JASC 5711

Service difficulty reports · 5,587

Reports filed under 5711 · Wing Spar, 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 = '5711'
  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 CKSA95160Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND OUTBOARD FLAP TOP SPAR CAP AT STATION 410 CORRODED. REPAIRED SPAR CAP IAW DC-8 SRM 57-2-0 FIGURE 2. ALODINED AND PRIMED IAW DC-8 SRM 51-1-21. INSTALLED HI-LOCKS IAW DC-8 SRM 51-1-20. REPAIRED LOWER FLAP SKIN IAW DRAWING SKADec 17, 1995 · N801CK · Doug DC855SDR CKSA95158Spar Cap · crackKOSC - DURING C-CHECK INSPECTION, FOUND LEADING EDGE STATION XFS 86 (APPROX) TOP SPAR CAP CRACKED AND CORRODED. INSTALLED REPAIR AS IT REQUIRED IAW AIA/E2119 AND DC-8 SRM 51-1-20D. (M)Dec 17, 1995 · N801CK · Doug DC855SDR GAIA9526Spar · crackedDURING C-CHECK INSPECTION, AN 4.5 INCH LONG CRACK WAS FOUND IN THE LT TOP OUTBOARD SPAR RAIL. THE CRACKED SPAR WAS REPAIRED IAW TRACOR SERVICE ENGINEERING REPORT CODE 340/440-57-50 DATED 12/11/95 AND KHAC EA CV-57-25, DATED 12-9-95. AIRCRAFT RETURNED TO SERVDec 15, 1995 · N3412 · Cvac 34031SDR DL72S954726Web · fatigueMTC REPORTS, DAMAGE TO THE REAR SPAR WEB OF THE CENTER SECTION FUEL TANK. THE DAMAGE IS LOCATED APPROXIMATELY BETWEEN LBL 17.2 AND LBL 25.5. DAMAGE REMOVAL RESULTED IN A 3 I/B - O/B BY 1 UP/DOWN CUTOUT. THE WEB IS MANUFACTURED FROM 0.375 2024-T351 MACHINED Dec 13, 1995 · N403DA · Boeing 727232SDR DL72S954662Stiffener · crackedFRONT SPAR STIFFENER, NOSE RIB ATTACH BRACKET CRACKED BETWEEN TWO LOWER FASTENERS AT NR 7 SLAT INBOARD TRACK AT APPROX IWS 588. REPLACED STIFFENER PER MM 57-20-21.Dec 8, 1995 · N475DA · Boeing 727232SDR DLL13960047Rear Spar · crackedCRACKS WERE FOUND ON THE REAR SPAR UPPER CAP AND THE UPPER WING-S IN EMANATING FROM THE BAY 8 ROW 6B FATSENER. DAMAGE FOUND WHILE ACCOMPLISHING ME-04 OF SI 7-63370-12AD.Dec 2, 1995 · N788DL · Lkheed 10113851SDR DLL10954628Spar Cap · crackedDURING ACCOMPLISHMENT OF SI 7-63370-12AD, A CRACK WAS NOTED AT HOLE NR 10A BETWEEN IWS 319.83 AND IWS 346.109 IN THE RT WING REAR SPAR UPPER CAP. THE WING SKIN IS NOT DAMAGED IN THIS LOCATION. ERA272791 AUTHORIZES INSTALLATION OF A BUSHING IN THE DISCREPANT Nov 29, 1995 · N733DS · Lkheed 10113851SDR GTIA96NK008Spar · corrodedDURING C-CHECK, FOUND LEFT AND RIGHT WING UPPER REAR SPAR CAP FLANGES AT RIGHT STATION XRS129 AND LEFT STATION XRS127.5 CORRODED. REWORKED LEFT AND RIGHT UPPER REAR SPAR CAP FLANGES IAW MCDONNELL DOUGLAS INSTRUCTION ON FILE 95-11-06-014/AJC00146 DATED NOV 8, Nov 21, 1995 · N941ML · Doug DC932SDR ABXA9600020Spar · crackedDURING 820AX C-CHECK INSPECTION, FOUND LEFT HAND WING LOWER AT STATION 69.5, HOLES 2 THROUGH 5 UNDER SKI FITTING HAVE CRACK INDICATIONS BY HFEC INSPECTION. ALL CRACKS ARE IN SPAR AND ALL CRACKS ARE ON OUTBOARD SIDE OF HOLES. REPAIRED LEFT HAND LOWER REAR SPANov 15, 1995 · N820AX · Doug DC863SDR 96ZZZM267Spar Chord · defectiveFLT NR 52 - SVMI-MDSD - THE FLIGHT ENGINEER FOUND A FUEL LEAK FROM NR 3 MAIN TANK AT THE LOWER AFT SECTION OF THE BEAVER TAIL. THE A/C WAS INSPECTED, TANK DRAINED COMPLETELY OF FUEL AND FERRIED TO MIAMI, FL. DYNAIR TECH OF FLORIDA REMOVED AND REPLACED THE RINov 14, 1995 · N707HE · Boeing 707330CSDR 95ZZZX6916Spar · corrodedAFTER FLIGHT WHILE PERFORMING ACCELERATED STALLS, 6 RIVETS WERE FOUND MISSING FROM TOP OF SPAR BETWEEN STRUT ATTACH AND THE LANDING LIGHT AREA. A HOLE WAS MADE PER CESSNA MANUAL INSTUCTIONS AND THE SPAR CAP ANGLE WAS FOUND SEVERELY CORRODED. NO ACCESS AVAILANov 13, 1995 · N6141G · Cessna 150KSDR UPS805003Spar Cap · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING I/B LOWER ANX SPAR CORRODED BEYOND LIMITS. REPLACED LT ANX SPAR PER DOUGLAS BWG 561508 AND SRM 57-1-0.Nov 10, 1995 · N729UP · Doug DC871FSDR UPS804991Spar Cap · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING I/B LOWER AUX SPAR CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANX SPAR RT WING LOWER I/B IAW DWG 5615058 AND SRM 51-1-20.Nov 10, 1995 · N729UP · Doug DC871FSDR ABXA9500942Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR UPPER CAP CORRODED AT XRS 566 TO 568. REPAIRED IAW ABX REA D957-13436-MR.Nov 8, 1995 · N951AX · Doug DC941SDR 96ZZZX81Plate · corrodedSPAR CAP ANGLE EXHIBITED INTERGRANULAR CORROSION IN SEVERAL LOCATIONS ALONG ITS LENGTH AND AFFECTED THE DOUBLER PLATE AT THE POINTS WHERE THE CORROSION CONTACTED. SUBMITTER STATED THIS INTERGRANULAR CORROSION IS DISPLAYING SIGNS OF PRESENCE IN THE LT SPAR CAPNov 7, 1995 · N6390J · Cessna 172NSDR 96ZZZX80Angle · corrodedSPAR CAP ANGLE EXHIBITED INTERGRANULAR CORROSION IN SEVERAL LOCATIONS ALONG ITS LENGTH AND AFFECTED THE DOUBLER PLATE AT THE POINTS WHERE THE CORROSION CONTACTED. SUBMITTER STATED THIS INTERGRANULAR CORROSION IS DISPLAYING SIGNS OF PRESENCE IN THE LT SPAR CAPNov 7, 1995 · N6390J · Cessna 172NSDR 96ZZZX79Angle · corrodedSPAR CAP ANGLE EXHIBITED SEVERE INNER CORROSION IN 2 LOCATIONS AND MODERATE INTERGRANULAR CORROSION IN SEVEREAL OTHER LOCATIONS. CORROSION AFFECTED THE DOUBLER PLATE WHERE THE POINT OF CORROSION CONTACTED.Nov 7, 1995 · N7598D · Cessna 172NSDR 95FDEA01623Spar · corrodedCORROSION (C53-132-02-1) WING CENTER SECTION FRONT SPAR LOWER SPAR, BS 740, RBL 35.Nov 3, 1995 · N191FE · Boeing 72722SDR DLL16954314Rear Spar · crackedDURING THE ACCOMPLISHMENT OF EO 7-59089-3 FOR THE RIGHT WING, CRACKS WERE FOUND EMANATING FROM EXISTING FASTENERS HOLES BETWEEN IWS 293.58 AND IWS 346.109. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP AT LOCATION 12A AND IN THE REAR SPAR WEB AT LOCATION 1Nov 2, 1995 · N762DA · Lkheed 10113853SDR 95ZZZX6561Spar Cap · crackedDURING A ROUTINE INSPECTION, THE LT WING LOWER SKIN WAS NOTICED CRACKED AFT OF THE LANDING GEAR TRUNNION. FURTHER INVESTIGATION BY REMOVAL OF SKIN REVEALED THE AFT SPAR WAS CRACKED. SUSPECT CAUSE, HARD LANDING. WING HAD HAD PREVIOUS DAMAGE HISTORY, FATIGUE.Nov 2, 1995 · N742WP · Piper PA60600ASDR 9522089608Spar Cap · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING REAR SPAR UPPER 'T' CAP XRS 445 TO 454. REPAIRED 'T' CAP (P/N 5911300-1), PER EA 99-102931.Nov 2, 1995 · N608NW · Doug DC932SDR 96ZZZX56Spar · crackedON INSPECTION, MAIN SPAR FOUND WITH LATERAL CRACKS 18 INCHES IN LENGTH. WING OPENED FOR RECOVER. WING HAD HIT 'POLE' IN 1956 (?) WAS IN STORAGE.Nov 1, 1995 · N11747 · Mncoup 90ASDR 96ZZZX252Spar · corrodedA STUDENT PILOT WAS CONDUCTING ROUTINE PRE-FLIGHT INSP & WITH FLAPS DOWN, HE NOTICED 2 RIVETS MISSING HEADS ON RT WING REAR SPAR NEXT TO FUSELAGE. BROUGHT PLANE INTO SHOP & INVESTIGATED. STABILIZED ACFT ON JACKS UNDER WING & FUSELAGE & DRILLED PLATE OFF THE Nov 1, 1995 · N7091W · Piper PA28180SDR 95ZZZX6747Spar · corrodedDURING REPAINT, FOUND EARLY CORROSION INSIDE SPAR CENTER SECTION, JUST FORWARD OF REAR SEATS.Nov 1, 1995 · N9900K · Piper PA28181SDR 95FDEA01638Spar Chord · corrodedBS 740, LBL 40 - 46: WING CENTER SECTION FRONT SPAR LOWER CHORD TO LOWER TANK SKIN HAS HEAVY CORROSION. RIVET HEADS SHEARED AND SKIN BULGING. REPAIR PER EA NR 7-5710-26102 DATED 10-24-95.Oct 29, 1995 · N133FE · Boeing 72725CSDR 95FDEA01634Spar Web · corrodedWING CENTER SECTION, RT SPAR LOWER PORTION OF WEB, SHOWS EVIDENCE OF BULGING AND CORROSION AT LBL 20, BS 870, WEB AND LOWER SPAR CHORD. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS, TRIPLERS AND REPAIR ANGLES PER ESO 11782 AND EA 7-5710-25952 AND 51-10-1.Oct 23, 1995 · N133FE · Boeing 72725CSDR 95FDEA01574Spar · corrosionCORROSION (C53-132-02-1/2), DETERIORATED FINISH, WING CENTER SECTION BS 870 UPPER SPAR CHORD, ENTIRE LENGTH. REMOVED CORROSION ON STA 870 UPPER SPAR CHORD, FOUND CHORD TO BE OUT OF LIMITS PER FEDEX 727 SRM (57-10-1). REMOVED AND REPLACED STA 870 UPPER CHORD Oct 20, 1995 · N188FE · Boeing 72722SDR 95FDEA01573Spar · corrodedCORROSION (C53-132-02-1/2), WING CENTER SECTION BS 920 LOWER SPAR CHORD RBL 34 TO 44. REMOVED CORROSION ON STA 870 LOWER SPAR CHORD. FOUND CHORD IS OUT OF LIMITS PER FEDEX 727 SRM 75-10-1. REMOVED AND REPLACED STA 870 LOWER CHORD PER EWO NR 95-3133 (EA NR 7Oct 20, 1995 · N188FE · Boeing 72722SDR CA951027007Spar · cracked(CAN)SUBJECT SPAR INDICATED IRREGULAR LINES ACROSS THE GRAIN AT 163 INCHES FROM THE ROOT END. FORE AND AFT SPAR FACES CLEANED AND SANDED & THE VERTICAL LINES REMAINED. PRESSURED APPLIED TO THE SPAR EACH SI DE INDICATED SLIGHT MOVEMENT. A HARD DOWNWARD PRESSUREOct 19, 1995 · Bbavia 7GCBCSDR 95ZZZX6185Spar · crackedDURING ANNUAL INSPECTION, A CRACK 3.25 INCHES LONG WAS FOUND IN LT WING REAR SPAR. THE CRACK STARTED AT FLAP PULLEY BRACKET, P/N 0460205-102, AND EXTENDED OUTBOARD, RUNNING HORIZONTALLY 3.25 INCHES. INBOARD HALF OF SPAR WAS REPLACED AND ACFT RETURNED TO SERVOct 18, 1995 · N714YE · Cessna 152SDR CAL950989Spar Cap · corrodedHOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M)Oct 17, 1995 · N17535 · Doug DC932SDR CA951030008Spar · cracked(CAN)REAR WING SPAR FOUND CRACKED AT WING STA. 123.5, AT THE OUTBOARD FLAP HANGAR.Oct 12, 1995 · Dhav DHC2MK1SDR A6WR95007Bolt · required resealDURING STRUCTURAL INSPECTION, FOUND RT WING REAR SPAR ROOT JOINT ATTACH FITTING LEAKING AT BOLT 'A'. REMOVED AND INSPECTED BOLT. RESEALED AND INSTALLED BOLT. (X)Oct 12, 1995 · N881DV · Bag BAE146200ASDR 9522049601Spar Cap · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER CAP XRS 477-509. REPAIRED CAP (P/N 5911301), PER EA 12-5720-9-C0486.Oct 12, 1995 · N601NW · Doug DC932SDR UPS204772Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON INDICATIONS ON UPPER REAR SPAR ON LT WING AT WS 571. REMOVED CORROSION IAW 57-10-1, REPAIRED SPAR IAW SRM 57-10-6.Oct 9, 1995 · N936UP · Boeing 727108CSDR UPS204764Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT WING L/E LOWER FRONT SPAR CHORD AT FSS 200. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 57-10, FRONT SPAR LOWER CHORD REPAIRED IAW UPS EO 727-57-1642.Oct 9, 1995 · N936UP · Boeing 727108CSDR ABXA9600157Spar · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING LOWER REAR SPAR HAD A PREVIOUS REPAIR BETWEEN XRS 509 AND XRS 531 WITH FURTHER DAMAGE. REPAIRED REAR SPAR IAW DC-9 SRM 57-09 FIG 11 AND ABX REA D957-13115-MR.Oct 9, 1995 · N989AX · Doug DC932SDR 96ZZZX3665Spar Fitting · corrodedFOUND LEVEL 2 CORROSION WHILE PERFORMING TASK NR C57-581-03. THE CORROSION EFFECTED A FITTING ON THE RIGHT WING REAR SPAR LOWER CHORD AT WBL 94 INCHES, AT ZONE 6-85. REPLACED FITTING AND CLEANED CHORD PER SRM 51-10. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL Oct 9, 1995 · N552NA · Boeing 7272J7SDR ABXA9600153Spar Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR SPAR LOWER VERTICAL LEG CORRODED JUST INBOARD OF THE OUTBOARD FLAP HINGE FITTING. REPAIRED LEFT WING REAR SPAR IAW ABX REA D957-13003-MR.Oct 5, 1995 · N989AX · Doug DC932SDR A6WR95005Bolt · wrong nutDURING STRUCTURAL INSPECTION, FOUND RIGHT WING REAR SPAR ROOT JOINT ATTACH FITTING BOLT 'B' HAD INCORRECT NUT INSTALLED. REPLACED WITH PROPER NUT. (X)Oct 5, 1995 · N881DV · Bag BAE146200ASDR DLL17954189Rear Spar · crackedDURING THE ACCOMPLISHMENT OF EO 7-59089-3, CRACK INDICATIONS WERE FOUND EMANATING FROM TWO FASTENER HOLES COMMON TO THE UPPER WING SKIN AND THE UPPER SPAR CAP. ACCOMPLISHED REPAIRS PER DL ERA 271961-14AD.Oct 3, 1995 · N765DA · Lkheed 10113853SDR 95ZZZX6177Spar · holes elongatedPILOT SQUAWKED THAT AT CERTAIN POWER SETTINGS AND FLIGHT ATTITUDE, THE RT WING WOULD DEMONSTRATE A SLIGHT FORE AND AFT MOVEMENT. INSPECTED WING ATTACH SHOULDER BOLTS IAW AM GEN SB 185. FOUND THE RT WING FORWARD WING SPAR BOLT HOLE ENLARGED BEYOND LIMITS. WIOct 2, 1995 · N1193A · Amrgen AG5BSDR UPS204542Spar Chord · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT LOWER BEAM SPAR CHORD HORIZONTAL FLANGE AT WING STA 228. REMOVED CORROSION AND FOUND OT OF LIMITS. CUT OUT DAMAGE AREA OF SPAR CHORD AND SHEAR TIE, FABRICATED REPAIRS AND INSTALLED PER SRM 51-30-10, 51-Sep 28, 1995 · N954UP · Boeing 727185CSDR UPS204534Spar Chord · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-01) LT WING LOWER SPAR CHORD IS CORRODED AT WS 180 TO 184 IN HEEL OF CHORD. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS, REPAIRED PER UPS E.O. B727-5710-7411-A.Sep 28, 1995 · N954UP · Boeing 727185CSDR UPS204533Spar Chord · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-02) RT WING UPPER SPAR CHORD IS CORRODED FROM WS 130 TO 224.5 AND GOING UNDER TRUNNION FITTING. REMOVED AND REPAIRED RT WING SPAR CHORD IAW UPS E.O. B727-5710-7410-A.Sep 28, 1995 · N954UP · Boeing 727185CSDR UPS204530Spar Web · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REMOVED CENTER CELL REAR SPAR WEB FOR ACCESS OF 870 TENSION STRAP. AFTER WEB REMOVAL, FOUND CORROSION ON WEB TO BE OUT OF LIMITS PER SRM 57-10-1. REPLACED BS 870 WEB PER SRM 51-30-2, 51-10-1, 51-10-2, 51-10-6, 51-30-5, 51-20Sep 28, 1995 · N954UP · Boeing 727185CSDR CAL950882Spar Web · crackedHOU - INSPECTION FOUND A 1.25 INCH CRACK IN RT WING SPAR WEB AT STA XCW 58.1. THE CRACK WAS ROUTED OUT IAW EA 5761-01003. (X)Sep 28, 1995 · N12539 · Doug DC932SDR DLL13954168Rear Spar · crackedTHE RT WING REAR SPAR WAS FOUND WITH A CRACK LOCATED AT OWS 126 (2.75 INCHES LONG). THE CRACK EXTENDS ABOVE AND BELOW A FASTENER HOLE. DURING REMOVAL OF THE ATTACHING STRUCTURE, ANOTHER 1 INCH CRACK WAS FOUND AT OWS 147. ACCOMPLISHED REPAIRS PER DL ERA 2719Sep 27, 1995 · N782DL · Lkheed 10113851SDR 95FDEA01442Spar · corrodedWHILE WORKING CUST ID NR0443, FOUND CORROSION EVIDENCE ON LT WING FRONT UPPER SPAR CHORD UPPER SURFACE AT SIX FASTENER HOLES, LES 331.7 - LES 339.7. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 57-30-4 AND EA NR 7-5710-25816. AT Sep 27, 1995 · N508FE · Boeing 72725SDR 95ZZZX6602Spar Cap · corrodedFOUND BLISTERS ON TOP, RIGHT OUTBOARD SPAR CAP AT STA 102 AND STA 94.8 DURING DAILY INSPECTION. AFTER PICKING AT BLISTERS, FOUND WHITE POWDER. CONSULTED BEECH CUSTOMER SUPPORT. REMOVED WING FROM AIRCRAFT, SEPARATED LEADING EDGE WING AND BOX WING FROM SPAR. Sep 26, 1995 · N623AW · Beech 65A90
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