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 CA000801003Spar · cracked(CAN) DURING INSPECTION OF WING FOLLOWING WIND DAMAGE, CRACK FOUND IN UPPER EDGE OF LEFT REAR SPAR, OUTBOARD OF STRUT ATTACH PLY PLATES. SPAR REPLACED.Jul 17, 2000 · Bbavia 11ACSDR AALA20001188Spar · corrodedTUL - FORWARD LOWER SPAR CORD HAS INTERGRANULAR CORROSION BELOW NR 3 LEADING EDGE FLAP ACTUATOR SUPPORT STRUCTURE. INSTALLED REPAIR PER ESO 11697 DATED 7-7-00. (X)Jul 14, 2000 · N731AA · Boeing 727227SDR DLL19001304Spar Cap · crackedWHILE ACCOMPLISHING REPETITIVE INSPECTIONS OF PREVIOUSLY OVERSIZED AND BUSHED HOLES IN THE UPPER SPAR CAP OF THE RT WING BETWEEN IWS 319 & 346, ADDITIONAL HOLE DAMAGE AND CRACK INDICATIONS WERE FOUND. ALL HOLES WERE OVERSIZED TO REMOVE DAMAGE/CRACKS. BUSHEDJul 7, 2000 · N764DA · Lkheed 10113853SDR RRXA10688Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE LEFT HAND WHEEL WELL BETWEEN TRAPEZOID AND REAR SPAR OF CENTER WING ON INBOARD AND OUTBOARD LEGS AT STA 1392 AND LBL 118.2, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DCJul 6, 2000 · N68042 · Doug DC1010FSDR 20001208AP002Spar Cap · crackedDURING AN INSPECTION OF THE PYLON FOUND FORWARD SPAR CRACK AT STATION XFS 550. REPAIRED FORWARD PYLON IAW DOUGLAS DRAWING NR 5802712. (M)Jul 6, 2000 · N426FB · Doug DC8F54SDR CA000824018Spar · wrong part(CAN) PART IS STAMPED WITH P/N C6WM1147-27 BUT IS NOT THIS PART.Jul 5, 2000 · Dhav DHC6SDR RRXA003004Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E I/B BOTTOM #5 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D Jun 30, 2000 · N997GE · Doug DC871FSDR COMA0010207Spar Cap · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 191-01Z, THE LEFT WING AUX SPAR UPPER CAP WAS FOUND TO BE CHAFED BY FAIRING 191. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR #SST-1567-/00.Jun 28, 2000 · N259CA · Emb EMB120RTSDR UPS00833007Spar Cap · corrodedINSPECTION TYPE: C1 RT WING AUX. TANK SPAR UPPER CAP IS CORRODED BEYOND LIMITS BETWEEN XFS 107.5 AND XFS 126.25 REPAIRED SPAR CAP I.A.W. SRM. 57-2-1 FIG. 36.Jun 25, 2000 · N772UP · Doug DC871FSDR AT0000441Spar Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT OUTBOARD LOWER SPAR CAP CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW DC9 SRM 57-09 FIG 11 AND 51-10-03.Jun 23, 2000 · N817AT · Doug DC932SDR AT0000353Spar · corrodedFOUND RIGHT HAND OUTBOARD LOWER SPAR CAP WAS CORRODED. REMOVED CORROSION, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 57-09 FIGURE 11, 51-10-3.Jun 23, 2000 · N817AT · Doug DC932SDR WX0A00001Spar · crackedFAT - DURING ACCOMPLISHMENT OF CARD 4027 .5 INCH CRACK DETECTED AT RIGHT WING REAR SPAR LOWER CAP AT THE NR 2 FLAP HINGE ATTACH BRACKET. AIRCRAFT FERRIED TO MHV FOR REPAIRS. INSTALLED TEMPORARY REPAIR KIT IAW SB A57-146, REV 3, DATED 1-30-89, AND DRAWING J06Jun 22, 2000 · N410EA · Doug DC951SDR 20001128AP001Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AFT FLANGE AT THREE LOCATIONS, STATIONS ORS 433, 451 AND 455. FOUND CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-007 AND BOEING TLX ALI-FCO 00-0244H DTD 10 APR 00. RELEASED AIRCJun 21, 2000 · N141WE · Doug DC1040SDR 20001127AP011Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR CAP AFT TANG UPPER SURFACE BETWEEN STATION XORS 917 TO 885. FOUND CORROSION BLENDED OUT IAW EO CH-00-012 AND BOEING TLX CAC-FCO- 00-00006H DATED 17, APR 00, AND SRM VOL 2 CHAPTER 51-21-02. RELEASED AIRCJun 21, 2000 · N141WE · Doug DC1040SDR 20000717SH009Spar Cap · corrodedUPON REMOVAL OF RT INBOARD LEADING EDGE FUEL CELL FOR REPAIRS OF A FUEL LEAK, FOUND THERE WAS PITTING CORROSION IN THE UPPER SURFACE OF THE LOWER INBOARD SPAR CAP CASTING. (INSPECTION OF THE LEFT WING CASTING SHOWED NO DEFECTS). SUBMITTER STATED IT APPEARS TJun 20, 2000 · N302NC · Beech 300BEECHSDR DL72K001176Spar · crackedTHE WING CENTER SECTION REAR SPAR WEB WAS FOUND WITH 2 SMALL .25 INCH CRACKS JUST BELOW THE UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF BAC S/B 727-57A0182 AND AD 97-25-15 AND WERE LOCATED AT RBL 5 AND LBL 15. THE CRACKS WERE ROUTED OUT OF THE WEB AND REPAIJun 18, 2000 · N496DA · Boeing 727232SDR 20000615SH001Spar · corrodedFORWARD LOWER EDGE OF MAIN SPAR INBOARD BEHIND FUEL TANK BADLY CORRODED. DEFOLIATED BY ABOUT 50 PERCENT OF THICKNESS. MICE NESTS AND FECAL MATTER FOUND. SUBMITTER RECOMMENDED FUEL TANK REMOVAL FOR INSPECTION AT LEAST EVERY 5 YEARS. ALSO, INSTALL INSPECTIONJun 15, 2000 · N5158W · Piper PA28160SDR AU000472Spar Cap · corroded(AUS) LOWER SPAR CAP CORRODED IN WING ROOT AREA. FOUND FOLLOWING REMOVAL OF ANTI-CHAFING TAPE.Jun 14, 2000 · Piper PA31SDR 0002189623Spar · corrodedINTERGRANULAR CORROSION ON RT WING AFT SPAR, JUST O/B OF LOWER O/B MOUNT FOR AILERON CONTROL BUS SECTOR. REPAIRED PER EA 96-172526. L/P 1452411.Jun 14, 2000 · N623NW · Doug DC932SDR 20000626SH003Spar · corrodedEXFOLIATION CORROSION AT LEAST .01 INCH TO .1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BELJun 13, 2000 · N310J · Cessna 310JSDR 20001103SH003Web · corrodedCORROSION ON THE RIGHT WING FRONT SPAR WEB INNER SURFACE AT APPROXIMATELY FSS 400.5, 6 INCHES BY 1.25 INCHES. (X)Jun 10, 2000 · N64742 · Boeing 727224SDR UPS00433288Frame · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON WING BULL NOSE AT CONNECTION FOR WAI VLV. REPAIR CARRIED OUT IAW QUERY NOTE 42/2000 AND SRM 51-40-04 FIG 1 AND SRM 57-10-03 FIG 7. CUT OUT CORRODED AREA AND INSTALLED SPLICE SECTION OF CHORD.Jun 9, 2000 · N521UP · Boeing 747212BSDR TWAA0012105Spar · corrodedDURING CHECK-C MAINT ON THE RT WING, CORROSION WAS FOUND ON THE REAR SPAR BETWEEN CENTER AND O/B AILERON HINGE. FABRICATED ACCORDING TO SRM 59-09 FIG 5. FABRICATED, FINISHED, AND INSTALLED FILLER SHIM AND DOUBLER PER SRM 57-09 FIG 5 AND SRM 57-01 PARAGRAPH 3Jun 7, 2000 · N9305N · Doug DC983SDR UPS00233236Spar · corrodedINSPECTION TYPE: C, CORROSION ON CENTER WING BS 870 REAR SPAR WEB BL 0 - BL 6, WL 160 REPAIRED IAW ER 00-0662Jun 2, 2000 · N907UP · Boeing 72727CSDR UPS00832929Spar · crackedINSPECTION TYPE:C2, RT WING LOOKING I/B TO O/B AT WING TIP AREA, STATIC WICKS 2 AND 3 HAVE DAMAGED T/E SKIN. REMOVED WEDGE PNL, FOUND T/E SPAR CRACKED. FAB NEW WEDGE PNL AND T/E SPAR CHANNEL IAW DAC DWG NR 5644654. ALODINED AND PRIMED IAW DC8 SRM 51-1- 8. Jun 2, 2000 · N803UP · Doug DC873FSDR ASAA0080357Spar Cap · damagedOAK: DURING C CHECK 2 SMALL DRILL HOLES WERE FOUND IN RT WING L/E LOWER SPAR CAP AT XRS 522.7. TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW ASA EA 5710-01060.Jun 1, 2000 · N933AS · Doug DC982SDR EIA2000186Structure · corrodedC2-CHECK -FX-WING CENTER CENTER BS 1241 LBL 82-87 REAR SPAR WEB LOWER CHORD AREA BOTTOM ATTACH STRAP, CORROSION FOUND. BLENDED AREA, NDT INSPECTED, FILLER FABRICATED AND TAPER SHANK FASTENERS INSTALLED PER BOEING MSG EVR-HKG-00-00089F/00091H AND RS R57-12-343May 29, 2000 · N470EV · Boeing 747273CSDR EIA2000164Fitting · crackedC2-CHECK, RIGHT WING BS 1241 CENTER SECTION REAR SPAR LOWER CHORD KICK FITTING ATTACH ''O'' BOLT HOLE FOUND CRACKED. NDT INSPECTED. FREEZE PLUG AND OVERSIZE FASTENER INSTALLED PER BOEING MSG EVR-HKG-00-00077H/-00076F AND RS R57-12-34360. (M)May 29, 2000 · N470EV · Boeing 747273CSDR RRXA002687Frame · damagedDURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE CENTER L/E LOWER FORMER AT STA XFS 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 AND May 15, 2000 · N8084U · Doug DC871FSDR RRXA002684Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 ANMay 15, 2000 · N8084U · Doug DC871FSDR RRXA002683Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 15, 2000 · N8084U · Doug DC871FSDR RRXA002681Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 442, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 15, 2000 · N8084U · Doug DC871FSDR RRXA002682Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002680Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 366, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002679Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002678Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 348, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002677Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT XFS 328, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 ANMay 12, 2000 · N8084U · Doug DC871FSDR 20000530SH003Spar Cap · crackedDURING ROUTINE INSPECTION OF JE24 PIVOT FITTING, IT WAS RECOMMENDED BY THIS REPAIR STATION TO INSPECT THE LOWER VERTICAL STABILIZER FRONT SPAR CAP DOUBLERS FOR POSSIBLE CRACKS. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT OUTER DOUBLERS. THIS IS THE FORTH AIRCMay 12, 2000 · N787WB · Lkheed 132925SDR TWAA0007702Spar · crackedDURING CHECK-C MAINT, THE LOWER SPAR ON RT WING TRAILING EDGE WAS CRACKED AT STA 164, BELOW INBOARD LOWER HOLE FOR THE FLAP HINGE CASTING. INSTALLED DOUBLER REPAIR PER MO 72J86 AND DAC J06271 PER EMLR 70877.May 9, 2000 · N921TW · Doug DC983SDR DL72S000935Frame · corrodedTHE VERTICAL LEG OF THE LOWER CHORD OF THE FRONT SPAR ON THE LT WING WAS FOUND CORRODED AT FSS 402. THE CHORD PLATE WAS ALSO FOUND WITH CORROSION DAMAGE ON ITS LOWER SURFACE IN THE SAME AREA. DAMAGE WILL BE REPAIRED BY NESTED ANGLES AND A STRAP. ER/A 3343May 8, 2000 · N805EA · Boeing 727225ASDR RRXA002246Spar · crackedDURING A MAINTENANCE VISIT FOUND A 2 INCH CRACK TO THE LWR AUX SPAR ANGLE IN RADIUS OF THE RIGHT T/E REAR AUX SPAR AT XRS 86, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTMay 6, 2000 · N995CF · Doug DC862SDR MWEA00409Spar · damagedOUT OF ROUND HOLE ON SPAR AT STATION XRS 383 LEFT WING LOWER TANG. FABRICATED AND INSTALLED REPAIR SPLICE, ANGLE, CUTOUT FILLERS, SHIMS, AND RADIUS FILLERS.May 5, 2000 · N900ME · Doug DC915SDR 20000503SH011Spar · damagedEXISTING FRONT SPAR WEB REPAIR AT APPROXIMATELY BS 5.695 - 713 RT WING (LEADING EDGE) INTERFERRED WITH ACCOMPLISHMENT OF FRONT SPAR MOD. REPAIRED PER ECRA 479-57-137-2. (X)May 3, 2000 · N479EV · Boeing 747132SDR 20000503SH010Spar · misdrilledONE EACH DIAMETER HOLE MISLOCATED IN OUTBOARD MID-SPAR UNDERWING FITTING COMMON TO OVERSIZE HOLES IN LOWER SKIN AT NR 3 PYLON-WING POSITION. REPAIRED PER ECRA 479-57-136-2. (X)May 3, 2000 · N479EV · Boeing 747132SDR QXEA0001189Spar Cap · scratchedYYC- RIGHT HAND WING UPPER AND LOWER SPAR CAP ANGLES SCRATCHED. REPAIRED IAW RD 8-57-1119.Apr 27, 2000 · N829PH · Dhav DHC8102SDR CA000501015Spar · cracked(CAN) ON TAKEOFF THE PILOT HEARD A LOUD BANG. A VISUAL INSPECTION REVEALED NOTHING UNUSUAL AND HE CONTINUED THE FLIGHT. ON LANDING THE ENGINEER DISCOVERED THE LT REAR SPAR CRACKED COMPLETELY. FLEET NDT CAMPAIGN BEING CARRIED OUT.Apr 24, 2000 · Doug B26CSDR 20000712SH020Spar · crackedDURING ROUTINE INSP, NOTED THE RT WING AFT SPAR WEB CRACKED IN 5 PLACES AND THE ROLL SERVO ATTACH BRACKET 60931 CRACKED AT THE OTBD SERVO ATTACH HOLE. ALL CRACKS ARE IN VICINITY OF S-TEC ROLL SERVO BRACKET ATTACHMENT BOLTS. S-TEC TWO AXIS AUTOMATIC FLIGHT GUApr 24, 2000 · N783 · Cessna U206GSDR TWAA0006417Spar Cap · crackedDURING OP 16 MAINT CHECK, ON LT WING A CRACK IN LOWER SPAR CAP AT I/B FLAP HINGE SUPPORT FITTING, I/B LOWER HOLE, WAS FOUND. REPAIRED PER DOUGLAS DRAWING JO60271.Apr 22, 2000 · N984Z · Doug DC931SDR EIA2000146Spar · crackedFOUND LT WING REAR SPAR TO CENTER SECTION SPLICE FITTING NR 5 FASTENER HOLE FOUND CRACK AT WING SKIN UPPER SURFACE APPROX .125 INCH IN LENGTH RUNNING FORWARD. SKIN REWORKED, BUSHING INSTALLED PER EO 57-747-1011-90A AND SB 747-57-2110 FIG 6. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIA2000140Spar · corrodedLEFT WLG W/W BS 1241 BULKHEAD WEB TO BULKHEAD FITTING MATING SURFACE CORROSION REVEALED AT NR 7, 8, 9, 19 AND 20 RIVETS. CORROSION REMOVED AND REPAIRED PER EO 57-747-1544-99. (M)Apr 21, 2000 · N482EV · Boeing 747212B
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