOVED AND REPLACED BRACE, RIVETS AND BRACKET AT LH OB AILERON OB PANEL BRACE IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454607Intercostal · crackedDURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN ACA3820 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA3820-4 ONPAX #3 DOOE AT MIDDLE SIDE FROM TOP IAW MD-11 SRM 51-33-01 AND SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454606Intercostal · crackedDURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN ACA3820-10 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA 3820-10 ON PAX #3 DOOR AT AFT SIDE 2ND FROM TOP IAW MD-11 SRM 51-35-01 AND SRM 51-33-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454605Track · crackedPNL BELOW PILOTS SLIDING WINDOW TRACK, CRACKED AT FWD SCREW. REPAIRED PILOTS SLIDING WINDOW TRACK PNL IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025041454603Intercostal · crackedDURING HEAVY MAINTENANCE PAX #3 DOOR INTERCOSTAL P/N ACA3820-16 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN:ACA3820-16 AT PAX #3 DOOR AT MIDDLE SIDE 3RD FROM TOP IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA202041454601Bracket · brokenL/H MLG AFT WIRE HARNESS BRACKET BROKEN. REMOVED AND REPLACED BRACKET AT L/H MLG AFT WIRE HARNESS IAW MD-11 AMM 20-20-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR 9WGA2026010954683Skin · puncturedDURING HEAVY MAINTENANCE CHECK PAX NR 3 DOOR OUTER UPPER SKIN HAS A HOLE IN IT. ACOMPLISHED REPAIR ON PAX NR3 DOOR OUTER UPPER SKIN IAW MD-11 SRM 52-00-00-2R-0, SRM 52-40-01. REPAIR 1, SRM 51-33-01 AND BOEING MESSAGE REPAIR SKETCH: WGN-WGN-25-0020-01C. THE SDR 9WGA2025042854615Mount · corrodedDURING HEAVY MAINTENACE PNL 513AT MOUNT FLANGE HAS SURFACE CORROSION. REMOVED SURFACE CORROSION BY HAND AT LEFT WING ACCESS PNL 531AT ATTACHING FLANGE IAW MD-11 SRM 51-21-01 PAR. 36 NO MATERIAL LOSS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA20250428015Mount · corrodedPNL 513AT MOUNT FLANGE HAS SURFACE CORROSION.SDR 2022F00294None · corrodedKSHV-DURING INSPECTION OF #2 ENGINE INLET POSSIBLE CORROSION WAS FOUND UNDER ACOUSTIC PANEL. MAINTENANCE REMOVED AND REPLACED CORRODED #2 ENGINE INLET T-BRACKET WITH A NEW FABRICATED ONE IAW MD-11 DRAWING AJC8118. AIRCRAFT IS GOOD FOR CONTINUED SERVICE.SDR 9WGA2021102954601None · noneAFTER 1 HOUR IN CRUISE, FUEL QUANTITY FAULT LEVEL 2 ALERT. NO FUEL INDICATION FOR TANK 2 TANKS.SDR 9WGA2021091154602Unknown · multiple failINITIAL CLIMB OUT, SIMULTANEOUS FAILURE 3 SYSTEMS - RADAR ALTIMETER "ERRONEOUS AUDIO ALTITUDE", AUTO PILOT 1 & 2 FAIL - AUTO THROTTLE.SDR 9WGA2021091154601Autopilot Sys · failedON INITIAL CLIMB OUT, SIMULTANEOUS FAILURE 3 SYSTEMS - RADAR ALTIMETER (ERRONEOUS), AUTO PILOT 1 & 2 FAIL, AUTO THROTTLE.SDR 9WGA2019100493001Director · failedFLIGHT DIRECTOR 1 FAIL, NAV WON'T ENGAGE, WON'T COME OUT OF TAKEOFF THRUST GCP MODE FMS MODE NOT ENGAGING, NO PERFORMANCE DATA CLIMBSDR 9WGA5462018032602Transmitter · intermittentDURING CRUISE, OBSERVED HYDRAULIC SYSTEM 1 REDUCTION IN QUANTITY .1 GALLON IN 6 MINUTES AND INCREASED TO .1 GALLON IN 4 MINUTES. RETURNED TO DEPARTURE. REMOVED AND REPLACED THE HYDRAULIC SYSTEM 1 QUANTITY TRANSMITTER IAW AMM 29-32-02. HYDRAULIC INDICATION SYSDR 9WGA5462018032601Line · looseIN FLIGHT, THE HYDRAULIC SYSTEM 1 LEAKING 1 GALLON IN 2 MINUTES. LEVEL ONE HYDRAULIC SYSTEM OFF DISPLAYED BELOW 2.5 GALLONS REMAINING. RETURNED TO DEPARTURE. FOUND THE HYDRAULIC OUTBOARD SUPPLY LINE LOOSE IN THE NR 1 PYLON. TORQUED IAW AMM 20-50-01. OPS & L
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