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 TRAX200700007Angle · crackedRANRC 82. RT WING MID LE, IB ATTACHMENT ANGLE IS CRACKED. REMOVED AND REPLACED RT WING AND LE IB ATTACHMENT ANGLE WITH SERVICEABLE ANGLE PN 600-12045-12 IAW CRJ AMM 20-21-00 MC892SDR.SDR CA070115013Fillet · cracked(CAN) DURING INSPECTION OF THE AIRCRAFT A CRACK WAS SUSPECTED IN THE RT UPPER FILLET WING TO FUSELAGE. NON DESTRUCTIVE TESTING CONFIRMED (2) CRACKS, 25 MM AND 18 MM LENGTH. LT UPPER FILLET INSPECTED BY NDT AND NO CRACKS FOUND. AN APPROVED REPAIR CARRIED OUT.SDR QXEA200603196Bracket · crackedC4 PDX - RIGHT "Z" ANGLE BRACKET CRACKED AT STATION YW 58.00 AT FORWARD SPAR. REPAIRED IAW SRM 51-25-06, 51-21-11, AND 51-40-11.SDR DALA1154269258Structure · damagedREPAIR OF WING LEADING EDGE WORN DAMAGE OD2006-SR-042 NRC B55-061119-228 BOEING APPROVAL 1-255950271-5.SDR COMA0660677Channel · crackedLEFT REAR SPAR CHANNEL IN WHEEL WELL AT WS 58.88 FWD OF COVER PANEL HAS A 1 INCH CRACK IN THE TOP CORNER. APPLIED DOUBLER TO LEFT REAR SPAR CHANNEL PER EA 10-5720-01477.SDR SWIA200617621Angle · crackedCRACKED ANGLE FS625 LBL40 WL80, DISCOVERED DURING C-CHECK INSPECTION. REPLACED TEAR DROP SHAPED ANGLE PN 601-35012-51 AT FS 625 LBL 40 WL 80 IAW CRJ 200 REO 601R-53-61-422.SDR ASAA0671261Support Bracket · crackedLEFT WING FIXED UPPER T/E PANEL RIB ASSY AFT SUPPORT BRACKET CRACKED AT WS 278.5. REPAIRED IAW SRM 51-40-02.SDR C2XA06TY076Bracket · damagedTYS DURING A CURRENT 3C INSPECTION THE LEFT PCA BRACKET I/B BUSHION FITTING WAS FOUND TO BE OUT OF ROUND. MAINTENANCE REMOVED AND REPLACED THE LT PCA BRACKET IAW EC 5770-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR COMA0660645Channel · crackedLEFT CHANNEL CRACKED AT LEFT WS 53.600 FWD OF HYDRAULIC SHIELD. REPAIRED IAW EA 10-5720-01477.SDR COMA0660644Channel · crackedRIGHT CHANNEL CRACKED AT RT WS 53.600 FWD OF HYDRAULIC SHIELD. REPAIRED IAW EA 10-5720-01477.SDR DHL2006746005Attach Angle · crackedCRACK FOUND IN LEFT WING BELOW NR 7 SPOILER IN THE RADIUS OF THE ATTACH ANGLE COMMON TO SPOILER ACTUATOR FITTING, APPROX WBL 124.2, CRACK LENGTH APPROX 1.5". REMOVED LOWER CHORD PREVIOUS REPAIR AND DOUBLERS PER B727 SRM 51-30-2. FABRICATED NEW CHORD FROM BACSDR DHL2006807527Pan · crackedRT WING CTR L/E ZEE PAN 2" CRACK APPROX, STA XFS 520.168. REMOVED CRACKED ZEE PAN IAW SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 TABLE I (TORQUE). REFER TO JC ESDR CA061121003Line · split(CAN) WHILE CARRYING OUT ZONAL INSPECTION 263 AND 264, BOTH WING ROOT DRAIN LINES WERE FOUND BLOCKED AT THE BELLY DRAINS. THE ACCUMULATED WATER IN THE DRAIN LINE IN TURN FROZE AND SPLIT THE DRAIN LINE CAUSING PRESSURIZATION LEAK AND WATER AND SKYDROL TO LEAK ISDR 06FDEA03972Doubler · crackedLT WING, AT XOS 654 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03971Doubler · crackedLT WING, AT XOS 645 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03970Doubler · crackedLT WING, AT XOS 639 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03969Doubler · crackedLT WING, AT XOS 631 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03968Doubler · crackedLT WING, AT XOS 518 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03950Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 665. RT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 665 REPAIRED AS PER SRM TR 57-5 57-10-00 FIGURE 25B VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03948Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 669. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03947Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XORS 636-643. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR AMTA200600640Stiffener · crackedRT WING IWS 503 AREA NR 3 PYLON LATERAL REINFORCEMENT STRUCTURE VERTICAL STIFFNER CRACKED FROM ATTACHMENT TO IWS 503 RIB. (K) DAMAGED VERTICAL STIFFENER WAS REMOVED AND REPLACED AS PER DWG NR 1527479 ITEM 8. (M)SDR AMTA200600639Stiffener · crackedLT WING TANK IWS 503 AREA NR 1 PYLON LATERAL REINFORCEMENT STRUCTURE VERTICAL STIFFENER CRACKED FROM ATTACHMENT TO IWS 503 RIB. (K) DAMAGED VERTICAL STIFFENER WAS REMOVED AND REPLACED AS PER DWG NR 1527479. (M)SDR UPS06448663Stiffener · crackedINSPECTION TYPE:C RIGHT WING REAR SPAR WEB WS 405 STIFFENER THE SECOND MOST UPPER HOLE FOUND CRACK RUNNING UP APPROX 1 INCH. RIGHT WING REAR SPAR WEB WS 405 STIFFENER UPPER PORTION REPAIRED AS PER SRM 51-40-04 FIG 3.SDR 06FDEA03909Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 357 RIB FWD STIFFENER CRACKED. REMOVED AND REPLACED TEE CLIP AT L/W STE 357 IAW SRM 51-30-5, 51-30-6, 51-30-2.SDR 06FDEA03908Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 410 RIB FD STIFFENER CORRODED. REMOVED AND REPLACED TEE CLIP AT L/W STA 410 IAW SRM 51-30-5, 561-30-6, 51-30-2.SDR USAA061310Structure · crackedLEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2.5 INCHES.SDR USAA061300Angle · crackedLOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCHES.SDR 2006FA0001071Web · crackedDURING PHASE 1 THROUGH 4 INSPECTION, AFTER REMOVING MOVING ALL WING INSPECTION PANELS. 4 (EA) CRACKS NOTICED IN WEB FLANGE COMMON TO AND EMITTING FROM RIVETS ON LT IB WING BOX AREA, BL-65.50, (2EA) CRACKS AT WS 65, (1EA) CRACK AT WS 56. (K)SDR USAA061258Stiffener · crackedREAR SPAR BULKHEAD STA 663 LBL 6.15 LBL 24 CRACK. FABRICATED AND INSTALLED REPAIR PART IAW DWG 654502, DEFECT SIZE: .25 INCH.SDR QXEA200602900Strap · corrodedC3 YYC - RIGHT WING RE-INFORCING STRAP AT INBOARD FLAP HINGE ARM IS SHOWING CORROSION EMANATING FROM FASTENERS. REPAIRED IAW SRM 51-21-06, 51-25-16.SDR QXEA200602898Strap · corrodedC3 YYC - LEFT WING RE-INFORCED STRAP AT INBOARD FLAP INBOARD HINGE ARM HAS CORROSION EMANATING FROM FASTENERS. REPAIRED IAW SRM 51-25-16, 51-21-06.SDR QXEA200602916Structure · damagedC3 YYC - RIGHT WING LOWER MAIN LANDING GEAR CUTOUT AFT EDGE REBATE DAMAGED. REPAIRED IAW SRM 51-42-06.SDR QXEA200602915Structure · damagedC3 YYC - LEFT WING LOWER MAIN LANDING GEAR CUTOUT AFT EDGE REBATE DAMAGED. REPAIRED IAW SRM 51-42-06.SDR 2006UALA02017Stiffener · crackedWHEEL WELL FWD WING SPAR CENTER SECTION REAR SPAR STIFFENERS ARE CRACKED LBL 6.15 AND RBL 6.15. MAJOR REPAIR: REMOVED AND REPLACED CRACKED STIFFENERS PER MM 57-12-96 REPAIR 2.SDR TRAX200600870Angle · crackedRIGHT BENT ANGLE AT WING RIB 4 FR 28 UPPER FUSELAGE CRACKED. RT BENT ANGLE AT WING RIB 4 FRM 28 REPLACED IAW SRM 51-25-01. REPAIRE DETERMONED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPAIRE ACCOMPLISHED IAW SRM 51-25-01. (CLOSED 10/31/06)SDR TRAX200600869Angle · crackedLEFT BENT ANGLES AT WING RIB 4 FR 28 UPPER FUSELAGE CRACKED (2 PIECES). LT BENT ANGLE AT WING RIB 4 FR 28 UPPER FUSELAGE FABRICATED IAW SRM 53-91-42 AND INSTALLED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPASDR QXEA200602649Channel · misdrilledC3 PDX-RT WING BOX PANEL 621BT HAS 12 RIVETS HOLES MISDRILLED FOR GANG CHANNEL. REPAIRED IAW SRM 51-42-05, 51-21-10, AND SRM 51-25-40.SDR EIA2006264Structure · corrodedLEFT WING LEADING EDGE LOWER CHORD AT FRONT SPAR STATION 1410 CORRODED. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PARTS PER ECRA 479-57-215-2 AND B747 SRM 57-30-03, FIG 4 & 9.SDR QXEA200602702Plate · gougedLT WING INNER FUEL TANK 526AT LADDER PLATE HAS MECHANICAL GOUGE. REPAIRED IAW RD8-57-611.SDR ABXA060281Support Fitting · crackedLEFT WING INBOARD SPOILER TORQUE TUBE SUPPORT ASSEMBLY CRACKED AT XRS-236. REMOVED AND REPLACED INBOARD SPOILER SUPPORT FITTING IAW DC9 MM.SDR TRAX200600775Bracket · crackedRIGHT WING RIB 13, O/B ARM, 2 OMEGA BRACKET CRACKED.SDR CALA0600332Slat Track · crackedINSPECTION FOUND A 1 INCH CRACK AROUND RIVET HOLES IN RT WING NR 6 SLAT I/B AUX TRACK LOWER AREA. THE AREA WAS REPAIRED IAW SRM 57-43-01.SDR 06FDEA03233Angle · crackedRT WING NR 3 TANK ACCESS PANEL 634CT INTERIOR BETWEEN STR 8 AND STR 9 TEE ANGLE FOUND CRACKED. TEE ANGLE AT RHW NO. 3 TANK BETWEEN STRINGER 8 AND STRINGER 9 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-1SDR HALA0600754Web · crackedLT WING FIXED L/E NOSE WEB IS CRACKED AT FSS 578. REMOVED CRACKED WEB AND RIB FOR ACCESS. FABRICATED NEW WEB USING 7075 -0- .050 INCH LOT 662986, HEAT TREATED TO -T-6- ON W/O 20862. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED AND INSTALLED WEB AT I/B RIB ATSDR AALA20060831Channel · crackedMCI - RIGHT AND INBOARD WING PANEL SUPPORT U-CHANNEL CRACKED AT AFT INBOARD SIDE OF FALSE SPAR TRAILING EDGE (WING BUTT LINE 110). FABRICATED AND INSTALLED REPAIR L-ANGLE PER SRM 57-51-02 AND MRB 767 2878 DATED 31 AUGUST 2006.SDR 06FDEA03217Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 682 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103502, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03216Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 737 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103501, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03209Intercostal · crackedRT WING L/E CRACK LONG 1" ON INTERNAL INTERCOSTA AT STA XORS 540 REPAIRED IAW SRM 57-00-01 FIG 10 SHEET 1.SDR 06FDEA03183Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. REPAIRED AS PER FEDEX E.A 1-5730-103500, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
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