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 USAA050737Skin · crackedCLT - Q3/QX4 - WING L/E SKIN, .2500 INCH CRACK AND DENT; L/E SKIN ABOVE IB KREUGER FLAP. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM. (K)SDR USAA050738Channel · crackedCLT - C4- CHANNEL, 1 INCH CRACK, NR 3 SLAT JUST BELOW ROD END ACTUATOR ATTACHMENT POINT (L) CHANNEL. FABRICATED AND INSTALLED NEW CHANNEL. (K)SDR AWXA200500715Skin · debondedDURING C-13 CHECK DISCOVERED DISBONDED AREA LOCATED AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25. MX REMOVED DISBONDED AREA AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25 IAW BOEING 737-300 SRM 51-70-10 FIG 16. FABRICATED SDR 2005FA0001000Skin · delaminatedDURING A POST FLIGHT CHECK, A MECHANIC NOTICED A BULGE ON THE UNDERSIDE OF THE IB LEADING EDGE OF THE LT WING. UPON FURTHER INVESTIGATION, A DELAMINATION AREA OF APPROXIMATELY 22 INCHES X 10 INCHES WAS FOUND. AFTER REMOVAL OF THE LEADING EDGE AND CLOSER EXASDR DL764050311Bolt · brokenEMERGENCY DECLARED INTO LAX DUE L/E SLAT ASYM MESSAGE PSEU FAULTING NR 12 OUTBOARD SLAT SENSOR. FOUND BOLT BROKEN. REPLACED BOLT.SDR ASAA0580298Skin · dentedOKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M)SDR AWXA200500710Skin · crackedMCN - DURING C-21 CHECK FOUND 2 CRACKS .275 INCHES IN LENGTH. BOTH CRACKS LOCATED ON THE BOTTOM OF THE NR 4 SLAT SKIN, AT SS 72 TO SS 74. MAINTENANCE CUT OUT DAMAGED AREA AT NR 4 SLAT SKIN AND FABRICATED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 57-43SDR AWXA200500691Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .275 INCHES LONG LOCATED AT THE BOTTOM OF THE NR 6 SLAT SKIN, SLAT STATION 307 TO SLAT STATION 309. MAINTENANCE REMOVED DAMAGED AREA FROM THE BOTTOM OF NR 6 SLAT SKIN FROM SLAT STATION 307 TO SLAT STASDR AWXA200500741Skin · delaminatedFOUND DISBOND AREA ON UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, FROM RT SS 252 TO RT SS 253. MAINTENANCE CUTOUT SKIN AND DISBOND CORE FROM UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. SDR P5CA0501364Panel · brokenNR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK PER MM 27-81-00.SDR SWAA051610Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 5 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER SRM.SDR SWAA051609Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 4 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR ASAA0540276Skin · chafedNR 4 SLAT IB T/E CHAFED. REMOVED DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND INSTALLED REPAIR IAW SRM. (K)SDR ASAA0540266Skin · delaminatedNR 2 SLAT HAS DELAMINATED AT IB TRAILING EDGE. REPAIRED DAMAGED AREA OF NR 2 SLAT IAW SRM. (K)SDR ASAA0540264Skin · corrodedNR 5 SLAT IB TRAILING EDGE CHAFED. REMOVED DAMAGE, BONDED FILLER SKIN AND DOUBLER IAW SRM. (K)SDR DHL2005741600Rib · crackedNR 7 SLAT O/B OF ACTUATOR ROD HAS CRACKED RIB AT WS 650. REMOVED CRACK RIB, FABRICATED NEW RIB, MATL 2024-T3 .040 PO 9002248, 16 X 5 INCH IAW B727 SRM 51-30-2 AND 57-50-2 FIG 2. TREATED AND PRIMED RIB IAW B727 SRM 51-10-2, INSTALLED RIB IAW B727 SRM 51-30-2.SDR DHL2005784519Skin · crackedFOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR AND FABBED NEW IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10 DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10.SDR DHL2005784551Doubler · crackedFOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR. FABBED NEW REPAIR IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10. DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10.SDR SWAA051507Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR AWXA200500652Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK, 4 CRACKS EACH .3 INCH IN LENGTH FOUND ON BOTTOM OF NR 2 SLAT SKIN BELOW OUTBOARD MAIN TRACK AT SLAT STATION 228 TO SLAT STATION 232. MAINTENANCE CUT OUT AND REMOVED CRACKED SECTION OF NR 2 SLAT SKIN. FABRICATED FILLER SDR AWXA200500651Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK, 3 CRACKS, .3' IN LENGTH EACH, FOUND ON BOTTOM NR 1 SLAT SKIN. MAINTENANCE REMOVED PREVIOUS REPAIR AND CRACKED SECTION ON NR 1 SLAT. FABRICATED FILLER AND SPLICE PLATE. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-SDR AWXA200500650Wedge · debondedDURING C-19 CHECK, NR 2 SLAT WEDGE WAS FOUND TO BE DISBONDED ON TOP AND BOTTOM AT SLAT STATION 168. MAINTENANCE REMOVED DISBONDED SKIN AND CORE FROM TOP AND BOTTOM OF SLAT WEDGE. FABRICATED REPAIR CORE AND DOUBLER. BONDED REPAIR PIECES TO NR 2 SLAT WEDGE IASDR DHL2005784518Rib · crackedFOUND NR 6 SLAT LE INTERIOR AT WS 491 INBOARD AND OUTBOARD RIBS CRACKED. REMOVED AND REPLACED RIBS AT NR 6 SLAT LE WS 491 INBD AND OUTBOARD IAW B727 SRM 51-30-2 PN 65-17289-20 AND 65-17289-22 BOTH PO NR 5080320.SDR 05FDEA01390Slat Track · damagedRIGHT WING NR 3 SLAT, NR 10 TRACK, SLAT ATTACH POINT FITTING DAMAGED ON REMOVAL OF SLAT KNUCKLE. UPON REMOVAL OF RT NR 3 SLAT, NR 10 TRACK ATTACH POINT FITTING WAS DAMAGED AND LOWER SKIN OF NR 3 SLAT NR 10 TRACK. BLENDED GOUGES FOUND TO BE WITHIN LIMITS. ALSDR DHL2005784517Rib · crackedFOUND NR 5 SLAT LE INT AT ACTUATOR ATTACH POINT INBD AND OUT RIBS CRACKED. PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 L/E SLAT ACT ATTACH ON SLAT PN 65-17276U1 AND 65-17276-9 BOTH PO NR 516347 IAW 727 SRM 51-30-2.SDR DHL2005784515Rib · crackedNR 5 SLAT L/E INTERIOR AT ACTUATOR ATTACH POINT INBD AND OUTBD RIBS CRACKED, PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 SLAT L/E SLAT ATTACH ON SLAT P/N 65-17276U11 AND 65-17276-9,BOTH PO NR 518347 IAW B727 SRM 51-30-2.SDR AWXA200500597Skin · crackedDURING C-14 CHECK A CRACK WAS FOUND ON THE NR 1 SLAT LOWER SKIN AT SLAT STATION 256 TO SLAT STATION 260. MAINTENANCE REPAIRED THE NR 1 SLAT LOWER SKIN AT STATION 256 - 260 IAW B737-300 SRM CHAPTER 57-43-01-2 FIGURE 206 AND DWG 65C26779.SDR DHL2005741606Rib · crackedNR 7 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. REMOVED CRACKED RIB AT I/B OF ROD END IAW B727 SRM 51-30-2 FIG 7. LOCATED, DRILLED AND INSTALLED NEW RIB, P/N 65-17310-3, PO 5096251 IAW B727 SRM 51-30-2 FIG 1 AND 57-50-2 FIG 2.SDR DHL2005741605Rib · crackedNR 7 SLAT O/B RIB AT ACTUATOR ROD END IS CRACKED. REMOVED NR 7 SLAT RIB O/B OF ROD END IAW B727 SRM 51-30-2 FIG 7 LATE ENTRY, REMOVED ACCESS PANELS IAW B727 SRM 51-30-2 FIG 7. LOCATED, DRILLED AND INSTALLED NEW RIB PN 65-17310-4 PO 5096251 IAW B727 SRM 51-3SDR SWAA051420Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT INBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR DHL2005784506Spar · crackedRT WING NR 7 SLAT SPAR WEB CRACKED AT TAI DUCT CUT OUT AT WS 610.5. STOP DRILL CRACK IAW B727 SRM 51-10-1. NDT IAW B727 NDT MAN 51-00-0. FABRICATED ANGLE USING 2024-T3 .040 PO 9002219. DIM.5 3/4"X 4 1/4" IAW B727 SRM 57-50-3 FIG.4 ALODINE AND PRIME IAW B727SDR DHL2005784505Skin · dentedRT WING, DENT IN NR 6 L/E SLAT AT WS 491 ON L/E. FOUND DENT OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED SKIN IAW B727 SRM 57-50-3 AND INNER SKIN FOR ACCESS. CUT OUT SKIN DIM 10" BY 5" IAW B727 SRM 57-50-3 FIG 1. FAB PART FOR OUTER SKIN REPAIRSDR DHL2005784502Skin · dentedNR 3 SLAT UPPER SKIN IS DENTED AT WING STA.495. EVALUATED AREA TO BE CREASED AND OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED AREA AND FABBED FILLER IAW B727 SRM 57-50-3 FIG 1 REPAIR 4. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND ISDR USAA050665Skin · crackedBFM - FOUND NR 1 LE FLAP CRACKED .125 INCH, WS 505, NR 1 LE FLAP LOWER SKIN. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER AND FILLER PER SRM 57-43-01, 51-40-02, 51-21-00, 51-20-05. (M)SDR USAA050643Skin · debondedCLT - FOUND NR 6 SLAT SURFACE DISBOND 2 INCHES BY 5 INCHES, NR 6 SLAT OUTBOARD T/E. ACCOMPLISHED COMPOSITE REPAIR IAW EA 96487. (M)SDR DHL2005807521Bracket · crackedRIGHT OUTBOARD SLOT MECHANISM BRACKET CRACKED. REMOVED AND REPLACED (1EA) RIGHT OUTBOARD SLOT MECHANISM BRACKET IAW MM 20-16-0 PG 201-202. REFER TO NR 036397 FOR OPS CHECK.SDR 05FDEA01262Skin · damagedRIGHT WIN , DROOP LEADING EDGE, TOP SURFACE, FOUND WITH A EXISTING REPAIR DOUBLER AND EXISTING FASTENERS HEAD EMITTING RUST. REPAIRED IAW SRM 57-10-00 FIG. 26 VOL I.SDR 05FDEA01244Slat Track · wornLEFT SLAT TRACK NR 8 WEAR IS BEYOND ALLOWABLE LIMITS PER A310-200 SRM 57-40-00 TABLE 101 AND FIGURE 108 AND REQUIRES REPLACEMENT PER NOTE ON EA 6-5740-49974A. REMOVED AND REPLACED SLAT TRACK AND BUSHINGS IAW A310-200 AMM 27-80-14-4 AND COMPLIED WITH EA 6-5750SDR DHL2005741594Attach Bracket · crackedNR 1 SLAT ROD END ATTACH BRACKET IS CRACKED. REMOVED NR 1 SLAT ATTACH BRACKET. FABRICATED BRACKET IAW B727 SRM 57-20-2 FIG 3. TREATED AND PRIMED BRACKET IAW B727 SRM 51-10-2. INSTALLED ATTACH BRACKET IAW B727 SRM 51-30-2.SDR DHL2005741593Rib · crackedNR 1 SLAT AT ACT ROD END HAS O/B SLAT RIB CRACKED. REMOVED DAMAGED O/B RIB IAW B727 SRM 51-30-2. DRILLED, TREATED AND PRIMED RIB IAW B727 SRM 51-30-2. DRILLED, TREATED AND PRIMED RIB AND AREA IAW B727 SRM 51-30-2 AND SRM 51-10-2. INSTALLED O/B RIB IAW B727 SDR ASAA0540235Skin · delaminatedOKC - NR 5 SLAT OUTBOARD TRAILING EDGE IS DELAMINATING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, AND DOUBLER IAW BOEING 737-400 SRM 51-70-10 PAGE 8. (M)SDR ASAA0540234Skin · delaminatedOKC - FOUND NR 2 SLAT OUTBOARD UPPER/AFT EDGE IS DELAMINATING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE, FILLER, AND DOUBLER IAW BOEING 737-400 SRM 51-70-10 PAGE 8. (M)SDR USAA050639Wedge · debondedCLT - FOUND SLAT WEDGE DEBONDED 4 INCHES BY 3 INCHES, SLAT WEDGE INBOARD TRAILING EDGE. REMOVED DAMAGED CORE, INSTALLED NEW CORE, NEW FILLER AND DOUBLER IAW TR 57-42-02. (M)SDR MWEA050040Skin · crackedNUMBER TWO SLAT, RIGHT LOWER SURFACE SKIN HAS TWO SMALL CRACKS EMANATING FROM CHERRY MAX RIVETS. FABRICATED AND INSTALLED DOUBLER.SDR MWEA050039Skin · crackedNUMBER THREE SLAT, RIGHT LOWER SURFACE SKIN HAS 3 SMALL CRACKS EMANATING FROM CHERRY MAX RIVETS. FABRICATED AND INSTALLED DOUBLER.SDR 05FDEA01222Hinge Fitting · gougedGOUGE IN THE NR 6 K-FLAP CENTER HINGE FITTING COMMON TO L/E FIXED. REPLACED NR 6 K-FLAP CENTER HINGE FITTING PER SRM 51-30-2.SDR USAA050594Wedge · debondedCLT - FOUND SLAT WEDGE DISBOND 4 INCHES BY 4 INCHES, OUTBOARD END OF UPPER AND LOWER SKIN OF NR 5 SLAT. SDA COMPLETE ACCOMPLISHED COMPOSITE REPAIR IAW 57-42-04. (M)SDR USAA050593Wedge · debondedCLT - FOUND NR 3 SLAT WEDGE DISBOND 2 INCHES, UNDERSIDE SKIN AT INBOARD END. SDA COMPLETED ACCOMPLISHED COMPOSITE REPAIR IAW SRM 57-43-02. (M)SDR USAA050591Wedge · debondedCLT - FOUND WEDGE HAS AREA OF DISBOND 3 INCHES BY 5 INCHES, OUTBOARD TE WEDGE OF NR 3 SLAT. REMOVED DAMAGED CORE, INSTALLED NEW CORE FILLER AND DOUBLER IAW TR 57-42-02. (M)SDR 05FDEA01199Mount Bracket · crackedNR 1 SLAT OUTBOARD TRACK MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.
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