JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap 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 = '2750' 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 = '2750' 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 01FDEA00888Connector · faulty01-337 ASSYMETRICAL INBD T/E FLAP BETWEEN 2 & 5 DEG AFT T/O. R&R RIGHT INBD FLAP POS TRANSMITTER ELECTRICAL CONNNECTOR.SDR CA011114009Connector · corroded(CAN) FLAP FAIL AMBER CAUTION MESSAGE APPEARED DURING APPROACH (SPEED 250 KNOTS, 5000 FT FLAPS SET 0 DEGREES) FOUND CIRCUIT BREAKER 2-F4 TRIPPED. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND UNEVENTFUL FLAPLESS LANDING COMPLETED. NOTE: THIS IS LAST OF A SDR DL764011653Indicator · malfunctionedAIR TURNBACK- TRAILING EDGE FLAP DISAGREE MESSAGE ON DEPARTURE, FLAPS LOWERED USING ALTN FLAPS. MAINT-- FSEU BITE SEE FIM 27-51104 MSG, T/S PER FIM 27-51-00 PG 150 FIG 105A SHT 1 AND 2. FOUND OVERLOAD TRIP INDICATORS ON TRAILING EDGE ACTUATORS NR 3, 6 & 8. SDR GAI2001F00000Wire · dirtyAFTER TAKE OFF, THE FLIGHT CREW DISCOVERED THAT THE OUTBOARD FLAPS WERE STUCK AT THE 2 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. RESET ASYMMETRY CIRCUIT AND CLEANED CANNON PLUG SDR 2001F00684Flap · malfunctionedBGI - FLT 7106 - FIVE MINUTES INTO FLIGHT, FLIGHT CREW RECEIVED A FLAP DISAGREE FAULT INDICATION AND RETURNED TO BGI AND PERFORMED FLAPLESS LANDING DURING WHICH THE FAULT CLEARED ITSELF. INSPECTED FLAPS AND CYCLED FLAPS THROUGH ALL POSITIONS THREE TIMES AND CSDR C2XA01TY156Shaft · brokenTYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE LEFT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETSDR C2XA01TY155Shaft · brokenTYS DURING A SCHEDULED INSPECTION THE NR 1 FLAP FLEX SHAFT ON THE RIGHT HAND SIDE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FLAP FLEX SHAFT IAW EMB-145 MM 27-51-06, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLESDR BEM2001F00000Motor · damagedFLAPS FAILED TO MOVE.SDR COMA0160789Bpsu · malfunctionedFLIGHT #5431. FLAPS FAILED AT 39 DEGREES.REPLACED THE L/H BPSU.SDR S01257039Jackscrew · damagedB-18751 GRD CHK FOUND NR 1 FLAPTRACK JACKSCREW FITTING BROKEN.C/A:1.ISSUED REVISION OF EO 740-57-50-0004 TO PERFORM THE REPLACEMENT/OVERHAUL IN LIEU OF INSPECTION. 2.REPLACED WITH NEW FITTING NR 1 THROUGH NR 8 PER 742-57-639359-001R1. 3.PROVIDE BROKEN FITTISDR COMA0160788Flap · failedFLIGHT 5671, FLAPS FAILED AT 30 DEGREES DURING LANDING APPROACH. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE.SDR COMA0160787Flap · failedFLIGHT 5234 - FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE.SDR UPS01237058Panel · crackedINSPECTION TYPE:C RH WING, WHILE BLENDING PAINT FROM A DENT ON PANEL 65-21655-470 IT W AS NOTED THAT THE UPPER SKIN WAS CRACKED REPAIRED IAW SRM 51-40-20SDR 01FDEA00822Support · crackedN 1137 L/W I/B SPOILER SUPPORT BEAM CRACKED OF I/B END. ** S/D ** COMINGSDR 2001F00624Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR 2001F00623Shaft · defectiveINSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M)SDR 2001F00622Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR 2001F00621Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.SDR COMA0160793Actuator · failedFLIGHT 5420. FLAPS FAILED AT 23 DEGREES DURING LANDING APPROACH. POST FLIGHT INSP. FOUND R/H OUTBD FLAP TWISTED.REPLACED THE R/H OUTBD FLAP, BOTH FLAP ACTUATORS AND THE FLEX DRIVE SHAFT.SDR ABXA010526Control Cable · brokenA FLAP RUDDER STOP INOP LIGHT ILLUMINATED WHEN FLAPS WERE SET TO FIVE DEGREES. THE LIGHT EXTINGUISHED AT 15 DEGREES FLAP SETTING AND REMAINED EXTINGUISHED. MAINTENANCE INSPECTED AND REPLACED FLAP CONTROL UP CABLE 75B IAW DC9 MM 27-52-00-02, DUE TO IT BEING BROSDR SWIA200110220Fcu · malfunctionedON TAKEOFF WE GOT THE FLAP AND ADVANCED SWS ON MAP AND CONTROL FAULT. ASYMMETRY AND DISAGREEMENT ON OVERHEAD FLAP PANEL AND FLAP DEG. INDICATOR WENT TO 0 DEGREES. ABORTED TAKEOFF. POWERED DOWN 5 MINUTES AND IT REPLICATED SAME PROBLEM AFTER POWER UP. RE-RACKSDR COMA0160776Transmitter · faultyFLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A FLAP CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITH FLAPS OSCILLATING BETWEEN 2 AND 5 ABOVE SELECTED POSITION.REPLACED THE FLAP POSITION TRANSMITTER.SDR COMA0110148Roller · wornFLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY.SDR DHL2001720012Flap · malfunctionedON TAXI OUT ELP, INBOARD FLAPS WOULD NOT EXTEND TO THE SELECTED POSITION OF 15 DEGREES. MX ADVISED TO RESET INBOARD T/E FLAP POSITION CB. RESET INDICATOR WENT FROM 0 DEGREES TO 20 DEGREES. TAXI BACK TO GATE. WENT TO APU AND FLAPS THEN INDICATED 15 DEGREES.SDR F3LA200100108Coupling · disconnectedAIR TURN BACK. FLIGHT CREW REPORTED FLAPS DID NOT RETRACT AFTER TAKEOFF. LT. TORQUE TUBE COUPLING AT NO. 4 FLAP TRANSMISSION WAS DISCONNECTED. RECONNECTED COUPLING PER MM 27-51-251. ADJUSTED TRAILING EDGE FLAPS PER MM 27-51-01 AND PERFORMED OPERATIONAL TESSDR 01FDEA00855Control Unit · malfunctionedAFT T/O FLAP RETRACT AND ECAM ALERT FLAP 1 & 2 FAULT. SFCC 1 & 2 RESET. SLAT AND FLAP CYCLE CK NORMAL.SDR SWIA200110212Fcu · malfunctionedON CLIMBOUT RECEIVED A FLAP DISAGREEMENT AND FLAPS WOULD NOT FULLY RETRACT. RETURNED TO FAT. AIRCRAFT IN FOR C CHECK INSPECTION. DETAILS FORTHCOMING. UPDATE: PULLED FCU, MEGGED WIRES TO BOTH INBOARD FLAP ACTUATORS. NO DEFECTS NOTED. CHECKED ANNUNCIATORS FOSDR SWIA200110178Control Unit · malfunctionedTAXI OUT RECEIVED FLAP CONTROL FAULT ANNUNCIATION ON OUTBOARD PAIR, ONE ROW OF LIGHTS. RETURNED TO GATE.REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.S/N ON: 0016 S/N OFF: 156SDR SWAA012580Flap · delaminatedDURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND LH T/E OTBD FLAP DELAMINATED AT UPPER INBD SURFACE. REPAIRED FLAP PER SRM.SDR AWXA200100452Flap · malfunctionedSFO - FLAP LOCKOUT - FLT 815 - C - ON APPROACH TO SFO FLAPS 5 WAS SELECTED AND THE FLAP POSITION INDICATOR NEEDLES SPLIT AT FLAPS 1 AND THE FLAPS STOPPED AT FLAPS 1. THE AIRCRAFT LANDED AT FLAPS 1 AND UPON TOUCHDOWN THE FLAPS MOVED TO FLAPS 5 AS WAS SELECTED.SDR COMA0160732Bpsu · malfunctionedFLIGHT #5589. FLAPS FAIL CAUTION MESSAGE DURING TAXI. DISCREPANCY DID NOT DUPLICATE BUT COMPUTER INDICATED R/H BPSU AS MOST LIKELY SUSPECT.REPLACED THE R/H BPSU.SDR SWIA200110174Selector Switch · malfunctionedFLAPS WILL NOT MOVE WHEN 45 DEGREES IS SELECTED.REMOVED AND REPLACED FLAP SELECTOR LEVER IAW MM 27-50-01. OPS CHECK GOOD IAW 27-50-00.SDR CA011003014Bracket · broken(CAN) FLAPS WOULD NOT EXTEND PROPERLY FOR TAKEOFF. PILOT LEFT FLAPS IN UP POSITION AND RETURNED TO BASE. BRACKET IS MOUNTED TO LOWER BULKHEAD USING 4 SCREWS AND LOCKNUTS ON THE 4 MOUNT TABS. BOTH INBOARD TABS ON BRACKET HAD FAILED AT THE BEND RADIUS, ALLOWING SDR ZW0A0108604Pulley Bracket · crackedDURING CHECK-C MAINT IN RT WHEEL WELL FOUND CRACK IN MOUNT BRACKET FOR FLAP BUS CABLE PULLEY MOUNT AT STA 994 TO 1003, BETWEEN LONGERON 20R AND 21R. ACCOMPLISHED NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND CONFIRMED CRACK. REMOVED CRACKED PART. INSTASDR CA010914004Bolt · bent(CAN) DURING A 100/500 HOUR INSPECTION THE LT FLAP BELLCRANK BOLT (P/N ONL3120.146X77)WAS FOUND TO BE BENT. THE BOLT WAS REPLACED WITH A NEW ONE. IT IS SUSPECTED THAT A STUDENT PILOT EXTENDED THE FLAPS ABOVE THE MAXIMUM SPEED ALLOWED FOR FLAP EXTENSION. THE MASDR 01FDEA00816Flap · vibrationVIBRATION ON SELECTING FLAPS TO 50 DEG. NO PROBLEMS FOUND ON FLT CONTROL INSP. AC OK FOR SERVICE.SDR SWIA200110153Control Unit · malfunctionedFLAP FAIL MESSAGE ON EICAS WHEN FLAPS SELECTED TO 30 DEGREES.COMPLIED WITH AD 98-20-01 BY COMPLYING WITH PARAGRAPH (B)(1) 1-4. NO DISCREPANCIES NOTED.SDR AUS20010975Jackscrew · contaminated(AUS) FLAP SCREWJACK BALLNUTS WATER CONTAMINATION. NR 2 LT, NR 2 RT AND NR 3 RT SCREWJACKS AFFECTED.SDR AUS20010969Computer · faulty(AUS) FLAP COMPUTER FAULTY.SDR SWIA200110145Control Unit · malfunctionedFLAP CONTROL FAULT IN CRUISE FLIGHT. DID NOT RESET AS PER QRH PROCEDURE. OUTBOARD FLAPS REMAINED IN UP POSITION THROUGHOUT APPROACH AND LANDING.REMOVED AND REPLACED ANNUNCIATOR. REMOVED LEFT INBOARD FLAP AND REPLACED ALL BEARINGS AND LEFT INBOARD MOVEABLE TSDR SWIA200110143Connector · dirtyAFTER TAKEOFF ON RETRACTION FLAP DISAGREEMENT WITH ASSOCIATED AIRCRAFT ROLL TO THE RIGHT. INSPECTED FLAP SYSTEM WITH BREAKOUT BOX AND THE MAINTENANCE MODE. FOUND NO FAULTS. CLEANED CANNON PLUGS. FOUND MOISTURE AND GREASE. OPS CHECK GOOD.SDR AUS20010959Controller · malfunctioned(AUS) FLAP SYSTEM FAULTY. FLAP DRIVE SYSTEM INSPECTED AND NO FAULTS FOUND. FLAPS CYCLED AND FAULT DISAPPEARED. LIMITED INFORMATION PROVIDEDSDR C2XA01IA351Control Handle · dirtyIAH - FLIGHT 3745, THE CREW REPORTED A LANDING GEAR AURAL WARNING IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED THE FLAP CONTROL LEVER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR SWIA200110141Control Unit · malfunctioned''FLAPS FAIL'' MESSAGE APPEARED WHEN SELECTING FLAPS TO ''30''.FLAPS FAIL MESSAGE CLEARED AFTER POWER CYCLE. COMPLIED WITH AD 98-20-01. FECU FAULT CODE 311/5/A. FLAPS VISUAL INSPECTION CHECKS GOOD, FUNCTIONAL CHECKS GOOD.SDR P2EA01171Flap · malfunctionedFLT 451-MCI- ON APPROACH INTO MCI WHEN FLAPS SELECTED TO 1, FLAPS DID NOT EXTEND. RECYCLED AND FLAPS EXTENDED UP TO 15, BUT WOULD NOT GO TO 25. RECYCLED THE HANDLE A COUPLE OF MORE TIMES AND FLAPS FINALLY EXTENDED TO 25 AND THEN 30. AFTER LANDING, FLAPS RETRACSDR STZ2001F00001Transmission · inoperativeON TAXI AFTER LANDING, PILOT SELECTED FLAPS UP, HEARD A LOUD POPPING SOUND, FLAPS STOPPED RETRACTING, AND FLAP FAULT LIGHT ILLUMINATED. MAINTENANCE FOUND RIGHT HAND FLAP HANGING LOOSE IN FULL DOWN POSITION. FLAP JACKSCREW BECAME SEPARATED FROM FLAP TRANSMISSDR SWIA200110136Control Unit · malfunctionedAFTER FLAP RETRACTION AFTER TAKEOFF INBOARD FLAP DISAGREEMENT. ATTEMPTED CONTROL WITH FLAP HANDLE PER QRH TO NO EFFECT.TROUBLESHOT FLAP SYSTEM IAW MM 27-50-01 AND IAW FIM 27-50-01. COULD NOT GET A FAILURE. ALSO REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.SDR CA011003008Switch · failed(CAN) DURING DESCEND IN PREPARATION FOR LANDING FLIGHT CREW SELECTED FLAPS DOWN TO 17 DEGREES. THE FLAPS DID NOT OPERATE AND THE SELECTOR WAS RETURNED TO ZERO. CREW LANDED AIRCRAFT WITH ZERO FLAPS. MAINTENANCE DISCOVERED THE R/H SPLIT FLAP SAFETY SWITCH FAILESDR DHL2001727610Jackscrew · looseAT C CHECK; LT WING INBD FLAP INBD JACKSCREW (NO.4)HAS EXCESSIVE PLAY AT UNIVERSAL BUSHINGS AND AT JACKSCREW TO YOKE ATTACH BOLT. REMOVED AND REPLACED INBD FLAP JACKSCREW NR 4 AS PER DHL 727 M/M 27-51-41, RIGGED AND ADJUSTED FLAPS PER B727 M/M 27-51-1, OPS CHESDR SWIA200110126Control Unit · malfunctionedFLAP ASYMMETRY THEN DISAGREEMENT ON THE GROUND AFTER APU START. NO HYDRAULIC PUMPS ON.INSTALLED A SERVICEABLE FCU. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO FAULTS NOTED. S/N ON: 0028 S/N OFF: 0221
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