# Service difficulty reports: JASC 7397

A list on [JASC 7397](https://openairdocs.org/jasc/7397.md).

Reports filed under 7397 · Engine Fuel System Wiring, newest first.

Page 1 of 11 · 532 reports

- [SDR CALA2026092919959](https://openairdocs.org/sdr/CALA2026092919959.md): Wire Harness · faulted · Sep 28, 2026 · N33289 · Boeing 737824
  > REPLACE NR 2 ENG MW0311 HARNESS IAW AMM 73-21-06-400-802-F00, BEFORE DEPARTING SFO DUE HISTORY OF NO BLEED ON NR 2 ENGINE. STARTED REMOVAL OF MW0311 HARNESS FROM FIREWALL DOWN TO STRUT FAIRING. REMOVED AND INSTALLED MW0311 IAW AMM 73-21-06-400-802-F00. REF
- [SDR SWAA2026092113661](https://openairdocs.org/sdr/SWAA2026092113661.md): Ground Wire · failed · Sep 19, 2026 · N8775Q · Boeing 7378
  > AHM MOC MMSG 77-44610 ENGINE N1 VIBRATION IS APPROACHING EXCEEDANCE LIMITS. HJ8A HARNESS CHANGE. REF WDM 77-31-11. FOUND SHIELD GROUND BAD ON HJ8A HARNESS. JOB STOP FOR PARTS TRANSACTION REMOVED AND REPLACED #1 ENG HJ8A ENGINE CONTROL ELECTRICAL HARNESS PER A
- [SDR CALA2026092119613](https://openairdocs.org/sdr/CALA2026092119613.md): Wire Harness · faulted · Sep 18, 2026 · N807UA · Airbus A319131
  > NORMAL START ON NUMBER 1 ENGINE. REJECTED TAKEOFF APPROX 60 KNOTS DUE TO NR 1 EGT READING 162 DEGREES. OTHERWISE NORMAL ENGINE INSTRUMENTS AND ACCELERATION NO SWERVING. ADDED FADEC 1B TEST RESUT PICTURE REF TSM 77-20-00-810-801-B, PERFORMED ENG 1 ECTRICAL CA
- [SDR CALA2026091819530](https://openairdocs.org/sdr/CALA2026091819530.md): Wire Harness · faulted · Sep 16, 2026 · N66893 · Boeing 737924ER
  > FUEL FILTER BYPASS LIGHT FOR NR 1 ENGINE. DEBRIEFED CREW, FUEL FILTER BYPASS LIGHT CAME ON FOR ABOUT 30 MINS, FLIGHT ATTENDANTS REPORTED A FUEL ODOR IN CABIN. THE FUEL BYPASS LIGHT EXTINGUISHED DURING DESCENT & REPORTED THE FUEL ODOR DIMINISHED. THE LIGHT RE
- [SDR YENA2026090100718](https://openairdocs.org/sdr/YENA2026090100718.md): Wire Harness · failed · Aug 29, 2026 · N4080J · Airbus A321271NX
  > FLT 1408, CDG-JFK. (ETOPS). FOUND W04 HARNESS CHAFED AND DAMAGED ON NR 2 ENG. INSTALLED NEW W04 HARNESS PER AMM 73-21-64. REQUIRES OPS CHK CHAFFING TAPE AND FADEC CONNECTORS TO BE INSTALLED."
- [SDR DXTA2026082709424](https://openairdocs.org/sdr/DXTA2026082709424.md): Wire Harness · faulted · Aug 24, 2026 · N831QS · Textrn TEXTRON700
  > ON THE DESCENT WE HAD A WHITE ENG CTRL FAULT L CAS MESSAGE THAT REVERTED TO AMBER ENG CTRL FAULT L UPON LANDING. REMOVED LT ENG W6 WIRE HARNESS AND REPLACED WITH NEW HARNESS IAW LMM 76-10-01. OPS CHECKED GOOD.
- [SDR SWAA20260720694UI](https://openairdocs.org/sdr/SWAA20260720694UI.md): Wire Harness · faulty · Jul 17, 2026 · N225WN · Boeing 7377H4
  > ON CLIMBOUT APPROX 5,000FT NUMBER ONE ENGINE EGT WENT INTO REDLINE & COMPLETED APPROPRIATE QRC AND QRH CHECKLIST AND DIVERTED TO LAX. LANDED NORMALLY WITHOUT ISSUE PERFORMED EA M-21-177-01860 UP TO STEP 19 FOUND CJ10 HARNESS FAULTY. R & R CJ10 HARNESS PER AMM
- [SDR QMLA2026071420046](https://openairdocs.org/sdr/QMLA2026071420046.md): Elec Connector · pulled · Jul 13, 2026 · N404LL · Bell 407
  > RESTART FAULT AND FADEC DEGRADED LIGHTS ILLUMINATED ON TAKE OFF. PULLED FAULT ADAPTOR ELEC CONNECTOR. CLEANED AND REINSTALLED. CLEARED CODE, OPS GROUND RUN GOOD. NO DEFECTS NOTED.
- [SDR 2026FA0000575](https://openairdocs.org/sdr/2026FA0000575.md): Wire Harness · chafed · Jul 9, 2026 · N385L · Diamon DA42NG
  > DUAL ECU FAILURE ON LH ENGINE. EMERGENCY LANDING INTO KBMI. THE DOWNLOAD SHOWED, "PRESSURE CONTROL VALVE POWER FAILURE." WHEN GAINING ACCESS TO THE PRESSURE CONTROL VALVE, THE ENGINE CONTROL HARNESS WAS FOUND TO BE CHAFFING ON THE CYLINDER HEAD AND THE FUEL
- [SDR DXTA2026062208495](https://openairdocs.org/sdr/DXTA2026062208495.md): Wire Harness · faulted · Jun 17, 2026 · N620QS · Cessna 680A
  > WE RECIEVED AN ENG CNTRL FAULT R CAS MESSAGE DURING CRUISE. RAN THE QRH PROCEDURE BUT MESSAGE DID NOT CLEAR. POWERED UP ACFT VIA APU AND INTERROGATED CMC FOUND 2 FAULT CODES SA & SB. BOTH ISSUES HAPPENED AT CRUISE, CONTINUED. GAINED ACCESS TO DCU CONNECTOR IN
- [SDR ANCF20260414009](https://openairdocs.org/sdr/ANCF20260414009.md): Eiu · warning message · Apr 15, 2026 · N951AV · Airbus A320214
  > ENG 1 EIU FAULT COME ON ECAM. IAW AMM 73-25-34-04 CONF 06 THE EIU NR 1 WAS REMOVED AND REPLACED, OPS TEST OF EIU WAS PERFORMED, TESTED OK
- [SDR QMLA2026032120022](https://openairdocs.org/sdr/QMLA2026032120022.md): Wire Harness · faulted · Mar 20, 2026 · N773AL · Bell 407
  > ON SHORT FINAL THE FADEC CHANNEL FAIL CAUTION LIGHT ILLUMINATED; IT WAS FOLLOWED BY THE CHECK INSTRUMENT WARNING LIGHT A SECOND LATER, THEN FINALLY THE FADEC MAINTENANCE LIGHT CAME ON FOLLOWED BY A MARRIED LOSS OF MY NR AND NP NEEDLES. MUCH LIKE A BIT TEST THE
- [SDR CALA2026030214211](https://openairdocs.org/sdr/CALA2026030214211.md): Terminal Block · faulty · Feb 27, 2026 · N14118 · Boeing 757224
  > RTO APPROX 30 KTS. RT ENG LIMITER RT ENG EEC MESSAGES. REPLACED R ENG LIMITER SWITCH MASTER MODULE REF B757-200 AMM 33-13-00-962-041. ADD EMP:U257092 NOTE: RT LIMITER SWITCH S6 WAS REPLACED ON O/H P5 PNL. REF. AMM B757-2 AMM 33-13-00-962-041. EEC, BVCU, AND T
- [SDR ABXA20260203047](https://openairdocs.org/sdr/ABXA20260203047.md): Circuit Card · defective · Feb 3, 2026 · N363CM · Boeing 767338
  > DURING TAXI, IDLE DISAGREE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED OLD, THEN INSTALLED NEW EEC DISCRETE CARD PER AMM 73-21-11. OPS CHECKED GOOD, A/C REMAINS NO ETOPS
- [SDR K11A2025120100359](https://openairdocs.org/sdr/K11A2025120100359.md): Elec Connector · dirty · Dec 1, 2025 · N326FL · Boeing 737883
  > REJECTED TAKEOFF ENGINE NR 1 N1 AT 20% WHILE ENGINE NR 2 WAS AT 70% N2. REMOVED CLEANED AND RE-CONNECTED ELECTRICAL CONNECTORS ON NR 1 ENGINE EEC IAW SWPM 20-60-01. OPS CHECKED NR 1 ENGINE IAW AMM 71-00-00 NO DEFECTS NOTED AT THIS TIME.
- [SDR SWAA2025120241854](https://openairdocs.org/sdr/SWAA2025120241854.md): Elec Connector · disconnected · Nov 29, 2025 · N217JC · Boeing 7377H4
  > AFTER EXITING RUNWAY, AFTER LANDING. NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS.NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOFF COMPARED TO NR 2 ENGINE. NR 1 ENG FUEL PUMP AND HMU R & R PER MT 773-11-00. PS3 CONNECTOR FOUND D
- [SDR YENA2025101401028](https://openairdocs.org/sdr/YENA2025101401028.md): Wire Harness · faulted · Oct 10, 2025 · N2193J · Airbus A321271NX
  > FLT#687, BOS-LAX. (ETOPS) "ENG 2 TURB COOL FAULT ECAM AFTER LANDING. ( TCC/TACC VALVE)REF L/P 4502538 ITEM #2 R/R ON ENG #2 EEC WIRING HARNESS (W03). PERFORMED OPS TEST NO. 15 IAW AMM 73-21-00-710-809-A. ALL BITE CHECK OK. NO FAULTS NOTED. MDDR CLEARED PLACA
- [SDR YENA2025100801012](https://openairdocs.org/sdr/YENA2025100801012.md): Wire Harness · failed · Oct 7, 2025 · N2165J · Airbus A321271NX
  > FLT#72, EDI-JFK. (ETOPS) "ENG 1 FADEC SYS FAULT HAPPENED AT CRUISE FL 350; PERFORMED TSM 77-11-00-810-812A FOUND W04 HARNESS CHAFFED AT N2 SENSOR. REMOVED AND REPLACED W04 HARNESS REF AMM 73-21-64 FADEC SYSTEM TEST OK PERFORMED IDLE RUN REF AMM 71-00-00 ALL PA
- [SDR 2025FA0000673](https://openairdocs.org/sdr/2025FA0000673.md): Wire · damaged · Sep 30, 2025 · Cessna TU206G
  > DURING FLIGHT, PILOT REPORTED FUEL FLOW DISCREPANCY AND ENGINE ROUGHNESS AND RETUNRED TO BASE FOR A PRECAUTIONARY, ALBEIT IF VERY STRESSFUL, LANDING. UPON INSPECTION OF THE FUEL FLOW SENSOR ( PART OF THE JPI 930 ENGINE INSTRUMENTAION - STC SA01435SA) IT WAS
- [SDR AALA202509081643](https://openairdocs.org/sdr/AALA202509081643.md): Elec Connector · dirty · Sep 6, 2025 · N354PT · Boeing 737823
  > AIRCRAFT WAS NOT GROUNDED: RIGHT ENGINE FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLETED QRH PROCEDURE AND ENGINE INDICATIONS WERE NORMAL. CONTINUED TO DESTINATION. EVENTUALLY IT EXTINGUISHED. MAINTENANCE CLEANED CONNECTOR TO DIFFERE
- [SDR DALA2025082406281](https://openairdocs.org/sdr/DALA2025082406281.md): Wire Harness · faulted · Aug 21, 2025 · N544DN · Airbus A321271NX
  > SHIP 5044 -ATO- CREW REPORTED THEY RECEIVED ENG 2 MINOR FAULT MESSAGE AT 60 KNOTS. CONTACTED MCC APPLIED MEL CONTINUED WITH FLIGHT. LATER, REPLACED NBR 2 ENGINE WC08 HARNESS. (LP 7881510)
- [SDR SWAA2025081100403](https://openairdocs.org/sdr/SWAA2025081100403.md): Wire Harness · failed · Aug 5, 2025 · N238WN · Boeing 7377H4
  > NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARNESS PER AM 73-21-06 R&R EEC PER AMM 73-21-60; OPS CK GOOD. C/W RII STEPS FOR HMU; FUEL PUMP PACKA
- [SDR HALA20250804238](https://openairdocs.org/sdr/HALA20250804238.md): Wire Harness · faulted · Aug 4, 2025 · N215HA · Airbus A321271N
  > ETOPS - ENG 1 MINOR FAULT AFTER START. FOUND WC08 HARNESS WIRE SHOWING. REMOVED AND REPLACED PER AMM 73-21-68. PERFROMED IDLE ENGINE RUN. OPS GOOD.
- [SDR NACA2025073100002](https://openairdocs.org/sdr/NACA2025073100002.md): Elec Connector · out of limits · Jul 31, 2025 · N566NC · Boeing 7673BG
  > FOUND THE LEFT ENGINE EEC C2 MAINT MESSAGE. FOUND LH ENG 21B LVDT CONNECTOR 0830OP BETWEEN P2N AND PIN 2 RESISTANCE OUT OF LIMIT REPLACED LH ENG INBD TR LOCK HYD ACTUATOR AND CARRIED OUT INSTALL TEST. ENGINE INFORMATION UNAVAILABLE.
- [SDR NACA2025073000001](https://openairdocs.org/sdr/NACA2025073000001.md): Elec Connector · out of limits · Jul 30, 2025 · N566NC · Boeing 7673BG
  > FOUND THE LEFT ENG EEC C2 MAINT MSG. PERFORMED TIS FOUND LT ENG 21B LVDT CONNECTOR 0834OP BETWEEN P2N & PIN 2 RESISTANCE OUT OF LIMITS IAW FIM TASK 8038-71-01, TASK 848, REV 145. REMOVED AND REPLACED LT ENG INBD TR LOCK HYD ACTUATOR & CARRIED OUT INSTALL TE
- [SDR HALA20250618186](https://openairdocs.org/sdr/HALA20250618186.md): Wire · damaged · Jun 16, 2025 · N216HA · Airbus A321271N
  > ETOPS - DURING FOM FOUND WIRE DAMAGE ON #2 ENG N2 SENSOR O/B 4065KS-J64. FOUND WIRE BUNDLE DAMAGE ON #2 ENG BY TACC (FLAGGED) 4055KS-J31. REMOVED & REPLACED WIRE HARNESS W03 ON ENG #2 PER AMM 73-21-63. EEC OPS CK GOOD. OK FOR SVC
- [SDR YENA2025051900507](https://openairdocs.org/sdr/YENA2025051900507.md): Circuit · failed · May 17, 2025 · N4083J · Airbus A321271NX
  > FLT#33, BOS-CDG. (ETOPS). 'DURING # 1 ENG START ENG 1 FADEC SYS FAULT, AS PER MCC CONTROL RESTART WAS ATTEMPTED WITH SAME RESULT. BOTH ENG SHUTDOWNS HAD ENG 1 FUL VALVE FAULT / F.V NOT OPEN ECAM ON ECNG SHUTDOWN; REMOVED AND REPLACED # 1 ENG IFPC & W-3 HARNES
- [SDR DXTA2025042403169](https://openairdocs.org/sdr/DXTA2025042403169.md): Wire Harness · faulted · Apr 21, 2025 · N793QS · Bombdr BD1001A10
  > R FADEC FAIL AMBER CAS: AT FL410, RECEIVED AN AMBER R FADEC FAIL CAS. RIGHT ENGINE AUTOMATICALLY REDUCED TO IDLE. RAN APPRIATE QRH PROCEDURE FOR DISPLAYED CAS. B3-302584 CORRECTIVE ACTION: REMOVED W5 HARNESS CAREFULLY AND ROUTED OUT OF THE ENGINE. SWAPPED AS
- [SDR CALA2025040103399](https://openairdocs.org/sdr/CALA2025040103399.md): Elec Connector · faulted · Mar 27, 2025 · N13113 · Boeing 757224
  > A/T DIDNT ENGAGE ON TKF RH ENG CAME UP ONLY TO 1.3EPR 50N1/LH EN G CAME UP TO 1.6ERRCREW DE-BRIEF. TOP SPEED REACHED WAS 90 KNOTS. AUTO THROTTLE DID NOT ENGAGE, CREW MANUALLY RAISED THROTTLES TO REDUCED TAKE OFF. WITH THROTTLES MATCHED E1 100% N1 AND E2 AT 50%
- [SDR YENA2025011700067](https://openairdocs.org/sdr/YENA2025011700067.md): Wire Harness · damaged · Jan 15, 2025 · N4058J · Airbus A321271NX
  > FLT#1621, LHR-BOS. (ETOPS) ' FOUND HARNESS ELECTRONIC CONTROL (WC08) CHAFFED AND BURNT; REMOVED AND REPLACED WCO8 HARNESS IAW AMM 73-21-68. OPS CHECK GOOD.'
- [SDR HALA20241202347](https://openairdocs.org/sdr/HALA20241202347.md): Circuit Card · malfunctioned · Nov 29, 2024 · N383HA · Airbus A330243
  > ETOPS - ENG 2 MINOR FAULT. PERFORMED TSM 73-21-809-810-817-A. REMOVED AND REINSTALLED DATA ENTERY PLUS PER AMM 73-21-12. INSPECTED PINS PER 70-50-02-910-802-A.NO DEFECT NOTED. PERFORMED ENG RUN PER AMM 72-00-00-860-816-A.NO DEFECTS NOTED NO FAULTS ON MOTOR
- [SDR CALA2024110801078](https://openairdocs.org/sdr/CALA2024110801078.md): Elec Connector · dirty · Nov 6, 2024 · N14106 · Boeing 757224
  > CTRL SW ENG DID SHUT DOWN BUT STRONG FUEL SMELL IMMED AFTERWARD SEE LP 9791798 - FOLLOWING MULTIPLE ENGINE RUNS AND NORMAL SHUTD OWNS, NO SMELL OR ODOR WAS NOTICED FOLLOWING ENGINE 1 SHUTDOWNS. OK TO CONTINUE. SEE REFERENCED LP FOR PARENT WRITE UP. ON LEFT ENG
- [SDR CALA2024110601053](https://openairdocs.org/sdr/CALA2024110601053.md): Elec Connector · unsecure · Nov 2, 2024 · N13113 · Boeing 757224
  > REPEAT WRITE UP RTO 80 KTS ENGINE 2 WILL NOT GO ABOVE 1.5 EPR REFERENCE FIM 71-06 TASK 807 FOR TROUBLESHOOTING. TOMC-MEREDITH CARRIED OUT TROUBLE SHOOTING AS PER FIM 73-21-00-301. EEC BITE CARRIED OUT PER FIM 73-21-00-902-001-R01, BITE SHOWS FAULT CODE 35 (LV
- [SDR CALA2024100300741](https://openairdocs.org/sdr/CALA2024100300741.md): Transmitter · faulty · Oct 1, 2024 · N225UA · Boeing 777222
  > PERFORMED NO.1 ENGINE FOR FUEL FLOW INDICATION ERRATIC REF AHM 9327445. FOUND INDICATION ERRATIC AT IDLE ABOUT 30LBS UP AND DOWN. NUMBER ONE ENGINE, REMOVED AND REPLACED THE FUEL FLOW TRANSMITTER REFERENCE: TASK 73-31-01-400-803-N01. PERFORMED 5 MINUTE IDLE, L
- [SDR CALA2024092500690](https://openairdocs.org/sdr/CALA2024092500690.md): Wire Harness · faulty · Sep 25, 2024 · N674UA · Boeing 767322
  > CREW REPORTED THAT #2 ENG SN. 727337 (TSI= 28340 HRS). E GT RED ON T-OFF. EGT WENT TO 886 WITH EGT RED ON GAUGE. RETRIEVE EGT EXCEEDANCE AS PER FIM 71-08 FAULT TREE 801 (TAKE PICTURE OF EGT ECXD. PG. & ATTACH TO L/P) REF FIM 71-05 FAULT TREE 810 F OR HIGHT E
- [SDR YENA2024091601276](https://openairdocs.org/sdr/YENA2024091601276.md): Wire Harness · failed · Sep 13, 2024 · N4048J · Airbus A321271N
  > FLT#552, MCO-BOS. (ETOPS) 'RE FL/P 4113863, ITEM 2 (#1 ENG NAI UPSTREAM PT FAULT ON ENG START; REMOVED AND REPLACED #1 ENG PT NACELLE ANTI ICE IAW AMM 30-21-00 FAULT IS STILL PRESENT AT THE MOMENT.) #1 ENG NAI UPSTREAM PT FAULT; REMOVED AND REPLACED # 1 ENG EE
- [SDR CALA2024082700501](https://openairdocs.org/sdr/CALA2024082700501.md): Connector · faulty · Aug 25, 2024 · N422UA · Airbus A320232
  > ENG 1 EPR MODE FAULT CREW REPORTED ENGINE OPERATING IN UNRATED MODE, A/C FAULTING P2T2 SENS/HC/EEC1 REF TSM 73-22-00-810-817-B. NOSE COWL JUST REPLACED PRIOR TO FLIGHT, SUGGEST CHECKING P2T2 PROBE CONNECTION. NO C/B OPENED, PULLED PFR, FAILURE MESSAGE P2 T2
- [SDR AALA202408196892](https://openairdocs.org/sdr/AALA202408196892.md): Wire Harness · faulted · Aug 16, 2024 · N830NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: EGT DISPLAYED AMBER INDICATION ON CLIMBOUT THROUGH FLIGHT LEVEL 200; AIRCRAFT LANDED SAFELY AT DFW. ENGINE NUMBER 2 CJ10 HARNESS REPLACED AND TESTED PER AMM 73-21-06-400-803-F00.
- [SDR HALA20240808218](https://openairdocs.org/sdr/HALA20240808218.md): Wire Harness · damaged · Aug 7, 2024 · N230HA · Airbus A321271N
  > ATB - AIR TURN BACK DUE TO ENG 1 SYS FAULT ON CLIMB OUT. REMOVED AND REPLACED WO3 HARNESS PER AMM 73-21-63 OPS CHECK GOOD. PENDING BIFFLE INSTALL. INSTALLED BIFFLE PER AMM 73-21-63. OK FOR SVC.
- [SDR SWAA2024080822699](https://openairdocs.org/sdr/SWAA2024080822699.md): Wire Harness · disconnected · Aug 5, 2024 · N235WN · Boeing 7377H4
  > RED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 805 AND ACCOMPLISHED EA M-21-177-01860. FOUND CJ10 HARNESS; S3; AND S4 EGT PROBES FAILING RESISTANCE
- [SDR AALA202407024506](https://openairdocs.org/sdr/AALA202407024506.md): Wire Harness · overheated · Jun 24, 2024 · N823NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 ENGINE OVER TEMP AT ABOUT V1 TEMPERATURE REACHED AROUND 970-990 DEGREES; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CVG. REMOVED AND REPLACED J9 (AALA202406254506) HARNESS AND J10 (A
- [SDR AALA202407025825](https://openairdocs.org/sdr/AALA202407025825.md): Wire Harness · overheated · Jun 24, 2024 · N823NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 ENGINE OVER TEMP AT ABOUT V1 TEMPERATURE REACHED AROUND 970-990 DEGREES; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CVG. REMOVED AND REPLACED J9 (AALA202406254506) HARNESS AND J10 (
- [SDR CALA2024061701817](https://openairdocs.org/sdr/CALA2024061701817.md): Connector · loose · Jun 14, 2024 · N456UA · Airbus A320232
  > ENG 2 EPR MODE FAULTON CLMB OUT.OTHER ENG IDICATIONS WERE GOOD. CLEANED AND RECONNECTED, NO DMG NOTED AT THIS TIME. REF TSM 73-22-00-810-818-B AND AWM 71-51-04 PG 3 PIREP FAULT APPEARED ON CLIMBOUT FL17, EPR AMBER XX AND CREW UPDATING WITH FADEC 2A FINDINGS FO
- [SDR YENA2024051700766](https://openairdocs.org/sdr/YENA2024051700766.md): Wire Harness · exposed · May 17, 2024 · N4073J · Airbus A321271N
  > FLT#43, JFK-LGW. (ETOPS) 'WHILE DOING T/C A7323059-01 FOUND 4065KS -J63 WIRE EXPOSED; REFER TO LOGPAGE 4020011 ITEM #2 (R/R W04 HANRESS IAW AMM 73-21-64. REF FOLLOWING LOGPAGES FOR REQUIRED OPERATIONAL CHECKS LP 4020013. ITEM 1 (ACCOMPLISHED #6 IDLE TEST IAW A
- [SDR YENA2024030600363](https://openairdocs.org/sdr/YENA2024030600363.md): Wire Harness · chafed · Mar 3, 2024 · N4074J · Airbus A321271N
  > FLT#1621, LHR-BOS. (ETOPS)' #1 ENG W03 HARNESS CHAFED; REMOVED AND REPLACED #1 ENG W03 HARNESS IAW AMM 73-21-63.'
- [SDR DALA2023121510277](https://openairdocs.org/sdr/DALA2023121510277.md): Unknown · unknown · Dec 14, 2023 · N511DE · Airbus A321271N
  > SHIP 5011 DURING WATERWASH ON ENGINE 1 FOUND W4 HARNESS DAMAGED/ CHAFING. CORRECTIVE ACTION: REPLACED W4 HARNESS PER A321NEO AMM 73-21. OPS CHECKS GOOD. (5072307)
- [SDR ASAA2023110546009](https://openairdocs.org/sdr/ASAA2023110546009.md): Wire Harness · damaged · Nov 5, 2023 · N530AS · Boeing 737890
  > WHILE PERFORMING T/C N842001 RIGHT ENG FOUND J9 HARNESS DAMAGED. GROUNDED - YES. REPLACED NEW J9 HARNESS AND PERFORMED INSTALLATION TEST GOOD AMM 73-21-06/401.
- [SDR ASAA2023110245988](https://openairdocs.org/sdr/ASAA2023110245988.md): Wire Harness · faulty · Nov 2, 2023 · N423AS · Boeing 737990ER
  > PIECE OF ELECTRICAL CONNECTOR FELL OUT OF #1 ENGINE WHILE OPENING REVERSER. ALT. DEACTIVATION PROCEDURES USED PER CHP 5, TABLE 3, ITEM 7. GROUNDED - YES. FOUND CONNECTOR DP1102 DAMAGE & DISCONNECTED FROM ENG #1 BEED AIR REGULATOR. ENG HARNESS MW0311 REQUIRES R
- [SDR ASAA2023101745712](https://openairdocs.org/sdr/ASAA2023101745712.md): Wire Harness · damaged · Oct 17, 2023 · N459AS · Boeing 737990ER
  > MW311 HARNESS, #2 ENGINE, HAS DAMAGE NEXT TO BLEED AIR REGULATOR. GROUNDED - YES. REMOVED AND PARTIALLY INSTALLED SERVICEABLE MW0311 REF MM 73-21-06. 4 C/B'S TAGGED.RM 53815 10/17/2023 COMPLETED INSTALLATION OF MW0311, REF AMM 73-21-06 PERFORMED GROUND WING TA
- [SDR CALA2023101803107](https://openairdocs.org/sdr/CALA2023101803107.md): Connector · loose · Oct 16, 2023 · N836UA · Airbus A319131
  > EPR MODE FAULT - ENG 1. REFER TO TSM CHAPTER 77 ECAM AND UAL A32 0 MEL CARD 73 120. P2 T2 SENSOR FAULT ON POST FLIGHT REPORT INSPECTED AND FOUND CONNECTOR "B" LOOSE ON ENGINE 1 P2/T2 SENSOR. RESECURED AND NO FAULT MSG ACTIVE AT THIS TIME. REQUIRES OPS CHECK. A

Next page: https://openairdocs.org/jasc/7397/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 = '7397'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/7397/reports

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