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 TWAA9903102Angle · crackedDURING OP 15 MAINT CHECK, FOUND THE RT WING OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLES CRACKED INBD AND OTBD SIDE. THE RIB AND HINGE CASTING WAS REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01.Feb 22, 1999 · N923L · Doug DC932SDR QXEA9900531Tip · crackedYXX - RIGHT-HAND WING TIP UPPER ANCHOR NUT LAND CRACKED. REPAIRED IAW DHC-8 RD 8-57-1331, CONAIR EO 2223 AND HORIZON AIR EA 9-57-403.Feb 22, 1999 · N815PH · Dhav DHC8102SDR QXEA9900447Angle · crackedPDX - LEFT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11.Feb 22, 1999 · N823PH · Dhav DHC8102SDR AALA990393Fitting · corrodedTUL - FORWARD TRUNNION FITTING BEARING BORES CORRODED. REPLACED RMG FORWARD TRUNNION FITTING PER SRM 51-10-1. (M)Feb 22, 1999 · N893AA · Boeing 727223SDR DL72K990333Vent Box · crackedFWD VENT BOX CRACKED AT AFT EAR TO RIB STA 686.5 ATTACH PT. CUT OUT ACCESS HOLE PER MM 57-13-0, FIG 803. DRILLED AFT AND FWD ANGLE ASSY AND RADIUS FILLER. HFEC CRACK, FOUND CRACK, RUNS FROM BOLT HOLE AFT AND OUTWARD TO EDGE OF FLANGE. DRILLED RADIUS FILLERFeb 19, 1999 · N417DA · Boeing 727232SDR 99FDEA00065Angle · corrodedRT WING LWR SURFACE OF FRONT SPAR CHORD ANGLE HAS EXFOLIATED CORROSION AFT OF NR 5 L/E SLAT T DUCT. REMOVED CORROSION SPAR CHORD METAL. CORROSION BEYOND LIMITS (ORIG THICK 0.316 AFTER BLEND 0.0220). REPAIR STRAP INSTALLED ON UPPER SURFACE OF FRONT SPAR CHORFeb 17, 1999 · N288FE · Boeing 7272D4SDR AU990142Bracket · cracked(AUS) DUCKTAIL FAIRING LOCATED UNDER THE RT FLAP VIBRATING DUE TO THE ATTACHMENT BRACKET BEING CRACKED AT THE INBOARD AND OUTBOARD FORWARD ENDS. PART TC: 6,100.Feb 16, 1999 · Jetair JETSTM4101SDR CALA9900158Beam · crackedINSPECTION FOUND A .25 CRACK IN J BEAM ABOVE LT WING NR 7 SPOILER ACTUATOR. THE J BEAM WAS REMOVED IAW SRM 51-30-2. A NEW J BEAM WAS INSTALLED WITH NUT PLATE IAW SRM 51-30-2 AND 51-10-2.Feb 15, 1999 · N69741 · Boeing 727224SDR UPS99828791Doubler · crackedINSPECTION TYPE-C1, RT WING L/E LWR INTERNAL DOUBLER, JUST O/B OF THE XOLDI 6.225 RIB IS CRACKED AT THE T/E. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5669891 AND SRM 51-1-20D.Feb 14, 1999 · N811UP · Doug DC873FSDR RAIA990220Doubler · crackedSTL - RIGHT AFT WING SPAR CRACKED NEAR RIB NR 67. MAINTENANCE REPAIRED WING SPAR IAW EO NR J3200-57-012-1. (M)Feb 12, 1999 · N338TE · Bag JETSTM3201SDR DL733990278Fitting · crackedLT LANDING GEAR BEAM ATTACH FITTING CRACK IN FASTENER ATTACH HOLES. REPAIRED PER ERA 332754-14.Feb 11, 1999 · N307WA · Boeing 737347SDR RRXA991066Mount · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS OVERSIZED HOLES, NR 4 PYLON MOUNT AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH Feb 10, 1999 · N105WP · Doug DC873SDR DL72L990275Support · corrodedWING MLG SUPPORT BEAM, LT AFT ATTACH LUG, REPAIR FOR CORRODED LUG. THE AFT ATTACH LUG OF THE LT MLG SUPPORT BEAM WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG HOLE BORE AND SPOTFACING THE SURFACE OF THE LUG. THE LUG WAS REPAIRED BY INSFeb 10, 1999 · N505DA · Boeing 727232SDR DHL9974029CStiffener · corrodedAT C CHECK, FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT LOWER LEG W/S 170. REMOVED WEB, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 4 BY 6, N/R 2108.Feb 10, 1999 · N740DH · Boeing 7272Q9SDR GAIA9917Tip · unserviceableDURING SCHEDULED PHASE IN C-CHECK, A INCORRECT STATIC WICK BASE WAS FOUND INSTALLED ON THE LEFT WING TIP. DURING REMOVAL FOUR .1875 INCH FASTENERS HOLES WERE LEFT. THE DAMAGED AREA WAS REMOVED A FILLER WAS FABRICATED USING SAME MATERIAL AS REMOVED. THE FILLFeb 9, 1999 · N6811 · Boeing 727223SDR P2EA99055Web · corrodedSJO - Q-CHECK ITEM. VERTICAL PRESSURE WEB CORRODED AT WING CENTER SECTION AT BS 663. REPLACED WING CENTER SECTION SPAR VERTICAL PRESSURE WEB RIGHT SIDE ONLY BS 663, RBL 24.98 AND RBL 45.64 PER BOEING SB 737-57-10-95, REV 6 DATED 4-27-89, FIG 2. SEE COOPESA Feb 3, 1999 · N912MP · Boeing 737247SDR DHL9974005CAngle · corrodedAT C CHECK, ANGLE CRACKED AT LT WING 32 L/E SLAT WELL. REMOVED CRACKED ANGLE AND REPLACED PER SRM 51-30-2, 10 BY 5, N/R 1097.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR DHL9974004CAngle · crackedAT C CHECK, RT WING FIXED LEADING EDGE CAVITY LOWER OUTBD SUPPORT ANGLE AT FS 130.7 IS CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-3, 18 BY 1 BY 1, N/R 2072.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR DHL9974001CAngle · crackedAT C CHECK, RT FIXED LEADING EDGE CAVITY LOWER INBD SUPPORT ANGLE FSS 130.7 IS CRACKED. CUT OUT ANGLE, INSTALLED NEW SUPPORT ANGLE PER SRM 51-40-3, 9.5 BY 1 BY 1, N/R 2911.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR RRXA991069Fitting · mismanufacturedDURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 3616112-3 FITTING IS MADE FROM P/N: 3616111 7075-T6 FORGING. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AFeb 1, 1999 · N105WP · Doug DC873SDR P5CA9900182Fairing · delaminatedLEFT WING UPPER SURFACE INBOARD OF OUTBOARD AILERON TRAILING EDGE FIXED FAIRING FOUND DELAMINATED. REPAIRED PER SRM 51-40-12.Jan 29, 1999 · N854FT · Boeing 747122SDR A6WA9900031Bracket · crackedLEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)Jan 29, 1999 · N290UE · Bag BAE146200ASDR A6WA9900029Bracket · crackedLEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)Jan 27, 1999 · N290UE · Bag BAE146200ASDR EIAA990125Fitting · corrodedMZJ - DURING C-CHECK, THE LEFT MLG FITTING BRACE ATTACH LUG FACE WAS FOUND CORRODED. REPAIRED PER ECRA NR 942-57-003-2. (X)Jan 25, 1999 · N942F · Doug DC933FSDR UPS99828672Doubler · crackedINSPECTION TYPE:C3 RT, WING L/E LWR SKIN BUTT SPLICE DOUBLER HAS A 30 CRACK AT XFS 341.5. REPAIRED DOUBLER IAW DH SK713-051.Jan 23, 1999 · N713UP · Doug DC871FSDR ABXA9900116Channel · crackedLEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED AT AFT SIDE OF LANDING GEAR CUT-OUT. REPLACED CHANNEL IAW DWG 5611020 AND DC8 SRM 51-01-21.Jan 23, 1999 · N825AX · Doug DC863SDR ABXA9900092Channel · crackedLEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED, AFT SIDE OF LANDING GEAR CUTOUT. INSTALLED REPLACEMENT CHANNEL IAW DWG 5611020 AND DC8 SRM 51-1-21.Jan 23, 1999 · N825AX · Doug DC863SDR UPS99828626Web · crackedINSPECTION TYPE:C NR 2 MAIN TANK VERT WEB PREVIOUS REPAIRED CRACK HAS EXTENDED BEYOND DOUBLER AT STA XRS 23 STR 13. REPAIRED IAW DH SK 701-152 AND DH SK 701-453.Jan 22, 1999 · N701UP · Doug DC871FSDR ABXA9900127Former · crackedLEFT WING INBOARD FORMER CRACKED ABOVE DUCT AT STATION XOLD 6.225. REPAIRED DAMAGE IAW DC8 SRM.Jan 22, 1999 · N825AX · Doug DC863SDR RRXA991050Fitting · wornDURING A MAINTENANCE VISIT, FOUND WORN AREA, WING, LT I/B FLAP ATTACH FITTING AT STA 3 WORN GREATER THAN 20 PERCENT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FJan 21, 1999 · N105WP · Doug DC873SDR P2EA99060Angle · crackedSJO - RIGHT WING FRONT SPAR ANGLE CRACKED AT FSS 270. DEFECT SIZE, LENGTH .5 INCH. REPLACED RIGHT WING FRONT SPAR ANGLE AT FSS 270 PER SRM 51-10-1, PAGE 5. (M)Jan 21, 1999 · N912MP · Boeing 737247SDR AU990027Angle · cracked(AUS) FORWARD WING SPAR RIGHT AFT SPAR CAP ANGLE FOUND TO BE CRACKED IN THE AREA OUTBOARD OF THE RIGHT WING ATTACHMENT. FOUND DURING INSPECTION IAW AD/P68/45 (SB/65). PART TC: 6,062.Jan 21, 1999 · Parten P68BSDR RRXA991048Fitting · gougedDURING A MAINTENANCE VISIT, FOUND GOUGE, LT WING, CANOE FITTING, AT STA 97.906, ON OUTBD AFT EDGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR Jan 20, 1999 · N105WP · Doug DC873SDR TWAA9901308Doubler · crackedDURING CHECK-C MAINT, FOUND ONE INCH CRACK IN LT WING IN UPPER WING FUEL TANK ACCESS PLATE DOUBLER NR 1307. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 57-03 AND SRM 51-60-0.Jan 19, 1999 · N490SA · Doug DC915SDR RRXA991042Fitting · wornDURING A MAINTENANCE VISIT, FOUND ATTACH FITTING WORN, RT I/B FLAP I/B ATTACH FITTING WORN AREA IS GREATER THAN 20 PERCENT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTJan 19, 1999 · N105WP · Doug DC873SDR AU990030Angle · corroded(AUS) LEFT WING ROOT LEADING ATTACHMENT ANGLE CORRODED. FOUND DURING INVESTIGATION OF A FUEL TANK PROBLEM. PART TC: 8,168.Jan 19, 1999 · Cessna 152SDR AU990849Vortex Generator · misinstalled(AUS) VORTEX GENERATOR KIT INCORRECTLY INSTALLED.Jan 16, 1999 · Cessna 441SDR A6WA9900033Stiffener · crackedRIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)Jan 16, 1999 · N290UE · Bag BAE146200ASDR A6WA9900027Stiffener · crackedLEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)Jan 16, 1999 · N290UE · Bag BAE146200ASDR CALA9900011Angle · crackedRIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51-10-3, AND 51-10-2.Jan 13, 1999 · N14524 · Doug DC932SDR AU990012Splice · cracked(AUS) LEFT WING AFT LOWER SPLICE PLATE CRACKED APPROXIMATELY 2 MM (0.079 INCH) IN LENGTH. ALSO, THE FORWARD RIGHT ANGLE DOUBLER WAS CRACKED IN THE LOWER BEND RADIUS FOR APPROXIMATELY 25 MM (0.984 INCH). FOUND IAW AD/ROBIN/8A2. PART TC: 5,707.Jan 13, 1999 · Avions R2160SDR AALA990243Trunnion · crackedTUL - FOUND NR 1 SLAT ACT OUTBOARD TRUNNION MOUNT HAS VISABLE INDICATION OF CRACK AT TOP BOLT. REMOVED DOUBLER PLATE WITH CRACK IN IT AND INSTALLED NEW DOUBLER PER SRM 51-10-1. ALODINED AND PRIMED DOUBLER. (M)Jan 13, 1999 · N894AA · Boeing 727223SDR AALA990089Bracket · corrodedTUL - FOUND CORROSION ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET FOR NR 3 LE SLAT ACTUATOR. INSTALLED NEW MOUNT BRACKET ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET NR 3 SLAT ACTUATOR. (M)Jan 13, 1999 · N727AA · Boeing 727227SDR UPS99828514Doubler · crackedINSPECTION TYPE-C3, LT WING L/E LWR SKIN, THE INTERNAL DOUBLER AT XOLDI 6.225 IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769891 AND SRM 51-1-20D, 51-1-21.Jan 12, 1999 · N713UP · Doug DC871FSDR RRXA991037Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK, EXTENDING FROM BOLT HOLE RT I/B FLAP I/B HINGE ATTACH FITTING AT XW 3.125. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. MACHINE REPAIRED FITTING AND INSTALLED IAW FAA APPRJan 11, 1999 · N8085U · Doug DC871FSDR MWEA99029Tip · crackedFOUND CRACK AND DENT ON LEFT WING TIP. MTC PERFORMED A TEMPORARY DOUBLER REPAIR.Jan 11, 1999 · N808ME · Doug MD88SDR ASOA99022Angle · crackedDURING INSPECTION FOUND LEFT WING, RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0067, REFERENCE DATA EAC FAX SST-0251/99 AND SRM 51-00-00. (M)Jan 11, 1999 · N229AS · Emb EMB120RTSDR 99ZZZX928Support · crackedDURING A VISUAL INSPECTION OF THE WING, A CRACK WAS NOTED IN THE UPPER PORTION OF THE INBOARD WING BETWEEN THE FUSELAGE AND THE NACELLE (WS 49.0). FURTHER INVESTIGATION SHOWED THE TWO SUPPORT ANGLES THAT HOLD THE LANDING GEAR BUMPER ASSY (P/N 43016-00 AND P/NJan 11, 1999 · N132MF · Piper PA31350SDR 99ZZZX927Support · crackedDURING A VISUAL INSPECTION OF THE WING, A CRACK WAS NOTED IN THE UPPER PORTION OF THE INBOARD WING BETWEEN THE FUSELAGE AND THE NACELLE (WS 49.0). FURTHER INVESTIGATION SHOWED THE TWO SUPPORT ANGLES THAT HOLD THE LANDING GEAR BUMPER ASSY (P/N 43016-00 AND P/NJan 11, 1999 · N132MF · Piper PA31350SDR UPS99828487Clip · corrodedINSPECTION TYPE-C, FS 855 REAR SPAR IS CORRODED BEYOND LIMITS AT LBL 28. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-1-20D AND 51-3-0.Jan 9, 1999 · N701UP · Doug DC871F
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