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 QXEA9900942Strap · gougedPDX - SCREW GOUGE IN LOWER WING BUTT STRAP AT FORWARD END. REPAIRED IAW HORIZON AIR EA 4-57-226, STEP 2.SDR MWEA99223Clip · corrodedRIGHT WING TANK LOWER SHEAR CLIP STR 11 AND REAR SPAR IS CORRODED STA XRS 137. FABRICATED AND INSTALLED REPAIR CLIP.SDR ABXA9900269Fitting · crackedKEEL WEB FORWARD ATTACH ANGLE FITTING CRACKED AT LEFT SIDE. REPLACED ANGLE IAW DC9 SRM 51-30-3 AND 51-30-1.SDR EIA990149Fitting · crackedMZJ - DURING C-CHEC, THE LEFT WING OUTBOARD TRAILING EDGE CONE WAS FOUND TO HAVE A CRACK IN THE FITTING. REMOVED AND REPLACED PER DC-9 SRM 51-10-1 PAGE 4-6. INSTALLED FITTING AND WEB AT STATION 164 PER 51-30-2 PAGE 1-14. (M)SDR DHL9970130DAngle · crackedAT D-CHECK, RIGHT I/B LEADING EDGE WEB AT LEADING EDGE STA 130 I/B SIDE UPPER OLD ANGLE REPAIR CRACKED. REMOVED ANGLE REPAIR, INSTALLED ANGLE REPAIR PER SRM 51-30-2, 12 X 3.SDR DHL9970129DAngle · crackedAT D-CHECK, RIGHT WING I/B LEADING EDGE STA 130 I/B LOWER ATTACH ANGLE CRACKED AT ATTACH FASTENER. REMOVED CRACKED ANGLE SUPPORT, REPLACED ANGLE SUPPORT AND INSTALLED ANGLE REPAIR PER SRM 51-30-2, 20 X 8.SDR SWAA990587Beam · crackedDURING SERVICE CHECK, WALKAROUND INSPECTION FOUND THE LEFT WING LOWER TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED BEAM PER SRM.SDR P5CA9900537Fairing · delaminatedFOUND DELAMINATED CRACK ON RT WING AFT SIDE FAIRING AT BL 1120. REPAIRED CORROSION PER SRM 51-40-09.SDR P5CA9900525Fairing · delaminatedRIGHT WING AFT SIDE FAIRING AT BL1120 FOUND DELAMINATED. REPAIRED PER SRM 51-40-09.SDR UPS99829297Doubler · crackedINSPECTION TYPE:C1, RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED FWD OF ACCESS PANEL 524B. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-21.SDR DHL9980718CFrame · crackedAT C-CHECK FOUND RT WING FLAP WELL AT STA 90.00 UPPER FRAME FOR L/E FLAP CONTOUR CRACKED. FABRICATED NEW COVER PANEL RT WING O/B FLAP L/E STA 90.00 IAW DC-8 SRM 51-1-7.SDR UPS99229215Chord · corrodedINSPECTION TYPE:C, CORROSION ON WING CENTER SECTION AFT LOWER CHORD RBL 42-48 AND AFT UPPER CHORD RBL 38-42. REPLACED UPPER AND LOWER CHORD PER SRM 51-30-2 AND ER 99-5195.SDR DHL9970132DWeb · crackedAT D-CHECK, RT WING L/E WEB AT WBL 92.8 FWD VERTICAL STIFFENER AT TAI DUCT SUPPORT HAD CRACK AT UPPER AND LOWER ATTACH HOLES. STOP DRILLED CRACK, HFEC, FABRICATED AND INSTALLED ANGLE REPAIR DOUBLER ON RT WING PER SRM 51-40-3, 1.5 X 3. CUT OUT CRACKED SECTIONSDR CALA9900296Stiffener · corrodedINSPECTION FOUND STIFFENER CORRODED AT RT WING FRONT SPAR FS 249. THE CORRODED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-02, PAGE 4.SDR ABXA9900342Clip · crackedRIGHT WING LEADING EDGE RIB CLIP CRACKED AT STATION XOLDI 6.225. REPLACED CLIP IAW DC8 SRM 57-3-0.SDR DHL9980743CFitting · crackedAT C CHECK, CENTER WING TANK, THROUGH LOWER ACCESS PANEL 516A RT SIDE BAY ON STA 46 STR 67 UPPER AREA CRACK ON FITTING APPROX 1 LONG. REMOVED AND FABRICATED FITTING PER DER DRAWING MHA 3123 AND INSTALLED PER SRM 51-120D. N/R 1234SDR ABXA9900338Angle · crackedRIGHT WING LEADING EDGE, INBOARD OF STATION XS 250.084 RIB AT THE AFT SIDE OF THE SLOT, VERTICAL ANGLE IS CRACKED. REPLACED VERTICAL ANGLE IAW DRAWING 5769859 AND DC8 SRM 57-3-3 AND 51-1-20D.SDR RRXA991008Fastener · shearedDURING A MAINTENANCE VISIT, FOUND SHEARED, WING, HI-LOCK SHEARED IN SKATE ANGLE NR 4 ALT TANK 508 CONT AT STA 58. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW FAA APPROVED TENNESSEE TECSDR ABXA9900340Fitting · crackedNR 2 MAIN TANK, INBOARD OF XRS 74 BULKHEAD, FORWARD STRINGER 51, END FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR CALA9900247Support · corrodedINSPECTION FOUND LT AND RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. THE BOLT HOLES WERE REPAIRED IAW ECRA 5743-01015.SDR AT9900206Fairing · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT WING UPPER TOP SIDE BEAVER TAIL CORRODED. REMOVED CORROSION, CUT OUT AREA AND INSTALLED SEALANT REPAIR IAW DC9 SRM 57-03 FIG 27.SDR HALA9900083Splice · crackedTUL - FOUND LEFT LONGERON 16 TO 22 SPLICE CRACKED INSIDE NR 1 FUEL TANK WING STATION XORS 372. INSTALLED AND SECURED SERVICEABLE LONG 16 TO 22 IAW AARD 51-01-00-05. (M)SDR GAIA99040Beam · corrodedDURING ROUTINE C-CHECK, CORROSION WAS FOUND IN THE MLG BEAM AT NR 4 FLAP TRACK OUTBOARD ATTACH POINT. THE CORROSION WAS REMOVED AND IT WAS DETERMINED TO BE BEYOND LIMITS. INSTALLED OVERSIZED BUSHING PER BOEING IPC. THE REPAIR WAS CARRIED OUT IAW AIA ENGINEESDR DL72W990476Angle · crackedCRACK ORIGINATING UNDER I/B UPSTOP PAD ON NR 7 SLAT ANGLE RUNNING I/B .25 INCH. REPAIRED PER MM 57-40-0 PAGE 816.SDR CALA9900204Bracket · crackedINSPECTION FOUND BRACKET CRACKED THROUGH AND A 2 INCH CRACK AT SPLICE INSIDE LT WING FIXED L/E AT JOINT BETWEEN NOSE RIBS, TEN INCHES O/B OF NR 2 SLAT O/B TRACK, XRS 254. AN ANGLE AND STRAP WERE INSTALLED IAW SRM 51-10-2, 51-00-00, 51-10-3, 51-30-2, AND 51-30SDR DL72S990407Stiffener · crackedTPA - LTR CHK C-1 02/26/99, WING LE SPAR STIFFENER CRACKED AT I/B SIDE NR 2 SLAT I/B TRACK BOX. REPLACED STIFFENER PER MM 57-20-21.SDR DHL9974130CAngle · crackedAT C CHECK, LEFT WING TRAILING EDGE TEMPORARY COVE PANEL SUPPORT ANGLE INSTALLED AT WS 543 CRACKED. REMOVED AND REPLACED ANGLES PER SRM 51-30-2, N/R 1422.SDR DHL9974129CAngle · crackedAT C CHECK, LEFT WING FIXED LEADING EDGE CAVITY UPPER OUTBD SUPPORT ANGLE AT SLAT STA 0 IS CRACKED AT AFT ATTACH FASTENERS. REMOVED ANGLE, FABRICATED NEW SUPPORT ANGLE, PER SRM 51-40-3, 16 BY 1.625, N/R 1390.SDR DHL9974107CAngle · crackedAT C CHECK, LEFT WING LEADING EDGE CAVITY INBD MOUNT SUPPORT ANGLE FOR THE NR 2 LEADING EDGE FLAP ACTUATOR IS CRACKED AT THE UPPER CORNER RADIUS. REPLACED MOUNT SUPPORT ANGLE PER SRM 51-30-2, 10 BY 6. REPLACED O/B MOUNT SUPPORT PER SRM 51-30-2, 10 BY 6, N/R SDR DHL9974101CHeat Shield · crackedAT C CHECK, LEFT WING LEADING EDGE INTERIOR ANTI-ICE HEAT SHIELD IS CRACKED AT 3 ATTACH RIVETS. CUT OUT DAMAGED SECTION INSTALLED DOUBLER PER SRM 57-30-4, 13 BY 7, N/R 1440.SDR AALA990397Casting · crackedTUL - FOUND CRACK IN RADIUS AND VERTICAL AREA OF LEFT 760 CASTING (BEHIND RIB). REPAIRED LEFT 760 CASTING PER BOEING SERVICE BULLETIN 727-57-0112 REV 5 LARGE REPAIR. (M)SDR UPS99829103Fitting · crackedINSPECTION TYPE:C3 NR 2 MAIN TANK, INBD SIDE OF THE XRS 74 BULKHEAD, THE FWD STR 51 END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.SDR QXEA9900445Angle · crackedPDX - RIGHT-HAND AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11.SDR QXEA9900444Angle · crackedPDX - LEFT-HAND AFT REAR WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11.SDR DHL9974155CChannel · crackedAT C CHECK, RT WING LOWER T/E PANEL SUPPORT CHANNEL CRACKED, O/B OF NR 14 SPOILER ACTUATOR STA 601. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2848.SDR DHL9974153CChannel · crackedAT C CHECK, RT WING LOWER T/E COVE PANEL I/B SUPPORT CHANNEL CRACKED I/B OF NR 12 SPOILER ACTUATOR STA 495. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2852.SDR DHL9974123CTip · gougedAT C CHECK, LEFT WING TIP LEADING EDGE THE INBD SIDE WHICH MATES NEXT TO SLAT IS GOUGED ON THE LOWER SURFACE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 51-30-2, 11 BY 8, N/R 1349.SDR UPS99829152Fitting · crackedINSPECTION TYPE-C123, NR 3 MAIN TANK O/B SIDE OF THE XRS 74 RIB, THE STRINGER AFT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.SDR UPS99829073Fitting · crackedINSPECTION TYPE-C123, THE NR 3 MAIN TANK I/B SIDE OF THE XRS74 RIB, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.SDR DHL9974156CAngle · crackedAT C CHECK, RT WING UPPER L/E INTERIOR WEB AT STA 0 O/B SUPPORT ANGLE CRACKED L/E STA 349. REMOVED AND FABRICATED SUPPORT ANGLE PER SRM 51-40-3 1, 65 BY 15, 65 N/R 2826.SDR AT9900356Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 209 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.SDR AT9900355Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 222 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.SDR AT9900354Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 238 BRACKET CORRODED. REMOVED AND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2.SDR ABXA9900195Strap · crackedRIGHT WING LEADING EDGE INNER BUTT SPLICE CRACKED AT LOWER AFT INBOARD END AT STATION XOLDI 6.225. REPAIRED IAW DC8 SRM 51-1-20 AND DWG 5769891.SDR UPS99828854Doubler · crackedINSPECTION TYPE-C123, RT WING L/E AT STA FS 564 AND 571 THE LWR I/B SKIN DOUBLER IS CRACKED IN 3 PLACES. REPAIRED AREA IAW SRM 57-3-3 FIG 6.SDR UPS99828833Clip · crackedINSPECTION TYPE-C3, LT WING L/E OUTBOARD ATTACH CLIP AT FS 520.168 IS CRACKED. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5769580 AND SRM 51-3-0.SDR QXEA9900446Angle · crackedPDX - RIGHT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-41-11.SDR UPS99829032Doubler · crackedINSPECTION TYPE-C1, NR 2 MAIN TANK I/B AFT ACCESS PANEL INTERNAL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-2 FIG 36.SDR UPS99828829Doubler · crackedINSPECTION TYPE-C3, LT WING L/E LWR SKIN DOUBLER IS CRACKED AT FS 570, AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.SDR TWAA9903103Angle · crackedDURING OP 15 MAINT CHECK, FOUND THE LT WING INBD AND OTBD SIDE OF OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLE CRACKED AT ATTACH HOLES. RIBS AND HINGE CASTING REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01.
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