# Service difficulty reports: JASC 5497

A list on [JASC 5497](https://openairdocs.org/jasc/5497.md).

Reports filed under 5497 · Nacelle/Pylon System Wiring, newest first.

Page 1 of 2 · 53 reports

- [SDR WX0A2026080332908](https://openairdocs.org/sdr/WX0A2026080332908.md): Wire Harness · damaged · Aug 1, 2026 · N297NV · Airbus A320214
  > (AIRCRAFT GROUNDED) (EMERGENCY DECLARED) THROUGHOT FLIGHT INTERMITENT ECAM EBG 1 THR LEVER DISAGREE / R/R ENGINE CONTROL UNIT (CHANNEL A) HARNESS IAW AMM 71-51-43-00-046-A, REMOVE AND AMM 71-51-43-400-046-A, INSTALL. R/R ENGINE CONTROL HARNESS UNIT (CHANNEL B)
- [SDR AALA202604295221](https://openairdocs.org/sdr/AALA202604295221.md): Wire Harness · failed · Apr 16, 2026 · N958AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 ENGINE THRUST RECERSER INDICATION AND AUTO THROTTLE CAME ON, AND THROTTLE BECAME UNRESPONSIVE. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT JAX. REMOVED AND REPLACED NUMBER 1 (EEC)-ELECTRONIUC ENG
- [SDR AALA202604298741](https://openairdocs.org/sdr/AALA202604298741.md): Wire Harness · faulty · Apr 16, 2026 · N958AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 ENGINE THRUST RECERSER INDICATION AND AUTO THROTTLE CAME ON, AND THROTTLE BECAME UNRESPONSIVE. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT JAX. REMOVE AND REPLACED NUMBER 1 (EEC)-ELECTRONIUC ENGIN
- [SDR HALA20250818250](https://openairdocs.org/sdr/HALA20250818250.md): Jumper · worn · Aug 15, 2025 · N220HA · Airbus A321271N
  > ETOPS - DURING TASK CARD E1128-321-26-011 PYLON. FOUND JUMPER ON LPT ACC COOLING TUBE ON 3 OCLOCK WORN OVER LIMIT. REMOVED LPT ACC COOLING TUBE PER AMM 75-00-00-210-802-A ALEX 023895. INSTALLED LPT ACC TUBE WITH NEW JUMPER 1EA. IDLE RUN. FOUND NO LEAK. OK FOR
- [SDR 2025F00178](https://openairdocs.org/sdr/2025F00178.md): Elec Connector · dirty · Aug 10, 2025 · N921PK · Raythn HAWKER850XP
  > CREW REPORTED OBSERVING THE #2 ENGINE OIL PRESSURE DECREASE STEADILY ON THE GAUGE FROM NORMAL TO APPROXIMATELY 16 PSI CREW DID NOT NOTE A MASTER WARNING INDICATION LIGHT FOR OIL PRESSURE UNTIL AFTER COMPLETING THE ENGINE SHUTDOWN.. CREW INITIATED AN ENGINE SHU
- [SDR UIEA2024080900812](https://openairdocs.org/sdr/UIEA2024080900812.md): Jumper · deteriorated · Aug 15, 2024 · N645GT · Boeing 767324
  > ENGINE 1, ACCESS PANEL 416AR, DETERIORATED GROUND JUMPER OF HIGH STAGE VALVE.(<P>ENGINE 1, ACCESS PANEL 416AR, JUMPER OF HIGH STAGE VALVE WAS REPLACED I.A.W AMM 70-20-00-702-002-H00 AND AMM 36-11-18-404-018-001 REV. 142 DATE 22 APR 2024 BONDING VALUE 1 MILLIOH
- [SDR DALA2024071107031](https://openairdocs.org/sdr/DALA2024071107031.md): Junction Box · cracked · Jul 10, 2024 · N336NB · Airbus A319114
  > SHIP 3136 FOUND CRACK ON FWD CANNON PLUG JUNCTION BOX ON THE FWD INBD SIDE OF BOX #1 ENG. CORRECTIVE ACTION: REPAIRED PER A319 SRM 54-50-00-283-012. (0439437)
- [SDR ASAA2021072035448](https://openairdocs.org/sdr/ASAA2021072035448.md): Wire Harness · damaged · Jul 20, 2021 · N481AS · Boeing 737990ER
  > #2 ENGINE NACELLE HARNESS MW033 HAS DAMAGE AT JUNCTION OF DP1101 FFCC VIBE SENSOR CONNECTOR AND #2 ENG PRESS REQ HARNESS SEGMENT. GROUNDED - YES. REPLACED MW0311 HARNESS B737-900 AMM 73-21-06-400-802. ACCOMPLISHED GROUND WING THERMAL ANTI ICING SOLENOID VALVE
- [SDR AALA202103099025](https://openairdocs.org/sdr/AALA202103099025.md): Wire Harness · defective · Mar 7, 2021 · N996AN · Airbus A321231
  > AIRCRAFT WAS GROUNDED: #1 ENG MODE FAULT CAME ON IN CLIMB AROUND 23000 WE DID ECAM PROCEDURE CONTINUED CLIMB AT LEVEL OFF 330. WE COULD NOT MAINTAIN SPEED.WE TOLD ATC FOR LOWER ALTITUDE AND RETURNED TO DFW. POWER WAS BACK DESCEND THRU MID 20S. THROTTLE SPLIT W
- [SDR AALA202010039002](https://openairdocs.org/sdr/AALA202010039002.md): Wire Harness · chafed · Oct 2, 2020 · N669AW · Airbus A320232
  > AIRCRAFT IN BASE MAINTENANCE: CHAFING IDG POWER CABLES 4000XU AT 5 O CLOCK ON #1 ENGINE. REPLACED ELECTRICAL HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 71-51-02, AWM 71-51-03 AND AMM 71-00-00-710-022-B
- [SDR AALA202009269004](https://openairdocs.org/sdr/AALA202009269004.md): Wire Harness · worn · Sep 25, 2020 · N912UY · Airbus A321231
  > BASE MAINTENANCE IDG CABLE, WORN WIRES, 9 O'CLOCK POSITION, ENGINE 2. REPLACED IDG CABLE HARNESS, PER AMM TASK 24-21-43-400-010-A. PERFORMED SATISFACTORY IDLE POWER TEST, PER AMM TASK 71-00-00-710-012-B. PERFORMED CHECK ELECT PAGE FOR IDG PARAMETERS, PER AM
- [SDR AALA202006299007](https://openairdocs.org/sdr/AALA202006299007.md): Wire Harness · chafed · Jun 28, 2020 · N830AW · Airbus A319132
  > AIRCRAFT IN BASE MAINTENANCE - CHAFING, ELECTRICAL WIRING, UPPER FORWARD RH PYLON OUTBOARD AT RIB 9 (INTEGRATED DRIVE GENERATOR CABLES). REMOVED AND REPLACED ELECTRICAL WIRING (IDG CABLES), PERFORMED VOLTAGE AND FREQUENCY CHECK, PER AMM TASK 24-92-00-400-002-
- [SDR AALA202004159004](https://openairdocs.org/sdr/AALA202004159004.md): Wire · cracked · Apr 14, 2020 · N744P · Airbus A319112
  > AIRCRAFT IN BASE VISIT: EXPOSED WIRE (SHIELD CRACKED OPENED) BY SLAT LE O/B RH PYLON TOP. REPAIRED DK-6 WIRE ON # 2 ENG TOP PYLON O/B BY SLAT LE. REF ESPM 20-53-21.
- [SDR DALA201908064591](https://openairdocs.org/sdr/DALA201908064591.md): Wire Harness · damaged · Mar 6, 2019 · Boeing 717200
  > NOSE LIP DAMAGED, WIRE HARNESS DAMAGED, PAINT IN POOR CONDITION. REPAIRED IN ACCORDANCE WITH CMM 71-11-05 REVISION 23, REFERENCE ATTACHED FAA FORM 8119-3DATED 03/JUN/10. TOTAL ACOUSTICAL LOSS: 10,75 INCHES. INCORPORATED SERVICE BULLETIN R715.71-010. CER
- [SDR SWIA201904035728](https://openairdocs.org/sdr/SWIA201904035728.md): Bonding Strap · corroded · Feb 22, 2019 · N449SW · Cndair CL6002B19
  > LEFT ENGINE PYLON TRAILING EDGE. 1EA UPPER AND 1EA LOWER BONDING STRAPS CORRODED. (C-CHECK) RO: 04/01/2019 REPLACED BONDING STRAPS ON RH ENGINE PYLON TRAILING EDGE IAW RIL.
- [SDR P5CA2016081800231](https://openairdocs.org/sdr/P5CA2016081800231.md): Cable · damaged · Aug 16, 2016 · N498MC · Boeing 74747UF
  > FOUND WIRE CABLE DAMAGED NEAR NR 4 PYLON. REPAIRED THE WIRE CABLE IAW SWPM 20-30-13 REV 62, & WDM 24-21-41 REV 41. OPS CHECKED GOOD.
- [SDR ASAA2016010514655](https://openairdocs.org/sdr/ASAA2016010514655.md): Wire Harness · damaged · Jan 5, 2016 · N597AS · Boeing 737890
  > FOUND NR 1 ENGINE NACELLE WIRE HARNESS DAMAGED AT DP1202 OF HARNESS MW0312. ACFT GROUNDED. REPLACED NR 1 ENGINE NACELLE HARNESS MW0312 WITH NEW ONE. ACCOMPLISHED ENGINE TEST, TEST 1, 2, 3A, A2,13 ALL PASS NO FAULTS NOTED. REF AMM 71-00-00-800-811 & 71-51-03-
- [SDR R61A201501280092](https://openairdocs.org/sdr/R61A201501280092.md): Bonding Jumper · corroded · Jan 28, 2015 · N802MD · Emb ERJ170100SU
  > DURING HEAVY CHECK, BONDING JUMPERS RT PYLON BEHIND PANEL 429PL ARE CORRODED. MX R & R BONDING JUMPERS RT PYLON BEHIND PANEL 429PL IAW AMM 20-13-21, P/N PE88001-5664, JUMPER.
- [SDR R61A201501280069](https://openairdocs.org/sdr/R61A201501280069.md): Bonding Jumper · corroded · Jan 28, 2015 · N802MD · Emb ERJ170100SU
  > DURING HEAVY CHECK, UNDER PANEL 515DT, SEVERAL JUMPERS ARE CORRODED. MAINTENANCE R & R ALL CORRODED JUMPERS.
- [SDR R61A201501280068](https://openairdocs.org/sdr/R61A201501280068.md): Bonding Jumper · corroded · Jan 28, 2015 · N802MD · Emb ERJ170100SU
  > DURING HEAVY CHECK, BONDING JUMPERS UNDER PANEL 419CT ARE CORRODED. MX R & R THE BONDING JUMPERS IAW AMM 20-13-27.
- [SDR R61A201501280067](https://openairdocs.org/sdr/R61A201501280067.md): Bonding Jumper · corroded · Jan 28, 2015 · N802MD · Emb ERJ170100SU
  > DURING HEAVY CHECK, SEVERAL BONDING JUMPERS LT PYLON BEHIND PANEL 419RL ARE CORRODED. MAINTENANCE R & R BONDING JUMPERS LT PYLON BEHIND PANEL 419RL IAW AMM 20-13-21. PN PE88001-5GG4 JUMPER. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
- [SDR ASOA2014070210797](https://openairdocs.org/sdr/ASOA2014070210797.md): Insulation · torn · Jun 16, 2014 · N861AS · Cndair CL6002B19
  > TORN PROTECTIVE SHEATHING ON WIRE BUNDLES INSIDE LT PYLON ZONE 412. REPAIRED WIRES IAW REO 601R-20-12-001.
- [SDR JJBA20131107006](https://openairdocs.org/sdr/JJBA20131107006.md): Bonding Strap · loose · Nov 7, 2013 · N369PH · Dhav DHC8202
  > BONDING STRAP HANGING FROM LT ENGINE COWLING. SECURED BONDING STRAP.
- [SDR R61A201311061131](https://openairdocs.org/sdr/R61A201311061131.md): Screw · corroded · Nov 6, 2013 · N123HQ · Emb ERJ170200LR
  > DURING HEAVY CHECK, BONDING JUMPER ON LT PYLON OTBD SIDE HAS CORRODED ATTACHING HARDWARE. R & R ATTACH HARDWARE IAW AMM 20-10-01.
- [SDR ASOA2013070308557](https://openairdocs.org/sdr/ASOA2013070308557.md): Wire · damaged · May 22, 2013 · N720EV · Cndair CL6002C10
  > ICG POWER LEAD WIRE G1 T3 (ORANGE WIRE) GOUGED 3" OTBD OF LT PYLON. REPAIRED WIRING IAW REO 670-24-21-001 AND ESPM 20-33-00. REPAIR CLASSIFIED AS MAJOR.
- [SDR CA121101004](https://openairdocs.org/sdr/CA121101004.md): Wire Harness · broken · Nov 1, 2012 · Cndair CL6002B19
  > (CAN) DURING ROUTINE MTC THE LH JET PIPE LOOP A WAS FOUND U/S. TROUBLESHOOTING FOUND THAT THE ENGINE FIRE DETECTION WIRING HARNESS WAS BROKEN AT THE PYLON CONNECTOR. THE FIRE DETECTION (P590) AND FIRE PROTECTION (P592) WIRING HARNESSES WERE REPLACED. THIS DEFE
- [SDR FDEA201206152246](https://openairdocs.org/sdr/FDEA201206152246.md): Feeder Cable · burned · Jun 15, 2012 · N320FE · Doug MD1030F
  > NR 1 ENGINE PYLON VIEW THROUGH DOOR 438BL, FEEDER CABLES FOUND CHAFING AGAINST STRUCTURE, ARCING, AND BURNED. FEEDER CABLE REPLACED EO 8-2450-7-5009 01, PART 1.
- [SDR J8UR20111219001](https://openairdocs.org/sdr/J8UR20111219001.md): Connector · chafed · Dec 19, 2011 · N6321R · Beech B300C
  > RT FUEL SHUT-OFF VALVE ELECTRICAL CONNECTOR IS COMING IN CONTACT WITH ACCESS PANEL NUTPLATE ON RT NACELLE (PANEL NR 5RH). THE CLOSE PROXIMITY OF THE FIREWALL ELECTRICAL CONNECTOR AND THE ACCESS PANEL NUTPLATE CAUSED WIRING TO BECOME CHAFED. NUTPLATE PROTRUDE
- [SDR CA111129007](https://openairdocs.org/sdr/CA111129007.md): Connector · dislodged · Nov 25, 2011 · Beech C90A
  > (CAN) DURING PREFLIGHT WALK AROUND THE PILOT NOTICED THE RT ENG OTBD FIREWALL CONNECTOR, EVEN THOUGH LOCK WIRED SECURELY, WAS LOOSE. FURTHER INSPECTION REVEALED THE LOCKING MECHANISM THAT HOLDS THE CONNECTOR THREADED COLLAR TO THE BODY OF THE CONNECTOR WAS DI
- [SDR CA100924004](https://openairdocs.org/sdr/CA100924004.md): Wire Harness · burned · Sep 20, 2010 · Emb ERJ170200SU
  > FOUND HARNESS PEVIOUSLY REPAIRED, WHEN RE-INSPECTED FOUND EVIDENCE OF BURNED HARNESS BEYOND LIMITS. DAMAGE TO HARNESS CAUSED BY PRECOOLER GASKET FAILURE.
- [SDR CA100924002](https://openairdocs.org/sdr/CA100924002.md): Wire Harness · burned · Sep 20, 2010 · Emb ERJ170200SU
  > FOUND HARNESS PEVIOUSLY REPAIRED, WHEN RE-INSPECTED FOUND EVIDENCE OF BURNED HARNESS BEYOND LIMITS. DAMAGE TO HARNESS CAUSED BY PRECOOLER GASKET FAILURE. (SDR20100728002/003 AND 201000802002)
- [SDR CA100728003](https://openairdocs.org/sdr/CA100728003.md): Wire Harness · burned · Jul 21, 2010 · Emb ERJ170200SU
  > WHILE PERFORMING J/C Z419-001ACR-U "DURING THE INSP, PAY PARTICULAR ATTENTION TO HOT AIR LEAKS FROM THE PRE-COOLER ON ELECTRICAL CABLES" --WIRING HARNESS W607 AND CLAMPS IN RT PYLON ARE HEAT DAMAGED FROM HOT AIR LEAKAGE AT PRECOOLER.
- [SDR UALA2009111203527](https://openairdocs.org/sdr/UALA2009111203527.md): Wire · chafed · Nov 11, 2009 · N646UA · Boeing 767322
  > NR 1 ENG OIL FILTER MSSG, FLIGHT DIVERTED. FOUND CHAFED WIRE IN WIRE HARNESS ON TOP OF NR 1 ENG CLOSE TO ELEC CONNECTOR JUNCTION BOX ON PYLON. WIRE WAS CHAFING ON METAL INSULATION BLANKET ON ENG, 3" AFT OF WIRE HARNESS SUPPORT BRACKET. NO STRANDS WHERE BROKE
- [SDR CA090904006](https://openairdocs.org/sdr/CA090904006.md): Wire · chafed · Sep 4, 2009 · Swrngn SA226TC
  > DURING THE COURSE OF AN IMPORT, NACELLE WAS DISCOVERED TO HAVE SEVERAL DAMAGED STRUCTURAL COMPONENTS. ENTIRE SKIN WAS REMOVED FROM INBD SIDE OF THE LT NACELLE. 4 GAUAGE WIRES, RUNNING THROUGH THE NACELLE FROM THE GENERATOR TO GENERATOR RELAY AND FROM WING TO
- [SDR GUUA94132040609A](https://openairdocs.org/sdr/GUUA94132040609A.md): Wire · chafed · Apr 6, 2009 · N17541 · Beech 1900D
  > DURING FLIGHT, DISCOVERED LANDING GEAR CIRCUIT BREAKER POPPED. REPAIRED CHAFED WIRE D6D22 ON TOP LT NACELLE.
- [SDR USA2008F00023](https://openairdocs.org/sdr/USA2008F00023.md): Connector · burned · Aug 23, 2008 · N409US · Boeing 737401
  > CLT FLT1577 AFTER TAKEOFF FROM CLT, CREW REPORTED THE FIRST OFFICER’S GYRO AND IRU FAILING INTERMITTENTLY. ALSO, THE NR 2 AND NR 3 TRANSFORMER/RECTIFIER CIRCUIT BREAKERS WERE TRIPPED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO E
- [SDR 2008UALA03690](https://openairdocs.org/sdr/2008UALA03690.md): Connector · deteriorated · Jul 2, 2008 · Boeing 767322
  > NR 1 ENG HYD BAY (PYLON) CONNECTOR D00916 HAS DETERIORATED INSULATOR.
- [SDR 2008UALA03688](https://openairdocs.org/sdr/2008UALA03688.md): Wire · chafed · Jul 2, 2008 · N657UA · Boeing 767322
  > NR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED.
- [SDR 2008UALA03687](https://openairdocs.org/sdr/2008UALA03687.md): Connector · damaged · Jul 2, 2008 · Boeing 767322
  > NR 1 ENG PYLON HYD BAY CONNECTOR D02118 HAS DAMAGED SOCKET. REPLACED SOCKET AT CONNECT OR D02118P PER BSWPM 20-60-09 AND WDM 78-34-11. OPS CHECKS GOOD ON NR 37006, NR 36897.
- [SDR 2008UALA03686](https://openairdocs.org/sdr/2008UALA03686.md): Wire · damaged · Jul 2, 2008 · N657UA · Boeing 767322
  > NR 1 ENG PYLON HYD BAY WIRE AT CONNECTOR D00 036 PIN 2 (SWITCH S310) IS HEAT DAMAGED. FOUND WIRE AT CONNECTOR D00036 PIN 2 (SWITCH S310) IS HEAT DAMAGE. REPLACED WIRE AT D00036P PER BSWPM 20-61-11 AND WDM 29-32-11. OPS CHECKS GOOD
- [SDR 2008UALA03190](https://openairdocs.org/sdr/2008UALA03190.md): Wire · corroded · Jun 2, 2008 · N538UA · Boeing 757222
  > NR 2 PYLON HAS SEVERAL CORRODED WIRES AT GROUND STUD LOCATION SHEARED FROM GROUND. RE-TERMINATED WIRES IAW BSW PM 20-30-11.
- [SDR 2008UALA01099](https://openairdocs.org/sdr/2008UALA01099.md): Connector · damaged · Feb 29, 2008 · N651UA · Boeing 767322
  > NR 2 PYLON J BOX CONNECTOR D4240J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4266J PER BSWPM 20-63-13. OPS CHECK ACCOMP.
- [SDR 2008UALA01096](https://openairdocs.org/sdr/2008UALA01096.md): Connector · damaged · Feb 29, 2008 · N651UA · Boeing 767322
  > NR 2 PYLON J BOX CONNECTOR D4236J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4236J REF BSWPM 20-63-13. OPS CHECK ACCOMP.
- [SDR 2008UALA01095](https://openairdocs.org/sdr/2008UALA01095.md): Connector · damaged · Feb 29, 2008 · N651UA · Boeing 767322
  > NR 2 PYLON J BOX CONNECTOR D4148J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4148J PER BSWPM 20-63-13. OPS CHECK ACCOMP.
- [SDR 2008UALA01093](https://openairdocs.org/sdr/2008UALA01093.md): Connector · damaged · Feb 29, 2008 · N651UA · Boeing 767322
  > NR 2 PYLON J BOX CONNECTOR D4256J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4256J PER BSWPM 20-63-13. OPS CHECK ACCOMP.
- [SDR CA070219010](https://openairdocs.org/sdr/CA070219010.md): Wire · damaged · Feb 19, 2007 · Bag JETSTM3212
  > (CAN) CREW REPORTED THAT THE AIRCRAFT NR 2 ENGINE STARTED TO SURGE AND THE TORQUE INDICATION FLUCTUATED BETWEEN 0-120 PERCENT. TTL AND SRL COMPUTERS TURNED OFF AND ENGINE SURGE STABILIZED AND CONTINUED TO RUN NORMALLY. INDICATION CONTINUED TO FLUCTUATE. TROUBL
- [SDR QXEA200600886](https://openairdocs.org/sdr/QXEA200600886.md): Wire Harness · chafed · Mar 22, 2006 · N407QX · Bombdr DHC8402
  > PDX: BRAIDED SHIELDING ON WIRE BUNDLE UNDER LEADING EDGE PANEL 611AR IS CHAFED INBOARD OF RT NACELLE INBOARD SIDEWALL. MAINTENANCE REPAIRED IAW Q400 WDM CHAPTER 91 - HOOK-UP LIST, HORIZON EA 6-57-447, AND NDTM PART 6, 51-00-02.
- [SDR SB05118](https://openairdocs.org/sdr/SB05118.md): Connector · burned · Sep 21, 2005 · N430US · Boeing 7374B7
  > BOS - FLT822 - ON FINAL APPROACH TO BOS, THE TR2 AND TR3 CIRCUIT BREAKERS POPPED. CREW INITIATED A GO-AROUND THE FIELD AND POWERED UP THE APU. EVERYTHING WAS NORMAL FOR LANDING. UPON SECOND FINAL APPROACH, THE SAME THING HAPPENED AS WITH THE FIRST APPROACH.
- [SDR CA050427005](https://openairdocs.org/sdr/CA050427005.md): Wire Harness · arced · Apr 22, 2005 · Aerosp ATR42300
  > (CAN) AFTER DEPARTING, THE NR 2 AC GENERATOR WENT OFF LINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE GCU WHICH DID NOT RECTIFY THE PROBLEM. FURTHER INVESTIGATION REVEALED THAT ARCHING BETWEEN THE AC HARNESS AND THE ENGINE CASE AT T
- [SDR 0302156745](https://openairdocs.org/sdr/0302156745.md): Connector · shorted · Dec 10, 2003 · N645NW · Boeing 747222B
  > DURING NR 1 ENGINE START, THE GROUND CREW REPORTED A FIRE IN THE NR 1 ENGINE. THE FLIGHT CREW DISCHARGED BOTH FIRE BOTTLES AND THE GROUND CREW USED GROUND FIRE EXTINGUISHING AGENT TO SUPPRESS THE FIRE. MAINTENANCE INSPECTED THE ENGINE AND FOUND PYLON PLUG D001

Next page: https://openairdocs.org/jasc/5497/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 jasc_code = '5497'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5497/reports

---
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