JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 RRXA11221Angle · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT O/B FLAP PANEL, LT HINGE ANGLE AT STA.410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG 5761745-39.SDR AWXA0001818Angle · crackedRT WING - SUSPECTED CRACK ON ANGLE RADIUS AT I/B SIDE OF ENGINE TOWER SHAFT ACCESS PANEL CUTOUT JUST FWD OF WING FRONT SPAR. FORMER P/N 69-37894-8 AT STA 226.47 CRACK REPAIRED IAW ER 15-6740-01137-JS4 AND REF DWG 65-49535 AND SRM 51-30-2 PG 2-5; NDT CONFIRMEDSDR QXEA0100928Angle · damagedPDX - TRAILING WING ANGLE AT LEFT-HAND WING AT YW171.4 IS CHAFED. REPAIRED IAW HORIZON AIR EA 2-57-109.SDR QXEA0100927Angle · damagedPDX - TRAILING WING ANGLE AT RIGHT-HAND YW171.4 HAS BEEN BENT BY CONTACTING SOMETHING. REPAIRED IAW HORIZON AIR EA 2-57-109.SDR RRXA11204Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT AFT WING TO BODY FAIRING SUPPORT BRACKET LOWER FORWARD ANGLE BRACKET AT STA.910, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DSDR DL72L010863Stiffener · crackedBOTH L/E SPAR STIFFENERS CRACKED AT NR 2 SLAT I/B TRACK. REPAIR PER M/M 57-20-021-8.SDR ABXA010260Fitting · corrodedLEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA (P/N 3641117-1). REPAIRED AREA IAW DC-8 SRM 51.SDR ABXA010270Fitting · corrodedLEFT WING TRAPEZOID FITTING VERTICAL ATTACH FITTING P/N 5616344-1 WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51.SDR ABXA010269Fitting · corrodedLEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA. P/N 3641117-2. REPAIRED AREA IAW DC-8 SRM 51.SDR ABXA010265Fitting · damagedRIGHT WING SKI FITTING AREA HAS 2 DAMAGED FASTENER HOLES AT STA 51 AND AFT SPAR. REPAIRED AREA IAW DC-8 SRM 51-1-12, 51-1-8, 51-1-20D, AND REA D857-40385.SDR ABXA010259Fitting · corrodedLEFT WING REAR SPAR XRS 0 AFT FACE OF VERTICAL WEB HAD CORROSION OMITTING AROUND FASTENERS. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG'S 4753127, 4652943, 4652944, 5751690, AND REA'S D857-40389, AND D857-40382MR.SDR CA010626049Structure · damaged(CAN) DURING PREFLIGHT INSPECTION MECHANIC OBSERVED THAT THE RT WING TIP HAD BEEN DAMAGED BY CONTACT WITH A HARD OBJECT 9LIKE A RUNWAY) THE WINGTIP FAIRING HAD BEEN GROUND DOWN TO THE UNDERLYING STRUCTURE AND ALSO DAMAGE THE WING EXTENSION LOWER SKIN. WING EXTSDR DL76S010854Stiffener · crackedCRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14.SDR DL72L010822Stiffener · crackedA 2 INCH CRACK AT WING L/E FRONT SPAR STIFFENER AT NR 6 SLAT O/B TRACK-O/B STIFFENER. REPAIR PER M/M 57-20-021-8.SDR 0102391153Stiffener · corrodedIn L check, found corrosion on lower end of stiffener outboard of panel 143CZ of wing center section. Repaired per EA11-182723.SDR 0102381153Skin · crackedDuring L check, found crack in upper corners of cutout on wing leading edge. Repaired per EA11-183471.SDR ERKR200100129Fitting · corrodedADDITIONAL WING REAR SPAR TO WING CENTER SECTION UPPER SPLICE FITTING REWORK. A DEVIATION TO AND ADDITIONAL REWORK FOR S/B 747-57-2110 TERMINATING ACTION PER FIG 4. THE DEVIATION CONSISTS OF USING A FILLER BETWEEN THE REPLACEMENT (NEW) 65B17223-5 SPLICE FITTSDR RRXA11151Rub Strip · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO RT WING L/E O/B SLOT VANE ATTACH FITTING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 5769857-1.SDR DL72S010737Stiffener · crackedA 2 INCH CRACK WING L/E SPAR STIFFENER I/B TRACK NR 2 SLAT I/B STIFFENER. REPLACED ANGLE PER M/M 57-200021-8.SDR UPS01835859Angle · crackedINSPECTION TYPE:C1,3 LT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED,FABRICATED, AND REPLACED ANGLESDR USAA010548Strap · brokenPIT - FOUND TIE STRAP CRACKED AND BROKEN, BETWEEN WING RIBS 22 AND 24 LEFT WING UPPER SURFACE. REMOVED AND REPLACED BROKEN PARTS, REPAIRED PER EA 71017. (M)SDR UPS01835986Intercostal · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.SDR AUS20010414Rivet · loose(AUS) LT WING STRUT ATTACHMENT RIB TO OUTBOARD TIP RIVETS LOOSE AND MISSING. LEADING EDGE HAD BEEN REPLACED IN 1972.SDR C2XA01IA278Support · crackedSJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, ONE SKIN SUPPORT WAS FOUND TO BE CRACKED ON THE LEFT HAND WING UPPER SURFACE AT RIB 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR UPS01835853Angle · crackedINSPECTION TYPE:C1,3 RT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE.SDR UPS01835868Splice · crackedINSPECTION TYPE:C1,3 LT WING L/E. LOWER INNER SPLICE IS CRACKED AT XS 520.168. REMOVED, FABRICATED, AND REPLACED DOUBLER AND PLATE.SDR UPS01835684Bracket · crackedINSPECTION TYPE:C2 LT WING LE SECTION BETWEEN NR 1 & 2 ENGINE SLOT DOOR ACTUATOR ATTACH BRACKET IS CRACKED APPROX 50 INCHES FROM OTBD LWR SIDE RMVD OB SECTION OF LT OB SLOT, SETAINER & SEAL FABBED NEW ATTACH BRA CKET FITTING IAW DAC DWG 4770278 INSTALLED SDR ZW0A0100832Clip · crackedDURING CHECK-C MAINT ON RT WING THE RIB JUST INBD OF JACKPAD HAD A 2 INCH CRACK IN ATTACH CLIP. REPAIRED PER SERVICE BULLETIN 57-170.SDR COMA0110127Support · crackedDURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.SDR COMA0110125Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDARD PRACTICES.SDR COMA0110124Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDRAD PRACTICES.SDR COMA0110121Angle · crackedDURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. THE ANGLE WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1126-21, REV IR, 7/6/99.SDR AALA20010816Angle · crackedTUL - FOUND CHORD ANGLE CRACKED BELOW NR 7 SPOILER ACTUATOR MOUNT BRACKET. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER SRM 51-20-1. MAT 7075-T6 ORIG REPAIR .063 301.5 HARD INSTALLED 3 ROWS PAST DAMAGE .25 INCH STEEL PER 51-40-4 PAGE 1. (M)SDR UPS01835682Fitting · crackedINSPECTION TYPE:C2, NR 2 MAIN FUEL TANK STRINGER SPLICE FITTING PN 3704841 IS CRACKED. LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 INSTALLED NEW FITT ING IAW DC8 SRM 51-1-20DSDR MWEA010592Fitting · gougedFOUND DEEP GOUGES ON FITTING AT STATION XRS 353 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. REMOVED FITTING, FABRICATED, DRILLED AND INSTALLED NEW FITTING.SDR MWEA010591Clip · corrodedCORROSION FOUND ON OUTBOARD OF XCW 58 LOWER TEE CAP, HORIZONTAL LEG BETWEEN STRINGER 23. REMOVED 2 CLIPS FOR OUT OF LIMITS CORROSION. FABRICATED DRILLED AND INSTALLED NEW CLIPS.SDR MWEA010590Structure · corrodedAT LEFT WING FOUND CORROSION ON LOWER TEE CAP HORIZONTAL LEG BETWEEN STRINGER 13 AND 14. REMOVED CORROSION, SUBMITTED BLENDOUTS TO BOEING AND ARE ACCEPTABLE PER TELEX MWX-ORD-01-00146H DATED 21, FEB, 2001. PLACED ON WATCH ITEM 5616 FOR REPETITIVE INSPECTION.SDR DHL2001705516Angle · crackedAT C-CHECK-T/E LWR PANEL SUPPORT ANGLE IS CRACKED AT STA 545. REPLACED T/E LWR PANEL SUPPORT ANGLE AT R/W STA 545 PER B727 SRM 51-30-2.SDR ABXA010150Fitting · crackedTHE LEFT WING LOWER TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-5-2.SDR MWEA010577Stiffener · corrodedXRS 86 WEB SUPPORT STIFFENER END TEE IS EXFOLIATED. FABRICATED AND INSTALLED END TEE.SDR RRXA11011Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH WING LOWER FALSE SPAR AFT OF MLG TRUNION AT STA XW75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-2SDR 20010606CW004Doubler · corrodedWING WAS BEING DISASSEMBLED FOR RIB REPLACEMENT. REINFORCEMENT PLATE WAS DRILLED OFF AND CORROSION FOUND ON AFT FACE OF SPAR WEB AND FACE OF REINFORCEMENT PLATE. CAUSE: MOISTURE WICKING BETWEEN PLATES AND LACK OF CORROSION PROTECTION.SDR RRXA10694Nut Plate · damagedDURING MAINTENANCE VSIT FOUND LT WING L/E FUEL TANK ATTACH SCREW TO LONG DAMAGE TO NUT PLATE AT XW-0 TO XW200 (EO), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR MWEA010554Stiffener · tool damageREMOVED STIFFENER TO FACILITATE OTHER MAINTENANCE, LEFT WING STATION XRS 85. FOUND TOOL MARKS AND LIGHT CORROSION ON STIFFENER. FABRICATED AND INSTALLED STIFFENER.SDR MWEA010553Stiffener · corrodedREMOVED STIFFNER TO FACILITATE OTHER MAINTENANCE, STATION XRS 95. FOUND TOOLMARKS AND LIGHT CORROSION ON STIFFENER. FABRICATED AND INSTALLED STIFFENER.SDR MWEA010548Web · corrodedWEB SUPPORT ASSY AT STATION XRS 137 REMOVED TO FACILITATE OTHER MAINTENANCE. CORROSION PRESENT BY FASTENER HOLES. REMOVED AND REPLACED PART.SDR RRXA10936Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING CENTER L/E O/B END ATTACH CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5769928.SDR QXEA0100488Support · chafedPDX- RIGHT HAND WING TRAILING EDGE SUPPORT ANGLE, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-57-91.SDR QXEA0100486Support · chafedPDX- LEFT HAND WING TRAILING EDGE SUPPORT ANGLE, STATION YW175.0 HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-57-91.SDR 2001FA0000082Angle · crackedWHILE PREPARING PRE-PURCHASE CONDITION REPORT ON ABOVE AIRCRAFT. THE LEFT LOWER SPAR DOUBLER WAS FOUND CRACKED. VISUAL INSPECTION SHOWED LOWER SPAR ANGLE CRACKED.
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