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 04FDEA00171Skin · crackedLEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 LEADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.SDR 04FDEA00170Skin · crackedLEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING EDGE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I.SDR 04FDEA00169Skin · crackedLEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25SDR 04FDEA00168Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.SDR COMA0460051Skin · corrodedWHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED THE CORROSION AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV C.SDR EWG2004F00000Skin · wrinkledIAW REQUIREMENTS OF FAR 145.63, SUBMITS THIS 8010-4. IN THE PROCESS OF PERFORMING A PHASE 2 AND 3 INSPECTION, DIAGONAL WRINKLES WERE DISCOVERED ON THE TOP LT WING PANEL BETWEEN THE AUX AND AFT SPARS IB OF THE NACELLE. AFTER CONTACT WITH AND REVIEW BY MFG ENGSDR 04FDEA00148Skin · dentedDENT ON LT WING FIXED L/E SKIN AT NR 3 SLAT TAI DUCT. DENT ON L/W FIXED L/E SKIN AT NR 3 SLAT TAI DUCT, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-1. REPAIRED DENT IAW SRM 57-30-4 PG 2SDR COMA0460040Skin · crackedLEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (WVAC PO 21137) AND FILLER FROM 2024-T3.100 (WVAC PO 27013), INSTALLED IAW BOMBARDIER, INC REO 601R-57-21-120 REV D.SDR DHL2004806553Skin · corrodedLEFT WING OTBAORD L/E CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2H. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED EXISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUSDR 04FDEA00099Skin · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235, RIGHT X = 30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RH X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PSDR SWAA040107Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING FIXED L/E SKIN CRACKED AT WING STATION 213. REPAIRED WING SKIN CRACK PER EA.SDR GTIA040094Access Panel · corrodedFTW - FOUND LEFT WING ACCESS PANEL HAS SURFACE CORROSION AROUND FASTENERS ON EXTERIOR SIDE. REMOVED CORROSION. FABRICATED REPAIR PART. INSTALLED REPAIR PART. (M)SDR COMA0460027Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE CUTOUTS HAVE CORROSION AT 540CB AND 550 AB. REMOVED THE CORROSION AND RESTORED SURFACE FINISH IAW REO 601R-57-21-030 REV C.SDR 04FDEA00074Skin · crackedLEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I.SDR GTIA040168Skin · corrodedFTW - FOUND LEFT WING LOWER SKIN PANEL UPPER SURFACE HAS 4 INCH BY 5 INCH DIAMETER EXFOLIATION AT XCW 121 9 INCHES AFT OF WING REAR SPAR AND 9 INCHES MLG TRUNNION FITTING. WING SKIN FSXCW 121 OUTBOARD OF TRUNNION FOUND OUT OF LIMITS. ALT SPAR FS XCW 121 FORWSDR DHL2004752512Panel · dentedDURING C-CHECK, LT WING UPPER T/E PANEL WBL 124 HAS ONE SMOOTH DENT OUTBOARD AND ONE SHARP DENT INBOARD. CUT OUT 2 DENTED AREAS ON LT WING UPPER T/E PANEL, 1 APPROX 1.75 INCH DIA & 2 APPROX 2.25 INCH DIA. FABRICATED FILLERS 1 APPROX 1.75 INCH & 2 APPROX 2.2SDR UPS04841822Skin · nickedINSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27.SDR COMA0460033Skin · crackedREPAIR WING PLANK CRACK AT WS 148.019 LT SIDE. REPAIRED LT HAND LOWER WING PLANK AT WS148.019 IAW EO 601R-57-21-130.SDR COMA0460032Skin · crackedREPAIR WING PLANK CRACK AT WS 148.019 RIGHT HAND SIDE. REPAIRED RT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH AEROSPACE REPAIR ENGINEERING ORDER 601R-57-21-130.SDR COOSDR030074Panel · corrodedRT WING, LOWER SURFACE FIXED PANEL PN 65-19281-158, OUTER SKIN, CORRODED.SDR COOSDR030073Panel · corrodedLT WING, LOWER SURFACE FIXED PANEL PN:65-21656601, OUTER SKIN, CORRODED.SDR COOSDR030050Panel · delaminatedRT WING, FIXED PANEL PN 65-50820-142, TMC-284 DELAMINATED.SDR COMA0460001Skin · corrodedTHE LEFT AND RIGHT LOWER WING TANK ACCESS PANEL CUTOUTS HAD CORROSION AT PANELS 640AB, 640CB, 640DB, 640FB, 640BB, 540BB, 540FB, 550AB AND 550BB. REMOVED CORROSION AND RESTORED THE FINISH IAW REO 601R-57-21-030 REV C.SDR UPS04841686Skin · corrodedINSPECTION TYPE: C3, INTERGRANULAR CORROSION ON RT WING L/E UPPER SKIN AT AFT END AT XFS 347. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8-5720-7767-A.SDR UPS04841696Doubler · corrodedINSPECTION TYPE: C3, LT WING L/E INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 622.75 TO XFS 610, LOWER INTERNAL DOUBLER AT PANEL OPENING. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-21.SDR UPS04M41693Skin · crackedINSPECTION TYPE: 1C, RT WING LOWER FIXED LE SKIN CRACKED AT NR 7 SLAT IB TRACK CUTOUT AT XOS 888. NDT VERIFIES CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-10-00 FIG.21.SDR UPS04841689Doubler · crackedINSPECTION TYPE: C3, LT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. 5769600 AND SRM. 51-1-21,51-1-20D,57-3-0 FIG. 2D.SDR 03FDEA02304Panel · crackedLT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT FOUND CRACKED APPROXIMATELY 1.5 INCHES IN LENGTH. C/A: SNRM N0235 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT CRACKED PANEL REMOVED IAW AMM 20SDR A6WA200340201Skin · corrodedLT WING LOWER SKIN PLANK HAS CORROSION AT PANEL OPENING 540CB, FORWARD AND AFT OF PANEL OPENING. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION AND TREATING METAL IAW REO 601R-57-21-030. (M)SDR COMA0360577Skin · crackedTHE LEFT LOWER WING PLANK FUEL DRAIN FORWARD SCREW HOLE AT WS 85.5 HAD AN INDICATION WHILE PERFORMING EDDY CURRENT INSPECTION (FUEL BOOST PUMP DRAIN VALVE FORWARD SCREW HOLE). DRILLED THE SCREW HOLE TO .3125 INCH TO REMOVE THE INDICATION. FABRICATED AND INSTSDR DL73S031132Skin · dentedDAMAGE FOUND ON LOWER SKIN PANEL OF RIGHT WING AT STA 525 NEAR OUTBOARD TIP. REPAIRED PER ERA 426849-14.SDR 2004F00054Skin · debondedLEFT IB LEADING EDGE WING PANEL WAS REMOVED TO REPLACE THE DE-ICE BOOT AND IT WAS DISCOVERED THAT SUBSTANTIAL DEBONDING OF THE LOWER HALF OF THIS PANEL HAD OCCURRED. THERE WAS NO APPARENT DAMAGE TO THE OUTSIDE SKIN THAT WOULD EXPLAIN THIS AND ITS UNLIKELY THASDR COMA0360575Skin · corrodedFRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH REO 601R-57-21-030.SDR 2003FA0001277Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NASDR 2003F00653Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NASDR 2003FA0001250Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NSDR 2003FA0001249Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NSDR 2003UALA00959Skin · damagedLEFT WING INBOARD L/E HAS 4 EACH INTERIM REPAIR DOUBLERS INSTALLED AT L/E STATIONS 330, 415, & 543. MAJOR REPAIR ACCOMPLISHED. PERMANENT FLUSH REPAIRS WERE ACP PER SRM 57-41-01.SDR DHL2003802564Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA XW 5.000 - XW 33.000. REMOVED AND REPLACED RIGHT WING T/E UPPER PANEL (STA XW 5.000 - XW 33.000) IAW SRM 51-3-0 PG 1.SDR AUS20031267Skin · damaged(AUS) FOLLOWING REMOVAL OF THE LT WING THE UPPER SKIN AND INNER RIB FLANGE WAS FOUND TO BE GROUND AWAY TO THE EXTENT THAT THE RIVET EDGE DISTANCE WAS COMPROMISED. SOME RIVETS ALSO EXHIBIT GRINDINGMARKS. THE RT WING WAS THEN REMOVED AND INSPECTED AND FOUND TO BSDR CALA0300707Skin · dentedINSPECTION FOUND A DENT IN RT WING L/E SKIN BETWEEN NR 2 ENGINE AND WING ROOT. A FLUSH REPAIR WAS INSTALLED USING REPAIR PLATE AND FILLER IAW SRM 57-41-01-201.SDR COMA0360535Skin · crackedWHILE PERFORMING TASK CARD 002-57-540/640-603 FOUND LEFT WS 85.50 DRAIN HOLE FORWARD SCREW HOLE CRACKED. DRILLED HOLE, PERFORMED EDDY CURRENT INSP, FABRICATED AND INSTALLED FREEZE PLUG IAW BOMBARDIER, INC REO 601R-57-21-383.SDR CALA0300706Skin · crackedINSPECTION FOUND A 4.5 INCH CRACK IN RIGHT WING FIXED LEADING EDGE SKIN BETWEEN OSS 397 AND OSS 421. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, OP 4 AND SRM 57-41-01.SDR CALA0300704Skin · crackedINSPECTION FOUND A 6.25 INCH CRACK IN RT WING FIXED L/E SKIN AT STA OSS 421- OSS 471. THE SKIN WAS REPLACED IAW EA 5731-01010, REV D, OP 3.SDR AWXA200301624Skin · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 2 SLAT OUTBOARD AUXILIARY TRACK CUTOUT WS 346 TO WS 349. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16 PG 27, REPAIR 11.SDR DHL2003802553Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, STA XW 5.000 - XW 47.000. REMOVED AND REPLACED PANEL ON RIGHT WING T/E STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1.SDR TSAA0457017Skin · corrodedREMOVED CORROSION FROM RIGHT FIXED LEADING EDGE AT WBL 375. TRIMMED OUT DAMAGED AREA. FABRICATED A FILLER AND DOUBLER PER TABLE 1. ALODIZED ALL TRIMMED EDGES AND BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 57-4SDR ABXA040007Skin · corrodedLEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR.SDR DHL2003802571Skin · delaminatedRIGHT WING CENTERWING 723 PANEL LOWER SKIN DELAMINATED STA 742.000. REMOVED AND REPLACED NR 723 PANEL ASSY ON RIGHT WING CENTERWING, STA 742.000 IAW SRM 51-3-0 PG 1.SDR AWXA200301516Skin · crackedDURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON RT WING UPPER LEADING EDGE SKIN AT NR 8 SLAT INBOARD CORNER. MAINTENANCE REMOVED CRACKED RT WING UPPER LEADING EDGE SKIN PANEL FROM WS 425.50 TO WS 471.30; FABRICATED 3 EACH REPAIR STRAPS & FILLERS; INSTALLED REPA
Back to JASC 5730