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 2000ZZZM214Spar · crackedFOUND DURING C-CHECK, A 4.75 INCH CORROSION CRACK APPROX STATION XCW 31 LEFT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK. REMOVED, TREATED AND PRIMED. FILLED SEALER CONTINUED THE INSTALLATION OF LOWER FRONG SPAR CAOct 29, 1999 · N812TC · Doug DC8F55SDR UIEA9994Spar Web · corrosionWING CENTER SECTION, BS 1241 REAR SPAR WEB CORROSION. CORROSION REMOVED FROM WEB AND REWORKED, THIS IS AN APPROVED ALTERNATE METHOD OF COMPLIANCE REF 8110-3. (M)Oct 19, 1999 · N505MC · Boeing 7472D3BSDR UIEA9991Spar Web · crackedRIGHT WING MID SPAR UPPER CHORD FOUND WEB CRACKS. INDICATIONS VERIFIED USING HFEC INSPECTION, BETWEEN MSS 563.24 AND 592.45. AT MSS 575 THE WEB AT THE TWO CRACKED FASTENER HOLES WERE TRIMMED OUT AND A PERMANENT REPAIR WAS ACCOMPLISHED USING FILLERS, A DOUBLEOct 19, 1999 · N505MC · Boeing 7472D3BSDR QXEA9902243Spar · damagedPDX - LEFT WING INBOARD FORWARD SPAR INBOARD END HAS SMALL FRETTING DAMAGE TO END. REPAIRED IAW RD 8-57-811, STEPS 5 THROUGH 7.Oct 14, 1999 · N827PH · Dhav DHC8102SDR QXEA9902235Angle · gougedPDX - UPPER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613CR ATTACHMENT. REPAIRED IAW DHC-8-100 M/M 20-32-02.Oct 13, 1999 · N827PH · Dhav DHC8102SDR AT9900810Spar Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT WING AFT SPAR UPPER CAP AT XRS 387-400. FABRICATED AND INSTALLED REPAIR STRAP AT XRS 387-400 IAW DC9 SRM 57-09 FIG 12, 51-10-03, 51-30, AND EO 99-1344.Oct 12, 1999 · N846AT · Doug DC932SDR DL733992235Spar · gougedTHE RIGHT WING REAR SPAR WAS GOUGED AT THE MLG BEAM AFT ATTACH FITTING. THE DAMAGE WAS REPAIRED AT MV PER ER/A 333653-14.Oct 8, 1999 · N313WA · Boeing 737347SDR 9904826635Spar Web · crackedDURING M-CHECK, FOUND CRACK IN MID SPAR WEB INSIDE TANK. REPAIRED PER EA 66-168400.Oct 8, 1999 · N635US · Boeing 747227BSDR MWEA99662Spar · gougedLEFT WING AILERON TRAILING EDGE SPAR HAS PUNCTURE AND GOUGE. BLENDED GOUGE FABRICATED AND INSTALLED NEW ANGLE.Oct 4, 1999 · N302ME · Doug DC932SDR DL72E992202Spar · misdrilledONE FASTENER HOLE WAS MISDRILLED AND ELONGATED IN THE WING CENTER SECTION REAR SPAR WEB AT APPROXIMATELY LBL 41 DURING THE ACCOMPLISHMENT OF A MODIFICATION TO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333636-14AD.Oct 4, 1999 · N282WA · Boeing 727247SDR DL72S992211Spar Web · crackedCENTER WING, REAR SPAR, WEB LBL 17, CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A .5 TYPICAL CRACK NEAR THE UPPER SPAR CAP. THE CRACK IS TYPICAL OF BAC S/B 727-57A0182. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLEROct 3, 1999 · N416DA · Boeing 727232SDR ABXA9900730Spar · corrodedRIGHT WING FORWARD SPAR HAD CORROSION DAMAGE FROM XFS 207 TO 255. REPAIRED IAW ABX REA D857-32981MR.Sep 29, 1999 · N818AX · Doug DC863SDR 99ZZZX4370Spar · corrodedDURING MAINTENANCE C-CHECK, BEJ FOUND SEVERE CORROSION ON THE REAR SURFACE OF VERTICAL LEG OF THE LEFT WING REAR SPAR UPPER CHORD AT WS 550, WS 520, AND WS 444.Sep 29, 1999 · N602FF · Boeing 747124SDR 9904836635Spar Web · corrodedDURING M-CHECK, FOUND CORROSION ON FRONT SPAR LOWER CHORD. REPAIRED PER EA 66-167487.Sep 28, 1999 · N635US · Boeing 747227BSDR CA991209023Spar Cap · corroded(CAN) DURING A ROUTINE ULTRASONIC INSPECTION AS PER CF83-23, SPAR CAP INSPECTION, A DEFECT WAS DETECTED BEHIND AN INTACT HINGE TANG IN THE UPPER SPAR CAP AREA. UPON FURTHER INVESTIGATION OF THE DEFECTIVE SECTION IT WAS NOTED THE CORROSION HAD ORIGINATED FROM Sep 23, 1999 · Dhav DHC2*SDR UPS99230753Spar · corrodedINSPECTION TYPE:C, CORROSION (C57-562-02.00E-01) AT LT WING STA 525 UPPER SPAR CHORD. REMOVED AND REPLACED SPAR (UPPER CHORD) IAW BFG ER 99-5890 (UPS FILE NR 727-57-2118).Sep 22, 1999 · N935UP · Boeing 7271A7CSDR MZZA99217Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION OWAS FOUND ON LEFT WING FRONT SPAR WEB ABOVE FUEL BYPASS VALVE ACTUATOR. THE DAMAGED AREA WAS BLENDED OUT AND REPAIRED PER CMI EC/RA NR 5710-01978. (M)Sep 22, 1999 · N15781 · Boeing 727232SDR MZZA99213Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD VERTICAL LEG AT FSS 401. THE CORRODED SECTION WAS CLEANED UP AND REPAIRED PER CMI EC/RA NR 5710-01975. (M)Sep 22, 1999 · N15781 · Boeing 727232SDR 9904589963Spar Web · crackedDURING M CHECK, A .75 INCH CRACK WAS FOUND ON THE WINGS REAR SPAR WEB AT WS XRS144. THE CRACK EMANATED FROM A FASTENER HOLE COMMON TO THE END FASTENER OF THE AUXILIARY SPAR LOWER ANGLE. THE TRIM OUT WAS 1.25 WIDTH BY 2.5 LENGTH. INSTALLED .080 STEEL DOUBLERSep 22, 1999 · N913RW · Doug DC931SDR TWAA9915907Spar · crackedDURING OP 16 MAINT CHECK, FOUND LEFT WING HAD CRACK APPROX 1 INCH LONG AT LOWER I/B HOLE ON FACE OF REAR SPAR AT I/B FLAP HINGE AREA, 5 O'CLOCK POSITION. STOP DRILLED CRACK PER DWG JO60271. REPAIRED LT WING REAR SPAR AT I/B FLAP HINGE AREA PER DOUGLAS PRINT Sep 20, 1999 · N983Z · Doug DC931SDR UPS99230638Spar · crackedINSPECTION TYPE:N/A, LT WING AFT FALSE SPAR LWR. CAP CRACKED BELOW I/B GROUND SPOILER ACTUATOR SUPPORT BRACKET AT TERMINATING END. DAMAGE APROX 1.25 INCHES IN LENGTH. *S/D* REPAIRED CRACK PER UPS EO B727-5750-11867-A, PARA 6A. CRACK STOP DRILLED IAW SRM 5Sep 19, 1999 · N925UP · Boeing 72731CSDR EIA990281Skin · corrodedTLV - SWELLING ON RIGHT WING UPPER SKIN, UPPER SURFACE ABOVE FRONT SPAR AT WS 1360. PERFORMED REPAIR PER EO MF-MAN-B47-57-88838 NEW REF BOEING SERVICE ENGINEERING MESSAGE M-7200-99-07260 DATED AUGUST 16, 1999. INSTALLED DOUBLER. (M)Sep 17, 1999 · N3203Y · Boeing 747128SDR EIA990277Spar Web · crackedTLV - DURING THE ACCOMPLISHMENT OF THE TERMINATING OF THE SB 747-57A2266 REV 6 CRACK FOUND AT FASTENER HOLES IN THE FRONT SPAR WEB STATION 660, COMMON TO THE LOWER CHORD. PERFORMED REPAIR IAW IAI EO MF MAN B47-57-88849 AND AS APPROVED BY FAA REPAIR 8110-3 ATTSep 17, 1999 · N3203Y · Boeing 747128SDR AALA991437Spar · corrodedTUL - FOUND CORROSION ON LOWER SPAR CHORD BELOW NR 6 SLAT ACTUATOR. INSTALLED REPAIR STRAP IAW AARD 57-30-00-2 PAGES 1-3. (M)Sep 17, 1999 · N870AA · Boeing 727223SDR 99ZZZX4622Spar · crackedINTERNAL CORROSION AND CRACKS ON MAIN WING SPAR. INDICATIONS WERE FOUND ON RADIOGRAPHIC VIEWS. REFERENCE AD 75-27-09 R2 COPY OF INSPECTION.Sep 16, 1999 · N954 · Beech H18SDR QXEA9901993Spar · scratchedYXX - SEVERAL TOOLING SCRATCHES ON THE LEFT-HAND WING SPAR CAP LEADING EDGE UPPER ATTACH AREA. REPAIRED IAW RD 8-57-119.Sep 14, 1999 · N352PH · Dhav DHC8202SDR 9904491162Rib · crackedDURING M-CHECK, FOUND CRACK IN RIGHT WING LEADING EDGE RIB AT WS XW344 RIGHT. REPAIRED PER EA 11-167483.Sep 14, 1999 · N162US · Doug DC1040SDR ABXA9900707Spar Cap · crackedDURING C-CHECK, FOUND RIGHT WING AFT LOWER SPAR CRACKED AT HOLE NR 4. REPAIRED IAW DC9 SERVICE REWORK DRAWING J060123 AND ABX DRAWING M07181.Sep 10, 1999 · N938AX · Doug DC931SDR ABXA9900706Spar Cap · crackedDURING C-CHECK, FOUND RIGHT WING LOWER SPAR CRACKED. REPAIRED IAW DC9 DRAWINGS M07181 AND J060173.Sep 10, 1999 · N938AX · Doug DC931SDR 2000ZZZX24Spar · corrodedSJO - REPAIRED LEFT WING FRONT SPAR LOWER CHORD PLATE LEADING EDGE BETWEEN FSS 124 AND FSS 152 DUE TO WEAR AND CORROSION IAW COOPESA EO COO-2-57-549-99 DATED 9-22-99, AND, BOEING FAX NR COO-5J0-99-00306 H, DATED 9-22-99, AND BOEING FAX NR M-7200-99-08778 DATEDSep 7, 1999 · N901PG · Boeing 727260SDR AU990880Spar · cracked(AUS) WING SPAR WEB CRACKED IN THE AREA BETWEEN STRINGER NR 14 CUT-OUT AND THE ADJACENT TRIM CABLE CUT-OUT. CRACK LENGTH 1.016 MM (0.040 INCH).Sep 2, 1999 · Frchld SA227DCSDR 2000ZZZM242Spar · corrodedDURNG C-CHECK INSPECTION, FOUND THE FOLLOWING, RIGHT WING HAS CORROSION DAMAGE ON REAR SPAR AT STATINO XRS 763. REPAIRED CORROSION DAMAGE AT RIGHT WING XRS 763 IAW FINE AIRLINES EA NR G5711-01:00. SEMAN EO NR 990083 AND BOEING MESSAGE SEU-LIM-99-00023H. (M)Sep 2, 1999 · N29UA · Doug DC861SDR UIEA99068Spar Web · crackedRIGHT WING FUEL TANK INTERIOR WS 382 TO WS 411 MID SPAR AFT UPPER WEB SURFACE FOUND CRACK PROPAGATING FROM EXISTING REPAIR. MID SPAR WEB CRACK AT MSS 400 WAS TRIMMED OUT AND A PERMANENT REPAIR INSTALLED. AT MSS 394 A FREEZE PLUG WAS INSTALLED COMMON TO THE WAug 31, 1999 · N509MC · Boeing 747230BSDR UIEA99067Spar Web · crackedLEFT WING MID SPAR AND UPPER CHORD, FASTENER HOLES ELONGATED AND CRACKED. ALSO, EXISTING REPAIR DOUBLER FASTENER HOLE CHIPPED FROM WS 400 TO WS 385. AT 12 HOLE LOCATIONS BETWEEN WS 388 AND 407 OVERSIZE HI-LOCKS WERE INSTALLED AND AT ONE LOCATION SEPARATE FREAug 31, 1999 · N509MC · Boeing 747230BSDR UIEA99066Spar Web · corrosionLEFT WING FRONT SPAR WEB CORRODED BETWEEN FSSO 1314 TO FSSO 1322. TRIMMED OUT CORRODED AREAS, NDT WEB NO CRACK INDICATION. REPAIRED IAW BOEING TELEXS. (M)Aug 31, 1999 · N509MC · Boeing 747230BSDR 2000ZZZM231Spar · crackedDURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVICE ENGINEERING FAX FAS-MIA-99-0010RR AND SRO8570012 PER FINE AIR EA G5710-02, 00. (M)Aug 31, 1999 · N426FB · Doug DC8F54SDR 9904156636Spar · crackedDURING M CHECK, FOUND CRACK AT FASTENER HOLES 127 AND 129 ON RIGHT WING MID SPAR. REPAIRED PER EA 66-168597.Aug 23, 1999 · N636US · Boeing 747251BSDR 9904146614Spar · corrodedDURING L CHECK, FOUND CORROSION ON LEFT WING FRONT SPAR LOWER CHORD TO PLANK AT WS 1390. REPAIRED PER EA 66-169480.Aug 22, 1999 · N614US · Boeing 747251BSDR UPS99230830Spar Chord · corrodedINSPECTION TYPE:SI CORROSION C57-581-03.00E-02 ON R/W AFT UPPER SPAR CHORD AT WBL 85.0. REMOVED DAMAGED SECTION OF CHORD INSTALLED NEW SECTION OF REAR SPAR CHORD IAW ER NR 99-6007.Aug 20, 1999 · N951UP · Boeing 72725CSDR RRXA991628Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW DAug 20, 1999 · N8087U · Doug DC871FSDR RRXA991439Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW DC8 Aug 20, 1999 · N8087U · Doug DC871FSDR MZZA99170Front Spar · corrosionTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 6 INCH BY 1.5 INCH AREA CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 551 AND FSS 557. THE CORRODED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5710-0196Aug 18, 1999 · N79743 · Boeing 727224SDR MZZA99168Chord Plate · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 1.28 INCH AREA CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 513 AND FSS 516. THE CORODED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5710-0196Aug 18, 1999 · N79743 · Boeing 727224SDR MALA976558Spar · crackedDURING HEAVY CHECK INSPECTION, CRACK FOUND AT WS 142 REAR SPAR. MAINTENANCE REPAIRED WITH GENERIC EO NR S57007 IAW SRM 57-80-10.Aug 16, 1999 · N76XJ · Saab SF340ASDR MALA976547Spar · crackedDURING HEAVY CHECK INSPECTION AND WHILE PERFORMING EO AD990417-02, NOTED REAR SPAR CRACK AT FLAP WS 142. MAINTENANCE REPAIRED IAW EO S57007.Aug 13, 1999 · N46XJ · Saab SF340ASDR ABXA9900676Frame · crackedDURING C-CHECK, FOUND LEFT MAIN FRAME AT STATION 718 CRACKED IN THE FORWARD AND AFT POCKETS. INSTALLED DOUBLERS IAW DACO SERVICE BULLETIN 53-100 AND DACO DWG 5934375.Aug 13, 1999 · N981AX · Doug DC932SDR 99ZZZX3443Rivets · shearedDURING AN ANNUAL INSPECTION, THE RT AFT ATTACH FITTING, UNDER THE AFT BAGGAGE FLOOR, WAS FOUND TO HAVE SEVERAL MISSING RIVETS AND THE PLATE WAS MISALIGNED WITH THE FITTING ASSY. THE RIVETS THAT WERE STILL IN THE HOLES WERE ALL SHEARED. THE LT ATTACH WAS INSPAug 13, 1999 · N5850P · Piper PA24250SDR SMPA99002Spar · corrodedPPG - DISCOVERED SEVERE CORROSION ON RT WING MAIN SPAR CAPS DURING AD 94-08-10, AND SP NR 57 INSPECTION. CORROSION WAS FOUND ON BOTH LOWER FORWARD AND AFT SPAR CAPS. THE FORWARD SPAR CAP IS CORRODED IN WING BAY STA 197.5 TO 210.0. THE AFT SPAR CAP CORROSIONAug 6, 1999 · N711AS · Dhav DHC6200SDR SMPA99001Spar · corrodedPPG - RIGHT WING WAS INSPECTED IAW AD 94-08-10 AND EMMA SP NR 57, MAIN SPAR CAP INSP FOR CORROSION. A SPOT OF CORROSION WAS FOUND ON THE LOWER FORWARD SPAR CAP CENTERED AT WS 57. THE DAMAGE MEASURED APPROX 2.5 INCHES IN LENGTH BY 0.2 INCH WIDE AT MAX DEPTH OAug 6, 1999 · N719AS · Dhav DHC6200SDR 99ZZZX3094Spar · crackedWHILE C/W AD 98-05-04 INSPECTING WING SPARS FOR CRACKS, FOUND A CRACK ON THE RT FORWARD INBOARD SPAR ATTACH POINT. THE CRACK PROTRUDED OUT FROM UNDERNEATH A PLYWOOD DOUBLER ABOUT 2 INCHES. INSTALLED NEW WINGS WITH METAL SPARS FROM CHAMPION AIRCRAFT.Aug 5, 1999 · N36233 · Bbavia 7GCBC
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