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 P5CA9800304Fairing · spongedLT WING NR 2 FIXED FAIRING MARKED AREA FOUND SPONGED. NR 2 FIXED FAIRING FIBERGLASS REPAIRED AS PER SRM 51-40-15.SDR MZZA98095Angle · crackedKUL - NR 6 KRUEGER LEADING EDGE FLAP ACTUATOR TRUNNION MOUNTING BOX STRUCTURE FOUND CRACKED AT INBOARD LOWER AND OUTBOARD UPPER CORNERS. INBOARD AND OUTBOARD ANGLES FABRICATED IAW BOEING DRAWING 65-16275 AND INSTALLED IAW SRM 51-30-2. ACTUATOR REINSTALLED ANSDR AALA980349Stiffener · corrodedTUL - VERTICAL STIFFENER CORRODED RT WING FRONT SPAR STA 230. (ABOVE NR 5 L/E FLAP ACTUATOR.) REMOVED AND REPLACED CORRODED VERTICAL STIFFENER AT STA 230 ABOVE NR 5 L/E FLAP ACTUATOR. PRIMED, PAINTED, AND SEALED IAW SRM 53-10-01. TST: 49,071 HOURS. CYCLESSDR ABXA9800180Angle · crackedRIGHT WING INBOARD LEADING EDGE AT THE WING ROOT UPPER AFT CORNER, THE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DWG 5613901 AND DC8 SRM 51-1-8.SDR ABXA9800169Angle · crackedLEFT WING LEADING EDGE INBOARD END, UPPER CORNER OF THE AFT LEADING EDGE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DWG 5613901 AND DC8 SRM 51-1-8.SDR ABXA9800100Fitting · crackedLEFT WING TRAILING EDGE PANEL VERTICAL SUPPORT FITTING BETWEEN SPOILER HINGE RIBS IS CRACKED AT UPPER EDGE JUST AFT OF MAIN LANDING GEAR TRUNNION. REPAIRED IAW DC8 SRM 57-1-0.SDR DLL10980396Stiffener · crackedTHE LBL 30 STIFFENER ON THE FRONT SPAR OF THE CENTER WING WAS FOUND WITH A .5 INCH CRACK EMANATING FROM THE SECOND LIGHTENING HOLE FROM THE TOP. THE TOP SECTION OF STIFFENER WAS TRIMMED OFF AND A NEW SECTION SPLICED IN PER ER/A 363992-14, REV A.SDR DL72S980381Support Beam · chaffedFOUND DURING F-1 LETTER CHECK, MLG SIDE BRACE NUT CHAFING MLG SUPPORT BEAM. REPAIRED PER M/M 57-43-0.SDR CALA9800246Beam · corrodedINSPECTION FOUND CORROSION ON BEAM ALONG AFT END OF ACCESS OPENING 541AB ON LT WING INBOARD LOWER TRAILING EDGE. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-00.SDR CALA9800252Doubler · crackedINSPECTION FOUND A 2 INCH CRACK IN DOUBLER OF RT WINGTIP TRAILING EDGE AT WBL 626. THE WINGTIP WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. THE WINGTIP WAS REINSTALLED IAW SRM 51-30-2 AND MM 33-40-0.SDR CALA9800222Splice Plate · crackedINSPECTION FOUND A 2 INCH CRACK AT SPLICE PLATE INSIDE LEFT WING UPPER LEADING EDGE ABOVE NR 2 LEADING EDGE FLAP ACTUATOR/ANTI-ICE DUCT AREA, WS 224.5. THE SPLICE PLATE WAS REMOVED AND A STRAP WAS FABRICATED AND INSTALLED IAW SRM 57-50-2 AND 51-30-2.SDR CALA9800221Angle · crackedINSPECTION FOUND A .5 AND 1 INCH CRACK AT FASTENERS IN CURVED ANGLE INSIDE LEFT WING LEADING EDGE RIB OUTBOARD SIDE AT SLAT STA 0 (AFT OF NR 4 SLAT INBOARD MOST END). THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2SDR AU980165Bracket · cracked(AUS) WING MAIN SPAR SUPPORT BRACKET CRACKED.SDR 98ZZZX2066Nut Plate Flange · corrodedSAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LT WING FUEL ACCESS PANEL 522CT NUT PLATE FLANGE CORRODED BEYOND LIMITS. INSTALLED NEW FLANGE IAW ATR72 JIC 57-00-00 OAC 100000-001. AIRCRAFT RETURNED TO SERVICE.SDR 98ZZZX2061Nut Plate Flange · corrodedSAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT WING PANEL 622CT NUT PLATE FLANGE CORRODED. REPLACED PANEL 622CT NUT PLATE COLLAR IAW ATR72 JIC 57-00-00 OAC 100000-001. AIRCRAFT RETURNED TO SERVICE.SDR 98FDEA00101Beam · corrodedNR 0794 7-5750-7-231, LEFT MLG BEAM CORRODED ON UNDERSIDE WHERE NR 4 FLAP TRACK CONTACTS IT. REMOVED CORROSION BLENDED AREA PER EA 7-5730-29358 EA - DATE 2/10/98.SDR AALA980297Support · crackedTUL - CRACK IN VERTICAL STIFFENER ATTACH ANGLE AT FORWARD SPAR, STA 112 LEFT, OTBD OF FORWARD BOTTLE PIN. REPAIRED VERTICAL STIFFENER PER SRM 51-40-3, PAGE 2. TST: 51,688.24 HOURS. CYCLES: 31,372. (X)SDR UPS98825841Fitting · corrodedINSPECTION TYPE-C, LT WING LWR AUX SPAR TO REAR SPAR TIE FITTING HAS HEAVY CORROSION. REMOVED FABRICATED AND INSTALLED REPLACEMENT FITTING IAW 8110-3 APPROVED DHC SK 866-507.SDR EIAA98054Shim · damagedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING LANDING GEAR SUPPORT BEAM OUTBOARD END FITTING SHIM DAMAGED. SHIMS REPLACED IAW MM 57-15-01. (M)SDR QXEA9800389Clip · crackedPDX - CENTER WING LOWER SKIN 2 STRINGER TO BELLY FAIRING ATTACH CLIP IS CRACKED AT THE 7TH STRINGER BACK FROM FRONT OF CENTER WING AND WS 1700. REPAIRED IAW FOKKER SRM 53-02-17, PAGE 10, FIGURE 6 AND SRM 51-30-02.SDR UPS98825840Doubler · crackedINSPECTION TYPE-C, RT WING L/E AUX TANK O/B END INTERNAL DOUBLER HAS A 6 INCH CRACK. REPAIRED CRACKED INTERNAL DOUBLER IAW EO DC-8 5720-7767.SDR QXEA9800388Vane · dentedPDX - RIGHT WING OUTBOARD FLAP VANE INBOARD TOP SIDE DENTED DOWN AT DOUBLER FOR SHROUD PANEL. REPAIRED IAW FOKKER SRM 57-02-06, FIGURE 4, PAGE 6-7.SDR DHL9872456CAngle · crackedAT C-CHECK, LT WING FIXED LEADING EDGE INTERIOR, LOWER SUPPORT ANGLE AT STA 130 IS CRACKED AT ATTACH HOLES. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-10-1, 20 X 3. N/R 1089.SDR DHL9872428CTip · erodedAT C-CHECK, RT STAB TIP FAIRING ERODED AT LEADING EDGE. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 4 X 6. N/R 4019.SDR DHL9872411CAngle · crackedAT C-CHECK, LEFT WING LOWER TRAILING EDGE COVE PANEL I/B SUPPORT ANGLE CRACKED AT ATTACH BOLTS. REPLACED LEFT WING ATTACH BRACKET PER SRM 51-30-2. N/R 1121.SDR DHL9872410CWeb · crackedAT C-CHECK, LEFT WING FIXED LEADING EDGE INTERIOR VERTICAL WEB AT WBL 92.8 CRACKED AT ATTACH FASTENERS AT AFT END. STOP DRILL, HFEC STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 15 X 3. N/R 1093.SDR DHL9872409CAngle · crackedAT C-CHECK, LT WING LOWER TRAILING EDGE COVE PANEL SUPPORT ANGLES ARE CRACKED. REMOVED AND REPLACED SUPPORT ANGLES PER SRM 51-10-1.SDR DHL9872407CClip · crackedAT C-CHECK, NR 2 SLAT O/B TRACK TO SLAT LOWER SKIN ATTCH CLIP IS CRACKED. REPLACED SLIP PER SRM 51-30-2, N/R 1076.SDR DHL9872402CAngle · crackedAT C-CHECK, RT WING T/E PANEL UPPER SURFACE SUPPORT ANGLE I/B SIDE HAS INTERIM REPAIR CRACKED AT WS 568 . REPLACED T/E PANEL ATTACH BRACKET PER SRM 51-30-2, N/R 2346.SDR QXEA9800319Clip · crackedAT WS 1700 AND STRINGER 2.17 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01.SDR DHL9872441CStiffener · crackedAT C-CHECK, RT L/E WING STIFFENER CRACKED AT WS 304 I/B SIDE JUST ABOVE L/E FLAP ACTUATOR. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-30-4, 3 X 3. N/R 2309.SDR DHL9872406CClip · crackedAT C-CHECK, NR 1 SLAT OUTBD TRACK TO SLAT LOWER SKIN ATTACH CLIP IS CRACKED AT RADIUS. REPLACED CLIP PER SRM 51-30-2, N/R 1070.SDR DHL9872405CBracket · crackedAT C-CHECK, LEFT WING T/E CAVITY FOUND LOWER PANEL SUPPORT BRACKET CRACKED AND LOOSE BELOW NR 3 FLIGHT SPOILER. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-10-1, N/R 1049.SDR IXXA9800039Fitting · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT WING NUMBER FIVE SPOILER HINGE FITTING CRACKED. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION NEW HINGE FITTING IN ACCORDANCE WITH DAC DRAWING 3654073 AND ENGINEERING ORDER 27-DC8SDR DL72L980308Angle · crackedFOUND AT F1 LETTER CK, .5 INCH CRACK AT NR 6 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72L980305Doubler · crackedREPAIR DOUBLER CRACKED NR 1 L/E FLAP ACT MOUNT BOX I/B SIDE. REPAIRED PER MM 57-20-21 P 811.SDR DL72L980304Stiffener · cracked1 INCH VISIBLE CRACK SPAR STIFFENER AT NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21 P 813.SDR CALA9800172Doubler · crackedINSPECTION FOUND A 1 INCH CRACK IN DOUBLER INBOARD OF NR 3 SLAT OUTBOARD TRACK ON RT WING LOWER LEADING EDGE, XORS 445. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-21-01.SDR CALA9800170Flange · corrodedINSPECTION FOUND CORROSION AT AFT ANCHOR NUTS OF LT WING LOWER LEADING EDGE FLANGE, XORS 794-799. A PLATE WAS FABRICATED AND INSTALLED IAW SRM 57-10-00 AND 51-20-00.SDR P5CA9800086Tip · dentedON WALKAROUND, FOUND DENT IN LEFT WING TIP PANEL FWD SECTION. REMOVED AND REPLACED WING TIP PER MM 57-23-01.SDR B4MR98002Stiffener · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LT WING REAR SPAR STIFFENER IS CORRODED (TOP AND BOTTOM) AT WBL 108 (INBD SIDE OF LANDING GEAR TRUNNION). REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-10-1. INSTALLED REPAIR IAW B727SDR UPS98826059Fitting · crackedINSPECTION TYPE-C, FWD OF ACCESS 560-B, 30 FT INBD OF XW408 CRACKED IN STRINGER END FITTING. REMOVED CRACKED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-1-20D.SDR 98FDEA00067Fitting · crackedNR 0833 056, STA-PAE - UPON REMOVAL OF LOWER RT SPLICE FITTING FOR WING CENTER SECTION, FOUND FITTING (P/N 65-18596-2) TO BE CRACKED AND CORRODED. REMOVED AND REPLACED LOWER RT SPLICE FITTING FOR WING CENTER SECTION PER FEDEX SRM 51-30-2.SDR DLL14980244Doubler · oversizedAD95-20-04 MANDATES INSPECT OF WING UPPER SKIN SPLICE ON BOTH RT AND LT WING. APPROX 40 FASTENERS PER WING ARE TO BE INSPECTED USING LFEC. DUE TO THE -250 MOD THERE IS AN EXTERNAL DOUBLER WHICH PREVENTS INSPECTION OF ALL FASTENERS, AS ALL FASTENERS WHERE NOTSDR DL72S980243Fitting · mislocatedWHILE PERFORMING A REPAIR TO WING STR 9 PER MM 57-13-0, FIG 802 AT WS656.5 AN EXISTING HOLE ON THE TOP FLANGE OF THE RIB CHORD ASSY FALLS OUT IN THE RADIUS OF THE STRINGER TO RIB ATTACHMENT ANGLE. REWORKED PER ERA 331251-14AD.SDR 98ZZZX798Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR 98ZZZX797Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR 98ZZZX796Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR EIAA98031Tie Cap · crackedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING WS 669.5 UPPER MOST FWD SHEAR TIE CAP CRACKED. SHEAR TIE CAP REPAIRED IAW SB 57-2273 FIG 8 AND 9. (M)SDR RRXA98030Doubler · chafedDURING A MAINTENANCE VISIT, FOUND RIGHT WING OUTBD LEADING EDGE SLOT BULLNOSE SKIN CHAFED ON OUTBD EDGE. SKIN WORN THRU AND INTO THE DOUBLER AT THE OUTBD ATTACHING POINTS. REMOVED CHAFED DAMAGED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED
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