REPAIRED AND REPOSITIONED WIRE BUND (N1997A) - [SDR UIEA2019030503479](https://openairdocs.org/sdr/UIEA2019030503479), Mar 5, 2019: Boeing 76736N. WIRE HARNESS. CHAFED. ENGINE NR 1 WIRE HARNESS RUBBING ON HPSOV SUPPORT BRACKET(
REROUTED ENG NR 1 WIRE HARNESS PER W/D 71-51-52 AND SWPM 20 (N1013A) - [SDR ASAA2018121067271](https://openairdocs.org/sdr/ASAA2018121067271), Dec 6, 2018: Boeing 737890. WIRE HARNESS. DAMAGED. FOUND DAMAGE ON MW311 HARNESS ON #2 ENG. GROUNDED - YES. REMOVED AND REPLACED MW311 HARNESS ON #2 ENG PER B737-800 AMM 7 (N562AS) - [SDR PRIA20170725001](https://openairdocs.org/sdr/PRIA20170725001), Jul 24, 2017: Amd FALCON900B. WIRE HARNESS. SHORTED. CRUISE ALTITUDE FL410 ENG NR 1 COMPUTER LIGHT ILLUMINATED WITH SLIGHT RPM ROLLBACK. FOLLOWED CHECKLIST, RESETTING COMPUT (N454AJ) - [SDR UIEA2017040300494](https://openairdocs.org/sdr/UIEA2017040300494), Apr 5, 2017: Boeing 767375. FEEDER CABLE. CHAFED. FWD STRUT FEEDER WIRES FOUND WITH CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPE IAW SWPM 20-10-13, REV 64, AND FOU (N1217A) - [SDR UIEA2017040300495](https://openairdocs.org/sdr/UIEA2017040300495), Apr 5, 2017: Boeing 767375. FEEDER CABLE. CHAFED. FWD STRUT, TWO FEEDER WIRES FOUND CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPES IAW SWPM 20-10-13, REV 64, AND FO (N1217A) - [SDR G41A20160628002](https://openairdocs.org/sdr/G41A20160628002), Jun 24, 2016: Lear 55LEAR. WIRE. PULLED. ON THE AFTERNOON OF 6-24-2016, ACFT DEPARTED, AT FL290, THE CAPTAIN NOTICED THE NR 2 ENGINE HAD STARTED A SLIGHT ROLLBAC (N824MG) - [SDR DALA2016051103852](https://openairdocs.org/sdr/DALA2016051103852), May 8, 2016: Boeing 717200. WIRE HARNESS. DAMAGED. THE FLIGHT WAS DIVERTED FOLLOWING THE SHUTDOWN OF THE NR 2 ENGINE. ALSO, ALL OF THE ENGINE COWLING EXITED THE ACFT WHILE (N939AT) - [SDR ASAA2016010614665](https://openairdocs.org/sdr/ASAA2016010614665), Jan 6, 2016: Boeing 737890. CONNECTOR. CONTAMINATED. DURING IDG OIL CHANGE FOUND CONNECTOR PLUG TO NR 2 ENGINE DRIVEN HYDRAULIC PUMP SHUTOFF SOLENOID DISCONNECTED. ACFT GROU (N513AS) - [SDR CA150824006](https://openairdocs.org/sdr/CA150824006), Aug 15, 2015: Dhav DHC8102. DIODE. BURNED. (CAN) DURING PRE-FLIGHT CHECK, FLIGHT CREW REPORTED AN INDICATION PROBLEM WITH THE RIGHT ENGINE FUEL EMERGENCY SHUT-OFF - [SDR DATA2015033101](https://openairdocs.org/sdr/DATA2015033101), Mar 31, 2015: Stbros SD360300. WIRE. BROKEN. ON TAKEOFF ROLL RT ENG RTOP SYS FAILED TO ACTIVATE. TAKEOFF WAS ABORTED IAW ACC SOP'S. ACFT RETURNED TO BLOCK. UPON TROU (N376AC) - [SDR HYIA20150206001](https://openairdocs.org/sdr/HYIA20150206001), Feb 1, 2015: Cessna 402C. WIRE HARNESS. CHAFED. PILOT REPORTED SEEING SMOKE FROM RT ENG ON SHUT DOWN. FURTHER INVESTIGATION FOUND CHAFED WIRE HARNESS IN RT ENG BAY. ACF (N401TJ) - [SDR SIMA20141124004](https://openairdocs.org/sdr/SIMA20141124004), Nov 24, 2014: Emb EMB145LR. WIRE HARNESS. CHAFED. IN FLIGHT AFTER EXITING ICING CONDITION E2 ANTI-ICE FAIL WITH VLV IN OPEN POS, SHOULD HAVE CLOSED. RESET IAW AOM VOL 1 P (N665BC) - [SDR CA141104012](https://openairdocs.org/sdr/CA141104012), Oct 31, 2014: Boeing 727223. WIRE. FAILED. (CAN) NR 3 ENGINE OIL TEMP INDICATION PEGGED PAST RED BAND. SUPPLEMENTAL CHECK LIST COMPLIED WITH AND ENGINE SHUTDOWN. M - [SDR CALA2014032490677](https://openairdocs.org/sdr/CALA2014032490677), Mar 24, 2014: Airbus A320232. WIRE. CHAFED. IAW TO EM4478-1 SEQ 3512011 FOUND CHAFED WIRE IN 90 DEGREE CONNECTOR 4021KS-A, WIRE GOES TO SOCKET E WIRE 5B416B20. (N408UA) - [SDR CA130215005](https://openairdocs.org/sdr/CA130215005), Feb 11, 2013: Dhav DHC8311. CONNECTOR. CONTAMINATED. (CAN) DURING THE PUSHBACK WITH BOTH ENGINES RUNNING IN FEATHER, NR 2 ENGINE TORQUE STARTED TO CLIMB AND WAS SHUTDOWN. IM - [SDR YENA20130204029](https://openairdocs.org/sdr/YENA20130204029), Feb 4, 2013: Emb ERJ190100IGW. WIRE HARNESS. FAILED. FLT 1794 NAS-FLL, CREW DECLARED EMERGENCY AT 18000 FT AND LEVEL DUE TO OIL PRESSURE LOW EICAS AND OIL PRESSURE. SHUTDOWN (N193JB) - [SDR NSVA20120311470](https://openairdocs.org/sdr/NSVA20120311470), Mar 11, 2012: Bombdr DHC8402. CONNECTOR. DIRTY. RETURNED TO GATE DUE TO POWERPLANT MESSAGE. MX OPENED ENGINE COWLS, CLEANED CONNECTORS PER FIM, ENGINE RUNS AND OP'S CHE (N345NG) - [SDR CA080828006](https://openairdocs.org/sdr/CA080828006), Aug 27, 2008: Beech 200BEECH. WIRE. OUT OF POSITION. (CAN) WHEN DESCENDING THROUGH FL 180, CREW NOTICED RT ENG WOULD NOT GO BELOW 1600 FT/LBS TORQUE WITH PWR LEVER AT FLIGHT - [SDR QXEA200600829](https://openairdocs.org/sdr/QXEA200600829), Mar 27, 2006: Bombdr DHC8402. CONNECTOR. LOOSE. PDX FLIGHT NR 2383: POWERPLANT MESSAGE ON ED DURING TAXI. MAINTENANCE INSPECTED NR 2 FADEC IAW AMM FIM TASK 73-20-00-810 (N415QX) - [SDR 03FDEA01206](https://openairdocs.org/sdr/03FDEA01206), Aug 3, 2003: Doug DC1030. HEAT SHIELD. CRACKED. NR 473 NR 3 ENG AFT ELECTRICAL JUNCTION BOX HEAT SHIELD IS CRACKED. REMOVED AND REPLACED HEAT SHIELD IAW SRM 51-31-01 @ (N311FE) - [SDR HEEA088432](https://openairdocs.org/sdr/HEEA088432), Jul 19, 2003: Aerosp AS355*. WIRE HARNESS. FAILED. RED GOVERNOR LIGHT ON GROUND RUN UP. FAULT CODE 129 FAIL CODE 4002. (N972AE) - [SDR IXXA0300008O](https://openairdocs.org/sdr/IXXA0300008O), Jan 28, 2003: Doug DC871. CONNECTOR. DIRTY. AFTER DEPARTURE FROM LRD DURING CRUISE CREW NOTED NR 3 ENGINE EGT ROSE ABNORMALLY. CREW SHUTDOWN NR 3 ENG PER COMPANY PO (N829BX) - [SDR HEEA076250](https://openairdocs.org/sdr/HEEA076250), Oct 3, 2001: Snias AS350B. HARNESS. ERRATIC. T-4 ERRATIC. PENDING VENDOR RETURN. (N856PH) - [SDR CA011012005](https://openairdocs.org/sdr/CA011012005), Sep 10, 2001: Amd FALCON50MYST. HARNESS. FAILED. (CAN) ON CLIMB THROUGH 7,000 FT, ENGINE NR 3 N1 ROLL BACK APPROXIMATELY 10 PERCENT. IGNITION LIGHT WOULD COME ON AND ENG - [SDR 97ZZZX4085](https://openairdocs.org/sdr/97ZZZX4085), Apr 5, 1997: Doug MD900. WIRE HARNESS. CORRODED. ELECTRICAL WIRING HARNESS INSTALLATION. REMOVED DUE TO EXCESSIVE CORROSION ON PMA PLUG. REMOVED UNIT FROM LOANER ENGINE. (N901CF) - [SDR 96ZZZX5401](https://openairdocs.org/sdr/96ZZZX5401), Sep 1, 1996: Piper PA31T. WIRE. SHORTED. WIRES IN THE ENGINE COMPARTMENTS RUNNING BY EXHAUST DUCTS ARE MELTING AND SHORTING OUT DUE TO LONG TERM EXPOSURE TO HEAT (N737WB) ## Other codes in chapter 71 - [JASC 7100](https://openairdocs.org/jasc/7100): Powerplant System (634 reports) - [JASC 7110](https://openairdocs.org/jasc/7110): Engine Cowling System (2,324 reports) - [JASC 7111](https://openairdocs.org/jasc/7111): Engine Cowl Flaps (57 reports) - [JASC 7112](https://openairdocs.org/jasc/7112): Engine Air Baffle Section (27 reports) - [JASC 7120](https://openairdocs.org/jasc/7120): Engine Mount Section (3,028 reports) - [JASC 7130](https://openairdocs.org/jasc/7130): Engine Fireseals (66 reports) - [JASC 7160](https://openairdocs.org/jasc/7160): Engine Air Intake System (1,161 reports) - [JASC 7170](https://openairdocs.org/jasc/7170): Engine Drains (130 reports) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.