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 08FDEA01383Fitting · crackedRT UPPER CIRCUMFERINTIAL FITTING LOWER FASTENER INDICATES EDDY CURRENT CRACK INDICATION PER NTM 57-10-54. REMOVED AND REINSTALLED FLOOR TRIM AND AIRDUCT, AND FLOOR FITTING IAW A310 SRM 51-40-21 PARA 5, EDDY CURRENT INSP, INDICATION OF CRACK IN FITTING IAW A31SDR DHL2008753518Bracket · crackedNR 3 KRUEGER FLAP ACTUATOR I/B MOUNT ANGLE (BRACKET) CRACKED. REMOVED, FABBED AND INSTALLED IAW BOEING DWG 65-16263 REVC AND B727 SRM 51-20-1 FIG 2, 51-10-2 AND 51-30-2 MATERIAL 7075 T6 .063 INCH 9 INCH BY 6 1/4 INCH.SDR DHL2008753517Mount · crackedWHILE AT C CHECK, NR 1 KRUEGER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3.5 INCH.SDR DHL2008752516Mount · crackedWHILE AT C CHECK, NR 1 KRUEBER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3 1/2 INCH.SDR 08FDEA01361Fitting · corrodedFOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AND DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710-114882.SDR 08FDEA01360Fitting · corrodedFOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AND DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710-114882.SDR A6WA200840320Bracket · crackedON LEFT WING ANGLE BRACKET FOUND CRACK, CRACK LENGTH .900. (M) REPLACED ON LEFT WING AT WS 149.58 IAW SRM 51-41-02 AND SRM 51-41-04 (A)SDR HALA0800521Bracket · crackedSLATS NR 9 AND NR 10 INBOARD AND OUTBOARD CONTROL ROD FORWARD BRACKETS CRACKED. REPLACED BRACKETS AND RIGGED PER AIRCRAFT MAINTENANCE MANUAL 27-81-02 AND 57-41-56.SDR 08FDEA01342Attach Fitting · corrodedCORROSION FINDINGS ON RT ASA ACTUATOR ATTACH FITTING UNDER BUSHING IN OUTER LUG REPAIR PERFORMED BY INCREASING THE HOLE DIAMETER, NDT FOR CRACK FREE AND INSTALLING A BUSH PER DRAWING A576-61546-200 AND A576-61024 IAW RAS/FOK/067/2008 ISS A, APPROVED BY EA 6-57SDR DLM90080601Fitting · crackedLEFT WING GROUND SPOILER PANEL O/B HINGE MOUNT FITTNG IS CRACKED. REMOVED AND REPLACED FITTING, IAW MD90 SRM 51-30-02.SDR 08FDEA01311Attach Fitting · crackedLEFT WING INBD L/E, NR 1 SLAT TRACK FWD ATTACHMENT TO SLAT TRIM PANEL AFT SUPPORT "C" CHANNEL HAS FASTENERS LOOSE. UPON FURTHER INVESTIGATION FOUND SIDE BRACKET ON THE SLAT TRACK ATTACHMENT CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET REF DSDR DLM88080499Attach Fitting · crackedDURING HMV A CRACK WAS FOUND ON RIGHT WING LEADING EDGE CLIP AT STA XRS=271. CLIP WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.SDR IXXA08SMN115SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT INTERCOSTAL SUPPORT FITTING CRACKED AT STATION 902.000 LONGERON19 RIGHT. REMOVED CRACKED INTERCOSTAL SUPPORT. FABRICATED NEW INTERCOSTAL SUPPORTS. PERFORMED NDT INSPECTION. CLEANED, TREATED ANDSDR 08FDEA00979Bracket · crackedLT WING OUTBD FLAP FWD HINGE; POSITION TRANSMITTER SUPPORT BRACKET IS CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-33-01 & 51-35-01; VOL II. FABRICATED IAW DWG ARC0873 REV 6. ALODINED & PRIMED IAW SRM 51-21-01 PGS 24 THRU 24 VOL II. INSTALLED IAW SRM 51-33SDR 08FDEA00968Attach Fitting · gougedRIGHT WING SKIN ABOVE THE PYLON OUTBD ATTACH FITTING IS GOUGED. REPAIRED AREA IAW EA 6-5730-118443.SDR DHL2008763510Attach Angle · crackedR/WING L/E INTERIOR, CRACKED RIB ATTACH ANGLE AT RWS 125 (FRONT SPAR). FABRICATED AND INSTALLED REPAIR DOUBLER, 7075-T6 .050 INCH BY 10.5 INCH BY 2.5 INCH, PO NR 9006153, AND FILLER, 7075-T6 .040 INCH BY 3 INCH BY 2.5 INCH, PO NR 9006639, PER B727 SRM 51-40-3SDR UPS08851964Fitting · crackedINSPECTION TYPE:C2 NR 1 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. REPLACED NR 1 ALT FRONT SPAR FITTING BETWEEN XRS 428 AND XRS 463 IAW DWG 3644046, SRM 51-03-02, SRM 51-01-08, SRM 51-01-20D AND SRM 51- 01-12.SDR AMTA200800182Clamp · corrodedRT WING FUEL TANK ACCESS 632RB HAS PITTING CORROSION ON CLAMP RING. REMOVED PITTING CORROSION ON CLAMP RING IAW B737-800, SRM 51-10-02-0G, ORG MAT .129, MAT LOSS .002, REM MAT .127, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-1A, ALODINE CLAMP RING IAW SRM 51-SDR DHL2008752606Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5SDR 08FDEA00563Fitting · crackedLT WING, THREE CRACKS AT CENTRAL FITTING ATTACHMENT TO ACTUATOR AT NUMBER 4 LT SPOILER REPLACED FITTING IN ACCORDANCE WITH EA 6-5750-115315, SB A310-57-2057, IPC 57-73-11-01 AND SRM 57-73-11.SDR KCSA081097Attach Angle · crackedRIGHT WING L/E RIB ATTACH ANGLE CRACKED AT FSSI 512.SDR KCSA081096Attach Angle · crackedRIGHT WING L/E/ RIB ATTACH ANGLE CRACKED AT FSSI 540.SDR KCSA081095Attach Angle · crackedRIGHT WING L/E RIB ATTACH ANGLE CRACKED AT FSSI 598.SDR QXEA200800202Cradle · crackedPDX - C4 CHECK - RIGHT SIDE OUTBOARD FORWARD SPAR WING ATTACH BOLT BARREL NUT CRADLE AT YW42 IS CRACKED ON AFT SIDE. REMOVED RIGHT FORWARD OUTBOARD BOLT, NUT AND WASHERS AND INSTALLED SERVICEABLE HARDWARE FROM STOCK, REF TASK CARD SB84-57-19/B.SDR 08FDEA00348Support Fitting · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 01 EACH HOLE WITH CRACK INDICATION AT RIGHT WING OUTBOARD FLAP, AFT SIDE OF FLAP HINGE SUPPORT FITTING. RT OUTBOARD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS SDR QXEA200800187Mount · loosePDX - C5 CHECK - THE BOTTOM RIVETS ON THE AILERON TRIM ACTUATOR HINGE ARM MOUNTING PLATE ARE LOOSE AND WORKING. REMOVED AND REPLACED RIVET AT AILERON TRIM ACTUATOR AS PER DHC 8 200 SRM 51-40-11.SDR DHL2007873515Fitting · crackedNR 3 MAIN TANK EXTERNAL FITTING CRACKED 2" AT STA XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1SDR DHL2007873514Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACKED BETWEEN STA XRS 74.000 AND S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-SDR DHL2007873542Fitting · crackedNR 3 MAIN TANK INTERNAL FITTING CRACKED 2 INCHES AT STA XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRSDR DHL2007873540Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACKED BETWEEN STA XRS 74.000 AND S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1 SRM 51-1-20D. CLEANED APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1-12 SDR DLM90080042Attach Fitting · crackedRT ELEV AFT FAIRING CLIP CRACKED. REMOVED AND REPLACED RT ELEV AFT FAIRING CLIP IAW 51-30-2.SDR QXEA200802067Bracket · crackedPDX - C5 CHECK - LEFT WING LOWER LEADING EDGE BRACKET IS CRACKED YW 139.0. REMOVED BRACKET AND INSTALL NEW BRACKET REF -8 200 SRM 51-40-11.SDR UPS08M51416Fitting · crackedINSPECTION TYPE:1C RT WING FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED RIB FITTING IAW MD-11 SRM 51-35-01 AND 51-33-01.SDR UPS08M51415Fitting · crackedINSPECTION TYPE:1C LT WING FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED RIB FITTING IAW MD-11 SRM 51-35-01 AND 51-33-01.SDR DHL2007742038Attach Angle · crackedNR 4 SLAT LOWER TRAILING EDGE ACCESS PANEL ATTACH "L" ANGLE IS CRACKED AT UPSTOP PAD. REMOVED OUTBOARD NR 4 SLAT ACCESS PANEL AND BUMP STOP IAW B-727 SRM 51-30-2. NDT CRACK FOR END VERIFICATION IAW B-727 NDT MANUAL CH. 51-00-0 PT 6 FIGURE 23. CUT OUT 4 INCHSDR UPS07851240Bracket · crackedINSPECTION TYPE:SP BRACKET CRACKED AT 3 BOLT HOLES L/WING FRONT SPAR UPPER INBD CORNER STA 680. REMOVED, FABRICATED, AND INSTALLED REPAIR BRACKET AT L/WING FRONT SPAR STA 680 IAW SRM 51-1-21, AND DWG 5615800.SDR 07FDEA04984Lug · crackedFOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I.SDR TRAX200701803Attach Bracket · crackedFOUND WING BOX AT BLO ATTACHING BRACKET OF PANEL 291AL CRACKED.
SDR TRAX200701769Attach Bracket · crackedLEFT WING CENTER L/E INBOARD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED ATTACH BRACKET WITH SERVICEABLE BRACKET PN 600-12045-11 IAW CRJ MM 20-21-00.
SDR IXXA07SMN272SSupport · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL PART SUPPORT HAS A CRACK AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW SUPPORT ISDR DHL2007742035Bracket · crackedNR 2 SLAT ACTUATOR UPPER MOUNT HAS PLAY WITH CRACK INDICATION AT INBOARD UPPER BOLT. VERIFIED BY NDT. REMOVED PREVIOUS DOUBLER AT NR 2 SLAT ACTUATOR MOUNT INBOARD BRACKET IAW B-727 SRM 51-30-2 FIGURE 1. C/W HFEC ON STIFFENER/WEB IAW B-727 NDTM PT 6, 51-00-0SDR SWIA200719274Bracket · crackedFOUND AT C-CHECK, RIGHT WHEEL BRAKE TRANSDUCER BRACKETS ARE CRACKED. REPLACED BRACKETS PER CRJ200 SRM 51-42-06 PG 11.SDR DHL2007801513Fitting · crackedLT WING CTR L/E UPPER INTERNAL SPLICE FITTING CRACKED 3" AT STA XOLDI 6.2246. REMOVED SPLICE FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20DSDR 2007FA0001031Support Bracket · crackedDRAG LEG SUPPORT BRACKETS FOUND CRACKED ON BOTH LT AND RT SIDES DURING A ROUTINE INSPECTION. MOST LIKELY FATIGUE CRACKS OR A ROUGH LANDING. (K)SDR 2007FA0001030Support Bracket · crackedDRAG LEG SUPPORT BRACKETS FOUND CRACKED ON BOTH LT AND RT SIDES DURING A ROUTINE INSPECTION. MOST LIKELY FATIGUE CRACKS OR A ROUGH LANDING. (K)SDR SWIA200719191Bracket · crackedLEFT MAIN LANDING GEAR WHEEL WELL TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM 51-42-06 PG 11-18.
SDR CA071108003Attach Fitting · cracked(CAN) WHILE ACCOMPLISHING THE REQUIREMENTS OF SB 2/55, CRACKS WERE DETECTED ON THE LOWER LUGS OF BOTH WING LIFT STRUTS. IN BOTH CASES THE CRACKS WERE LOCATED ON THE IB FACE OF THE LUG AND WERE .7500 INCH LONG LT STRUT P/N C2W1103A, S/N 0140 WAS CRACKED ON THE SDR DHL2007801518Fitting · crackedNR 4 ALT TANK FITTING CRACKED 0.500" AT STA XRS 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00590-001, DOUGLAS DWG 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALSDR 07FDEA04710Fitting · damagedRT WING I/B LOAD FITTING HAS 3 FASTENER HOLES DAMAGED COMMON TO THE SIDE LOAD FITTING. REF S/B 757-54-0035 FIG 7, PANEL 3, STEPS 2 AND 3 IAW EA NR F-5450-108908, REAMED EACH HOLE TO REMOVE DAMAGE. ACCOMPLISHED BHEC OF THE REWORKED HOLES PER 757 NDT MANUAL D6SDR VGCA200700001Attach Fitting · crackedDURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).
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