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 IPXA09M57095Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W4-06 RIGHT NR 8 SLAT BETWEEN STA XOS 1158 - XOS 1173 EXTERIOR EXISTING DOUBLER NOT PER SRM 57-10-00 VOL 1 PG 13 NOTE -1. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR UPPER AND LOWER SEALS, SPLSDR IPXA09M57068Slat · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W4-04 RT NR 3 SLAT BETWEEN STA XOS484-490 REPAIR DOUBLER NOT IN SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-345 91-A AND SAA EA 011-5754-01-A1964.SDR IPXA09M57066Slat · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W3-13 LT NR 5 SLAT BETWEEN STA XOS 659-662 REPAIR DOUBLER NOT PER SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-3457 6-A AND SAA EA 011-5754-01-A1958.SDR IPXA09556941Skin · debondedINSPECTION TYPE:C 1 REPAIR 415-W4-01 IS DISBONDED, NR 8 SLAT UPPER T/E WEDGE UPPER SURFACE AT OSS 476-479. REPAIRED NR 8 SLAT UPPER T/E WEDGE UPPER SURFACE SKIN IAW SRM 51-70-10.SDR IPXA09M57069Skin · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ 296-W4-02 AND VALIDATION EO MD11-5100-34211-A ITEM 8 RT WING NR 2 SLAT UNDERSIDE PREVIOUS LARGE DOUBLER 1EA 5/32 CHERRY MAX RIVET HAS ED OF .25. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-34 566-A ASDR FDEA200907282793Skin · crackedLT WING EXT STRUCTURE FOUND CRACKED ON LWR EXT SKIN L/E SLAT NR 4. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 & SRM 57-10-00 FIG 43 VOL I.SDR USAA2009081892160Wedge · delaminatedSAL - Q6 - MAJOR REPAIR - DELAMINATION ON NR 3 SLAT TRAILING EDGE WEDGE AT INBOARD END BETWEEN SS12.25 TO SS31.25. REPAIRED NR 3 SLAT TRAILING EDGE WEDGE AT INBOARD END SS12.25 TO SS31.25 IAW B737 SRM 51-70-10.SDR IPXA09556937Skin · delaminatedINSPECTION TYPE:C1 NR 7 SLAT HAS A DENT ON UPPER SURFACE NR 6 FROM THE TRAILING EDGE 15 INCHES FROM I/B EDGE. TAP TEST REVEALS DISBOND. REPAIRED DISBOND ON NR 7 SLAT IAW SRM 57-43-02-1A 1 AND SRM 51-70-10-2R 3.SDR SWAA094897Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR FDEA200907272806Angle · crackedNR 2 SLAT AFT LWR CHORD ANGLE PREVIOUS REPAIR IS CRACKED BELOW T-DUCT. REMOVED INNER ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. REMOVED CHORD ANGLE AT NR 2 SLAT IAW SRM 51-30-2. FABRICATED NR 2 SLAT AFT LWR CHORD ANGLE USING BAC 1514-1559 2024 T3511, PO NR 2SDR SWAA094783Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 3 SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA094782Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.SDR IPXA09M57093Fastener · looseINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 296-W4-07 RT WING NR 8 SLAT BETWEEN STA XOS 1188- XOS 1177 REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR UPPER AND LOWER SEALS, SPLICE PLATE, SKIN FILLER, BAFFLESSDR UALA2009072402211Skin · delaminatedNR 6 LEADING EDGE SLAT IS DELAMINATING ON UPPER SURFACE IN AREA OF PREVIOUS REPAIR. DETERMINED THAT AREA IS BEYOND LINE REPAIRABLE LIMITS. DAMAGED SLAT REMOVED, INSTALLATION. COMPLETED INSTALLATION OF SLAT. INSPECTED INSTALLATION AND RIG OF NR 6 LE SLAT. ALLSDR ASAA0946255Skin · wornNR 2 SLAT T/E WEDGE WORN THROUGH LOWER SKIN I/B END. REPAIRED NR 2 SLAT T/E WEDGE ON I/B END LOWER SURFACE.SDR ASAA0946249Doubler · chafedNR 3 SLAT T/E WEDGE PREVIOUS REPAIR AT I/B END IS CHAFED. REPAIRED NR 3 SLAT T/E WEDGE AT I/B END.SDR SWAA094728Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA094639Skin · puncturedDURING SCHEDULED SPV CHECK, FOUND LT WING L/E NR 1 SLAT SKIN PUNCTURED. REPAIRED SKIN PER SRM.SDR FDEA200907212683Skin · chafedCHAFING MARKS AT LOWER SKIN OF RIGHT NR 1 SLAT BETWEEN ROBS 21 AND 23 REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5740-131244SDR IPXA09556756Panel · crackedINSPECTION TYPE:C2 NR 10 SLAT AT I/B ACT TRACK 2EA CRACKS IN COVE PANEL 1 I/B & 1 O/B. REMOVED & REPLACED NR 10 SLAT.SDR SWAA094602Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 3 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER MM.SDR USAA2009081292096Wedge · debondedMCN - C22 - MAJOR REPAIR - DEBONDED NR 2 SLAT TRAILING EDGE WEDGE AT WBL 408.38 TO WBL 414.38. REPAIRED NR 2 SLAT TRAILING EDGE WEDGE AT WBL 408.38 TO WBL 414.38 IAW B737-300 SRM 51-70-10-2R4.SDR USAA2009080592020Skin · debondedMCN - C22 - MAJOR REPAIR - NR 6175438 - NR 2 SLAT TRAILING EDGE DISBONDED ON UPPER SURFACE. REPAIRED NR 2 SLAT TRAILING EDGE UPPER SURFACE IAW B737 SRM 51-70-10-2R4.SDR USAA2009080592019Skin · delaminatedMCN - C22 - MAJOR REPAIR - NR 6175442 - NR 5 SLAT DELAMINATED ON UPPER AND LOWER SURFACES. REPAIRED NR 5 SLAT UPPER AND LOWER SURFACES IAW B737 SRM 51-70-10-2R4.SDR USAA2009073191969Slat · crackedMCN - MAJOR REPAIR - C22 CHECK - RIGHT WING NR 4 SLAT LOWER LEADING EDGE CRACKED. REPAIRED RIGHT WING NR 4 SLAT LOWER LEADING EDGE IAW B737 SRM 57-43-01.SDR IPXA09656860Skin · crackedINSPECTION TYPE:C LT WING NR 4 SLAT I/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 4 SLAT OSS573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-T6-0.0SDR IPXA09656857Skin · crackedINSPECTION TYPE:C RT WING NR 9 SLAT O/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. RT WING NR 9 SLAT AT OSS 641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-SDR IPXA09656855Skin · crackedINSPECTION TYPE:N/A LT WING NR 4 SLAT O/B NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 4 SLAT OSS 641.55 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-TSDR IPXA09656853Skin · crackedINSPECTION TYPE:C LT WING NR 3 SLAT I/B AREA NOSE SKIN FASTENER HOLE AREA FOUND CRACKED, CRACK LENGTH 0.125 INCH. LT WING NR 3 SLAT AT OSS 724.49 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL SDR UALA2009072002141Panel · damagedRIGHT SIDE WING LEADING EDGE SLAT NR 12 LINKAGE FAIRING PANEL NR 24 DAMAGED. SLATS OPERATE NORMALLY. PANEL REMOVED AND PLACED IN LOB BOX. REMOVED AND REPLACED SLAT NR 12 LINKAGE PANEL.SDR FDEA200907172649Skin · chafedFOUND CHAFING MARKS ON LOWER SKIN OF LT SLAT NR 1 REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW. RAS/FOK/156/2009 ISS. A, APPROVED BY EA 6-5740-131245.SDR AALA20090716TUL01Rib · crackedNUMBER 15 SLAT RIB SHOWS CRACK INDICATION WITH HIGH FREQUENCY EDDY CURRENT. REMOVED CRACKED NUMBER 15 ATTACHED RIB, LOCATED DRILLED AND INSTALLED NEW ATTACH RIB PER ESO 80117.SDR USAA2009071791871Slat · warpedCLT - Q2 - MAJOR REPAIR - NR 5 SLAT HAS AN "OUT OF TOLERANCE" CONDITION BETWEEN THE TRAILING EDGE OF SLAT AT THE OUTBOARD END AND THE INBOARD END AND THE WING FIXED LEADING EDGE. REPAIRED NR 5 SLAT IAW US AIRWAYS EA 101265.SDR FDEA200907162647Rib · crackedNR 6 SLAT RIB IS CRACKED, OTBD SIDE OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIB AT NR 6 SLAT OUTBD SIDE OF ACTUATOR IAW SRM 51-30-2 FABRICATED NEW SLAT RIB, HEAT TREATED RIB TO T6 IAW FAS ENGINEERING REPORT 2-37153-801 REV A VERIFIED HARDNESS IAW NDTMSDR ASAA0946246Skin · activatedNR 5 SLAT I/B CORNER LOWER SURFACE CHAFED. PREPPED CHAFED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.SDR FDEA200907152626Skin · corrodedLT WING L/E NR 4 SLAT PANEL NR 522HB T/E WEDGE TOP SKIN INTERNAL SURFACES WITH CORROSION. LT WING L/E NR 4 SLAT, T/E WEDGE REPLACED. REFER TO THE MFG REPAIR ORDER DISCREPANCY WORKSHEET AND FAA FORM 8130-3 WITH TRACKING NRS FA2009/0282 AND NSFC187868-002 , SDR USAA2009072791922Skin · delaminatedCLT - Q-2 - MAJOR REPAIR - DELAMINATION ON NR 2 LEADING EDGE SLAT SKIN AT UPPER OUTBOARD END. REPAIRED NR 2 LEADING EDGE SLAT SKIN AT UPPER OUTBOARD END IAW B737 SRM 51-70-10.SDR ASAA0946355Slat · chafedNR 4 SLAT LWR SURFACE I/B AFT CORNER CHAFED. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER REPAIR.SDR FDEA200907092560Angle · crackedNR 4 SLAT AFT LOWER ANGLE IS CRACKED BELOW T-DUCT. REMOVED NR 4 SLAT INNER PANELS IAW SRM 51-30-2. REMOVED LOWER ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 57-50- 2. TREATED AND PRIMED. REPAIR PARTS IAW SRM 51-10-2 INSTALLED ANGLE IAW SRM 51-SDR IPXA09M56702Slat · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 281-W3-01 LT WING NR 1 SLAT BETWEEN STA XIS204 TO XIS211 DOES NOT CORRELATE WITH EFN2812005118 FIG 3 EN1642-05 CALL OUT ON DOUBLER 17 ROWS FASTENERS, INSTALLED 16 ROWS ONLY. REMOVED EXISTING REPAIR AT LT WING NR 1 SLAT LOWSDR SWAA094357Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT WING NR 3 SLAT L/E SLAT SKIN CRACKED. REPAIRED SLAT PER MM.SDR FDEA200907082540Web · crackedRT WING NR 1 SLAT VERTICAL WEB AT RIB 24 HAS A 0.30 INCH CRACK. REMOVED DAMAGED VERTICAL WEB, FABRICATED REPLACEMENT WEB AND INSTALLED ON NR 1 SLAT RIB 24 IAW DWG A57863063 AND A300-600 SRM 57-42-11 AND SRM 51-72-10.SDR FDEA200907072502Skin · misrepairedLT WING EXISTING REPAIR FOUND ON NR 7 SLAT. REPAIRED AS PER EA1-5750-132686. (MAJOR REPAIR)SDR USAA2009072091886Slat · delaminatedCLT - Q2 - MAJOR REPAIR - RIGHT WING NR 5 SLAT DELAMINATED ON TRAILING EDGE 10 .5 INCHES FROM OUTBOARD END. REPAIRED RIGHT WING NR 5 SLAT DELAMINATED ON TRAILING EDGE 10.5 INCHES FROM OUTBOARD END IAW B737 SRM 51-70-17.SDR IPXA09656653Slat · debondedINSPECTION TYPE:7C LEFT WING - NR 4 SLAT O/B UPPER CORNER FOUND DEBOND. DEBOND AREA REPAIR PERFORMED AS PER SRM 51-70-10, REPAIR 1, FIG 201, SHEET 1, REV 44.SDR IPXA09556839Doubler · debondedINSPECTION TYPE:C NR 4 SLAT UPPER SURFACE T/E WEDGE EXISTING BONDED REPAIR DOUBLER. FWD EDGE DISBONDING CONTACT ENGINEERING AS REQUIRED PER APPENDIX C, STEP E. REMOVE EXISTING DOUBLER IAW SRM 51-70-10-2R4 FIG 202, NO FURTHER DAMAGE FOUND. FAB REPAIR DOUBLERSDR IPXA09656655Skin · dentedINSPECTION TYPE:7C LEFT WING NR 4 SLAT UPPER SURFACE FOUND DENT. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4, FIG 202, SHEET 8, REV 44.SDR IPXA09656659Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B NOSE SUPPORT SKIN FOUND CRACKED (CRACK 0.125 INCH LENGTH). LEFT WING NR 4 SLAT OSS 573.18 AREA NOSE SKIN REPAIRED AS PER SRM 57-43-01- 2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-SDR FDEA200907042475Fitting · crackedRIGHT WING NR 2 SLAT FOUND CRACKED AT INBOARD FITTING. REMOVED AND REPLACED RT WING NR 2 SLAT AND ADJUSTED IAW AMM 27-80-01-4.SDR IPXA09656672Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT O/B NOSE SUPPORT SKIN FOUND CRACKED (CRACK 0.125 INCH LENGTH). LEFT WING NR 4 SLAT OSS 641.49 AREA NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075-0
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