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 CALA0100718Skin · dentedINSPECTION FOUND L/H "0" SLAT EXTERNAL SKIN DENTED. THE SKIN AND ATTACHING PARTS WERE REMOVED IAW SRM 51-30-6 AND 51-30-1. A DOUBLER WAS INSTALLED IAW SRM 57-09, FIGURE 10A. THE SKIN AND ATTACHING PARTS WERE REINSTALLED IAW SRM 51-30-6 AND 51-30-1.SDR AWXA0002219Skin · crackedNR 2 SLAT HAS CRACKS PROTRUDING FROM UNDER 2 RIVETS AT BOTTOM ROW UNDER O/B AUX ARM. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW B737-300 SRM 57-43-01 PG 216-219.SDR QXEA0101231Skin · damagedPDX-RIGHT HAND WING LEADING EDGE 612AR HAS A FASTENER HOLE TORN OUT 9.5 INCHES FROM INBOARD END IN BOTTOM ROW. REPAIRED IAW HORIZON AIR EA 2-57-124 AND RD8-57-2030.SDR DL72S011294Attach Angle · crackedNR 7 SLAT COVE SKIN ATTACH ANGLE CRACKED INBD OF INDB UP STOP. REPAIRED PER M/M 57-54-000-8SDR MWEA011089Skin · crackedRIGHT WING SLAT DOOR CUT OUT BETWEEN NR 4 AND NR 5 SLAT SKIN IS CRACKED. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER.SDR SWAA012019Slat · crackedDURING SCHEDULED C3 CHECK, FOUND 2 EA CRACKS AT # 5 L/E SLAT LOWER SKIN AFT ROW OF RIVETS, CRACKS ARE 1 & 5/8 IN LENGTH. REPAIRED SKIN PER SRM.SDR MWEA011049Rib · corrodedRIGHT WING NR 1 SLAT INBOARD IDLER TRACK, OUTBOARD RIB HAS EXFOLIATION CORROSION AROUND TRACK DOOR FORWARD HINGE BOSS. REMOVED CORROSION, DRILLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS, INSTALLED NEW INBOARD AND OUTBOARD IDLER TRACK RIBS. LEVEL 2 CORROSION.SDR SWAA011991Slat · crackedDURING SCHEDULED 1/2D CHECK, FOUND # 4 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR ATTACH. REPAIRED SKIN PER SRM.SDR COOSDR010068Skin · delaminatedLEFT WING, IB FORE FLAP UPPER SKIN DELAMINATED.SDR COOSDR010066Skin · delaminatedLEFT WING SLAT NR 3 UPPER SKIN DELAMINATED.SDR 2001UALA01348Track · out of adjNR 6 SLAT WOULD NOT RETRACT. *S/D* ACCOMPLISHED ADJUSTMENT OF THE NR 6 SLAT AUXILIARY TRACKS. EXTENDED AND RETRACTED SLATS SEVERAL TIMES. NO BINDING NOTED. OPERATION SMOOTH, ALL INDICATIONS NORMAL.SDR P2EA01127Skin · damagedSJO - DURING C-CHECK, FOUND LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BUDGED SKIN, DELAMINATION AND DENTS. LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) , NEW PART INSTALLED (P/N 65-46431-243, S/N BN188). (MSDR P2EA01116Skin · delaminatedSJO - DURING C-CHECK, LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BULGED SKIN, DELAMINATION AND DENTS. (M)SDR CALA0100636Slat · dentedINSPECTION FOUND R/H WING #2 SLAT DENTED AT LEADING EDGE. THE DENT WAS FILLED IAW SRM 57-03, FIGURE 20A & B.SDR SWAA011914Slat · crackedDURING SCHEDULED D CHECK AT DALFORT, FOUND #1 L/E SLAT LOWER SURFACE SKIN CRACKED AT OTBD END. REPAIRED SLAT PER SRM.SDR DL72S011219Rib · crackedAT HMV FOUND RIB CRACKED #3 O/B RIB OF O/B SLAT TRACK(#6 SLAT) CORR: TRIMED OUT DAMAGE FABD REPAIR DOUBLER PER MM 57-54-000-8,REMOVED SLAT TRACK,OK INSTL REPAIR,INSTLD #3 OB RIBDOUBLER PER MM 57-54,INSTLSDR SWAA011982Slat · crackedDURING SCHEDULED D CHECK AT DALFORT, FOUND # 1 L/E SLAT LOWER SKIN CRACKED AT OTBD END. REPAIRED SKIN PER SRM.SDR SWAA011849Slat · crackedDURING SCHEDULED C3 CHECK, FOUND # 1 & # 3 L/E SLATS TRAILING EDGE SKINS CRACKED ON AFT ROW OF RIVETS. REPAIRED SLATS PER SWA RA.SDR DL72S011071Skin · crackedA 2 INCH CRACK IN NR 1 L/E FLAP OUTER SURFACE OUT OF INBD LIP HINGE CUTOUT. REPAIR PER M/M 57-53-000-8.SDR 01FDEA00514Skin · gougedSEVERAL GOUGES LT WING LWR MIDDLE SURFACE OF SLATS NR 6, 7, 8. ALSO SEVERAL GOUGES ON UPPER SURFACE OF LT WING AT SLATS NR 6, 7, 8. REPAIRED PER EA 8-5750-56805 AND NR N415 UNDER WO 16747.SDR DL764011054Bolt · failedLEADING EDGE SLAT TRACK BOLT FAILED ALLOWING PROX TARGET AND BEARING TO DEPART AIRCRAFT. REPLACED BOLT.SDR DL72S011086Skin · crackedLOWER LEADING EDGE SKIN SPAR CRACKED AT ACTUATOR ARM CUTOUT. REPAIRED PER 727 AMM 57-54-000-8.SDR 2001UALA01681Slat · dentedHAIL DAMAGE DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.SDR COMA0160391Flap · chafedRT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S.B. 601R-57-022SDR AWXA0001874Skin · damagedLEFT INBOUND FOREFLAP LOWER SKIN 15 INBOUND OF O/B END REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REMOVED REPAIR ON LT INBOUND FOREFLAP LOWER SKIN 15 INCHES INBOUND OF O/B END AND INST PERMANENT REPAIR IAW B737-300 SRM 51-70-10 PAGE 88C, 88D, 88E.SDR AWXA0001867Skin · damagedLEFT I/B FORE FLAP SKIN 61.5 INCH FROM O/B END. REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REPAIRED I/B LEFT FORE FLAP SKIN WITH PERMANENT REPAIR IAW B737-300 SRM 51-70-10 PG 88C, 88D, 88E.SDR P2EA01106Slat · delaminatedSJO - DURING C-CHECK, LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS15.00. REPAIRED LEFT WING NR 3 SLAT P/N 65-46423-273A, S/N BN-7 DUE TO DELAMINATION BETWEEN SLAT STATION .27 AND 18.52 IAW COOPESA EO NR COO-CMP-SDR P2EA01107Slat · delaminatedSJO - DURING C-CHECK, FOUND RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 AND FROM SS417 TO SS 430. REPAIRED RT WING NR 6 SLAT TRAILING EDGE SECTION P/N 65-46421-228A, S/N BN-19 DUE TO DELAMINATION BETWEEN SLSDR P2EA01095Slat · delaminatedSJO - DURING C-CHECK, RIGHT WING NR 6 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 352 TO SS 360 AND FROM SS 417 TO SS 430. (M)SDR P2EA01096Slat · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING NR 3 LEADING EDGE SLAT WITH DELAMINATION AT TRAILING EDGE AREA, FROM SS 0.00 TO SS15.00. (M)SDR UPS01236182Rib · crackedINSPECTION TYPE:C, NUMBER ONE SLAT HAS CRACK IN RIB O/B OF I/B TRACK. REPAIRED IAW SRM 57-50-3.SDR GTIA010995Rib · crackedFTW - FOUND CRACKED RIB AT NR 3 SLAT INBOARD OF PULLEY. REMOVED RIVETS, INSTALLED COMPLETE IAW SRM MD-80 57-01. (M)SDR ZW0A0103404Doubler · looseTHE RT WING NUMBER 8 SLAT HAD A REPAIR ON THE INBD EDGE THAT WAS LOOSE. A 6 IN BY 3 IN DOUBLER INSTALLED PER SRM 51-70-10. APPLIED METAL TO METAL HOT BOND 250 DEG APPROX PER 57-71-10. CHECK-C 1-7-01 LAX.SDR 2001F00415Rib · crackedDURING C-CHECK, THE RIGHT WING NR 8 SLAT RIB AT STATION XOS1158 WAS FOUND CRACKED, 12 INCHES LONG. THE CRACK WAS REPAIRED IAW EA NR 10-5755-24-A0886. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DL72L010922Angle · crackedFOUND ON A2 LETTER CK, .25 INCH CRACK NR 4 SLAT T/E CHORD AT O/B TRACK CUTOUT. REPAIRED PER MM 57-54-000-8.SDR 2001UALA00953Wedge · departedNR 5 LEADING EDGE SLAT WEDGE, 49 INCH SECTION DEPARTED AIRCRAFT. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 5 LEADING EDGE SLAT. THE LOSS OF THE 49 INCH SECTION OF THE TRAILING EDGE WEDGE WAS DUE TO DELAMINATION BETWEEN THE SKIN-TO-CORE BOND LINE. DELAMINATIONSDR AWXA0001831Skin · crackedleft wing NR 2 leading edge slat lower surface has 4 cracks from rivet holes. cut out damaged area and installed filler and repair doubler IAW SRM 57-43-01 fig 206.SDR DL72L010912Rib · crackedFOUND ON C1 LETTER CK NR 1 SLAT NOSE RIB IS CRACKED I/B SIDE OF ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8.SDR DL72L010911Angle · crackedFOUND ON C1 LETTER CK NR 2 SLAT LOWER COVE SKIN ANGLE IS CRACKED AT THE TAI DUCT. REPAIRED PER MM 57-54-000-8.SDR CALA0100530Skin · dentedINSPECTION FOUND RT WING EXTERNAL SURFACE OF ZERO SLAT SKIN DENTED I/B OF THE DRIVE TRACK. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, EA 9-5740-2-A0890, AND ECRA 5740-01040.SDR DL72S010924Fastener · looseNR 2 SLAT I/B ACTUATOR RIB FASTENERS LOOSE. REQUIRING A SKIN SPLICE PER 727 SRM CH 57-54-000-8 FIG 801. ACTUAL DAMAGE NOT RELATED TO METHOD USED TO GAIN ACCESS. REASON FOR MAJOR REPAIR CLASSIFICATION UNKNOWN.SDR SWAA011593Skin · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AFT ROW OF RIVETS, 31 FROM OUTBOARD END.SDR AWXA0001774Doubler · chafedRT WING OUTBOARD FOREFLAP OUTBOARD L/E REPAIR DOUBLER CHAFED 2 SPOTS. REMOVED DOUBLER IAW SRM 51-40-02 PG 9; TRIMMED OUT CRACKED AREA IAW SRM 57-53-01 PG 201-201; FORMED, DRILLED AND LOCATED IAW SRM 57-53-01 PG 202; TREATED AND PRIMED IAW SRM 51-20-01; INSTALSDR AWXA0001767Slat · crackedRIGHT WING NR 6 SLAT CRACKED AT FASTENER HOLE WBL 550 LOWER SURFACE. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01.SDR AWXA0001766Slat · crackedNR 5 SLAT LOWER SURFACE CRACKED AT TWO FASTENER HOLES WBL 392. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 PG 216-219.SDR AWXA0001765Slat · crackedRIGHT WING NR 4 SLAT CRACKED AT 3 FASTENER HOLES AT WBL 253-257. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01.SDR USAA010568Doubler · crackedCLT - FOUND REPAIR DOUBLER CRACKED .5 INCH, NR 2 SLAT, OUTBOARD OF ACTUATOR ATTACH. REMOVED CRACKED DOUBLER, INSTALLED NEW DOUBLER PER SRM 57-43-01. (M)SDR DL757010837Wedge · dentedDURING CURRENT PSV, DENT WAS FOUND ON THE NR 3 LEADING EDGE SLAT TRAILING EDGE WEDGE. REPAIR PER ER/A 380892-14AD.SDR SWAA011531Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT LWR SKIN CRACKED AT AFT ROW OF RIVETS, IN 4 PLACES. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.SDR P2EA01070Skin · delaminatedDURING C-CHECK, FOUND LEFT WING NR 2 SLAT, P/N 65-46422-281, S/N BN-60 WITH SKIN DISBONDED AT THE T/E SECTION. REPAIRED NR 2 SLAT, P/N 65-46422-281, S/N BN-60 AT INNER SKIN BETWEEN SLAT STATION 254.27 AND 237.27 DUE TO DELAMINATION. SLAT INBOARD SECTION BETW
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