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 95ZZZZ183Angle · corrodedDURING D-CHECK, CORROSION ON R/W FRONT SPAR LONGITUDINAL STIFFENER ANGLE JUST BELOW FUEL TANK ACCESS PLATE WS 193.0. REMOVED AND DISCARDED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9SDR COM11801Skin Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AT RIBS 15 AND 16. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17057-005, 2 EA; 120-17057-007, 1 EA; 120-17056-011, Feb 26, 1995 · N269CA · Emb EMB120RTSDR MALA954340Angle · crackedMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE INBOARD, UPPER WING SKIN TO NACELLE ATTACH ANGLE, PN 27-35112-026, CRACKED AT LT NACELLE. COMPLETED REPAIR TO THE ATTACH ANGLE IAW FAIRCHILD ARP 54-20-9101, REV B AND THE SRM. (X)Feb 23, 1995 · N27465 · Swrngn SA227ACSDR USAA950291Fitting · crackedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .25 INCH CRACK IN KEEL FITTING BELOW CENTER TANK REAR SPAR FWD OF MLG DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (W)Feb 22, 1995 · N971VJ · Doug DC931SDR 95ZZZW208Support Plate · crackedL/E BETWEEN NR 3 AND 4 ENGINE AT XFS341.500 RIB LOWER SUPPORT PLATE HAS TWO CRACKS EMANATING FROM FASTENER HOLES. REF N/R 1101 WO NR 950007.Feb 20, 1995 · N791AL · Doug DC862SDR 95FDEA00164Stiffener · corrodedMCM - LT WING FRONT SPAR STIFFENER CORRODED AND EXFOLIATED UNDER HYD LINE CLAMP STANDOFFS. LOCATED JUST OUTBD OF BOOST PUMP PRESSURE SWITCHES APPROX. FRONT SPAR STA 260. REMOVED HYD LINES LT WING F.O.M. INSTALLED SPAR STIFFENER REF EA 7-5710-3813 REV A. Feb 20, 1995 · N241FE · Boeing 727277SDR COM11800Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-O1I AT WING RIBS 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT 1327-2, 120-17056-019 (2 EA), 120-17056-017 (2 EA), 120-17056-015 (4 EA), 120-170Feb 19, 1995 · N267CA · Emb EMB120RTSDR UPS202404Angle · crackedDURING 'C' CHECK, MAINTENANCE REPORTED ATTACH ANGLES CRACKED AT WING CENTER SECTION LEFT SIDE AT STA 744. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2.Feb 16, 1995 · N907UP · Boeing 72727CSDR CAL950162Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 469. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236 AND CAL DRAWING 5720 DC8908. (Z)Feb 15, 1995 · N571PE · Boeing 727243SDR CAL950161Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 521. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236. (Z)Feb 15, 1995 · N571PE · Boeing 727243SDR 95ZZZW223Castellation · crackedMCI - DURING SPECIAL CHECK, FOUND CRACK IN CASTELLATION, EMANATING UNDER UPPER RIB, OUTBOARD SIDE IWS 555.00, AT STRINGER 18, 19 AND 20, RESPECTIVELY. REPAIRED PER DRAWING 1647070 AND TWA STANDARD PRACTICES. TOTAL CYCLES 23,012.Feb 13, 1995 · N31008 · Lkheed 10113851SDR COM11785Support · crackedTHE FOLLOWING WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERO DESIGN REPORT NR 1387-2, AT WING RIBS 15, 16 AND 18. P/N 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120Feb 10, 1995 · N268CA · Emb EMB120RTSDR 95FDEA00137Aux Spar · crackedLEFT WING AUXILIARY SPAR LOWER CHORD CRACKED AT INBD FWD (FWD OF NR 7 SPOILER FITTING). CUTOUT CRACKED LW-AUX-SPAR LWR CHORD. FABRICATED NEW CHORD AND REPAIR ANGLES AND INSTALLED PER FEDEX EA 75810-23728.Feb 10, 1995 · N284FE · Boeing 727233SDR MALA954292Doubler · wornMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT AND RT FLAP WALKING BEAM ROLLER DOUBLER WORN AT STATION WS 27.103. MAINTENANCE REPLACED LT AND RT AFT RIB DOUBLERS. (X)Feb 7, 1995 · N438MA · Swrngn SA227ACSDR DL72S950821Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER.Feb 6, 1995 · N467DA · Boeing 727232SDR DL72S950818Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813.Feb 6, 1995 · N467DA · Boeing 727232SDR COM11774Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1387-2. P/N 120-17056-019 2 EA; 120-17056-017 2 EA; 120-17056-015 1 EA; 120-17056-013 1 EA; 120-17057-Feb 5, 1995 · N259CA · Emb EMB120RTSDR COM11773Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSP TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1387.2. P/N 120-17056-015 4 EA; 120-17057-008 2 EA; 120-17056-007 1 EA; 120-17057-015 1 EA; 120-17056-013 1 Feb 3, 1995 · N261CA · Emb EMB120RTSDR ABXA9500239Tee Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER STA 58.5 TEE CAP. REPLACED TEE CAP IAW EA AD-57-03766-MR.Feb 2, 1995 · N902AX · Doug DC932SDR ABXA9500238Tee Cap · corrodedDURING C-CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER TEE CAP AT STA XCW 58.5. RIGHT WING TEE CAP WAS ALSO REPLACED DUE TO DISCREPANCIES NOTED ON THE LEFT TEE CAP IAW EA AD-57-03766-MR.Feb 2, 1995 · N902AX · Doug DC932SDR DL72S950455Stiffener · crackedFOUND ON F1 LETTER CHECK 1. 2 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK INBD ANGLE LOWER END 2. 1 .5 INCH CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK OUTBD ANGLE LOWER END, REPAIR - 1. REPLACED STIFFENER PER Jan 31, 1995 · N494DA · Boeing 727232SDR DL72S950451Stiffener · crackedFOUND ON F1 LETTER CHECK, 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 6 SLAT OUTBD TRACK INBD ANGLE LOWER END, REPAIR. INSTALLED NEW ANGLE PER M/M 57-20-21 PG 813.Jan 31, 1995 · N494DA · Boeing 727232SDR 95ZZZX882Castellation · crackedMCI - DURING SPECIAL CHECK, FOUND 1.1250 INCH CRACK IN RT WING FT CASTELLATION, STA 503, FORWARD OF STR 13. REPAIRED PER SB 093-57-207 AND REPLACED CHORD PER DWG. NR 1647070. AIRCRAFT TOTAL TIME: 59,528 HOURS; 23,327 CYCLES.Jan 31, 1995 · N11004 · Lkheed 10113851SDR COM11759Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT WING RIBS 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-17056-015, 2 EA; 120-Jan 29, 1995 · N258CA · Emb EMB120RTSDR UPS802107Support Fitting · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D.Jan 27, 1995 · N707UP · Doug DC871FSDR COM11758Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT RIBS NR 15 AND NR 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN E.O. 1327-2. P/N: 120-17056-007, 3 EA; 120-17056-015, 4 EA; 120-17056-013, 1 EA; 120-1705Jan 26, 1995 · N254CA · Emb EMB120RTSDR SWAA950087Angle · crackedDURING SCHEDULED C-2 CHECK, FOUND SUPPORT ANGLE CRACKED AT WING TO FUSELAGE TRANSITION PANEL INBOARD OF GROUND SPOILER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.Jan 25, 1995 · N53SW · Boeing 7372H4SDR AWXA9500056Strut Assy · brokenRNO-PHX - FLT 460 - ON TAKEOFF AND INITIAL CLIMB, ACFT EXPERIENCED ROLL TO RT TENDENCY, 20 DEGREES LT AILERON WAS REQUIRED TO COUNTER UNTIL APPROXIMATELY 170/180 KIAS. ACFT CONTINUED TO PHX WITHOUT FURTHER PROBLEMS. MX FOUND STRUT ASSEMBLY FOR RT WING UPPER Jan 25, 1995 · N155AW · Boeing 7373G7SDR 9501499947Trap Panel · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN LEFT AND RIGHT TRAPEZOIDAL PANEL INBOARD FITTINGS AT FASTENER HOLES. REPLACED BOTH PER BULLETIN 53-115, AC54284.Jan 22, 1995 · N8938E · Doug DC931SDR IXXA9535Fitting · crackedDURING REPLACEMENT OF LT MLG TRUNNION FITTING, INSPECTION FOUND LT SPAR CAP FITTING CRACKED. THE SPAR CAP FITTING WAS REPLACED IAW DOUGLAS INSTALLATION GUIDE, THE AIRCRAFT SRM, AND MM. (X)Jan 18, 1995 · N821BX · Doug DC871FSDR 95ZZZX4590Gap Seal · damagedLT WING, TRAILING EDGE INBOARD AT ROOT, FLAP-TO-WING GAP SEAL. INSTALLATION IAW STC SA780GL AND STC SA928GL. WHEN FLAP LOWERED, GAP SEAL WAS CRUMPLED AND JAMMED INTO GAP AREA CAUSING POSSIBLE BINDING OF FLAP. RT WING GAP SEAL CRACKED AT 7 RIVETS ALONG LENGTJan 16, 1995 · N56717 · Piper PA28180SDR COM11727Skin Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651 01I AT RIBS NR 15 AND 16, LEFT AND RIGHT WINGS, P/N 120-17056-015, 120-17056-017, 120-17056-019, 120-17057-007, 120-17056-015, 120-17056-013, 120-17056-015; 120-1705Jan 11, 1995 · N263CA · Emb EMB120RTSDR DL72W950164Uplock Frame · damagedDURING HMV, FOUND THE RT UPLOCK FRAMES AT STA 910 AND 913 HAVE TEMPORORARY REPAIRS, REPAIRED PER M/M 53-11-0.Jan 10, 1995 · N291WA · Boeing 727247SDR 9500509945Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN CENTER WING TANK FITTING XCW O, BETWEEN WING STRINGERS 17 - 18. REPLACED FITTING PER SRM 51-10-4.Jan 9, 1995 · N8925E · Doug DC931SDR DL72L950168Web · crackedDURING HMV, FOUND WEB CRACKED INSIDE LT WING L/E O/B OF NR 2 SLAT ACTUATOR. REPAIRED PER M/M 57-54-0.Jan 6, 1995 · N514DA · Boeing 727232SDR MALA954224Channel · crackedMSP - DURING SCHEDULED MAINTENANCE, THE LOWER WING SKIN FAIRING TO FUSELAGE ATTACHMENT CHANNEL (P/N 27-31110-8023), WAS FOUND TO BE CRACKED AT BL 0.00. REPAIRS WERE COMPLETED THROUGH INSTALLATION OF A CHANNEL STIFFENER IAW THE FAIRCHILD SRM. (W)Jan 4, 1995 · N442MA · Swrngn SA227ACSDR DL72S950044Stiffener Angle · crackedDURING LETTER CHECK, A 3 INCH CRACK WAS FOUND IN THE VERTICAL STIFFENER ANGLE ON THE WING FRONT SPAR ON THE OUTBOARD SIDE OF NR 3 SLAT OUTBOARD TRACK ROLLER FITTING. REPAIRED PER MM 57-20-21 PG. 813.Jan 4, 1995 · N484DA · Boeing 727232SDR C2XA95IA267Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jan 3, 1995 · N12709 · Emb EMB120RT
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