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 UPS96820071Attach Points · chafINSPECTION TYPE 'C', RT WING LEADING EDGE O/B EDGE ATTACH POINTS HEAVY CHAFED. FAB DOUBLER, ALODINED AND INSTALLED IAW UPS EO DC8-57-0665.May 4, 1996 · N805UP · Doug DC873FSDR UPS96220053Web · crackedINSPECTION TYPE 'C', RT WING WEB CRACKED AT FS 106.8 APPROX 6 INCHES FROM LWR END. FAB AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-20-2, 51-40-2 AND 51-30-2.May 4, 1996 · N911UP · Boeing 72727CSDR CAL960569Support · crackedHOU - INSPECTION FOUND A 2 INCH CRACK IN UPPER AFT LEG OF LEFT WING CROSS BRACE SUPPORT. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW ECRA 5710-01727 AND SRM 51-30-5. (M)May 2, 1996 · N14879 · Doug DC983SDR AALA960688Wing Tip · damagedTUL - FOUND RIGHT WING TIP DAMAGED. REMOVED DAMAGED PARTS AND REPLACED WITH NEW PER SRM 51-10-1 PG 1-15. (M)Apr 30, 1996 · N880AA · Boeing 727223SDR EISA96047Angle · crackedLEFT WING STIFFENER ANGLE CRACKED AT UPPER TE JUST OUTBOARD OF NR 5 SPOILER. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2. (M)Apr 29, 1996 · N316NE · Boeing 727223SDR EISA96046Angle · crackedLEFT WING TRAILING EDGE ANGLE CRACKED WHERE IT ATTACHES TO UPPER TRAILING EDGE JUST FORWARD OF INBOARD AILERON INBOARD LEADING EDGE. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-01 AND 51-30-02. (M)Apr 29, 1996 · N316NE · Boeing 727223SDR CALA9600800Aux Track · crackedINSPECTION FOUND A .5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-30-2.Apr 29, 1996 · N16232 · Boeing 737217SDR AU960574Winglet · damaged(AUS) LH WINGLET STRUCK RUDDER OF A STATIONARY PC-12 (VH-FMP) DURING TAXI - WINGLET DAMAGED - DAMAGE ALSO TO UPPER RUDDER HINGE AND RUDDER TRIM TAB ACTUATOR SUPPORT OF THE STATIONARY AIRCRAFTApr 28, 1996 · Pilats PC12SDR 96ZZZX2695T-Angle · crackedDURING C-CHECK, FOUND LEFT WING AUXILIARY SPAR AREA INBD LOWER VERTICAL SUPPORT T-ANGLE CRACKED AT STA XW 33.000. INSTALLED NEW VERTICAL SUPPORT T-ANGLE IAW SRM 51-1-20, SRM 53-1-0, AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862SDR 96ZZZX2681Strap · corrodedDURING C-CHECK, FOUND LEFT WING LEADING EDGE, INBOARD SLOT AREA OUTBOARD END HAS TWO AREAS OF EXFOLIATION WITH CORROSION ON STRAP. REMOVED CORROSION, FOUND BEYOND LIMITS IAW SRM 57-3-0. FABRICATED NEW STRAP IAW SRM 57-3-0. TREATED, PRIMED, AND INSTALLED IAWApr 26, 1996 · N8969U · Doug DC862SDR IXXA9662Cover Plate · crackedDURING ROUTINE C-CHECK INSPECTION, FUEL PROBE ATTACH PLATES 9, 15, AND 17, OF THE LEFT WING WERE FOUND CRACKED. REPAIR OF THE ATTACH PLATES WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCHES 96108-1, 96108-2, AND 96108-3.Apr 24, 1996 · N728PL · Doug DC862SDR EISA96050Doubler · crackedLEFT WING INBOARD LEADING EDGE STIFFENER, ATTACHED TO LEADING EDGE RIB, HAS DOUBLER CRACKED AT LOWER FASTENER ACCESS THROUGH PANEL 6301, JUST OUTBOARD OF FORWARD BOTTLE BOLT. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM 51-40-2. (M)Apr 24, 1996 · N316NE · Boeing 727223SDR DL72S960984Stiffener · crackedFOUND ON F1 LETTER CHECK, 1.25 INCH CRACK AT L/E EDGE SPAR VERTICAL STIFFENER AFT OF NR 6 SLAT OUTBOARD TRACK OUTBOARD SIDE. REPLACED STIFFENER PER MM 57-20-21.Apr 24, 1996 · N402DA · Boeing 727232SDR CAL960606Le Splice · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SPLICE AT STA XFS 198 BETWEEN NR 3 AND NR 4 SLAT TRACK. THE AREA WAS REPAIRED IAW ECRA 5710-01726. (X)Apr 24, 1996 · N12507 · Doug DC932SDR IXXA9661Aux Spar Web · crackedDURING ROUTINE C-CHECK AND MLG ATTACH FITTING REPLACEMENT, THE LEFT AUXILIARY SPAR WEB WAS FOUND WITH LOCAL CORROSION AND CRACKS. THE WEB WAS REPLACED WITH A NEW WEB IAW DOUGLAS DRAWING 3641823-1. (X)Apr 23, 1996 · N728PL · Doug DC862SDR CALA9600654Beam · corrodedINSPECTION FOUND THE LT WING UPPER CAP TRAILING EDGE BEAM CORRODED. THE BEAM WAS REPAIRED IAW ECRA 5720-01518.Apr 23, 1996 · N68042 · Doug DC1010SDR C2XA96IA101Support Rod · wornDURING C-CHECK INSPECTION, THE INBOARD SUPPORT ROD FOR THE UPPER FLAP WELL PANEL UNDER 632BB WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ROD AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612.Apr 23, 1996 · N14821 · Aerosp ATR42320SDR W8PA960041Angle · crackedDURING C-CHECK, FOUND SUPPORT ANGLE FOR UPPER SURFACE PANEL CRACKED (INBOARD OF INBOARD-MOST SPEED BRAKE, DIRECTLY ABOVE NR 5 FLAP TRACK). REPAIRED IAW SRM 51-30-01. (X)Apr 22, 1996 · N948WP · Boeing 737301SDR AU960505Fitting · cracked(AUS) WING STRUT FITTINGS (4OFF) PNO 3-1632-1 AND PNO 3-1632-2 CRACKED IN THE CORNER OF THE RECTANGULAR HOLLOW SECTIONS - FOUND DURINGINSPECTION IAW AD/CHA/25 AND SL408 - AIRCRAFT HAS ONLY 103 HOURS TIME SINCE NEW WITH 20 HOURS OF AEROBATIC TIMEApr 19, 1996 · Bbavia 8KCABSDR UPS96820121Doubler · corrodedRT WING O/B WEDGE CORROSION DAMAGE ON LWR INNER SKIN DOUBLER. REPLACED DOUBLER PER SRM 51-1-21.Apr 18, 1996 · N880UP · Doug DC873FSDR IXXA9655Aux Spar Web · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT AUXILIARY SPAR WEB AT APPROXIMATE WS XW 97 WAS FOUND WITH LOCAL CORROSION. THE CORROSION WAS REMOVED, TREATED, AND PROTECTED IAW AIRCRAFT SRM 51-1-8. (X)Apr 16, 1996 · N728PL · Doug DC862SDR DL72S960886Stiffener · crackedFOUND ON B-1 LETTER CHECK, VERT SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK O/B SIDE. REPLACED PER M/M 57-20-21.Apr 16, 1996 · N485DA · Boeing 727232SDR DL72S960884Stiffener · crackedFOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT SPAR STIFFENER AT NR 7 O/B SLAT TRACK O/B ANGLE. REPLACED STIFFENER PER M/M 57-20-21 PG 813.Apr 16, 1996 · N485DA · Boeing 727232SDR AU960491Fitting · cracked(AUS) BOTH FORWARD WING STRUT FITTINGS PNO 3-1362-1 AND PNO 3-1632-2 CRACKED - ALL FOUR FORWARD AND REAR FITTING PIECES CRACKED - FOUND DURING DYE PENETRANT INSPECTIONApr 16, 1996 · Bbavia 8KCABSDR AALA960723Carriage Journal · corrodedATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, THE OUTBOARD CARRIAGE LARGE JOURNAL OF THE LT INBOARD FLAP WAS FOUND CORRODED. MAINTENANCE MACHINED THE OUTER DIAMETER DOWN TO 2.957 INCH AND THE INNER DIAMETER OUT TO 2.010 INCH ON THE TAPERED SECTApr 16, 1996 · N715AA · Boeing 727223SDR 96ZZZX2500Stiffener · crackedRIGHT WING INBOARD LOWER FORWARD SKIN STIFFENER CRACKED ACROSS STIFFENER. SUBMITTER STATED THIS IS THE THIRD CRACKED STIFFENER FOUND IN APRIL, 1996.Apr 16, 1996 · N302FG · Piper PA28161SDR 96ZZZM898Vent Box · crackedMCI - DURING C-CHECK, FOUND FRONT AND REAR TANGS CRACKED ON FORWARD VENT BOX, WS 629. REPAIRED PER SSRM 52-20-201.Apr 16, 1996 · N54329 · Boeing 727231SDR 96ZZZX3020Vent Tube · crackedJFK - DURING CHECK C-4D, FOUND A CRACK IN EAR ON VENT TUBE, STA 629, WS ABOVE RIB. INSTALLED AND SECURED REPAIR PER SB 727-57A159. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES.Apr 13, 1996 · N54325 · Boeing 727231SDR UPS96805984Splice Cap · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING STA 408.343 HAS 4.5 INCH CRACK JUST ABOVE RADIUS BETWEEN STR 51 AND 52. REPAIRED XW 408.343 LWR SPLICE CAP ON RT WING THAT HAD 2 CRACKS IN VERT LEG BETWEEN STR 51 AND 52 IAW UPS EO DC8-5710-8090A.Apr 12, 1996 · N803UP · Doug DC873FSDR 96ZZZX3113Jo Bolts · looseATW - DURING DV INSPECTION OF THE CENTER TANK, EVIDENCE OF LOOSE JO BOLTS WERE NOTED. UPON EVALUATION, NO CORROSION NOTED AND ALL ACCESSIBLE JO BOLTS IN CENTER TANK RIB ON AND LEFT/RIGHT WING TANK RIB 2 WERE TORQUE CHECKED TO 15. DETAILS REPORTED TO AVRO RDOApr 12, 1996 · N616AW · Bag BAE146300ASDR AALA960724Wing Chord · crackedATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, CRACKS WERE DISCOVERED IN THE VERTICAL FLANGE OF THE LBL AND RBL 70.5 WING CHORD AT FS 760.95. REPAIRS WERE ACCOMPLISHED PER SB 727-57-0112, REV B. ACFT TT: 39,457 HRS. ACFT TOTAL CYCLES: 21,587Apr 9, 1996 · N715AA · Boeing 727223SDR 9608419968Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE WING BOX FITTING AT FS 598 TO 617, LBL 50. REPLACED FITTING PER SRM 51-30-5.Apr 9, 1996 · N9332 · Doug DC931SDR AU960439Fitting · worn(AUS) WING STRUT ATTACHMENT FITTINGS (4OFF) FOUND WITH CHAFE MARKS - ALSO TWO OF THE FITTINGS HAVE SEVERAL BOLT HOLES NOT DEBURRED -FOUND DURING INSPECTION IAW AD/CHA/25 AMDT 1Apr 7, 1996 · Bbavia 8KCABSDR 96ZZZX2654Stiffener · crackedLOWER RIGHT INBOARD SKIN STIFFENER AT REAR OF WING FOUND CRACKED.Apr 6, 1996 · N84400 · Piper PA28161SDR 96ZZZX2299V-Channel · crackedV-CHANNEL CRACKED WHERE AILERON HINGE RIVETED TO IT. DIFFICULT TO SEE CRACK. SUSPECT DEFECTIVE IF MOVEMENT NOTICED WHEN PRESSURE APPLIED UPWARD TO FLAT OF AILERON LOWER SURFACE.Apr 4, 1996 · N569QL · Cessna U206SDR UPS96205951Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING AT ACCESS PANEL JUST I/B OF NR 4 K-FLAP I/B END BULKHEAD ANGLE AT LOWER END HAS NUMEROUS CRACKS AT FASTENERS. REMOVED CRACKED CHORD, FABRICATED CHORD PER SRM 57-20-2, ALODINED AND PRIMED PER SRM 51-10-2 AND IApr 3, 1996 · N915UP · Boeing 72727CSDR UPS96406061Tube · wornWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT L/E INTERIOR I/B OF PYLON NR 1 FOUND WEAR HOLE IN SUPPORT TUBE ON AISLES 1071.25. REMOVED TUBE IAW MM 20-50-03, INSTALLED BUSHINGS IAW OHM 20-50-03 AND INSTALLED NEW TUBE IAW MM 20-50-03.Apr 2, 1996 · N676UP · Boeing 747123SDR 96ZZZX3359Stiffener · crackedFOUND LOWER INBOARD WING SKIN STIFFENER ON RT WING CRACKED.Apr 2, 1996 · N4325V · Piper PA28161SDR MALA964935Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE TRANSIT/ATTACH ANGLE CRACKED APPROXIMATELY .750 INCHES AT THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-00-00 AND ARP 54-20-Apr 1, 1996 · N159MC · Swrngn SA227ACSDR DL72P960825Beam · corrosionNR 4 FLAP TRACK TO SPOILER BEAM HAS CORROSION EMANATING FROM MATING SURFACE. REMOVED CORROSION.Apr 1, 1996 · N8875Z · Boeing 727225SDR AU960539Fitting · corroded(AUS) LH STUB WING ATTACHMENT FITTING CONTAINED EXFOLIATION CORROSION - FURTHER CORROSION FOUND FOLLOWING REMOVAL OF THE FITTINGMar 30, 1996 · Cessna 402CSDR ASAA9680088Doubler · corrodedPAE - DURING 15K CHECK, CORROSION WAS FOUND ON THE INNER SKIN AT Y231 TO Y237, X PLUS 1 TO X-1, Z-50. REPAIRED PER EO 0322966M2, SRM 51-10-3 AND 53-01. (M)Mar 29, 1996 · N967AS · Doug DC982SDR UPS96205851Web · corrosionWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON SHEAR WEB BS 1131, RBL 62, WL 208. REMOVED AND REPLACED SHEAR WEB RT IAW SRM 51-30-2, 51-10-1, AND M/M 51-20-151.Mar 28, 1996 · N907UP · Boeing 72727CSDR CAL960568Former · crackedKUL - INSPECTION FOUND A 1 INCH CRACK AT XOS 1089 AND A 1.5 INCH CRACK AT XOS 759 IN LEADING EDGE FORMER. THE FORMER WAS REPAIRED IAW SRM 57-00-00, FIGURE 3. (X)Mar 28, 1996 · N68044 · Doug DC1010SDR 96FDEA00723Bracket · corrodedLT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING IS CORRODED AROUND MAIN PULLEY BOLT HOLE AND TWO OTHER AREAS ON CASTING WBL 410. REMOVED CORRODED LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING AND INSTALLED NEW CASTING IAW FEDEX MM 27-10-0,Mar 28, 1996 · N154FE · Boeing 72725SDR DL72S960683Stiffener · crackedFOUND ON D-1 LETTER CHECK, WING FRONT SPAR VERTICAL STIFFENER ANGLE CRACKED AT NR 3 SLAT O/B TRACK. REPAIRED PER M/M 57-20-21 AND ERA NBR 303369-14.Mar 27, 1996 · N8875Z · Boeing 727225SDR CAL90456Doubler · crackedHOU - INSPECTION FOUND A 2 INCH CRACK IN L/E SKIN SPLICE DOUBLER AND ANGLE CLIP JUST OUTBOARD OF LEFT WING VORTILON. A DOUBLER AND CLIP WERE INSTALLED IAW ECRA 5710-01697. (X)Mar 27, 1996 · N16521 · Doug DC932SDR 96ZZZX2791Filler · corrodedLEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 37-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002.Mar 27, 1996 · N8931E · Doug DC931SDR 96ZZZX2790Clips · corrodedLEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 57-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002.Mar 27, 1996 · N8931E · Doug DC931SDR UPS96205948Bottle Pin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FWD WING SPAR BOTTLE PIN IS CORRODED ON MATING FLANGE. REMOVED AND REPLACED RT FWD WING BOTTLE PIN PER MM 57-41-00.Mar 25, 1996 · N915UP · Boeing 72727C
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