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 SWAA002165Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND INBOARD T/E FOREFLAP DELAMINATED AT CENTER, 3 X 6. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA002152Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT, 6 CRACK, AT LOWER T/E SKIN, O/B OF THE O/B ACTUATOR STOP. REPAIRED SKIN PER SRM.SDR DL72L002118Angle · crackedA 1.25 INCH VISIBLE CRACK ON NR 3 SLAT AT O/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.SDR DL72L002117Rib · crackedA .75 INCH CRACK IN L/E NOSE RIB OF NR 7 SLAT AT O/B SIDE OF ACTUATOR ATTACH FITTING. REPAIR PER M/M 57-54-0.SDR 20010108AP010Structure · damagedON POSTFLIGHT, FOUND NR 15 LEADING EDGE KRUEGER FLAP DAMAGED AND APPROX HALF OF FLAP PARTIALLY SEPARATED ROM MOUNTS CAUSING IMPACT DAMAGE TO THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AND UPPER SURFACE. REPLACED NR 15 LEADING EDGE KRUEGER FLAP. REPAIRED DASDR 20010108AP009Structure · damagedON POSTFLIGHT, FOUND NR 15 LEADING EDGE KRUEGER FLAP DAMAGED AND APPROXIMATELY HALF OF FLAP PARTIALLY SEPARATED FROM MOUNTS CAUSING IMPACT DAMAGE TO THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AND UPPER SURFACE. REPLACED NR 15 LEADING EDGE KRUEGER FLAP. REPSDR TWAA0017303Structure · dentedDURING CHECK-C MAINT, THE LT WING L/E NUMBER 3 SLAT INBOARD L/E HAD WIND EROSION ON DENT FILLER IN DENT APPROX 2 FEET FROM INBOARD END. ACCOMP NDT AND NO CRACK FOUND PER PART 6 OF 51-00-03. SANDED OUT OLD FILLER AND REPLACED WITH NEW PER SRM 57-03 PAGE 20A.SDR MWEA001109Skin · crackedRIGHT HAND WING NR 4 SLAT HAS A 4 INCH WRAP AROUND DOUBLER ON INBOARD END OF SLAT. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 00FDEA00734Attach Fitting · shearedDURING ROUTINE INSP THE NR 2 LEAD EDGE SLAT INBOARD LWR ATTACH FITTING FOUND SHEARED. REMOVED, REPLACED AND FAB PER IAW BAC SRM 51-10-1, 51-30-2.SDR P2EA00332Skin · damagedSJO - DURING Q-CHECK, FOUND THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN WITH WEAR 10 INCHES BY 1 INCH. IDENTIFIED AS REPORTABLE ON 11-07-00. REPAIRED THE LEFT WING OUTBOARD FORE FLAP, OUTBOARD END, LEADING EDGE SKIN IAW BOEING FAX COO-SSDR TWAA0017616Structure · damagedDURING CHECK-C MAINT, THE LT WING NUMBER 5 L/E SLAT BOTTOM L/E WAS DAMAGED BY ANTI-ICE DUCTING WHILE CHECKING RIG. INSTALLED A 2 IN BY 4 IN FIBERGLASS HOT BOND REPAIR PER SRM 51-70-07.SDR SWAA002117Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT 2 FASTENER HOLES, APPROX 13 I/B OF ACTUATOR STOP. REPAIRED SLAT PER RA 1-A57-0691.SDR CALA0001611Skin · dentedINSPECTION FOUND THE LT NR 3 SLAT DENTED ON THE LEADING EDGE. THE SLAT WAS REPAIRED IAW SRM 57-06, FIGURE 1 AND ECRA 5720-01170.SDR USAA001786Skin · crackedCLT - FOUND NR 3 SLAT SKIN CRACKED .25 INCH, LOWER SKIN AFT FASTENER ROW 4 INCHES L/B ACTUATOR. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR SWAA002072Slat · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 SLAT LOWER SKIN CRACKED 6 AFT OF ANTI-ICE DUCT. REPAIRED SLAT PER T1-657-012.SDR DL72L002042Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT O/B ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.SDR DL72L002041Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT INBOARD ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.SDR SWAA002041Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 5 SLAT CRACKED AT ACTUATOR. REPAIRED SLAT PER RA 1-257-0555.SDR SWAA002030Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 4 SLAT I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR P5CA0000333Rod · damagedDAMAGE FOUND L/E SUPPORT ROD ASSY FOR RIB AT WING STA 878.55 FOUND CHAFED THRU. SUPPORT ROD ASSY REPLACED PER SRM 51-30-04.SDR P5CA0000331Fitting · damagedABNORMALITY FOUND ON RT WING I/B FOREFLAP O/B SEQ CARRIAGE ATTACHMENT FITTING BEARING FOUND MIGRATED. NEW FITTING P/N 65B39025-34 INSTALLED PER MM 27-51-02.SDR RRXA003286Skin · damagedDURING A MAINTENANCE VISIT FOUND L/E SCREWS PULLING INTO SKIN AND STICKING UP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.SDR RRXA003285Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT SLOT DOOR AT THE BOTTOM I/B L/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.SDR USAA001729Wedge · crackedCLT - FOUND SLAT TRAILING EDGE WEDGE CRACKED 12.5 INCHES, ENTIRE WIDTH OF THE WEDGE. REMOVED DAMAGED CORE PER EA 68081 AND SRM 51-40-10 AND 51-70-10. (M)SDR ABXA000470Fitting · crackedRIGHT WING LEADING EDGE FITTING CRACKED INBOARD OF NR 2 SLAT TRACK AT LOWER POCKET. REPAIRED FITTING IAW ABX REA D957-38812-MR.SDR DL72L001973Fitting · crackedROUTINE INSPECTIONS OF THE LT AND RT WING LEADING EDGE SLAT DOWNSTOP FITTINGS REVEALED A BROKEN BOLT IN A FITTING FOR THE NR 6 SLAT. THE CONDITION IS TYPICAL OF BAC S/B 727-57-171AND AD 94-07-08. THE DOWNSTOP FITTINGS OF THE NR 6 SLAT WERE MODIFIED PER THESDR DL72L002020Rib · crackedAT HMV THE NR 11 RIB FLANGE OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE, FABRICATED REPAIR PARTS PER MM 57-54-0, REPAIRED PER MM 57-54-0.SDR DL72L002019Rib · crackedAT HMV THE NR 13 RIB OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE FOR FABRICATED DOUBLER. REPAIRED PER MM 57-54-0.SDR DL72L002018Rib · crackedAT HMV NR 7 RIB OF SLAT FOUND TO BE CRACKED. REMOVED LWR AFT SPAR REPAIR DOUBLER IN AREA, FABRICATED REPAIR DOUBLER PER MM 57-54-0, ROUTED OUT DAMAGE, INSTALLED DOUBLER AND FILLER PER MM 57-54-0, REINSTALLED SPAR DOUBLER.SDR CALA0001499Skin · gougedRIGHT WING FLAP NUMBER 8 LEADING EDGE HAS CUT ON SURFACE. FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 57-01.SDR DLL14001892Skin · crackedFOUND DURING WALKAROUND, LT WING NR ONE L/E SLAT HAS A 3 INCH CRACK IN LWR FLANGE JUST I/B OF I/B SLAT TRACK. REPLACED SLAT.SDR TWAA0015408Skin · dentedDURING CHECK-C MAINT ON THE RT WING FOUND 2 DENTS TOGETHER 16 INCHES TO 18 INCHES OUTBOARD OF THE INBOARD END OF THE NR 2 L/E SLAT, .5 IN BY .75 IN BY 0.050, AND .75 BY .75 BY 0.020. ACCOMP HFEC OF AREA PER NDT 51-00-03 PART 6 AND NO DEFECT FOUND. REPAIRED PSDR TWAA0015407Structure · damagedDURING CHECK-C MAINT ON THE RT WING L/E OUTBOARD END OF NUMBER 1 L/E SLAT HAD A PREVIOUS DENT IN L/E WITH FILLER COMING OUT. ACCOMP HIGH FREQ EDDY CURRENT OF DENT PER 51-00-03, PART 6 OF NDT MANUAL AND NO CRACKS. MEASURED DENT 0.140 IN DEEP. REPAIRED PER SRSDR UPS00233860Rib · crackedINSPECTION TYPE:C SUSPECT CRACK NR 4 SLAT ACTUATOR O/B RIB PREVIOUS (AFT) RADIUS OF ANGLE. REPAIR CARRIED OUT IAW MM 27-81-32 SRM 51-40-02 & MM 27-81-32.SDR DL72S001870Rib · crackedA 1 INCH CRACK AT NR 3 SLAT I/B NOSE RIB AT SLAT ACTUATOR ROD END BOLT. REPAIR PER M/M 57-54-0 FIG 814.SDR UPS00233833Skin · crackedINSPECTION TYPE:C, NR 6 SLAT INNER SKIN CRACKED AROUND CTR FASTENER I/B OF ACTUATOR. REPAIRED INNER SKIN IAW UPS EO B727-5750-3082.SDR AWXA0000658Skin · crackedC-CHECK, NR 5 SLAT AT I/B AUX TRACK CUTOUT, OUTER SKIN HAS CRACKS MIGRATING FROM FASTENER HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737 SRM 57-43-01.SDR SWAA001821Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 1 SLAT T/E SKIN CRACKED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR CA001019010Rib · cracked(CAN) DURING A ROUTINE A CHECK IT WAS NOTICED THAT THE NR 8 SLAT ACTUATOR MOUNT WAS CRACKED AT THE ROD END ATTACH POINT. SLAT WAS REMOVED AND MOUNT BRACKETS AND RIB FOUND TO BE BROKEN. SLAT WAS REPLACED AND AIRCRAFT RELEASED. REPLACEMENT PER BOEING M.M. 27-81-SDR DL72W001842Fitting · looseDURING REPETITIVE INSPECTIONS, THE I/B SLAT TRACKS ON THE NR 3 AND NR 4 SLATS WERE FOUND TO HAVE LOOSE BOLTS IN THE DOWNSTOP FITTINGS. THE CONDITION IS TYPICAL OF BAC S/B 727-57-0171. BOTH SLAT TRACKS FOR THE NR 3 AND NR 4 SLATS WERE MODIFIED PER THE SSDR UPS00233798Skin · damagedINSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 171.5 ABOVE NR 3 LEADING EDGE FLAP DAMAGED. INSTALLED SKIN REPAIR FROM WS 171.5 TO 160.0, DOUBLER MATERIAL USED, 2024-T3, 0.080, 8 X 7 INCHES. ANGLE REPAIR INSTALLED MATERIAL USED 7075-T6, 20 TRACK PART NUMBERSDR DL72E001778Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 2 SLAT O/B TRACK O/B SIDE. TPA E-1 LETTER CHECK. REPLACED STIFFENER PER M/M 57-20-21 NR 14.SDR DHL200070809CFlange · crackedNR 9 L/E SLAT I/B TRACK O/B MOUNT AFT FLANGE IS CRACKED. ROUTED OUT CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-3. TREATED AND PRIMED PER SRM 51-10-3.SDR DHL2000708005Rib · crackedLEFT WING LEADING EDGE SLAT RIB AFT FLANGE IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-50-3. SIZE OF REPAIR 8 X 2 INCH.SDR TWAA0015005Skin · dentedDURING CHECK-C MAINT ON LT WING, FOUND 2 DENTS AT FWD EDGE OF WEDGE, TOP SIDE I/B ON NUMBER 6 L/E SLAT. APPLIED HOT BOND REPAIR TO NUMBER 6 L/E SLAT APPROX SIZE 3.5 BY 3.5 INCHES PER SRM 57-43-02 AND 51-70-10, PAGES 34 AND PAGES 12, 103, AND 201. SEALED PER SDR ABXA000459Doubler · crackedDOUBLER CRACKED AT LEADING EDGE LOWER SIDE BETWEEN NR 3 AND NR 4 SLAT TRACKS. REPLACED DOUBLER IAW DC9 SRM 51-30-2.SDR 0003572709Flange · crackedDURING L CHECK, FOUND CRACK ON UPPER FLANGE OF BULLNOSE 2 INCHES INBOARD OF CENTER HINGE ON NUMBER 2 KRUEGER FLAP. REPAIRED PER EA 27-178740.SDR UPS00233739Structure · corrodedINSPECTION TYPE:N/A, NR 3 L/E FLAP HAS HOLE DUE TO CORROSION. *S/D* REMOVED AND REPLACED NR 3 L/E FLAP ASSY PER MM 27-81-01. OPS NORMAL. (P/N 65-16225 -1) (S/N BN592) ON, (S/N 373) OFFSDR AALA20001538Skin · gougedTUL - FOUND TWO DEEP GOUGES IN FIXED L/E AFT OF NR 2 SLAT INBOARD OF NR 7 SLAT TRACK. REPAIRED FORWARD DAMAGED AREA PER SRM 57-06B. (M)SDR DHL200070808CRib · crackedRT WING NR 4 6 L/E SLAT O/B TRACK I/B MOUNT RIB AFT FLANGE IS CRACKED AT HORIZ NUT PLATE STRAP UPPER ANGLE. REMOVED FASTENERS AT NR 6 SLAT O/B TRACK I/B RIB PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. INSP CRACK AT STOP DRILL PER NDT MAN 51-00-00.
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