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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL2004803520Clip · crackedLT WING CTR L/E UPPER INTERNAL PART FORMER DOUBLER CLIP CRACKED 0.500 XFS 427.000. REMOVED CRACKED CLIP IAW SRM 51-1-21 PG 1. FABRICATED NEW CLIP (ALCLAD 2024-T3 0.063) IAW SRM 57-2-0 PG 1, 2. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. SDR UPS04842162Angle · crackedINSPECTION TYPE:C3 LEFT WING I/B STUB WING VERTICAL ANGLE IS CRACKED AT LOWER END AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.SDR UPS04842117Angle · crackedINSPECTION TYPE: C3, RT WING L/E STUBWING HAS VERTICLE ANGLE CRACKED AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753295 AND SRM 51-1-20D, 51-3-0.SDR UPS04842116Stiffener · crackedINSPECTION TYPE: C3, LT WING I/B STUB WING HAS VERTICLE STIFFENER CRACKED AT LOWER END AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.SDR DHL2004803527Bracket · crackedNR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET (NR 1 ALT TANK) IAW DC8 SRM 51-1-20D PG 9, 21.SDR DHL2004740004Channel · corrodedCORROSION ON CHANNEL LOCATED IN RIGHT-HAND LEADING EDGE WING WELL STA 220 THRU STA 224. REMOVED DAMAGE, INSTALLED MINOR EXTRUDED REPAIR IAW B-727 SRM 51-40-4.SDR DXTA200400271Tape · looseCLIMBING THROUGH APPROXIMATELY FL280, EXPERIENCED A SEVERE LONGITUDINAL OSCILLATION. THE YOKE OSCILLATED LEFT AND RIGHT RAPIDLY AND WINGS WERE FLEXING 4 TO 6 INCHES, DISCONNECTED AUTOPILOT WITH NO POSITIVE AFFECT, CONDITION IMPROVED BY SLOWING DOWN THE AIRCRAFSDR QXEA200400227Attach Bracket · crackedPDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX98-75. REPAIRED IAW RD 8/4-57-177.SDR QXEA200400228Attach Bracket · crackedPDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX135.25. REPAIRED IAW RD 8/4-57-177.SDR MWEA040025Angle · corrodedCORROSION ON ANGLE SUPPORT BRACKET ON RIGHT FLAP TRAILING EDGE AT RIGHT WING STATION XCW 104.5. FABRICATED AND INSTALLED REPAIR ANGLE.SDR 2004FA0000399Strap · crackedDURING AN ANNUAL INSPECTION THE BUTT WELDS IN THE LOWER MAIN SPAR REINFORCEMENT STRAP. APPROX 6.50 INCHES IB FROM EACH END OF THE REINFORCEMENT STRAP. DO NOT HAVE PROPER PENETRATION AND ARE CRACKED THRU THE WELD. MFG WAS CONTACTED AND REPAIR INSTRUCTIONS WERSDR 2004FA0000398Strap · crackedDURING AN ANNUAL INSPECTION THE BUTT WELDS IN THE LOWER MAIN SPAR REINFORCEMENT STRAP, APPROX 3.25 INCHES IB FROM EACH END OF THE REINFORCEMENT STRAP, DO NOT HAVE PROPER PENETRATION AND ARE CRACKED THRU THE WELD. MFG WAS CONTACTED AND REPAIR INSTRUCTIONS WERESDR 04FDEA00624Bracket · corrodedLEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-75296 TITLE: WINGS - O/B TRAILING EDGE FLAPS - I/B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR.SDR AWXA200400279Angle · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK .625 INCH CRACK WAS FOUND ON RT WING OUTBOARD EXHAUST GATE ANGLE WBL 205. MAINTENANCE REMOVED CRACKED RT WING OUTBOARD EXHAUST GATE ANGLE AT WBL 205; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW AWA ER 0SDR UPS04842190Channel · crackedINSPECTION TYPE:C1 HAT CHANNEL FWD OF J-HOOK (FOR MLG DOOR RELEASE) IS CRACKED. REMOVED CRACKED HAT CHANNEL, FABRICATED NEW HAT CHANNEL IAW DAC DWG S-1 289798, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW HAT CHANNEL IAW DC8 SRM 51-3-1.SDR AWXA200400282Intercostal · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND ON INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AND BS 251.6, STR 21 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AND BS 251.6, STR 21 LT; FABRICATED A NESDR DHL2004750037Stiffener · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WBL 92 INT FRAME INBOARD SIDE UPPER STIFFENER 1ST FWD OF SPAR HAS UPPER END CRACKED. CUT OUT DAMAGE AREA & FABRICATED DOUBLER FROM 2024 T3 .040 PO 900226, 7 X 1.5 X 1.5 INCH, FILLER FROM 2024T3 .0SDR DHL2004750030Stiffener · crackedDURING C-CHECK, LEFT WING FRONT SPAR & WBL 92.8 VERTICAL STIFFENER CRACK INDICATION FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2, STOPDRILLED CRACK AT LEFT WING FRONT SPAR VERTICAL STIFFENER IAW B727 SRM 51-10-1, FABRICATED ANGLE REPAIR SDR DHL2004750029Stiffener · crackedDURING C-CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 1ST FWD OF SPAR HAS LOWER END CRACKED THRU FASTENER. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075-T6 .040 PO 900226 DIM 5 X 2 X 2 INCH AND DOUBLER FROM 7075-T6 .050 PO 900489 DIM 7 X 2 X 2 INCHSDR DHL2004750028Attach Angle · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WS 130.7 INBOARD SIDE OF INT FRAME UPPER ATTACH ANGLE HAS 12 INCH CRACK IN RADIUS. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 2024-T3, .050, 7 X 2 INCH, PO 900641 IAW B727SDR UPS04841989Pad · corrodedDROP CORROSION ABOVE WING BOTTLE BOLT, LOCATED IN RIGHT W/W FWD BULKHEAD, UPPER O/B CORNER. REMOVED RIGHT OVERWING EMERGENCY HATCH AND PANEL 292F TO FOM. REMOVED CORRODED PAD FROM RIGHT WHEEL WELL IAW DC8 SRM 51-1-20D. INSTALLED PAD AND PANEL 292F IAW DC8 SSDR C2XA04SH092Channel · crackedSHV- DURING C-CHECK THE RIGHT WING UPPER NUT PLATE CHANNEL ON SPAR 1 WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CALA0400140Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN BRACKET AT LT WING TRAILING EDGE JUST AFT OF NR 1 ENGINE PYLON BULB SEAL. A NEW BRACKET WAS INSTALLED IAW BOEING DRAWING 115A2982 AND SRM 51-40-02.SDR SWAA040503Web · crackedDURING SCHEDULED D CHECK, FOUND LT WING FSS 223, INBOARD OF FITTING (D) CRACKED AT WEB CHORD. REMOVED AND REPLACED WEB CHORD PER SRM AND ER.SDR GKZR200482306Clip · crackedLEFT WING UPPER CLIP INSIDE NR 1M ACCESS HOLE 505C AT STA 252-351 BETWEEN REAR SPAR NR 1 STRINGER CLIP CRACKED. REMOVED LT UPPER WING CLIP INSIDE NR 1 MAIN TANK ACCESS HOLE 505C AT STA 252-351 ON STRINGER NR 1. FABRICATED AND INSTALLED REPLACEMENT PART IAW DCSDR 0479Fitting · crackedDURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61.SDR 04FDEA00402Bracket · crackedRIGHT WING O/B FLAP I/B HINGE AFT FAIRING (FLAP SIDE) AFT SUPPORT BRACKET FOUND CRACKED. RT WING O/B FLAP I/B HINGE AFT FAIRING - CRACKED AFT SUPPORT BRACKET REMOVED. FABRICATED AS PER DRWG ARC4230 (REF EARN 047) & INSTALLED AS PER AMM 20-50-02.SDR CALA0400086Bracket · crackedINSPECTION FOUND LT WING X-SUPPORT BRACKET AT T/E BETWEEN UPPER AND LOWER PANELS O/B OF GROUND SPOILER ACTUATOR CRACKED AT STA XW 99.016. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-05.SDR 04FDEA01719Cap · crackedRIGHT AND LEFT WING UPPER CAP CRACKED AT XORS 372. THE CRACKS ARE AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED. REPAIR ANGLE AND DOUBLERS HAVE BEEN INSTALLED IAW FEDEX EA 8-5710-73236.SDR DHL2004806570Intercostal · crackedRIGHT WING T/E INTERCOSTAL LWR SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED INTERCOSTAL (7075-T6AL 0.090) IAW SRM 57-1-0. HEAT TREATED IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA ANDSDR DHL2004806569Intercostal · crackedLEFT WING T/E INTERCOSTAL LOWER SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (7075-TO-0.090) IAW SRM 57-1-0 PG 1. HEAT TREATED NEW INTERCOSTAL IAW SRM 51-1-1 PG 11, 13-21. CLEANED, TREASDR SWIA200412820Support · crackedA 7 INCH CRACK IN RIGHT WING INBOARD LEADING EDGE SUPPORT. DISCOVERED DURING LINE INSPECTION. REPLACED RIGHT WING INBOARD LEADING EDGE INBOARD SUPPORT IAW SRM 51-40-02.SDR SWIA200412974Clip · crackedLEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301.SDR DHL2004806557Clip · crackedNR 3 MAIN TANK CLIP CRACK 1.000 BETWEEN REAR SPAR AND S-51, XRS 22.750. REMOVED CRACKED CLIP (NR 3 MAIN TANK XRS 22.750). CLEANED, TREATED AND APPLIED COATING MATERIAL TO CLIP AND AREA IAW SRM 51-1-12 PG 7-21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9.SDR 2004F00259Washer · out of positionRT WING CENTER SECTION MAIN SPAR UPPER FITTING HAS A DEPRESSION, DUE TO THE WASHER NOT PROPERLY IN PLACE. DEPRESSION BLENDED TO A SMOOTH PROFILE WITH A .125 FINISH, ALL WORK DONE IAW FIELD REPAIR FR-KA-01188, REV A. (M)SDR DHL2004745007Bracket · crackedCOVE PANEL BELOW BELOW NR 2 SPOILER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW B-727 SRM 51-30-2.SDR 2004FA0000256Hinge · wornRECEIVED 2 NEW HINGES FROM API WITH EXCESSIVE PLAY BETWEEN PIN AND HINGE HALFES. DATE CODES: 12/23/03 AND 01/16/04. HINGES ARE MADE BY AC MFG.SDR QXEA200400047Bracket · crackedPDX - FRONT SPAR BLEED AIR ATTACH BRACKET CRACKED AT TOP, 2 RIVETS AT WS YW45.00 RIGHT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-11.SDR SWIA200412844Bracket · crackedLEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME.SDR UPS04841746Clip · crackedINSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED, APPROX STATION XW 485. REMOVED, FABRICATED AND INSTALLED CLIP IAW DWG 5804007 AND SRM 51-1-20D.SDR UPS04841722Clip · crackedINSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE AT NR 4 PYLON IS CRACKED IN NR 4 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5804007 AND SRM 51-1-20D.SDR UPS04841721Clip · crackedINSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 61 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED AT NR 1 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED SLIP IAW DWG 5804007 AND SRM 51-1-20D.SDR DHL2004752505Stiffener · corrodedDURING C-CHECK, RT WING HAS L/E OF FRONT SPAR VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER IAW B-727 SRM 51-30-2. FABBED NEW FROM BAC 1517-1406 PO 3448268 DIM 32 INCHES AND FILLER (SHIM) FROM 7075-T6 .190 PO 314676 DIM 27.5 X 1.5 INCH IAW B-727 SRM 57-10-2SDR 04FDEA00050Angle · corrodedRIGHT WING L/E AT NR 6 K-FLAP OPENING, L/E LOWER SURFACE, PANEL TO SEAL RETAINER ANGLE IS EXFOLIATED (BELOW & FWD OF NR 6 K-FLAP ACTUATOR). REMOVED SEAL RETAINER ANGLE IAW 727 SRM 51-30-2. FABRICATED NEW SEAL RETAINER ANGLE IAW 727 SRM 51-20-1 FROM BAC 1506-SDR 04FDEA00017Support Bracket · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE FOUND CORROSION. CORROSION ON LT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE SURFACE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES - LT O/B FLAP SDR COOSDR030059Splice · crackedRT WING, REAR SPAR LOWER CHORD SECTION, OUTBOARD SPLICE PN 6550821144 CORRODED AND CRACKED.SDR COOSDR030049Channel · corrodedRT WING TRAILING EDGE CAVITY UPPER FIXED PANEL CHANNEL CORRODED.SDR COOSDR030043Angle · corrodedRT WING, TRAILING EDGE - RSS486, ANGLE CORRODED.SDR 03FDEA02225Strap · crackedCRACK FOUND ON THE LOWER EDGE OF THE BOTTOM BOLT HOLE / OUTBD FLAP INBOARD HINGE TENSION STRAP SUPPORT - LT WING. DAMAGED HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. NEW TENSION STRAP INSTALLED AS PER SRM 51-33-01 VOL. II. REFER TO FEDEX EO 1-5SDR QXEA200301561Attach Bracket · crackedPDX - LT WING LEADING EDGE 511AL OUTBOARD LOWER ATTACH BRACKET SHOWS EVIDENCE OF CRACKING. REPAIRED IAW DHC-8 SRM 51-40-00.
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