JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 AALA201807029024Plate · wornAIRCRAFT WAS IN BASE MAINTENANCE. PLATE MOUNTING ON BOTTOM SKIN LOWER SURFACE REAR SPAR BETWEEN RIB 7 AND RIB 8, AND STA 375 TO STA 407 ON LEFT HAND WING SHOWS WORN SIGNS. REPLACED PLATE MOUNTING PER SRM 51-72-11 AND DRAWING D57251216.SDR FDEA201806181535Doubler · corrodedRT WING UPPER SURFACE DIAMOND DOUBLER SURFACE FOUND CORROSION. REPAIRED AS PER EA 1-5730-T0340753, PT 1.SDR FDEA201806181534Doubler · corrodedLT WING UPPER SURFACE DOUBLER FOUND CORRODED. REPAIRED IAW EA 1-5730-T0340596 P1.SDR FDEA201806181533Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 584. FOUND CRACK AFTER REMOVAL OF FORMER. DOUBLER REMOVED AND REPLACED AS PER 51-31-01-0G. DOUBLER FABRICATED AS PER DWG ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201806181523Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER AT STA XOS 613 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.SDR FDEA201806181522Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201806181521Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 755 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201806181514Skin · chafedLT WING I/B FIXED L/E UPPER SURFACE STA XIS 247 FOUND WITH CHAFED MARK. REPAIR CARRIED OUT ON LT WING I/B FIXED L/E UPPER SURFACE AT STA XIS 247 AS PER SRM 57-40-02-2R FIG 201 REPAIR 8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SRXR201806180058Skin · corrodedRT WING AFT AND CENTER UPPER SKIN BTWN XORS-270 AND XROS-505, BTWN STRINGER 4 AND 5 HAS LEVEL 1 CORROSION. REPAIRED RT WING AFT AND
CENTER UPPER SKIN BTWN XORS-270 AND XROS-505, BTWN STRINGER 4 AND 5 PER EA 011-5720-52-A7290-I/R. REF: NRC A040770 AND
WO 14676SDR 2018FA0000188Skin · dentedRT WING SKIN DENTED. REPAIRED.SDR SRXR201806170057Skin · corrodedLT WING UPPER CENTER AND AFT SKIN HAS CORROSION AT XORS 131/163 AT STR 6. ACCOMPLISHED BLENDOUT REPAIR AT LT WING UPPER CENTER AND AFT SKIN BETWEEN XORS 131 AND 163 AT STR 6 PER EA 011-5710-52-A7259 I/R REF NRC A040750.SDR RAIA2018091970001Skin · crackedFOUND 2 1/2 INCH CRACK ON BOTTOM OF LT WING 8 INCHES BEHIND PANEL 531DB (FOUND CRACK TO BE SEEPING FUEL). C/W RIB 9 LEFT WING LOWER SKIN REPAIR REFERENCE EO EMB145-57-019-0.SDR SRXR201806160056Skin · corrodedCENTER AND AFT RT WING UPPER SKIN BETWEEN XORS 130 TO XORS 264 BETWEEN STR 5 AND 8 HAS CORROSION. ACCOMPLISHED REPAIR ON RT WING CENTER AND AFT UPPER SKIN BETWEEN XORS 130 AND XORS 264 STRINGER 5 AND STR 8 PER EA 011-5720-52-A7282 I/R REF NRC A040768.SDR REXA2018070300584Skin · corrodedLT WING FUEL ACCESS PANEL LAND 540BB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 540BB IAW REO 601R-57-21-030.SDR REXA2018070300580Access Panel · corrodedRT WING FUEL ACCESS PANEL LAND 640BB HAS FRETTING CORROSION. REPAIRED RIGHT ACCESS PANEL LAND 640BB IAW REO 601R-57-21-030.SDR REXA2018070300579Access Panel · corrodedLT WING FUEL ACCESS PANEL LAND 510AB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 510AB IAW REO 601R-57-21-030.SDR REXA2018070300578Panel · damagedRT LE PANEL 630BL HAS ELONGATED AND OVER COUNTERSUNK ATTACH FASTENERS HOLES. REMOVED AND REPLACED WITH NEW PANEL 630BL IAW SRM 51-40-11.SDR SRXR201806150054Skin · corrodedRIGHT WING CENTER AND AFT UPPER SKIN HAD CORROSION AT XORS 270 TO XORS 505 BETWEEN STRINGERS 4 AND 9. REPAIRED IAW EA 011-5720-52-A7290, I/R.SDR SRXR201806150053Skin · corrodedLEFT WING UPPER SKIN HAD CORROSION AT XORS 340 - 375 BETWEEN STRINGERS 4 AND 6L. REPAIRED THE LT WING UPPER SKIN IAW EA 011-5720-52-A7292, I/R.SDR SRXR201806150052Skin · gougedRIGHT WING LOWER SKIN WAS GOUGED AT XORS 264 AND THE FRONT SPAR. ACCOMPLISHED A REPAIR IAW EA 011-5740-52-A7266, I/R.SDR SWAA2022021824137Plate · crackedRT WING WIGGLE PLATE CRACKED AT RSS 261 (VERIFIED WITH HFEC ) / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.SDR SWAA2022021708103Plate · elongatedR/H WING REAR SPAR WAFFLE PLATE NOT SECURED AND HAS ELONGATED MOUNT HOLE LOCATED JUST IB OF #2 ENG SAIL TAIL / REMOVED AND REPLACED R/H WING REAR SPAR WAFFLE PLATE JUST I/B OF #2 ENG SAIL TAIL IAW B737 SRM 51-40-02-0G-0 & BOEING DWG 115A2001 REV - ATAG WN3853SDR SWAA2022021724136Plate · crackedRT WING WIGGLE PLATE CRACKED ABOVE #6 FLAP TRACK (VERIFIED WITH HFEC ) / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02. FLAP SKEW ADJUSTMENT CHECK; INBD TRAILING EDGE FLAP ADJUSTMENT AND TRAILING EDGE FLAP DRIVE SYSTEM ADJUSTMENT TO BE ACCOMPLISHED ON N/RSDR FDEA201806141483Skin · crackedDURING HFEC INSPECTION ON LT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AND ACCESS DOORS, CRACKS FOUND APPROX 1/8 INCH IN LENGTH AT CORNER NR 5 AT SLAT ACTUATOR ACCESS DOOR FWD INBD CORNER, AT STA XOS 490.850. REPAIR CARRIED OUT AT LT WING FIXED LEADING ESDR SWAA2022021708072Panel · delaminatedLH WING LEADING EDGE PANEL 521EB; FWD OUTBOARD CORNER IS DELAMINATED / BONDED DELAMINATION FWD OUBOARD CORNER AND RESTORED DECORATIVE FINISH TO LH WING L/E PANLE 521 EB IAW B77-700 SRM 51-0-04-2R-12 REV 64 SRM 51-70-04-2R-0 REV 64; AMM 51-21-99-300-802 REV 65;SDR SWAA2022021708075Panel · delaminatedRH WING LEADING EDGE PANEL 621JB; FWD CORNER OF PANEL IS DELAMINATED. / REPAIRED R/H L/E PANEL 621JB; FWD CORNER I/A/W 737-700 SRM 51-70-04-2R-13 REV 64 PER SRM 57-41-01-2R-1 TABLE 202 REV 64.SDR SWAA2022021708078Panel · brokenRH WING LEADING EDGE PANEL 621DB; FWD INBOARD CORNER HAS COMPOSITE SECTION BROKEN OFF. / REPAIR BONDED FWD INBOARD CORNER SECTION MISSING FIBER LAYERS AND RESTORED DECORATIVE FINISH ON RH WING L/E PNL 621DB. IAW B737-800 SRM 51-70-04-2R-6 REV 64; SRM 51-70-04-SDR SWAA2022021746705Support Bracket · crackedRIGHT WING UPPER TRAILING EDGE PANEL BETWEEN #7 AND 8 SPOILERS AFT SUPPORT BRACKET TO RAY GUN ATTACH BRACKET IS CRACKED AT OUTBOARD FASTNERS. / REMOVED AND REPLACED RH WING AFT SUPPORT BRACKET TO RAY GUN ATACH BRACKET @ UPPER TRAILING EDGE PANEL BETWEEN #7 & #SDR AALA20180703014Skin · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON THE RIGHT WING UPPER SKIN AT THE DIAGONAL BRACE NR 4 FASTENER HOLE. REPAIRED RIGHT WING UPPER SKIN PER EA 281687.SDR FDEA201806121450Doubler · crackedLT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 663 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 663 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA201806121449Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 613 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2018062983180Skin · damagedLEFT WING TE, UPPER SURFACE SHROUD FASTENERS WERE PULLING THROUGH. REPLACED THE SKIN, REINFORCEMENT PLATE, AND INSTALLED A REPAIR DOUBLER IAW EO A300-5730-68973-A, AND REO-G21442, REV IRSDR IPXA2018061430660Landing · crackedINSPECTION TYPE:12YR, LEFT WING PANEL 513AB LAND CRACKED FORWARD O/B CORNER. REPAIRED IAW SRM 53-15-63.SDR IPXA2018062543991Doubler · crackedRT WING FIXED L/E BEADED DOUBLER WAS CRACKED AT XOS 494 - 500. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.SDR IPXA2018062093825Doubler · crackedLEFT UNDERWING ACCESS PANEL LANDING WAS CRACKED AT XORS 542. REMOVED, FABRICATED, AND REPLACED THE ACCESS PANEL LANDING DOUBLER IAW DWG ARB2933, SRM 51-33-01, AND 51-35-01.SDR DALA2018061203951Panel · crackedPERFORM GVI OF RT WING UPPER SURFACE. DUE TO PASSENGER REPORT OF A CRACK ON THE RT WING UPPER SURFACE AS OBSERVED FROM THE CABIN, PLEASE SET- UP TO PERFORM A GVI OF THE RT WING UPPER SURFACE FOR ANY SIGNS OF A CRACK. WHILE WORKING MD LOG 0592224 FOR POSSIBLE SDR SWAA2022021712072Panel · delaminatedSERVERAL AREAS OF DISBOND OVER CORE FOUND ON T/E PANEL 661BB / REPAIRED SEVERAL AREAS OF DISBOND OVER CORE ON T/E PANEL 661BB I.A.W 737 SRM 57-51-01-2R-1 TABLE 201; I.A.W SRM 51-70-05-2R-1.SDR SWAA2018061122646Seal · leakingAIR TURNBACK, FUEL REPORTED LEAKED FROM A/C ON TAKEOFF BY AN AIR CARRIER ON THE GROUND. FOUND LEFT WING PANEL 63BB SURGE TANK ACCESS DOOR LEAKED FROM SEAL. R&R SEAL IAW AMM.SDR SWAA2022021715690Panel · crackedLEFT WING PANEL 561AB HAS SEVERAL SCREW HOLES BULGEDAND CRACKING ON LEADING EDGE UNDER SEAL AREA MARKED / REPAIRED HOLES PER SRM 51-70-04; REPAIR #9. RESTORED FINISH PER AMM 51-21-73 AND AMM 51-21-81.SDR AALA201806076006Skin · corrodedCORROSION FOUND ON THE LEFT WING LOWER SKIN, LWS 540 DRAG LINK, THE CORROSION WAS BUSTING THROUGH THE SEALANT ABOUT 2-3 INCHES AFT OF FRONT SPAR. REPAIRED THE LEFT WING LOWER SKIN IAW EA 280942.SDR SRXR201806060048Skin · corrodedCORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM XROS 192 - 216. BLENDED OUT THE CORROISION IAW SRM 52-21-04, PG 4. REPAIRED THE WING SKIN IAW EA 011-5720-52-A7293.SDR SRXR201806060047Skin · corrodedRIGHT WING FWD AND CENTER UPPER SKIN HAD CORROSION BETWEEN XORS 145 AND 231, STRINGER 14R. ACCOMPLISHED A BLENDOUT REPAIR IAW EA 011-5720-52-A7293, I/R.SDR SRXR201806060046Skin · corrodedCORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM APPROX XORS 285 - 318. BLENDED THE CORROSION IAW SRM 51-21-04, PG3. REPAIRED IAW EA 011-5720-52-A7293.SDR SRXR201806060045Skin · corrodedRIGHT WING UPPER SKIN HAD CORROSION BETWEEN XORS 91 AND XORS 230, STRINGER 14. ACCOMPLISHED A BLENDOUT REPAIR ON THE RT WING SKIN IAW EA 011-5720-52-A7293, I/R.SDR AALA2018071622003Skin · corrodedLEFTOVERWING FUEL PORT FAILED A RESISTANCE BONDING CHECK. DURING DISSEMBELY, DISCOVERED CORROSION ON THE UPPER AND LOWER LANDINGS OF THE WING SKIN BETWEEN LWS 469.5 - 479.5. REPLACED THE LT WING OVERWING FILL PORT IAW AMM 28-11-04-404.SDR COEA2018071307917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: RT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 622CT. LEVEL 2 REPAIRED PER DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.SDR COEA2018071306917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 521DT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08.4888 ISSUE D, DATED 7/2/2018.SDR COEA2018071305917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 522CT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.SDR C77A2018060500001Skin · crackedINSPECTION DISCOVERED THE RT WING LOWER REAR ROOT SKIN WAS CRACKED AT THE SPAR II AND RIB 4A JUNCTION. THE CRACK WAS VERIFIED AT APPROXIMATELY 2.9 INCHES LONG IAW HFEC NDI. THE CRACK IS LOCATED APPROXIMATELY 0.482 INCH OUTBOARD OF THE RIB 4A LOWER SKIN DOUBLESDR SRXR201806050041Doubler · corrodedRIGHT WING L/E BEADED DOUBLER WAS CRACKED AT WS 584. REMOVED, FABRICATED AND INSTALLED A NEW BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15.
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