JASC 5730
Service difficulty reports · 27,269
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 DHL2004803533Access Door · crackedRT INNER WING AFT TOP PANEL PLATING ACCESS DOOR (505F) INTERNAL DOUBLER TWO CRACKS DAMAGE (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. FABRICATED INTERNAL DOUBLER (7075-T6 0.063) IAW DC8 SRMSDR DHL2004803519Doubler · crackedLEFT WING OUTBOARD STUB WING DOUBLER CRACKED 0.500 AT XFS 529.000 (LWR PART). REMOVED CRACKED DOUBLERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW DOUBLERS: INTERNAL (7075-T6AL 0.063), EXTERNAL (7075-T6AL 0.080) IAW SRM 57-2-1A PG 3. CLEANED, TSDR 04FDEA00814Skin · corrodedCORROSION LT WING UPPER SKIN T/E SPAR AREA 8 INCHES FROM WING TO BODY FAIRING UPPER SURFACE OF SKIN. BLENDED CORROSION LT WING UPPER SKIN T/E SPARE 8 INCHES FROM WING TO BODY FAIRING. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA 1.25 X 1 INCH AND REPAIRED IAW SDR AUS20040241Skin · corroded(AUS) WING TOP SKIN SUSPECT CORRODED. REMOVAL OF PAINT FINISH AND FURTHER INSPECTION FOUND THE SKIN TO BE SERVICEABLE WITH NO CORROSION OR CRACKING EVIDENT. INSPECTION CARRIED OUT IAW AD/BAE146/61 AMDT2.SDR UPS04842262Skin · crackedINSPECTION TYPE: C3, RT WING CENTER LE. INNER SKIN IS CRACKED AT FASTENER HOLES XW408 TO XS520. REMOVED, FABRICATED AND REPLACED INNER SKIN AND DOUBLER IAW DWG. 5769759 AND 5769857 AND SRM. 51-1-20D,51-1-21SDR IXXA0400056SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-3-0 PG. 1, SRM 51-1-21 PG. 1, REMOVED CORROSION IAW SRM 51-1-8 PGSDR IXXA0400055SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB L/E OUTER SECTION LWR SKIN SURFACE CORODED, STA. XFS 710.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTERNERS IAW DC8 SRM 51-120D PG. 21, SRM 51-1-21 PG. 1, SRM 51-3-0 PG.1, REMOVED CORROSION IAW SRM 51-1-8 PSDR IXXA0400054SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION LT OB WING L/E IB SECTION LWR SKIN SURFACE CORRODED, STA XFS. 710.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT, REMOVED FASTENERS, REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVED DAMAGED AREA, PERFSDR IXXA0400053SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA XW 485.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT DWG V22-R02, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, 51-1-20D PAGE 21, 51-3-0 PAGE 1, REMOVED COSDR ASOA04244Skin · crackedDURING HANGER MAINTENANCE, THE SKIN UNDER THE RT IB MULTIFUNCTIONAL SPOILER AT THE IB BRACKET WAS FOUND CRACKED. MAINT IS TO PERFORM A DETAILED VISUAL INSP FOR PROGRESSION OF THE CRACK AT EVERY SUBSEQUENT SERVICE CHECK, UP TO A MAX OF 100 FLIGHT HRS IAW REO 6SDR 04FDEA00760Skin · corrodedLT WING, CORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 264 TO 317 AND BETWEEN STRINGERS S10 TO S21. REMOVED PER SRM 57-10-00 VOL I FIG 32SDR MWEA040037Doubler · corrodedRIGHT WIND EXTERIOR BOTTOM AFT SKIN HAS A CORROSION SPOT AT STATION XRS234 STRINGER 17. FABRICATED AND INSTALLED DOUBLER.SDR DHL2004803514Doubler · crackedLT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 0.500 AT XFS 335.250. REMOVED CRACKED DOUBLER IAW DC8 SRM 57-1-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6AL 0.090) IAW SRM 57-3-3 PG 14. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51SDR ASMF200403015Panel · damagedDURING TRANSIT CHECK THE FUEL PANEL WAS DETECTED WITH DAMAGE OF 2.5 INCHES AND LEADING EDGE WITH CRACK OF 1.5 INCH IN STATION XRS 220. THE FUEL PANEL WAS REPAIRED IAW SRM 52-01 AND RIGHT WING LEADING EDGE WAS REPAIRED IAW SRM 57-06.SDR 04FDEA00694Skin · corrodedCORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 197 TO 264 AND BETWEEN STRINGERS S11 TO S21. LEFT WING XORS 197 TO 264 AND BETWEEN STRINGERS S11 TO S21 UPPER SKIN SURFACE CORROSION REMOVED AS PER SRM 57-10-00 VOL I FIG 32.SDR MWEA040027Skin · corrodedRIGHT WING EXTERIOR BOTTOM AFT SKIN HAS A SPOT OF CORROSION AT STATION XRS410 AFT SPAR TEE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR COMA0460235Access Panel · damagedLEFT WING FUEL ACCESS HOLE WS 188.040 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030.SDR COMA0460234Access Panel · damagedLEFT WING FUEL ACCESS HOLE WS 136.676 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030.SDR CALA0400249Skin · dentedINSPECTION FOUND LEADING EDGE SKIN UNDER NR 6 SLAT DENTED. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-70-04.SDR E812004F00004Skin Panel · damagedNOTED LOOSE/DAMAGED RIVETS ATTACHING LT WING CENTER SECTION UPPER LEADING EDGE SKIN PANEL. UPON REMOVAL FOR SKIN PANEL REPLACEMENT, NOTED PANEL ATTACHED IN SEVERAL PLACES WITH MS20426AD TYPE RIVETS WHERE NAS1097 RIVETS ATTACHED ORIGINALLY. SKIN RIVET ATTACH SDR 04FDEA00647Skin · crackedLT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XORS 759 CRACKED. LT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XORS 759 SMOOTH END AND FOUND WITHIN LIMITS AS PER SRM 57-00-01 VOL 1 FIG 3 HFEC INSPECTION CARRIED OUT AS PER NDT SPM PART 06-10-01.001 REV 1SDR COMA0460207Skin · crackedRIGHT HAND LOWER WING PLANK AT WS 148.019 IS CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-67-21-130.SDR GTIA040455Panel · corrodedLT L/E WING PANEL NR 1165C EXFOLIATED CORROSION AROUND FASTENER HOLES. FABRICATED NEW PANEL.SDR P5CA040154Panel · crackedLEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL.SDR IXXA0400029SSkin Panel · damagedDURING ROUTINE C-CHECK INSPECTION RT WING INBD VANE SLOT UPPER SKIN HAS ELONGATED HOLES AT STA XS 247.000 (MAJOR REPAIR). REPAIR IS ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-3-3 FIG 10 PAGE 22. REMOVED DETERIORATED SKIN IAW DCSDR COMA0460190Skin · crackedCRACK FOUND AT LEFT HAND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24-11, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00.SDR COMA0460189Skin · crackedCRACK FOUND AT LEFT AND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24-11, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00.SDR 04FDEA00575Access Panel · corrodedCORROSION ON FUEL TANK ACCESS 534CB, AT MATING SURFACE. RECEIVED NEW PANEL P/N ARB0872-507, TO BE INSTALLED ON WORK CARD 575I5503-01.SDR 04FDEA00568Access Panel · corrodedPITTING INSIDE SEAL GROOVE/MATING SURFACE ON FUEL TANK ACCESS PANEL 638BB. PITTING OUT OF LIMITS. REPLACED PANEL 638BB IAW DC10 MM 28-00-00-2.SDR GTIA040267Access Panel · crackedFTW - FOUND RIGHT WING LOWER FUEL ACCESS PANEL RL56C HAS CRACKED/DAMAGED AT FASTENER HOLES. REMOVED OLD FUEL ACCESS PANEL. INSTALLED NEW PANEL. (M)SDR CALA0400204Skin · crackedINSPECTION FOUND TWO CRACKS IN THE LT WING FIXED L/E SKIN AT OSS 421 T0 471. THE CRACKS WERE 3 INCH AND 5 INCH LONG. REPAIRED IAW EA 5731-01010, REV D.SDR ASAA0480144Access Panel · corrodedOKC - DURING HV6 CHECK, FOUND LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M)SDR COMA0460188Access Panel · crackedFUEL PANEL 550AB ACCESS HAS INDICATION OF POSSIBLE CRACK ON INBOARD FACE AT APPROXIMATELY 9 O`CLOCK POSITION. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-030.SDR CALA0400198Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT STA OSS 425. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR ASAA0480136Access Panel · corrodedOKC - DURING HV6 CHECK, - FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1361 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M)SDR ASAA0480139Access Panel · corrodedOKC - DURING HV6-CHECK, LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M)SDR ASAA0480135Access Panel · corrodedOKC - DURING HV6-CHECK, FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1367 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M)SDR SWIA200413155Skin · corrodedLT WING; LOWER WING PLANK FUEL ACCESS HOLES HAVE CORROSION ON REBATES. (DISCOVERED DURING C-CHECK INSPECTION.)REPAIRED AREA IAW CRJ REO 601R-57-21-030 REV. ''C'' AND SB 601R-57-030 REV. ''C''.SDR QXEA200400181Skin · chafedPDX - CHAFE MARK ON RIGHT HAND WING UNDER JUNCTION OF NR 1 AND NR 2 SLATS. REPAIRED IAW HORIZON AIR EA R-57-55.SDR CALA0400179Skin · crackedINSPECTION FOUND A 2.125 INCH CRACK IN RIGHT WING L/E SKIN AT NR 3 KRUEGER FLAP. THE AREA WAS REPAIRED IAW SRM 57-41-01, FIGURE 203.SDR IXXA0400028SSkin · corrodedDURING ROUTINE INSPECTION RIGHT WING CTR L/E UPPER SKIN SURFACE CORRODED (STA XFS 341.500-416.500) MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D, REMOVED CORROSION FROM UPPER SKIN SURFACE OF LT WING CIR L/E IAW DC8 SRM 51-1-8 PG 1SDR UPS04842139Skin · corrodedINSPECTION TYPE: C1, FWD UPPER LT W/W AT STA 857-000 UPPER SPAR CAP AND PLATING HAVE CORROSION BULGING AREA LBL 46. REMOVED CORROSION; (ORIG .270, REM .141) OUT OF LIMITS. FABRICATED REPAIR FILLER, DOUBLER, TRIPLER, PRESSURE PANEL ASSEMBLY DOUBLER, SHIMS, PSDR CALA0400161Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER FIXED L/E SKIN LOCATED I/B OF SLAT NR 7 AT WS 418. REPAIRED IAW ECRA 5721-01119.SDR CALA0400160Skin · crackedINSPECTION FOUND TWO 3.5 INCH CRACKS IN LT WING UPPER L/E SKIN PANEL AT WS 539 BETWEEN NR 3 AND NR 4 SLATS. REPAIRED IAW ECRA 5721-01120.SDR CALA0400136Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER L/E SKIN AT NR 3 SLAT ACTUATOR. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-41-01.SDR DL76L040176Skin · wornTHE LOWER WING SKIN ON THE LT WING WAS FOUND WITH WEAR DAMAGE AT LBL 103 FROM THE REAR SPAR EXTENDING TO THE FRONT SPAR. THE WEAR WAS DUE TO CONTACT WITH UNDERWING FAIRING STRUCTURE. THE DAMAGE WAS MACHINED SMOOTH, INSPECTED, ROTO PEENED, AND SURFACE FINISHESDR AWXA200400202Skin · corrodedMCN - MAJOR REPAIR - DURING AN UNSCHEDULED MAINTENANCE VISIT TO VENDOR REPAIR FACILITY, CORROSION WAS FOUND LT WING UPPER SKIN NEAR WING ROOT AT STR 1A, WBL 150. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; BLENDED DAMAGED AREA OSDR GTIA040170Panel · corrodedFTW - FOUND LEFT WING PANEL 1163C SCRATCHED LIGHT SURFACE CORRODED. REMOVED CORROSION FROM LEFT PANEL 1163C. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)SDR COMA0460165Panel · damagedFRETTING DAMAGE NOTED ON LT LOWER WING ACCESS HOLE CUTOUT AT 540CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030.SDR COMA0460164Skin · corrodedFRETTING DAMAGE NOTED ON RIGHT LOWER WING ACCESS HOLE CUTOUT AT 650AB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030.
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