JASC 7397

Service difficulty reports · 532

Reports filed under 7397 · Engine Fuel System Wiring, 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 jasc_code = '7397'
  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.

SDR ASAA2017012819914Wire Harness · faultedNR 1 ENGINE SHOWS MESSAGES 75-10601 (TBV POSITION SIGNALS DISAGREE) SHORT TIME FAULT, 75-10591 (TBV POSITION SIGNALS DISAGREE) LONG TIME FAULT, AND 75-20601 (TBV POSITION SIGNALS DISAGREE), SHORT TIME FAULT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINEJan 28, 2017 · N569AS · Boeing 737890SDR ASAA2016121519071Connector · corrodedON TAXI LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED FOR 30 SECS. ENGINE WAS AT IDLE POWER. GROUNDED - YES. ACCOMPLISHED FIM 73-05 TASK 801 FOUND MAINT MESSAGE 73-31071. NR 1 ENG FUEL DIFFERENTIAL PRESSURE SWITCH CONNECTOR RUSTY. INSTALLED SERVICEABLE FUEL FILTERDec 15, 2016 · N560AS · Boeing 737890SDR CALA2016120901046Wire Harness · faultyAT FL 310 CLIMB, 98% N1, NR 1 EGT WENT TO 912 DEGREES, WHILE NR 2 WAS 750 DEGREES. EGT WAS CONTROLLABLE WITH REDUCTION OF THRUST, UNABLE TO MAINTAIN CLIMB POWER WITHOUT REACHING TEMP LIMIT. R & R THE J10 HARNESS IAW MM 73-21-06. FADEC TEST NORMAL IAW 73-21-00Dec 9, 2016 · N37413 · Boeing 737924ERSDR ASAA2016112618840Connector · corrodedAFTER STARTING THE NR 1 ENGINE THE FILTER BYPASS LIGHT ON THE FUEL PANEL ILLUMINATED. ACFT GROUNDED. VERIFIED ALL C/B'S ARE CLOSED AND PERFORMED EEC BITE AND FOUND MAINTENANCE MESSAGE 73-31071. OPENED NR 1 ENGINE FAN COWL AND PERFORMED FIM TASK 73-05 TASK 80Nov 26, 2016 · N559AS · Boeing 737890SDR SWAA2016102408979Wire Harness · faultyNR 2 ENGINE AT FL410, EGT SURGED TO 810 DEGREE. RAN SURGE QRC/QRH AND HAD TO RUN NR 2 AT IDLE TO MAINTAIN EGT 500 DEGREE. DID NOT SHUT DOWN NR 2. USED ENGINE NORMALLY AT 10,000 MSL. NO VIBRATION NO N1/N2 OR OIL ISSUES. JUST ERRATIC EGT UNTIL LOWER ALTITUDE. Oct 22, 2016 · N202WN · Boeing 7377H4SDR DXTA2016101206318Wire Harness · faultedCLIMBING THROUGH 11,000 FEET AT 93 % N1, THE NR 1 ENGINE COMPUTER LIGHT ILLUMINATED. THE LEFT ENGINE ROLLED BACK APRX 20 % N1. QRH CHECKLIST WAS COMPLETED. LIGHT REMAINED ILLUMINATED THE ENTIRE TIME UNTIL ENGINE SHUTDOWN. REMOVED AND REPLACED THE LT ENGINE WOct 12, 2016 · N811QS · Raythn HAWKER800XPSDR ASAA2016100518225Connector · damagedFOUND FAULT CODE 75-20832 ON NR 2 ENGINE CDU CHECK. THE T3 SIGNAL IS OUT OF RANGE LONG TERM FAULT. ACFT GROUNDED. ACCOMPLISHED T/S FOR FAULT 75-20832 IAW FIM 75-33 TASK 803 - EEC BITE SHOWED FAULT LOGGED FOR TWO OUT OF TEN LEGS AND INPUT MONITORING SHOWED COct 5, 2016 · N457AS · Boeing 737990ERSDR ASAA2016100318224Wire Harness · chafedNR 1 ENG CJ9 HARNESS HAS CHAFING DAMAGE NEAR 3'OCLOCK STRUT IN CORE NEAR HPTACCV ESN896938. ACFT GROUNDED. REPAIRED IAW AMM 70-70-01-350-801-F00. PERFORMED ALL TESTS PER POWER PLANT REF TABLE IAW AMM 71-00-00, ALL TESTS PASS.Oct 3, 2016 · N517AS · Boeing 737890SDR ASAA2016100318223Wire Harness · chafedNR 1 ENGINE CJ10 HARNESS HAS CHAFFING DAMAGE NEAR 3'OCLOCK STRUT AT HPTACCV ESN896938. ACFT GROUNDED. REPAIRED THE HARNESS IAW AMM 70-70-01-350-801-F00. PERFORMED ALL TESTS PER POWERPLANT TEST TABLE PER B737-800 AMM 71-00-00 ALL TESTS PASS.Oct 3, 2016 · N517AS · Boeing 737890SDR CALA2016092700700Wire Harness · damagedRT ENGINE HAS 3 FAULTS AND IS SURGING N1 AND N2 89-96%. EEC WILL NOT REVERT TO ALT. ENG IGN RT ENG C1 RT ENG CTL RT THERE IS NO PROCEDURE FOR THE PILOT TO MANUALLY SELECT ALTERNATE MODE. DIVERTED TO EWR.. R & R THE T25 SENSOR, W725 AND W726 ELECTRICAL HARNESep 27, 2016 · N69020 · Boeing 777224SDR ASAA2016092118100Wire Harness · out of toleranceWHILE PERFORMING TASKCARD 78273000, FMC, CDU FAULTS FOUND A FAULT ON THE NR 1 ENGINE, FAULT CODE 75-10371, HMU VSV IS OUT OF RANGE. SHORT TERM FAULT OF 50 HRS. ACFT GROUNDED. R & R J5 HARNESS, REF AMM 73-21-06. ELECTRONIC ENGINE CONTROL TEST GOOD, REF AMM Sep 21, 2016 · N594AS · Boeing 737890SDR ASAA2016091518016Wire Harness · faultyENGINEERING REQUEST FOLLOW UP FOR HISTORY OF T25 FAULTS ON NR 1 ENGINE. ETOPS SIGNIFICANT SYSTEM. ACFT GROUNDED. ACCOMPLISHED STEP 1 AND STEP 2 OF TSR. R & R J9 HARNESS ON NR 1 ENGINE REF AMM 73-21-06-400-802-F00. ACCOMPLISHED FADEC SYSTEM TEST REF AMM 73Sep 15, 2016 · N594AS · Boeing 737890SDR ASAA2016080917660Wire Harness · corrodedWHILE ACCOMPLISHING T/C N8420001, FOUND NR 2 ENGINE CJ10 WIRE HARNESS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE WIRE HARNESS IAW AMM 73-21-06, OPS CHECKED NORMAL.Aug 9, 2016 · N531AS · Boeing 737890SDR HNAA2016072500228Connector · dirtyDOWNLOADED CMC AND FOUND ND ENG 2 COMM A AND B MESSAGES. TROUBLESHOT IAW FIM 77-44-00-810-807 AND ARRIVED AT BLOCK 09. CLEANED THE J2 CONNECTOR AND RECEPTACLES AS REQUIRED. PD PU EICAS MESSAGES EXTINGUISHED OK FOR SERVICEJul 22, 2016 · N637AE · Emb EMB145SDR ASAA2016071917435Connector · dirtyPERFORMED TASK CARD 78273000, NR 1 ENGINE HAD LONG TIME FAULT 75-20831 - THE T3 SIGNAL IS OUT OF RANGE. ACFT GROUNDED. IAW FIM 75-33, TASK 802. ACCOMPLISHED INITIAL EVALUATION IAW FIM 75-36, TASK 802, STEP E. FAULT ACTIVE. CLEANED CONNECTORS DP0905 AND Jul 19, 2016 · N530AS · Boeing 737890SDR ASAA2016070417265Wire Harness · failedIAW TASK CARD 78273000, PERFORMED INTERROGATION TEST FOUND NR 2 ENGINE MESSAGE 75-10822. THE T25 SIGNAL IS OUT OF RANGE. ACFT GROUNDED. IAW FIM 75-33 T805, ACCOMPLISHED RESISTANCE CHECKS AT T25 SENSOR & DP0909 / DP1010. ALL CHECKED NORMAL. A & B CHANNELJul 4, 2016 · N474AS · Boeing 737990ERSDR CALA2016070195501Connector · looseNR 2 ENGINE INCREASING SURGE DURING CLIMB, CLOSE TO NORMAL AT IDLE. FOUND J1 EEC CONNECTOR LOOSE. SECURED, PERFORMED POWER ASSURANCE RUNS TWICE. ALL ENGINE PARA NORMALJun 28, 2016 · N822UA · Airbus A319131SDR ASAA2016062517160Connector · contaminatedWHILE ACCOMPLISHING T/C 7827300 FAULT CODE, APPEARED ON NR 2 ENGINE. THE FMV POSITION SIGNALS DISAGREE. MUST BE CORRECTED IN 50 HRS. ACFR GROUNDED. REF LOG 11622130 FOR WORK ACCOMPLISHED. INITIAL EVALUATION HAD EEC CHANNEL B HMU RESOLVER COSINE RESISTANCEJun 25, 2016 · N423AS · Boeing 737990ERSDR ASAA2016062217104Wire Harness · faultyNR 1 ENGINE TREND DATA CONTINUES TO SHOW EGT TRENDS AND DATA SCATTER INDICATIVE OF EGT SYSTEM INDICATION ERRORS. ACFT GROUNDED. R & R J9, PN 325-025-401-0, J10 325-043-502-0, AND CJ10, PN 325-043-401-0, NR 1 ENGINE HARNESS IAW AMM 73-21-06.Jun 22, 2016 · N597AS · Boeing 737890SDR ASAA2016061117021Connector · contaminatedWHILE ACCOMPLISHING T/C 78273000, FMC CDU FAULTS, FOUND NR 2 ENGINE FAULT CODE 75-10802, T25 SIGNAL DISAGREE, SHORT TERM. ACFT GROUNDED. REF L/P 11678020 FOR FAULT CODE 75-20802. REACCOMPLISHED T/C 78273000 FAULT CODE FOR NR 2 ENGINE 75-10802. NO LONGER PRJun 11, 2016 · N474AS · Boeing 737990ERSDR UIEA2016051700327Connector · dirtyRIGHT EEC INOPERATIVE STATUS MSG RT ENG CONTROL. PERFORMED FIM 73-21 TREE 878 & NO MSGS ON RT PIMU BITE TEST 71-01-00 201. RESET & CLEANED RT HMU ELEC CONNECTORS. PERFORMED HI POWER ENG RUN IAW AMM 71-00-00 501 CONFIG 3. NO FAULTS SYS OK FOR SERVICE.May 17, 2016 · N640GT · Boeing 7673S1SDR ASAA2016040716317Wire Harness · failedON TAXI IN, NR 2 ENGINE CONTROL LIGHT CAME ON. ACFT GROUNDED. ACCOMPLISHED BITE. FOUND FAULT CODE 75-20582, TBV DEMAND AND POSITION SIGNALS DISAGREE. R & R NR 2 ENGINE J10 HARNESS IAW AMM 73-21-06. OPS CHECK NORMAL.Apr 7, 2016 · N530AS · Boeing 737890SDR QMLA2016022916013Connector · dirtyTHE PILOT REPORTED THAT UPON TAKEOFF WITH CREW & PATIENT ONBOARD HE HEARD A WARNING TONE AS HE WAS CLIMBING & TRANSITIONING TO FWD FLIGHT. HE IMMEDIATELY REDUCED POWER & GLANCED AT THE CAUTION & WARNING PANEL & VEMD. THERE WAS AN EXCEEDANCE DETECTED INDICATIFeb 29, 2016 · N259AM · Urocop EC130B4SDR ASAA2016020315237Connector · looseHISTORY OF FAULT CODE 75-10581, TBV DEMAND AND POSITION SIGNAL DISAGREE. ACFT GROUNDED. ACCOMPLISHED ELECTRIC ENGINE CONTROL TEST AND ACTUATORS TEST ON NR 1 ENGINE REF AMM 71-00-00-700-807-F00, NO FAULTS LOGGED. ACCOMPLISHED FIM 75-23, TASK 801, ALL RESISTAFeb 3, 2016 · N529AS · Boeing 737890SDR M3XA2016012402Connector · loosePILOT & CREW WERE COMING IN WITH A PATIENT ONBOARD. ENROUTE TO THE HOSPITAL PILOT ENCOUNTERED A FADEC FAULT ILLUMINATION ON THE CWP. TAKING PRECAUTIONARY MEASURES, THE PILOT LANDED AT THE MX FACILITY WHICH WAS CLOSER THAN THE HOSPITAL. THE PATIENT WAS THEN Jan 24, 2016 · N522MT · Bell 407SDR U5QA201601060073Connector · dirtyDURING CLIMB OUT RT ENG ROLLED BACK TO LESS THAN 35% N1. AUTO RELIGHT ENGAGED & ENG STARTED & RETURNED TO NORMAL. TROUBLE SHOT, CLEANED CONNECTORS ON EEC & RANG N2 SENSORS WITH SATISFACTORY RESULTS. SWAPPED EEC'S FROM SIDE TO SIDE & CLEANED CONNECTORS. ENGJan 2, 2016 · N405DC · Lear 60LEARSDR ASAA2015112013908Connector · dirtyDURING COMPLETION OF TC 78273000, FOUND FAULT 73-21272, "THE ALTERNATOR VOLTAGE INPUT TO THE ELECTRONIC ENGINE CONTROL IS OUT OF RANGE" SHORT TIME FAULT, NR 2 ENGINE, ESN 895-406, ACFT GROUNDED. PERFORMED FIM 73-27, TASK 804. FOUND DIRTY CONNECTOR AT NR 2 B Nov 20, 2015 · N566AS · Boeing 737890SDR ASAA2015102713542Connector · looseON DECK AT IDLE, NR 1 FILTER BYPASS ILLUMINATED FOR APPROXIMATELY 2 MINUTES, THEN WENT OUT ON ITS OWN. NO ENGINE ABNORMALS OBSERVED. ACFT GROUNDED. FOUND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH CONNECTOR PLUG LOOSE. CLEANED AND SECURED CONNECTOR PLUG ON FOct 27, 2015 · N513AS · Boeing 737890SDR ASAA2015102213522Connector · looseACOMPLISHING TASKCARD 78273000, FOUND NR 2 ENGINE SHORT TIME FAULT 73-10342, THE FMV POSITION SIGNAL IS OUT OF RANGE, LONG TIME FAULT 75-10392 THE VSV POSITION SIGNAL IS OUT OF RANGE, AND LONG TIME FAULT 75-10442 THAT VBV POSITION SIGNAL IS OUT OF RANGE. ACFT Oct 22, 2015 · N530AS · Boeing 737890SDR ASAA2015102113489Connector · unsecureDURING ELECTRONIC ENGINE CONTROL TEST 73-21-700-800-F00, FOUND 3 MAINTENANCE MESSAGES. 73-10752, 75-10892 AND 73-20762. ACFT GROUNDED. FOUND PIN ON NR 2 ENGINE ID PLUG NOT SEATED. SEATED PIN IAW MM 73-21-61-800, ELECTRONIC ENGINE CONTROL TEST PASSED.Oct 21, 2015 · N565AS · Boeing 737890SDR ASAA2015090412954Wire Harness · failedDURING TAXI IN, AFTER CHANGING POWER SOURCE, SHIP POWER APU-NOTICED NR 1 ENGINE FILTER BYPASS LIGHT ILLUMINATED. ACFT GROUNDED. REMOVED & REPLACED ENGINE 1. J8 HARNESS IAW AMM 73-21-06-000-801-F00, PERFORMED ELECTRONIC ENGINE CONTROL TEST IAW AMM 73-21-00-7Sep 4, 2015 · N568AS · Boeing 737890SDR ASAA2015082012931Wire Harness · unknownWHILE ACCOMPLISHING TASK CARD 78273000, FOUND FAULT FMV POSITION SIGNAL IS OUT OF RANGE. MSG NR: 73-10342. SHORT TERM. NR 2 ENGINE. FOUND FAULT VSV POSITION SIGNAL IS OUT OF RANGE. MSG 75-10392. LONG TERM, NR 2 ENGINE. FOUND FAULT VSV POSITION SIGNAL ISAug 20, 2015 · N530AS · Boeing 737890SDR ASAA2015081112841Connector · disconnectedAFTER LANDING ON TAXI-IN, NR 1 ENGINE FILTER BYPASS LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM TASK 73-05, TASK 801. FOUND ELECTRICAL CONNECTOR OF THE J8 WIRE HARNESS DISCONNECTED FROM SWITCH RECEPTACLE. RECONNECTED CONNECTOR AS NEEDED ON FUEL FILTAug 11, 2015 · N568AS · Boeing 737890SDR ASAA2015071812489Wire Harness · damagedNR 1 ENGINE EGT SHOWED HIGH TEMPERATURE EXCEEDANCE. ON TAKEOFF, APPROXIMATELY 1000 DEGREES FOR A FEW SECONDS. AUTO THROTTLES WERE ON ENGINE OPERATED NORMALLY AFTER THAT EVENT. AT CRUISE NR 1 ENGINE TEMPERATURE SHOWED 30 DEGREES HIGHER THAN NR 2 ENGINE. ACFJul 18, 2015 · N586AS · Boeing 737890SDR AALA20150705001Wire Harness · faultyAFTER THRUST PUSHED UP FOR TAKEOFF NR 1 ELEC ENG CONTROL LIGHT ILLUMINATED. TAKEOFF ABORTED AT LOW SPEED. R & R HARNESS HAR 5423 IAW AMM 73-21-06-400-802-F00. ACCOMPLISHED TEST AS REQUIRED WITH NO FAULTS NOTED.Jul 5, 2015 · N922AN · Boeing 737823SDR ASMF201507018Wire · damagedAIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISION TO LT ENG, DETECTING LT HIGH PRESS FUEL SOV POSITION IN DISAGREE WITH COMMAND POSITION. THE FIMJun 29, 2015 · N776AM · Boeing 7772Q8SDR ASAA2015062912271Wire Harness · chafedNR 2 ENGINE RT SIDE CORE AREA WIRE HARNESS J9 AND J10 INPUTS TO T3 SENSOR, CONNECTORS DP0905 AND DP1005, HAVE CHAFED THROUGH WIRE HARNESS CLOTH OVERBRAID. ACFT GROUNDED. REPAIRED NR 2 ENGINE CHAFING WIRE HARNESS J9 AND J10 CLOTH OVERBRAND NEAR T3 SENSOR, CONJun 29, 2015 · N512AS · Boeing 737890SDR ASAA2015061112081Wire Harness · not reportedNR 1 ENGINE HAS FAULT CODE 75-10361, HPTACC POS. SIGNAL OUT OF RANGE. ECONOMIC FAULT. ACFT GROUNDED. TSR ISSUED. REPLACED J9 HARNESS IAW MM 73-21-06-400-802-F00, OPS NORMAL IAW MM 73-21-00-700-804-F00, EEC TEST AND MM 71-00-00-700-807-F00, ACTUATOR TEST.Jun 11, 2015 · N536AS · Boeing 737890SDR N6WA2015060601Connector · dirtyLEFT FADEC CAUTION IN FLIGHT. CLEANED CONNECTORS ON THE FMU & MASTER VG ACTUATOR. PERFORMED GND ENG RUN IAW AMM 71-00-00. NO MSGS OR DEFECTS NOTED.Jun 6, 2015 · N655CA · Cndair CL6002C10SDR ASAA2015050311625Wire Harness · malfunctionedNR 1 ENGINE HAS HISTORY OF HPTACC FAULTS. POSITION SIGNAL DISAGREE AND SIGNAL OUT OF RANGE FAULTS BEING SET. ACFT GROUNDED. VERIFIED HPTACC FAULTS ARE STILL ACTIVE. ACCOMPLISHED FIM 75-21/802, STEP F, NO OBVIOUS DISCREPANCIES NOTED. ACCOMPLISHED AND REVERSEDMay 3, 2015 · N563AS · Boeing 737890SDR ANCF2015032901Connector · looseENG 2 FADEC B FAULT PRESENT ON ECAM. IAW AMM 73-21-60-000-001 400-001-A REMOVED & INSTALLED ECU, NO HELP. IAW TASK 71-00-00-991- 91300A, SHEET 1 1 POWER PLANT RT SIDE WAS FOUND, CONNECTORS 403VC-A & 404VC-A LOOSE. IAW TASK 71-00-00-410-094-A PARA C ITEM 2 CMar 29, 2015 · N446AV · Airbus A320214SDR UIEA2015031800183Connector · dirtyDURING DESCENT ENG 1 BECAME UNRESPONSIVE TO THROTTLE MOVEMENT. EGT WAS 659 DEGREES & CLIMBING WITH THROTTLE AT IDLE. PRECAUTIONARY SHUTDOWN ACCOMPLISHED, NO CMC MSG FOUND 1. PERFORMED VISUAL CHECK ENG INTAKE, TAIL PIPE & MAG CHIP DETECTOR, METAL NOT FOUND IMar 18, 2015 · N477MC · Boeing 74747UFSDR ASAA2015030310846Wire Harness · chafedWHILE ACCOMPLISHING TC 78472000, "ENG INLET AND FAN INSP" WIRE HARNESS FOR LPT ACCOMPLISHED, CHAFE DAMAGE FROM CONTACT WITH "C" DUCT HEAT BLANKET. ENGINE NR 1. ACFT GROUNDED. R & R NR 1 ENGINE J10 HARNESS IAW MM 73-21-06-400-802-F00 THROUGH STEP 5.F.,1, B. Mar 3, 2015 · N536AS · Boeing 737890SDR ASAA2015010410147Connector · corrodedWIRE HARNESS BAD ON NR 2 ENGINE, S1 CONNECTOR CORRODED AND DETERIORATED, ENTIRE CJ9 HARNESS REQUIRES REPLACEMENT. ACFT GROUNDED. REPLACED CJ9 HARNESS IAW AMM 73-21-06-400-803-F00 PARA E, FADAC SYS TEST GOOD IAW AMM 73-21-00-700-802-F00. IN ADDITION, R & R EGJan 4, 2015 · N569AS · Boeing 737490SDR ASAA2014121109940Insulation · wornJ9 & J10 WIRE HARNESSES WORN THROUGH, OUTER SHEATHING WEAR CONNECTORS DP 0905 AND DP 1005. REF T/C N8420000. ACFT GROUNDED. R & R J9 AND J10 HARNESS IAW MM 73-21-06-000-802-F00. COMPLETED EEC TEST IAW MM 73-21-00-700-804-F00, IDENT/CONF TEST IAW MM 73-21-00-Dec 11, 2014 · N581AS · Boeing 737890SDR ASAA2014121109939Insulation · wornLEFT ENGINE MW0311 HARNESS WORN THROUGH OUTER SHEATHING AND INTO INNER METAL BRAIDING WEAR, CONNECTOR DP1103, REF TC N8420000. ACFT GROUNDED. REPLACED LT ENGINE MW0311 HARNESS. REF AMM 73-21-06/401. ALL OPS CHECKS NORMAL, REF MM 73-21-06-400-802-F00.Dec 11, 2014 · N581AS · Boeing 737890SDR ASAA2014120309853Wire · detachedLEFT "ENGINE VALVE CLOSED" LIGHT ILLUMINATED BRIGHT AFTER ENGINE SHUTDOWN. ACFT GROUNDED. FOUND WIRE W2508-6025-20 AT TB261Y NOT SEATED AT A9. RESEATED WIRE IN TERMINAL BLOCK. ALL OPS NORMAL. REF WDM 76-21-11.Dec 3, 2014 · N563AS · Boeing 737890SDR 2014FA0000647Connector · unsecureAFTER ENGINE START, RECEIVED A RT ENGINE COMPUTER FAULT, CHECKLIST PROCEDURES CLEARED FAULT, ON TAKEOFF ENGINE ONLY ATTAINED 60 PERCENT N1. INSPECTION REVEALED THE N2 CONNECTOR PLUG WAS NOT CONNECTED COMPLETELY.Oct 24, 2014 · N452CJ · Lear 45LEARSDR DBCA2014092600004Connector · dirtyON DEPARTURE THE NR 1 ENG DEEC TRIPPED TO MANUAL MODE. CREW RETURNED & LANDING WAS UNEVENTFUL. DOWNLOADED THE NR 1 DEEC DATA & CONTACTED TECH SUPPORT. REVIEWED DATA DOWNLOAD & RECOMMENDED COMPLYING WITH P2T2 PROBE RESISTANCE CHECK & CLEANING PROBE CONNECTORSep 26, 2014 · N110WS · Raythn HAWKER800XPSDR ASAA2014091909190Wire Harness · malfunctionedWHILE COMPLETING T/C 78273000, 75-30411 HPTASS SIGNAL DISAGREE. ACFT GROUNDED. PERFORMED HPTACC VALVE, EEC AND WIRE HARNESS J10, CH B AND J9, CH A, ALL RESISTANCE CK WITHIN LIMITS, AND RECEPTACLE ARE IN GOOD CONDITION, REF FIM 75-21, TASK 802. IAW PG A, STEP Sep 19, 2014 · N563AS · Boeing 737890
Back to JASC 7397