JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740' 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 = '5740' 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 LR7A2024090303563Riser · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING KINGPIN RISER CRACKED AT OWS6L, FS523. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 0136.SDR LR7A2024090303561Riser · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING KINGPIN RISER FASTENER HOLE CRACKED AT OWS6L, FS536. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 0134. / PSE# 57-50-15, AD 2012-06SDR SWAA2024101633473Attach Angle · cracked(RIGHT WING) UPPER WING PANEL SUPPORT U CHANEL AT 9-INCH O/B OF FUSELAGE; ATTACH ANGLE CRACKED AT REAR SPAR ATTACH POINT<[01] REMOVED AND REPLACED ANGLE P/N 115A5582-2 AT R/WING PANEL SUPPORT U CHANEL AND REAR SPAR ATTACH POINT IAW SRM 51-40-02-0G-0.;[02] VERISDR SWAA2024101632859Attach Angle · crackedLT WING T/E DEFLECTION CONTROL RIB I/B ATTACHED ANGLE CRACK<[01] VERIFIED;[02] VERIFIED;[03] REMOVED AND REPLACED LEFT WING T/E DEFLECTION CONTROL RIB I/B ATTACHMENT ANGLE IAW SRM 51-40-02-0G-0 PAR 4.;[04] REJECT ACTION 3: MISSING INSTALLATION DRAWING ON STATESDR CALA2024090602393Fitting · crackedSHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED.SUPPORT TAS K NSA EMX N/R 00100.SDR A6WA202408128818Bracket · corrodedLEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R120371-23 BETWEEN WS:139.54 TO WS:149.58 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R120371-23 BETWEEN WS:139.54 TO WS:149.58 LHSSDR A6WA202408128819Bracket · corrodedLEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R120371-24S BETWEEN WS:139.54 TO WS:149.58 RHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R120371-24S BETWEEN WS:139.54 TO WS:149.58 RSDR A6WA202408098817Bracket · corrodedLEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R21071-24S BETWEEN WS:139.54 TO WS:149.58 RHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R21071-24S BETWEEN WS:139.54 TO WS:149.58 RHSSDR IXXA20240808023Attach Angle · damagedR/W FRONT SPAR ATTACH ANGLE P/N 112T2277-2 HAS ELONGATED HOLESSDR SWAA2024082926057Barrel Nut · missingLEFT WING L/E AT #4 SLAT OUTBD UP STOP MISSING.<[01] REPLACED BARREL NUT; RETAINER AND UPSTOP PAD PER AMM 27-81-00;[02] INSPECTED THE REPLACED BARREL NUT; RETAINER AND UPSTOP PAD PER AMM 27-81-00;[03] CLEARANCE CHK GOOD PER M/M REF. 27-81-21SDR VNAA20240908010Hinge · corrodedCORROSION WAS FOUND ON CENTER FITTING BORE LUG L1 & L2 AT LH AILERON. CENTER FITTING BORE LUG L1 & L2 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--SDR SWAA2024090320833Nut Plate · corrodedCORROSION RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS290 AT LT WING 2024-454607<[01] REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS290 AT LT WING I.A.W SRM B737-700 51-40-02 AND DRAWING 112A4402 REV:-;[02] REPLACED RAIL NUT PLATSDR VNAA202409020007Fitting · corrodedAFTER REMOTION OF BUSHINGS AND BEARINGS ON RH AILERON///CORROSION ON LUGS R1, R2, R5 AND R6. RH AILERON LUGS R1, R2, R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR IPXA2024072973714Bracket · crackedCRACKED BRACKET, ATTACH FRONT SPAR OF L/H WING INBD L/E UPPER RIB ILES 338. (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.101. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B13921 SH 2 REV:H, 112U2001 SH 5 REV:B.SDR VNAA202407120025Trunnion · corrodedHN150978 DISCREPANCY: FOUND CORROSION ON L/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.SDR VNAA202407120024Trunnion · corrodedHN150977 DISCREPANCY: FOUND CORROSION ON LH I/B FLAP VANE ACTUATOR FWD TRUNNION BODY. (FLS65.50) CORRECTIVE ACTION: RECEIVED SERVICEABLE TRUNNION BODY (P/N: 601R14261-1),SDR VNAA202407120023Trunnion · corrodedHN150974 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.SDR VNAA202407120022Trunnion · corrodedHN150973 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS65.50) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHEDSDR VNAA202407120021Trunnion · corrodedHN150971 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS102.90) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHEDSDR VNAA202407120020Trunnion · corrodedHN150970 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS140.40) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.SDR DALA2024071006990Fitting · crackedSHIP 3309 LEFT HAND WING / RIB 6 FITTING / FWD LUG CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 614005-14AD REV B. (0438146)SDR 2024FA0000531Shim · migratedLH WING #1 AND #2 SHIMS FOUND MIGRATED DURING INSPECTION PER ADSI IB777570077.SDR 2024FA0000530Fitting · migrated#3 SUPPORT FLAP TRACKFORWARD FITTING ASSEMBLY BEARING FOUND MIGRATED.SDR SWIA202409160630Bracket · corrodedFOUND CORROSION ON ATTACHING ANGLE BRACKET FOR PANEL 642AZ. (C-CHECK RO 9/15/2024) ORIGINAL MATERIAL THICKNESS IS 0.063", REF CRJ900 SRM 57-22-55-001-001-A01. REMAINING THICKNESS IS 0.055",REMOVED 0.008" MATERIAL. IT IS OUT OF LIMIT REF CRJ900 SRM 57-00SDR SWAA2024071008167Rib · wornLEFT WING MID DEFLECTION CONTROL RIB LOOSE & WORN AT FASTENER ATTACH POINT TO FIXED UPPER PANEL. CUT OUT DAMAGE IAW SRM 57-51-02-2R-4. VERIFIED NO CRACK INDICATIONS EXIST WHILE PERFORMING AN HFEC INSPECTION OF CUTOUT AREA IAW NDT MANUAL PART 6 51-00-00 PROC.SDR SWAA2024080704330Nut Plate · crackedCRACK ON RAIL NUT PLATE LOCATED OFSS485 INTERNAL CAVITY LEADING EDGE AT LT WING 2024-404907<[01] REPLACED RAIL NUT PLATE AND FASTENERS LOCATED ON OFSS485 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. <BR>TOOL USEDSDR SWAA2024061903113Attach Angle · crackedRH WING PANEL 651CT ATTACHMENT INTERCOSTAL IS CRACKED; UPPER ROW OF RIVETS;O/B SIDE.<[01] REMOVED RW PANEL 651 ATTACHMENT INTERCOSTAL. REMOVED BULB SEAL RETAINER FROM INTERCOSTAL. MATCH DRILLED AND DEBURRED NEW PART. INSTALLED BULB SEAL RETAINER ON NEW PART. WSDR SWAA2024072403070Attach Angle · crackedRIGHT WING; TRANSVERSE WEB O/B ATTACH ANGLE IS CRACKED AT UPPER ATTACH POINT ON PROGRAM ROLLER SUPPORT FITTING<[01] REMOVED AND REPLACED RT WING TRANSVERSE WEB O/B ATTACH ANGLE;IAW SRM 51-40-02 AND DWG# 115A6200 REV B.SDR AALA202406212989Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING UPPER FIXED TRANSLATING PANEL BETWEEN INBOARD AND OUTBOARD FLAPS, ATTACH ANGLE CRACKED FOR LOWER LATERAL SEAL RETAINER PANEL AT OUTBOARD SIDE (DEFLECTION RIB ATTACH POINT). FABRICATED NEW CLIP AND INSTALLED, PER BOEING DSDR R61A2024060800255Doubler · crackedRH WING SLAT TRACK #6 CUT OUT DOUBLER FOUND CRACKED. REPLACED DOUBLER WITH REPAIR PART IAW SRM 51-41-02 AND 51-43-04 AND DRAWING 171-03066-403 AND SRM 47-49-02SDR SWAA2024070500900Attach Angle · crackedLH WING - T/E MIDSPAN BULKHEAD SEAL RETAINER ATTACH ANGLE CRACKED (PHOTO ATTACHED)<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR N6WA2024061801Attach Fitting · crackedR/H AILERON INBOARD PCU OUTPUT LINK ATTACH FITTING IS CRACKED. REMOVED AND REPLACED R/H AILERON IAW CRJ AMM 27-15-01.SDR SWAA2024070997588Fitting · crackedL/W REARE SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED BULB SEAL FITTING AT L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER AREA; PER B 737-700 SRM 51-40-02-0G-0 AND BOEING DWSDR HNAA2024070500514Fitting · wornE039831 LH AILERON PCA ACTUATOR FITTING HAS WORN / GOUGED LUG HOLE. REMOVED AND REPLACED LH AILERON PCA ACTUATOR FITTING IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.SDR HNAA2024070500513Fitting · gougedE039830 RH AILERON PCA ACTUATOR FITTING HAS WORN / GOUGED LUG HOLE. REMOVED AND REPLACED RH AILERON PCA ACTUATOR FITTING IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.SDR SWAA2024070291399Attach Angle · wornL/W FLAP TRACK AFT FAIRING 542BB AFT ATTACH BEAM AND ADJUST LINK ARE WORN<[01] REMOVED AND REPLACED L/W FLAP TRACK AFT FAIRING 542BB AFT ADJUST LINK AND ATTACH IAW AMM 27-51-18-400-802 STEPS 5.G.(1).<BR>CAL TOOL ID ATS2099 D/D 09/2024SDR SWAA2024062589195Bracket · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB ROD CONNECTED TO I/B AFT BRACKET UPPER BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ASDR JJBA20240603066Bracket · corrodedL-SHAPE BRACKET FOUND HEAVY CORROSION ON RH WING UNDER INBD FLAP SHROUD. RH WING UNDER INBD FLAP SHROUD L-SHAPE BRACKET BLENDED OUT OF LIMITS. RH WING INBD FLAP L-SHAPE BRACKET REMOVED AND REPLACEDSDR SWAA2024052087245Bracket · crackedRIGHT WING I/B UPR ACCESS PANEL SUPPORT FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING I/B UPR ACCESS PANEL SUPPORT FWD ATTACH BRACKET IAW SRM 51-40-02.SDR SWAA2024061485650Attach Angle · crackedL/H WING TRAILING EDGE; 1 EACH ANGLE CRACKED AT THE I/B SIDE OF THE DEFLECTION SUPPORT BEAM ( APPROX WS 278.5)<[01] REMOVED AND REPLACED L/H WING TRAILING EDGE; NEW ANGLE AT THE I/B SIDE OF THE DEFLECTION SUPPORT BEAM IAW B737NG-SRM51-40-02 AND BAC DWG#115A620SDR SWAA2024061485651Attach Angle · crackedL/H WING TRAILING EDGE; ATTACH ANGLE HAS 1 EACH CRACK INDICATION APPROX. WS 268.50 ( APPROX. 10' INCHES FROM THE DEFLECTION SUPPORT BEAM)<[01] REMOVED AND REPLACED L/H WING TRAILING EDGE; ATTACH NEW ANGLE APPROX. WS 268.50 (APPROX. 10' INCHES FROM THE DEFLECTISDR SWAA2024061485411Bracket · crackedLT WING T/E PANEL FWD MOUNTING BRACKET IS CRACKED (MARKED) PANEL 551FB<[01] REMOVED AND REPLACED LT WING T/E PANEL FWD MOUNTING BRACKET IAW SRM 51-40-02 AND AIPC 57-50-00-38.<BR>BRACKET PART NUMBER: 287A9152-23;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024052085305Angle · crackedL/H W/W FWD SPAR ABOVE #1 BOOST PUMP; 'Z' ANGLE CRACKED<[01] REMOVED AND REPLACED Z ANGLE IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR IXXA2024051105Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED.SDR SWAA2024053177681Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS632 AT LT WING 2024-270037<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS632 AT LT WING . IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10SDR DALA2024041104292Bracket · crackedSHIP 3139 CRACK BRACKET TELESCOPIC DUCT INBOARD OB FIXED LEADING EDGE ON LH WING. CORRECTIVE ACTION: REPLACED BRACKET AND FASTENERS ON TELESCOPIC DUCT INBOARD OB FIXED LEADING EDGE ON LH WING AS PER A319 SRM 51-72-11-001. (0287144)SDR HNA202405090002Attach Bracket · corrodedCORROSION FOUND ON UPPER AND LOWER ATTACHMENT BRACKETS ON RH WING TIP. FABRICATED AND INSTALLED UPPER AND LOWER BONDING STRAPS ON R/H WINGTIP IAW EMB-145LR SRM 51-40-02SDR SWAA2024041971406Lug · looseRT WING DEFLECTION CONTROL RIB UPPER T/E PANEL ATTACH LUG HAS LOOSE FASTENERS.<[01] REPAIRED RT WING DEFLECTION CONTROL RIB UPPER T/E PANEL ATTACH LUG AND CHECKED T/E FLAP TO PANEL GAP IAW SRM 57-51-02-2R-1; SRM 57-51-02-2R-4; MM 27-51-11-820-801; STEP 2.H.(7)SDR SWAA2024041971405Lug · looseLT WING DEFLECTION CONTROL RIB UPPER T/E PANEL ATTACH LUG HAS LOOSE FASTENERS.<[01] REPAIRED LT WING DEFLECTION CONTROL RIB UPPER T/E PANEL ATTACH LUG AND CHECKED T/E FLAP TO PANEL GAP IAW SRM 57-51-02-2R-1; SRM 57-51-02-2R-4; MM 27-51-11-820-801; STEP 2.H.(7)SDR CALA2024040300964Skate Angle · crackedGEN ITEM: 63-0600-1-2803 (B767-06-3-7290) THE I/B SKATE ANGLE IS CRACKED, LOCATED ON THE UPPER I/B EDGE OF WHERE PANEL 447DR ATTACHES TO THE LOWER SURFAC E OF THE RIGHT WING.#6173 REF AMES NR 167037-0400-0059 REPAIRED I/B SKATE ANGLE ON THE #2 ENG INBD EDGE IA
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