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 USAA051091Skin · chafedRT WING I/B FLAP O/B EDGE OF L/E CHAFED. CUT OUT DAMAGE AND REPAIRED PER SRM 57-53-01 FIG 201, 51-40-03, DEFECT SIZE: 9.9" X 6.5".SDR QXEA200501313Skin · chafedYYC - RIGHT WING SLAT PANEL NR 622CB CHAFED. BLENDED OUT DAMAGE IAW EA R-57-108 AND REO 670-57-42-069. NO CRACKS FOUND. RESTORED FINISH.SDR TAMF20050006OSkin · crackedDURING TAKE OFF, THE CREW FELT A SUSPECTED BIRD STRIKE IN THE RIGHT PART OF THE AIRPLANE. DURING MAINTENANCE INSPECTION WAS FOUND A DENT AND CRACK ON THE NOSE SKIN AT SLAT NR 7. TIME LIMITED REPAIR WAS PERFORMED IAW EWO AND MFG APPROVAL NR 1-124395785-2 IN ORSDR DHL2005748752Channel · looseNR 1 SLAT HAS PLAY AT ACTUATOR TO SLAT ATTACH POINT. REMOVED CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5070637 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CHANNEL SDR IXXA05RNG075SDoubler · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON DOUBLER AT LEADING EDGE OB SLOT UPPER DOOR LT. CORRODED DOUBLER WAS REMOVED AND NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 12 AND EWO ATI-57-050.SDR DL76G050548Bolt · brokenLE SLAT ASYM EICAS MSG ON APPROACH. FOUND NR 5 SLAT IB S286 TARGET BOLT BROKEN. REPLACED SAME.SDR USAA051085Skin · crackedLOWER SKIN, OUTBOARD END CRACKED. INSTALLED DOUBLER, IAW BOEING 737-400, SRM 57-43-01 DEFECT SIZE: 1.5 INCH.SDR UPS05245518Slat Track · corrodedON REMOVAL OF NR 6 SLAT I/B TRACK SKIN SUPPORT BRACKET, CORROSION ON TEE TRACK FOUND BENEATH BRACKET. NR 6 SLAT TRACK REPLACED IAW MM 27-81-11.SDR AWXA200501175Skin · crackedMCN - DURING C18 CHECK DISCOVERED 5 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN AT THE INBOARD AUXILIARY TRACK, SS 175.00L. MAINTENANCE CUT OUT AND REMOVED DAMAGE PART OF SKIN IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW SDR AWXA200501167Skin · crackedMCN - DURING C15 CHECK DISCOVERED 4 CRACKS, .5 INCHES IN LENGTH, ON THE NR 1 SLAT SKIN BELOW THE OUTBOARD MAIN TRACK. MAINTENANCE TRIMMED OUT DAMAGED SKIN ON THE NR 1 SLAT IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PATE IAW BOEISDR AWXA200501166Skin · crackedMCN - DURING C15 CHECK, DISCOVERED 4 CRACKS, .5 INCHES IN LENGTH, AT BOTTOM OF THE NR 2 SLAT SKIN AT OUTBOARD MAIN TRACK. MAINTENANCE TRIMMED OUT DAMAGED SKIN ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PATE IAW SDR C8GA20050019Bracket · crackedFLT 718 FROM STL TO ELP, DURING CLIMB-OUT, THE NR 2 SLAT WILL NOT RETRACT. AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. INSPECTED SLAT ACTUATOR AND LUBED SLAT TRACKS. NO OTHER DEFECTS NOTED. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SSDR MWEA050104Skin · corrodedLEADING EDGE AT STATION 375 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR C2XA05SH111Skin · dentedSHV - DURING C-CHECK, RT LEADING EDGE NR 3 HAS DENT BETWEEN 2ND AND 3RD VORTILLON. MAINTENANCE REPAIRED RT LEADING EDGE NR 3 BETWEEN 2ND AND 3RD VOTILLON IAW EMB 145 SRM 57-40-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR AWXA200501127Skin · crackedMCN - DURING C18 CHECK, DISCOVERED SEVERAL CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN INBOARD OF THE TELESCOPING ANTI-ICE TUBE FROM SS 210L TO SS 230L. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 2 SLAT IAW BOEING 737-300 SRM 57-43-02-2R. FABRICATED REPAIR FILLERSDR GTIA050248Skin · dentedLT WING NR 1 SLAT DENTED STATION XTS 128.000, DENT DIAMETER = 2.0 DEPTH = .048. LEFT WING, NR 1 SLAT DENT FOUND OUT OF LIMIT. REPAIRED DENT AREA. (M)SDR UPS05245466Rib · crackedINSPECTION TYPE:C-CRACK ON NR 8 SLAT O/B RIB AT I/B TRACK ATTACHMENT AREA. SLAT STOP DRILLED IAW AAAE EO 2005-081-004 REV 1 (UPS ENG FILE NR 727- 57-20133).SDR 05FDEA02667Doubler · damagedRIGHT L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. RIGHT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-00-01 FIG 24 VOL I. THIS REPAIR CLSDR 05FDEA02668Skin · chafedLHW L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. LT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIG 24 VOL I. THIS REPAIR CLASSSDR AWXA200501046Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 3 CRACKS, .375 INCHES IN LENGTH, FROM SS 167.5L TO SS 172L, ON THE BOTTOM OF THE NR 2 SLAT SKIN, INBOARD OF THE TELESCOPING ANTI ICE TUBE. MAINTENANCE REMOVED THE DAMAGED SKIN ON THE NR 2 SLAT IAW BOEING 737-30SDR AWXA200501044Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 8 CRACKS ON BOTTOM OF THE NR 4 SLAT SKIN, BELOW ACTUATOR AT SS 61.01. MAINTENANCE REMOVED DAMAGED SKIN ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300SDR AWXA200501037Skin · crackedDURING C16 CHECK DISCOVERED 1 CRACK, .375 INCHES IN LENGTH, LOCATED ON THE BOTTOM OF THE NR 5 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED CRACKS FROM NR 5 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE ISDR AWXA200501036Structure · crackedDURING C16 CHECK DISCOVERED, 2 CRACKS, .375 INCHES IN LENGTH, LOCATED ON THE BOTTOM OF THE NR 1 SLAT SKIN BELOW OUTBOARD MAIN TRACK. MAINTENANCE REMOVED CRACKS FROM NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEISDR USAA051052Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, OUTBOARD LOWER SKIN OF NR 6 SLAT. INSTALLED DOUBLER IAW SRM 57-43-01. (M)SDR 05FDEA02606Skin · crackedRT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM.SDR DHL2005806505Splice · crackedLT INNER WING OB EXTENDED L/E SLOT SPLICE CRACKED 10 IN STA XFS 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-3-3 FIG. 3 SHEET 1. REMOVED CRACKED SPLICE IAW SRM 57-1-0 PG. 1, SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW SPLICE IAW SRSDR 2005UALA00855Skin · delaminatedNR 4 SLAT HAD LOCAL DELAMINATION AT THE OUTBOARD END LOWER SURFACE OF THE TRAILING EDGE WEDGE. *S/D* THE LOCAL DELAMINATION FOUND IN THE NR 4 SLAT IS SYSTEMIC ON THE TRAILING EDGE WEDGES ON THE 777 SLATS. BOEING IS CURRENTLY WORKING ON A MODIFIED DESIGN TO SDR DHL2005748532Support Angle · crackedNR 2 K FLAP LWR O/B ACTUATOR MOUNTING SUPPORT ANGLE CRACKED IN L/WING L/E. REMOVED O/B ACTUATOR MOUNTING SUPPORT ANGLE IAW B727 SRM 51-30-2 FAB NEW SUPPORT ANGLE FROM 7075 T6 .063 PO 9001417 8" X8" IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED NEW PARTS IAWSDR 05FDEA02498Rib · crackedRIGHT WING, NR 5 SLAT, LEADING EDGE RIB CRACKED OUTBOARD OF OUTBOARD MAIN TRACK. REMOVED AND REPLACED RIB IAW SRM 51-30-5, 51-30-2.SDR DHL2005748516Skin · dented8 SLAT LE LWR SKIN SHOW DENT WS 716 (MARKED). CUT OUT DAMAGED AREA OF SKIN 2.5" BY 1.7" AND FAB DOUBLER 3.3" BY 5.7" .040 2024T3 PO 9051237 IAW B727 IAW B727 SRM 57-50-3. FAB FILLER 2.5 BY 1.6 .040 2024T3 PO 9051237 IAW B727 SRM 57-50-3. TREATED AND PRIMED SDR DHL2005748515Skin · damagedNR 8 SLAT LE LWR SKIN CREASE AND DENTED TO O/B END WS760. CUT OUT DAMAGED AREA OF SKIN 6" BY 4" AND FAB FILLER 6.0" BY 4.0 .050 2024 T3 PO 9002435 IAW B727 SRM 57-50-3 FIG 1 FAB SPLICE STRAPS 5 BY 2.2 2EACH 3.3 BY 2.2 2EACH 2.4 BY 3.5 1EACH .080 2024 T3 PO 50SDR DHL2005806502Frame · crackedRT WING CTR L/E FORMER UPPER PART CRACKED 0.250 INCH, STA XFS 416.500. PERFORMED STOP HOLE AND FABRICATED 2 THIN FORMED ANGLE DOUBLERS (AL7075T6 0.032 INCH) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND 2 THIN FORMED ANGLE DOUBLERS IAW SRM 51-1SDR DHL2005806503Doubler · damagedINTERIM REPAIR ON RT OB FLAP UPPER PLATING (STA XF 208.000-213.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-7-1 FIG. 4, TR NR 57-94. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG. 1, SRM 51-3-0 PG. 1. FABRICATED NEW PSDR 05FDEA02458Skin · unknownLEFT NR 3 SLAT L/E LOWER SKIN INBOARD OF INBOARD TRACK HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3.SDR 05FDEA02457Skin · unknownRIGHT NR 6 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.SDR 05FDEA02456Skin · unknownRIGHT NR 8 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3.SDR 05FDEA02455Skin · unknownLEFT NR 3 SLAT LOWER SURFACE HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.SDR 05FDEA02454Skin · unknownLEFT SLAT NR 2 HAS PREVIOUS REPAIR ON LWR SURFACE THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.SDR ABXA050184Slat · missingDURING INSPECTION OF AIRCRAFT AT ILN, FOUND RIGHT WING NR 12 LEADING EDGE SLAT OUTER SKIN MISSING. HONEYCOMB EXPOSED AT UPPER INBOARD SIDE, APPROXIMATELY 9.5 WIDE AND 11.0 LENGTH. REMOVED AND REPLACED NR 12 LEADING EDGE SLAT IAW B767 MM 27-81-02-4.SDR 05FDEA02388Rib · crackedLT WING NR 3 SLAT INTERNAL STRUCTURE AT O/B ACTUATOR MOUNTING SUPPORT RIB CRACKED. REMOVED AND REPLACED SUPPORT RIB IAW SRM 51-40-3 FIG 1.SDR 05FDEA02374Skin · chafedRIGHT WING, FIXED LEADING EDGE UPPER SURFACE FOUND CHAFED MARK AT OUTBOARD OF NR 19 SLAT TRACK. CHAFED MARKED REMOVED FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE UPPER SURFACE AREA AT OUSDR 05FDEA02363Skin · damagedLEFT WING SLAT 1 XORS 130 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. ACCOMPLISH EA 8-5710-84123.SDR 05FDEA02358Rib · crackedSLAT 2 R O/B SIDE ON RIB FOUND 1EA CRACK 2" LONG. REPAIR PER SRM 57-00-01 VOL 1 FIG 10 SHT 2 AND SRM 51-35-01 PAR 1-5 VOL 2.SDR 05FDEA02352Skin · damagedRIGHT WING SLAT 6 CENTRAL TRACK EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 31 VOL 1.SDR 05FDEA02349Angle · damagedLT WING SLAT 2 XDLE 309 EXISTING REPAIR ANGLE ON CLOSURE ANGLE. REPLACE REPAIR PER SRM 57-00-01 FIG 10 VOL 1.SDR 05FDEA02343Skin · damagedRIGHT WING SLAT NR 1 XCW 118 EXISTING 1 EA REPAIR DOUBLER ON UPPER SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 84 SHEET 2 VOL 1.SDR 05FDEA02333Skin · damagedRIGHT WING, SLAT NR 1, EXT TRACK FITTING, ONE EXT REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-01 FIG 4 SHT 2 VOL 1, SRM 51-35-02 VOL 2 PG 3/9.SDR PIDA20050095Rib · crackedNR 3 SLAT HAS A CRACK IN THE RIB O/B OF SLAT ACTUATOR. REPLACED SLAT RIB PER SRM 51-10-1 AND SRM 51-30-1.SDR USAA050971Skin · crackedCLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K)SDR SWAA052311Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SWA EA.
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