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 DHL2005807531Fitting · crackedNR 2 MAIN TANK AFT FITTING CRACK 2.000 STA XRS 74.000 INBD SIDE S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL IAW SRM 51-1-12. INSTALLED NEW FITTING (PN SDR DHL2005807534Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACK 1.000, STA XRS 74.000 OUTBD SIDE, S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITSDR DHL2005807530Fitting · crackedNR 3 MAIN TANK FWD FITTING CRACK 1.000 STA XRS 74.000 S-51 (INBD SIDE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL IAW SRM 51-1-12. INSTALLED NEW FITTING (SDR DHL2005807532Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACK 1.000 STA XRS 74.000 AT INBD SIDE, S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FSDR QXEA200500942Shroud · crackedPDX - RT WING IB, LOWER TRAILING EDGE SHROUD 6TH FORWARD BRACKET FROM IB EDGE IS CRACKED. REPAIRED IAW RD 8/4-57-253 AND Q400 SRM 51-42-15.SDR QXEA200500941Shroud · crackedPDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD THIRD BRACKET FROM INBOARD END FORWARD BRACKET CRACKED. REPAIRED IAW RD 8/4-57-253.SDR QXEA200500849Bracket · crackedPDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD SECOND BRACKET FROM INBOARD END AFT BRACKET CRACKED. REPAIRED IAW RD 8/4-57-261.SDR QXEA200500850Diaphragm · crackedPDX - YW 191.20 AND TRAILING WING SHROUD NACELLE DIAPHRAGM CRACKED. REPAIRED IAW DHC8/400 SRM 51-42-05-330-801.SDR 05FDEA01241Plate · damagedLEFT WING LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND STA WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLE OVERSIZED AT 0.328, AND CARD E6-5710-7-5008 A PT 3 MOD REQUIRES TO REAM THESE HOLES TO 0.313 DIAMETER. COMPLIED WITH EA 6-5730-88784 PART 1 AND RAS/BAE/10SDR 05FDEA01239Plate · damagedRIGHT WING AILERON LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLES OVERSIZED AT 0.328 AND 0.371 DIAMETER, WORK CARD E6-5710- 7-5008A PT 4 REQUIRES THESE HOLES TO BE REAMED UP TO 0.313 DIAMETER. COMPLIED WITH EA 6-5SDR 05FDEA01230Support Angle · crackedLEFT WING LOWER T/E SUPPORT ANGLES CRACKED BELOW INBOARD END OF NR 4 SPOILER. REMOVED AND REPLACED INBOARD AND OUTBOARD SUPPORT ANGLES IAW SRM 51-30-2.SDR 05FDEA01212Support Angle · crackedLEFT WING LOWER FIXED T/E PANEL SUPPORT ANGLE CRACKED AT STA WS 522. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2.SDR USAA050550Angle · crackedBFM - FOUND LE WEB, LOWER ANGLE CRACKED .75 INCH LONG, LEFT WING INBOARD OF FUELING PANEL. DAMAGE AREA REMOVED, INSTALLED REPAIR STRAP, FILLERS AND DOUBLER PER SRM 57-41-13 FIG 202 AND 51-40-02. (M)SDR DHL2005741552Stiffener · bulgedVERTICAL STIFFENER AT R/W WBL 92 BULGED AT LWR END. REMOVED DAMAGED EXISTING DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-30-2 FABRICATED REPAIRED DOUBLER FOR VERTICAL STIFFENER AT R/W WBL 92 DIM 8.375 X 2.125 INCH P/N 7075 T6 .071 PO 900573 IASDR DHL2005741535Stiffener · bulgedVERTICAL STIFFENER AT RT WING WBL 92 BULGED AT LOWER END. REMOVED DAMAGED EXISTING DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-10-2. FABRICATED REPAIR DOUBLER FOR VERTICAL STIFFENER AT RT WING WBL 92 DIM 8.750 BY 2.125 MAT ID 7075T-6 .071 PO SDR SWAA051135Floor Support · crackedDURING SCHEDULED 1/4D CHECK, FOUND 3 EA CRACKS AT NR 3 LONGITUDINAL FLOOR SUPPORT TEE, BS 662.5, BS 665.5 & BS 669. REPAIRED FLOOR FLOOR SUPPORT PER SWA EA.SDR GTIA050147Support Bracket · brokenLEFT WING LEADING EDGE PANEL NR 1160C HAS BROKEN SHIELD SUPPORT BRACKET. REMOVED AND FABRICATE NEW SHIELD SUPPORT BRACKET. TREAT, PRIMED AND INSTALLED SHIELD SUPPORT BRACKET. (M)SDR DHL2005741507Stiffener · corrodedL/WING FRONT SPAR VERTICAL STIFFENER CORRODED BETWEEN TANK 2 FWD AN AFT FUEL PRESSURE SWITCHES WS 260. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-10-1 FIG 1. REMOVED DAMAGED VERT STIFFENER ON L/WING FRONT SPAR AN FABBED NEW FROM BAC 1517-1372 PO NR SDR DHL2005807504Bracket · crackedNR 1 ALT TANK BOOSTER PUMP FWD BRACKET CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW ONE IAW SRM 51-1-20D PG 21-9. TORQUED NUT IAW SRM 51-3-1 PG 2A.SDR 05FDEA00845Splice · crackedRIGHT WING I/B FLAP, I/B ACTUATOR ENCLOSURE CUTOUT FOUND FUSELAGE STIFFENER CRACKED. RIGHT WING I/B FLAP, I/B ACTUATOR ENCLOSURE CUTOUT CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II, NEW SPLICE PART NUMBER: FX SDR DHL2005367509Floor Support · corrodedDURING C-CHECK, CABIN FLOOR AT FR 14 BL 78R FLOOR SUPPORT BEAM HAS CORROSION ( MKD.) REMOVED CORROSION AT FR 14 BL 78R FLOOR SUPPORT IAW A-300 SRM 51-40-11. MAT LOSS .018 "OUT OF LIMITS" IAW SRM 53-10-00. INSTALLED NEW SEAT TRACK AT FR 14 RBL 78 IAW A-300 SSDR 05FDEA00810Support · crackedRIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT RIGHT WING FIXED LSDR 05FDEA00808Support · crackedLEFT WING, FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT LEFT WING FIXED LEADINSDR DHL2005783516Support Angle · crackedNR 6 SLAT ACTUATOR INBD SUPPORT ANGLE IS CRACKED AT BOTTOM, WING STA 519. REMOVED NR 6 SLAT ACT IAW 727 MM 27-81-32. REMOVED DAMAGED I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW SUPPORT ANGLE FROM PN AND 10133-1401 PO NR 501952 DIM.10" BY 3 1/4" IAW 727 SRM SDR DHL2005782565Web · crackedRT WING TIP WEB CRACKED AT THE UPPER AND LWR FLANGES. ON RT WING TIP REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FAB NEW WEB FROM 7075T6 .040 PO NR 9001068 14" BY 9" IAW B727 SRM 57-20-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2 INST IAW B727 SRM 51-30-2SDR DHL2005740516Support Angle · crackedLEFT WING ROOT FIXED LEADING EDGE HAS LOWER ANGLE SUPPORT CRACKED L/E STA 130. REMOVED FASTENERS FOR ACCESS AT LEFT WING ROOT FIXED EDGE L/E STA 130 STOP DRILLED CRACK .250 TERMINATED AT END OF CRACKED IAW B727 SRM 51-10-1 NDT HFEC INSP PER B727 NDT MAN PT6 5SDR DHL2005805573Cap · crackedRT WING LWR CAP CRACKED BETWEEN CTR AND FRONT SPAR, STA XRS 238.000 CANT (NR 3 MAIN TANK) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-09-05, EO NR AST050214 EO AST 050215, DWG 5615767. REMOVED DAMAGED BULKHEAD LWR CAP IAW SRM 51-1-20D SDR A6WA200540119Angle · crackedRT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED RT 621-00 ANGLE AT STRINGER 14 IAW CRJ SRM 57-42-06. (M)SDR ASOA05299Channel · crackedDURING C-CHECK, THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 IAW SRM. (K)SDR IXXA0500155SPlate · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RT INNER WING FWD TOP PANEL PLATING WITH CRACK DAMAGE AT STA XRS 74.869, S-14. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER PLUG. CLSDR IXXA0500151SPlate · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER AFT PLATING DENT DAMAGE AT STA XW 110.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING AND FINGER DOUBLER. CLEANED, TREATED AND PRIMED NEW PLATING INTERNASDR IXXA0500150SPlate · crackedDURING A ROUTINE C CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGED AT STA XRS 74.869, S-5. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. PERFORMED NDT INSPECTION AND FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CSDR 375PA0033Stiffener · damagedVERTICAL STIFFENER FOR THE FRONT SPAR BULKHEAD AT RBL 6.25 WAS TRIMMED OFF TO ALLOW FOR REPAIR OF KEEL BEAM (SDR 375PA0032). REPAIRED PER EA 57-029.SDR DXTA200500602Panel · leakingFUEL LEAKING OUT OF RT WING IN FRONT OF AILERON ON TOP. AIRCRAFT WAS INFLIGHT FOR 1.4 HRS AND LOST APPROX 1000 LBS OF FUEL OVER THE NORMAL BURN. INSPECTED RT WING FOUND SEEPAGE FROM RT BOTTOM WING VENT (NACA SCOOP). OPEN WING PANEL 640UT, REMOVED OLD SEALANSDR IXXA0500154SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING INBOARD EXTENDED LEADING EDGE ELONGATED HOLE AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH IMPROPER REPAIR. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA AND NEW SDR IXXA0500153SPlate · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP LOWER AFT PLATING DENTS DAMAGE BETWEEN STA XF 415.000 AND XW 408.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN. FABRICATED NEW SKIN, CLEANED, TREATED AND PRIMED AREA + NEW SKIN INTERNASDR USAA050310Support Angle · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, TRAILING EDGE OF SUPPORT PANEL, RT WING JUST ABOVE INBOARD EDGE OF NR 5 FLAP. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER BOEING DWG 69-47542 AND SRM 57-51-02. (M)SDR MASA200500120Bracket · crackedIN C-CHECK, RT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07.SDR MASA200500119Bracket · crackedIN C-CHECK, LT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07.SDR ASOA05198Web · crackedDURING A C-CHECK IN YUL, THE WEB IN WING BOX FRAME 28 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE WEB IN THE WING BOX FRAME 28 RT IAW SRM 51-25-01. (M)SDR DHL2005781521Angle · crackedDURING A "C" CHECK: RT WING LEADING EDGE COVE PANEL INBD SUPPORT ANGLE IS CRACKED AT WS 130. REMOVED R/W L/E COVE PNL SUPPORT ANGLE AND FABBED NEW FROM 2024-T3 .050 PO NR 9001417 DIM 17 1/2 INCH BY 1 1/2 INCH IAW 727 SRM 57-20-2 FIG 1. NEW ANGLE TREATED AND SDR A6WA200540044Doubler · mismanufacturedWHILE PERFORMING SB 601R57037 (WING SPAR MOD) IT WAS DISCOVERED THAT THE JOINT STRAP ON THE RT WING LACKS PROPER LENGTH FOR EDGE DISTANCE. COMPLIED WITH BRAS EO 601R575944A, BY FABRICATING DOUBLER FROM 2024T3, .050 INCH AND USING TO EXTEND CUTLINES TO OBTAIN SDR 05FDEA00254Hanger Assy · corrodedRIGHT WING LOWER AFT BEAM SUPPORT FITTING PN ARC0459-2 REQUIRES FABRICATION. FABRICATED FITTING ARC0459-2 IAW DAC DWG ARC0459-2 AND FEDEX EA 8-5732-83971, WINGS- RIGHT HAND WING, LOWER AFT BEAM, SUPPORT HANGER.SDR 05FDEA00264Sill · crackedFOUND CRACK IN RIGHT WING ISLAND SILL PART ARC7008-2.SDR UPS05243879Angle · crackedLT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02.SDR IXXA0500165SAngle · crackedDURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 790 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 5SDR QXEA200500399Bracket · crackedYYC - LEFTHAND WING FLAP TRACK NR 4 CANOE FAIRING BRACKET CRACKED. REPAIRED IAW Q400 SRM SUB TASK 51-42-05-330-001.SDR 05FDEA00145Bracket · crackedLEFT WING L/E, LOWER SURFACE SUPPORT BRACKET IS CRACKED AT WS 165 (INBOARD OF NR 3 K-FLAP ACTUATOR). REMOVED BRACKET IAW SRM 51-30-2. FABRICATED NEW BRACKET FROM 2024-T3 .050 BATCH 0000837762 IAW SRM 51-10-1. INSTALLED NEW BRACKET IAW SRM 51-30-2.SDR IXXA0500166SAngle · crackedDURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 785 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 5SDR EIA2005002Web · crackedLEFT WING AFT SPAR AREA SUPPORT STRUCTURE WEB IS CRACKED AT WBL 285 AT LANDING GEAR BEAM. PERFORMED TYPICAL WEB REPAIR PER B747 SRM 51-40-02 PG 1-5 STEP 1-10.
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