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 2004FA0000090Stiffener · damagedIN COMPLIANCE WITH AD, INSPECTED WING CENTER SECTION IAW SB AND AC. FOUND MINOR CORROSION IN RT WING CENTER SECTION ON FIRST STIFFENER AHEAD OF REAR SPAR IB, ITEM. REPLACED STIFFENER. FOUND DAMAGED STIFFENER IB FRONT OF MAIN SPAR, ITEM. REPLACED STIFFENER.Dec 12, 2003 · N99780 · Univar 415CDSDR SWIA200312776Clip · crackedLEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE OUTBOARD CLIP IS CRACKED AT AFT END, RIB 16. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE CLIP TO LEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE, OUTBOARD CLIP IAW EMB SRM 51-40-00.Dec 9, 2003 · N221SW · Emb EMB120ERSDR CALA0300702Splice · crackedINSPECTION FOUND A 1 INCH CRACK IN WING SPLICE STRAP AT WING SPAR STA XRS 164 JUST O/B OF RIGHT VORTILION. THE WING SPLICE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 7, 2003 · N16806 · Doug DC982SDR QXEA200301544Attach Fitting · chafedRIGHT HAND OUTBOARD FLAP NR 4 FLAP CARRIAGE FRONT SPAR ATTACH BRACKET INBOARD FITTING AND OUTBOARD LUG IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228.Dec 6, 2003 · N406QX · Bombdr DHC8401SDR QXEA200301543Attach Fitting · chafedLEFT HAND OUTBOARD FLAP NR 4 CARRIAGE FRONT SPAR ATTACH BRACKET INBOARD FITTING AND OUTBOARD LUG IS CHAFED. REPAIRED IAW Q400 RD 8/4-57-228.Dec 6, 2003 · N406QX · Bombdr DHC8401SDR AWXA200400005Plate · chafedMCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER IN LT FLAP WELL CHAFING ON LT OUTBOARD FORE FLAP JUST OUTBOARD OF NR 3 FLAP TRACK WS 205 LT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE LT FLAP WELL WS 205 LT; FABRICATED A NEW REPLACEMENT PLATE; Dec 4, 2003 · N174AW · Boeing 73733ASDR CALA0300687Angle · crackedRT WING 90 DEGREE GREEN ANGLE CRACKED AT FORWARD SIDE OF RT MLG INBOARD DOOR OPENING WBL 71 UNDER STRUT DOOR. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-02.Dec 4, 2003 · N16648 · Boeing 737524SDR AWXA200301642Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON LT WING LEADING EDGE BRACKET (Z-ANGLE) INSIDE PANEL 5748, WS 191. MAINTENANCE REMOVED CRACKED Z-ANGLE WS 191, UPON REMOVAL OF ANGLE FOUND LOWER SKIN CRACKED. REMOVED CRACKED SECTION OF SKIDec 3, 2003 · N174AW · Boeing 73733ASDR WVE2003F00025Support Bracket · crackedWHILE PERFORMING IRN 27-50-26 REPLACEMENT OF LT WING FLAP NOSE ROLLER ATTACHMENT FITTINGS, THE LT FLAP ACTUATOR UPPER ATTACHMENT BRACKET WAS FOUND TO BE CRACKED. THIS BRACKET IS LOCATED UNDER ACCESS PANEL 540EB WHICH IS NOT REQUIRED TO BE REMOVED FOR THE 1200Dec 3, 2003 · N233FX · Lear 60LEARSDR QXEA200301517Angle · crackedPDX - CRACKED Z-ANGLE RIGHT HAND WING FORWARD SPAR AT TOP FROM FIRST RIVET TO TOP EDGE OF STATION YW45-00. REPAIRED IAW DHC-8-200 SRM 51-40-11.Dec 3, 2003 · N352PH · Dhav DHC8202SDR AWXA200400003Plate · chafedMCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER AT INBOARD END OF RT OUTBOARD FLAP WELL CHAFED WS 205 RT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE AT INBOARD END OF RT OUTBOARD FLAP WELL WS 205 RT; FABRICATED A NEW REPLACEMENT PLATE; INSTALLEDec 2, 2003 · N174AW · Boeing 73733ASDR AWXA200301640Support Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL, JUST INBOARD OF NR 5 SPOILER AT WBL 71.24. MAINTENANCE STOP DRILLED CRACK ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL WBL 71.24Dec 2, 2003 · N174AW · Boeing 73733ASDR DHL2003742505Attach Angle · corrodedDURING C-CHECK, N/R 60695 NR 7 SPOILER FITTING FWD ATTACHMENT ANGLES AT FALSE SPAR ARE CORRODED AND CRACKED WITH LOOSE AND PULLING FASTENERS. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA AT NR 7 SPOILER FITTING FWD ATTACHMENT ANDec 2, 2003 · N742DH · Boeing 727225SDR DHL2003742504Support Angle · crackedDURING C-CHECK, N/R 60546 LT WING PLANK FAIRING SUPPORT ANGLE AT NR 3 FLAP TRACK PORTION IS CRACKED WBL 203 AND SPOILER BEAM. CUT OUT DAMAGED AREA AT NR 3 FLAP TRACK MOUNT DIMENSIONS 5.5 INCH X 3 INCH AND FABRICATED ONE FILLER DIMENSION AND FABRICATED ONE STRNov 30, 2003 · N742DH · Boeing 727225SDR DHL2003802549Angle · crackedRIGHT OUTBD STUB WING WEB REINFORCING ANGLE CRACK 2.000, STA XS 503.000. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-Nov 28, 2003 · N802DH · Doug DC873SDR DHL2003802550Bracket · crackedNR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 1, SRM 51-1-21 PG 1.Nov 25, 2003 · N802DH · Doug DC873SDR DHL2003802548Bracket · crackedNR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 21, 9 AND SRM 51-1-21 PG 1.Nov 25, 2003 · N802DH · Doug DC873SDR DHL2003742530Stiffener · crackedDURING C-CHECK, RT WING L/E BL 92 INT FRAME VERT STIFFENER IS CRACKED ON BOTTOM THRU FASTENER HOLE. CUT OUT DAMAGED AREA DIM 2.5 X 2 INCH IAW B-727 SRM 51-40-4. FABRICATED NEW FILLER IAW B-727 SRM 51-40-4. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALNov 24, 2003 · N742DH · Boeing 727225SDR DHL2003802533Bracket · crackedRIGHT WING NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9, 21.Nov 24, 2003 · N802DH · Doug DC873SDR DHL2003802532Bracket · crackedLEFT WING CTR L/E NR 1 ENG FIREWALL S/O VALVE SUPPORT ARM BRACKET CRACKED. REMOVED CRACKED BRACKET FROM NR 1 ENG FIREWALL S/O VALVE SUPPORT ARM AND FABRICATED A NEW ONE IAW SRM 51-3-0 PG 1, SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTANov 24, 2003 · N802DH · Doug DC873SDR DHL2003802545Bracket · crackedRIGHT WING NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING NR 4 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9, 21.Nov 24, 2003 · N802DH · Doug DC873SDR DHL2003802529Clip · crackedNR 2 MAIN TANK CLIP CRACK 4.000, STA XRS 22.750 BETWEEN S-5L AND REAR SPAR. REMOVED CRACK CLIP AND INSTALLED A NEW ONE AT STA XRS 22.750, BETWEEN S-5L AND REAR SPAR (NR 2 MAIN TANK) IAW SRM 51-1-20D PG 21, 9 REFER TO NR 1467 FOR LEAK CHECK.Nov 18, 2003 · N802DH · Doug DC873SDR 2003FA0001201Tab · brokenOUTBOARD RIB OF EACH CANARD WING CRACKED. OUTBOARD TAB LEFT SIDE CANARD BROKEN IN TWO. OUTBOARD HINGE TAB OF RT CANARD WING CRACKED.Nov 18, 2003 · N29821 · Cessna 182PSDR DHL2003802522Fitting · crackedRT WING L/E FITTING (ZEE PAN) CRACKED 2.000, STA XW 454.000. REMOVED AND REPLACED FITTING (ZEE PAN) ON RIGHT WING L/E, STA XW 454.000 IAW SRM 51-1-20D PG 9, 21.Nov 17, 2003 · N802DH · Doug DC873SDR ASAA0380747Bracket · brokenOKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE AT APPROX XRS 100 CABLE BRACKET BROKEN. REPAIRED PER ASA EA 5740-01365 AND AAR EA 10105. (M)Nov 14, 2003 · N960AS · Doug DC983SDR AWXA200301500Panel · chafedMCN - MINOR REPAIR - DURING C-15 CHECK FOUND THE RT WING OUTBOARD FLAP WELL BOX PANEL CHAFED AT RS 275.03. MAINTENANCE REMOVED THE RT WING OUTBOARD FLAP WELL BOX PANEL AT RS 275.03; FABRICATED A NEW REPLACEMENT PANEL; INSTALLED REPAIR PART IAW AWA ER 03-5752-Nov 13, 2003 · N305AW · Boeing 7373G7SDR WVE2003F00021Support Bracket · crackedWHILE INSTALLING LT WING AILERON CABLES, THE LT FLAP ACTUATOR UPPER AND LOWER SUPPORT BRACKETS WERE FOUND TO BE CRACKED. THESE BRACKETS ARE UNDER ACCESS PANEL 540EB WHICH IS NOT REQUIRED TO BE REMOVED FOR 1200 HOUR INSPECTION. REMOVE PANELS 540EB ON LT WING Nov 12, 2003 · N235FX · Lear 60LEARSDR TSAA0353209Vent · corrodedBLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. FABRICATED A .020 INCH EXTERNAL DOUBLER FROM 7075-T6. ALODINED AND ONE COAT BMS 10-11, TYPE I PRIMER TO REPAIR PARTS AND EXPOSED SURFACNov 11, 2003 · N818AL · Boeing 737230SDR A6WA200340167Beam · damagedLT OB FLAP HAS THE OB HING BEAM DAMAGED BY A SCREW BETWEEN THE HINGE AND THE FITTING. CLEANED DAMAGED AREA, BLENDED SMOOTH, PERFORMED ROTO/FLAP PEEN OF REPAIR AREA, ALODINED AND TREATED IAW ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4391.Nov 11, 2003 · N401AW · Cndair CL6002B19SDR 2004FA0000029Stiffener · crackedDURING A ROUTINE INSPECTION, A MECHANIC NOTED THE AFT STIFFING CHANNEL, PN 62086-002, CRACKED AT THE MIDDLE LIGHTENING HOLE. ADDITIONAL INSPECTION REVEALED NO FURTHER DAMAGE. THE CRACKS APPEAR NEW. THIS CRACK IS NOT TYPICAL OF THE CRACKS FOUND PREVIOUSLY. Nov 5, 2003 · N430PA · Piper PA28181SDR DHL2003807554Fitting · crackedNR 3 MAIN TANK INTERIOR FITTING CRACKED STA XRS 22.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM PO201734, DWG 5615910. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW FITTING IAW ATM PNov 3, 2003 · N807DH · Doug DC873FSDR DHL2003802539Support Angle · crackedLEFT WING RIB OTBD STUB WING SUPPORT ANGLE CRACKED 0.500 AT STA XS 520.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW SUPPORT ANGLE IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED SUPPORT ANGLE IAW SRM 5Nov 1, 2003 · N802DH · Doug DC873SDR DHL2003807530Splice · crackedRIGHT WING SPLICE FITTING LOWER PLATING CRACKED AT STA XW 408.000, S-59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-20D. REMOVED SPLICE FITTING (CRACKED) IAW SRM 51-1-20D PG 21. INSTALLED NEW SPLICE FITTING ON RIGHT WING, STA XW 408Oct 25, 2003 · N807DH · Doug DC873FSDR DHL2003807533Clip · crackedNR 4 MAIN TANK INTERNAL PART CLIP CRACKED STA XRS 172.000, S-74, REF ACCESS DOOR 505D. REMOVED AND REPLACED CRACKED CLIP ON NR 4 MAIN TANK INTERNAL PART STA XRS 172.000, S-74 (ACCESS DOOR 505D) IAW SRM 51-1-20D. FOR LEAK CHECK SEE NR 1482.Oct 24, 2003 · N807DH · Doug DC873FSDR DHL2003807532Clip · crackedNR 4 MAIN TANK INTERIOR (1EA) CLIP CRACKED, STA XRS 172.000 S-75R (INSIDE ACCESS DOOR 505D). REMOVED AND REPLACED (1EA) CRACKED CLIP IN NR 4 MAIN TANK STA XRS 172.000 S-75R, REF ACCESS DOOR 505D IAW SRM 51-1-20D PG 21, 9. REFER TO NR 1482 FOR LEAK CHECK.Oct 24, 2003 · N807DH · Doug DC873FSDR DHL2003807535Clip · crackedNR 4 MAIN TANK INTERNAL PART CLIP CRACKED AT STA XRS 172.000, S-73 (REF ACCESS DOOR 505D). REMOVED AND REPLACED CRACKED CLIP ON NR 4 MAIN TANK INTERNAL PART STA XRS 172.000 S-73 (ACCESS DOOR 505D) IAW SRM 51-1-20D. FOR LEAK CHECK SEE NR 1482.Oct 24, 2003 · N807DH · Doug DC873FSDR DHL2003807534Clip · crackedNR 4 MAIN TANK INTERIOR (1EA) CLIP CRACKED, STA XRS 172.000 S-76R (INSIDE ACCESS DOOR 505D). REMOVED AND REPLACED CRACKED CLIP IN NR 4 MAIN TANK STA XRS 172.000 S-76R (REF ACCESS DOOR 505D) IAW SRM 51-1-20D PG 21, 9. REFER TO NR 1482 FOR LEAK CHECK.Oct 24, 2003 · N807DH · Doug DC873FSDR 03FDEA01798Angle · mismanufacturedRIGHT WING FRAME NR 40 HAS NUMEROUS HOLES DRILLED THRU FUSELAGE SKIN ONLY. THAT IS OUT OF ROUND/ELONGATED. ACCOMPLISHED WORK CARD EA6-5310-7-5003 02 PT4 AND EA6-5310-73419A AT CWF BY DRILLING FASTENER HOLES TO CORRECT SIZE AND INSTALLING PICKUP ANGLE TO ENGIOct 24, 2003 · N442FE · Airbus A310203SDR 03FDEA01797Angle · misrepairedLEFT WING RIB NR 40 HAS 24 EA EXISTING HOLES THAT IS ( 2-AND) OVERSIZE IN FRAME 40. PICKUP ANGLE C/T FUEL TANK EO6-5310-7-5003 WORK INSTRUCTION - DRILL HOLES TO THE (1ST) OVERSIZE. COMPLIED WITH WORK CARD (EA6-5310-7-5003 02 PT3) , EA6-5310-73418, EA6-5310-Oct 24, 2003 · N442FE · Airbus A310203SDR QXEA200301371Stiffener · chafedPDX- PANEL 524AT HAS CHAFED STIFFENER, SECOND STIFFENER FROM OUTBOARD END FORWARD SIDE OF LEFT HAND WING. REPAIRED IAW DHC-8 RD 8-57-1568.Oct 22, 2003 · N379PH · Dhav DHC8202SDR DHL2003807503Support Angle · crackedLEFT OUTBD L/E STUB WING SUPPORT ANGLE CRACKED AT STA XOLDO 67.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D PG 21. FABRICATED NEW ANGLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE ON LEFT OUTBD L/E STUB WINGOct 10, 2003 · N807DH · Doug DC873FSDR PCZ2003F00000Brace · corrodedDURING A 100 HOUR INSPECTION, THE UPRIGHT VERTICAL BRACE AT STATION 61 IN THE LEFT WHEEL WELL WAS FOUND CORRODED AND CRACKED. THE CORROSION WAS INTERNAL. THE BRACE (TUBULAR) WAS CRACKED COMPLETELY AROUND ITS CIRCUMFERENCE AT TWO PLACES APPROXIMATELY FOUR INCOct 10, 2003 · N445DM · Beech TC45GSDR DHL2003807511Clip · crackedLEFT WING CTR L/E FORMER CLIP CRACKED AT STA XOLD 6.2246. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED CLIP (2024-T3AL 0.050) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 57-2-0 PG 9, 10, SRM 51-3-0 Oct 7, 2003 · N807DH · Doug DC873FSDR 03FDEA01682Vent · crackedLT WING FWD VENT BOX TAB CRACKED AT STA. 656.60. REPAIRED IAW EA 7-5710-55011.Oct 2, 2003 · N468FE · Boeing 727200SDR SWIA200312555Clip · crackedFOUR CRACKED SKIN SUPPORT CLIPS ON RT WING, RIB 15 LOWER SURFACE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FOUR SKIN SUPPORT CLIPS ON RIGHT WING, RIB 15 LOWER SURFACE PER SRM 51-40-02 AND RII 57-301.Sep 30, 2003 · N565SW · Emb EMB120ERSDR ABXA030395Attach Fitting · crackedINBOARD RIB OF NR 5 SLAT DRIVE LINK HAD AN AFT ATTACH FITTING ATTACHED VERTICALLY TO SPAR AND RIB CRACKED IN 3 PLACES. REPAIRED ATTACH FITTING IAW DC-9 SRM 57-09.Sep 27, 2003 · N906AX · Doug DC931SDR AWXA200301117Angle · crackedMCN - MAJOR REPAIR - DURING C-07 CHECK THE LEFT WING LEADING EDGE SUB SPAR TO RIB ANLE WAS FOUND CRACKED NEAR NR 3 UPSTOP PAD AT LT RIB 15 STA. 8268 . MAINTENANCE REMOVED,FORMED,AND INTALLED LEFT WING LEADING EDGE SUB SPAR TO RIB ANGLE IAW A320 SRM 51-42-11 PASep 26, 2003 · N619AW · Airbus A320232SDR 03FDEA01647Stiffener · crackedRT WING FUEL TANK RIB, OB VERTICAL STIFFENER CRACKED, UPPER END, WS 171.5 BETWEEN STR 9 AND STR 10. REMOVED DAMAGED VERTICAL RIB STIFFNER AT WS 171.5 BETWEEN STR 9 & 10 RIGHT. DRILLED UP & INSTALLED NEW STIFFNER (P/N 65-8338-30) IAW SRM 51-30-5, SRM 51Sep 26, 2003 · N469FE · Boeing 727200SDR AUS20031200Flying Wire · failed(AUS) FLYING WIRE BROKEN. INVESTIGATION FOUND FLYING WIRES WERE UNDERSIZE. AIRCRAFT IS AMATEUR BUILT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Sep 21, 2003 · Amtr RV8SDR DHL2003749516Stiffener · crackedDURING C CHECK, DISCREPANCY AS FOLLOWS N/R 64533 W.B.L. 70 LT. WING LE VERT. STIFFENER BOTTOM END CRACKED. REMOVED LEFT LT WING PANEL. REMOVED FASTENER FOR ACCESS BOTTOM SIDE OF VERTICAL STIFFENER. STOP DRILL CRACK BOTTOM END OF VERTICAL STIFFENER. ACCOMPSep 20, 2003 · N749DH · Boeing 727200
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