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 AT0000068Tee Cap · corrodedFOUND TEE CAP IN LT WING BETWEEN STRINGER 12 AND 17 CORRODED. FABRICATED AND INSTALLED REPAIR CLIPS IAW SB 57-98R8.Dec 20, 1999 · N824AT · Doug DC932SDR CALA9901625Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN SUPPORT ANGLE FOR BODY TO FUSELAGE FAIRING AT RT WING AFT VERY I/B T/E PANEL. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-3.Dec 16, 1999 · N33785 · Boeing 727232SDR CALA9901611Angle · corrodedINSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION, STA 760 LOWER TORQUE BOX KEEL AREA. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.Dec 16, 1999 · N33785 · Boeing 727232SDR CALA9901610Bracket · crackedINSPECTION FOUND A 3 INCH CRACK IN SUPPORT BRACKET AT LEFT WING L/E PANEL NR 6215. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232SDR USAA991392Fitting · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LEFT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED FASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M)Dec 15, 1999 · N423US · Boeing 737401SDR USAA991382Fitting · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK RIGHT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED FASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M)Dec 15, 1999 · N423US · Boeing 737401SDR MWEA99886Fitting · corrodedFOUND CORROSION AROUND TWO LOWER ATTACH BOLTS OF RIGHT MAIN LANDING GEAR TRUNNION FITTING, LOWER OUTBOARD FLANGE. MAINTENANCE REWORKED HOLES PER MIDWEST EXPRESS AND BOEING ENGINEERING INSTRUCTIONS.Dec 10, 1999 · N502ME · Doug DC932SDR AT0000040Fitting · gougedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND GOUGE IN WING LEADING EDGE FITTING XRS 111-500. BLENDED GOUGE AND NDT TESTED IAW EO 99-1406.Dec 9, 1999 · N833AT · Doug DC932SDR 20000511AP022Flap Track · corrodedRIGHT OUTBOARD MID FLAP INBOARD TRAILING EDGE FLAP TRACK CORRODED. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED RETAINER IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEL IAW 51-30-3 PAGE 2. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP017Retainer · corrodedFOUND SEAL RETAINER CHANNEL CORRODED, LOCATED AT TRAILING EDGE OF RIGHT OUTBOARD MID FLAP. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED NEW RETAINER CHANNEL IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEDec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP014Fairing · crackedFOUND .75 INCH CRACK AT TOP OF RIGHT INBOARD FLAP AFT TEARDROP FAIRING. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT TEARDROP FAIRING. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP013Fairing · crackedFOUND 1.5 INCH CRACK AT AFT MOUNT HOLE OF LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP006Strap · crackedFOUND .03125 INCH CRACK AT RIGHT WING FIXED LEADING EDGE AT AFT INBOARD END OF CUTOUT WHERE NR 5 SLAT INBOARD HOOK GOES INTO. REMOVED FASTENERS IAW 51-30-2 PAGE 1-2. STOP DRILLED CRACK IAW 51-10-1 PAGE 6. HFEC INSPECTION CONFIRMED CRACK CONTAINED IAW 51-00-Dec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP002Angle · crackedFLAP FAIRING SUPPORT ANGLE HAS 1.125 INCH CRACK AT INBOARD SIDE OF LEFT WING NR 3 FLAP TRACK BELOW AFT FALSE SPAR AREA. REMOVED FAIRING, ACCOMPLISHED HFEC INSPECTION CONFIRMED ENDS OF CRACK IAW 51-00-00 PAGE 6. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC IDec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP001Angle · crackedANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR 99T64R483EWAFitting · corrodedFOUND DURING D-CHECK, NR 3 FLAP CANOE T/E CHAFFED TRACK BOLT HOLES HAVE CORROSION EMANATING FROM THEM. REAMED HOLES TO REMOVE CORROSION. TREATED AND PRIMED. INSTALLED TWO NAS4653151-7-27 BOLTS AND ASSOCIATED HARDWARE PER EO NR 99-186 WITH APPROVED 8110-3 DADec 3, 1999 · N605AL · Doug DC873FSDR 99T64R738EWAAngle · corrodedFOUND DURING D-CHECK, ATTACH ANGLE IN FRONT OF WING LIGHT LENS CORRODED ON WING FILLET PANEL 262A RIGHT. BLENDED OUT CORROSION. FABRICATED DOUBLERS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (M)Dec 2, 1999 · N605AL · Doug DC873FSDR MWEA99863Angle · crackedLEFT WING TRAPAZOIDAL PANEL ANGLE BRACKET AT FORWARD BOTTOM CORNER WAS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW ANGLE.Dec 2, 1999 · N602ME · Doug DC932SDR AALA991846Angle · crackedTUL - RIGHT 760 CHORD ANGLE HFEC INDICATES CRACK BELOW RPR DOUBLER. INSTALLED REPAIR DOUBLER AT STATION 760 RIB CHORD ANGLE IAW SERVICE BULLETIN 727-57-0112, REV 5 AFTER CRACK STOP DRILLED. (M)Dec 1, 1999 · N875AA · Boeing 727223SDR USAA119919Bracket · chaffedRIGHT WING AFT SPAR AREA SPOILER BRACKET, FOUND AILERON CABLE CHAFFING INTO BRACKET JUST FORWARD OF INBOARD AILERON AT WING STATION 410. ACCOMPLISHED REWORK OF RIGHT WING AFT SPAR SPOILER BRACKET, P/N 65-74284-4 IAW AVITAS ENGINEERING REPAIR ORDER 99 AVHM.081Nov 29, 1999 · N924TS · Boeing 727227SDR 2000ZZZX225Fitting · unapproved partNOTE: FITTING WAS STEEL SUBMITTER STATED FITTING LOOKED HOMEMADE. INSTALLED FORGED NEW CORRECT CESSNA PART MADE FORM ALUMINUM. PART TOTAL TIME UNKNOWN.Nov 29, 1999 · N767RR · Cessna T310QSDR K4HA99093Flange · corrodedPERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND SPOTS OF CORROSION ALONG LEADING EDGE FLANGE. CORROSION DAMAGE ON INNER WING CENTER EXTENDED LEADING EDGE. LT/RT SIDE BL, WL, STRINGER, FRAME, BULKHEAD, ETC., STA XW-257000 Nov 26, 1999 · N811CK · Doug DC863FSDR COMA9960720Vane Cap · chafedTHE LEFT AND RIGHT INBOARD FLAP MOVEABLE VANE CAPS AT WS 53.60 ARE CHAFED BEYOND LIMITS. REPLACED LEFT AND RIGHT INBOARD FLAP VANE CAPS AT WS 53.60 IAW WVAC EO 601R-57-0643.Nov 26, 1999 · N951CA · Cndair CL6002B19SDR USAA991301Angle · crackedTPA - DURING A-4 CHECK, FOUND 3 INCH CRACK AT INBOARD SUPPORT ANGLE AT LT WING UNDER AILERON CLOSE OUT PANE NR Z57S. INSTALLED ANGLE, FABRICATED FROM 301 1/2 HARD .032 INCH STAINLESS STEEL PER EA 94088. (X)Nov 24, 1999 · N712US · Airbus A319112SDR 99ZZZX4623Plank · corrodedDURING NDT OF WING CLOTHESPIN FITTINGS, FOUND CORROSION ON TOP OF UPPER AFT WING PLANK. CORROSION MAY BE DUE TO HARSH AREA THAT IT IS SUBJECTED TO.Nov 24, 1999 · N928GF · Gulstm G1159BSDR GAIA99202Tube · chafedLEFT WING NR 1 TANK, VENT TUBE IS CHAFED ON LOWER SIDE. LOCATED ON TOP OF WING RIB AT WS 601.50. ACCOMPLISHED LEFT WING VENT LINE CHAFING REPAIR AT STA 601.5 IAW WITH AVITAS ENGINEERING REPAIR ORDER 99AVHM.052R0-1 RIV IR. 8110-3 DATED 7-22-99 ISSUED. REF: Nov 23, 1999 · N916PG · Boeing 727287SDR DL72W992587Stiffener · crackedA 1 INCH CRACK WING L/E SPAR STIFFENER O/B SIDE OF I/B TRACK BOX NR 4 SLAT. REPLACED SPAR STIFFENER PER MM 57-20-21.Nov 23, 1999 · N2814W · Boeing 727247SDR RRXA000309Fitting · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING FLAP STOP FITTING CRACKED AT XFS 410. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FLAP STOP FITTING IAW DC-8 SRM 51-3-0.Nov 22, 1999 · N605AL · Doug DC873FSDR K4HA99087Panel · separatedFLAP PANEL ON RT WING FOUND MISSING ON POST FLIGHT (FLAP PANEL NR 7). INSPECTED L/E FLAP AREA FOUND DAMAGE TO L/E FLAP PANEL NR 19 AND I/B LEFT AND RIGHT ROTORY ACTUATORS. REPLACED NR 19 L/E FLAP PANEL ASSY PER MM 27-81-02. REMOVED AND REPLACED LEFT AND RIGNov 20, 1999 · N709CK · Boeing 747132SDR 20000613AP007Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH PREVIOUS REPAIR ABOVE RIGHT WING NR 8 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)Nov 18, 1999 · N802EA · Boeing 727225SDR 20000615AP014Angle · crackedDURING C-CHECK, FOUND TWO RIVETS PULLING, AND .375 INCH CRACK AT DOUBLER AT LT WING LOWER FAIRING SUPPORT ANGLE AFT FALSE SPAR AREA, OUTBOARD OF NR 3 FLAP TRACK. REMOVED DOUBLER FOR CRACK AND TWO RIVETS PULLING AS PER SRM 51-30-2 PAGE 1. FABRICATED NEW DOUBLNov 13, 1999 · N802EA · Boeing 727225SDR 20000615AP013Channel · crackedDURING C-CHECK, FOUND 1.5 INCH CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT CHANNEL. INSTALLED NEW CHANNEL IAW SRM 51-30-2 PAGE 1. (M)Nov 13, 1999 · N802EA · Boeing 727225SDR 99T64R533EWAFastener · missingFOUND DURING D-CHECK. RT WING L/E ABOVE NR PYLON. ONE LOOSE FASTENER WITH SKIN WASHER, ONE FASTENER MISSING. (EO). TIGHTENED THE LOOSE FASTENER. INSTALLED NAS1670L4 JO-BOLT IN OPEN HOLE. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8Nov 13, 1999 · N8079U · Doug DC871SDR 20000615AP010Bracket · crackedDURING C-CHECK, FOUND BRACKET HAS 1 INCH CRACK WHERE RT WING NR 8 SLAT LOWER SKIN EXTENSION ATTACHES TO BOTTOM OF INBOARD TRACK. REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2 PAGE 1 AND PAGE 4. (M)Nov 12, 1999 · N802EA · Boeing 727225SDR 20000615AP009Channel · crackedDURING C-CHECK, FOUND RIGHT WING LOWER TRAILING EDGE SUPPORT INBOARD CHANNEL CRACKED APPROX 1 INCH. REPLACED CHANNEL IAW SRM 51-10-1 PAGE 4. (M)Nov 12, 1999 · N802EA · Boeing 727225SDR 20000615AP008Angle · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT ANGLE ON BOTTOM OF RIGHT WING UPPER T/E PANEL AT WEB 5 INCHES FORWARD OF INBOARD AILERON L/B LEADING EDGE. FABRICATED NEW ANGLE PER SRM 51-10-1 PAGE 4. INSTALLED ANGLE PER SRM 51-30-2 PAGE 1. (M)Nov 12, 1999 · N802EA · Boeing 727225SDR 20000615AP005Angle · crackedDURING C-CHECK, FOUND RIGHT WING RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)Nov 11, 1999 · N802EA · Boeing 727225SDR 20000613AP008Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH IMPROPER PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)Nov 11, 1999 · N802EA · Boeing 727225SDR UPS99231072Bracket · corrodedINSPECTION TYPE:C RT WING AFT SPAR AT WS 380.0 THE NR 6 T/E FLAP JACKSCREW OUTBOARD ATTACH BRACKET HAS CORROSION ON LOWER ATTACH POINT. REMOVED AND REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2.Nov 9, 1999 · N939UP · Boeing 72727CSDR CALA9901479Angle · crackedINSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01.Nov 9, 1999 · N14079 · Doug DC1030SDR 99T64R463EWAShim · crackedFOUND DURING D-CHECK, LEFT WING FRONT LOWER SPAR CAP STATION XFS 520 SHIM PLATE HAS CRACK APPROX .75 INCH. CUT OUT DOUBLER AT CRACK. FINISHED ENDS OF SHIM SMOOTH. TREATED AND PRIMED. BONDED PIECE OF SHIM IN PLACE. IT IS ACCEPTABLE TO RETURNE TO SERVICE PENov 8, 1999 · N605AL · Doug DC873FSDR 99T64R482EWAFitting · chafedFOUND DURING D-CHECK, NR 2 FLAP CANOE XW 98 T/E CHAFFED. REMOVED GOUGES BY BLENDING. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M)Nov 5, 1999 · N605AL · Doug DC873FSDR A6WA9900131Stiffener · crackedLEFT WING 10 INCHES INBOARD OF RIB 8, TOP WING SKIN STIFFENER IS CRACKED AT FORWARD END. REMOVED, REPAIRED AND INSTALLED SAID STIFFENER. REPAIRED STIFFENER IAW BAE FAX DJR/RJ0630-98 AND FOUND SERVICEABLE. (M)Nov 4, 1999 · N183US · Bag BAE146200ASDR 2000ZZZX670Tee · corrodedTHROUGH ACCESS HOLE 506C AND THROUGH INBOARD RIB CUT-OUT, INBOARD LOWER WING STR 63-72 AT STA XW.000 IN NR 3 MAIN TANK HAS CORROSION BETWEEN STRINGER. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND T-CHORD OUT OF LIMITS IAW DC-8 SRM 57-2-0. REPLACED T-CHORD INov 4, 1999 · N812TC · Doug DC8F55SDR 99T64R478EWAFitting · gougedFOUND DURING D-CHECK, NR 3 CANOE FITTING INBOARD AFT SIDE IS GOUGED. REMOVED GOUGES BY BLENDING SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/02/99. (M)Nov 3, 1999 · N605AL · Doug DC873FSDR UPS99231058Support · crackedINSPECTION TYPE:SI CRACKED, T/E UPPER PANEL SUPPORT L CHANNEL JUST ABOVE THE VERTICAL BULB, APPROX 1 FT FROM THE OB END OF THE I/B AILERON. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-20-1.Nov 2, 1999 · N950UP · Boeing 72725CSDR ASAA9980228Fitting · crackedPHX - DURING C-CHECK, FOUND CRACK ON RIGHT WING LEADING EDGE RIB FITTING AT XFS 195. REPAIRED IAW ASA EA 5740-01182. (M)Nov 2, 1999 · N967AS · Doug DC982SDR A6WA9900130Stiffener · crackedRIGHT WING 10 INCHES INBOARD OF RIB 9, TOP WING SKIN STIFFENER IS CRACKED AT FORWARD END. REMOVED, REPAIRED AND INSTALLED TOP WIN STIFFENER. REPAIR ACCOMPLISHED IAW BAE FAX-REF DJR/RJ0630-98. (M)Nov 2, 1999 · N183US · Bag BAE146200ASDR DL72S992464Stiffener · crackedFOUND DURING D1 LETTER CHECK/SHUTTLE MOD NRC 69, NR 3 L/E SLAT SPAR STIFFENER CRACKED APPROX 1.5 INCH AT INBD TRACK OUTBD STIFFENER. REPLACED SPAR STIFFENER PER M/M 57-20-21 P 813.Nov 1, 1999 · N495DA · Boeing 727232SDR 99FDEA00460Support · chaffedRIGHT WING TRAILING EDGE FLAP AFT REMOVAL FWD FAIR 635AL FOUND HINGE UNDRWING SUPPORT FITTING FWD SIDE I/B AND O/B EDGE WITH DEEP CHAFE MARK. INBD AND OTBD MATERIAL ORIG THICKNESS - 0.210 AFT BLEND-OUT, MATERIAL REMAIN - 0.096 FOR I/B & 0.168 FOR O/B. *S/D* Nov 1, 1999 · N582FE · Doug MD11F
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