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 SWAA2021052669515Attach Angle · crackedDOT#12 A-186 RH WING T/E PANEL BOTTOM ATTACH ANGLE INBD OF DEFLECTION RIB CRACKED AT LOWER FWD FASTENER HOLE. REMOVED AND REPLACED R/H WING DEFLECTION CONTROL RIB AFT LOWER ATTACH ANGLE IAW SRM 51-40-02 AND AIPC 57-50-000-25.SDR FDEA202105051120Attach Angle · crackedLEFT WING FIXED LEADING EDGE, NOSE FORMER ATTACH ANGLE IS CRACKED REMOVED & REPLACED NOSE FORMER ATTACH ANGLE IAW BAC DWG 114T2240 REV - & FEDEX FEDEX EA H-5720-T0361433-P1SDR FDEA202104281065Attach Fitting · damagedWHILE ACCOMPLISHING STEP 9 OF E0 6-5710-7-3301 PT1 THE CUTTER INCREMENTS WERE NOT NOT FOLLOWED THEREFORE CUTTING MORE MATERIAL THAN REQUIRED ON ATTACHED FITTING ACCOMPLISHED EA 6-5740-T0361294 P1. WINGS - ATTACH FITTING - DAMAGE TO REAR SPAR FITTING.SDR SWIA202158653Attach Bracket · cracked* RIGHT WING SLAT TRACK CANISTER 1-3 ATTACHING BRACKET IS CRACKED. (C-CHECK RO 6/04/2021) PERFORMED REPAIR ON SLAT CANISTER NO 3, SLAT TRACK 1-3 RHS. COMPLIED WITH ALL STEPS OF REO 670-57-42-577 REV-- DATED: 2016-12-02 / LEAK CHECK GOOD. COMPLIED WITH SDR IPXA2021042068451Fitting · crackedINSPECTION TYPE:SEGREMOVE O/B DRAG LINK FITTING P/N 653N0002-15 FROM #1 PYLON. REMOVED AND REPLACED IAW EA 757-5720-27-A2563 REVSDR IPXA2021050569030Bracket · crackedINSPECTION TYPE:3CRT WING FIXED L/E FUEL DISPLAY MODULE O/B SUPPORT BRACKET IS CRACKED.REMOVED AND REPLACED CRACKED RT WING FUEL DISPLAY MODULE O/B SUPPORT BRACKET IAW SRM 51-33-01, 51-35-01 & 51-35-02. (MINOR)SDR CALA2021041400466Bracket · crackedR/H WING T/E CAVITY REAR SPAR BELOW NO.9 SPOILER BRACKET FND CRA CK - REF HAECO NON-ROUTINE NO.9430770, ORIGINATED BY EMP V943077 0, SPEC NO.B787-06-3-0073 PERFORMED BY EMP V902987, RII BY HAECO TA511 - R/H WING T/E CAVI TY REAR SPAR BELOW NO.9 SPOILER RIB REPSDR CALA2021041400465Bracket · crackedL/H WING T/E CAVITY REAR SPAR BELOW NO.6 SPOILER BRACKET FND CRA CK - REF HAECO NON-ROUTINE NO.9430768, ORIGINATED BY EMP V902987 , SPEC NO.B787-06-3-0055 PERFORMED BY EMP V902987, RII BY HAECO TA511 - L/H WING T/E CAVI TY REAR SPAR BELOW NO.6 SPOILER RIB REPASDR CALA2021041400451Fitting · crackedSUPPORT TASK - EA 5510-01896 REV C (AD 2013-08-02) L/H ELEVATOR OUTBOARD ACTUATORFITTING FOUND CRACK. PRINT AND ACCOMPLISHED 26- 0555-8-0003 OP 16 REF NR L/P 9130406 LH ELEVATOR OUTBOARD ACTUATOR FITTING REPLACED AND INSTALLED AS PER EA 5510-01896 REV C OP 16.SDR CALA2021033000397Fitting · crackedSHEAR FITTING AT STA540 LBL6.14 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737- 700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/202 1 INSSDR CALA2021033000396Fitting · crackedSHEAR FITTING AT STA540 RBL54.60 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/20 21 INSDR CALA2021033000395Fitting · crackedSHEAR FITTING AT STA540 LBL32.40 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 AND SUPP ORT BRACKET. IAW B737-700 SRM 51-40-02 AND UNITED ECRA 5714-0120 5 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPEC TIONSDR CALA2021033000394Fitting · crackedSHEAR FITTING AT STA540 RBL40.87 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87. IAW B73 7-700 SRM 41-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 ISDR CALA2021033000393Fitting · crackedSHEAR FITTING AT STA540 LBL40.87 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 ISDR CALA2021033000392Fitting · crackedSHEAR FITTING AT STA540 LBL15.04 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04. IAW B73 7-700 SRM AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2021 INSPECTION CSDR CALA2021033000391Fitting · crackedSHEAR FITTING AT STA540 RBL15.04 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U345651,3/29/20 21 INSDR CALA2021033000390Fitting · crackedSHEAR FITTING AT ST540 RBL32.40 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 INSDR CALA2021033000389Fitting · crackedSHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14. IAW B737 -70SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR RE PORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2021 INSSDR SIMA20210325004Spar · crackedRH WING, OUTBD OF RIB 26, THERE IS A CRACK ON THE WING TIP ALONG SPAR 1. (MARKED)-C/A-COMPLETE:SEE NRTC E853951 FOR REPLACEMENT OF RH WING TIP SPAR 1.SDR SWIA202158336Bracket · cracked*ANGLE BRACKET UNDER R/H LEADING EDGE GAP PNL 620ML IS CRACKED. (BRACKET FLAGGED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED BRACKET REF. CRJ 200 SRM 51-40-11SDR SWIA202158335Bracket · cracked*ANGLE BRACKET UNDER L/H LEADING EDGE GAP PNL 520ML IS CRACKED. (BRACKET FLAGGED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED BRACKET REF. CRJ 200 SRM 51-40-11SDR FDEA202103250763Fitting · crackedNDT INSP - RH WING FR47 171# HOLE FOUND CRACKED SINGNAL. REPAIRED THE CRACKED HOLE 171 OF RH WING FR47 AFT FITTING PER EA 6-5710-T0353473 B P10 & SRM 51-40-44 & SRM 51-40-21. THIS IS A CAT B REPAIR. THE FURTHER INSPECTION REQUIREMENT PER EA 6-5710-T0353473SDR DALA2022031701788None · noneSHIP 692 REPAIR TO LH ENGINE DRAG FITTINGS. ACCOMPLISH SECTION II: REPETITIVE GVI INSPECTIONS INSTRUCTIONS PER ER/A 590601-14AD REV . ORIGINAL. CORRECTIVE ACTION: REF ER/A 590601-14 REVISED TO REV. A. (1763171)SDR DALA2022052603656None · noneSHIP 692 REPAIR TO RH ENGINE DRAG FITTINGS. ACCOMPLISH SECTION II: REPETITIVE GVI INSPECTIONS INSTRUCTIONS PER ERA 590589-14AD REV ORIGINAL. CORRECTIVE ACTION: REF ERA 590589-14 REV A.SDR SWIA202157679Bracket · cracked*L/H FUEL TANK, INSIDE PNL 551AB, FWD INBD BAY HAS A CRACK ON THE SLAT CANISTER BRACKET (MARKED) (C-CHECK RO 4/21/2021) PERFORMED REPAIR TO LH SLAT CANISTER SLAT TRACK 1-3 REF ALL STEPS OF REO 670-57-42-577 REV--, DATED 2016-12-02. COMPLIED WITH TASK CASDR DU4R2021031900046Attach Fitting · corrodedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND EXFOLIATED CORROSION ON ATTACH FITTING OF R/H UNDER WING SKIN PANEL O/B OF LANDING GEAR. S/O 660004 N/R 45078SDR IPXA2021032667308Bracket · crackedINSPECTION TYPE:CRH WING AT ABX 0 TE SUPPORT STRUCTURE IS CRACKED ON ATTACH LEGREPLACED SUPPORT STRUCTURE USING FABRICATED A57240071201 MADE FROM 2024 T3.040C IAW SRM 51-40-21SDR FDEA202103130853Fitting · crackedCRACK INDICATION ON FRAME 47 RH SIDE ON CWB REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE AT OPEN FASTENER HOLE F (CRACK DIRECTION IS 7 OCLOCK) AT LOWER FUSELAGE (1EA) REPAIRED IAW EA 6-5710-T0360412 (P1) RELEASE DATE 06-APR-21 EA TITTLE: WINGS - BASDR DALA2021031501439Bracket · crackedDURING HCK MAINTENANCE FOUND CRACKED LUG ON BRACKET TO ATTACHED AILERON TRIM ACTUATOR AT LH WHEEL WELL. REPAIRED PER ERA 590491-14. (LP 1753656)SDR SWAA2021031654855Attach Angle · crackedR/H MLG WING W/W UPPER WING PANEL SUPPORT FWD 'Z' ATTACH ANGLE IS CRACKED / R&R R/H MLG WING W/W UPPER WING PANEL SUPPORT FWD 'Z' ATTACH ANGLE PER SRM 51-40-02.SDR DALA2021031501435Fitting · damagedDURING INSPECTION MAINTENANCE FOUND CORROSION AND SCRATCHES AFFECTING HOLES 4, 8, 13 & 17, COMMON TO RH WING UPPER SKIN AND FORWARD DRAG FITTINGS ALSO, CORROSION WAS REPORTED ON THE WING SKIN LOWER SURFACE AND MAJOR SHIM MIGRATION WAS NOTED AT SHIMS 1C & 1D. RSDR SWAA2021030853168Bracket · crackedRH INBD REAR SPAR UPPER TE SUPPORT BRACKET CRACKED (JUST ABOVE WW LIGHT). REMOVED AND REPLACED SUPPORT BRACKET PER SRM 514002.SDR FDEA202103040569Attach Angle · crackedRIGHT WING L/E ATTACH ANGLE CRACKED @ OSS 441 REMOVED CRACKED NOSE FORMER AND ATTACH ANGLE ON R/H WING L/E OSS441 IAW B767SRM B767SRM 51-40-05,51-40-02,BAC DWG 114T2241 REV-,AND FED EX EA #H-5720-T0360115 (P1),TITLED "SECONDARY WING STRUCT-R/H WING,L/E,ANGLESDR DALA2021030401255Brace · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON OPEN HOLES RH ENG DRAG FTG CLAMP-UP & DIAG BRACE WERE FOUND AS FOLLOW; HOLE #8 CORROSION AND TOOL MARKS ON SKIN AND FITTING AT 12 O'CLOCK POSITION, HOLE #10 CORROSION AND TOOL MARKS ON FITTING AT 10 O'CLSDR SWIA202157337Mount Bracket · corrodedFOUND MOUNT BRACKET ON THE O/B SIDE OF THE LH INTERNAL REAR SPAR TO THE AUXILLARY SPAR SECTION BEHIND PANEL 542AZ CORRODED. / (AREA MARKED) (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW MOUNT ANGLE WITH PN CC670-10338-1 O/B SIDE LH INTERNAL REAR SPAR RESDR IPXA2021032767352Stringer Clip · crackedINSPECTION TYPE:3C#1 MAIN FUEL TANK STRINGER 38 CLIP IS CRACKED AT STA XORS 506.REMOVED AND REPLACED CRACKED #1 MAIN FUEL TANK STRINGER CLIP AT STA XORS 506 IAW SRM 51-33-01. (MINOR)SDR DALA2021030401250Drag Fitting · looseDURING INSPECTION MAINTENANCE FOUND LOOSE FASTENER NBR 3 AT LH WING DRAG FITTING AND REPLACED PER ERA 590310-14AD.SDR DALA2021030401245Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND RIGHT ENGINE DRAG FITTING HOLE # 16 HAS INDICATIONS OF LEVEL 2 CORROSION IN THE FITTING 360 DEGREES AROUND HOLE. REPAIRED #16 HOLE PER ERA 589987-14.SDR DALA2021030401244Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RIGHT ENGINE DRAG FITTING HOLE # 17 HAS INDICATIONS OF CORROSION IN SKIN AND FITTING 360 DEGREES AROUND HOLE. REPAIRED PER ERA 589987-14.SDR DALA2021030401243Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 18 HAS INDICATIONS OF CORROSION IN THE FITTING 360 DEGREES AROUND HOLE. REPAIRED PER ERA 589987-14.SDR DALA2021030401242Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND RIGHT ENGINE DRAG FITTING HOLE # 12 HAS INDICATION OF CRACK AT 9 OCLOCK IN FITTING. REPAIRED RIGHT ENGINE DRAG FITTING HOLE #12 PER ERA 589987-14AD (LP 1744278).SDR DALA2021030401240Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITING HOLE # 14 HAS INDICATION OF CRACK WITH CORROSION AT 9 OCLOCK POSITION FACING AFT IN THE SKIN AND AN INDICATION OF CRACK WITH CORROSION AT 3 OCLOCK IN SKIN AND FITTING. REPAIRED PER ERASDR DALA2021030401239Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 13 HAS INDICATION OF CORROSION IN SKIN. REPAIRED PER ERA 589971-14 (LP 1744246)SDR DALA2021030401237Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 5 HAS INDICATION OF CORROSION IN SKIN AND FITTING 360 DEGREES AROUND HOLE. REPAIRED FITTING PER ERA 589971-14. (LP 1744242)SDR DALA2021030401235Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 2 HAS INDICATION OF CRACK AND CORROSION AT 9 OCLOCK POSITION FACING AFT IN SKIN AND FITTING. REPAIRED PER ERA 589971-14 (LP 1744239)SDR DALA2021030401234Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 3 HAS INDICATION OF CRACK AND CORROSION AT 10 OCLOCK POSITION FACING AFT IN FITTING AND INDICATION OF CRACK AND CORROSION AT 5 OCLOCK IN SKIN. REPAIRED PER ERA 589971-14. (LP 1SDR DALA2021030401233Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH ENG DRAG FITTING HOLE # 4 HAS INDICATION OF CRACK AT 10 OCLOCK POSITION FACING AFT IN FITTING. CORROSION REPAIRED PER ERA 589971-14. (LP 1744233)SDR DALA2021030401231Drag Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 7 HAS INDICATION OF CORROSION IN SKIN. REPAIRED PER ERA 589987-14. (LP 1744219)SDR DALA2021030401230Drag Fitting · contaminatedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RH ENG DRAG FITTING HOLE # 9 HAS INDICATION OF CRACK AND 10 - 11 OCLOCK POSITION FACING AFT IN THE FITTING. REPAIRED PER ERA 589971-14 (LP 1744218)SDR SWIA202157139Nut · corrodedRH WING HINGE BOX ATTACHING HARDWARE NUTS FWD AND AFT AT WS 178, WS 220, AND WS 264 ARE CORRODED/ RUSTED AND REQUIRE REPLACEMENT. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED SERVICEABLE HARDWARE ON R/H FLAP HINGE BOX WS 178.00,WS 220.00AND WS 264.00 IAW C
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