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 MWEA020507Stringer · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.SDR MWEA020494Stringer Clip · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.SDR MWEA020487Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTENDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION.SDR MWEA020486Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTENDING UNDER STRINGER 11. -- REMOVED CORRORION.SDR MWEA020480Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXTENDING UNDER STRINGERS 16 AND 17.SDR COOSDR020224Stiffener · crackedLEFT WING TRAILING EDGE AREA AT XRS407.000 CRACKED STIFFENER.SDR UPS02438931Fitting · crackedINSPECTION TYPE:C, RIGHT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 8 HOLE CRACK FOUND APPROX 0.030 INCH, RUNNING I/B AND NR 3 HOLE CRACK FOUND AT FWD AND AFT DIRECTION. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPSDR CA020715003Attach Angle · cracked(CAN) CRACK FOUND AT ATTACH FASTENER HOLE AT LOWER SPAR LOCATION DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLIGHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 1250 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS SDR UPS02438929Fitting · crackedINSPECTION TYPE: C, CRACK REVEALED AT RT OF BS 1241 REAR SPAR TO WING CENTER SECTION SPLICE FITTING SIGNAL INDICATION GREATER THAN 50 PERCENT FSH. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-F APPENSDR ABXA020110Spar Cap · crackedRIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25.SDR UPS02238841Pin · corrodedINSPECTION TYPE:C+SI CORROSION ON RT WING FRONT SPAR BOTTLE PIN HEAD AFT FLANGE. BOTTLE PIN REPLACED IAW MM57-41-01.SDR S5248Fitting · corrodedRIGHT AFT WING ATTACMENT FITTING CORRODED,INSPECTED IAW PSB977 CORROSION MORE THAN SURFACE DEEP PITSSDR ASAA0210124Fitting · crackedPAE - DURING SCHEDULED C-CHECK, FOUND LT MLG BEAM TO SPAR FITTING AT WING STATION 150-162 CRACKED. REPAIRED FITTING PER EA AND SERVICE BULLETING. (M)SDR ABXA010892Strap · brokenLOWER FRONT SPAR CAP, OUTBOARD OF #3 PYLON, #4 MAIN STRAP WAS BROKEN. REPLACED STRAP AND COMPLIED WITH REA #D857-43875.SDR KQ72002F00000Fitting · crackedDURING C5 AND C6 CHECK WITH FLAPS REMOVED FOR CPCP INSPECTION FOUND THE RT INBOARD FLAP INBOARD CARRIAGE AFT TRUNION BEARING SUPPORT CRACKED THROUGH INTIRE UPPER PART OF CASTING WHERE AFT BEARING SUPPORTS THE INBOARD FLAP CARRIAGE ASSEMBLY SPINDLE. THE FLAP CSDR 2002F00792Pin · corrodedAT C-CHECK, FOUND LEFT WING FORWARD BOTTLE PIN CORRODED. (M)SDR DHL2002807561FittingLT WING REAR SPAR AUX INTERIOR SHOWS A CRACKED FITTING 2 IN AT STA XW 80.000.REMOVED CRACKED FITTING PER SRM 51-3-0 PG 1.FABRICATED NEW FITTING (7075-T651).CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG1SDR EIAA2002029Fitting · crackedMZJ - FOUND IN C-CHECK, LT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT T-FITING CRACKED AT THE NR 4 FLAP TRACK. INSTALLED NEW T-FITTING PER SRM 51-30-05. (M)SDR DHL2002705543Support FittingUPON COMPLYING WITH VISUAL INSP OF LEFT WING, FOUND # 4 SPOILER ACTUATOR SUPPORT BRKT BOTTOM LEG CRACKED AND INBD AFT SPAR MOUNT ANGLE CRACKED AT LOWER END.SDR DHL2002807558FittingDURING C CHECK, FOUND L/H INBD FLAP WELL FITTING WITH CRACK IN IT AT STA XW 70.000.REMOVED DAMAGED FITTING AT STA. 70.000 PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG 1.SDR COOSDR02025Fitting · corrodedRT WING, TRAINLING EDGE AT WS383.5, FITTING CORRODED.SDR CA020304001Fitting · cracked(CAN) INSPECTION REVEALED A SMALL CRACK IN THE WEB WHERE IT JOINS THE LOWER RIGHT BOLT HOLE.THE CRACK RUNS PERPENDICULAR TO THE WEB.PART TIME IS UNKNOWN, TIME GIVEN IS AIRFRAME TIME.SDR USAA020068Fitting · crackedPIT - FOUND LEFT MLG BEAM SUPPORT FITTING 1 INCH LONG VERTICAL CRACK, TOP INBOARD FASTENER FROM BEAM PIN SLOT TO FTG EDGE. REPLACED FITTING PER BOEING SB 737-57-1216 REV 2 DATED 5/6/99 AND EA 73242. (M)SDR ABXA010738Fitting · crackedRIGHT WING AUX SPAR, LOWER "L" ANGLE, WAS CRACKED APPROXIMATELY 10 INCHES LONG AT XRS 47. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-1-8 AND 51-1-20D.SDR 2002F00044Attach Bolt · wornRIGHT FORWARD LOWER WING ATTACH BOLT WORN WHICH ALLOWED MOVEMENT BETWEEN RIGHT LOWER WING AND FUSELAGE ATTACH FITTINGS. THIS CONDITION WAS DETECTED AUDIBLY WHILE TAXING WITH A FULL FUEL LOAD.SDR AWXA200200087Attach Fitting · chafedDURING C-13 CHECK DAMAGE WAS FOUND TO THE LT WING NR 2 L/E SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 2 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.SDR UPS02237448Pin · corrodedINSPECTION TYPE:C+SI LEFT BS 740 TERMINAL PIN IS CORRODED IN AREA UNDERNEATH HEAD, AND PIN RETAINING BOLT HAS PITTING CORROSION. LEFT BS 740 TERMINAL PIN AND RETAINING BOLT REPLACED IAW MM 57-41-04.SDR 0200063215Fitting · corrodedDuring "M" check found corrosion in three holes of inner rear spar anchorage fitting. Repaired per EA 32-184839.SDR AWXA200200086Attach Fitting · damagedDURING C-13 CHECK DAMAGE WAS FOUND TO THE RT WING NR 5 SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 5 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.SDR MWEA030040Doubler · crackedLEFT WING LEADING EDGE INTERNAL DOUBLER IS CRACKED AT STATION XIS 194 -- REMOVED, FABRICATED AND INSTALLED INTERNAL DOUBLER.SDR F3LA200100138Bushing · corrodedDURING C-1 CHECK, INSPECTION REPORTED ALL BUSHINGS CORRODED ON RT WING SWING LINK ASSY. REPLACED RT WING SWING LINK ASSY PER BOEING DRAWING 65-82770 AND MM 57-15-0, STEP 5E.SDR FGQ2001F00000Fitting · corrodedINSPECTION OF LEFT WING ASSEMBLY REVEALED SEVERE EXFOLIATION CORROSION OF WING ATTACH FITTING (FWD) EXTENDING, APPROXIMATELY 18 INCHES OUTBOARD WING SKIN WAS LIFTED UP FROM SPAR.SDR 0104839855Fitting · corrodedDuring Mck in DHN, the LH MLG fitting side brace lug was found with corrosion on the forward and aft faces. Repaired per EA 98-186771.SDR DL73K011796Track · corrodedTHE REAR ENGINE MOUNT ATTACH HOLES ON THE #2 AND #3 TE O/B FLAP TRACKS WERE FOUND CORRODED. THE BORES WERE OVERSIZED TO .939" AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR ABXA010643Fitting · damagedDURING THE SIDE LINK FITTING REPLACEMENT ON THE RIGHT WING, DISCOVERED THAT TWO EXISTING ATTACHMENT HOLES WERE ALREADY SECOND OVERSIZED, WHILE SERVICE BULLETIN ALLOWED THE HOLES TO BE ENLARGED (AFTER COLDWORK) TO A MAXIMUM OF SECOND OVERSIZE. ONE OF THE HOLESSDR UPS01237075Splice Plate · crackedINSPECTION TYPE:C RIGHT MAIN W/W CENTER SPLICE PLATE CRACKED AT STR 18A RT. STA 935 STOP DRILLED END OF CRACK IAW B727 SRM 51-10-1. INSTALLED REPAIR IAW EO B727-5330-3815A ON FUSELAGE SKIN BS 935 STR 18A R/H SIDE.SDR UPS01237072Splice Plate · crackedINSPECTION TYPE:C LEFT MAIN WHEEL WELL CENTER SPLICE PLATE, CRACK AT STR 18 ALT BS935 STOP DRILED END OF CRACK IAW B727 SRM 51-10-10, INSTALLED REPAIR STR 18 ALT SIDE FUSELAGE SKIN IAW B727 EO B727-5330-3815A.SDR 2002F00861Attach Fitting · crackedWING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP, SMALL ANGLE, CRACKED AT BS 870 AND BBL 0. (M)SDR QXEA0101315Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW195. REPAIRED IAW DHC-8 RD8-57-1675, RM 51-20-16, AND SRM 51-20-36.SDR QXEA0101314Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW288. REPAIRED IAW DHC-8 RD8-57-1675, SRM 51-20-36, AND SRM 51-20-16.SDR QXEA0101313Flange · gougedPDX-GOUGES ON TOP SURFACES OF RIGHT WING LEADING EDGE FLANGE AT YW202. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-16 AND SRM 51-20-36.SDR QXEA0101312Flange · gougedPDX-GOUGES ON TOP SURFACE RIGHT WING LEADING EDGE FLANGE AT YW315. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.SDR QXEA0101311Flange · gougedPDX-GOUGES ON TOP SURFACEOF RIGHT WING LEADING EDGE FLANGE AT YW297. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.SDR QXEA0101310Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE FROM YW321 TO YW326. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.SDR QXEA0101308Flange · gougedPDX-GOUGES ON TOP SURFACE OF LEADING EDGE FLANGE AT RIGHT WING STATION YW376. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.SDR MWEA011078Rib · crackedLEFT WING #3 SLAT DRIVER OUTBOARD FITTING HAS A SMALL 1/8" CRACK ACROSS THE SIDE TO SIDE GUIDE ROLLER LOBE. -- REMOVED CRACKED RIB, LOCATED BOTH INBOARD AND OUTBOARD FITTING, INSTALLED RIB.SDR MWEA011054Skin · crackedNUMEROUS CRACKS ON LEFT WING UPPER AND LOWER INNER SKIN OF #2 LEADING EDGE, BETWEEN STATIONS XFS 202.400 - 299.939. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR AUS20010642Bolt · corroded(AUS) LOWER RH SIDE STRUT LOWER BOLT SEIZED. FOLLOWING BOLT REMOVAL ITWAS FOUND TO BE VERY RUSTED AND PITTED.SDR 0104379971Skin · crackedDuring A H Ck inATL, a crack was found in the lower skin of the LH inbd slat at station Xis =136.42. Stopped drilled and doubler installed 2014-t6 AL. Repaired per EA 99-181273SDR CA010625017Bracket · cracked(CAN) AILERON SUPPORT BRACKET AT BOLT HOLE WERE FOUND CRACKED WITH THE RIGHT HAN D PART COMPLETLY BROKEN AS PER PHOTO. SUSPECT CAUSE-CONTROLS NOT SECURED BUT ALLOWED TOFLOP AROUND DURING WINDY CONDITIONS, PROBABLY OVER A PERIOD OF TIME._P/N'S 62102-000(LEFT) 6
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