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 CA160215021Connector · damaged(CAN) WHILE CARRYING OUT THE RESTORATION ON THE ACFT THE RT ELEVATOR TAB VALVE CIRCUIT BREAKER WAS FOUND POPPED. INSPECTION REVEALED EVIDENCE OF ARCING AT CONNECTOR D40192 LOCATED AT THE AFT PRESSURE BULKHEAD THAT RUNS TO THE ELEVATOR TAB SOLENOID VALVE. THEFeb 8, 2016 · Boeing 737*SDR CA160128007Wire · corroded(CAN) SPOILER NR 2 PUSH-OFF LIGHT ILLUMINATED ON THE GROUND. A SPLICE IN THE SPOILER WIRING HARNESS WAS FOUND WITH A SHORT CIRCUIT CAUSED BY CORROSION, AND REPLACED.Jan 26, 2016 · Bombdr DHC8400SDR HNAA2016012000014Connector · damagedRUDDER PRESSURE CAUTION LIGHT ILLUMINATED DURING CLIMBOUT, EXTINGUISHED AFTER LANDING. R & R CONNECTOR. OPS CHECKED GOOD IAW 27-20-06.Jan 20, 2016 · N331EN · Dhav DHC8311SDR CA160120008Wire · shorted(CAN) CIRCUIT BREAKER F6 ON THE R/H ESSENTIAL BUS WHICH WAS LABELED SPLRS-INBD ARM POPPED TWICE. IT WAS FOUND POPPED DURING PRE-FLIGHT CHECKS, THEN RESET, AND POPPED AGAIN DURING TAXI OUT. MAINTENANCE ACTION HAD THE CONNECTOR 2700-P31 RETERMINATED. WIRE 2700-WJan 18, 2016 · Bombdr DHC8400SDR CALA2016010400024Connector · contaminatedSTAB TRIM INOPERATIVE & AIR RETURNED. FOUND DIRT & GREASE IN THE STAB TRIM ELEC MOTOR CONNECTOR. CLEANED & RESEATED CONNECTOR STAB TRIM ELEC MOTOR. TESTED NORMAL IAW AMM 27-41-00-700-803.Jan 4, 2016 · N73278 · Boeing 737824SDR CA151202008Connector · failed(CAN) CREW REPORTED ELEVATOR ASYMMETRY CAUTION LIGHT DURING FLIGHT. FOR UNKNOWN REASONS CREW DECLARED EMERGENCY. AFTER TOUCH DOWN ELEVATOR ASYMMETRY CAUTION LIGHT EXTINGUISHED. MAINTENANCE CHECKED CDS AND FOUND ELEV ASYM FAILURE. TROUBLESHOOTING IAW FIM WAS Nov 25, 2015 · Bombdr DHC8402SDR AALA20151117001Connector · defectiveDURING FLAP RETRACTION, BETWEEN 1 DEGREE & UP, LE SLAT ASYM EICAS MSG APPEARED & LE LIGHT ILLUMINATED. AN EMER WAS DECLARED & ACFT DIVERTED WITH AN UNEVENTFUL LANDING. THE ACFT WAS REMOVED FROM SERVICE. REPLACED CONNECTOR D40302J IAW WDM 27-81-31. FSEU 1 &Nov 16, 2015 · N677AN · Boeing 757223SDR VNAA2015102700027Wire · chafedCREW REPORTED SLATS FAIL CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPAIRED CHAFED WIRE IN CONNECTOR PLUG FOR RT SLAT BRAKE POSITION SENSOR UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SEOct 27, 2015 · N705PS · Cndair CL6002C10SDR HNAA2015102500312Wire · brokenON TAKEOFF ROLL, SPOILER PUSH OFF LIGHT FLICKERED. R & R BROKEN WIRE AT QUADRANT SWITCH. OPS CHECKED GOOD.Oct 26, 2015 · N326EN · Dhav DHC8311SDR VNAA2015092300021Connector · damagedCREW REPORTED FLAPS FAIL MESSAGE WHILE SELECTING FLAPS FROM 8 TO 20 DEGREES. FLAPS REMAINED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R MATING CONNECTOR PLUG FOR LT BRAKE AND POSITION SENSOSep 23, 2015 · N230PS · Cndair CL6002B19SDR DXTA2015091506085Circuit Board · failedELECTRICAL BURNING ODOR OBSERVED BY BOTH CREW DURING FLIGHT. COFFEE HEATERS WERE TURNED OFF & ODOR REMAINED. LT & RT GEN SHOWED 170 & 130 AMP, SPLIT RESPECTIVELY & WERE FLUCTUATING +/- 20 AMPS RAPIDLY. WHEN GALLEY & CABIN POWER WAS REMOVED AMP LOAD SEEMED Sep 14, 2015 · N719QS · Gulstm 200SDR AALA20150910007Splice · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE LE SLAT IN TRANSIT LIGHT ILLUMINATED. ADJUSTED POSITION OF NR 1 LE OTBD SENSOR S994 IAW AMM 27-88-11. R & R WIRING SPLICES AT SENSOR S994 IAW AMM 27-88-11. R & R FSEU IAW AMMSep 8, 2015 · N800NN · Boeing 737823SDR DALA2015081204906Wire · damagedDIVERTED DUE TO MULTIPLE FLIGHT CONTROL WARNINGS; A CONSTANT AUDIBLE "STABILIZER MOTION" WARNING ACCOMPANIED WITH A STICK SHAKER WERE THE KEY INDICATIONS FOLLOWED BY NUMEROUS OTHER FLIGHT CONTROL WARNINGS/MESSAGES. THE FLIGHT CREW DECLARED AN EMERGENCY, DIVERAug 11, 2015 · N951AT · Boeing 717200SDR 2015FA0000373Wire · damagedWHILE PERFORMING OPS CHECK OF THE HORIZONTAL STAB SYSTEM IT WAS NOTED THAT THE SYSTEM ONLY WORKS IN CHANNEL 1 BUT NOT ON CHANNEL 2. TROUBLESHOOTING LEAD TO DEFECTIVE WIRING ON CONNECTOR P12 SOCKETS DD AND EE. SOCKETS SHOWED EVIDENCE OF ARCING AT SOCKET TO WIAug 7, 2015 · N276GR · Cndair CL6002B19SDR CA150817022Wire · damaged(CAN) YAW DAMPENER CONTROL BREAKER POPS AFTER THE COMPASS FLAG PULLS ON THE HSI. FOUND SEVERAL WIRES BARE AND SHORTING IN CAPTAINS CONTROL COLUMN CURLY CORD. CORD WIRES RE-TERMINATED AND YAW DAMPER TESTED SERVICEABLE.Jul 30, 2015 · Beech 1900CSDR VNAA2015073000042Connector · shortedCREW REPORTED FLAPS FAIL CAUTION MESSAGE AND FLAPS STUCK AT 38 DEGREES ON APPROACH. CREW EXECUTED A MISSED APPROACH PROCEDURE, RAN QRH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW FAULT ISOLATION MANUAL, R & R Jul 30, 2015 · N718PS · Cndair CL6002C10SDR CA150714001Wire · chafed(CAN) AFTER TAKEOFF DURING THE INITIAL CLIMB, THE CREW COULD NOT GET THE FLAPS TO RETRACT. THE CREW RETURNED TO ORIGIN & CONTACTED MX. THE FLAPS WERE RESET TO ZERO & THE ACFT WAS RELEASED UNDER THE MEL PROTOCOL & THE ACFT CONTINUED ITS RUN. ONCE THE ACFT WAJul 12, 2015 · Beech 1900DSDR DJFA20150711001Connector · dirtyWHILE IN CLIMB OUT PHASE AT FL 240, AURAL WARNING TONE SOUNDED MULTIPLE TIMES, ACFT PITCHED UP UN-COMMANDED & VERTICAL SPEED INCREASED BY 2200 FPM. CREW SWITCHED TO VS MODE & REDUCED PITCH. NO EMER DECLARED, NO FURTHER INCIDENT. CLEANED & RESEATED THE NR 1 Jul 11, 2015 · N730FL · Cessna 750SDR CA150714004Wire · broken(CAN) RETURN DUE AILERON LOCKOUT FAULT & CTR AUTOPILOT. CTR AUTOPILOT ENGAGEMENT SWITCH IS CAUSING FLIGHT CONTROL COMPUTER TO FAIL. AILERON LOCKOUT WORKS & ONLY AN INDICATION FAULT. MEL APPLIED. RESOLUTION FOUND WIRE AT PIN 30 OF CONNECTOR D479 BROKEN. REJul 7, 2015 · Boeing 7673Q8SDR CA150616007Wire · chafed(CAN) CREW REPORTED THAT THE ELEC TRIM WAS UNSERVICEABLE ON BOTH SIDES. DURING INVESTIGATION MX FOUND WIRES AT ELEC TRIM MOTOR CHAFED & ARCHING ON RT SIDE COVER. PREVIOUSLY WRAPPED IN SPIRAL WRAP BUT CUT THROUGH. WIRES WERE REPAIRED & PROTECTED, AS A PREVENJun 16, 2015 · Beech 1900DSDR R61A201506160372Wire Harness · damagedON GEAR RETRACTION, CREW RECEIVED A SLAT FAIL MESSAGE. RAN QRH, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND R & R THE RT OTBD SLAT HARNESS AND SKEW SENSOR IAW AMM AND OPS CHECKEDJun 16, 2015 · N135HQ · Emb ERJ170200LRSDR CA150615020Connector · disconnected(CAN) DID A MISSED APPROACH TO RUNWAY DUE TO THE FLAPS NOT EXTENDING. THEY DECLARED A PAN PAN & DID A FLAPLESS LANDING WITHOUT FURTHER INCIDENT. RESOLUTION FOUND CONNECTOR 4035VC-A DISCONNECTED & 4037VC-A NOT CONNECTED PROPERLY. BOTH CONNECTORS RECONNECTEDJun 15, 2015 · Airbus A320211SDR CALA2015060800493Connector · corrodedAFTER TAKEOFF CAPTAIN`S PITCH BAR & COMMAND BAR INOPERATIVE. ALSO SPD LIM ON SPEED TAPE. THRU FL 270 WE GOT THE STICK SHAKER, AIR RETURN. REMOVED CONNECTOR D229 FOR FLAP TRANSMITTER RT. FOUND MORE THAN 20% CORROSION. R & R D229 RT TE FLAP XMITTER CONNECTOJun 8, 2015 · N33266 · Boeing 737824SDR REXA2015051100477Pin · brokenFLAP FAIL CAUTION AT ZERO DEGREES ON AML 3224819-1. COMPLIED WITH FLAP FAIL TROUBLESHOOTING IAW TS 001100R1. AFTER PUSH BACK BOX ITEMS WHEN I ASKED FOR FLAPS 8 DEGREE BOX. FLAPS FAILED CAUTION MSG AT FLAPS 0 DEGREE. PERFORMED TROUBLESHOOTING IAW FIM CHAPTERMay 11, 2015 · N836AY · Cndair CL6002B19SDR CA150427009Connector · shorted(CAN) ON APPROACH CONDITIONS DRY ON RUNWAY, CREW REPORTED A PAN PAN DUE SLAT FAIL. NO EMERGENCY WAS DECLARED, BUT EMERGENCY VEHICLES MET THE FLIGHT. NO NEGATIVE PAX AND/OR IFS REACTION TO INCIDENT. MOC ADVISED. CARRIED OUT FIM 27-83-00-810-814-A, FOUND PINSApr 23, 2015 · Emb ERJ190100IGWSDR ASOA20150412093Connector · damagedFLIGHT 4263, SPOILER FAIL INFLIGHT AT FL370, SPOILERS OPEN INDICATION DISPLAYED ON EICAS. MAINTENANCE FOUND DAMAGED HARNESS AND PINS AT CONNECTOR P1166 FOR THE RT SPEED BRAKE PROXIMITY SWITCH. REMOVED DAMAGE SECTION AND REPAIRED IAW EMB-145 SWPM 20-21-00. RApr 12, 2015 · N16919 · Emb EMB145LRSDR CALA2015040700258Connector · looseFLAPS 25 DEGREES TAKEOFF. FLAPS WOULD NOT RETRACT TO LESS THAN 15 DEGREES. FOUND LT FLAP POSITION TRANSMITTER CONNECTOR D400241 VIBRATED LOOSE CAUSING ERRATIC FLAP INDICATIONS. SECURED D400241 CONNECTOR IAW AMM 27-58-01 & WDM 27-52-11 PG 1 SHEET 2. OPERATIApr 7, 2015 · N37408 · Boeing 737924SDR AALA20150329010Connector · looseAIR INTERRUPT, RETURNED, & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CREW OBSERVED, FLIGHT CONTROLS CAUTION, EICAS MSG. FOUND ELEC CONNECTOR D4310P LOOSE. SECURED CONNECTOR. ACCOMPLISHED AN OPERATIONAL CHECK WITH NO DEFECTS NOMar 29, 2015 · N726AN · Boeing 777323ERSDR AALA20150402003Connector · looseAIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. FLIGHT INTERRUPTION DUE TO FLIGHT CONTROL CAUTION EICAS MSG CAME ON AT 1500 FT. CHECKED WIRING & FOUND ELECTRICAL CONNECTOR D4310P LOOSE, FROM ACE L1 TO LT OTBD ELEVATOR PCU,Mar 29, 2015 · N726AN · Boeing 777323ERSDR HNAA2015032500106Connector · corrodedFLAP DRIVE CAUTION LIGHT ILLUMINATED IN FLIGHT. INSPECTED AND FOUND 2452-P5 HAS CORROSION IN THE PINS AND 2452-E1, 2452-E2, SPLICE NEEDING REPLACED DUE TO MOISTURE EGRESS. REPLACED SPLICES, CONNECTOR PLUG AND PINS. OPS CHECKED GOOD AT THIS TIME IAW 27-50-01 Mar 25, 2015 · N838EX · Dhav DHC8102SDR AALA20150321007Connector · contaminatedAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RETURNED DUE TO FLAP ASYMMETRY INDICATION, FAULT FLAP 1 SKEW MSG 27-53250. FOUND ELEC CONNECTOR ON NR 1 SKEW SENSOR WET & DIRTY. CLEANED SENSOR & VERIFIED NO DAMAGE. ACCOMPLISHED SMar 21, 2015 · N938AN · Boeing 737823SDR UHLA2015031400163Connector · contaminatedFLAP FAIL MESSAGE IN FLIGHT. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. FOUND RT T3 SKEW SENSOR CONNECTOR FULL OF FOD AND DIRTY. CLEANED CONNECTOR AS REQUIRED AND RECONNECTED TO SKEW SENSOR. OPS CHECK OF FLAPS/SLATS GOOD AT THIS TIME THROUGH MULTMar 14, 2015 · N657RW · Emb ERJ170100SESDR O2GA2015021621201Wire · chafedAT CRUISE FL370 45 MINUTES AFTER DEPARTURE, EICAS INDICATIONS SLAT MOVED INTERMITTENTLY BETWEEN 0* & 2*. CAS MSG, SLAT & FLAP MAINTENANCE. ON ARRIVAL FOR LANDING, SLATS & KRUEGERS DID NOT EXTEND. LANDING WAS PERFORMED WITH 20 DEGREES FLAPS IAW CHECKLIST. LFeb 16, 2015 · N212U · Gulstm 200SDR VNAA2015012500031Wire · looseCREW REPORTED STABILIZER TRIM DISCONNECTED AND WOULD NOT RESET. CREW RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, INSPECTED YOKE TRIM DISCONNECT SWITCHES AND FOUND LOOSE WIRE ON CAPTAIN’S DISCONNECT SWITCH. MAINTENANCE RESOLDERED WIRE TO DISJan 25, 2015 · N259PS · Cndair CL6002B19SDR CA141217018Connector · damaged(CAN) WHILE CARRYING OUT TASK AMM 27-34-07-000-801. UPON REMOVAL OF THE TRANSMITTER, WE NOTICED A ROLL PIN/STOP WAS BENT, AND HAD INDICATIONS OF CONTACT WITH ANOTHER STOP PIN. WITH THE UNIT PROPERLY INSTALLED, THERE IS NO INDICATION THAT THESE PINS SHOULD BE Dec 16, 2014 · Cndair CL604SDR Y2PA20141212049Connector · shortedCREW REPORTED ON APPROACH, AFTER AUTOPILOT DISENGAGED, COPILOT FLEW FROM APPROX 2000’ AGL TO SHORT FINAL USING WHAT FELT LIKE MORE AFTER PRESS THAN NORMAL, MAINTAINING CONTROLLABILITY & REMAINING ON APPROACH PROFILE & PROPER AIRSPEED. UPON LANDING AT 20’ AGL Dec 11, 2014 · N827AA · Amd FALCONESDR CA141215011Connector · damaged(CAN) DURING CRUISE FLIGHT, CREW REPORTED THAT RIGHT HAND ELEVATOR HAD UN-COMMENDED PITCH CHANGES ON AUTOPILOT A/B AND MANUAL +/- 300 FT WHEN LEVEL. THE DECISION WAS MADE TO RETURN THE AIRCRAFT, WHERE THE AIRCRAFT LANDED SAFELY. TROUBLE SHOUTING CARRIED OUT FODec 10, 2014 · Boeing 737800*SDR CA141128002Wire Harness · failed(CAN) SLAT FAIL EICAS ON APPROACH, THE FLAP LEVER WAS NOT SELECTED YET. PAN PAN DECLARED, LANDED WITHOUT INCIDENT. REPLACED THE W511 SLAT WIRE HARNESS IAW AMM 27-83-07. CHECKED GOOD.Nov 27, 2014 · Emb ERJ190100IGWSDR FDEA201411223863Pin · bentLEADING EDGE SLAT LIGHT CAME & FLAP NEEDLE WENT TO INTERMEDIATE POSITION BETWEEN 0 & 1 DEGREE. 38,000 FT SLOWED TO 220 KTS DESCENDED BELOW 20,000 FT FOR TROUBLESHOOTING. UNABLE TO CORRECT, RTB TO TROUBLESHOOT. FOUND PIN 29 BENT & SHORTED TO PIN 14 OF CONNECNov 22, 2014 · N784FD · Boeing 757222SDR FDEA201410073001Pin · bentUNCOMMAND RT RUDDER ON CLIMB OUT 11.3K FOR 1-3 SECONDS. AUTOPILOT STAYED CONNECTED. NO STATUS OR ADV MSG OR OVERHEAD LIGHT ON WITH HYD POWER ON. PERFORMED TROUBLE SHOOTING. TROUBLE SHOOTING FOUND ON RT RUDDER RATIO CHANGER MODULE, MODULE FAULT, FAULT BALL Oct 7, 2014 · N916FD · Boeing 75727BSDR 2014FA0000477Wire · frayedFLAPS STOPPED MOVING AT 7 DEGREES AND STABILIZER DIDN'T NOT MOVE TO POSITION FROM CRUISE. THRUST REVERSORS DID NOT DEPLOY ON LANDING. LOAD VALVE WIRES FRAYED ADJACENT TO VALVE. SHORTED AND TRIPPED HYDRAULIC CONTROL CIRCUIT BREAKER.Aug 9, 2014 · N851AC · Cessna 560XLSDR C77A20140721004Wire Harness · failedSLAT FAIL, SPOILER FAULT, SHAKER ANTICIPATED & AOA LIMIT FAIL MSG ON APPROACH. RAN QRH, MSGS REMAIN. R& R RT 2 & 3 SLAT HARNESS & SKEW SENSORS IAW AMM 27-83-07 & AMM 27-83-01. OPERATIONS CHECKED GOOD, OK FOR SERVICE.Jul 15, 2014 · N628CZ · Emb ERJ170200LRSDR CA140702007Connector · failed(CAN) AFTER TAKEOFF WHEN THE FLAPS WERE RETRACTED THEY LOCKED UP AT 5 UNITS. THE CREW DECLARED AN EMERGENCY AND DIVERTED, THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A SHORTED NR 3 FLAP SKEW SENSOR, THE CONNECTOR WAS REPLACED AND THE SYS TESTED SERVICJul 1, 2014 · Boeing 73776NSDR UG82014F00001Wire · meltedWIRES COMING FROM LAVATORY PURGE SWITCH OVERHEATED & MELTED SHEATHING FROM WIRE. DURING ACCOMPLISHMENT OF LAV WATER SYSTEM 6 MO STERILIZATION.Jun 27, 2014 · N235EF · Bombdr BD1001A10SDR ERAA201406230043Wire · damagedSPOILER 2 PUSH OFF SWITCH LIGHT CAME ON IN FLIGHT. VERIFIED PROBLEM ON RT WING BY DISCONNECTING 2700-P4 & THEN 9811-J172, IT WENT AWAY. RAN NEW WIRE FROM 9811-J172 TO 2762-S6 TO E2 REPLACED. GND TEST GOOD IAW MM 27-19-00.Jun 22, 2014 · N883EA · Dhav DHC8106SDR CA140623001Connector · damagedCREW REPORTED, UNABLE TO DISCONNECT PITCH TRIM USING BOTH CONTROL WHEEL DISCONNECT BUTTONS. PROBLEM DETERMINED TO BE LOW VOLTAGE (22V) AT PIN -K-, CONNECTOR P312, THUS PREVENTING K1 TO REMAIN ENERGIZED ONCE PITCH/TRIM DISCONNECT SWITCH WAS RELEASED. CAUSE OFJun 19, 2014 · Beech 1900DSDR CALA2014061391272Connector · disconnectedSPOILER SQUIB TEST DOES NOT LIGHT UP EMER ESCAPE GREEN TEST LIGHTS ON TEST 1 & 2. FOUND CONNECTOR M961 DISCONNECTED FROM BATTERY PACK. CONNECTED BATTERY PACK CONNECTOR M961 IAW AMM25-65-00. SQUIB LIGHTS NOW TEST OK.Jun 10, 2014 · N670UA · Boeing 767322SDR CA140603004Wire · misinstalled(CAN) IT WAS DISCOVERED AT THE GLOBAL COMPLETION CENTER, THAT THERE WAS A SIGNIFICANT REDUCTION IN CABLE TENSION, OUT-OF-TOLERANCE, FOR THE FORWARD FUSELAGE AILERON CABLE CIRCUIT, SDGC419-1000-1, FORWARD FUSELAGE RUDDER CABLE CIRCUIT, SDGC419-2000-1, AND AFT FJun 3, 2014 · Bombdr BD7001A10SDR FDEA201405271207Wire Harness · chafedON REMOVAL OF RT WING TO BODY CLOSURE PANEL 196AR CHAFING FOUND ON CABLE BUNDLE W3405. ON INVESTIGATION SYS FOUND TO BE ELEC CONTROL OF SPOILER NR 8. THIS CABLE IS A SEVEN CORE SHIELDED WIRE RUNNING BETWEEN AFT WING BREAK AD1148, CONNECTOR D40579P & INBD SPOMay 27, 2014 · N901FD · Boeing 7572B7SDR IXXA201405290100Connector · looseEICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS 30 SELECTED & FAILED TO POSITION WITH AIR, AIR SPEED LESS THAN 165. CYCLED FLAPS 3 TIMES & INSPECTED SLATS. CHECKED FSGU & DVI OF FLAP PDU XMT FOUND LOOSE CONNECTOR. CLEANED & SECURED CONNECTOR. RECYCLED FLAMay 27, 2014 · N752CX · Boeing 7572G5
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