JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720'
  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 200200189Angle · corrodedREPAIR OF CORROSION ON BS 1241 PRESSURE WEB ANGLE. THE CORROSION WAS REMOVED BY TRIMMING AWAY THE DAMAGED SECTION OF PRESSURE WEB ANGLE AT APPROXIMATELY LBL 80 AND RBL 70.Apr 1, 2002 · N480EV · Boeing 747121SDR ASOA02197SFitting · crackedDURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AILERON INBOARD CLOSURE RIB IAW SRM 51-00. (M)Mar 28, 2002 · N858AS · Cndair CL6002B19SDR ASOA02197Fitting · crackedDURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL REPLACE THE RIGHT WING TRAILING EDGE RIB. (M)Mar 28, 2002 · N858AS · Cndair CL6002B19SDR UPS02838042Clip · crackedINSPECTION TYPE:C1 O/B SKATE ANGLE CLIP BETWEEN STRINGER 62 AND STRINGER 63 CRACKED NR 1 PYLON NR 1 ALT. REMOVED AND REPLACED CLIP IAW DC8 SRM 51-1-20D.Mar 28, 2002 · N709UP · Doug DC871FSDR DL72S020374Stiffener · crackedOUTBOARD SPAR STIFFENER CRACKED NR 4 SLAT INBOARD TRACK. REPLACED SPAR STIFFENER.Mar 26, 2002 · N8875Z · Boeing 727225ASDR 2002F00433Channel · corrodedDURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR TORQUE BOX LOWER AFT BATHTUB FITTING CHANNEL WAS CORRODED (LEVEL 2). MAINTENANCE REMOVED AND REPLACED THE FITTING CHANNEL IN ACCORDANCE WITH LOCKHEED SRM 51-40-01, FS 1230, WS 319 LEFT.Mar 24, 2002 · N188AT · Lkheed 10113851SDR QXEA0200580Web · crackedPDX - LIGHTENING HOLE CRACKED BOTTOM SIDE, RIGHT TRAILING EDGE, BELOW AND OUTBOARD OF RIGHT OUTBOARD ROLL SPOILER CENTER HINGE. REPAIRED IAW DHC-8 SRM 51-10-21.Mar 24, 2002 · N358PH · Dhav DHC8202SDR AALA20020431Support · damagedAFW - FOUND CORROSION IN MOUNT HOLE AFT OUTBOARD HOLE, ON RIGHT INBOARD FLAP SUPPORT BEAM. PERFORM A DETAILED VISUAL INSPECTION OF THE RE-WORKED HOLE TO VERIFY COMPLETE CORROSION REMOVAL. APPLY ALODINE AND TWO COATS OF PRIMER TO RE-WORKED AREAS. (M)Mar 22, 2002 · N384AA · Boeing 767323SDR C1HA200288004Strap · crackedRIGHT WING FIXED LEADING EDGE INNER STRAP IS CRACKED AT APPROX W.S. 226. REPAIRED INNER STRAP RIGHT WING AT WS 226.Mar 22, 2002 · N688CA · Boeing 7272S7SDR C1HA200288001Strap · crackedLEFT WING FIXED LEADING EDGE INNER STRAP IS CRACKED AT APPROX WS 226. REMOVED AND REPLACED STRAP, CUT STRAP INSTALL REPAIR.Mar 22, 2002 · N688CA · Boeing 7272S7SDR AUS20020390Bracket · corroded(AUS) LT WING BRACKET ATTACHED TO LOWER CHORD DELAMINATED FROM CORROSION ZONE 72, STN WS204.0. CPCP - LEVEL 2 CORROSION.Mar 21, 2002 · Boeing 727281SDR GTIA020306Attach Angle · crackedFTW - RIGHT WING CRACK AT ANGLE ATTACH NOSE CAP VORTILON. REMOVED VORTILON FAIRING ATTACH ANGLE. STOP DRILLED CRACK ANGLE. UPON REMOVAL OF VERTICAL ANGLE FITTING FOUND TO BE CRACKED. FABRICATED REPAIR DOUBLERS. LOCATED AND DRILLED HOLES IN NEW ATTACH ANGLMar 20, 2002 · N806NK · Doug DC981SDR QXEA0200578Bracket · crackedPDX - LEADING EDGE PANEL 511AL OUTBOARD NUT PLATE BRACKET APPEARS TO BE CRACKED IN RADIUS BEHIND NUT PLATE. REPAIRED IAW DHC-8-200 SRM 51-40-11.Mar 20, 2002 · N358PH · Dhav DHC8202SDR QXEA0200577Bracket · crackedPDX - LEADING EDGE PANEL 511AL OUTBOARD UPPER NUT PLATE BRACKET APPEARS TO BE CRACKED IN RADIUS BEHIND NUT PLATE. REPAIRED IAW DHC-8-200 SRM 51-40-00, PAGE 4 AND SRM 51-40-11.Mar 20, 2002 · N358PH · Dhav DHC8202SDR QXEA0200571Bracket · crackedPDX - LEADING EDGE PANEL 611AR OUTBOARD LOWER NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40-00.Mar 20, 2002 · N358PH · Dhav DHC8202SDR QXEA0200570Bracket · crackedPDX - LEADING EDGE PANEL 611AR OUTBOARD UPPER OUTBOARD NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 4, TABLE 4.Mar 20, 2002 · N358PH · Dhav DHC8202SDR CA020318002Angle · cracked(CAN) ON THE LEFT HAND SIDE OF THE FUSELAGE, THE DRAG ANGLE THAT JOINS THE FUSELAGE AND WING AT WS 51 WAS FOUND CRACKED DURING THE NORMAL "B" CHECK.THE CRACK IS APPROXIMATLEY ONE INCH(1")LONG FROM THEFRONT FACE TOWARDS THE REAR OF THE ANGLE IN THE BEND RADIUS.Mar 18, 2002 · Cndair CL2151A10SDR GTIA020343Bracket · crackedFTW - FOUND RIGHT WING, UPPER DOG LEG, BRACKET ATTACH TO BODY CRACKED. REMOVED DAMAGED BRACKET RIGHT WING UPPER SURFACE. FABRICATED NEW BRACKET. INSTALLED NEW BRACKET. (M)Mar 16, 2002 · N806NK · Doug DC981SDR ABXA010791Strap · crackedT-CAP DOUBLER STRAP AT WS 485.00, FORWARD SPAR, LOWER CRACKED NR 4 ALT. REMOVED AND REPLACED DOUBLER STRAP IAW DC-8 SRM 51-1-20D, 51-1-24 AND DAC DWG 5803958.Mar 15, 2002 · N849AX · Doug DC861SDR NAFA20020002Cap · crackedRIGHT WING NR 23 STRINGER CAP CRACKED AT STA 325. FABRICATED AND INSTALLED 2 DOUBLERS PER DRAWING NAC2002-02.Mar 13, 2002 · N7780B · Doug DC6ASDR 200200181Support · brokenLEFT WING LEADING EDGE LOWER FIXED FAIRING SUPPORT ROD WAS FOUND BROKE (SEPARATED). REPLACED SUPPORT ROD PER 747 MM 20-51-01.Mar 13, 2002 · N471EV · Boeing 747273CSDR ABXA010776Stiffener · crackedOUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.Mar 4, 2002 · N925AX · Doug DC914SDR UPS02837860Splice · crackedINSPECTION TYPE:C STRINGER 51 SPLICE FITTING CRACKED APPROX 10 INCHES OUTBOARD OF XRS74, LT WING. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D AND 51-3-0.Mar 3, 2002 · N707UP · Doug DC871FSDR UPS02837859Splice · crackedINSPECTION TYPE:C STRINGER 51 SPLICE CRACKED APPROX 12 INCHES OUTBOARD OF XRS 74, NR 3 ALT TANK, RT WING, FIRST STRINGER FWD OF REAR SPAR CAP. REMOVED AND REPLACED STRINGER 51 SPLICE PER SRM 51-1-20D AND 51-3-0.Mar 3, 2002 · N707UP · Doug DC871FSDR COOSDR020007Doubler · corrodedRIGHT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863SDR COOSDR020006Doubler · corrodedLEFT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863SDR SIMA200210025Angle · corrodedSAW - DURING CPCP8 INSPECTION, FOUND RIGHT WING REAR SPAR UPPER SPAR ANGLE TO BE CORRODED JUST OUTBOARD OF INBOARD AILERON HINGE. REPAIRED IAW ATR FAX DO/TE/S560.0401/02-1004. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 27, 2002 · N319AM · Aerosp ATR42300SDR DHL2002364504Beam · corrodedRT OUTBOARD TOP SIDE AT WING TIP INSIDE OUTER COVER PLATE, THERE IS CORROSION. REMOVED WING TIP PER AMM 57-24-11 TO ACCESS CORROSION, R&R NEW BEAM PER A300 SRM.Feb 18, 2002 · N364DH · Airbus A300B4203SDR QXEA0200381Attach Angle · crackedPDX - LT WING LOWER WING-TO-FUSELAGE CONNECTION ANGLE FOR WING-TO-FUSELAGE FAIRING CONNECTION ANGLE IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-31-02, PAGES 9-10, PARAGRAPHS 4B AND 4C.Feb 17, 2002 · N480AU · Fokker F28MK4000SDR QXEA0200308Attach Fitting · crackedPDX - LT WING FAIRING ATTACH STRUCTURE IS CRACKED ALONG THE FORWARD CIRCUMFERENCE OF PANEL 91J.Feb 17, 2002 · N480AU · Fokker F28MK4000SDR R2J2002F00004Splice Plate · improper partDURING AAIP PHASE INSPECTION DISCOVERED IMPROPER PARTS HAD BEEN INSTALLED WHILE INSTALLING AVIADESIGN WING SPAR STRAP PER STC SA 1602CE. STC HOLEDER WAS CONTACTED AND APPROVED PART, WHICH IS A SPECIAL ALLOY, WAS INSTALLED. FAA-PMA PART. SUGGEST CALLING THE Feb 13, 2002 · N574GS · Beech 200BEECHSDR 0200699865Spar Cap · corrodedDuring MCK in ATL, corrosion was found above the inboard and outboard stud holes in the right wing rear spar upper cap at station xrs 267. Repaired per EA 98-185519.Feb 12, 2002 · N774NC · Doug DC951SDR 0200429865Spar · corrodedDuring Mck in ATL, corrosion was found above the inboard and outboard stud holes in the right wing rear spar upper cap at station 267. Both holes were spot faced. Repaired per EA 98-185519.Feb 12, 2002 · N774NC · Doug DC951SDR QXEA0200187Fitting · gougedPDX - LT WING LOWER STRINGER 2.9 END FITTING IS GOUGED AT STATION 11130. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 6, PARAGRAPH 5B(A).Feb 10, 2002 · N480AU · Fokker F28MK4000SDR 0200409865Spar · crackedDuring Mck in ATL, 2 cracks were in the upper spar cap at STA 267. The cracks extend around the upper stud holes for the # 3 flap hinge fitting. Repaired per EA 98-185533.Feb 8, 2002 · N774NC · Doug DC951SDR 2002FA0000181Bracket · failedIN-TRANSIT LIGHT STAYED ON AFTER GEAR WAS RETRACTED. GEAR WAS EXTENDED AND A/C LANDED WITHOUT INCIDENT. UPON INSPECTION, THE RT GEAR WELL PLACARD CLOSEOUT PANEL WAS FOUND TORN AND BENT UP. THE INBOARD Z-BRACKET HAD FAILED, AS WELL AS THE LOWER ANGLE, THAT TFeb 8, 2002 · N300QS · Cessna 560CESSNASDR UPS02837720Clip · crackedINSPECTION TYPE:C2 LEFT WING NR 1 ALT TANK HAS 2 ATTACH CLIPS CRACKED AT O/B SKATE ANGLE AT XW485 BETWEEN STRINGER 62 & 63. REMOVED, FABRICATED ONE CLIP, REPLACED OTHER CLIP AND INSTALLED BOTH CLIPS IAW DWG 5804006 AND 5804007 AND SRM 51-1-20D.Feb 7, 2002 · N703UP · Doug DC871FSDR UPS02837652Clip · crackedINSPECTION TYPE:C2 RT WING CLIP CRACKED AT XW467 BETWEEN S62 AND S63. REMOVED AND REPLACED CLIP IAW SRM 51-1-20D AND DAC DWG 5804006.Feb 7, 2002 · N703UP · Doug DC871FSDR QXEA0200212Strap · chafedPDX- LT WING HAS CHAFE DAMAGE TO WING JOINT STRAP AT WS 1700, LOWER WING SURFACE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND HORIZON AIR EA 4-57-575.Feb 6, 2002 · N480AU · Fokker F28MK4000SDR UPS02837723Fitting · crackedINSPECTION TYPE:C2 STRINGER FITTING CRACKED BETWEEN XRS 50 AND XRS 74 AT STRINGER 51 IN LEFT WING TANK. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D, 51-1-20D, 51-1-23.Feb 6, 2002 · N703UP · Doug DC871FSDR 200200174Fitting · wornTHE REINSTALLATION OF THE FITTING REQUIRED THE SUBSTITUTION OF STRAIGHT SHANK FASTENERS IN LIEU OF THE TAPER SHANK FASTENERS, ORIGINALLY USED THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-57-141-02.Feb 6, 2002 · N482EV · Boeing 747212BSDR ARWA20020203Fitting · crackedDURING C-CHECK, RIGHT WING NR 4 ALTERNATE FUEL TANK INTERIOR S-58 END FITTING WITH 1 INCH CRACK AT STA XRS 408.00.Feb 4, 2002 · N802BN · Doug DC862SDR ARWA20020202Fitting · crackedDURING C-CHECK, LT WING NR 1 ALTERNATE FUEL TANK INTERIOR S-57 END FITTING WITH 1 INCH CRACK STA XRS 408.00. REMOVED AND REPLACED STRINGER END FITTINGS IAW DC-8 SRM 51-1-20D.Feb 4, 2002 · N802BN · Doug DC862SDR UPS02837606Attach Angle · crackedINSPECTION TYPE:C2 LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 520. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297 AND SRM 51-1-20D.Feb 4, 2002 · N703UP · Doug DC871FSDR UPS02437687Fitting · crackedINSPECTION TYPE:C LT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 3 HOLE FOUND CRACKED, PLS REFER ATTACH SKETCH. LT BS 1241 WING REAR SPAR UPPER SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-E APPENDIX F, H AND I.Jan 31, 2002 · N673UP · Boeing 747123SDR QXEA0200120Flange · chafedPDX - INBOARD BOTTOM LEADING EDGE FLANGE CHAFED AT YW57.00. REPAIRED IAW RD 8-57-811, DHC-8 SRM 51-20-16, PAGE 3 AND SRM 51-20-26.Jan 24, 2002 · N356PH · Dhav DHC8202SDR UPS02437664Stiffener · crackedINSPECTION TYPE:C L/W - L/E CAVITY FRONT SPAR 1 EA VERTICAL STIFFENER FOUND CRACKED AT LOWER END ABOUT 2 INCHES AT WS 382 JUST BEHIND NR 13 K/FLAP. STIFFENER IS REPAIRED AS PER HAECO RS R-57-21-34726.Jan 24, 2002 · N673UP · Boeing 747123SDR ABXA010739Fitting · crackedRIGHT WING REAR SPAR, XRS 340, ACTUATOR ATTACH FITTING TO REAR SPAR WAS CRACKED. REPLACED FITTING IAW DC-8 DAC DWG 5773254, MM 20-16-00, 20-14-00 AND 27-51-09.Jan 23, 2002 · N847AX · Doug DC861SDR 200200171Support Fitting · corrodedFLAP TRACK WING SKIN AND BACKUP FITTING HOLE CORROSION. REPAIR IS ACCOMPLISHED BY REPLACING THE ORIGINAL BUSHINGS EXCEPT THE OUTER DIAMETER IS INCREASED TO COMPENSATE FOR THE HOLE BORE DIAMETER INCREASE. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRAJan 23, 2002 · N639FE · Boeing 7472R7FSDR QXEA0200106Bracket · chafedPDX - BRACKET CHAFED OUTBOARD BOTTOM END OF INBOARD LEADING EDGE FLANGE AT STATION YW138.00. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-36.Jan 17, 2002 · N356PH · Dhav DHC8202
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