JASC 2797

Service difficulty reports · 920

Reports filed under 2797 · Flight Control 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 = '2797'
  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 UALA2012051002718Wire Harness · damagedFLAP SYS MONITOR STATUS MESSAGE, SHOWING MESSAGE NUMBERS 27638 AND 27639. TROUBLESHOOT FLAP SYS MONITOR FOUND LOOSE PIN IN WIU AND RETERMINATED. REPLACED WIRE HARNESS TO LT OTBD FLAP RVDT. OPS CHECKED OK.May 9, 2012 · N127UA · Boeing 747422SDR UALA2012050702651Connector · contaminatedAIR RETURN DUE TO STAB TRIM INDICATION. TROUBLESHOOTING FOUND STAB WOULD RUN AT FULL SPEED IN NOSE UP DIRECTION AND HALF SPEED IN NOSE DOWN DIRECTION. IN BLOCK 6 OF FIM FOUND STAB WOULD NOT GO IN NOSE DOWN DIRECTION 104400 ALSO HAD 0.2 OHMS, AND IN NOSE UP DIMay 4, 2012 · N663UA · Boeing 767322SDR REXA2012050100603Wire Harness · damagedFLT 4299, FLAPS FAIL AT 8 DEG. REMOVED AND REPLACED RT FLAP WIRING HARNESS TO BPSU IAW AMM 27-51-00.May 1, 2012 · N8877A · Cndair CL6002B19SDR CA120502002Wire · broken(CAN) REF CADORS REPORT NR: 2012O1034. FROM CREW INCIDENT/SAFETY REPORT: - "ON SELECTION OF FLAP 1, FLAP INDICATORS STOPPED PRIOR TO REACHING FLAP 1 AMBER FLAP TRANSIT LIGHT STAYED ILLUMINATED. ADVISED CENTER, WE WERE VECTORED NORTH WEST TO RUN CHECKLIST. QApr 28, 2012 · Boeing 7378ASSDR REXA2012042400567Connector · damagedFLAPS FAIL AT 12 DEGREES AT 11C - DESCENDING 3-20000' AIRSPEED 190-180 - 45 MIN AT TOUCHDOWN AT 150 KTS - 200 FLT FPM - NO BRAKING UNTIL BELOW 80 KTS. OVER HALF OF RUNWAY REMAINING. RESET FLAPS FAIL PER FIM OPS CHECK IS NORMAL - DEFERRED PER MEL 27-50-00 FOR Apr 24, 2012 · N8877A · Cndair CL6002B19SDR UALA2012042302417Connector · shortedFLT CONTROL SYSTEM STATUS MESSAGE. ACCOMPLISHED WIRING CHECKS IAW WDM 27-61-15. FOUND SHORT AT CONNECTOR DM27116 BETWEEN PINS 3 & 7. CONFIRMED SHORT BETWEEN D7435J & DM27116. REMOVED & CLEANED CONNECTOR D2139P & SECURED. ACCOMPLISHED WIRING CHECKS, ALL NORApr 23, 2012 · N223UA · Boeing 777222SDR UALA2012042302432Wire · faultyFSEU 2 TRIPPED DURING CRUISE. MEGGER WIRES FROM CB FSEU 2 SENSOR TO BENCH PLUG D3258A PIN F3, & TO T153 PWR TFMR, CHECKED GOOD. CHECKED ALL FLAP POSITION SENSOR OHMS, RESISTANCE TO FSEU M10332, CHECKED OKAY.Apr 22, 2012 · N560UA · Boeing 757222SDR UALA2012042302427Wire Harness · faultySPOILERS EICAS MSG ON TAXI OUT. REPLACED HARNESS 585-2185 FROM DM27116 TO D2139J. OPS CHECKED IAW MM.Apr 21, 2012 · N223UA · Boeing 777222SDR F3LA2012041900746Transducer · defectiveELAC 2 FAULT (UNCOMMANDED PITCH +/··150'). TROUBLESHOT IAW TM 27-93-Q0-810-808-A, R & R F/O SIDE STICK TRANSDUCER (4E4) REF AMM 27-92-41-Q00-002-A AND 27-92-41-40O-Q02-A. OPS CHECKED GOOD, REF AMM27-92-41-710-001-A.Apr 18, 2012 · N930FR · Airbus A319111SDR CA120417002Wire Harness · failed(CAN) SLAT FAILURE ON DECENT YOW, PAN DECLARED WITH ATC. NO FURTHER INCIDENT. SLAT FAIL EICAS MESSAGE ON DESCENT. QRH ACTIONS CARRIED OUT SLATS DID NOT EXTEND PAST 0 ZERO INDICATION. CMC INTERROGATED FAULT CODE RECORDED 27831005AC3. SLAT HARNESSES AT POS SLApr 16, 2012 · Emb ERJ190100IGWSDR SIMA20120410017Connector · looseFLIGHT 4103, THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A PITCH TRIM MAIN AND PITCH TRIM BACK UP FAIL MESSAGE. THE CREW COMPLETED THE CHECKLIST AND DECLARED AN EMERGENCY AND RETURNED TO LIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMApr 10, 2012 · N676AE · Emb EMB145LRSDR SIMA201204101008Connector · looseFLIGHT 4103, CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A PITCH TRIM MAIN AND PITCH TRIM BACK UP FAIL MESSAGE. THE CREW COMPLETED THE CHECKLIST AND DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS RApr 10, 2012 · N676AE · Emb EMB145LRSDR UALA2012040602138Connector · dirtyELEVATOR FEEL STATUS MESSAGE ON EICAS IN FLIGHT. CLEANED ELECTRICAL CONNECTOR AND CHECKED LINES FOR TIGHTNESS ON ELEVATOR FEEL COMPUTER. MESSAGE CLEARED. OPERATED ELEVATOR SYSTEM. MESSAGE DID NOT RETURN.Apr 6, 2012 · N664UA · Boeing 767322SDR FDEA201203271153Connector · looseON INITIATION OF DESCENT, A YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH T/E FLAP ASYM AND T/E CAUTION LIGHTS ON THE EICAS AND FOWARD PANEL. THE FLAP HANDLE WAS UP AND FLAP INDICATION GAUGE SHOWED UP AS WELL. THERE WAS NO ROLL TENDENCY. TROUBLESHOOTING FOUNDMar 27, 2012 · N946FD · Boeing 757236SDR USAA2012032700016Connector · dirtyCREW REPORTED AN ASYMMETRICAL TRAILING EDGE FLAPS L25/R15. NO UNCOMMANDED ROLL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SLATS AND FLAPS. NO FAULTS DETECTED. CLEANED AND RESEATED RIGHT FLAP POSITION TRANSMITTER CONNECTOR. FLAP INDICATION ANDMar 26, 2012 · N529AU · Boeing 7373B7SDR IPXA2672594Connector · looseT/E FLAP DISAGREE ON APPROACH, WHEN FLAPS SELECTED PAST 5. ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR LOOSE. SYS CHECKED NORMAL IAW FIM 27-51-00, FIG 105.Mar 22, 2012 · N337UP · Boeing 76734AFSDR IPXA12672517Connector · looseT/E FLAP DISAGREE ON APP WHEN FLAPS SELECTED PAST 5, ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20 EMERGENCY DECLARED. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR PLUG LOOSE. SYS CKS NORMAL IAW FIM 27-51-00, FIG 105.Mar 22, 2012 · N337UP · Boeing 76734AFSDR 9JLA2012032200793Wire · brokenDURING APPROACH, FLAPS WOULD NOT EXTEND PAST 20 DEGREES. AFTER LANDING, FLAPS STILL FAILED TO RETRACT. TROUBLESHOOTING REVEALED HYD FLUID LEAKING FROM FLAP POWER UNIT. FLAP POWER UNIT REPLACED. FUNCTIONAL CHECKED SATISFACTORY. SAME PROBLEM OCCURRED ON NEXT Mar 17, 2012 · N904HD · Lear 45LEARSDR UALA2012031201625Wire Harness · shortedFLAPS PRIMARY EICAS MSG WHEN FLAPS RE-TRACTED FROM FLAPS 5 TO FLAPS 1. ALSO HAD THE C-B FOR L/E FLAP DRIVE CONT GRP B A/C TRIPPED AT THE SAME TIME. THIS SAME C-B TRIPPED PRIOR. DO NOT RESET C-B AND CLEAR WITHOUT POSITIVE DETERMINATION OF CAUSE AND REPAIR. Mar 12, 2012 · N118UA · Boeing 747422SDR UHLA2012030100076Wire Harness · defectiveSLAT FAIL ON DEPARTURE. LEVELED OFF AT 13,000 FT AND PERFORMED QRH, MESSAGE DID NOT CLEAR. DECLARED EMERGENCY AND RETURNED TO FIELD. APPROACH AND LANDING ACCOMPLISHED WITH NO INCIDENT. MAINTENANCE INSPECTED SKEW SENSORS AND HARNESSES AND FOUND NO DEFECTS, Mar 1, 2012 · N215JQ · Emb ERJ170200LRSDR R61A20120301140Wire Harness · failedCREW REPORTED SLAT FAIL ON APPROACH INTO PHL, DECLARED AN EMERGENCY AND A GO AROUND. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT 2/3 SLAT HARNESS PER EMB AMM, AND OPS CHECK GOOD.Mar 1, 2012 · N822MD · Emb ERJ170200LRSDR CA120221007Wire Harness · failed(CAN) CREW HAD A SLAT FAILURE ON ARRIVAL. CREW CHECKED LANDING DISTANCE REQUIRED AND MADE NORMAL LANDING WITH FLAPS 2, NO EMERGENCY WAS DECLARED AS "FLAP 1" WAS SELECTED, WE RECEIVED A "SLAT FAIL" MESSAGE ON THE EICAS. "SHAKER ANTICIPATED" WAS ALSO LATER DISFeb 18, 2012 · Emb ERJ190100IGWSDR UALA2012021500918Connector · looseINTERMITTENT FLAP SLAT ELEC STS MSG UPON SETTING FLAPS FOR T-O. ACP'D FSEU BITE-FAULTING FLAP POS XMTR 1-L, M473. STILL GET EICAS "FLAP-SLAT ELECTRIC" STATUS MSG UPON FLAP EXTENSION FULL DOWN & UP (BETWEEN 5-10 DEGREES POS). CONNECTOR TO XMTR SECURED. ACP'Feb 15, 2012 · N664UA · Boeing 767322SDR CA120215005Connector · contaminated(CAN) AIR TURNBACK DUE TO C/B P6-2, D19 TRIM CONTROL. RUD POPPED DEFECT STATES: RUDDER TRIM CONTROL C/B FOUND POPPED RESOLUTION STATES: INSPECTED RUDDER TRIM ACTUATOR CONNECTOR D2932, FOUND GLYCOL PUDDLES IN THE VICINITY. CLEANED CONNECTOR AND FUNCTION CHECFeb 14, 2012 · Boeing 7377CTSDR R61A201202080089Wire Harness · failedDURING PREPARATION FOR APPROACH, THE CREW RECEIVED A "SLAT FAIL" MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY INTO PHL. THE FLIGHT LANDED NORMALLY AND TAXIED TO THE GATE. MAINTENANCE WAS NOTIFIED, TROUBLESHOT THE SLAT SYSTEM. MAINTENANCE THEN REMOVED AND REPFeb 8, 2012 · N134HQ · Emb ERJ170200LRSDR AALA20120128MIA01Wire · damagedMIA - CREW REPORTED SLATS WOULD NOT RETRACT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED WIRE AT 5303 RIGHT OUTBOARD SLAT NUMBER 9 INBOARD PROXIMITY SWITCH STATION 581. SYSTEM GROUND CHECK NORMAL Jan 27, 2012 · N385AM · Boeing 767323SDR HNAA2012012300495Wire · damagedCIRCUIT BREAKER 1Q FOR PFCS INDICATOR POPPED AFTER TAKEOFF. RETURN TO FIELD. INSTALLED TEMP WIRE IAW SP 24.4. LOCATED BETWEEN 9800J172 AND 2705P10. WIRE IDENT IS IAB22. OPS CHECKED GOOD.Jan 23, 2012 · N815EX · Dhav DHC8102SDR UALA2012012000438Connector · looseALTN STAB TRIM CB B19 POPS WHEN ELEC PEDESTAL TRIM SWITCHES ARE MOVED. FOUND STCM CONN D01847 LOOSE BY 1 TURN. REMOVED & INSPECTED LOCK MECH. CLEANED & SECURED. CHECKED ALL REMAINING CONNECTORS OKAY. OPERATED ALT SYS MANY TIMES OK.Jan 19, 2012 · N595UA · Boeing 757222SDR UALA2012011600345Wire · faultyRIGHT ACE FAILS ACE MONITORING TEST. TRIED RESETTING, NO HELP. ACE ON ORDER FROM TERMINAL PCN: 483-9204. STARTED REMOVAL PER MM. PULLED APPLICABLE CBS ON PSA-R. ACE MONITOR TEST" FAILS TEST WITH MSG 27-13007, EICAS SHOWS "FLIGHT CONTROL STATUS" MSG. FOUNJan 15, 2012 · N210UA · Boeing 777222SDR WAIA2012FA0000030Current Limiter · failedAFTER TAKEOFF, SELECTED "FLAPS UP", FLAPS RETRACTED AS INDICATED. NOTICED "FLAP INOP" ANNUNCIATOR ILLUMINATED. FOLLOWED CHECKLIST TO RESET FLAP SYS BUT COULD NOT RESET THE FLAPS. RETURNED AND PERFORMED A ZERO FLAP LANDING. MX INSPECTED FLAP CONTROLLER BITJan 12, 2012 · N40FC · Cessna 650SDR UALA2012010600137Connector · corrodedFLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. STATUS MESSAGE 2710306 ACTIVE ER MODE. REPLACED RIGHT FLAPERON INBD PCU, NO HELP. CONNECTOR PIN 17 HAS CORROSION. REPLACED CABLE ASSY FLAPERON POWER. ACCOMPLISHED FLAPERON RIGGING PER MM. RIGHT Jan 5, 2012 · N793UA · Boeing 777222SDR FDEA201112285452Wire · damagedUPON INTIAL FLAP RETRACTION FROM 5 DEG TO 2 DEG, NR6 L/E FLAP DID NOT RETRACT, QRH PROCEDURE RAN WITH NO SUCCESSFUL RETRACTION. ON TAXI-IN, FLAP HANDLE BROUGHT UP AND NR6 L/E FLAP STILL INDICATED EXTENDED. TROUBLE SHOT TO WIRES AT CONNECTOR D916. BUILT UP ADec 28, 2011 · N204FE · Boeing 7272S2FSDR UHLA2011122300449Wire Harness · defectiveCREW DECLARED EMERGENCY ON DESCENT/LANDING DUE TO SLAT FAIL WHEN FLAPS WERE SELECTED TO FLAPS 5. SLATS SHOWED STUCK AT FLAPS 3. MAINTENANCE REPLACED THE LEFT 2/3 SKEW SENSOR. THE MESSAGE RETURNED LATER WITH NO EMERGENCY DECLARED AND MAINTENANCE REPLACED THEDec 23, 2011 · N657RW · Emb ERJ170100SESDR UALA2011122207058Connector · dirtyACFT RETURNED TO GATE WITH A SLATS PRIMARY FAIL EICAS MESSAGE. PREVIOUS INBOUND WRITE UP AND THE PRIMARY CONTROL VALVE WAS REPLACED. CLEANED AND RECONNECTED PRIMARY CONTROL VLV CONNECTOR AND ALL SLAT POS SENSORS CONDITION, CHECKED FLAP SLAT OPERATION PER AMMDec 21, 2011 · N218UA · Boeing 777222SDR R61A201112180435Wire Harness · inoperativeCREW REPORTED SLAT FAIL MESSAGE DURING CLIMB OUT, DECLARED AN EMERGENCY AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT SLAT 3/4 HARNESS, PER AMM, OPS CHECKED GOOD.Dec 18, 2011 · N176HQ · Emb ERJ190100LRSDR P5CA2011120900508Pin · defectiveELECTRIC FLIGHT CONTROLS {PSM} LEFT 2 AC, DC CIRCUIT BREAKERS FOUND POPPED AND WILL NOT RESET. NON-FDE CMC MSG 27506A NOTED. (PRELIMINARY INSPECTION FOUND WIRE WRAP PINS 15A AND 15E OF WIU TO BE MAKING CONTACT. CONTACT CAUSED THE RECEPTACLE TO DISCOLOR. RDec 7, 2011 · N451PA · Boeing 74746NFSDR CA111116001Wire Harness · failed(CAN) MAYDAY DECLARED WITH ATC. LANDED WITHOUT INCIDENT AT 170KTS. WING SLAT HARNESS W612 REPLACED AND TESTED SERVICEABLE IAW AMM 27-83-07-400-801A. DURING FAULT ISOLATION ALSO FOUND BOTH OTBD RT SLAT SKEW SENSORS OUT OF ADJUSTEMENT, REF AMM 27-83-01.Nov 15, 2011 · Emb ERJ190100IGWSDR UALA2011110105920Connector · faultyRUDDER TRIM INDICATOR SHOWS NO MOVEMENT. RUDDER TRIM CIRCUIT BREAKER AT P11 C10 TRIPS WHEN TRYING TO TRIM RUDDER. REMOVED CONNECTOR D1746 AT RUDDER TRIM ACTUATOR AND CIRCUIT BREAKER P11 C10 STAYS IN.Nov 1, 2011 · N589UA · Boeing 757222SDR CA111012003Wire · shorted(CAN) AILERON TRIM TRIPPED CIRCUIT BREAKER DURING CLIMB WHEN TRIM ATTEMPTED. FOUND ACTUATOR WIRING SHORTING TO ACTUATOR BODY. REPLACED AILERON TRIM ACTUATOR. SYS GROUND CHECKS SERV.Oct 11, 2011 · Dhav DHC8311SDR C2XA11CL221Connector · defectiveTHE CREW REPORTED SPOILER FAIL MESSAGE IN FLIGHT AND PERFORMED AN AIR RETURN BACK TO ORD. MX INSPECTED AND REMOVED AND REPLACED SPOILER PROX SENSOR CONNECTOR, CONNECTOR PIN P1166. OPERATIONAL CHECKS WERE GOOD.Sep 29, 2011 · N36915 · Emb EMB145LRSDR HNAA2011100600309Wire · brokenON TAKEOFF, FLAP HANDLE SELECTED TO ZERO. WOULD NOT RETRACT. STUCK AT 5. FOUND BROKEN WIRE ON FLAP HANDLE ARMING SWITCH, RESOLDERED SAID WIRE IAW AMM 20-45-04. OPS CHECKED GOOD AT THIS TIME.Sep 20, 2011 · N942HA · Dhav DHC8102SDR UALA2011091304955Connector · faultyNO RUDDER TRIM INDICATION OR MOVEMENT WITH RUDDER TRIM KNOB ELECTR. CONNECTOR REMOVED & RECONNECTED RUDDER TRIM ACTUATOR TEST PERFORMED PER AMM. SYS OPS NORMAL.Sep 12, 2011 · N656UA · Boeing 767322SDR CA110826002Wire · damaged(CAN) DURING TESTING OF THE FLAP ELECTRICAL SYS FOR AN UNRELATED REASON, MX FOUND AN OPEN CIRCUIT BETWEEN THE NR 1 FLAP POWER DRIVE UNIT (PDU) THERMISTOR AND THE FLAP ELECTRONIC CONTROL UNIT (FECU). FURTHER INVESTIGATION REVEALED THAT ELECTRICAL WIRE, 1CE46A2Aug 26, 2011 · Cndair CL6002B19SDR UALA2011082904628Connector · dirtyFLAP SLAT SKEW SENSORS STATUS AT DEPARTURE. DEFERRED DUE NIL TIME. MAINT MSG 27-20312. -INF- :ITEM SHOULD SAY FLAP SLAT SKEW SENSOR. BOEING AHM REPORTING MMSG 27-20312 'FLAP SKEW SENSOR L4B SIGNAL FAIL' REF WDM 27-59-12 P3. ENSURE WIRE HARNESS W8181 NOT AT Aug 26, 2011 · N224UA · Boeing 777222SDR UIEA2011081800457Wire · burnedWIRE BUNDLES BURNED INSIDE THE CONDUIT USED FOR THE AILERON LOCK OUT ACTUATOR, THE LATERAL NR 1 HYD SOV AND NR 1 REFUEL VALVE PERFORMED A TIME LIMITED REPAIR IAW PART 1.Aug 18, 2011 · N524MC · Boeing 7472D7BSDR CA110808004Wire Harness · failedDURING CLIMB THE FLAPS WERE RETRACTED TO ZERO, SHORTLY AFTER THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE FLIGHT CONTINUED AND THE CREW PERFORMED A FLAPLESS LANDING WITHOUT FURTHER INCIDENT. LOCAL MX FOUND THE FLAPS CONT CH1 AND FLAPS CONT CH2 CIRCUIT BRAug 5, 2011 · Cndair CL6002B19SDR C8GA2011000016Ground Wire · brokenAFTER TAKEOFF, DURING CLIMB, ON RETRACTING THE FLAPS, A SPLIT FLAP INDICATION WAS NOTED, THE OTBD FLAPS WERE AT 2 DEGREES AND THE INBD WERE INDICATING 2 DEGREES. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, NOTING TAug 2, 2011 · N801EA · Boeing 727225SDR SIMA201121507Connector · disconnectedON FLIGHT 2731 THE CREW REPORTED, RECEIVED A FLAP FAIL INDICATION ON EICAS UPON SELECTING FLAP UP ON CLIMBOUT. THE FLAPS DID NOT RETRACT, RECEIVED FLAP FAIL INDICATION. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN THE AIRCRAFT LANDED WITHOUT INCIDENTAug 1, 2011 · N670AE · Emb EMB145LRSDR AALA20110719MEX01Connector · dirtyMEX - CREW REPORTED UNABLE TO EXTEND LEADING EDGE DEVICES, EXTENDED LEADING EDGE DEVICES WITH ALTERNATE MODE. EMERGENCY DECLARED FLIGHT LANDED MEX WITHOUT INCIDENT. INSPECTED RIGHT FLAP TRANSMITTER AND CLEANED CONNECTOR. CYCLED SEVERAL TIMES NO DISCREPANCIEJul 19, 2011 · N905AN · Boeing 737823SDR E81RJT230776Wire · misinstalledDURING INVESTIGATION OF ELECTRIC ELEVATOR TRIM SYS, OPERATION NOTED TRIM RATE AS CONTROLLED BY THE PEDESTAL FLAP LEVER BAULK SWITCH BM TO OPERATE IN REVERSE. ELEVATOR TRIM OPERATES SLOW IN FAST-FLAPS DOWN MODE AND FAST IN SLOW-FLAPS UP MODE. FOUND WIRE RL1R CJul 15, 2011 · N832QS · Raythn HAWKER800XP
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