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 UPS98826498Angle · crackedINSPECTION TYPE:D, RIB SUPPORT ANGLE CRACKED AT RT STUB WING XFS 252.00. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 D AND 9753294.Apr 7, 1998 · N803UP · Doug DC873FSDR TWAA9805605Web · groovedSTL - DURING OP 9 MAINTENANCE CHECK, FOUND WING LEADING EDGE AREA CUTOUT FOR NR 2 LEADING EDGE SLAT DRIVE TRACK WITH A DEEP WORN GROOVE AT OUTBOARD RIB .3.75 INCH LONG. BLENDED AREA PER ARA 15082 AND SRM 51-10-3. (M)Apr 4, 1998 · N406EA · Doug DC951SDR UPS98826332Doubler · crackedINSPECTION TYPE:C LT O/B L/E SECTION O/B END, THE EXTERIOR L/E SKIN IS CKACKED AND THE INTERNAL, DOUBLER/STRAP IS ALSO CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER AND REPAIRED SKIN IAW SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Apr 2, 1998 · N867UP · Doug DC873FSDR CALA9800620Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN CURVED ANGLE INSIDE LT WING INBOARD FIXED LEADING EDGE AT STA 130. A DOUBLER WAS INSTALLED IAW SRM 51-40-3.Apr 2, 1998 · N15774 · Boeing 727227SDR UPS98826499Angle · crackedINSPECTION TYPE:D RT I/B STUB WING ATTACH ANGLE XS 240.126 LWR O/B END HAS CRACK IN RADIUS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 5739859.Apr 1, 1998 · N803UP · Doug DC873FSDR UPS98826496Doubler · crackedINSPECTION TYPE:D, LT WING IB STUB WING INNER DOUBLER AROUND SLOT PANEL CRACKED BTWN RIBS JUST OB OF SLOT PANEL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5769895. REMOVED AND REPLACED FITTING P/N 4640162- 502 IAW SRM 51-Apr 1, 1998 · N803UP · Doug DC873FSDR UPS98826328Doubler · crackedINSPECTION TYPE-C, RT I/B STUB WING DOUBLER AT STA XS230.089 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5769859 AND SRM 51-1-20D.Apr 1, 1998 · N803UP · Doug DC873FSDR UPS98826416Intercostal · crackedINSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -80, LBL 59, THE VERTICAL INTERCOSTAL IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5613785 AND SRM 51-1-20D.Mar 31, 1998 · N803UP · Doug DC873FSDR C2XA98IA096Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 7 NR 3 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS THE APPROVED FOR RETURN TO SERVICE. (M)Mar 29, 1998 · N40717 · Emb EMB120RTSDR UPS98826331Doubler · crackedINSPECTION TYPE:C RT WING L/E AT STA XFS.539.635, DIRECTLY ABOVE NR 3PYLON, THE WING DOUBLER PLATE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER AND INTERNAL DOUBLER IAW SRM 57-2-1A FIG 1.Mar 28, 1998 · N867UP · Doug DC873FSDR UPS98826442Doubler · crackedINSPECTION TYPE:C LT WING L/E SKIN DOUBLER ABOVE THE NR 1 PYLON IS CRACKED. REMOVED AND REPLACED INTERNAL AND EXTERNAL REPAIR DOUBLERS IAW SRM 57-2-1A AND 51-1-20D.Mar 27, 1998 · N867UP · Doug DC873FSDR AU980531Fastener · cracked(AUS) RT WING TOP SKIN GEAR SUPPORT RIB HI-LOCK FASTENER HEAD SHEARED. HEAD OF FASTENER ON THE LT SIDE WAS CRACKED. FURTHER, INVESTIGATION FOUND ALL REMAINING FASTENERS IN THE AREA TO HAVE VARYING DEGREES OF DISHING.Mar 26, 1998 · Airbus A320212SDR 99ZZZM500Bolts · looseFOUND LOOSE JOBOLTS AT VARIOUS LOCATIONS AT WING TANK RIB '0' AND RIB 2 LT/RT. COMPLETED LOOSE JOBOLT REPLACEMENT AT RIB 0 AND RIB 2 LT/RT PER RIL HC571H9033. NOTE, 6 POSITIONS WERE OVERSIZED.Mar 26, 1998 · N609AW · Bag BAE146200ASDR 99FDEA00322Splice · crackedN0337 - DURING A/C P-F CONVERSION AT OAN, FOUND A CRACK IN THE SPLICE PLATE P/N ARB0012-502 AT RT WING, XORS=372. REPAIR REQUIRES CUT OUT OF DAMAGED SPLICE PLATE AND INSTALLATION OF A 7075T8 REPAIR STRAP IAW EA NR 8-5711-39534.Mar 25, 1998 · N387FE · Doug DC1010SDR ARWA980308Wingtip · damagedON RAMP, WHILE BEING MANSHALLED INTO THE RAMP, THE LEFT WING TIP MADE CONTACT WITH ANOTHER AIRCRAFT. TEMPORARY REPAIR ACCOMPLISHED IAW MM 6 PAR 5-1 TO FLY A/C BACK TO MIAMI. REMOVED AND REPLACED DAMAGED WING TIP IAW SRM 51-30-00.Mar 24, 1998 · N802BN · Doug DC862SDR P5CA9800570Stiffener · corrosionLEVEL 1 CORROSION ON RT WING GEAR STA 1350 STIFFENER. REPAIRED CORROSION PER SRM 51-10-01.Mar 23, 1998 · N857FT · Boeing 747132SDR CA980331018Bracket · burnt(CAN) ON ATTEMPT TO START NR 1 ENGINE, THERE WAS NO ROTATION. THE SUPPORT BRACKET WHICH WAS USED FOR THE STARTER/GENERATOR GROUND LEAD WAS FOUND BURNED THROUGH. IT WAS BURNED AT THE HI-LOCKS AND WAS LOOSE. INCIDENT REPORTED TO ATR SUPPORT FOR FURTHER INVESTMar 23, 1998 · Aerosp ATR42300SDR DL72S980620Stiffener · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK IN LOWER END OF L/E SPAR STIFFENER NR 2 SLAT O/B TRACK, INBD STIFFENER. REPAIRED PER MM 57-20-21.Mar 20, 1998 · N406DA · Boeing 727232SDR CALA9800561Angle · crackedINSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.Mar 20, 1998 · N73751 · Boeing 727227SDR CALA9800560Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN J-ANGLE SUPPORT ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. A REPAIR CHANNEL WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914.Mar 20, 1998 · N73751 · Boeing 727227SDR CALA9800557Angle · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT BOLT HOLES OF LT WING LOWER LEADING EDGE SUPPORT ANGLE AT FS 120. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.Mar 20, 1998 · N73751 · Boeing 727227SDR CALA9800556Stiffener · crackedINSPECTION FOUND A .625 INCH CRACK IN STIFFENER AT BOTTOM OF LT WING LEADING EDGE RIB, WBL 92.0. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.Mar 20, 1998 · N73751 · Boeing 727227SDR CALA9800553Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL SUPPORT T-ANGLE. THE CRACK WAS LOCATED AT INBOARD AFT END, OUTBOARD OF NR 1 FLAP JACKSCREW. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-Mar 20, 1998 · N73751 · Boeing 727227SDR CALA9800527Angle · crackedINSPECTION FOUND A 2 CRACK IN LOWER LEADING EDGE SUPPORT ANGLE INSIDE LT WING LEADING EDGE AFT OF NR 3 LEADING EDGE FLAP AREA, FSS 120. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.Mar 19, 1998 · N73751 · Boeing 727227SDR CALA9800525Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN BRACKET AT OUTBOARD SIDE WHERE LT WING NR 1 SLAT LOWER SKIN ATTACHES TO INBOARD TRACK. THE BRACKET WAS REPLACED IAW SRM 51-10-1.Mar 19, 1998 · N73751 · Boeing 727227SDR CALA9800521Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN DOUBLER ANGLE INSIDE LT WING LEADING EDGE AT RIB, WS 330. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-03 AND 51-30-02.Mar 19, 1998 · N73751 · Boeing 727227SDR 99ZZZM564Stiffener · crackedLEFT WING TE TOP SKIN, TWO STIFFENERS CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0626-0000). REPAIRED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0627-002) Mar 19, 1998 · N609AW · Bag BAE146200ASDR UF6A980326Tip · damagedCWA - FOUND DAMAGE TO RIGHT HAND FORWARD WING TIP HALF. MAINTENANCE REMOVED RIGHT HAND FORWARD WING TIP. INSPECTED STRUCTURE BEHIND WING TIP. NO DEFECTS NOTED. INSTALLED NEW WING TIP. ACFT T: 13,209 HOURS. (X)Mar 18, 1998 · N854AW · Bag ATPSDR 99ZZZM567Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT AFT END BETWEEN RIBS 3/4. REMOVED AND REPLACED STIFFENER. (M)Mar 18, 1998 · N609AW · Bag BAE146200ASDR CALA9800469Stiffener · crackedINSPECTION FOUND A .1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A REPAIR WAS INSTALLED IAW SRM 51-14-1.Mar 17, 1998 · N17410 · Boeing 727243SDR CALA9800465Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075.Mar 16, 1998 · N17410 · Boeing 727243SDR ABXA9800237Tee Cap · corrodedLEFT AUX TANK TEE CAP CORRODED AT WING STA XFS 45.00 TO XFS 107.50. REPAIRED IAW REA D857-21955 MR.Mar 16, 1998 · N815AX · Doug DC863FSDR AALA980508Bracket · corrodedTUL - KRUEGER FLAP BRACKET EXFOLIATED AT LOWR OUTBOARD MOUNT BORE, OUTBOARD MOUNT PAD AND FLAP TO ARM ATTACH POINT. INSTALLED NEW MOUNT PER MM 27-87-11, OPS CHECK OK. (M)Mar 16, 1998 · N14061 · Airbus A300B4605RSDR 99ZZZM499Bolts · loosePERFORM RIL HC571H9033 LT RIB 2 OUTBOARD JOBOLTS. PERFORMED RIL HC571H9033 ON LEFT RIB 2 OUTBOARD JOBOLTS. (M)Mar 16, 1998 · N609AW · Bag BAE146200ASDR MWEA98365Vane · chafedFOUND 2 CHAFE MARKS ON LEADING EDGE OF RIGHT WING MIDDLE FIXED VANE. MAINTENANCE REPAIRED FIXED VAN BY BLENDING CHAFE MARKS.Mar 15, 1998 · N600ME · Doug DC914SDR MWEA98364Vane · chafedFOUND CHAFE MARK ON RIGHT WING INBOARD FIXED VANE LEADING EDGE. MAINTENANCE BLENDED MARK.Mar 15, 1998 · N600ME · Doug DC914SDR 99ZZZM568Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN 7/8. (M)Mar 14, 1998 · N609AW · Bag BAE146200ASDR 99ZZZM487Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 (OUTBOARD STIFFENER). REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 7/8. (M)Mar 14, 1998 · N609AW · Bag BAE146200ASDR 98FDEA00197Aux Spar · crackedAUX SPAR IS CRACKED, FWD OF NR 8 SPOILER FITTING. *S/D* REPAIRED AUX SPAR CHORD FWD OF NR 8 SPOILER FITTING, ALL WORK DONE IAW FED-EX EA 7-5710-38120.Mar 14, 1998 · N489FE · Boeing 727227SDR UPS98826440Fitting · corrodedINSPECTION TYPE:C/CK CORROSION ON CENTER WING SPAR FITTING FUSELAGE STATION 855 INSIDE LEFT HAND WHEEL WELL BELOW UPPER CORNER. REMOVED CLIP, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 57 2 3, THIS CLIP INSTALLED WITH -3 DOUBLER AFTER CORROSION REMOVAL IAW DCMar 13, 1998 · N836UP · Doug DC873FSDR UPS98826429Clip · corrodedINSPECTION TYPE-C, CORROSION ON CENTER WING SPAR FITTINGS FS 855 INSIDE LT W/W BELOW UPPER CORNER. REMOVED CLIP, DRILLED AND INSTALLED IAW DC8 SRM 57-2-3.Mar 13, 1998 · N836UP · Doug DC873FSDR CALA9800439Splice · crackedINSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2.Mar 13, 1998 · N17410 · Boeing 727243SDR CALA9800438Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 8405. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 51-10-2, AND 51-30-2.Mar 13, 1998 · N17410 · Boeing 727243SDR CALA9800437Angle · crackedINSPECTION FOUND A .5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.Mar 13, 1998 · N17410 · Boeing 727243SDR 99ZZZM489False Spar · crackedRIGHT WING TE FALSE SPAR CRACKED JUST INBOARD OF INBOARD LIFT SPOILER JACK. REPAIRED PER FAX JM/RJ0240-98, PER DRAWING HC572H9036. OPPOSITE HAND TO DRAWING. (M)Mar 13, 1998 · N609AW · Bag BAE146200ASDR UPS98826131Doubler · crackedINSPECTION TYPE-C, LT WING LWR SKIN DOUBLER ON NR 2 ENG STUB WING JUST FWD OF CUTOUT IS CRACKED. REMOVED DOUBLER AND STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 1A.Mar 12, 1998 · N813UP · Doug DC873FSDR RRXA98169Fitting · chafedDURING A MAINTENANCE VISIT, FOUND LEFT WING CANOE FITTING CHAFED AT STA 97.9. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04453.Mar 12, 1998 · N865F · Doug DC863FSDR CALA9800419Doubler · corrodedINSPECTION FOUND CORROSION ON RT WING LOWER LEADING EDGE SACRIFICIAL DOUBLER JUST INSIDE PANEL NR 617 AB FRONT SPAR AREA. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-21-01 AND ECRA 5720-0164Mar 12, 1998 · N68044 · Doug DC1010SDR MWEA98343Web · crackedCENTER FUEL TANK WEB AT XCW 20 LEFT SIDE WAS FOUND WITH PIECE MISSING. FABRICATED AND INSTALLED REPAIR DOUBLER.Mar 11, 1998 · N212ME · Doug DC932SDR DL72W980556Aux Spar · chafedMLG AUX SPAR CHAFED AT INBD FWD END LT SIDE. REPAIRED PER MM 57-43-0 P 801.Mar 11, 1998 · N2815W · Boeing 727247
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