# Service difficulty reports: N545JN

A list on [N545JN](https://openairdocs.org/aircraft/N545JN.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 2 · 74 reports

- [SDR 2025F00243](https://openairdocs.org/sdr/2025F00243.md): Fire Detector · failed · Oct 13, 2025 · N545JN · Doug MD11F · Fire Detection
  > DISCREPANCY: FIRE DET 2 FAIL.
- [SDR 9WGA2025063054519](https://openairdocs.org/sdr/9WGA2025063054519.md): Spar · corroded · May 27, 2025 · N545JN · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > DURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 THROUGH ACCESS 361BL WAS FOUND CORROSION SPOT. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 ACCE
- [SDR 9WGA2025063054518](https://openairdocs.org/sdr/9WGA2025063054518.md): Spar · corroded · May 27, 2025 · N545JN · Doug MD11F · Vertical Stabilizer, Spar/Rib
  > DURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SECTION BETWEEN STA 1927 AND STA 2486 ACCESS PANEL 361BL SUPPORT PLATE WAS FOUND WITH CORROSION SPOTS. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SE
- [SDR 9WGA2025063054517](https://openairdocs.org/sdr/9WGA2025063054517.md): Skin · corroded · May 24, 2025 · N545JN · Doug MD11F · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK ON HORIZONTAL STAB AFT FUSELAGE LH UPPER SIDE FOUND LIGHT CORROSION FROM STA 2007 TO STA 2163. REMOVED LITE CORROSION AT HORIZONTAL STABILIZER AFT FUSELAGE LH UPPER SIDE FROM STA 2007 TO STA 2163, MATERIAL REMOVED 0.002, ALODINED AND PRIMED
- [SDR 9WGA2025072354522](https://openairdocs.org/sdr/9WGA2025072354522.md): Pushrod · corroded · May 5, 2025 · N545JN · Doug MD11F · Elevator Structure
  > DURING HEAVT CHECK RH INBD/OUTBD ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS). MAINTENANCE REMOVED AND REPLACED RODS ON RH IB OB ELEVATOR PUSH RODS IAW MD-11 AMM 55-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR 9WGA2025072354521](https://openairdocs.org/sdr/9WGA2025072354521.md): Hinge · corroded · May 5, 2025 · N545JN · Doug MD11F · Elevator Structure
  > DURING HEAVY CHECK RH OUTBD ELEV DETACHABLE HING HAS HARDWARE WITH CORROSION. MAINTENANCE REMOVED AND REPLACED NUTPLATE RH OUTBD ELEV IAW MD-11F SRM 51-31-01-06-0 (HINGE). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025072354520](https://openairdocs.org/sdr/9WGA2025072354520.md): Pushrod · corroded · May 5, 2025 · N545JN · Doug MD11F · Elevator Control System
  > DURING HEAVY CHECK RH INBD /OUTB ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS).
- [SDR 9WGA2025062054516](https://openairdocs.org/sdr/9WGA2025062054516.md): Hinge · worn · May 5, 2025 · N545JN · Doug MD11F · Elevator Structure
  > DURING HEAVY CHECK R/H ELEVATOR HINGE PANELS 346HB, 346FB, 346DB, 346BB, 345FB BARE COMPOSITE MATERIAL. REPAIRED HINGE PANELS # 346HB, 346FB, 346BD, 346BB, 345FB AND 345DB AT R/H ELEVATOR HINGE IAW MD-11 SRM 51-62-01-06-0 PRIMED AND TOP COATED PANEL IAW MD-11
- [SDR 9WGA2025061754513](https://openairdocs.org/sdr/9WGA2025061754513.md): Hinge · rough · May 5, 2025 · N545JN · Doug MD11F · Elevator Structure
  > DURING HEAVY CHECK RH OUTBD ELEV HINGE DAMONER HAS ROUGH MATERIAL (EVALUATE IF WITHIN LIMITS). REMOVED ROUGH MATERIAL AT RH OUTBOARD ELEVATOR HINGE DAMPER MATERIAL. REMOVED 0.001 IAW MD-11 SRM 51-21-01-06-0, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06
- [SDR 9WGA2025061754512](https://openairdocs.org/sdr/9WGA2025061754512.md): Rib · corroded · May 5, 2025 · N545JN · Doug MD11F · Elevator, Spar/Rib
  > DURING HEAVY CHECK RH OUTB ELEVATOR FOUND CORROSION ON RIB INSTL BEHIND ACCESS PANEL 346BZ. CLEANED CORROSION AT RH OB ELEVATOR BEHIND ACCESS PANEL 346BZ, MATERIAL REMOVED 0.002, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06-0. THE AIRCRAFT WAS APPROVED
- [SDR 9WGA2025061754511](https://openairdocs.org/sdr/9WGA2025061754511.md): Paint · worn · May 5, 2025 · N545JN · Doug MD11F · Elevator Structure
  > DURING HEAVY CHECK RH LE INBOARD ELEVATOR PAINT/PRIMER LAYERS ARE WORN (BARE MATERIAL). RH LE IB ELEVATOR WAS PAINTED IAW MD11F SRM 51-21-02-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061354510](https://openairdocs.org/sdr/9WGA2025061354510.md): Rod · loose · May 5, 2025 · N545JN · Doug MD11F · Elevator Control System
  > DURING HEAVY CHECK R/H INBOARD ELEVATOR ROD IS LOOSE. RESECURED HARDWARE R/H INBOARD ELEVATOR ROD IAW MD-11 AMM 20-50-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025070154520](https://openairdocs.org/sdr/9WGA2025070154520.md): Support · cracked · May 2, 2025 · N545JN · Doug MD11F · Trailing Edge Flaps
  > DURING HEAVY CHECK MAINTENANCE LT FLAP HINGE SUPPORT WAS FOUND TO BE CRACKED. LT OTBD FLAP HINGE BRACKET ASSY WAS REMOVED AND REPLACED IAW MD-11 AMM 57-53-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025070154519](https://openairdocs.org/sdr/9WGA2025070154519.md): Support · cracked · May 2, 2025 · N545JN · Doug MD11F · Wing Structure
  > DURING HEAVY MAINTENANCE LH FLAP HINGE SUPPORT WAS FOUND CRACKED.
- [SDR 9WGA2025062054515](https://openairdocs.org/sdr/9WGA2025062054515.md): Thrust Reverser · delaminated · May 2, 2025 · N545JN · Doug MD11F · Engine Thrust Reverser
  > DURING HEAVY CHECK ENGINE #3 THRUST REVERSER INBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER I/B FIXED STRUCTURE IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025062054514](https://openairdocs.org/sdr/9WGA2025062054514.md): Cowling · corroded · May 2, 2025 · N545JN · Doug MD11F · Engine Thrust Reverser
  > DURING HEAVY MAINTENANCE ENGINE #3 THRUST REVERSER OUTBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER O/B FIXED STRUCTURE (COWL-ASSY) IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061054503](https://openairdocs.org/sdr/9WGA2025061054503.md): Case · corroded · May 2, 2025 · N545JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY CHECK ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION (RUSTY). CLEANED CORROSION (RUSTY) AT ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OGV'S BOLTS AND NUTS IAW MD-11 SRM 51-21-01. THE AIRCRAFT WAS APPROVED FOR R
- [SDR 9WGA2025061054502](https://openairdocs.org/sdr/9WGA2025061054502.md): Case · corroded · May 2, 2025 · N545JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY CHECKENGINE #1 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION. CLEANED CORROSION, APPLIED ALODINE, & PRIMER IAW MD-11 SRM 51-21-01 ON #1 ENGINE FAN CASE BY OGV'S AREA. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061100004](https://openairdocs.org/sdr/9WGA2025061100004.md): Door · cracked · May 1, 2025 · N545JN · Doug MD11F · Air Conditioning Doors
  > DURING HEAVY MAINTENANCE LEFT AIR CONDITIONING PACK 1 DOOR HAS CRACKED WEB. LEFT AIR CONDITIONING PACK 1 DOOR REPAIRED (WEB) IAW MD-11-F SRM 52-00-00-2R-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061354509](https://openairdocs.org/sdr/9WGA2025061354509.md): Rivet · corroded · Apr 30, 2025 · N545JN · Doug MD11F · Fuselage Main, Structure
  > DURING HEAVY CHECK ZONE 250 STA 1239 RIVETS WITH RUST (CORROSION) AROUND THE WINDOW. REPLACED RIVETS ZONE 250 STA 1239 THE WINDOW IAW MD-11F SRM 51-35-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061354508](https://openairdocs.org/sdr/9WGA2025061354508.md): Hinge · corroded · Apr 30, 2025 · N545JN · Doug MD11F · Fuselage, Door Hinge
  > DURING HEAVY CHECK FWD CARGO DOOR HINGE WITH SLIGHT RUST (CORROSION). CLEANED SLIGHT RUST (CORROSION) AT FWD CARGO DOOR HINGE. PRIMED AND TOP COATED AREA IAW MD-11 SRM 51-21-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061354507](https://openairdocs.org/sdr/9WGA2025061354507.md): Hinge · corroded · Apr 30, 2025 · N545JN · Doug MD11F · Fuselage, Door Hinge
  > DURING HEAVY CHECK MAIN DECK CARGO DOOR HINGE WITH SLIGHT RUST (CORROSION). CLEANED RUST (CORROSION) AT MAIN DECK CARGO DOOR HINGE. PRIMED AND TOP COATED AREA IAW MD-11 SRM 51-35-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061254506](https://openairdocs.org/sdr/9WGA2025061254506.md): Pressure Blkhd · corroded · Apr 28, 2025 · N545JN · Doug MD11F · Fuselage Main, Bulkhead
  > DURING HEAVY CHECK FWDPRESSURE BULKHEAD STA 464 (INTERIOR SIDE) WAS FOUND LIGHT CORROSION AT STA R-52 TO R-40. REMOVED LIGHT CORROSION AT FWD PRESSUREBULKHEAD STA 464 R-52 TO R 40, MATERIAL REMOVED 0.001, FOUND WITHIN LIMITS. ALODINED, PRIMED AND TOP COATED
- [SDR 9WGA2025061254505](https://openairdocs.org/sdr/9WGA2025061254505.md): Pressure Blkhd · corroded · Apr 28, 2025 · N545JN · Doug MD11F · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE FWD PRESSURE BULKHEAD STA 464 (INTERIORSIDE) STIFFNER WAS FOUND WITH EXFOLIATED CORROSION AT STIFFENER FROM R-52 TO R-40. CLEANED AREA AT FWD PRESSURE BULKHEAD STA 464 (INTERIORSIDE) STIFFENER, AFTER FURTHER EVALUATION FOUND LIGHT COR
- [SDR 9WGA2025060954501](https://openairdocs.org/sdr/9WGA2025060954501.md): Pressure Panel · corroded · Apr 4, 2025 · N545JN · Doug MD11F · Fuselage Main, Structure
  > DURING HEAVY CHECK HORIZONTAL PRESSURE PANEL, STA 464 (CANTED) - 595 SPOTS OF CORROSION (LIGHT CORROSION) AT ZONES 113 AND 114. REMOVED LIGHT CORROSION AT HORIZONTAL PRESSURE PANEL STA. 464 (CANTED) 515 ZONES 113 AND 114, MATERIAL REMOVED 0.001, IAW MD-11 SRM
- [SDR 9WGA2025100654523](https://openairdocs.org/sdr/9WGA2025100654523.md): Spar · cracked · Apr 2, 2025 · N545JN · Doug MD11F · Wing Spar
  > DURING HEAVY CHECK TRANSFERRED FROM DMI# 26493 "PERMANENT REPAIR NEED WITHIN 60 DAYS ON CRACK IN AFT SIDE OF LH WING EXTENDING FROM #1 TANK XFER PUMP HOLE". PERMANENT REPAIR AT REAR SPAR ON AFT SIDE LH WING WAS PERFORMED I.A.W REP-11-545-259-WG AND BOEING REP
- [SDR 2024FA0000800](https://openairdocs.org/sdr/2024FA0000800.md): Compressor · stalled · Oct 31, 2024 · N545JN · Doug MD11F · Powerplant System
  > DISCREPANCY: ENGINE #2 SUSPECTED COMPRESSOR STALL DURING ROTATION. CA: OPEN
- [SDR 9WGA2023121754501](https://openairdocs.org/sdr/9WGA2023121754501.md): Unknown · unknown · Dec 16, 2023 · N545JN · Doug MD11F · Aircraft Fuel System
  > DISCREPANCY: POSSIBLE TANK 1-2 XFR ON FINAL MAY HAVE CAUSED ENGINE 2 TO FLAME OUT ON FINAL. CORRECTIVE ACTION: AIRCRAFT REFUELED IAW AMM 12-11-02. PERFORMED FUEL SYSTEM TEST PER AMM 28-08-01, TEST SATIS. PERFORMED ENGINE RUN UP PER AMM 71-00-00-000-804, TEST S
- [SDR 9WGA2023060554501](https://openairdocs.org/sdr/9WGA2023060554501.md): Computer · inoperative · Jun 5, 2023 · N545JN · Doug MD11F · Autopilot System
  > DISCREPANCY: AIR RETURN DUE TO AMBER IAS & ALT FOLLOWED BY LOSS OF FD, FOLLOWED BY LOSS OF AUTOTHROTTLE. LOST ABILITY SELECT ALT ON FCP, LEVELED OFF AT 3000. AIRSPEED UNRELIABLE CHECKLIST DISCONNECTED AFS PROBLEM WENT AWAY ENTIRELY. RESELECTED NEW ALT 10000, S
- [SDR 9WGA2023053054502](https://openairdocs.org/sdr/9WGA2023053054502.md): Control Unit · inoperative · May 30, 2023 · N545JN · Doug MD11F · Navigation System
  > AIR RETURN DUE TO UNRELIABLE AIRSPEED. SWITCHING CADC SIDE TO 2, OPS NORMAL. R & R CADC #1 IAW AMM 34-16-01. PERFORM LEAK CHECK ON #1 SYSTEM IAW AMM 34-11-00-700-801. OPS CHECK NORMAL, NO FAULTS NOTED AT THIS TIME.
- [SDR 9WGA2023053054501](https://openairdocs.org/sdr/9WGA2023053054501.md): Cadc · inoperative · May 30, 2023 · N545JN · Doug MD11F · Flight Environment Data
  > DISCREPANCY: CADC 2 FAILURE ON TO. R & R #2 CADC PER AMM 34-16-01. CORRECTIVE ACTION: PERFORMED CADC LEAK CHECK PER AMM 34-11-00-700-801. OPS CHECK NORMAL. NO FAULT NOTED AT THIS TIME.
- [SDR 9WGA2023052854501](https://openairdocs.org/sdr/9WGA2023052854501.md): Unknown · unknown · May 28, 2023 · N545JN · Doug MD11F · Airspeed/Mach Indicator
  > DISCREPANCY: AIR TURN BACK DUE TO, AFTER TAKE-OFF AROUND 1000 FEET AIRSPEED UNRELIABLE. ACCOMPLISHED APPROPRIATE CHECK LIST. PERFORMED FIM 34-11-02. PERFORMED CAPTAIN AND FO PITOT/STATIC LEAK CHECK PER AMM 34-11-00. NO DISCREPANCIES FOUND AT THIS TIME.
- [SDR 9WGA2022011354501](https://openairdocs.org/sdr/9WGA2022011354501.md): Anti-Ice System · blew out · Jan 13, 2022 · N545JN · Doug MD11F · Powerplant System
  > DISCREPANCY: CLIMBING OUT OF FL 180 @1000Z LEVEL 1 ENGINE 3 FADEC MAINT FOLLOWED BY A LOUD BANG, THEN N1 ROLLED BACK PAST 41 TO X. CORRECTIVE ACTION: REMOVED AND REPLACED INLET NOSE COWL ANTI-ICE DUCT FORWARD PORTION IAW MD-11 AMM 30-22-09.
- [SDR 9WGA2021121554501](https://openairdocs.org/sdr/9WGA2021121554501.md): None · none · Dec 15, 2021 · N545JN · Doug MD11F · Flight Management Computing Hardware System
  > LEVEL 2 FCC 2A DATA FAULT. QRH PROCEDURES PERFORMED.
- [SDR 9WGA2021051154501](https://openairdocs.org/sdr/9WGA2021051154501.md): Fire Detector · intermittent · May 11, 2021 · N545JN · Doug MD11F · Fire Detection
  > INTERMITTENT FIRE DETECT II FAIL.
- [SDR 9WGA2021041854501](https://openairdocs.org/sdr/9WGA2021041854501.md): Fire Loop · failed · Apr 18, 2021 · N545JN · Doug MD11F · Fire Detection
  > FIRE DET 1 LOOP FAIL INFLIGHT.
- [SDR 9WGA2020111554501](https://openairdocs.org/sdr/9WGA2020111554501.md): Fire Warning · illuminated · Nov 16, 2020 · N545JN · Doug MD11F · Fire Detection
  > AIR RETURN DUE TO ENGINE 2 LVL 3 FIRE INDICATION.
- [SDR 9WGA2020100354501](https://openairdocs.org/sdr/9WGA2020100354501.md): Pump · inoperative · Oct 3, 2020 · N545JN · Doug MD11F · Fuel Boost Pump
  > TANK 1 & 3 FORWARD PUMP OFF.
- [SDR 9WGA20200120191](https://openairdocs.org/sdr/9WGA20200120191.md): Tire · leaking · Jan 19, 2020 · N545JN · Doug MD11F · Tire
  > IN FLIGHT - L1 TIRE-DIFF PRESS AND TIRE PRESS LOW - THE #6 TIRE SLOWLY DROOP PRESSURE (OVER 30 MINS) TO 49 PSI AND TIRE FAIL L-2 ON #6 ALERT. WE RETURNED TO MIA AND LANDED. FOLLOWED TIRE FAIL CHECKLIST, THE #6 TIRE WAS FLAT BUT NO VISUAL DAMAGE TO AIRCRAFT. IN
- [SDR 9WGA52017110801](https://openairdocs.org/sdr/9WGA52017110801.md): Warning Message · multiple fail · Nov 8, 2017 · N545JN · Doug MD11F · Central Warning
  > AT 39,000 FEET, A WARNING ON PNEUMATIC MANIFOLD SYSTEM 3, CLOSED THE BLEED VALVE ON ENGINE 3. AFTER A CABIN RATE ANNUNCIATION, REQUESTED DESCENT TO 31,000 FT, FOLLOWED BY A SECOND RED WARNING ON SYSTEM 1, FOLLOWED BY A RAPID CABIN CLIMB, EVEN THOUGH THE SYSTEM
- [SDR KO0R201705180016](https://openairdocs.org/sdr/KO0R201705180016.md): Web · cracked · May 18, 2017 · N545JN · Doug MD11F · Wing Miscellaneous Structure
  > RIGHT WING FIXED TRAILING EDGE COMPARTMENT BOX WEB IS CRACKED.
- [SDR KO0R201705180015](https://openairdocs.org/sdr/KO0R201705180015.md): Panel · cracked · May 18, 2017 · N545JN · Doug MD11F · Nacelle/Pylon, Plate/Skin
  > NR 3 PYLON PANEL 487AR VENT DUCT HAS A CRACKED CORNER.
- [SDR KO0R201705180014](https://openairdocs.org/sdr/KO0R201705180014.md): Channel · cracked · May 18, 2017 · N545JN · Doug MD11F · Wing Main, Frame Structure
  > RIGHT WING FIXED TRAILING EDGE COMPARTMENT AT XORS 350 LOWER CHANNEL IS CRACKED IN 3 PLACES.
- [SDR KO0R201705180013](https://openairdocs.org/sdr/KO0R201705180013.md): Fuel Tank · corroded · May 18, 2017 · N545JN · Doug MD11F · Hydraulic System, Main
  > EVIDENCE OF CORROSION AT UPPER SURFACE OF CENTER FUEL TANK AT BS 1229, RBL 60.
- [SDR 9WGA2016112501](https://openairdocs.org/sdr/9WGA2016112501.md): Regulator Valve · inoperative · Nov 25, 2016 · N545JN · Doug MD11F · Pneumatic Distribution System
  > ENGINE NR 2 FIRE WARNING LEVEL 3 ALERT CLIMBING THROUGH FL190. ENGINE SHUT DOWN. FIRE EXTINGUISHER DISCHARGED. FOUND PRESSURE REGULATOR VALVE (PRV) INOPERATIVE. REPLACED PRV.
- [SDR 9WGA5452016101301](https://openairdocs.org/sdr/9WGA5452016101301.md): Fire Warning · false activation · Oct 13, 2016 · N545JN · Doug MD11F · Fire Detection
  > DURING CLIMB, NR 2 ENGINE FIRE WARNING ILLUMINATED. RETURNED TO DEPARTURE. DURING INSPECTION, NO EVIDENCE OF FIRE IN NR 2 ENGINE/PYLON AREA. TROUBLESHOOTING FIRE DETECTION SYSTEM.
- [SDR 9WGA2016090101](https://openairdocs.org/sdr/9WGA2016090101.md): Fire Warning · false activation · Sep 1, 2016 · N545JN · Doug MD11F · Fire Detection
  > ON APPROACH, NR 1 ENGINE FIRE DETECTOR ILLUMINATED. ACTIVATED FIRE EXTINGUISHING BOTTLES, 2 EACH AND LANDED UNEVENTFULLY. NO EVIDENCE OF ACTUAL FIRE.
- [SDR 9WGA20151129001](https://openairdocs.org/sdr/9WGA20151129001.md): O-Ring · damaged · Nov 29, 2015 · N545JN · Doug MD11F · Turbine Engine Oil System
  > ENGINE NR 1 OIL LEAKAGE IN FLIGHT. OIL LEAK FROM DAMAGED O RING ON HYD PUMP LOCK OUT KIT, REFERENCE DMI 6588. REPLACED O RING IAW AMM 72-65-11. ENG RUN PERFORMED WITH NO LEAKS NOTED.
- [SDR KO0R201503120027](https://openairdocs.org/sdr/KO0R201503120027.md): Hinge Fitting · corroded · Mar 12, 2015 · N545JN · Doug MD11F · Trailing Edge Flaps
  > RIGHT-HAND OUTBOARD FLAP INBOARD HINGE FITTING IS CORRODED.
- [SDR KO0R201503120026](https://openairdocs.org/sdr/KO0R201503120026.md): Skin · corroded · Mar 12, 2015 · N545JN · Doug MD11F · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT BS 1295 LBL 110 STRINGER 8 UPPER CENTER WING SKIN.

Next page: https://openairdocs.org/aircraft/N545JN/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 = 'N545JN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N545JN/reports

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