JASC 2760
Service difficulty reports · 3,502
Reports filed under 2760 · Drag Control System, 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 = '2760' 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.
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 = '2760' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20210617003Warning Message · false activationINBND MIA DECLARED EMEREGNCY FOR SPOILER FAIL. COMPLIED W/QRH, NO CHANGE. THEN AT BASE LEG DROPPED MLG, CONFIGURED FOR LANDING, EICAS MSG -INDICATIONS WENT AWAY. REF. LOG PAGE 4770561-1 - C/W DEACTIVATION OF SPOILERS BY PULLING AND COLLARING CB S F13, F14 ANDSDR AALA202106189027Switch · faultedAIRCRAFT WAS GROUNDED: REJECTED TAKEOFF DUE TO TAKEOFF CONFIG WARNING FAULT 31-53007 ON PSEU. REPLACED SPEEDBRAKE WARNING SWITCH S651 WITH NEW IAW FIM 27-62-00-810-808, OPS CHECK GOOD.SDR SIMA20210616002Control Unit · failedSPOILER FAIL EICAS MESSAGE AT CRUISE WITH SPLRS INDICATION SHOWING OPN BUT SPOILERS VERIFIED CLOSED BY FA DECLARED EMERGENCY. QRH PROCEDURE C/W MESSAGES CLEARED AFTER PULLING CBS INSTRUCTED IN QRH-C/A-T/S PER FIM RAR SPOILER CONTROL UNIT IAW AMM 27-63-02 OPS CSDR SIMA20210614003Proximity Sensor · faultedSPOILER FAIL, EMERGENCY DECLARED.- R/H & L/H OUTBOARD SPOILER PROXIMITY SWITCH CONNECTOR IS CORRODED.-C/A-RAR L/H OB SPOILER PROX. SWITCH IAW EMB-145 MM 27-63-04. OPS CK GOOD. REF NRWC 653-ORD-05471 FOR SUPPORTING ACTIONSDR AALA202106089006Spoiler Sys · faultedAIRCRAFT WAS NOT GROUNDED: ON LANDING SPOILER MESSAGE EICAS WAS DISPLAYED #7 SPOILER DID NOT DEPLOY. FOLLOWED PROCEDURE AND TAXIED TO GATE. ACCOMPLISHED FIM TASK DMC-B787-A-2760-F1-SIA-921A-A TO RESET THE MESSAGE. NO FAULTS FOUND.SDR VNAA202106021111Control Unit · malfunctionedIN-FLIGHT DEPLOYED FLIGHT SPOILERS GOT OB FLT SPLRS AND OB SPOILERONS CAUTION MESSAGE FLT PAGE SHOWED OB RIGHT IN AMBER AND OB LEFT IN WHITE AND COMPLETED QRC AND QRH AND MESSAGE STAYED ON / REPLACED RIGHT O/B MFPCU IAW CRJ 700 AMM 27-62-01-000/400-801-A02-PSSDR VNAA202105311111Warning Message · illuminatedEMERGENCY DECLARED GOING INTO PWM DUE TO IB FLIGHT SPOILER MESSAGE. NO TRUCKS WERE ROLLED AND NO NEED TO BRACE. FLIGHT LANDED SAFELY AND IS ON THE PHONE WITH MX NOW / CYCLED SYSTEM CBS AND PERFORMED SPOST2 TEST IAW CRJ700 AMM 27ˆ’61ˆ’05ˆ’740ˆ’801-A03 FAULTSDR SWIA2021073059858Pcu · corroded* RH OTBD GROUND SPOILER TO PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT OUTBOARD GROUND SPOILER TO PCU REF CRJ 200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-65-01-400-801. OPERATIONAL TEST GOOD RSDR SWIA2021073059856Pcu · corroded* RH FLIGHT SPOILER INBD AND OTBD PCU€™S HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT FLIGHT SPOILER INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62-01-400-801. SDR SWIA2021073059855Pcu · corroded* RH SPOILERON INBD AND OTBD PCU€™S LOWER ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED LOWER ATTACH HARDWARE RIGHT SPOILERON INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62SDR SWIA2021073059852Pcu · corroded* LH INBD GROUND SPOILER PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH INB GROUND SPOILER PCU HARDWARE REF CRJ-200 AMM 27-63-01-000-801, AND 27-63-01-400-801SDR SWAA2021052074503Circuit Breaker · trippedSPEED BRAKE FAILED TO DEPLOY AUTOMATICALLY ON LANDING; AUTO SPEED BRAKE CIRCUIT ; SPEED BRAKE FAILED TO DEPLOY AUTOMATICALLY ON LANDING; AUTO SPEED BRAKE CIRCUIT BREAKER FOUND POPPED. / REMOVED AND REPLACED AUTO SPEED BRAKE ACTUATOR PER AMM 27-62-31. OPS CHECKSDR QXEA2021050700217Valve · malfunctionedPRIOR TO ADDING POWER FOR TAKEOFF, OUTBOARD SPOILERS SPONTANEOUSLY RETRACTED ASSOCIATED INDICATIONS INCLUDED ROLL OUTBD LIGHT EXTINGUISHED (GLARESHIELD) AND MASTER CAUTION & ROLL SPLR OUTBD GND CAUTION ILLUMINATED. PILOT VISUALLY CONFIRMED THAT INBOARD SPOILERSDR AALA202105059002Speed Brake · faultedAIRCRAFT WAS NOT GROUNDED: LOW SPEED REJECTED TAKE OFF AT 30 KNOTS DUE TO TAKE OFF CONFIGURATION WARNING AT THRUST APPLICATION ASSOCIATED WITH ILLUMINATION OF THE OVERHEAD PROXIMITY SENSOR ELECTRONIC UNIT LIGHT. ACCOMPLISHED PROXIMITY SENSOR ELECTRONIC UNIT TESDR VNAA202104271114Proximity Switch · failedON APPROACH INTO TYS, THE CREW RECEIVED A PAIR OF SPOILER WARNINGS (INBOUND GROUND AND GROUND SPOILER DEPLOY). THEY RAN THE QRH, AND THE DEPLOY WARNING REQUIRED THEM TO LAND WITH FLAPS 20. THE CAPTAIN DECLARED A MAINTENANCE EMERGENCY AT FL050 FOR PRECAUTIONARYSDR VNAA202104271111Control Unit · unserviceableSPOILER/STAB FAULT MESSAGE AND FLAPS/SLATS OVERSPEED MESSAGE ON TAKE-OFF. OVERSPEED CLACKER BEGAN GOING OFF AFTER THE ZERO POSITION WAS SUPPOSEDLY REACHED AND CREW MADE THE DECISION TO DIVERT / INTERROGATED THE MDC AND FOUND B1 CODE 008026. REMOVED AND REPLACSDR CALA2021041900490Sensor · failedLANDING GEAR LEVER DOES NOT MOVE TO THE UP POSITION IN FLIGHT, I S FREE TO MOVE TO THE UP POSITION WHEN THE LOCK OVERRIDE IS USED INFORMATIO ONLY - CREW STATED THAT THEY DID NOT ATTEMPT TO CHECK THE ALTERNATE GEAR EXTENSION DOOR. MM CHECKED DOOR AND FOUND DOORSDR DXTA2021041940900Sensor · defectiveGND SPLR FAIL YELLOW CAS: IN THE DESCENT FROM APPROXIMATELY 22,000', SPOILERS WERE SELECTED AND IMMEDIATELY FAILED. WHITE SPOILER FAULT CAS APPEARED SIMULTANEOUSLY WITH THE YELLOW GND SPLR FAIL CAS. // SIGN OFF // REMOVED AND REPLACED THE LH MULTIFUNCTION SPOISDR HNAA2021032500102Warning Message · false activationNDIS 632 27-00 0029100 24MAR21 PHF CLOSE
FOR MIR PURPOSE: PILOT DID ABORTED TAKE OFF WHEN HE NOTED A POSSIBLE SPOILER DEPLOYMENT WITH FAIL MESSAGE.DIRECTED CA TO DO CONFIG TEST WITH TRIM INDICATION SHOWING. HAD HIM RECONFIG A/C AND DO TEST AGAISDR SWIA202156980Spoiler · out of limitsREMOVED UPPER BOLT AND ASSOCIATED HARDWARE ON INBD RH FLIGHT SPOILER PCU (NAS6306U21D) FILED CLOSED REPLACED UPPER BOLT, ANTI-ROTATION DEVICE, BUSINGS AND CSTL NUT ON INBD RH FLIGHT SPOILER PCU (NAS6306U21D) IN ATTEMPT TO FIX OUT OF LIMITS FLIGHT SPOILSDR UIEA2021031400549Switch · out of adjustAUTO SPEED BRAKE INOP (AUTO SPEED BRAKE SYST WITH SPEED BRAKE LOAD ALLEVIATION SYST INSTALLED - NOTIFY DISPATCH)(<P>T/S FIM 27-62-00/815; ADJUSTED ARMING SW.S371 & S493 PER AMM 27-62-06-212. AUTO S/B OPS TEST OK AMM 27-62-00/715. MDDR 143256 CLEARED UP / PLACASDR ABXA2021228017Pca · leakingL HYD QTY LOW EICAS MSG,FLIGHT CREW DECLARED AN EMERGENCY AND EXECUTED AN AIR TURN BACK AND LANDED UNEVENTFULLY. MAINTENANCE DETERMINED #1 SPOILER WAS LEAKING HYDRAULIC FLUID AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED #1 SPOILER PCA OPS CHECK/RIG CHECK GOSDR DALA2021030101148Computer · fault messageSHIP 3240 AIRCRAFT DIVERSON EVENT FOR RT NUMBER 3 SPOILER FAULT MESSAGE. CORRECTIVE ACTION: REPLACED SEC 1 COMPUTER. OK FOR SERVICE. (1740933)SDR SWIA202157855Mount · corrodedRH FLIGHT SPOILER OB PCU MOUNTING HARDWARE IS CORRODED. (C-CHECK RO 4/25/2021) INSTALLED SERVICEABLE HARDWARE ON R/H FLIGHT SPOILER OB PUC LOWR MOUNT IAW CRJ-200 AMM 27-62-01-400-801, OP'S CHECK PASSEDSDR SWIA202157854Nut · corrodedRH FLIGHT SPOILER IB PCU MOUNTING NUT IS CORRODED. (C-CHECK RO 4/25/2021) INSTALLED SERVICEABLE HARDWARE ON R/H FLIGHT SPOILER PCU LOWR MOUNT IAW CRJ-200 AMM 27-62-01-400-801 OP' S TEST PASSEDSDR F3LA2021021700009Speed Brake · unwanted deployDURING DESCENT THROUGH 14000 @ 320 K SPEED BRAKES EXTENDED AUTOPILOT ENGAGED AIRCRAFT MADE AN UNCOMMANDED ROLL TO THE RIGHT. AUTOPILOT WAS DISENGAGED. AIRCRAFT HANDLED NORMAL AT THAT TIME. SPEED BRAKES APPEARED TO EXTEND SYMMETRICALLY AND RETRACTED EVENTUALSDR DXTA2021021304736Warning Message · false activationGND SPLR FAIL YELLOW CAS: ON APPROACH WE ATTEMPTED TO DEPLOY SPEEDBRAKES, BUT IMMEDIATELY GOT A FAIL MESSAGE AND A SWITCH DISAGREE MESSAGE. A MOMENT LATER, THAT WAS FOLLOWED BY A GND SPLR FAIL MESSAGE. THE FIRST TWO EXTINGUISHED WHEN THE SWITCH WAS PLACED IN TSDR K11A2021021100043Handle · out of positionREJECTED TAKEOFF CONFIGURATION WARNING ON TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND SPEED BRAKE HANDLE NOT STOWED, STOWED SPEED BRAKE HANDLE IAW B737 AMM 27-62-22, PERFORMED TAKEOFF WARNING TEST IAW B737 AMM 31-26-00
OPS CHECK GOOD.SDR FDEA202102060297Actuator · leakingMULTIPLE HYD EICAS MSGS. FIRST, C HYD QTY FOLLOWED BY C HYD PRIM 2. THEN HYD SYS PRESS ALTN FLAPS AND GEAR EXTENSION PER QRH. #9 SPOILER ACTUATOR LEAKING. CENTER HYD SYSTEM SHOWS EMPTY. INSTALLED #9 SPOILER PCA REF 767 AMM 27-61-02-4. SDR MASA2021012700032Control Module · fault messageMULTIPLE FLT CONTROL FAULTS/SPOILER/SPOILERON REMOVED AND REPLACED THE NR 1 SSCU.SDR SCNA20210203012Spoiler · dentedMULTIPLE DENTS ON UNDERSIDE OF NR 7 RT WING INBD GROUND SPOILER. REPAIRED MULTIPLE DENTS ON UNDERSIDE OF NR 7 RT WING INBD GROUND SPOILER B737-800 SRM 51-70-01 REPAIR GENERAL PARA 4 PG 202-205. ALODINED, PRIMED, AND RESTORED PAINT IN REF TO B737-800 AMM 57-2SDR VNAA202101111111Pcu · malfunctionedDURING THE LATER STAGES OF APPROACH INTO CLT, THE CREW DEPLOYED THE FLIGHT SPOILERS, AND FELT AN UNCONTROLLED YAW OF THE AIRCRAFT AFTER DEPLOYMENT. THEY THEN RECEIVED AN AMBER ALERT MESSAGE FOR THE OUTBOUND SPOILERS ABOUT 3 SECONDS LATER. THE CREW PROCEEDED SDR DXTA202101044555Electronic Unit · defectiveAIRCRAFT EXPERIENCED A MOMENTARY LOSS OF POWER TO THE STANDBY ATTITUDE INDICATOR THAT SUBSEQUENTLY REINITIALIZED. AT THAT POINT WE RECEIVED A RUDDER MAINTENANCE WHITE CAS MESSAGE. 2) YAW DAMP FAIL A-B WITH SIGNS OF DUTCH ROLL; 3) WE GOT THE GND SPOILER FAULTSDR AALA202012239016Switch · inoperativeAIRCRAFT WAS NOT GROUNDED. SPEEDBRAKE ARMED LIGHT DID NOT ILLUMINATE WHEN THE SPEEDBRAKE WAS ARMED FOR LANDING. AFTER LANDING, THE SPEED BRAKE HAD TO BE DEPLOYED MANUALLY. SUPPLEMENTAL REPORT: REPLACED SPEEDBRAKE ARM SWITCH AND ACCOMPLISHED ADJUSTMENT AND TSDR CALA2020122101404Computer · malfunctionedGROUND SPOILER 1 AND 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL FOUND F/CTL GROUND SPOILER 1 & 2 FAULT DISPLAYED ON UPPER ECAM. PRINTED PFR, FOUND THE SAME WARNING MESSAGE, AND SEC3 OR INPUT OF L THROTTLE CTL UNIT 8KS1 FAILURE MESSAGE. TROUBLESHOT PER TSSDR AALA202012219036Switch · malfunctionedSPEEDBRAKE ARMED LIGHT DOES NOT ILLUMINATE WITH SPEEDBRAKES IN ARMED POSITION, LIGHT CHECKS GOOD. SPEEDBRAKES DID NOT AUTO DEPLOY ON LANDING. REPLACED SPEED BRAKE SWITCH S276, IAW AMM 27-62-32. OPERATIONS CHECK GOOD. (CLOSED)SDR SWIA202055672Bolt · corrodedLT INBOARD FLIGHT SPOILER OUTBOARD PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACES CORRODED HARDWARE ON LT INBOARD FLIGHT SPOILER PCU, (ITEMS 20, 24 IN AMM), IAW CRJ-200-AMM 27-62-01-000-801 STEPS 3 D (6) & (7) AND CRJ-200-AMM 27-6SDR VNAA2020111211211Warning Message · illuminatedMAINTENANCE EMERGENCY FOR INBOARD SPOILERONS CAUTION MESSAGE IN FLIGHT. CREW DID NOT HAVE PASSENGERS BRACE OR THE FIRE TRUCKS ROLL. WAS ABLE TO LAND SAFELY AND TAXI TO GATE UNDER OWN POWER.SDR TIPR2020121044537Control Cable · frayedLEFT WING, REAR SPAR RSS 135+/- SPOILER CONTROL CABLES HAVE MULTIPLE BROKEN STRANDS, REPLACED CABLES.SDR AALA202010149010Motor · defectiveAIRCRAFT WAS GROUNDED. AT CRUISE EICAS MESSAGE "SPOILERS", NR 5 SPOILER NO OUTPUT APPEARED. A NOTICEABLE SLOW AIRCRAFT ROLL AND FLUTTER/BUFFETING WAS REPORTED BY THE FLIGHT CREW. THE AIRCRAFT DIVERTED TO ORD WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. SDR VNAA2020100711101Pcu · failedOUTBOARD SPOILERON/OUTBOARD FLT SPOILERS CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED RT OUTBOARD MULTI-FUNCTION SPOILERON PCU. LEAK CHECK AND OPS CHECK GOOD.SDR ASMF202011007Switch · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXIING, WHEN PRESS TOGA FOR TAKEOFF SOUNDS THE ALARM OF TAKEOFF CONFIGURE WITH FLAPS 1 AND STAB TRIM 6.1. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU, IAW FIM 32-09 TASK 801 PROCEDURE AND FIM 27-62 TASK 808 PROCEDSDR VNAA2020092411101Warning Message · false activationDESCENDING IINTO PHL CREW RECEIVED OB SPOILER ON MESSAGE AND SPOILER ON MESSAGE. PERFORMED OPERATIONAL CHECK OF MFS, IAW CRJ 700 AMM 27-62-01-710-801-A01. OPS CHECK GOOD. PERFORMED LEAK CHECK OF MFS PCU, IAW CRJ 700 AMM 27-62-01-790-801-A01. LEAK CHECK GOOSDR ABXA20200803180Spoiler Sys · malfunctionedABORTED T/O SPOILERS NOT FULLY STOWED. AIRCRAFT RETURNED TO GATE. AIRCRAFT WAS GROUNDED FOR MAINTENEANCE. PERFORMED OPERATIONAL CHECK OF SPOILERS/DEPLOYED AND STOWED PROPERLY, IAW B767 AMM 27-61-00. AIRCRAFT RETURNED TO SERVICE.SDR IPXA202009160250Speed Brake · malfunctionedINSPECTION TYPE: CK SPEED BRAKE DID NOT AUTO DEPLOY WHEN ARMED FOR LANDING.AUTO SPEED BRAKES FUNCTIONED NORMAL, PER AMM 27-60-00. NO DISCREPANCIES.SDR AALA202009039007Switch · dirtyAIRCRAFT NOT GROUNDED - ABORTED TAKE-OFF - TAKE-OFF CONFIGURATION WARNING ON TAKEOFF. FOUND SPEED BRAKE LEVER WAS NOT ALL THE WAY DOWN. CLEANED AND LUBED MICROSWITCH, AND ACCOMPLISHED SPEED BRAKE OPERATIONAL CHECK PER AMM 27-62-00, CHECKED GOOD, OKAY FOR SERVSDR FDEA2020090312078Switch · failedREJECTED T/O FOR CONFIG SPOILERS EICAS WARNING. RAN QRH, TRIED TO T/O AGAIN, SAME ISSUE. RAN QRH AND RETURNED TO GATE. REMOVED SPEED BRAKE HANDLE POSITION SWITCH S493 IAW AMM 31-51-03-4, AND REPLACED TB190 XA1 AND YA1 IAW SWPM 20-90-11, AND RETERMINATED NUMSDR HNAA2020090100251Spoiler Sys · malfunctionedDURING TAKEOFF ROLL AT ABOUT 70 KTS MASTER WARNING LIGHT ILLUMINATED, SPOILER INDICATED OPEN, AND AURAL WARNING TAKEOFF SPOILERS. SPOILERS CLOSED AFTER T/L RETURNED TO FLIGHT IDLE. NO RELATED CMC MESSAGES FOR TODAY. RESET SPOILER SYSTEM. OPERATIONS CHECK SDR FDEA202008292064Hinge Arm · delaminatedRT WING, NR 4 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 25MM,D=1.45MM). RT WING, NR 4 SPOILER I/B & O/B CTR HINGE ARM DELAMINATED. COMPLY WITH EA: 6-5750-T0356104; TITLESDR FDEA202008191929Servo Valve · leakingPASSING THRU 15,000 FT ON CLIMBOUT RECEIVED A YELLOW SYS LO PR ECAM INDICATIONL THE YELLOW SYS QUANITY DROPPED TO APPROX THE RED DOT IN THE YELLOW ARC. WE COMPLIED WITH ALL ECAM AND QRH PROCEDURES AN DECIDED UPON A DEVERSION TO KMEM. WHILE DEBREIFING CRE
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