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 AU981331Cap · cracked(AUS) WING LOWER SPAR CAP CRACKED VERTICALLY THROUGH THE ANGLE TO THE SECOND OUTBOARD MOUNT BOLT HOLE. PART TC: 970.Oct 16, 1998 · Conaer LA4250SDR CA981027008Spar · cracked(CAN) WHILE COMPLYING WITH AD CF-92-26, REF SB 215-A454, BOTH LEFT AND RIGHT REAR SPAR CAPS WERE FOUND CRACKED USING VISUAL METHOD. ON DISASSEMBLY, FOUND THE LEFT SPAR CAP WAS COMPLETELY CRACKED THROUGH, WHILE THE RIGHT HAND ONE WAS CRACKED ABOUT HALF WAY THROct 15, 1998 · Cndair CL2151A10SDR 98ZZZX4828Spar · bentDURING ANNUAL INSPECTION, THE DOUBLER WAS FOUND BENT DUE TO PRE-EXISTING DAMAGE TO FORWARD WEB OF FRONT SPAR CARRY-THROUGH STRUCTURE. SUBMITTER STATED AIRCRAFT HAS A HISTORY OF GEAR UP LANDING.Oct 14, 1998 · N8493N · Beech 95B55SDR 98ZZZX4827Spar · bentDURING ANNUAL INSPECTION, THE DOUBLER WAS FOUND BENT AND PARTIALLY SEPARATED FROM AFT WEB OF FRONT SPAR CARRY-THROUGH STRUCTURE DUE TO PRE-EXISTING DAMAGE TO WEB. SUBMITTER STATED AIRCRAFT HAS A HISTORY OF PREVIOUS GEAR UP LANDING.Oct 14, 1998 · N8493N · Beech 95B55SDR DL72S982085Spar · damagedDURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO TOOLING DAMAGE. REPAIRED PER ERA 332359-14AD.Oct 8, 1998 · N407DA · Boeing 727232SDR AU981271Cap · corroded(AUS) LEFT WING UPPER SPAR CAP CONTAINED EXFOLIATION CORROSION LOCATED ADJACENT TO PITOT HEAD AND EXTENDING OUTBOARD THROUGH THE LEADING EDGE RIBS. FOUND DURING INSPECTION IAW AD/BEECH55/29 AMDT 1. PART TC: 29,054.Oct 6, 1998 · Beech 95B55SDR EIAA980277Spar · crackedPHX - DURING C-CHECK, FOUND CRACK IN LEFT WING FORWARD SPAR UPPER CHORD AT XIS 84.5. NRC A182. REPAIRED PER, EA DC9-57-140 AND ECRA 935-51-038-1. (M)Oct 2, 1998 · N935F · Doug DC932FSDR EIAA980273Spar · crackedPHX - DURING C-CHECK, RIGHT WING AFT SPAR LOWER CHORD AT XRS 164 NR 2 FLAP HINGE ATTACH AREA A CRACK WAS FOUND. REPAIRED PER DRAWING J06027, EA DC9-57-136 AND ECRA 935-51-038-1. (M)Oct 2, 1998 · N935F · Doug DC932FSDR EIAA980268Spar · crackedPHX - DURING C-CHECK, RIGHT WING AFT SPAR UPPER CHORD AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SERVICE BULLETIN 57-179 REV 1, DRWG J060272 AND ECRA 935-51-038-1. (M)Oct 2, 1998 · N935F · Doug DC932FSDR EIAA980267Spar · crackedPHX - DURING C-CHECK, LEFT WING AFT SPAR UPPER CHORD XRS 267 AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SERVICE BULLETIN 57-179 REV 1, DRWG JO60272 AND ECRA 935-51-038-1. (M)Oct 2, 1998 · N935F · Doug DC932FSDR AU981262Cap · corroded(AUS) REAR SPAR CAP CONTAINED DELAMINATION IN THE AREA OF THE RIGHT WHEEL WELL. MINOR CORROSION OF THE SPAR CAP LOCATED IN THE LEFT WHEEL WELL. PART TC: 11,423.Oct 1, 1998 · Cessna 441SDR AALA981838Spar · corrodedTUL - DURING C-CHECK, FOUND CORROSION ON REAR SPAR UPPER CAP AFT TANG BETWEEN RIGHT WING STATION XORS 781-828. REMOVED CORROSION AND REPAIRED PER SRM 51-21-01 AND ESO 41000 DATED 10-1-98. (M)Oct 1, 1998 · N1761R · Doug MD11SDR 9810509970Spar Cap · crackedDURING M-CHECK, A CRACK WAS FOUND IN THE REAR SPAR LOWER CAP AT FS XRS 353. REPAIRED PER EA 99-159317 (P/N 5911301-502).Sep 29, 1998 · N9334 · Doug DC931SDR AALA981816Spar · corrodedTUL - UPPER SPAR CHORD CORRODED ABOVE NR 1 L/E SLAT ACTUATOR. REMOVED CORROSION AND INSTALLED STRAP PER ESO 11697 DATED 9-2-98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981802Spar · corrodedFOUND CORROSION ON LOWER SPAR CHORD ANGLE WS 620 JUST INBOARD OF NR 7 SLAT ICE TUBE. INSTALLED DOUBLER PER 57-30-2. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981801Spar · corrodedTUL - FOUND UPPER SPAR CHORD CORRODED ABOVE NR 5 L/E FLAP ACTUATOR, RIGHT WING. REMOVED CORROSION PER SRM 51-10-6 AND INSTALLED DOUBLER STRAP PER ESO 11697, DATED 9-2-98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981799Spar · corrodedTUL - FOUND WS 212-232 UPPER SPAR CHORD CORRODED INBOARD OF NR 5 L/E FLAP ACTUATOR. REMOVED CORROSION PER SRM 51-10-6 AND INSTALLED DOUBLER STRAP PER ESO 11697, DATED 9/2/98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981769Spar · corrodedTUL - FOUND CORROSION ON UPPER SPAR CHORD ABOVE NR 2 L/E SLAT ACTUATOR ALSO ON SKIN. INSTALLED REPAIR ANGLE PER ESO 11697, DATED 9/8/98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981745Spar · corrodedTUL - UPPER SPAR CHORD CORRODED ABOVE AND OUTBOARD OF NR 6 L/E SLAT ACTUATOR. REMOVED CORROSION AND REPAIRED AREA WITH 17-7 TH1050 DOUBLER .24 EA .1875 INCH AND 24 EA .25 INCH HI-LOCKS PER ESO 11697 DATED 9-2-98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981744Spar · corrodedTUL - UPPER SPAR CHORD CORRODED ABOVE AND OUTBOARD OF NR 6 L/E SLAT ANTI ICE TUBE. REMOVED CORROSION AND REPAIRED AREA WITH 17-7 TH1050 DOUBLER, 24 EACH .1875 AND 24 EACH .25 INCH HI-LOCKS PER ESO 11697, DATED 9-2-98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981742Spar · corrodedTUL - FOUND UPPER SPAR CHORD HAS HEAVY CORROSION ABOVE NR 4 L/E SLAT ACTUATOR. INSTALLED REPAIR ANGLE AT UPPER CHORD PER ESO 11697, DATED 09/02/98. (M)Sep 25, 1998 · N720AA · Boeing 727227SDR AALA981747Spar · corrodedTUL - LOWER SPAR CHORD STATION 383 REAR SPAR HAS CORROSION. REPAIRED LOWER SPAR CHORD PER SRM 57-30-2. (M)Sep 24, 1998 · N720AA · Boeing 727227SDR VJ9800482Spar · magnetizedREPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4 AND AIRTRAN RES 981625.Sep 23, 1998 · N911VV · Doug DC932SDR ARWA980910Spar · crackedRT WING FRONT SPAR LOWER CAP HAS TWO ADJACENT ATTACHMENT HOLES CRACKED BETWEEN STA XFS 515.000 AND XFS 526.760. CUT OUT DAMAGED AREA PER DRA J060232, FABRICATED FILLER, ANGLES AND DOUBLER PER DRG J060232 AND ROD SKETCH 97-02-10-005. LOCATED, DRILLED AND STRSep 19, 1998 · N802BN · Doug DC862SDR CA980930014Screw · corroded(CAN) DURING THE 13,000 CYCLE FUSELAGE INSPECTION, THREE SCREWS ON THE FORWARD SPAR CAP WERE FOUND CORRODED AND SHEARED OFF. FURTHER INVESTIGATION REVEALED THE PRC AROUND THE UPPER SPAR CAP AND FUSELAGE SKIN HAD WORKED LOOSE AND MAY BE THE SOURCE FOR THE CORRSep 18, 1998 · Beech A100SDR VJ9800479Spar · corrodedRT WING LOWER REAR SPAR XW 530 VERTICAL LEG CORRODED. FABRICATED, INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-1, 51-10-4, 53-22-1, AND AIRTRAN RES 981582.Sep 17, 1998 · N911VV · Doug DC932SDR TWAA9815307Spar · crackedDURING CHECK-C MAINT, FOUND LT WING AFT SPAR WITH EDDY CURRENT INDICATION OF 1.25 INCH CRACK IN AFT SPAR WEB, .75 INCH BELOW O/B LOWER BOLT HOLE FOR O/B FLAP HINGE CASTING. INSTALLED REPAIR PER ROD DRAWING 95-12-06-018, AND ARA 15388.Sep 17, 1998 · N986Z · Doug DC931SDR 98ZZZX4118Spar · corrodedFOUND MAIN SPAR LOWER CAP SEVERELY CORRODED. THIS CORROSION WAS FOUND WHERE MAIN SPAR PASSES THROUGH FUSELAGE BENEATH AIR CONDITIONER LOCATION. SUSPECT MOISTURE FROM AIR CONDITIONER COLLECTED ON SPAR CAUSING CORROSION. LOCATION FURTHER IDENTIFIED AS FS 288.Sep 16, 1998 · N5632C · Beech 1900CSDR ABXA9800825Spar Cap · corrodedDURING C-CHECK, FOUND RIGHT WING UPPER SPAR CAP CORRODED BEYOND LIMITS UNDER AND AROUND THE NUT PLATE JUST OUTBOARD OF RIGHT AILERON. REPAIRED IAW ABX REA D957-24791-MR.Sep 11, 1998 · N939AX · Doug DC932SDR 98ZZZX3577Fasteners · looseLOOSE FASTENERS AT RT WING FRONT SPAR UPPER CHORD. WS 330.5.Sep 11, 1998 · N912TS · Boeing 727254SDR EIAA980263Spar · corrodedPHX - DURING C-CHECK, LEFT WING REAR SPAR UPPER CHORD HORIZONTAL LEG HAS CORROSION AT WS 270. REPAIRED PER SABER TECH DC9-57-138 AND ECRA 935-51-038-1. (M)Sep 5, 1998 · N935F · Doug DC932FSDR DHL9870821CSpar · corrodedAT C-CHECK, LEFT WING UPPER FRONT SPAR SKIN FOUND CORROSION AROUND LEADING EDGE ATTACHMENT SCREWS AT WS 330. REMOVED CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-4, 16.75 X 2. N/R 1641Sep 2, 1998 · N708DH · Boeing 72725SDR EIAA980242Spar · corrodedHKG - DURING C2 CHECK, RT WING L/E FRONT SPAR WEB FITTING AT WS 1483 HAS CORROSION. NRC 5456. REPLACED PER SRM 51-10-01. (X)Sep 1, 1998 · N477EV · Boeing 747SR46SDR 98ZZZM832Spar · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR CAP AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR, JUST ABOVE THE EDGE OFAug 29, 1998 · N1563C · Beech 1900CSDR 98ZZZX3587Spar · corrodedRT WING UPPER SURFACE JUST INBOARD AND FORWARD OF NR 2 SPOILER HAS CORROSION THAT RUNS FROM (XORS 480) TO (XORS 492). REPAIR WAS C/W BY DOUGLAS PROVIDED E.A. NOTE: MAXIUM DEPTH OF CORROSION WAS .050 INCH.Aug 28, 1998 · N321FE · Doug DC1030FSDR 98ZZZX3398Spar · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR JUST ABOVE THE EDGE OF THE Aug 23, 1998 · N41UE · Beech 1900CSDR DLL10981751Spar Cap · crackedTHE UPPER SPAR CAP OF THE FS 1103 INTERMEDIATE SPAR WAS FOUND WITH TYPICAL CRACKING AT LEFT END. THE CRACK WAS BEYOND THE ALLOWABLE LIMITS SPECIFIED IN LAC S/B 093-57-087. THE CAP WAS CUT I/B OF LBL 94.5 AND A NEW SECTION WAS SPLICED IN WITH STEEL REPAIR ANGAug 22, 1998 · N728DA · Lkheed 10113851SDR CALA9801499Spar Cap · corrodedINSPECTION FOUND RT WING AFT LOWER SPAR CAP CORRODED AT WS XRS 364.5. THE AFT LOWER SPAR CAP WAS REPAIRED IAW SRM 57-09, FIGURE 11.Aug 21, 1998 · N14564 · Doug DC931SDR 98ZZZX3397Spar Cap Assy · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS SPAR JUST ABOVE THE EDGE OF THE SEALAug 20, 1998 · N45GL · Beech 1900CSDR AALA981564Spar · corrodedTUL - FRONT SPAR LOWER CHORD CORRODED BELOW NR 1 KRUGER FLAP ACTUATOR FS 300 TO 305. INSTALLED REPAIR PER AARD 57-30-00-2 PAGE 1-3. (M)Aug 18, 1998 · N881AA · Boeing 727223SDR MWEA98912Spar · chafedFOUND BARE METAL AND CHAFING ON LEFT WING FRONT SPAR UPPER AND LOWER CHORDS. MTC REWORKED CHAFED AREAS.Aug 17, 1998 · N40ME · Doug DC914SDR AU981127Spar · corroded(AUS) WING CENTER SECTION CARRY THROUGH SPAR CORRODED AND RIVET HEAD MISSING. RIVET HEAD HAD BEEN MISSING PRIOR TO RECENT RE-PAINT.Aug 17, 1998 · Cessna 172MSDR DL72S981699Spar Web · crackedTHE CENTER WING REAR SPAR WEB WAS FOUND WITH 5 CRACKS NEAR UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF THOSE IN BAC S/B 727-57A0182. THE SPAR WEB WAS MODIFIED PER THE S/B WITH A CHANGE TO THE REPAIR AT RBL 20 WHERE A PREVIOUS LOCAL REPAIR WAS INSTALLED. THEAug 14, 1998 · N528DA · Boeing 727232SDR AALA981512Spar · corrodedTUL - FOUND CORROSION ON TOP AND BOTTOM OF LE SPAR LOWR CHORD ANGLE AT WING LE STATION 392, BELOW FUEL VALVE. INSTALLED STRIP DOUBLER ON UPPER SIDE OF BLENDED AREA PER AARD 57-30-00-2, 14 INCHES IN LENGTH. (M)Aug 11, 1998 · N731AA · Boeing 727227SDR AALA981509Spar · crackedTUL - CHORD ANGLE CRACKED 3 INCHES FORWARD OF NR 7 SPOILER CASTING. CUT OUT DAMAGED SECTION OF LOWER CHORD ANGLE AND SPLICED IN NEW SECTION PER SRM 51-40-4. (M)Aug 11, 1998 · N731AA · Boeing 727227SDR CALA9801441Spar Channel · crackedINSPECTION FOUND U-CHANNEL AT REAR SPAR OF LT WING LOWER SURFACE JUST INBOARD OF SECOND OUTBOARD FLAP TRANSMISSION WORN AND CRACKED OUT OF NUT PLATE HOLE. THE CHANNEL WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.Aug 10, 1998 · N14788 · Boeing 727232SDR CALA9801429Spar Web · crackedINSPECTION FOUND A .25 INCH CRACK IN SECOND FROM AFT VERTICAL WEB AT RT WING FRONT SPAR CHORD INBOARD AREA JUST FORWARD OF BOTTLE PIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.Aug 7, 1998 · N32725 · Boeing 727224SDR AU980944Rivet · missing(AUS) WING LOWER SPAR CAP HAD NUMEROUS RIVETS MISSING. RIVETS HAVE A CROSS ON THE HEAD POSSIBLY INDICATING MAGNESIUM MANUFACTURE.Aug 5, 1998 · Cessna 172NSDR UPS98227266Spar · crackedINSPECTION TYPE-N/A, RT WING REAR SPAR U-CHANNEL CRACKED BETWEEN LIGHTENING HOLES DIRECTLY OVER RT MAIN LANDING GEAR STRUT, (MARKED IN RED). REPAIRED CRACKED AREA AS PER EO B727-5720-10177-A, INSTALLED REPAIR DOUBLER.Aug 3, 1998 · N909UP · Boeing 72727CSDR AU981076Rivet · loose(AUS) LOOSE AND WORKING RIVETS LOCATED IN AREA OF RIGHT WING INBOARD SPAR SECTION.Aug 3, 1998 · Beech 58
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