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 AALA20120327015Attach Bracket · crackedTHE SECOND FROM OUTBOARD SLAT TRACK ATTACH BRACKET FOR THE LEFT NUMBER 5 LEADING EDGE SLAT IS CRACKED. REPLACED SECOND FROM OUTBOARD POSITION ATTACH BRACKET FOR THE NUMBER 5 LEADING EDGE SLAT PER ESO 80117.SDR SWAA2012040902934Skin · delaminatedRT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE OF LEADING EDGE AT INBOARD EDGE. REPAIRED SLAT IAW SRM.SDR SWAA2012040902869Skin · delaminatedRT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE AT OUTBOARD EDGE. REPAIRED NR 5 SLAT IAW SRM.SDR SWAA2012050103623Skin · delaminatedLT WING NR 3 SLAT DELAMINATED ON OUTBOARD END UPPER SURFACE. REPAIRED NR3 SLAT IAW SRM.SDR SWAA2012040202749Slat · crackedRT WING NR 7 SLAT CRACKED AT HYDRAULIC ACTUATOR ATTACH POINT. REPAIRED SLAT IAW SRM.SDR DALA1218000180Skin · delaminatedLT WING NR 4 L/E SLAT EXTERIOR SKIN HAS DELAMINATION 17" AND 7" FROM O/B UPPER END. REPAIRED AS PER B767-300 SRM 57-43-02, REPAIR 1 AND B767-300 SRM 51-70-10 REPAIR 2, FIGURE 203.SDR SWAA2012032702623Skin · delaminatedLT WING NR 3 SLAT TRAILING EDGE INNER SURFACE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR SWAA2012032702619Slat · delaminatedLT WING NR 3 SLAT UPPER OUTBD CORNER IS DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR AALA20120323003Skin · crackedNUMBER 2 SLAT JUST FORWARD OF INBOARD DRIVE TRACK, SKIN HAS TWO CRACKS AT FASTENERS. INSTALLED REPAIR DOUBLER ON NUMBER 4 COVE SKIN ON NUMBER 2 LEFT SLAT PER AARD 57-43-00-4.SDR FDEA201203221052Wedge · delaminatedSLAT NR 5 T/E WEDGE LOWER SURFACE IS DELAMINATED AT INBD SIDE. REPAIRED IAW SRM 51-71-10 -2R1 AND 51-20-01. MAJOR REPAIR.SDR AALA20120321021Slat · debondedDISBOND ON INBOARD AFT CORNER NUMBER 5 SLAT. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10.SDR AALA20120321020Skin · debondedRIGHT WING LEADING EDGE SLAT NUMBER 9 INBOARD END TRAILING EDGE WEDGE ON LOWER SURFACE SHOWS DISBOND INDICATION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.SDR AALA20120321019Slat · delaminatedNUMBER 8 SLAT HAS DELAMINATION OUTBOARD AFT CORNER. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.SDR AALA20120321018Skin · debondedSMALL DISBOND ON NUMBER 2 SLAT OUTBOARD UPPER CORNER UPPER AND LOWER SURFACES. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.SDR DALA1217271606Skin · chafedLT WING NR 4 SLAT INTERIOR SKIN HAS DEEP CHAFING 34 INCHES FROM I/B END AND IS REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202.SDR AALA20120321001Skin · dentedLEFT NUMBER 5 SLAT HAS SHARP DENT IN LEADING EDGE UPPER SKIN. REWORKED DENTED AREA PER ESO 80117 TO WITHIN LIMITS. DYE CHECK AFTER REWORK SHOWS NO CRACKS.SDR SWAA2012032902703Skin · crackedLT WING NR 1 SLAT CRACKED ON LOWER SURFACE LOCATED AT STA 531. REPAIRED SKIN IAW SRM.SDR IPXA12B72501Panel · delaminatedINSPECTION TYPE:C, RT WING NR 15 KRUEGER FLAP DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 60.SDR VNAA2012032300014Skin · dentedCREW REPORTED BIRD STRIKE ON LEADING EDGE OF RIGHT WING DURING APPROACH. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND FOUND DENT IN RIGHT NUMBER ONE SLAT WITHIN LIMIT PER SRM (STRUCTURAL REPAIR MANUAL). NO FURTHSDR UALA2012031901752Slat · damagedDAMAGE FOUND ON LT NR 2 SLAT. REPLACED NR 2 SLAT.SDR UALA2012031901777Slat · dentedLEFT SLAT NR 2 HAS A DENT 18" FROM INBD EDGE 3" X 4 X .25" DEEP. SAMC TEXT: EDGE OF DENT IS 1.25" FROM NEAREST RIVET ROW AND IS IN AREA 3. REQUIRES TEMP FILLER REPAIR PER SRM AND APPLICATION OF SPEED TAPE PER SRM. ACP INTERIM REPAIR SRM. REQUIRES DAILY RESDR AALA20120316010Wedge · debondedNUMBER 5 LEADING EDGE SLAT AT INBOARD END ON TRAILING EDGE WEDGE HAS DELAMINATION AT INBOARD EDGE. ACCOMPLISHED BODED REPAIR PER SRM 51-70-10.SDR DALA1216000180Wedge · puncturedNR 6 SLAT INNER SURFACE OF T/E WEDGE IS PUNCTURED AT LES 300 AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 202.SDR ASAA12411232Skin · delaminatedRT WING NR 5 SLAT OUTBD T/E CORNER UPPER AND LOWER SURFACES DELAMINATED. REPAIRED DELAMINATION DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PG 201.SDR USAA2012040900025Wedge · delaminatedC4 CHECK - DELAMINATION ON NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00, 6 INCHES FROM INBOARD END AT LOWER SKIN. REPAIRED NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00 IAW B757 SRM 51-70-10.SDR ASAA12411264Skin · delaminatedRT WING 4 SLAT I/B TRAILING EDGE WEDGE UPPER SURFACE DELAMINATED. REPAIRED DAMAGED AREA IAW B737 400 SRM 51 70 10 PARA 20.SDR UALA2012030801526Structure · crackedKRUEGER FLAP 16 HAS CRACK APPROX 6 IN AT UPPER OTBD CORNER. REMOVED KRUEGER FLAP PER MM. ACCOMPLISHED PRE-INSTALLATION INSPECTION OF NR 16 KRUEGER FLAP ATTACH POINTS ON ACFT. INSTALLED FLAP AND TORQUED BOLTS UP TO STEP 3.E.(9) PG 406 MM. COMPLETED INSTALSDR SWAA2012031202097Skin · corrodedLT WING NR 2 SLAT O/B TRAILING EDGE LOWER SURFACE CORRODED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR AALA20120308009Skin · corrodedLEFT WING OUTBOARD SLAT NUMBER 3 UPPER SKIN CORRODED AROUND FASTENERS. INSTALLED DOUBLER REPAIR PER SRM 57-43-00-1.SDR SWAA2012040902913Skin · crackedRT WING NR 6 SLAT LOWER LEADING EDGE CRACKED AT O/B AUX TRACK. REPAIRED SKIN PER SRM.SDR SWAA2012111509378Skin · crackedNR 2 SLAT HAS 4EA SKIN CRACKS ON LOWER SKIN AT AFT ROW OF FASTENERS (BELOW O/B AUX TRACK). VERIFIED WITH HFEC. REPAIRED LEFT WING SLAT NR 2 TEE CHORD BETWEEN SS175 AND SS220 IAW EA N 1-357-7551 REV 0 AND EO N AEM-HC57-230/12.R0SDR IPXA2672252Wedge · chafedINSPECTION TYPE: 9C, LEFT WING NR 5 SLAT WEDGE LOWER SURFACE FOUND CHAFING. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8, REV 52.SDR DALA1213730180Slat · damagedLT WING 6 SLAT INSIDE SURFACE OF T/E WEDGE AT STA 300. REPAIRED USING METAL HOT BOND IAW B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 202.SDR SWAA2013042515203Skin · crackedLEFT WING NR 1 SLAT CRACKED ON LOWER SKIN I/B END AT AFT ROW OF FASTENERS. REPAIRED NR 1 SLAT PER EA AND SRM.SDR SWAA2013032814237Skin · crackedRIGHT WING NR 5 SLAT CRACKED ON LOWER SKIN AT AFT ROW OF FASTENERS. REMOVED AND REPLACED NR 5 SLAT IAW AMM.SDR SWAA2013032814236Skin · crackedLEFT WING NR 2 SLAT CRACKED ON LOWER SKIN AT AFT ROW OF FASTENERS. REMOVED AND REPLACED NR 2 SLAT IAW AMM.SDR DALA1213031503Wedge · delaminatedLEFT WING NR 5 SLAT EXT WEDGE UPPER O/B CORNER DELAMED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202.SDR DALA1213021503Wedge · dentedLEFT WING NR 5 SLAT EXT UPPER WEDGE SURFACE DENTED. REPAIR DATA REFERENCE B767-300 SRM 57-43-02 REPAIR 1 AND THE REPAIR INSTRUCTIONS REFER B767-300 SRM 51-70-10 REPAIR 2 FIG 203.SDR MASA2012030534527Slat Track · chafedLT WING, 5TH FROM INBD SLAT TRACK HAS WEAR/CHAFE ON LOWER SURFACE. PERFORMED A MAJOR REPAIR BY INCORPORATING BOMBARDIER REO 690-57-42-171 REV.SDR IPXA2672365Skin · damagedINSPECTION TYPE:9C, LEFT WING NR 5 SLAT T/E WEDGE SKIN REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 52.SDR AALA20120307017Skin · corrodedNUMBER 10 SLAT LEADING EDGE SKIN INBOARD CORRODED. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R AND AARD 57-43-00-1.SDR FDEA201203020733Skin · crackedRT WING NR 9 SLAT COVE PANEL OTBD OF INBD SLAT DRIVE TRACKED CRACKED. MAJOR REPAIR. R & R COVE PANEL IAW-SRM-51-40-02, RECEIVED PART ON STAM TRAV T12/ 920600, PN FX114N4076-20, BATCH 0002068786, CAT "A" MAJOR REPAIR. "MAJOR REPAIR".SDR USAA2012032000004Skin · debondedC3 CHECK - AREA OF DISBOND ON NR 5 SLAT UPPER TRAILING EDGE SURFACE APPROX. 2.5 INCHES FROM INBOARD END. REPAIRED NR 5 SLAT UPPER TRAILING EDGE SURFACE IAW B757 SRM 51-70-10.SDR SWAA2012031902296Wedge · delaminatedRT WING NR 5 SLAT TRAILING EDGE WEDGE IS DELAMINATED AT O/B CORNER. REPAIRED WEDGE IAW SRM.SDR DALA1211445648Skin · dentedDURING MAINTENANCE CHECK FOUND NR 6 SLAT INNER SKIN DENT AT O/B AREA POSITION. NDT TEST WAS CARRIED OUT PER BOEING NTM PT2, 51-00-01 NO WATER FOUND. HFEC INSPECTION FOUND NO CRACK. MAINTENANCE PERFORMED METAL HOT BOND REPAIR PER SRM 51-7-10 REPAIR 4 AND SRMSDR DALA1211415648Skin · crackedDURING CHECK MAINTENANCE FOUND NR 3 SLAT LOWER SURFACE GOUGED MARK. NDT INSPECTION FOUND AREA CRACKED APROX 1 & 1/4 IN LENGTH AS MARKED. HFEC INSPECTION C/OUT AS PER BOEING NTM PT 6.51-00. NO CRACK FOUND. CARRIED OUT HOT METAL BOND REPAIR PER SRM 51-70-10 SDR SWAA2012031202112Skin · delaminatedLT WING NR 2 SLAT SKIN DELAMINATED ON I/B END. REPAIRED SKIN IAW SRM.SDR UALA2012022901244Slat · dentedLEFT IB L/E SLAT (NR 5) HAS 3 EA DENTS. DENT NR 1 IS 6" FROM IB EDGE AND 13" DOWN FROM T-E WEDGE DAMAGE IS 3"X 2"X .020" A-Y IS 100. DENT NR 2 IS 5" FROM IB EDGE AND 12" UP FROM CLOSURE PANEL, DAMAGE IS 2"X 7"X .030" A-Y IS 67. DENT NR 3 IS 2.25" FROM IB EDGSDR DALA1211939202Slat · gougedDURING INSTALLATION OF #0 RT SLAT NR 2 TRACK FOUND I/B FWD RIB FWD/LWR EDGE GOUGED. BLENDED GOUGE AT #0 RT SLAT NR 2 TRACK INBD RIB FWD LOWER EDGE AS PER MD-90 SRM 57-00-01 PG 3. NO CRACKS NOTED AS PER NDT S.P.M. 06-10-01-01-001 MAT LOSS .040 LENGTH 2.65 AT SDR ASAA12411200Skin · delaminatedRIGHT NR 5 L/E SLAT INBD UPPER SURFACE DELAMINATED. REPAIRED RT NR 5 SLAT INBD UPPER SURFACE IAW B737 400 SRM 51 70 10.
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