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 ABXA9800754Doubler · corrodedRIGHT WING LEADING EDGE AT INBOARD UNDER WING FUEL ADAPTER, XFS 354.000, INTERNAL DOUBLER HAS SEVERE CORROSION. REPAIRED IAW DACO DWG 5641253 AND DC8 SRM 51-1-20 AND 51-1-21.Jul 25, 1998 · N803AX · Doug DC862SDR UPS98827398Fitting · crackedINSPECTION TYPE:C RT WING T/E AT STA 98.00, THE REAR SPAR VERTICAL STIFFNER FITTING WHICH TIES TO THE FLAP CYCLINDER FITTING IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3643319 AND SRM 51-1-20D.Jul 24, 1998 · N715UP · Doug DC871FSDR UPS98827397Fitting · crackedINSPECTION TYPE:C RT AUX SPAR AREA, THE REAR SPAR TO AUX SPAR LWR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DHC SK 715-421 AND DWG 5642205.Jul 24, 1998 · N715UP · Doug DC871FSDR DL72S981535Stiffener · crackedREPLACED SPAR STIFFENER PER M/M 57-20-21.Jul 23, 1998 · N515DA · Boeing 727232SDR SWAA981469Beam · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED RT MAIN LANDING GEAR BEAM FITTING. REPAIRED PER BOEING SRM.Jul 22, 1998 · N671SW · Boeing 7373G7SDR DL72L981542Doubler · crackedRIGHT WING LEADING EDGE FILLET PANEL DOUBLER CRACKED. REMOVED FILLET PANEL AND REPLACED DOUBLER PER SRM 51-40-3. REINSTALLED PANEL.Jul 22, 1998 · N501DA · Boeing 727232SDR SCNA98532Fitting · corrodedDURING HEAVY CHECK, DEEP PITTING CORROSION WAS DISCOVERED ON THE FRONT SPAR, ON THE LEFT WING, FOOTSTOOL FITTING ATTACH HOLES NR 4 AND NR 6 (AROUND HOLES ON FORWARD FACE). REPAIRED PER BCAG FAX DATED 6/30/98, ACTION NR 373025 AND DWGS SBX SBA 98 0170TR, 0177Jul 21, 1998 · N152SY · Doug DC1015SDR 99ZZZM587Stiffener · crackedLT WING TOP SKIN TE SHROUD OUTBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPAIRED ABOVE STIFFENER PER BAE FAX JM/RJO317/97 USING 2 024T3 .050. (M)Jul 20, 1998 · N611AW · Bag BAE146300ASDR SCNA98530Tip · dentedDURING HEAVY CHECK, THE LEFT WING TIP WAS FOUND TO HAVE SEVEN DENTS, ALL LOCATED AT THE RIBS, ALL AT A VERTICLE LENGTH OF 1 AND A DEPTH OF .075 TO .020 ALL ARE SMOOTH WITHOUT CRACKS. REMOVED AND REPAIRED LEFT AND WINGTIP IAW SRM 571000 FIG 39, REINSTALLED Jul 18, 1998 · N152SY · Doug DC1015SDR AU980951Seal · iced(AUS) AILERONS BINDING. FAULT WAS TRACED TO ICE FORMING BETWEEN THE GAP SEALS AND THE AILERON.Jul 17, 1998 · Piper PA34200TSDR CALA9801253Bracket · crackedINSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF LT WING SUPPORT BRACKET, XRS 332. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-1, 51-10-2, 51-10-2A, AND 51-10-3.Jul 15, 1998 · N18544 · Doug DC932SDR CALA9801251Clip · crackedINSPECTION FOUND RT WING LEADING EDGE RIB CLIP CRACKED JUST INBOARD OF WS XOS 429. THE CRACK WAS STOP DRILLED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.Jul 15, 1998 · N18544 · Doug DC932SDR ABXA9800619Shield · crackedWHILE COMPLYING WITH C-CHECK FOUND A CRACKED HEAT SHIELD IN THE RIGHT WING NR 1 LEADING EDGE SECTION. REPAIRED IAW ABX REA NR D957-24148.Jul 14, 1998 · N927AX · Doug DC915SDR SWAA981372Angle · wornDURING SCHEDULED 1/2D CHECK, FOUND PYLON SUPPORT ANGLE FOR PANEL WORN JUST BELOW HYD LINES NR 3 JACKSCREW CANOE FAIRING. REMOVED AND REPLACED PER BOEING MM.Jul 13, 1998 · N698SW · Boeing 7373Q8SDR SWAA981371Channel · crackedDURING SCHEDULED 1/2D CHECK, FOUND U CHANNEL SUPPORT FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM.Jul 13, 1998 · N698SW · Boeing 7373Q8SDR SWAA981370Strap · crackedDURING SCHEDULED 1/2D CHECK, FOUND STRAP FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM.Jul 13, 1998 · N698SW · Boeing 7373Q8SDR DHL9872161DAngle · corrodedAT D-CHECK, RT WING UPPER SURFACE BULGED AT REAR SPAR UPPER CHORD ANGLE WS 294. REMOVED UPPER CHORD RIGHT WING FROM STA 70.5 TO 348 AND REPLACED PER AVITAS EO 98PMSI233RO-Z. N/R 2564.Jul 13, 1998 · N721DH · Boeing 727228SDR DHL9872118DAngle · corrodedAT D-CHECK, WING TIP LOWER FWD ATTACH ANGLE CORRODED IN SEVERAL PLACES. REMOVED ATTACH ANGLE AND REPLACED PER SRM 51-30-2. N/R 1399.Jul 13, 1998 · N721DH · Boeing 727228SDR DHL9872117DAngle · corrodedAT D-CHECK, WING TIP LOWER FWD ATTACH ANGLE CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. N/R 1399.Jul 13, 1998 · N721DH · Boeing 727228SDR P2EA98141Stiffener · crackedSJO - C-CHECK ITEM - RIGHT WING L/E CAVITY WBL 321. FSS 395, STIFFENER CRACKED. DEFECT SIZE L=0.950 INCH. REPLACED CRACKED ANGLE AT FRONT SPAR, BS 395 PER SRM 51-10-1 PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. L1-0616-6-40, VAM 100 NR 289. (X)Jul 12, 1998 · N204AU · Boeing 737247SDR DHL9872149DStiffener · crackedAT D-CHECK, RT WING REAR SPAR VERT STIFFENER CRACKED WS 621. REMOVED VERTICAL STIFFENER, FABRICATED NEW STIFFENER PER SRM 57-10-2, 12 X 2 X 2. N/R 2557.Jul 12, 1998 · N721DH · Boeing 727228SDR DHL9872140DStiffener · crackedAT D-CHECK, LT WING ROOT ACCESS THRU PANEL 6302 VERTICAL STIFFENER BETWEEN FWD WING BOTTLE PIN CASTING AND ANIT-ICING DUCT SECTION CRACK. STOP DRILLED CRACK, INSTALLED DOUBLER 7 X 3 PER SRM 51-40-3. N/R 3147.Jul 12, 1998 · N721DH · Boeing 727228SDR DHL9872113DBracket · crackedAT D-CHECK, L/W LOWER TRAILING EDGE PANEL SUPPORT BRACKET CRACKED AT I/B SIDE OF NR 6 SPOILER ACTUTOR CASTING. REPLACED BRACKET PER SRM 51-10-1. N/R 1385.Jul 12, 1998 · N721DH · Boeing 727228SDR CALA9801291Beam · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE FLAP CORE AREA J BEAM JUST FORWARD OF NR 7 SPOILER CASTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914, 51-10-2, AND 51-30-2.Jul 12, 1998 · N17773 · Boeing 727227SDR DHL9872153DHeat Shield · damagedAT D-CHECK, RIGHT WING FIXED L/E INTERIOR HEAT SHIELD IS DAMAGED AT FWD END. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 57-30-4, 3.5 X 4.5. N/R 2464.Jul 10, 1998 · N721DH · Boeing 727228SDR DHL9872152DBracket · crackedAT D-CHECK, RIGHT WING BELOW NR 12 SPOILER PANEL COVE SUPPORT BRACKET CRACKED WS 505. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. N/R 2509.Jul 10, 1998 · N721DH · Boeing 727228SDR DHL9872121DWeb · crackedAT D-CHECK, RT WING FIXED L/E INTERIOR VERTICAL WEB AT WBL 92.8 IS CRACKED AT AFT LOWER ATTACH BOLTS. STOP DRILLED END OF CRACK. INSPECT STOP DRILL, INSTALLED WEB REPAIR PER SRM 51-40-2, 3 X 6. N/R 3454.Jul 10, 1998 · N721DH · Boeing 727228SDR DHL9872116DTip · chafedAT D-CHECK, LT WING TIP AFT OUTER FAIRING SECTION FWD CROSS RIB IS CHAFED WITH WORN OFF RIVET HEADS AND SECTION OF RIB MISSING ON AFT SIDE. REMOVED AND REPLACED WEB SECTION PER SRM 51-10-1, 10 X 6. N/R 1290.Jul 10, 1998 · N721DH · Boeing 727228SDR 99ZZZM593Angle · crackedRIGHT WING TE LOWER SKIN, INBOARD STIFFENER BETWEEN RIBS 8/9 TAG ANGLE CRACKED AFT END OF STIFFENER. REPLACED SAID TAG ANGLE AND FOUND SERVICEABLE. (M)Jul 9, 1998 · N611AW · Bag BAE146300ASDR AU980895Splice · misinstalled(AUS) LOWER SPAR SPLICE PLATES LOCATED AT W420 TRANSPOSED FRONT TO REAR. SHARP EDGES MARKED THE BULKHEAD. PERSONNEL/MAINTENANCE ERROR.Jul 7, 1998 · Amtr RV4SDR 98FDEA00454Chord · corrodedSTA-PAE - LOWER CHORD AT BS 740 IS CORRODED AT RBL 13 TO RBL 20. COMPLIED WITH EA 7-5710-39850 ACCESS BLENDED AND TREATED CORROSION ON LOWER CHORD 740, RBL 13 - RBL 20. RESTORED AREA IAW ER 98-2645.Jul 2, 1998 · N193FE · Boeing 72722SDR DL72W981379Beam · chafedMLG CHAFFING FWD SIDE OF MLG BEAM BELOW STR 18A. REPAIR PER M/M 57-43-0.Jul 1, 1998 · N2821W · Boeing 727247SDR CALA9801201Brackets · crackedINSPECTION FOUND LT WING LEADING EDGE FRAMES HAD CRACKED BRACKETS BETWEEN STA 383 AND 370, BETWEEN STA 414 AND 426, STA 506, AND STA 551. THE CRACKS WERE .25 TO .5 INCH LONG. THE CRACKED BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAJul 1, 1998 · N18544 · Doug DC932SDR CALA9801199Strap · crackedINSPECTION FOUND A 9/16 CRACK IN STRAP AT LT WING LOWER TRAILING EDGE AT OUTBOARD SIDE OF NR 3 FLAP TRACK MOUNT PAD AFT OF FALSE SPAR AREA. THE CRACKED AREA WAS REMOVED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-4Jul 1, 1998 · N17773 · Boeing 727227SDR AU981198Fitting · cracked(AUS) RIGHT WING SPAR FITTING CRACKED AND CORRODED. PART TC: 12,500.Jul 1, 1998 · Cessna 310RSDR AU981197Fitting · cracked(AUS) RIGHT WING SPAR FITTING CRACKED AND CORRODED. PART TC: 12,500.Jul 1, 1998 · Cessna 310RSDR P2EA98123Angle · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-50-5325C, A CRACK WAS NOTED ON AN ANGLE LOCATED ON THE WING CENTER SECTION AT LBL 52.5. THE CRACK WAS 1.5 INCH IN LENGTH. REPAIRED ANGLE AT WING CENTER SECTION BETWEEN BS 575 AND 615, LBL 52, IAJun 30, 1998 · N208AU · Boeing 737222SDR ABXA9800600Fitting · crackedCRACK IN LOWER NR 2 MAIN TANK JUST INBOARD OF XRS 74 STRINGER NR 51 ON FWD AND AFT SIDE OF SPLICE. REPAIRED TWO CRACKED FITTINGS IAW DC8 SRM'S 51-1-24, 51-1-8, AND 51-1-20D.Jun 30, 1998 · N853AX · Doug DC861SDR TWAA9810714Splice · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING 10 INCHES OTBD OF INBD END OF NR 3 SLAT, LE OF WING SPLICE PLATE, CRACKED. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW PART, DRILLED IN, INSTALLED AD RIVETS AND TENSION HI LOCKS PER SRM 51-30-0 PG 1. Jun 29, 1998 · N998R · Doug DC932SDR AU980850Strut · corroded(AUS) LEFT WING STRUT LINK ATTACHMENT FLANGES CONTAINED EXFOLIATION CORROSION. PART TOTAL CYCLES: 21,550.Jun 29, 1998 · Dhav DHC6300SDR ABXA9800670Strap · crackedRIGHT WING LEADING EDGE AT STATION XFS 610.000, UPPER RIB TRAILING EDGE STRAP IS CRACKED. REPLACED STRAP IAW DWG 5655441 AND DC8 SRM 51-1-21A.Jun 27, 1998 · N849AX · Doug DC861FSDR UPS98827160Doubler · corrodedINSPECTION TYPE-C, RT WING L/E LWR SKIN INTERNAL DOUBLER WS XFS347.75 TO 354.0 AND 379.0 TO 385.25 HAS HEAVY EXFOLIATION CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG NR 5641253 AND SRM 51-1-20D.Jun 26, 1998 · N708UP · Doug DC871FSDR UPS98827110Tripler · crackedINSPECTION TYPE:C, RT WING L/E LWR SKIN, THE INTERNAL TRIPLER AT THE I/B END OF THE O/ B SLOT IS CRACKED AT STA XOLDI 6.225. REMOVED, FABRICATED AND REPLACED TRIPLER IAW DWG 5769891 AND SRM 51-1-20D.Jun 26, 1998 · N708UP · Doug DC871FSDR DL72S981328Beam · chafedMLG STRUT DOOR CHAFING ON MLG BEAM 4 FEET I/B OF MLG STRUT. REPAIRED PER MM 57-43-0 PG 801.Jun 23, 1998 · N8873Z · Boeing 727225SDR ABXA9800716Angle · crackedRIGHT WING LEADING EDGE AT STATION XFS 766.250, THE INTERNAL DOUBLER ANGLE FORWARD OF ACCESS HOLE HAS A 5 CRACK. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.Jun 23, 1998 · N849AX · Doug DC861FSDR CALA9801133Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT RT WING REFUELING STATION. THE CRACK WAS ROUTED OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5730-01564.Jun 19, 1998 · N12538 · Doug DC932SDR AALA981228Bulkhead · crackedTUL - LEFT WING TIP BULKHEAD CRACKED, UPPER FLANGE AT 3 RIVETS, OUTBOARD SIDE PANEL VENT BOX. REPAIRED LT BULKHEAD UPPER FLAGNE CRACKS AT 3 RIVETS PER SRM 51-40-2 PAGE 3. (M)Jun 19, 1998 · N728AA · Boeing 727227SDR USAA980276Former · crackedCLT - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 10 INCH CRACK IN ANGLE FORMER RT WING L/E AT W STATION 219. INSTALLED MODIFIED PART. (M)Jun 18, 1998 · N231US · Boeing 7372Q9SDR B4MR98084Mount · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING NR 5 KRUEGER FLAP CENTER HINGE MOUNT DAMAGED. REPAIRED CENTER HINGE MOUNT IAW AIA EDR NR B2-05608 REF: AIA SKETCH E/2726. C-CHECK CARD NUMBER 1C-57. NON-ROUTINE TASK CARD NUMBER 115171. AMERICAN INTERNATIONAJun 18, 1998 · N504MG · Boeing 727191SDR RRXA98239Structure · damagedEXTENSIVE DAMAGE TO LEFT WING EXTENDED LEADING EDGE INTO NR 1 ALT FUEL TANK. AIRCRAFT STRUCK BY GROUND HANDLERS FORK LIFT. AIRCRAFT FERRIED FROM KMSP TO KGSO.Jun 17, 1998 · N950R · Doug DC863
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