JASC 2782
Service difficulty reports · 1,225
Reports filed under 2782 · Leading Edge Slat Actuator, 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 = '2782' 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 = '2782' 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 AU000801Actuator · corroded(AUS) NR 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR INTERNALLY CORRODED. RING GEAR SEAL MISSING.SDR 00FDEA00453Actuator · inoperativeSLAT FAULT LIGHT OVERHEAD AND ECAM SLAT SYS 1 & 2 CAME ON. FOUND LEFT O/B AND I/B, RT CENTER AND O/B LEADING EDGE SLAT JACK SCREW ACTUATORS OUT OF RIGG PER TSM 27-80-02 PG 107.SDR SWAA001104Actuator · inoperativeAIR TURNBACK, NR 1 L/E FLAP WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 1 L/E FLAP ACTUATOR PER MM.SDR 00FDEA00387Actuator · rupturedCOMPLETE LOSS OF SYS A HYD FLUID ON T/O. PER EMERGENCY AND ABNORMAL PROC HDBK CK LIST, 1 AND 2 ENG FLUID SHUTOFF SWITCHES CLOSED. NR 1 LEAD EDGE SLAT ACTUATOR FAILED WHILE EXTENDED. *S/D* REPLACED NR 1 SLAT ACTUATOR PER MM 27-81-32. LEAK AND OPS CK NORM.SDR DL72S001117Actuator · failedDURING FLIGHT BETWEEN DFW AND SEA AT FLT LEVEL 310, CREW EXPERIENCED AN A-SYSTEM LOW HYDRAULIC PRESSURE LIGHT FLICKERING. CREW THEN NOTICED THE A-SYSTEM QUANTITY INDICATION WAS AT ZERO. DIVERTED TO SLC. WHEN LOWERING FLAPS WITH ALTERNATE SYSTEM, CREW COULD SDR DL72S001107Actuator · leakingON T/O ROLL IN MSO, BOTH SYS A HYDRAULIC LOW PRESSURE LIGHTS CAME ON AT APROX 100 KIAS, SYS A QTY RAPIDLY WENT TO ZERO. T/O CONTINUED CHECKLIST C/W, UNEVENTFUL LANDING IN MSO. MTC FOUND NR 7 SLAT ACTUATOR LEAKING. REPLACED SAME.SDR EISA200000051Shuttle Valve · inoperativeNR 2 SLAT FAILED TO RETRACT AFTER TAKEOFF. COMPLETED ABNORMAL CHECK.SDR 20001114SH019Sensor · failedMBJ/ATL - FLT JM 053 - AIRCRAFT RETURNED TO RAMP DUE TO A RECURRENCE OF A SLAT/FLAP DISAGREEMENT LIGHT INDICATION FAULT AT 18,000 FEET. THE AIRCRAFT WAS ACCELERATED TO 280 KNOTS AND THE SLAT OVERSPEED AURAL WARNING CAME ON. QRH PROCEDURE ACCOMPLISHED, ACFT RSDR 00FDEA00363Actuator · leakingLOST A SYS QUANTITY ON LAND GEAR RETRACTION, LOST ALL A PRESSURE SHORTLY AFTER, COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 6 LEAD EDGE FLAP ACTUATOR PER 727-100 MM 27-81-22. NO LEAK, RE-SAFETY ALL SWITCHES IN COCKPIT WITH BREAK-AWAY WIRE.SDR WP012000B1305Stud · crackedFATIGUE CRACKS IN HOLE DETECTED DURING MAGNETIC INSPECTION.SDR L1GA200000066Shaft · shearedDURING POST FLIGHT WALK-AROUND INSPECTION AFTER THE COMPLETION OF FLIGHT NR 4, DAMAGE WAS NOTED TO PANEL 1242A RT WING. THE PANEL WAS REMOVED AND THE LOWER SLAT DRIVE CYLINDER WAS INSPECTED AND FOUND TO BE SHEARED.SDR 00FDEA00325Actuator · inoperativeAT CR ''A'' SYSTEM HYD QTY WENT TO ZERO, GEAR UP AND FLAPS UP. SHUT OFF ENGINE PUMPS (1 & 2) AND FLUID SHUT OFF (1 & 2) CRANKED GEAR DOWN. *S/D* REMOVED AND REPLACED NR 5 SLAT ACTUATOR AND NR 1 ENG A SYS HYD PUMP PER 727 MM 29-11-033-4, 29-11-033-5, 29-11-0SDR 0001789868Actuator · failedDURING APPROACH INTO DTW UPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE LEFT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND NO SLAT EXTEND INDICATION. PERFORMED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND INBOARD SLAT ACTUATOR BYPASSING. REPLASDR USAASB00133Actuator · failedIAD - FLT 2755 - ON CLIMB-OUT FROM IAD, THE NR 6 SLAT DID NOT RETRACT WHEN THE FLAPS WERE MOVED TO UP OR ZERO DEGREES. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 6 SDR 0001799856Actuator · malfunctionedDURING APPROACH INTO MSN UPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND NO SLAT EXTEND INDICATION. PLACED FLAP SELECTOR TO 15 DEGREES AND SLATS EXTENDED NORMALLY. MAINTENANCE FOUND NO OBVIOUS PROBLEM BUT LUBEDSDR DL72W000873Actuator · failedON DEPARTURE CLIMB WHEN FLAPS RETRACTED FROM 5 DEG TO 2 DEG, NR 8 LED REMAINED EXTENDED. REPLACED NR 8 SLAT ACT PER M/M, OPS AND LEAK CHECK GOOD.SDR DL72W000813Actuator · inoperativeNR 6 L/E FLAP WOULD NOT RETRACT ON CLIMB OUT. SYS NORMAL AFTER ACTUATOR REPLACEMENT.SDR USAASB00121Actuator · failedATL - FLT 2967 - ON DESCENT INTO ATL, WHILE EXTENDING FLAPS, CAPTAIN VISUALLY CONFIRMED THE NR 1 SLAT WAS NOT FULLY EXTENDED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AND EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AT ATL. MAINTENANCE RESDR DL72W000695Angle · crackedNR 8 SLAT I/B ACT ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.SDR DL757000688Actuator · failedAFTER TAKEOFF, GOT L/E SLAT DISAGREE, L/E SLAT LIGHT, EICAS MSG FLAP/SLAT ELECT. SLATS WOULD NOT RETRACT USING POM PROCEDURE. FLAPS/SLATS EXTENDED TO 20 DEG FOR RETURN/LANDGING. REPLACED O/B ROTARY ALT PER M/M, OPS CKS NORMAL.SDR AWXA0000249Actuator · failedDURING APPROACH INTO MCO, HAD LEADING EDGE DISAGREE MESSAGE AND LIGHT. ACCOMPLISHED L/E SLAT DISAGREE, WHICH LED TO THE L/E SLAT ASYMMETRY CHECK LIST. EMERGENCY DECLARED, HAD NORMAL APPROACH AND LANDING. T/S, FOUND L/E ROTARY ACTUATORS 4, 9, 11, 12 HAD POPPSDR 2000UALA00154Actuator · malfunctionedNR 4 LEADING EDGE SLAT CYCLING OPEN AND CLOSED IN FLIGHT. DIVERTED TO MCO. *S/D* REPLACED NR 4 LEADING EDGE FLAP ACTUATOR AND SWITCH PER 27-83-06, OPERATIONALLY CHECKS NORMAL.SDR 2000UALA00151Actuator · leakingON TAKEOFF AFTER FLAP RETRACTION A HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. LOW PRESSURE LIGHTS ILLUMINATED ON PUMPS. MANUALLY EXTENDED GEARS, ALTERNATE FLAP EXTENSION. RETURNED TO DEN. *S/D* REPLACED NR 2 LEADING EDGE FLAP ACTUATOR DUE TO LEAK.SDR SWAA000511Actuator · failedAIR TURNBACK, NR 3 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM.SDR DHL200072415CRod End · crackedAT C-CHECK, FOUND NR 6 L/E SLAT ACTUATOR ROD END ATTACH BOLT I/B AND O/B SUPPORT WEBS CRACKED AT LOWER AFT CORNERS. REMOVED NR 6 L/E SLAT IAW B727 M/M 27-81-11. STOP DRILLED CRACKED AREA PER M/M 51-10-01. PERFORMED HFEC INSP PER 727 NDT MAN PARTS 51.00.00 FSDR DHL2000705003Actuator · failedAFTER FLAP RETRACTION TO UP POSITION, FORWARD ANNUNCIATOR PANEL SHOWS AMBER LIGHT. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER MM 27-81-32.SDR AU000177Arm · corroded(AUS) DO 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR CORRODED INTERNALLY BENEATH BEARING.SDR 2000UALA00086Actuator · malfunctionedNR 1 LEADING EDGE FLAP DID NOT RETRACT ON CLIMBOUT AT FLAPS POSITION 2 BACK TO POSITION 5. RETURNED TO ORD. *S/D* REPLACED NR 1 L/E FLAP ACTUATOR PER MM 27-83-06. OPERATIONAL CHECK NORMAL. CHECKED ADJUSTMENT OF NR 1 L/E FLAP POSITION SWITCH PER MM 27-85-0SDR 2000UALA00079Actuator · leakingDIVERTED TO DEN DUE TO A HYDRAULIC SYSTEM PRESSURE AND FLUID LOSS. *S/D* FOUND NR 2 L/E FLAP ACUATOR LEAKING FROM SWIVEL. REPLACED NR 2 L/E FLAP ACTUATOR, OPERATIONAL CHECK AND LEAK CHECK PERFORMED. SYSTEM OPERATIONAL OK. NO LEAKS NOTED.SDR EISA2000043Actuator · crackedAFTER TAKEOFF, FLAPS UP APPROXIMATELY 225 INDICATED AIR SPEED AIRCRAFT WENT INTO LEFT BANK. HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO LEVEL FLIGHT. AIR TURN BACK TO CDG. REPLACED LEADING EDGE SLAT ACTUATOR IAW MM 27-81-00. (M)SDR EISA2000015Actuator · failedAFTER TAKEOFF FLAPS UP APPROX 225 IAS AIRCRAFT WENT INTO LEFT BANK, HAD TO USE 30 DEGREES RIGHT AILERON TRIM TO BRING AIRCRAFT BACK TO LEVEL FLIGHT. AIR TURN BACK TO (CDG). REPLACED LEADING EDGE SLAT ACTUATOR. OPS CHECK GOOD. (M)SDR CA000215019Actuator · failed(CAN) A/C TURNBACK DUE TO LE FLAP ACTUATOR WOULD NOT RETRACT. NR 2 LE FLAP INDICATES DOWN WHEN FLAP IN RETRACT POSITION. REPLACED.SDR 00FDEA00052Actuator · leakingAS FLAPS RETRACT AIR LIGHT FLICKERED ALONG WITH A SYS LOW PRESS LIGHT, THEN CAME ON STEADY. LOSS OF A SYS HYD LEFT NR 2 LEAD EDGE DEVICE FAIL. NR 2 KRUGER FLAP ACTUATOR LEAKING. *S/D* REMOVED AND REPLACED NR 2 LEAD EDGE ACT PER 727-200 MM 27-81-022-4.SDR DL757000206Actuator · malfunctionedL/E SLAT DISAGREE LIGHT ILLUMINATED ON TAKEOFF. PERFORMED PROC PER POM. LIGHT REMAINED ILLUMINATED. FLAPS INDICATED A LITTLE LESS THAN 1 DEG. REPLACED NR 6 I/B AND O/B SLAT ACTUATORS.SDR DHL200071798DMount · crackedAT D-CK, NR 1 SLAT ACTUATOR MOUNTS ARE CRACKED BOTH INBOARD AND OUTBOARD SIDES. PERFORMED HFEC INSPECTION TO VERIFY CRACKS. REMOVED AND REPLACED BOTH I/B AND O/B MOUNTS PER B727 S/B 727-57-0130 FIG 1 STEP 6. REF: N/R 1622.SDR DHL200071797DSupport · crackedAT D-CK, NR 1 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT INBOARD LOWER CORNER. REMOVED AND REPLACED I/B SUPPORT OF NR 1 L/E FLAP ACTUATOR MOUNT, PER B727 SRM 57-10-1 AND 51-30-2. REF: N/R 1637.SDR USAA010004Actuator · fracturedDCA/LGA - FLT 6378 - LOST A-SYSTEM HYDRAULICS ON FLAP EXTENSION. DIVERTED TO EWR. FOUND AFT END OF NR 8 L/E SLAT ACTUATOR BROKEN. REPLACED NR 8 L/E SLAT ACTUATOR. CHECKED RETURN AND CASE DRAIN FILTERS.SDR SWAA992149Actuator · inoperativeAIR TURNBACK, NR 3 KRUGER FLAP WOULD NOT FULLY RETRACT, TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 KRUGER FLAP ACTUATOR.SDR 99UAL900656Actuator · leakingFLIGHT RETURNED TO MIA DUE TO LOSS OF A SYSTEM HYDRAULIC FLUID. *S/D* REPLACED NR 5 LEADING EDGE FLAP ACTUATOR PER MAINTENANCE MANUAL.SDR DL72S992706Bracket · crackedA 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21.SDR 2000ZZZX190Body · crackedBODY ASSEMBLY IS CRACKED ON THE RETRACT PORT AT THE CROSS HOLE INTERSECTION IN TRUNNION BORE. BODY HAS SHARP CORNERS AT THE CROSS HOLE INTERSECTION IN THE TRUNNION BORE. INCORPORATE A RADIUS ON THE SHARP CORNERS OF THE INTERSECTION IN THE TRUNNION BORE IAW SSDR DL72S992683Bracket · crackedNR 1 LEADING EDGE SLAT I/B AND O/B ACTUATOR MOUNT BRACKETS CRACKED. REPAIRED PER MM 57-20-21.SDR DHL99742003Actuator · looseNR 1 L/E SLAT WOULD NOT RETRACT. FOUND NR 1 L/E SLAT ACTUATOR LOOSE IN MOUNT. TIGHTENED 4 MOUNT BOLTS, PERFORMED SYSTEM ADJ AND TEST. LIGHTS OPS CHECK GOOD PER MM 27-82-0.SDR DL72W992432Bracket · crackedINBD ATTACH BRACKET CRACKED NR 1 SLAT ACTUATOR BRKT. INSTALLED DOUBLER PER M/M 57-20-21. TPA F-1 LETTER CHECK.SDR DL72S992429Bracket · crackedA .125 INCH CRACK IN NR 2 L/E FLAP ACTUATOR SUPPORT BOX INBD LWR BRACKET. INSTALLED DOUBLER PER M/M 57-20-21.SDR DL72S992413Actuator · failedNUMBER THREE LEADING EDGE FLAP INDICATION AND UNCOMMANDED ROLL. REPLACED NUMBER THREE LEADING EDGE FLAP ACTUATOR.SDR DL72S992367Angle · crackedNR 8 SLAT ACTUATOR O/B ATTACH ANGLE WAS CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S992366Bracket · crackedTPA LTR CHK F-2, 1 VISIBLE CRACK O/B ATTACH BRACKET NR 1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21.SDR DL72S992326Fitting · crackedNR 4 L/E SLAT I/B ACTUATOR ATTACH FITTING WAS CRACKED 3 EA LOCATION THROUGH AN EXISTING REPAIR. REPAIRED DOUBLER PER M/M 57-54-0 FIG 804. REMOVED CRACKED PLATE, REPLACED CLIP PER 51-00. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-54-0 FIG 804.SDR DL72S992322Bracket · crackedNR 1 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER M/M 57-20-21 PG 812.
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