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 05FDEA00228Slat Track · wornM-TYPE-MOD 716-27-80-0264, NR 8 SLAT TRACK HAS SIDE ROLLER WEAR SPOTS. BLENDED AND POLISHED TRACK ROLLER WEAR SPOTS FOUND ONE AREA OUT OF ALLOWABLE DAMAGE LIMITS IAW A-300 SRM 57-40-00 3.A.(3)(D). THE TRACK MAYBE RETURNED TO SERVICE PROVIDED THE AREA IS INSSDR SWAA050274Skin · debondedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DISBONDED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR SWAA050272Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR AWXA200500226Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMAGED AREA OF UPPER NR 2 SLAT SKIN FROM SS 249.77 TO SS 254.27; FABRICATED A CORE FILLER AND EXTERNALSDR 05FDEA00197Skin · damagedCOMPLY WITH EA 8-5710-55426 WINGS - BASIC, LT, LEADING EDGE NR 7 SLAT SKIN REPAIR AT XOS=947.65. COMPLIED WITH EA 8-5710-55426.SDR AWXA200500243Skin · crackedDURING C-16 CHECK 4 EACH .25 INCH CRACKS WERE FOUND AT FASTENER HOLES ON LOWER NR 2 SLAT SKIN. MAINTENANCE FASTENERS AND PREVIOUS REPAIR IN LOWER NR 2 SLAT SKIN FROM SLAT STA 158.5 T0 SLAT STA 165; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTSSDR 0500145523Skin · crackedDURING H-CHECK FOUND CRACKED COVE SKIN PANELS AT NR 9 LEADING EDGE SLAT OUTBOARD DRIVE TRACK. REPAIRED PER EA 55-202250.SDR SWAA050185Attach Fitting · crackedDURING SCHEDULED D-CHECK, FOUND LT WING L/E NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPAIRED SLAT FITTING PER SRM.SDR ASAA0540046Skin · crackedOKC - NR3 SLAT LOWER SKIN CRACKED AT FASTENER OB END .6 INCHES LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)SDR ASAA0540045Skin · crackedOKC - NR 2 SLAT LOWER SKIN CRACKED 2 PLACES IB END AT FASTENER (.73 INCH LONG) AND CENTER (1.6 INCHES LONG). REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)SDR AWXA200500225Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LOWER SURFACE SKIN OF THE NR 3 SLAT WAS FOUND DELAMINATED AT SLAT STA 14.5. MAINTENANCE REMOVED PREVIOUS REPAIR AND DAMAGED AREA OF LOWER NR 3 SLAT SKIN; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PSDR 05FDEA00138Hinge · corrodedLEFT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIASDR ASAA0540037Wedge · delaminatedOKC - RT WING NR 5 LE SLAT TRAILING EDGE WEDGE HAS SMALL AREA OF DELAMINATION AND DETERIORATED EDGE POTTING ON OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER AND REPORTED IAW SRM. (K)SDR UPS05243707Skin · crackedINSPECTION TYPE: C, LE SLAT ACCESS PANEL (NR 6 SLAT) HAS 1/2 INCH CRACK ON SKIN. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-40-02 AND 51-30-02.SDR 05FDEA00084Skin · warpedLEFT WING, NR 5 SLAT LEADING EDGE SURFACE IS EXCESSIVELY WARPED THE ENTIRE WIDTH DUE TO TOO MUCH HEAT. LT WING NR 5 SLAT REMOVED AND REPLACED.SDR USAA050064Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 2.5 INCH AREA, NR 3 SLAT INBOARD TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, DOUBLERS PER SRM 51-70-10. (M)SDR UPS05243698Rib · crackedINSPECTION TYPE: C, NR 8 LE SLAT STRUCTURE HAS CRACKED RIB JUST O/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW SRM 57-50-03.SDR UPS05243697Rib · crackedINSPECTION TYPE:C NR 5 LE SLAT STRUCTURE HAS THREE RIBS CRACKED BETWEEN O/B TRACK AND O/B EDGE OF SLAT. REPAIRED CRACKED RIBS 3 PLACES AT NR 5 LE SLAT IAW SRM 57-50-03 FIG 9.SDR UPS05243687Hook · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 2 SLAT O/B HOOK UPPER FASTENER. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 10.SDR USAA050006Skin · crackedCLT - FOUND SLAT SKIN CRACKED 1 INCH, LOWER TRAILING EDGE OF SKIN, 6 INCHES OUTBOARD OF ACTUATOR ON THE NR 4 LE SLAT. INSTALLED DOUBLER. (M)SDR UPS05243686Bracket · crackedINSPECTION TYPE:C, NR 1 KRUEGER FLAP TRUNNION BRACKET IS CRACKED ON O/B SIDE. BRACKET REPLACED IAW DRG 65-16275.SDR USAA050063Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M)SDR UPS05243710Casting · corrodedINSPECTION TYPE:C, NR 3 KRUEGER FLAP INBOARD HINGE, FIXED LEADING EDGE CASTING HAS EVIDENCE OF INTERGRANULAR CORROSION. REPLACED AND INSTALLED NEW CASTING IAW DRG 64-8343.SDR ASMF200501004Skin · damagedDURING TRANSIT CHECK WERE DETECTED FUEL PANEL AND SLAT NR 2 DAMAGED. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS, THEREFORE AIRCRAFT WAS SENT TO THE HANGAR. SLAT NR 2 AND FUEL PANEL WERE REPLACED IAW MM 27-80-01 AND 57-30-03, RESPECTIVELSDR AWXA200500028Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER SURFACE AT INBOARD END BETWEEN SS 131.50 AND SS 132.50. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT UPPER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPSDR AWXA200500154Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK, FOUND THE A PREVIOUS REPAIR ON UPPER INBOARD END OF NR 4 SLAT WEDGE DELAMINATED BETWEEN SLAT STA 12.25 AND 16.25. MAINTENANCE REMOVED DAMAGED SKIN ON UPPER INBOARD END OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND REPAIR SDR USAA050198Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 1.5 INCH AREA, NR 3 SLAT TOP SURFACE OUTBOARD T/E. BONDED IN NEW CORE, BOND ON TOP DOUBLER PR SRM 51-70-10. (M)SDR AWXA200500139Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK, THE LOWER SURFACE OF NR 1 SLAT WEDGE WAS FOUND DELAMINATED FROM SLAT STA 358 TO 369. MAINTENANCE REMOVED DAMAGE FROM LOWER SURFACE OF NR 1 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300SDR SWAA050025Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR 05FDEA00019Rib · crackedSECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1.SDR LCQ18Skin · chafedNR 2 L/E SLAT UPPER T/E LOWER SURFACE CHAFING NEAR ACTUATOR AND O/B ENDSDR 05FDEA00009Slat Track · crackedLEFT HAND WING, SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01 AND SRM 51-35-01. NR 16 SLAT TRACK ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-80-00-2. OUTBOARD SLAT OPERATIONAL TEST CARRIED OUT PER AMM 27-80-00-5.SDR 05FDEA00006Skin · damagedLT WING, NR 2 SLAT EXTERIOR, FOUND 2EA DOUBLER REPAIR AND 1EA CUTOUT REPAIR. REMOVED AND REPLACED AS PER AMM 27-80-20 AND FUNCTIONAL CHECK CARRIED OUT AS PER AMM 27-80-00, FOUND SATISFACTORY.SDR USAA050206Skin · crackedPIT - FOUND SLAT CRACKED .5 INCH, FORWARD OF INBOARD AUX TRACK LOWER SURFACE AFT FASTENER. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR USAA050176Skin · chafedPIT - FOUND LOWER SKIN SURFACE WITH CHAFE DAMAGE, 1.5 INCH BY 2.5 INCH, NR 2 SLAT INBOARD CORNER AND OUTBOARD CORNER LOWER SURFACE. (M)SDR USAA050170Skin · bentPIT - FOUND SLAT EXT SKIN BENT AREA 3.5 INCH BY 1.5 INCH AREA, NR 1 SLAT UPPER T/E SURFACE INBOARD END. REMOVED DAMAGED AREA, INSTALLED FILLER AND INTERNAL DOUBLER PER SRM 51-70-10. (M)SDR USAA050168Skin · delaminatedPIT - FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCHES BY 2 INCHES AREA, NR 3 SLAT INBOARD T/E. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL, BONDED IN NEW CORE, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)SDR USAA050053Skin · crackedPIT - FOUND NR 1 SLAT WITH .125 INCH CRACKS ON 6 RIVET HOLES, CENTER OF SLAT BY ACTUATOR MOUNT LOWER SKIN. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR USAA050068Panel · delaminatedPIT - FOUND PANEL DELAMINATED, INBOARD AND OUTBOARD ENDS OF NR 5 SLAT PANEL. INSTALLED DOUBLER PER SRM 51-70-10. (M)SDR USAA050051Skin · crackedPIT - FOUND NR 3 SLAT CRACKED .125 INCH, LOWER SURFACE AT MID SPAN RIVET HOLE. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR USAA050069Skin · delaminatedPIT - FOUND SLAT DELAMINATED 4 INCHES BY 6 INCHES, NR 3 SLAT. REMOVED TOP SKIN CORE AND DAMAGE, INSTALLED FILLER, DOUBLER PER SRM 51-70-09. (M)SDR USAA050160Skin · crackedPIT - Q6 - NR 6 SLAT, .5 INCH CRACK; LOWER SKIN AFT ROW RIVET 4 INCHES FROM OB END; INSTALLED DOUBLER IAW SRM. (K)SDR USAA050156Skin · crackedPIT - Q6 - NR 1 SLAT, 1 INCH CRACK; LOWER SKIN AFT ROW RIVETS AT NR 2 AUX TRACK. INSTALLED DOUBLER IAW SRM. (K)SDR USAA050112Skin · delaminatedPIT - Q6 - SKIN, 6.5 INCH X 4.5 INCH AREA DELAMINATION; NR 5 SLAT OB END; REMOVED TOP SKIN AND CORE AND REPLACED IAW SRM. (K)SDR USAA050111Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 5 SLAT IB END; REMOVED TOP SKIN, CORE, REPLACED CORE AND TOP SKIN IAW SRM 57-70-10. (K)SDR USAA050110Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 2 SLAT, OB END; REMOVED TOP SKIN, CORE, REPLACED CORE, TOP SKIN IAW SRM 51-70-10. (K)SDR USAA050109Skin · delaminatedPIT - Q6 - SKIN - CORE, 4 INCH X 4 INCH DELAMINATION, NR 2 SLAT IB END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER, CORE, TOP EXT DOUBLER IAW SRM 51-70-10. (K)SDR USAA050107Structure · crackedPIT - Q6 - NR 2 SLAT, .1250 INCH CRACKS (3 EA); LOWER T CHORD AFT ROW OF FASTENERS AT ACTUATOR MOUNT; INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. (K)SDR USAA050095Structure · crackedPIT - Q6 - NR 1 SLAT, .1250 INCH CRACKS-2 EA; LOWER T-CHORD, AFT ROW OF FASTENERS, APPROX 40 INCHES FROM IB EDGE. INSTALLED DOUBLER IAW SRM. (K)SDR USAA050093Skin · crackedPIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K)
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