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 CAL950379Web · crackedGSO - INSPECTION FOUND RIGHT WING CENTER INBOARD OF STATION 139 WITH CRACKS IN WEBBING AROUND FASTENER HOLES. THE CRACKS WERE .8 INCH IN LENGTH. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-6. (W)May 10, 1995 · N17773 · Boeing 727227SDR C2XA95IA071Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 4 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT, TT, 11,575.6, CYC, 16,520. (X)May 4, 1995 · N40717 · Emb EMB120RTSDR C2XA95IA070Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 3 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT, TT, 11,575.6, CYC, 16,520. (X)May 4, 1995 · N40717 · Emb EMB120RTSDR C2XA95IA069Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED ADN REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT, 11,575.6, CYC, 16,520. (X)May 4, 1995 · N40717 · Emb EMB120RTSDR 9507299989Trapezoid · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT TRAPEZOIDAL PANEL AT THE FIXED STRUT ATTACH POINT. REPLACED PANEL.May 2, 1995 · N8944E · Doug DC931SDR COM11877Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2 P/N: 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 1 EA; 120-17057-0Apr 30, 1995 · N152CA · Emb EMB120RTSDR ABXA9500448T Cap · corrodedDURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT LOWER T-CAP BETWEEN STRINGERS 11 TO 12, 12 TO 13, 13 TO 14 AND 14 TO 15. REPAIRED IAW DC-9 SRM 51-22-1 AND DC-9 SB 57-98.Apr 26, 1995 · N983AX · Doug DC932SDR SWIA95570Clips · crackedLEFT WING OUTBOARD OF NACELLE HAS FIVE CRACKED CLIPS. FOUR AT POSITION YA-4533.5, AND ONE AT YA-6750. FABRICATED SAME AS ORIGINAL AND INSTALLED CLIPS AT YA-4533.5 (FOUR EACH) AND YA-6750 (ONE EACH).Apr 24, 1995 · N194SW · Emb EMB120ERSDR COM11871Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED, DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N 120-17056-007, 8 EA; 120-17056-009, 1 EA; 120-17056-019, 1 EA; 120-1705Apr 24, 1995 · N156CA · Emb EMB120RTSDR 9506919762Fitting · crackedDURING LINE CHECK, FOUND CRACK IN THE RIGHT TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REPLACED FITTING PER SRM 51-30-1.Apr 24, 1995 · N762NW · Doug DC941SDR UPS402985Stiffener · corrodedWHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION INSIDE RT WLG W/W STIFFENER RUNNING FROM STA 1241 TO 1255 ON CENTERLINE WEB. REPLACED PER SRM 51-30-02.Apr 23, 1995 · N673UP · Boeing 747123FSDR UPS203066Stiffener · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK AND CORROSION ON THE STIFFENER ON THE WING CENTER SECTION REAR WEB AT STATION 870 AND LBL 33. MAINTENANCE REMOVED THE DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER PER SRM 51-30-2.Apr 23, 1995 · N904UP · Boeing 72751CSDR UPS203013Upper Chord · crackedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON UPPER CHORD, LT WING BL 760.95. INSTALLED REPAIR PER UPS EO B727-5710-1271E.Apr 23, 1995 · N921UP · Boeing 727180CSDR ABXA9500526Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 22. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3.Apr 21, 1995 · N983AX · Doug DC932SDR ABXA9500523Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 16. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3.Apr 21, 1995 · N983AX · Doug DC932SDR C2XA95IA061Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE.Apr 19, 1995 · N17728 · Emb EMB120RTSDR C2XA95IA060Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W)Apr 19, 1995 · N17728 · Emb EMB120RTSDR C2XA95IA059Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W)Apr 19, 1995 · N17728 · Emb EMB120RTSDR C2XA95IA058Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W)Apr 19, 1995 · N17728 · Emb EMB120RTSDR C2XA95IA057Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W)Apr 19, 1995 · N17728 · Emb EMB120RTSDR C2XA95IA056Bracket · crackedIAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W)Apr 19, 1995 · N17728 · Emb EMB120RTSDR COM11864Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2. P/N 120-17056-013, 2 EA, 120-17056-007, 2 EA, 120-17062-013, 1 EA, 120-17060-0Apr 17, 1995 · N1105G · Emb EMB120RTSDR 9505846305Support · crackedDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING INBOARD TRAILING EDGE LATERAL SUPPORT AT PANEL 572BB TO WS 547. STOP DRILLED AND INSTALLED DOUBLER.Apr 15, 1995 · N665US · Boeing 747451SDR C2XA95IA054Support · crackedIAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 23 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 23 IAW EMB 120 SRM 51-40-02. AIRCRAFTApr 13, 1995 · N16731 · Emb EMB120RTSDR C2XA95IA053Support · crackedIAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 24 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 24 IAW EMB 120 SRM 51-40-02. AIRCRAFTApr 13, 1995 · N16731 · Emb EMB120RTSDR C2XA95IA052Support · crackedIAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 35 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 35 IAW EMB 120 SRM 51-40-02. AIRCRAFTApr 13, 1995 · N16731 · Emb EMB120RTSDR C2XA95IA051Support · crackedIAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 25 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 25 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELApr 13, 1995 · N16731 · Emb EMB120RTSDR C2XA95IA050Support · crackedIAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 22 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 22 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELApr 13, 1995 · N16731 · Emb EMB120RTSDR C2XA95IA049Support · crackedIAH - DURING LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 34 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 34 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEAApr 13, 1995 · N16731 · Emb EMB120RTSDR COM11857Support · crackedDURING INSPECTION TASK 5720-551/650-01I AND 5720-552/652-01I THE FOLLOWING WING SKIN SUPPORTS WERE FOUND TO BE CRACKED. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N 120-17056-013, 2 EA, 120-17056-015, 4 EA, 120-17056-017, 2 EA, 120-17Apr 12, 1995 · N164D · Emb EMB120RTSDR 9506019944Doubler · crackedDURING LINE CHECK, FOUND CRACK AND CORROSION IN LEFT UPPER WING DIAMOND DOUBLER APPROXIMATELY 12 INCHES FROM FORWARD END. REPAIRED PER EA 99-097073, SEC 1.Apr 8, 1995 · N1309T · Doug DC931SDR MALA954402Angle · crackedDURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT WING TO NACELLE UPPER INBOARD ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR ANGLE AS PER ARP 54-20-9101 REVISION B. (W)Apr 7, 1995 · N160MC · Swrngn SA227ACSDR DL72S951645Beam · crackedFOUND AT HMV. UPPER T/E SUPPORT BEAM CRACKED AT NR 8 SPOILER ACTUATOR CUTOUT. REPAIRED BEAM PER MM 57-20-22 FIG 809.Apr 7, 1995 · N494DA · Boeing 727232SDR DALR950006Fitting · corrodedATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVESIZED TO CLEAN UP CORROSION PER DL ERA 270605-14. TT 38155 HRS. CYCLES, 18905. (X)Apr 6, 1995 · N311EA · Lkheed 10113851SDR UPS202916Cell Cutout · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7607 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123.Apr 5, 1995 · N926UP · Boeing 72731CSDR UPS202915Cell Cutout · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7606 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123.Apr 5, 1995 · N926UP · Boeing 72731CSDR UPS202914Cell Cutout · corrodedDURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7206 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123.Apr 5, 1995 · N926UP · Boeing 72731CSDR UPS202913Cell Cutout · corrodedDURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7202 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123.Apr 5, 1995 · N926UP · Boeing 72731CSDR UPS202912Cell Cutout · corrodedDURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7207 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER EO 727-57-1123.Apr 5, 1995 · N926UP · Boeing 72731CSDR UPS202797Forging · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION IN LT FWD BOTTLE PIN FORGING AND FITTING 740. REPLACED BUSHINGS PER UPS EO FILE NR B727-53-1548.Apr 3, 1995 · N926UP · Boeing 72731CSDR 95ZZZX4147Cleat · crackedLEFT WING TRAILING EDGE STRUCTURE BETWEEN RIBS 7 AND 8 HAS A CRACKED CLEAT ATTACHING STIFFENER TO THE REAR FALSE SPAR. REMOVED AND REPLACED CLEAT BETWEEN LEFT WING TRAILING EDGE BETWEEN RIBS 7 AND 8 IAW BAE 146-300 SRM.Apr 1, 1995 · N612AW · Bag BAE146300ASDR UPS802785Frame · crackedDURING 'C' CHECK, MAINTENANCE FOUND RT WHEELWELL DOOR CUTOUT FRAME CRACKED ON FWD I/B CORNER. REPAIRED FRAME PER SRM 57-2-0.Mar 31, 1995 · N814UP · Doug DC873FSDR ABXA9500461Doubler · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING UPPER MAIN LANDING GEAR DOUBLER CORRODED IN PREVIOUS BLENDOUTS. REPLACED RIGHT WING UPPER MAIN LANDING GEAR DOUBLER IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Mar 31, 1995 · N990AX · Doug DC941SDR 95ZZZX4148False Spar · crackedLEFT WING TRAILING EDGE FALSE SPAR HAS A 2.50 INCH CRACK AT THE INBOARD LIFT SPOILER CENTER HINGE POINT. STOP DRILLED CRACK. C/W PLATE REPAIR OVER LEFT WING TRAILING EDGE OF FALSE SPAR JUST INBOARD OF LIFT SPOILER CENTER HINGE POINT IAW REPAIR DRG HC572H9036Mar 31, 1995 · N612AW · Bag BAE146300ASDR COM11843Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-013, 1 EA; 120-170Mar 30, 1995 · N205CA · Emb EMB120RTSDR C2XA95IA046Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W)Mar 30, 1995 · N27707 · Emb EMB120RTSDR C2XA95IA045Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 2, NR 4 AND NR 5 UPPER AND LOWER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED REPLACED THE AFFECTED SUPPORTS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W)Mar 30, 1995 · N27707 · Emb EMB120RTSDR C2XA95IA044Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 3 AND NR 4 UPPER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W)Mar 30, 1995 · N27707 · Emb EMB120RTSDR C2XA95IA043Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W)Mar 30, 1995 · N27707 · Emb EMB120RTSDR C2XA95IA042Support · crackedIAH - DURNG C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. ACFT APPROVED FOR RETURN TO SERVICE. (Z)Mar 30, 1995 · N27707 · Emb EMB120RT
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