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 RRXA98170Spar Cap · misdrilledDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING, FRONT SPAR CAP AT XFS=304. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04456.Mar 16, 1998 · N865F · Doug DC863FSDR VJ9800045Spar Chord · corrodedVISUAL INSPECTION OF BLEND AREA AT XRS80 PER AIRTRAN WO 30343, CORROSION WAS NOTED IN THE BLEND AREA AND AROUND 1 FASTENER NEXT TO TO THE BLENDED AREA ON THE RIGHT WING REAR SPAR LOWER CHORD. REMOVED CORROSION IAW DC9 SRM 51-10-3, BLENDED AREA TO MINIMUM OF 1Mar 12, 1998 · N909VJ · Doug DC932SDR EIAA980156Spar · corrodedMZJ - DURING 'C4' CHECK INSPECTION, LT WING L/E OUTBOARD OF NR 1 PYLON WS 1375 FRONT SPAR LOWER CHORD VERTICAL LEG HAS AREA OF EXFOLIATION CORROSION. REPAIRED SPAR IAW EVERGREEN INTERNATIONAL AIRLINES ECRA NR 481-57-122-2. (M)Mar 12, 1998 · N481EV · Boeing 747132SDR CALA9800418Angle · corrodedINSPECTION FOUND RT WING LEADING EDGE LOWER FRONT SPAR CAP ANGLE CORRODED NINE INCHES INBOARD OF FUEL VALVE. THE CORROSION WAS REMOVED IAW SRM 51-21-00. A METAL STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0.Mar 12, 1998 · N68044 · Doug DC1010SDR CALA9800417Angle · corrodedINSPECTION FOUND CORROSION ON LEADING EDGE LOWER SPAR CAP ANGLE LOCATED ABOVE AND JUST OUTBOARD OF NR 3 ENGINE PYLON OUTBOARD SIDE. SECTION OF SACRIFICIAL DOUBLER WAS CUT OUT AND AREA WAS REPAIRED IAW DOUGLAS DRAWING 26752-6204.Mar 12, 1998 · N68044 · Doug DC1010SDR ABXA9800317Spar · crackedRIGHT WHEEL WELL AT FWD LOWER OUTBOARD END, REAR SPAR LOWER CHORD HAS NUMEROUS CRACKS. REPAIRED IAW ABX REA D857-22747 MR.Mar 11, 1998 · N814AX · Doug DC863FSDR DLL19980543Spar · crackedDURING INSPECTION OF THE LT AND RT RS UPPER CAP FASTENER HOLES PER EO 7-59089-3 SEVERAL CRACK INDICATIONS WERE FOUND ON THE SPARS. THE REAR SPAR MODIFICATION WILL NOW BE ACCOMPLSIHED ON THIS AC. THIS REPAIR DOCUMENTS THE DEVIATIONS (REPAIRS) NEEDED TO COMPLEMar 9, 1998 · N756DR · Lkheed 10113853SDR 98ZZZX1113Fitting · corrodedDURING ANNUAL INSPECTION, FOUND REAR CABIN BULKHEAD SUPPORT (PN 0811075-10) BUCKLED. UPON FURTHER DISASSEMBLY, FOUND FITTING SEVERELY CORRODED.Mar 9, 1998 · N3038R · Cessna 320ASDR AU980294Fitting · corroded(AUS) LT AND RT REAR SPAR ATTACHMENT FITTINGS P/N 62448-02 (LT) AND P/N 62448-03 (RT) CORRODED.Mar 8, 1998 · Piper PA28R201SDR TWAA9807307Spar · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 44 INDICATING CRACK IN RT WING LOWER REAR SPAR STATION XSR 155. REWORKED PER SERVICE REWORK DRAWING JO60173 AND TWS STD PRACTICES. (M)Mar 7, 1998 · N929L · Doug DC932SDR TSAA9757168Spar · corrodedDURING LAP JOINT INSPECTION, FOUND WBL 92 LEFT WING L/E SPAR LEVEL 2 CORROSION 2 INCH BY 3 INCH ARUOND BOOST PUMP ATTACHMENT TO SPAR. REMOVED CORROSION IAW 57-10-01 AND 51-10-6. LIMITS FOUND TO BE ACCEPTABLE TO BOEING. REPAIRED IAW DRAWINGS SBX-SBA-98-0010TMar 5, 1998 · N726AL · Boeing 737297SDR RRXA98193Spar · crackedDURING A MAINTENANCE VISIT, AIRCRAFT ARRIVED WITH LOG ITEM PAGE 6736-01, LEFT WING, AFT SPAR WEB CRACKED XRS=337 TO XRS=380. FABRICATED AND INSTALLED REPAIR IAW DOUGLAS SERVICE SKETCH 1635, 1628 AND SKETCH NR 97147.Mar 5, 1998 · N796AL · Doug DC863SDR CALA9800384Spar Cap · corrodedINSPECTION FOUND RT WING REAR SPAR LOWER CAP CORRODED AROUND PLATE NUTS ON UPPER SURFACE FROM STA XORS 433 TO 500. A REPAIR WAS INSTALLED IAW SRM 51-31-01.Mar 5, 1998 · N68044 · Doug DC1010SDR 98FDEA00158Spar Chord · corrodedCORROSION (C53-132-02-1/2) ON UPPER REAR SPAR CHORD BS 870, LBL 65 - RBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER REAR SPAR CHORD BS 870 LBL 65 - RBL 65 WL 178 PER FEDEX EA 7-5710-38738.Mar 5, 1998 · N105FE · Boeing 72722CSDR 98FDEA00157Spar Chord · corrodedCORROSION (C53-132-02-1/2) ON LOWER REAR SPAR CHORD BS 870, LBL 65 TO RBL 65, WL 148. *S/D* REMOVED AND REPLACED LWR SPAR CHORD BS 870 LBL 65 - RBL 65 WL 148 PER FEDEX EA 7-5710-38738.Mar 5, 1998 · N105FE · Boeing 72722CSDR AU980252Plate · cracked(AUS) WING SPAR TOP PLATE CRACKED.Mar 4, 1998 · Ayres S2RT15NORMALSDR 98ZZZX1326Rib Assy · buckledDURING PHASE INSPECTION, RIB AT LT WS 58.94 WAS FOUND BUCKLED. DAMAGE EXTENDED FROM 2.50 INCHES AFT OF MAIN SPAR AT TOP TO 7 INCHES AFT OF MAIN SPAR AT BOTTOM. SUSPECT CAUSED BY HARD LANDING. MANUFACTURER HAS BEEN CONTACTED FOR RECOMMENDATIONS.Mar 3, 1998 · N98437 · Cessna 421CSDR 9805636719Spar · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR LOWER CHORD NEAR SUPPORT FITTING AT FSS 1383. REPAIRED PER EA 67-153232.Mar 2, 1998 · N619US · Boeing 747251FSDR EIAA980145Spar Cap · corrodedMZJ - DURING 'C6' CHECK INSPECTION, RT WING LOWER SPAR CAP HAS CORROSION AT WS 934. REPAIRED IAW ECRA 478-57-084-02. (X)Feb 28, 1998 · N478EV · Boeing 747SR46SDR ABXA9800140Spar Cap · corrodedLEFT WING UPPER SKIN FRONT SPAR CAP CORRODED. REPAIRED IAW ABX REA D857-21941MR.Feb 25, 1998 · N818AX · Doug DC863FSDR CA980302004Fastener · missing(CAN) ON INSPECTION RIB TO SPAR NAILS MISSING. FABRIC REMOVED AND IT APPEARS THAT THE FRONT SPAR HAD BEEN REPLACED AND THE NAILS WERE NOT INSTALLED.Feb 23, 1998 · Bbavia 11ACSDR USAA980098Spar Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND CRACK .25 INCH LONG LT HORIZONTAL STABILIZER AT STATION 200.5 FRONT SPAR WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 55-10-5. (M)Feb 23, 1998 · N254AU · Boeing 737201SDR 98ZZZM357Spar · corrodedDURING ACCOMPLISHEMENT OF SB ATR 42-57-0044R2 AD 97-26-11, FOUND CORROSION DAMAGE ON THE LEFT WING REAR SPAR LOWER EXTRUSION FOUND OUT OF LIMITS. THE MANUFACTURE WAS CONTACTED AND A TEMPORARY REPAIR WAS PROVIDED ALLOWING TO FLY THE AIRCRAFT TO A BASE WHERE THFeb 23, 1998 · N973NA · Aerosp ATR42300SDR AALA980391Spar Chord · corrodedTUL - HEAVY CORROSION ON LOWER SPAR CHORD UNDER NR 6 SLAT AT FSS 512 - FSS 515, RT WING. INSTALLED DOUBLER REPAIR PER B727 AARD/DC 57-30-00-2. ALODINED AND PRIMED AREA PER 51-10-2 AND 51-20-14 (SRM). SEALED REPAIR PER 51-30-0 FIG 4MM. TST: 51,688 HOURS. Feb 20, 1998 · N887AA · Boeing 727223SDR AALA980355Spar · corrodedTUL - HEAVY CORROSION ON LOWER FRONT SPAR CHORD FROM FSS 358 - FSS 370 ON BOTTOM OF CHORD RT WING. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED DOUBLER REPAIR PER B727 AARD/DC 57-30-00-2. TST: 51,688 HOURS. CYCLES: 31,372. (X)Feb 18, 1998 · N887AA · Boeing 727223SDR QXEA9900532Spar · scratchedYXX - LEFT-HAND WING FORWARD SPAR UPPER AND LOWER SPAR CAP FLANGES SCRATCHED. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.Feb 15, 1998 · N815PH · Dhav DHC8102SDR EIAA980119Spar · crackedHKG - DURING C5/D CHECK INSPECTION, RT WING SPAR UPPER CHORD FSS 688 CRACK AT FASTENER HOLE. REPAIRED IAW HAECO RS 554-52-33482. (M)Feb 15, 1998 · N471EV · Boeing 747273CSDR 98ZZZX1136Spar Block · corrodedBLOCK 5 ( 4, NR 0411129) REMOVED. CHECKED INSIDE OF FRONT AND REAR SPARS. SLIGHT CORROSION FOUND. CLEANED AND PAINTED WITH ZINC CHROMATE. MOST BOLTS FROZEN INTO BLOCKS. BOLTS HAD TO BE POUNDED OR DRILLED OUT. RECOMMEND THAT BLOCKS BE REMOVED IF WINGS AREFeb 15, 1998 · N77412 · Cessna 120SDR 98ZZZX1135Spar Block · corrodedBLOCK 5 ( 4, NR 0411129) REMOVED. CHECKED INSIDE OF FRONT AND REAR SPARS. SLIGHT CORROSION FOUND. CLEANED AND PAINTED WITH ZINC CHROMATE. MOST BOLTS FROZEN INTO BLOCKS. BOLTS HAD TO BE POUNDED OR DRILLED OUT. RECOMMEND THAT BLOCKS BE REMOVED IF WINGS AREFeb 15, 1998 · N77412 · Cessna 120SDR TWAA9805907Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING AFT FLAP INBD HINGE CASTING, LOWER INBD HOLE ON REAR SPAR, HAD A CRACK INDICATION ON FACE. INSTALLED REPAIR DOUBLER PER PRINT JO60271 PER WORK SHEET MC8-AD-36. ACFT TT: 70,732 HOURS. ACFT TC: 76,937. (XFeb 14, 1998 · N991Z · Doug DC931SDR RRXA98074Spar Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE BEYOND LIMITATIONS TO RIGHT WING, AUX SPAR WEB AT STA 879 TO STA 902. AUX SPAR WEB CORROSION REMOVED MATERIAL LOSS WAS MINIMAL USING DC-8 SRM 57-2-0 FIGURE 6 SHEET 1. THE MAJOR MATERIAL REMOVED WAS AT THE EDFeb 12, 1998 · N8177U · Doug DC871FSDR ABXA9800309Spar · corrodedRIGHT WING REAR SPAR UPPER CHORD AT STATION XRS 555 HAS EXFOLIATION CORROSION. REPAIRED IAW ABX REA D857-22332.Feb 11, 1998 · N814AX · Doug DC863FSDR 98ZZZX850Spar Cap · crackedINSPECTION FOUND LOWER SPAR CAP CRACKED ON RT WING. LENGTH OF CRACK IS APPROXIMATELY 32 INCHES LOCATED IN RADIUS. A STANDARD REPAIR WILL BE ACCOMPLISHED USING FALCON SRM. TOTAL AIRCRAFT TIME, 22,326.5 HOURS. LANDINGS, 16,576. CRACK WAS DISCOVERED WHILE INFeb 11, 1998 · N218CR · Amd FALCONDSDR ABXA9800079Spar · crackedDURING MOD/D-CHECK, FOUND THE RIGHT WING LOWER REAR SPAR CRACKED 1.375 INCH LONG JUST INBOARD OF STA 164 FLAP HINGE FITTING ATTACH STUD. REPAIRED REAR SPAR IAW ABX EA 51110027002.Feb 10, 1998 · N959AX · Doug DC941SDR DLL19980335Spar · crackedDURING INSPECTION OF THE LT AND RT WING REAR SPAR UPPER CAP FASTENER HOLES PER EO 7-59089-3 SEVERAL CRACK INDICATIONS WERE FOUND ON THE RT REAR SPAR. ALL NON CRACKED HOLES WERE COLD WORKED. THE AREA WAS THEN REPETITIVELY INSPECTED. ALL COVERED BY PREVIOUS EFeb 9, 1998 · N753DA · Lkheed 10113853SDR CA980311013Spar · corroded(CAN) DURING REPLACEMENT OF LEFT AND RIGHT LOWER WING SKINS, LEVEL 2 CORROSION WAS FOUND ON THE FORWARD SPAR CAPS IN THE AREAS BEHIND BOTH LEFT AND RIGHT NACELLE FIREWALLS. THESE AREAS CANNOT BE VISUALLY INSPECTED WITHOUT REMOVAL OF THE NACELLES. LEFT SPAR CFeb 9, 1998 · Dhav DHC6300SDR RRXA98017Spar Web · crackedDURING A MAINTENANCE INSPECTION, FOUND LEFT WING REAR SPAR WEB CRACKED IN TWO (2) LOCATIONS. RECEIVED (ONE TIME FERRY FLIGHT) AUTHORIZATION FROM FAA DER HOWARD PATTERSON REF NR 98-022/014-31, TO KMCN FOR REPAIR.Feb 8, 1998 · N796AL · Doug DC863SDR 9804589947Spar Web · crackedDURING H CHECK, FOUND A CRACK IN THE UPPER AFT SPAR IN THE CENTER TANK ACROSS THE VERTICAL LEG RADIUS AT WS 58. REPAIRED PER EA 99-153041.Feb 7, 1998 · N8938E · Doug DC931SDR SWAA980108Rib · damagedDURING SCHEDULED C3 CHECK, FOUND L/E RIB AT WS 208 DAMAGED BY KRUEGER FLAP SCREW. GOUGE STARTS AT VERTICAL WEB AND CONTINUES .375 INCH ACROSS ANGLE. REPAIRED PER BOEING SRM.Feb 5, 1998 · N302SW · Boeing 7373H4SDR EIAA980113Spar · crackHKG - DURING C5/D CHECK INSPECTION, RIGHT WING FRONT SPAR CHORD HAS A FASTENER HOLE THAT IS CRACKED BEYOND LIMITS. OVERSIZED HOLE TO REMOVED CRACK AND INSTALLED NEW FASTENER IAW HAECO RS R54-52-33482. (M)Feb 5, 1998 · N471EV · Boeing 747273CSDR EIAA980318Web · corrodedHKG - DURING C5/D CHECK INSPECTION, FOUND CORROSION AT LEFT WING FRONT SPAR WEB AT FSS 998.3. TRIMMED CORROSION FROM WEB, INSTALLED DOUBLER, ANGLE AND FILLER PER HAECO R57-21-33650 AND ECRA 471-99-176-1. (M)Feb 4, 1998 · N471EV · Boeing 747273CSDR DHL9872470CSpar · corrodedAT C-CHECK, CORROSION ON LEFT WING FRONT SPAR LOWER CHORD O/B FLANGE UPPER SURFACE WS 399. REMOVED CORROSION, INSTALLED CHORD REPAIR PER AVITAS EO 98PMSI191D-1, 13 X 2.75. N/R 1024.Feb 4, 1998 · N724DH · Boeing 727228SDR EIAA98058Spar Web · corrodedHKG - DURING 'C5/D' CHECK INSPECTION, RT WING FRONT SPAR WEB AT WS 1454 HAS CORROSION. CORRODED WEB WAS TRIMMED OFF. REPAIRED BY INSTALLING REPAIR DOUBLER, ANGLE AND FILLED AS PER HAECO RS R57-21-38620. (M)Feb 2, 1998 · N471EV · Boeing 747273CSDR 98ZZZX543Cap Strap · corrodedDURING THE PROCESS OF A NON-SCHEDULED INSPECTION, THE LEFT WING UPPER SPAR CAP STRAP WAS FOUND CORRODED AROUND THE EDGES. FURTHER, NDT INSPECTION REVEALED CORROSION BETWEEN THE STRAP AND THE DOUBLER. CAUSE OF THE CORROSION COULD HAVE BEEN IMPROPER SEALING ARFeb 2, 1998 · N293S · Cessna 500CESSNASDR DLL13980286Rear Spar · crackedDURING INSPECTIONS, SEVERAL HOLES IN THE LT AND RT WING REAR SPAR UPPER CAP WERE FOUND CRACKED IN THE SKIN-TO-CAP AND CAP-TO-WEB HOLES. THE HOLES WERE OVERSIZED, COLD-WORKED, AND BUSHED. REPAIR DOUBLERS WERE INSTALLED ON THE CAP, SKIN AND WEB PER ER/A 36378Jan 30, 1998 · N784DA · Lkheed 10113851SDR AU980149Spar · corroded(AUS) LH WING FORWARD SPAR RIVETS (20OFF) CORRODED AND RIVET HEADS POPPED OFF. LH WING SPAR SEVERELY CORRODED. RH WING FORWARD SPAR RIVETS HAD RIVET HEADS POPPEDJan 30, 1998 · Cessna 182HSDR DLL14980245Spar Cap · damagedSEVERAL FASTENERS COMMON TO THE LT WING REAR SPAR UPPER CAP, WING SKIN, -250 MOD DOUBLER AND EXISTING EXTERNAL REPAIR DOUBLER WERE REMOVED PER EO 7-71199-12AD BEFORE REALIZING THE THE EO HAD BEEN SCHEDULED INCORRECTLY. HOWEVER, SOME HOLES WERE DAMAGED DURING Jan 29, 1998 · N1738D · Lkheed 1011385115SDR AU980072Web · cracked(AUS) LH AND RH SPAR WEBS CRACKED BEYOND LIMITS.Jan 29, 1998 · Bnorm BN2A26SDR AU980071Web · cracked(AUS) LH WING SPAR WEB CRACKED BEYOND LIMITS.Jan 28, 1998 · Bnorm BN2A26SDR UPS98225663Rear Spar · crackedINSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314.Jan 27, 1998 · N214UP · Boeing 7272A1
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