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 04FDEA02973Fitting · corrodedRT WING IB FLAP VANE, OB TEE FITTING BORE HOLES HAVE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81570.SDR SWAA043063Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED. REPAIRED NR 1 L/E SLAT PER SRM.SDR DHL2004755501Structure · crackedDURING C-CHECK, NR 2 SLAT AT I/B TRACK ATTACH WBL 592 HAS OTBD FRAME WITH CRACK IN FWD LOWER RADIUS. STOP DRILLED CRACK NR 2 SLAT I/B TRACK WBL 592 IAW B727 SRM 51-10-1. FABRICATED DOUBLER P/N CRESS AISI 321.032 PO 900878, 5 X 3 INCH IAW B727 SRM 57-50-3, NDSDR SWAA043000Wedge · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR ABXA040374Structure · damagedEICAS MESSAGE, L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUMINATED. REPAIRED PER REA B657-50865 FOR NON-REV FERRY FLIGHT TO REPOSITION FOR PERMANENT REPAIRS IAW GMM CHAP 1, SECT 7.04. REPLACED NR 8 SLAT IAW B767 MM 27-81-02.SDR WLDA2004120Skin · crackedDURING 2C+12A CHECK, FOUND LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK AT XIS 360. REPAIRED LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK PER EGAT EI W2004A57B-592 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 33 AND FIG 10). PERFORMEDSDR WLDA2004119Skin Panel · nickedDURING C2+12A CHECK, FOUND NICK ON RT WING INBOARD FLAP ON STA XIFH 152WITH D=0.039" AND L=3/8". REPAIRED NICK ON RT WING INBOARD FLAP UPPER SKIN AT XIFH 152 PER EGAT EI W2004A57B-585 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 34 SHEET 3). CONDITION CHECK SATISFACSDR WLDA2004114Skin · dentedDURING 2C+12A CHECK, FOUND SHARP DENT ON LT WING NR 3 SLAT UPPER SKIN AND INNER RIB AT STA XOS 414. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-581 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33). PERFORMED SLAT OPERATION AND CONDITION CHECK, FOUND SATISFACTORY.SDR WLDA2004113Skin Panel · dentedDURING 2C+12A CHECK, FOUND 2EA SHARP DENT ON LT WING NR 1 SLAT UPPER SKIN PANEL LOCATED AT STA XIS 240. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-564 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). SLAT OPERATION AND CONDITION CHECK SATISFACTORY.SDR WLDA2004112Skin Panel · puncturedDURING 2C+12A CHECK, FOUND LT WING NR 1 SLAT L/E AREA HOLE DAMAGE AT STA XIS 186. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-560 REV 00 (MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). PERFORMED SLAT OPERATION CHECK, FOUND NORMAL.SDR IXXA0500075SVane · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND LT WING EXTENDED LEADING EDGE O/B VANE PLATING HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA. AN NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBELR, FILLER INTERNAL DOUBLER. CLEANED, TREATESDR IXXA0500072SVane · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENDED LEADING EDGE INBOARD VANE PLATING INTERIM REPAIR AROUND STA XS 247.000. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF THE FASTENERS WITHIN REPAIR AREA AND THE EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SSDR IXXA0500071SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENED LEADING EDGE OUTBOARD VANE PLATING REPAIR DOUBLER WITH ELONGATED HOLES AND CRACK DAMAGE BETWEEN STA XOLDO 67.000 AND XS 497.491. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER AND REMOVALSDR IXXA0500070SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT OUTER WING INBOARD EXTENDED LEADING EDGE OUTER LOWER PLATING WITH INTERIM REPAIR AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR. THE DAMAGED SECTION WAS REMOVED AND A NDT INSPECTION WASDR A6WA200160048Structure · wornWEAR DAMAGE TO THE LOWER L/E OF THE LT FLAP IN THE RECESSED AREA BETWEEN RIBS 25 AND 31. MAINTENANCE REPAIRED WEAR DAMAGE IAW BAE FAX BARA/AVR/6894/04-DC.SDR SWAA042905Skin · crackedDURING SCHEDULED C3 CHECK, FOUND LT WING L/E NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER SRM.SDR AWXA200401137Skin · crackedDURING C-18 CHECK, 2 EACH 3/4 INCH CRACKS WERE FOUND IN LOWER SKIN OF NR 1 SLAT BELOW OUTBOARD MAIN TRACK SLAT STA 355 - 357. MAINTENANCE CUTOUT DAMAGE IN NR 1 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-4SDR USAA040942Skin · delaminatedPIT - Q5 - NR 2 SLAT, 2 SQ INCH AREA, DELAMINATION, IB T/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10.SDR USAA040784Skin · crackedPIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.SDR AWXA200401145Skin · debondedDURING C-18 CHECK, A DISBOND AREA WAS FOUND ON UPPER SURFACE OF NR 6 LEADING EDGE SLAT AT THE INBOARD END WBL 254.40 - 257.90 RT. MAINTENANCE CUTOUT DAMAGED SECTION ON NR 6 LEADING EDGE SLAT; FABRICATED A FILLER AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW BSDR CALA0400660Skin · crackedNR 1 SLAT LOWER SKIN CRACKED AT TWO RIVETS FWD OF I/B AUX TRACK. REPAIRED SLAT SKIN PER SRM 57-43-01.SDR CALA0400656Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN THE NR 3 SLAT LOWER SKIN AT O/B MAIN TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01.SDR AWXA200401184Skin · crackedDURING C-18 CHECK, 18 CRACKS WERE FOUND AT FASTENER HOLES IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STA 150 AND SLAT STA 235. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE SKIN OF NR 5 SLAT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; SDR USAA040671Support Angle · crackedCRACK IN NR 7 SLAT SUPPORT ANGLE. NR 7 SLAT LOWER T/E, 54 INCHES FROM OB END. REPLACED WITH FABRICATED ANGLE IAW SRM 51-40-02.SDR UPS04M43170Fitting · crackedINSPECTION TYPE: C, LEFT WING LEADING EDGE NR 16 TRACK ROLLER FITTING FOUND CRACKED. LEFT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. LEFT WING LEADING EDGE NR 16 SLAT TRACK FITTING REMOVED PER SRM 51-33-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HSDR C1HA200497015Skin · crackedNR 4 SLAT EXTERNAL SKIN IS CRACKED 2 (EA) PLACES AT AERODYNAMIC FENCE MOUNTING AREA, (MARKED). REPAIRED 2 (EA) CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1 TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED.SDR C1HA200497016Skin · crackedNR 4 SLAT EXTERNAL SKIN IS CRACKED 2 PLACES AT AERODYNAMIC FENCE MOUNTING AREA (MARKED). REPAIRED 2 CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1. TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED.SDR ASAA0480501Slat Track · wornRT SLAT TRACK NR 3 AFT IB RUB BLOCK FAILS CLEARANCE CHECK AND WORN. REWORKED RUB BLOCK IAW EA 2780-01020.SDR 2004UALA00909Arm · crackedLT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING.SDR C1HA200497010Rib · crackedNR 3 SLAT O/B CAP END SKIN IS CRACKED. CRACK=8 INCHES. REPLACED RIB.SDR SWAA042710Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA.SDR SWAA042707Skin · crackedDURING SCHEDULED C1 CHECK, FOUND 5 EACH CRACKS AT LT WING NR 2 L/E SLAT. REPAIRED NR 2 L/E SLAT SKIN PER SRM.SDR USAA040681Skin · crackedPIT - FOUND NR 2 SLAT WITH 4 CRACKS .125 INCH, TWO .375 INCH CRACKS AND .0625 INCH CRACK, 4 RIVET HOLES, LOWER SKIN UNDER ACTUATOR ATTACH AREA. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR SWAA042689Skin · crackedDURING SCHEDULED D-CHECK, FOUND LT WING NR 2 L/E KRUEGER FLAP CRACKED. REMOVED AND REPLACED LT WING NR 2 L/E KRUEGER FLAP PER MM.SDR AWXA200401158Skin · crackedDURING C-18 CHECK, 4 EACH 3/8 INCH CRACKS WERE FOUND IN NR 4 SLAT LOWER SKIN BETWEEN SLAT STA 42 - 78. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206.SDR C1HA200497014Skin · crackedNR 4 SLAT LEADING EDGE LOWER SKIN IS CRACKED AT AERODYNAMIC FENCE AFT LOWER MOUNT AREA (MARKED). REPAIRED PER SRM.SDR UPS04243204Skin · corrodedINSPECTION TYPE:C, NR 4 KRUEGER FLAP HAS CORROSION ON INNER SURFACE BELOW ACTUATOR ATTACH AREA. CORROSION REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 57-50-01. L/ED GE KRUEGER FLAP REMOVED IAW AMM 27-81-01 STEP 2. ACTUATOR ROD END BEARING FOUND TO BE WORNSDR C1HA200497002Rib · gougedNR 4 SLAT O/B SIDE CHAFED & GOUGED. REPLACED RIB.SDR DHL2004780512Doubler · crackedDURING A C-CHECK, NR 6 SLAT RIB REPAIR DOUBLER IS CRACKED AT NUT PLATE, INBD OF ACTUATOR. REMOVED ACCESS PNL AT SLAT NR 6 ROUTED OUT CRACK AREA, FABRICATED DOUBLER FROM 0.032 CRES AISI 321 PO NR 900878 DIM 6 1/2 X 3 3/4 AND TREATED PRIMED AND INSTALLED DOUBLESDR DHL2004780511Web · crackedDURING A "C" CHECK, NR 5 SLAT OUTBOARD END WEB IS CRACKED NEAR LEADING EDGE. REMOVED WEB AT NR 5 SLAT OUTBD END NEAR LEADING EDGE TO BE FABRICATED IAW B727 SRM 51-30-2. FABRICATED NEW WEB MAT USED 2024T3 .032 PO NR 9001030 DIMENSIONS 5 X 4 1/2 IAW B727 SRM 5SDR C1HA200497012Spar · crackedNR 3 SLAT FWD SPAR CRACKED AT SLAT STA 177 FWD OF ACTUATOR CONNECTION. INSTALLED REPAIR DOUBLERS.SDR C1HA200497006Rib · crackedNR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF ACTUATOR PISTON ROB END MOUNTING NUT (MARKED) WS 519. CRACK = 1 INCH. REPLACED RIB.SDR C1HA200497005Rib · crackedNR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF ACTUATOR PISTON ROD END AT WS 515 (MARKED). REPAIRED RIB.SDR C1HA200497004Rib · crackedNR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF SLAT ACTUATOR PISTON ROD END MOUNTING BOLT WS 410. CRACK = 0.500. REPLACED RIB.SDR C1HA200497003Rib · crackedNR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF SLAT ACTUATOR PISTON ROD END WS 408 (MARKED) CRACK = 0.490. REPLACED RIB.SDR MALA040708Skin · chafedDURING C1 INSPECTION IN YYC, LT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT CENTER ATTACH POINT. MAINTENANCE REPAIRED IAW EO A57073. A/C RETURNED TO SERVICE 09/14/2004.SDR USAA040714Skin · delaminatedNR 2 SLAT, 3 INCH BY 3 INCH AREA, DELAMINATION, INBD AND OTBD ENDS LOWER SKIN. REPLACED CORE, INSTALLED DOUBLER IAW SRM 51-70-10.SDR C1HA200497009Rib · crackedRT WING NR 7 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 1 EA ON THE LEFT AS MARKED. REPLACED RIB.SDR C1HA200497008Rib · crackedRT WING NR 5 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 2 EA ON THE LEFT AS MARKED (5 EA CRACKS TOTAL 1 EA PREVIOUSLY STOP DRILLED). REPLACED RIB.SDR GAIA04123Rib · crackedDURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86614, REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2.
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