JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 DL767060016Skin · crackedCRACK DAMAGE WAS FOUND ON THE NR 8 LEADING EDGE SLAT, END RIB AT OSS 531.611. REPAIRED ERA 452170-14.SDR SWAA060058Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR DHL2006752524Attach Fitting · crackedFOUND RT WING NR 5 L/E SLAT ACT ROD END ATTACH FITTING, INTERNAL ANGLES INBOARD AND OUTBOARD ARE CRACKED. REMOVED INBOARD AND OUTBOARD RIBS ON RIGHT WING NR 5 SLAT ACT END ATTACH TO FITTING, IAW B727 SRM 51-30-2, FABRICATED 2 EA RIBS FROM 7075-0 .040 SIZE 16"SDR IXXA05SMN318SSkin · crackedDURING ROUTINE C CHECK, RT WING OTBD INNER L/E CRACKED .500 XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4139 DATED 01-04-06, EO SEMAN NR 20051476 DATED 01-06-06. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRMSDR IXXA05SMN317SVane · damagedDURING ROUTINE C CHECK INSPECTION, RT WING L/E SLOT VANE HOLE ELONGATED, XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4138 DATED 01-06-06, EO SEMAN NR 20051475 DATED 01-06-06. REMOVED EXISTING REPAIR DOUBLER IAW DSDR IXXA05SMN316SVane · damagedDURING C-CHECK, RT WING - L/E SLOT VANE HOLE ELONGATED, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05587 DATED 12-29-05, SEMAN DWG ED-4137 DATED 12-28-05, ED SEMAN 2005 1474 DATED 12-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC-8 SRM 51-3-0.SDR IXXA05SMN315SRepair · misinstalledDURING C-CHECK, RT WING - L/E SLOT VANE HAS NON STANDARD REPAIR, XOLDO 66. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05586 DATED 12-28-05, SEMAN DWG ED-4136 DATED 12-23-05, ED SEMAN 2005 1473 DATED 12-28-05. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED SECSDR DHL2006752502Skin · crackedDISCREPANCY FOUND NR 110620; CRACK INDICATION ON NR 2 SLAT SKIN UPPER SURFACE 6 INCHES O/B OF ACTUATOR MARKED. CUT OUT DAMAGED AREA DIMENSION 4" X 2" AND FABBED NEW DOUBLER FROM MATERIAL USE 2024 T3 0.80 PO 9002459 IAW B727 SRM 57-50-3 FIG 1 TREATED AND PRIMESDR UPS06145991Doubler · crackedINSPECTION TYPE:C2 RT WING KRUEGER FLAP BOX AREA CURVED DOUBLER HAS CRACK APPROX 1". REMOVED AND REPLACED DOUBLER IAW SRM 51-40-00.SDR 05FDEA04420Skin · dentedDENT ON RIGHT HAND INBOARD FLAP LEADING EDGE AT XIFH 174-179. REPAIRED LEADING EDGE SKIN IAW DC10-10 SRM 57-00-01 FIG 4 VOL I. ALODINED AND PRIMERED IAW DC10-10 SRM 51-21-01 VOL. II. SEE FEDEX SNRM NR N00291 OF WORK ORDER NR 00031297.SDR AWXA200600169Skin · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED 4 CRACKS, RANGING FROM .250 INCHES UP TO .500 INCHES IN LENGTH, ON THE BOTTOM NR 2 SLAT SKIN, BELOW THE OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED THE DAMAGE FROM THE NR 2 SLAT SKIN IAW BOEING 737-300 SRM 57SDR AWXA200600156Skin · crackedMCN - DURING C19 CHECK DISCOVERED 6 CRACK ON THE BOTTOM OF THE NR 1 SLAT SKIN, BELOW OUTBOARD AUX TRACK. MAINTENANCE REMOVED THE DAMAGED AREA ON THE BOTTOM OF THE NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-13-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEISDR AWXA200600040Wedge · debondedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE TOP OF THE NO. 6 SLAT WEDGE ABOVE THE INBOARD AUX TRACK AT WS 344R TO WS 348.5R. MAINTENANCE REMOVED DAMAGED AREA ON THE NO. 6 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILSDR UPS06245912Rib · crackedINSPECTION TYPE:C RIGHT NR 7 SLAT ACTUATOR RAM FWD ATTACHMENT FITTING INBOARD SUPPORT RIB CRACKED. PLS INVESTIGATE AND RECTIFY. SLAT ACTUATOR RIBS I/B AND O/B DISPLACED IAW SRM 51-30-3. HFEC CARRIED OUT AND FWD ATTACH FITTING INBOARD SUPPORT RIB CRACKS CONFSDR USAA051598Skin · damagedFOUND WS 1045.2 NR 12 SLAT RT WING. FAB'D A 4" ROUND DOUBLER PER SRM 57-43-02, DEFECT SIZE: 1.09"L BY .025"W (REPAIRED AS HOLE).SDR AWXA200600071Wedge · debondedMCN - DURING C15 CHECK DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 5 SLAT WEDGE DISBONDED FROM SS 124.0R TO SS 129.0R. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE AND DOUBLER IAW BOEING 737-300 SRM SDR AWXA200600073Skin · crackedMCN - DURING C15 CHECK DISCOVERED 5 CRACKS, .500 INCHES EACH, ON THE BOTTOM OF THE NR 3 SLAT SKIN FROM SS 102.75L TO SS 107.75L. MAINTENANCE CUT OUT THE DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SSDR AWXA200600070Wedge · debondedMCN - DURING C15 CHECK DISCOVERED THE UPPER SURFACE OF THE NR 3 SLAT WEDGE DISBONDED FROM SS 12.25L TO SS 16.25. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-SDR UPS06M46268Skin · dentedINSPECTION TYPE:C LEFT WING INBOARD NR 1 SLAT HAS DENT AS MARKED. LEFT WING INBOARD NR 1 SLAT DENT (QTY/01/EA) EVALUATED FOUND EXCEEDED PER SRM LIMIT. HFEC CUTOUT FOUND NO EVIDENT OF CRACK. DENT AREA FASTENERS REMOVED AS PER SRM 51-35-01V.2.R.38. DENT AREASDR SWAA053970Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE SKIN DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR USAA051557Wedge · damagedNR 3 LE SLAT ASSY IB TRAILING EDGE WEDGE. REMOVED DAMAGE ON THE WEDGE. DOUBLER REPAIR IAW 51-30-03 AND SRM 51-70-10 DEFECT SIZE: .6 IN X 8 IN.SDR 05FDEA04312Angle · crackedLT WING SLAT NR 4 FOUND 1 CRACK 1" LONG ON ANGLE AT STA XORS 506. REPLACED CLIP IAW MD-10-30 M/M 27-80-01-7 FIG 401 SHT 1 AND PERFORMED ADJUSTMENT IAW MD-10-30 M/M 27-80-01-7 FIG 408 SHT 1.SDR AU510001672Bearing · failedLT WING OUTBOARD KRUGER FLAP NOSE LINK EYE END SHEARED.SDR AU510001550Torque Tube · shearedINBOARD LEADING EDGE DRIVE SHAFT/TORQUE TUBE SHEARED. DRIVE SHAFT SHOWED SIGNS OF SEVERE CHAFING DAMAGE DUE TO WATER SUPPLY LINE AND ADJACENT CLAMP. TORQUE TUBE HAD BEEN WORN THROUGH BY MORE THAN 50 PERCENT OF THICKNESS PRIOR TO FAILURE DURING MAINTENANCE.SDR 05FDEA04255Skin · scratchedLT WING NR 2 SLAT UPPER SURFACE HAS SCRATCHES AND A PUNCTURE APPROX 2.7 BY 3.2" (NR 39 HURRICANE RITA) REF N00089. REPAIRED NR 2 SLAT IAW EA 6-5750-94524.SDR USAA051495Wedge · damagedFOUND NR 4 SLAT INBD LOWER CORNER BOTTOM SKIN WORK THROUGH ON TRAILING EDGE WEDGE. MAJOR REPAIR SRM 51-70-10, DEFECT SIZE: 1".SDR AWXA200600517Panel · delaminatedGYR - DURING C8 CHECK DISCOVERED DELAMINATION BETWEEN PLIES ON SLAT CLOSURE PANELS ON THE INBOARD AND OUTBOARD ENDS AT WS 425.50R. MAINTENANCE REPAIRED CLOSURE PANELS BY REMOVING DELAMINATED PLIES AND APPLYING REPAIR PLIES AND DOUBLERS USING BMS 9-3 FIBERGLASSDR SWAA053921Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND NR 5 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.SDR UPS06M46177Skin · chafedINSPECTION TYPE:C RHW DROOP L/E SLAT LWR I/B EDGE FOUND CHAFING MARK. CHAFING MARK BLENDED AND PROTECTED PER SRM51-21-01.V2.R.38.ORI THK 0.069 MAT REMOVED 0.055", REMAIN MAT THK 0.014", FOUND EXCEEDED LIMIT. REWORKED AREA EDGE TRIMMING FOUND REMAIN MAT THK 0SDR AWXA200600097Skin · crackedMCN - DURING C16 CHECK DISCOVERED 5 CRACKS, .80 INCHES EACH, ON THE BOTTOM OF THE NR 6 SLAT SKIN, FROM SS 320R TO SS 325R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FAB`D FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-4SDR AWXA200600096Skin · crackedMCN - DURING C16 CHECK DISCOVERED 4 CRACKS, .500 INCHES EACH, ON THE BOTTOM OF THE NR 4 SLAT SKIN, FROM SS 57R TO SS 61R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM SDR SWAA053901Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA053880Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OTBD UPPER CORNER. REMOVED AND REPLACED NR 5 SLAT PER MM.SDR AWXA200600099Skin · crackedMCN - DURING C16 CHECK DISCOVERED 1 CRACK, .375 INCHES, ON THE BOTTOM OF THE NR 3 SLAT SKIN, AT SS 92L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 2SDR AWXA200600098Skin · crackedMCN - DURING C16 CHECK DISCOVERED 2 CRACKS ON THE BOTTOM OF THE NR 3 SLAT SKIN, FROM SS 67L TO SS 69L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 20SDR 2005UALA01409Bracket · crackedLT WING KRUEGER FLAP INBD OF NR 1 PYLON, ROTARY ACTUATOR OUTBD SUPPORT BRACKET IS BUCKLED AND CRACKED. BRACKET FAILURE WAS DUE TO FATIGUE. PART WAS REPLACED.SDR 05FDEA04127Repair · properLT WING INBOARD FLAP FOUND A DOUBLER 8" BY 1" ON UPPER SKIN AT STA XIFH 147.300. PERFORMED A GVI OF REPAIR IAW SRM 57-20-00 FIG 11 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VSDR 05FDEA04100Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 67 TO WS 207. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVESDR DHL2005803523Skin · crackedNR. 032564: LT WING CTR LE UPPER SKIN HAS 2 CRACKS 0.250 INCH (STA XFS 285.250 - 291.500) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-30-05, DWG AA33-53-R04 REV JR DATE 11-14-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. TRIMMED OSDR 2005UALA01428Wedge · delaminatedT/E WEDGE DELAMINATED NR 5 SLAT. REPAIRED WEDGE IN SHOP 273 AUTOCLAVE PER SRM 50-57-56-01 ON R66 864.SDR SWAA053846Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR EIA2005261Skin · damagedLT WING LDG EDGE NR 2 KRUEGER FLAP IB HINGE ARE, IB FRAME WEB LOWER SECTION HAS 4 INCH CRACK AT APPROXIMATELY WS 426. REPAIRED NR 2 KRUEGER FLAP IB FRAME WEB LOWER SECTON AT WS 426 PER ECRA 477-57-107-2P, PART 1. AS APPROVED BY BACFAA FORM 8100-9, DATED NOV SDR DHL2005803520Structure · crackedITEM REF. NR. 033485: LT OB SLAT UPPER DOOR CRACKED (CTR DOOR). REMOVED AND REPLACED CTR DOOR ON LT OB SLAT UPPER DOOR IAW MM 27-80-2 PG. 201-203. FOR OPS CHECK SEE NR 038928.SDR 05FDEA03975Repair · improperLT WING L/E SLAT FOUND A DOUBLER 20 X 7 INCHES ON LOWER SKIN BETWEEN STA XW 340 AND STA XW 309. REMOVED PART. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 55 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001E3.SDR 05FDEA03965Skin · dentedRIGHT WING - NR 5 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR USAA051411Skin · crackedLWR SURFACE AT AFT ROW OF FASTNERS AT ACTUATOR MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR USAA051412Skin · crackedLWR SURFACE, AFT ROW OF FASTENERS AT ACTUATOR CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR USAA051413Skin · debondedNR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH.SDR USAA051410Skin · crackedLWR SURFACE, AFT FASTENER ROW AT OUTBOARD END TO 20.750 INCH INBOARD CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR 05FDEA03925Skin · dentedRIGHT WING, NR 3 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
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