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.

SDR AALA202404114077Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WINGLET MIDDLE LEADING EDGE PANEL (737-0351) AT WS 750, WBL 680.40. REPLACED PANEL PER SRM 51-40-02-0G.Apr 4, 2024 · N835NN · Boeing 737823SDR DALA2024040504109Skin · corrodedSHIP 3139 CORROSION SPOTS FOUND IN LOWER SURFACE, UPPER SKIN TRAILING EDGE OVERHANG AREA AT RIB 10 AND 11. CORRECTIVE ACTION: REPAIRED PER ER/A 616174-14. (0278113)Apr 4, 2024 · N339NB · Airbus A319114SDR DALA2024040504108Skin · corrodedSHIP 3139 CORROSION FOUND ON LWR WING SKIN PANEL #2. CORRECTIVE ACTION: REPAIRED PER ER/A 616132-14. (0277982)Apr 4, 2024 · N339NB · Airbus A319114SDR DALA2024040404060Skin · corrodedSHIP 3139 CORROSION UPPER SURFACE SKIN AT LEVEL RIB 17 TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-74-00. (0276598)Apr 4, 2024 · N339NB · Airbus A319114SDR UIEA2024040500265Skin · corrodedCORROSION - SKIN LEFT UNDERWING REAR SPAR OVERRIDE JETTISON PUMP AREA.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 119 2. ACCOMPLISHED EI T2024A57M-345 REV 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Apr 3, 2024 · N472MC · Boeing 74745ESDR UIEA2024040500264Skin · corrodedCORROSION - SKIN, LH WING INSPAR UPR SURFACE T/E AREA WS 469.82 ~ WS 478.80 REAR SPAR AREA(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB CARD ATTACHIApr 3, 2024 · N472MC · Boeing 74745ESDR UIEA2024040500258Skin · corrodedFOUND LH WING LOWER SKIN HAVE CORROSION AT FSSI 628 ~ FSSI 660(<P>1. REPAIR DAMAGED AREA IAW EI T2024A57M-480 REV 6 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Apr 3, 2024 · N472MC · Boeing 74745ESDR UIEA2024040500257Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3102-3) UPPER SURFACE NEAR WS 323.82 (WBL 150.00) , S-16 ~ S-17(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSApr 3, 2024 · N472MC · Boeing 74745ESDR UIEA2024040500256Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WS 469.82, S-3 ~ S-4(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB CApr 3, 2024 · N472MC · Boeing 74745ESDR UIEA2024040500255Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WBL 150.00, MID SPAR(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV=120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 517-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB Apr 3, 2024 · N472MC · Boeing 74745ESDR DALA2024040404061Skin · corrodedSHIP 3139 CORROSION UPPER SURFACE SKIN AT LEVEL RIB 16 TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-74-00. (0275775)Apr 3, 2024 · N339NB · Airbus A319114SDR JR2R20240403428Panel · chafedLH WING LEADING EDGE PANEL OVER PYLON CHAFFEDApr 3, 2024 · N85320 · Emb ERJ170200LRSDR JR2R20240403427Panel · chafedLH WING LEADING EDGE PANEL OVER PYLON CHAFFEDApr 3, 2024 · N85320 · Emb ERJ170200LRSDR IPXA2024042401644Skin · crackedRT WING L/E HAS CRACK BEHIND SLAT #7. ADJUSTMEN GOOD I.A.W. A.M.M. 27-81-02-424-021. VERIFIED OPS CHECK GOOD.Apr 2, 2024 · N454UP · Boeing 75724APFSDR SWAA2024040570063Panel · delaminatedR/H WING UPPER PANEL 651AT DELAMINATED<[01] CW EA 24-157-00869Apr 2, 2024 · N7752B · Boeing 7377BDSDR DALA2024040404064Skin · crackedRH WING LEADING EDGE CRACKED AT SLAT TRACK #7 CUT OUT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0684:2021-2065-RH/003 00095 ER/A 616956-14 PRI REV 0 AND FINAL ER/A 616956-14 REV ORIGINAL HAVE BEEN COMPLIED WITH.Apr 2, 2024 · N101DU · Airbus BD5001A10SDR DALA2024040304040Skin · corrodedSHIP 3139 CORROSION UPPER SURFACE SKIN AT LEVEL RIB 11 TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM51-74-00. (0274294)Apr 2, 2024 · N339NB · Airbus A319114SDR DALA2024040304038Skin · corrodedSHIP 3139 CORROSION UPPER SURFACE SKIN AT LEVEL RIB 14 TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPAIRED PER SRM 51-74-00. (0274851)Apr 2, 2024 · N339NB · Airbus A319114SDR DALA2024040203985Skin · corrodedSHIP 3139 CORROSION UPPER SURFACE SKIN AT LEVEL RIB 9 TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-74-00. (0273575)Apr 2, 2024 · N339NB · Airbus A319114SDR AALA202406107676Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 7 AND 8. REPAIRED SKIN PANEL PER EA 353372.Apr 1, 2024 · N745VJ · Airbus A319112SDR DALA2024040203986Panel · inflt separationSHIP 3142 PANEL 575GB DEPARTED A/C. CORRECTIVE ACTION: INSTALLED PANEL 575 GB REF. A319 AMM 57-51-37. (5402306)Apr 1, 2024 · N342NB · Airbus A319114SDR FDEA202404010430Skin · corrodedR / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN CORROSION R/H WING LOWER DRY BAY PANEL REPAIR AT ACCESS PANEL CUTOUT 644 AB, WS 775-806 WITH NO DEVApr 1, 2024 · N922FD · Boeing 75723ASDR R61A2024040600160Skin · damaged6 EACH MIS-DRILLED #8 FASTENER HOLES ON RH SPAR 1 UPPER SKIN. REMOVED DAMAGE FROM 6 EA HOLES ON RH SPAR 1 UPPER SKIN BY REAMING HOLE TO 0.312 AND INSTALLING #10 FASTENERS. REF EMB ETD2024-170-009341.Mar 31, 2024 · N455YX · Emb ERJ170200LRSDR WX0A2024040532006Skin · cracked(MAJOR REPAIR - DISCREPANCY NOTED DURING HEAVY) LH WING LEADING EDGE , CRACK FOUND ON UP STOP #3 / L/H WING LEADING EDGE SKIN AT UP STOP #3 PERMANENTLY REPAIRED AS PER SRM 57-41-11-300-006 REV.148. REPAIR CATEGORY A. NO FURTHER ACTION REQUIRE. P/N: 2024T3 .063Mar 31, 2024 · N278NV · Airbus A320214SDR 2024F00105Skin · delaminatedTHE 7422086-3 LH WING UPPER SKIN BOND ASSEMBLY INSTALLED ON 680A-0341 ESCAPED TO THE FIELD WITH A POSSIBLE NONCONFORMING FINISH ON THE 6922462-1 STRINGER 5. TEST PANELS ASSOCIATED WITH THIS STRINGER PROCESSING BATCH FAILED THE WEDGE CRACK EXTENSION TEST. SUBSEMar 30, 2024 · N919QS · Cessna 680ASDR SWIA20250311028Skin · crackedLH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 FROM TRAILING EDGE OF WING PLANK, APPROX. 2.4€? LONG. (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR OF LH LOWER WING PLANK APPROX WS 47.61 FROM TRAIMar 28, 2024 · N959SW · Cndair CL6002B19SDR SWIA20250110328Skin · crackedLH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 FROM TRAILING EDGE OF WING PLANK, APPROX. 2.4€? LONG. (FILED OPEN) COMPLIED WITH TEMPORARY REPAIR OF LH LOWER WING PLANK APPROX WS 47.61 FROM TRAILIMar 28, 2024 · N959SW · Cndair CL6002B19SDR 2024FA0000872Skin · crackedR/H WING FWD WING WALK SKIN CRACKED AT CORRUGATED SKIN. REPLACED ASSEMBLY WITH NEWMar 28, 2024 · N586K · Piper PA28181SDR JJBA20240418042Access Panel · corrodedRH WING ACCESS PANEL 632AB AREA, THE ANCHOR NUT RING ON THE WING STRUCTURE IS CORRODED. DOUBLER REPLACED AT RH WING ACCESS PANEL 632ABMar 28, 2024 · N14186 · Emb EMB145XRSDR DALA2024032903918Skin · corrodedSHIP 3139 CORROSION TRAILING EDGE LOWER SURFACE UPPER SKIN BTW RIB 18 AND RIB 19 ON LH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-74-00. (0266415)Mar 28, 2024 · N339NB · Airbus A319114SDR DALA2024032903917Skin · corrodedSHIP 3139 CORROSION TRAILING EDGE LOWER SURFACE UPPER SKIN BTW RIB 14 AND RIB 15 ON LH WING. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-74-00. (0266413)Mar 28, 2024 · N339NB · Airbus A319114SDR CALA2024032800893Skin · corrodedB767-53-3-7034 - CABIN - STA 852 L/H WING CENTER SECTION MOST O/B PRESSURE DECK SURFACE FOUND CORRODED AS RED MARK - TRANSFER REFER NON-ROUTINE WO.2885899 AND ORIGINATED BY CENTER SECTION WING UPPER SKIN AT STA 852 LH MOST O/B STR-U17 TO PART 2 BEFORE 22MAR202Mar 28, 2024 · N659UA · Boeing 767322SDR SWI2025F00314Skin · crackedRH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 EMANATING FROM FIRST RIVET ROW CLOSEST TO TRAILING EDGE, APPROX. .75€? LONG, FROM THE TRAILING EDGE OF THE RIVET TO TRAILING EDGE OF WING PLANK. (FILEDMar 27, 2024 · N959SW · Cndair CL6002B19SDR SWIA20250110047Skin · crackedRH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 EMANATING FROM FIRST RIVET ROW CLOSEST TO TRAILING EDGE, APPROX. .75€? LONG, FROM THE TRAILING EDGE OF THE RIVET TO TRAILING EDGE OF WING PLANK. (FILEDMar 27, 2024 · N959SW · Cndair CL6002B19SDR CALA2024032800898Panel · brokenWHISTLING NOISE REPORTED20A. PRESSURIZATION ANDOTHER INDICATIONS ALLNORMAL. PIC ADDED PANEL 191DT PANEL FASTENED AND TAPED. PICS ADDED APPROVED ACP INTERM REPAIR PER PART 1 OF ECRA 5330-07206. ACP PERMANENT REPAIR PER PART 3 WITHIN 1 FLT CYCLE. CARRY APPROVED Mar 27, 2024 · N497UA · Airbus A320232SDR CALA2024040200931Skin · damagedRIGHT WING FUEL TANK BOTTOM ACCESS DOOR CUTOUT BETWEEN RIBS 17- 18 HAS 1 EA ELONGATED FASTENER HOLE AT I/B . REAMED HOLE TO 0.3592?. ACP''D HFEC SUFACE &. ROTO PROBED HOLE & REAM HOLE TO 0.3851 WITH HOLE TOOL SET 12-0-N. INSTALLED REPAIR NG PANEL 640MB, LEAK Mar 26, 2024 · N452UA · Airbus A320232SDR JGVR202403260001Skin · corrodedREPAIR LH WING TRAILING EDGE. IAW ETD2024-P300-04893827-REV A. REPAIRED LH WING TRAILING EDGE USING PERMANENT REPAIR IAW ETD2024-P300-04893827-REV A. LH WING SKIN CORROSION. SEE TASK AND INSPECTIONS FOR DETAILS. THIS REPAIR IS CONSIDERED A MINOR REPAIR.Mar 26, 2024 · N379QS · Emb EMB505SDR FDEA202403250365Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 635. LEFT WING FIXED LEADING EDGE AT STATION XOS 635 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-Mar 25, 2024 · N610FE · Doug MD11FSDR FDEA202403250364Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 598. RIGHT WING FIXED LEADING EDGE AT STATION XOS 598 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM Mar 25, 2024 · N610FE · Doug MD11FSDR FDEA202403250361Skin · crackedLEFT WING - FIXED LEADING EDGE NUMBER 11 SLAT TRACK CUTOUT OUTBOARD LOWER CORNER FOUND CRACK AT STATION XOS 720.5. LEFT HAND WING FIXED LEADING EDGE NUMBER 11 SLAT TRACK CUT OUT OUTBOARD LOWER CORNER CRACKED AREA AT STATION XOS 720.5, REPAIR CARRIED OUT ASMar 25, 2024 · N610FE · Doug MD11FSDR JR2R20240323448Skin · chafedRH WING FIXED LEADING EDGE AT #1 PYLON CHAFED. REPAIREDMar 23, 2024 · N88301 · Emb ERJ170200LRSDR JR2R20240323447Skin · chafedLH WING FIXED LEADING EDGE AT #1 PYLON CHAFED. REPAIREDMar 23, 2024 · N88301 · Emb ERJ170200LRSDR COEA2024051401901Access Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: ACCESS PANEL 521DT HAS FRETTING AT ATTACH FLANGE. REPAIR PER SRAS ES_00236338_01...23419 ISSUE A,Mar 22, 2024 · N901FX · Aerosp ATR42320SDR DALA2024032703851Skin · crackedLH LEADING EDGE CUT OUT FOR SLAT TRACK #7 HAS CRACK. REPAIRED CRACK PER PRI 615984-14 REV 0, REV 01, REV 02 AND FINAL ERA 615984-14 REV ORIGINAL.Mar 22, 2024 · N101DU · Airbus BD5001A10SDR DALA2024032603761Skin · corrodedCORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFAMar 22, 2024 · N335NW · Airbus A320212SDR DALA2024032603763Skin · corrodedCORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFAMar 22, 2024 · N335NW · Airbus A320212SDR DALA2024032603762Skin · corrodedCORROSION UPPER SURFACE BTW RIBS 10 & 17 ON RT WING (8EA). EVALUATED REWORKED AREAS P1, P2 AND P6 TO P8 LOC. ON UPPER SURFACE & FOUND WITHIN LIMITS IAW SRM 57-21-11-283-014 STEP 2A FIG 001 & FIG 002 & EVALUATED REWORKED AREAS P3, P4 AND P5 LOC. ON UPPER SURFAMar 22, 2024 · N335NW · Airbus A320212SDR EE4Y2024032219625Skin · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-001 LH WING TRAILING EDGEBETWEEN RIB 15 AND RIB 16 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TOAIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG AREMar 22, 2024 · N219NV · Airbus A320214SDR EE4Y2024032219567Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD 572179-01-1-002 RH WING TRAILING EDGEBETWEEN RIB 13 AND RIB 16 OVERHANG AREA WITH CORROSION WAS FOUND.DAMAGE WAS REPORTED TO AIRBUS ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND OVERHANG ARMar 22, 2024 · N219NV · Airbus A320214SDR JR2R20240322333Skin · chafedRH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIREDMar 22, 2024 · N88335 · Emb ERJ170200LR
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