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 UPS04842407Fitting · crackedINSPECTION TYPE:C1 NR 1 ALT. TANK AT XRS 440 APPROX. STRINGER 59 FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW DWG.5644972, 3645612 AND SRM. 51-1-20D.SDR UPS04842410Fitting · crackedINSPECTION TYPE:C1 NR 4 ALT TANK HAS STRINGER 59 FITTING CRACKED AT XRS 428 AND XRS 440 REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 5644973 AND SRM. 51-1-20D.SDR SWIA200413524Bracket · crackedLEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413523Bracket · crackedLEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02.SDR SWIA200413494Support Bracket · crackedRIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02.SDR SWIA200413491Support Bracket · corrodedRIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02.SDR SWIA200413490Support Bracket · crackedRIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413489Support Bracket · crackedRIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413488Support Bracket · crackedRIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413487Support Bracket · crackedRIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02.SDR SWIA200413486Support Bracket · crackedRIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413484Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02.SDR SWIA200413483Support Bracket · crackedLEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.SDR SWIA200413482Support Bracket · crackedLEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.SDR SWIA200413481Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR QXEA200400319Nut Plate · brokenPDX - RT WING FUEL PANEL 623AT HAS ONE BROKEN NUTPLATE. REPAIRED IAW Q400 AMM TASK 57-11-01-400-801, PARAGRAPH 1, 2, 3 AND 4C.SDR 04FDEA01131Strip · tornRIGHT WING DLE CHAFE STRIP TORN WITH MISSING SECTION. REMOVED, FABRICATED CHAFE STRIP AND INSTALLED IAW DPS 4.710 & SRM 51-31-01 AT MAE.SDR CALA0400437Angle · wornLEFT WING TRAILING EDGE PANEL WORN JUST INBOARD OF NUMBER 3 FLAP TRACK FAIRING. REMOVED AND REPLACED ANGLE PER SRM 51-10-02.SDR WVE2004F00011Angle · crackedLT WING STA 48.30 ANGLE PN 600-1020427 IS CRACKED 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.SDR WVE2004F00010Angle · crackedRT WING STA 48.30 ANGLE PN 600-1020428 IS CRACKED , 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.SDR UIEA200400079Angle · crackedFOUND RT WING T/E LOWER ACCESS PANEL SUPPORT BEAM AFT L-ANGLE CRACK AT WS 670. REPLACED CRACKED PANEL SUPPORT BEAM ATTACH CLIP 'L' ANGLE WRT SRM 51-30-02. (M)SDR UIEA200400062Bushing · crackedFOUND LEFT WING WALKING BEAM SUPPORT FITTING ASSEMBLY. FORWARD BEARING HOUSING OUTBOARD UPPER/FWD BOLT HOLE LOCATION ON REAR SPAR STIFFENER WAS FOUND WITH A CRACKED BUSHING HOLE AND BUSHING WAS ALSO FOUND WORN. CRACKED HOLE REPAIRED AS PER SB 747-57-2226 REVSDR UIEA200400066Angle · crackedFOUND RIGHT WING T/E UPPER FIXED PANEL HORIZONTAL SUPPORT BEAM L-ANGLE CRACKED AT WING STATION 400. REPLACED CRACKED ANGLE WRT SRM 51-30-02. (M)SDR 04FDEA01019Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 04FDEA01018Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 04FDEA01017Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR ASAA0480345Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1361C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480348Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1303 RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUB STRIP PER EA 5720-01248. (M)SDR ASAA0480352Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1371C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480347Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1363C RUBSTRIP DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480346Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1367C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480349Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1355C RUBSTRIP IS DISBONED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480350Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1357C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR ASAA0480351Rub Strip · debondedOKC - DURING HV CHECK, FOUND WING PANEL 1379 RUBSTRIP IS DISBONDED. REAMED HOLES. INSTALLED PRP BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)SDR 04FDEA01012Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019, TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 04FDEA01011Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 04FDEA01010Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 04FDEA01009Support Bracket · corrodedLT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR DHL2004802003Flange · damagedSTA 966 INBOARD VERTICAL FLANGE OF SUPPORT, THERE IS A CRACK 2.5 INCHES LONG, FORWARD OF AFT BOLT. ACCOMPLISHMENT OF PERMANENT REPAIR REQUIRED BY 30 APR 04. STA. 966 XW3 THE INBOARD VERTICAL FLANGE OF THE SUPPORT, THERE IS A CRACK 2.5 INCH LONG, FORWARD OF ASDR ASAA0480287Angle · crackedOKC - FOUND DURING HV CHECK, FOUND LEFT WING LEADING EDGE ATTACH ANGLE IS CRACKED AT STATION XRS 164. REPLACED ANGLE PER SRM 51-10-2. (M)SDR CALA0400403Hinge Fitting · brokenRT WING DOOR LWR HINGE FITTING IS BROKEN AT NR 6 FLAP TRACK. REPLACED DOOR HINGE IAW SRM 51-40-02.SDR SWIA200413247Structure · crackedLEFT WING SECTION 48.30 PART NUMBER IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION.SDR SWIA200413246Angle · crackedRIGHT WING SECTION 48.30 ANGLE PART NUMBER 600-10204-28 IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION.SDR SWIA200413264Clip · crackedMIDDLE LOWER SKIN CLIP CRACKED AT RIB 16, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED MIDDLE LOWER SKIN CLIP AT RIB 16 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR SWIA200413263Clip · cracked2 ND FROM AFT LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED 2ND FROM AFT LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR SWIA200413262Clip · crackedMIDDLE LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. DISCOVERED DURING C-CHECK INSPECTION. REPLACED MIDDLE LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR DHL2004803528Clip · crackedNR 4 ALT TANK (1EA) CRACKED CLIP BETWEEN STA XW 495.665 AND CTR WING SPAR CORNER. REMOVED AND REPLACED CRACKED CLIP BETWEEN STA XW 495.665 AND CTR. WING SPAR (NR 4 ALT TANK) IAW DC8 SRM 51-1-20D PG. 21-9. REFER TO NR 0341 FOR LEAK CHECK.SDR DHL2004803529Bracket · crackedNR 4 ALT. TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET IAW DC8 SRM 51-1-20D PG. 21,9. REFER TO NR. 0341 FOR LEAK CHECKSDR DHL2004803525Angle · crackedLT WING OUTBOARD FLAP UPPER RT PART TEE ANGLE CRACKED 1.500 AT STA XF 164.000. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-0 PG 1-2. FABRICATED FILLER (AL 7075-T6 0.063) IAW SRM 57-2-0 PG 1-2. FABRICATED DOUBLER (AL 7075-T6 0.063) IAW SRM 57-2-0 PG 1-2. CLEANED,SDR DHL2004803524Support · crackedAFT BOOSTER PUMP SUPPORT CRACK. REMOVED AND REPLACED AFT BOOSTER PUMP SUPPORT IAW DC8 SRM 51-1-20D PAGE 219.
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