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.

SDR UPS96205915Bottle Pin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING FRONT SPAR WING BOTTLE PIN HAS CORROSION ON FLANGE. REMOVED BOTTLE PIN IAW MM 57-41-0.Mar 25, 1996 · N915UP · Boeing 72727CSDR 96ZZZM774Doubler · crackedDURING C-CHECK, FOUND DOUBLER CRACKED ON WING RIB AT STATION 686.5 AND STRINGER 1. REPAIRED BY REPLACING DOUBLER PER SRM 57-10-5.Mar 25, 1996 · N52311 · Boeing 727231SDR 96ZZZM772Hat Section · crackedDURING C-CHECK, FOUND CRACK ON FORWARD TANG OF HAT SECTION, RIGHT WING WS 601.5. REPAIRED PER SSRM 57-20-201 AND TWA STANDARD PRACTICES. (M)Mar 25, 1996 · N52311 · Boeing 727231SDR 9606779180L/E Fence · separationDURING LINE CHECK, FOUND THAT THE RIGHT WING LEADING EDGE FENCE WAS MISSING AFTER FLIGHT 0278, MEM-DTW. REPAIRED THE WING LEADING EDGE PER EA 91102665.Mar 23, 1996 · N3312L · Doug DC914SDR C2XA96IA078Bolt · not sealedIAH - DURING C-CHECK INSPECTION, THE LEFT ENGINE, INBOARD LOWER MOUNT BOLTS WERE FOUND TO BE LEAKING FUEL. MAINTENANCE REMOVED THE CENTER WING PLANK, REF ATR MM JIC 57-14-12, INSPECTED THE BOLT HOLES, REPLACED THE LOWER TWO BOLTS, AND RESEALED THE BOLTS ON INMar 22, 1996 · N16824 · Aerosp ATR42300SDR UPS96405748Support · corrodedWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT WING LOWER SURFACE FOUND CORROSION AT O/B SUPPORT JACK POINT WS 1280. REMOVED AND REPAIRED CORROSION DAMAGE IAW SRM 51-10-01, 57-30-01 AND UPS EFN 747-57-0322.Mar 21, 1996 · N681UP · Boeing 747121SDR AU960338Bolt · broken(AUS) WING REAR SPAR ROOT JOINT ATTACHMENT FITTING BOLT BROKEN AT POSITION 'A' AS REFERRED TO IN BAE SB57-33 REV3 - FOUND DURING INSPECTION IAW AD/BAE146/016 AMDT3Mar 21, 1996 · Bac 146200ASDR AU960588Bolt · corroded(AUS) WING BOLTS CORRODED DUE TO COVERING OF BARIUM CHROMATEMar 20, 1996 · Beech 58SDR DL72S960602Stiffner · crackedWING FRONT SPAR VERTICAL STIFFENER CRACKED AT NR 3 SLAT INBOARD TRACK, OUTBOARD SIDE (ON WING). FOUND DURING F-1 LTR CK TPA 3/18/96. REPAIRED PER 57-20-21.Mar 18, 1996 · N400DA · Boeing 727232SDR CAL960564Angle · crackedKUL - THE LEFT WING (MLG SUPPORT INSTALLATION) AUXILIARY SPAR SPLICE ANGLE WAS FOUND CRACKED DUE TO STRESS CORROSION. THE SPLICE ANGLE WAS REPLACED IAW DRAWING NR ARB06361. (X)Mar 18, 1996 · N68044 · Doug DC1010SDR CAL960562Beam · corrodedKUL - THE LEFT WING UPPER TRAILING EDGE BEAM WAS FOUND CORRODED BETWEEN STA XW 118 AND XORS 240. THE AREA WAS REPAIRED IAW ECRA 5720-01514. (X)Mar 18, 1996 · N68044 · Doug DC1010SDR 9606319139Fence · separationDURING LINE CHECK, FOUND THAT THE RIGHT WING LEADING EDGE FENCE WAS MISSING AFTER FLIGHT 1704, CVG-DTW. REPAIRED THE WING LEADING EDGE PER SRM 57-06, FIG 2 AND REPLACED THE FENCE.Mar 14, 1996 · N9481 · Doug DC914SDR DL72S960560Bracket · crackedFOUND DURING F-1 LETTER CHECK, CRACK EXTENDING FROM NR 2 SLAT ACTUATOR MOUNT BRACKET UPPER I/B BOLT HOLE. REPAIRED PER M/M 57-42-0.Mar 12, 1996 · N403DA · Boeing 727232SDR DL72S960558Bracket · crackedFOUND DURING F-1 LETTER CHECK, 1 INCH CRACK AT NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-54-21.Mar 12, 1996 · N403DA · Boeing 727232SDR DL72S960557Bracket · crackedFOUND DURING E-1 LETTER CHECK, NR 1 SLAT ACTUATOR SUPPORT BRACKET CRACKED I/B SIDE. REPAIRED PER MM 57-20-21 PG 812.Mar 12, 1996 · N478DA · Boeing 727232SDR 9605956739Beam · crackedDURING PERIODIC CHECK, FOUND UPPER FLANGE ON THE LEFT WING OUTBOARD LEADING EDGE BEAM CRACKED IN RADIUS. STOP DRILLED CRACK AND CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER FROM 7075 AND HEAT TREATED TO T6. REPAIR WAS ACCOMPLISHED PER EA 67-103263, SMar 11, 1996 · N639US · Boeing 747251FSDR AU960315Plate · cracked(AUS) WING CENTRE SECTION FORWARD SPAR WEB PLATE CRACKED IN AREA OF LH UPPER WING ATTACHMENT AREA - CRACK LENGTH 25MM (0.98IN) - SEVERALSMALLER CRACKS WERE FOUND AROUND THE LOCK BOLT HOLES - CRACK LENGTHS APPROXIMATELY 7MM (0.275IN)Mar 10, 1996 · Beech 58SDR TC8A96021Doubler · brokenRIGHT WING ERS 300.344, TE STEEL DOUBLER LOWER SURFACE IS BROKEN. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS REQUIRED PER SRM 57-2-3. (M)Mar 7, 1996 · N808CK · Doug DC8F55SDR TC8A96019Doubler · crackedLW T/E LOWER SURFACE XW 60.250, DOUBLER HAS A CRACK 4.5 INCH. REPLACED DOUBLER AS PER SRM 57-2-1. (M)Mar 7, 1996 · N808CK · Doug DC8F55SDR TC8A96018Rivets · looseLEFT WING, STATION XRS 230.500 T/E LOWER PART SHOWS STRUCTURAL REPAIR WITH 4 LOOSE RIVETS AND BUCKED HEAD OVERSIZED. REPAIRED AFFECTED AREA AS REQUIRED PER SRM 57-2-1. (M)Mar 7, 1996 · N808CK · Doug DC8F55SDR TC8A96017Doubler · brokenLW T/E LOWER SURFACE XW 408.343 HAS DOUBLER BROKEN AND CRACKED (5 INCHES). MADE AND INSTALLED NEW DOUBLER AS PER SRM 57-2-3. (M)Mar 7, 1996 · N808CK · Doug DC8F55SDR EISA96031Chord · crackedCRACK FOUND AT STATION 760 LBL 70.5 WING UPPER CHORD. INSTALLED PREVENTATIVE MODIFICATION KIT PER SB 727-57-0112 AND DRAWING 65C 33202. (M)Mar 6, 1996 · N315NE · Boeing 727223SDR 96ZZZX2442Panel · delaminatedDURING AN INSPECTION, A SMALL AREA OF DISBOND WAS NOTICED ON THE TRAILING EDGE PANEL OF THE LT WINGLET. WHEN A HOLE WAS CUT IN THE SKIN TO INITIATE A REPAIR, WATER SPILLED OUT. A SUBSEQUENT X-RAY SHOWED SEVERAL AREAS OF CORROSION ABOVE THE DELAMINATION. IT Mar 5, 1996 · N165G · Gulstm G1159ASDR AU960814Hinge · worn(AUS) LH AND RH WING LOWER FORWARD SPAR TO LEADING EDGE `D' SECTION HINGE AND HINGE PINS WORN - MAXIMUM AMOUNT OF WEAR IS LOCATED BETWEEN WING ROOT TO JUST OUTBOARD OF ENGINEMar 1, 1996 · Beech 95B55SDR 9605586729Support Beam · corrodedDURING P-CHECK, FOUND CORROSION ON THE RIGHT WING SPOILER SUPPORT BEAM UPPER CHORD AT WS 684. REPAIRED CHORD (P/N 65B11614-6) PER EA 67-99439.Feb 28, 1996 · N629US · Boeing 747251FSDR IXXA9625Le Formers · crackedDURING THE D-CHECK INSPECTION, FOUND TWO CRACKED FORMERS AT FS NR 422. REPAIR WAS ACCOMPLISHED PER DACO SRM 57-3-1 AND 57-0 CODE 5 AND DRAWING CF-N820, 7/96 DATED 1/18/96 WHICH HAS APPROVAL ON FAA FORM 8110-3 DATED 1/22/96. (M)Feb 26, 1996 · N820BX · Doug DC871SDR EISA96010Brace · crackedCENTER TANK INTERIOR CRACK AT FRONT SPAR SUPPORT BRACE LEFT OF BL '0'. REMOVED SUPPORT BRACE, FABRICATED NEW BRACE PER SRM 51-40-3. INSTALLED NEW BRACE PER SRM 51-30-02. (M)Feb 25, 1996 · N315NE · Boeing 727223SDR EISA96009Doubler · crackedNR 1 TANK INTERNAL RIB AT WS 656.50 REPAIR DOUBLER CRACKED THROUGH AT LOWER CHORD. REMOVED DOUBLER CRACK ON RIB PREVIOUSLY STOP DRILLED. HFEC CONFIRMS CRACK CRACK CONTAINED BY ORIGINAL STOP HOLE, FABRICATED NEW DOUBLER AND INSTALLED PER SRM 51-30-02.Feb 25, 1996 · N315NE · Boeing 727223SDR EISA96008Doubler · crackedNR 1 TANK AT WS 686.50 REPAIR DOUBLER CRACKED THROUGH AT LOWER CHORD. REMOVED DOUBLER, CRACK ON RIB, PREVIOUSLY STOP DRILLED. HFEC CONFIRMS CRACK CONTAINED BY ORIGINAL STOP HOLES. FABRICATED NEW DOUBLER AND INSTALLED PER SRM 57-10-5. (M)Feb 25, 1996 · N315NE · Boeing 727223SDR CAL960294Bracket · crackedHOU - INSPECTION FOUND A .3750 INCH CRACK IN RT WING UPPER TRAILING EDGE BRACKET AT AILERON OUTBOARD HINGE. THE BRACKET WAS REPLACED IAW SRM 51-30-1. (X)Feb 23, 1996 · N17812 · Doug DC982SDR DL72L960418Mount Bracket · crackedFOUND DURING D-1 LETTER CHECK, .375 INCH CRACK AT NR 6 L/E FLAP ACTUATOR MOUNT BOX UPPER O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.Feb 22, 1996 · N503DA · Boeing 727232SDR AU960379Panel · corroded(AUS) CENTRE WING INNER ACCESS PANEL EXCESSIVELY CORRODED ON THE INNER BONDED EDGE DOUBLERFeb 22, 1996 · Dhav DHC8102SDR DL72S960402Angle · crackedFOUND DURING A-1 LETTER CHECK, ANGLE CRACKED NR 7 SLAT O/B TRACK SUPPORT BOX I/B ANGLE. ANGLE CRACKED NR 6 SLAT I/B TRACK SUPPORT BOX I/B ANGLE. REPLACED ANGLES PER M/M 57-20-21 PG 813.Feb 21, 1996 · N493DA · Boeing 727232SDR DL72S960397Bracket · crackedA .4375 INCH CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BRACKET I/B UPPER CORNER. REPAIRED PER MM 57-20-21 PAR 12.Feb 21, 1996 · N493DA · Boeing 727232SDR DL72L960401Bracket · crackedFOUND DURING D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER MM 57-20-21.Feb 21, 1996 · N507DA · Boeing 727232SDR 96ZZZX1109Bulkhead · crackedDURING A ROUTINE INSPECTION, THE LT WING TIP FUEL TANK ATTACH BULKHEAD WAS FOUND CRACKED. THE CRACK WAS LOCATED TWO INCHES OUTBOARD OF THE WING ATTACH BOLT. SUBMITTER STATED THIS CONDITION GOING UNREPAIRED, WOULD RESULT IN LOSS OF WING TIP FUEL TANK AND LOSSFeb 21, 1996 · N3131K · Cessna 402BSDR CAL960435Channel · crackedINSPECTION FOUND A .5 INCH CRACK AT INBOARD SIDE OF OUTBOARD TRAILING EDGE LOWER SUPPORT CHANNEL, RIGHT WING STATION 447.9. THE CRACKED CHANNEL WAS REMOVED. A NEW CHANNEL WAS DRILLED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2. (M)Feb 19, 1996 · N17410 · Boeing 727243SDR CAL960323Former · crackedKUL - INSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 867. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960322Former · crackedKUL - INSPECTION FUOND A .75 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 981. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960321Former · crackedKUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 987. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960320Former · crackedKUL - INSPECTION FUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 928. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960319Former · crackedKUL - INSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 862. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960318Former · crackedKUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 879. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960317Former · crackedKUL - INSPECTION FOUND A .75 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 873. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR CAL960316Former · crackedKUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 709. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M)Feb 18, 1996 · N68041 · Doug DC1010SDR UPS405517Chord · corrodedWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING L/E STRIP OF RABBET AREA IS BULGED AT WS 1520, CORROSION FOUND ON UPPER CHORD. REWORKED CORROSION ON UPPER CHORD AND REPAIRED UPPER CHORD ACC TO KLM DFX 96-034 APPROVEL PER UPS EFN 747-57-0307.Feb 15, 1996 · N691UP · Boeing 747121SDR 9607069758Clip · crackedDURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE CENTER WING STRINGER 11R CLIP AT RBL 42 AT THE REAR SPAR. REPLACED CLIP (P/N 4912014) PER EA 97-106790.Feb 14, 1996 · N758NW · Doug DC941SDR UPS96205634Fitting · corrosionWHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION AROUND BUSHING IN FITTING, FORWARD SIDE OF RT WING REAR SPAR FOR ATTACHMENT OF MLG SUPPORT BEAM. REMOVED AND REPAIRED FITTING NR 65-16290 PER BOEING DWG NR 65-16290 AND SRM 51-30-2.Feb 13, 1996 · N940UP · Boeing 727185CSDR DL72L960332Stiffener · crackedFOUND DURING B-1 LETTER CHECK - 1 INCH CRACK LWR END SPAR STIFFENER AT NR 6 L/E SLAT I/B TRACK I/B ANGLE. REPLACED PER MM 57-20-21.Feb 13, 1996 · N511DA · Boeing 727232SDR CAL960376Support Brackets · crackedMIA - INSPECTION FOUND 3 SUPPORT BRACKETS CRACKED AT RT WING FIXED LEADING EDGE INNER RIB. TWENTY INCHES OUTBOARD OF SLAT TRACK NR 2. THE CRACKS WERE 2 INCHES, .50 INCH, AND .50 INCH LONG. THE BRACKETS WERE REMOVED. NEW BRACKETS WERE FABRICATED AND INSTALLFeb 13, 1996 · N14890 · Doug DC982
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