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 F3LA200300112Skin · crackedDURING EXIT CHECK, INSPECTION REPORTED RT WING LE SKIN PANEL CRACKED AT WBL 324. FABRICATED AND REPAIRED SKIN PANEL PER SRM 51-70-5, REPAIR 7 AND SRM 51-70-11, FIGURE 1.SDR UPS03240300Skin · corrodedINSPECTION TYPE:C&SI EVIDENCE OF CORROSION BETWEEN WING CENTER SECTION UPPER SKIN & SKIN UPPER SPLICE @ BS 856 - 860 I/B OF WBL 70.5 RIGHT REPAIR CARRIED OUT IAW SRM 51-10-1, 51-10-2, 51-30-02 & SMRO EO 2003 -008-018 UPS ENGINEERING FILE NO B727-5730-18440SDR DHL2003604750Skin · damagedLT WING CTR. L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224 PERFORMED MAJOR REPAIR IAW EODHL-030544, ED-3301. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT ELONGATED HOLES SKIN AREA IAW EODHL-030544, ED-3301. PERFORMED EDDY CURRENT INSPSDR 03FDEA00149Skin · bulgedLT WING FWD OF NR 5 SPOILER AREA WING REAR UPPER SPAR CAP FOUND SKIN BULGED. OUTER WING/REAR SPAR TRAILING EDGE LT REAR SPAR UPPER CAP REPAIR CARRIED-OUT AS PER FEDEX EA 1-5720-67571 PART 1.SDR 03FDEA00159Skin · corrodedRT WING, TOP SKIN JUST FWD OF FUEL DUMP VALVE PIPE FOUND WITH CORROSION. CENTER OUTER WING, UPPER SKIN CORROSION REWORK CARRIED OUT IAW EA 1-5720-67573.SDR EVAS092007Skin · gougedDURING WALK AROUND CHECK FOUND LT WING FIXED LEADING EDGE LOWER SURFACE ACCESS DOOR CUTOUT SKIN GOUGE DAMAGE AT STA SOX463.PER MD-11 SRM 57-10-00 PAGE 58A AND 58B TO REPAIR.SDR ZIAA03002Skin · corrodedYIP - FOUND CORROSION ON LEFT WING LOWER SURFACE NR 4 WING PLANK TRAILING EDGE BETWEEN APPROXIMATE LWS 448 AND LWS 533. REMOVED CORRODED SECTION OF NR 4 WING PLANK TRAILING EDGE PER ZANTOP DWG S59-R01. (M)SDR DHL2003804779Panel · delaminatedLT WING T/E LOWER PANEL EXTERNAL SKIN DELAMINATED 5.000 INCH AT STA. XW106.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0SDR P5CA0300787Skin · corrodedRT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9.SDR P5CA0300789Skin · corrodedRIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLER PER SRM 57-30-03 FIG -9.SDR DHL2003804873Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED ( STA XW 5.000-47.000) R & R RT WING UPPER T/E PANEL (STA. XW5.000-47.000) IAW SRM 51-3-0 PG. 1SDR DHL2003804890Skin · corrodedLT WING - L/E UPPER SKIN CORRODED AROUND STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030108, ED-3214. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED SDR DHL2003804556Skin · corrodedLT WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS291.5000 AND XFS 304.000 CORR: PERFORMED MAJOR REPAIR IAW EO DHL 030108 , ED-3214. REMOVED FASTNERS IAW SRM51-1-21 PG. 1 REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM57-2-0 PG 16 TRIMMEDSDR DL73K030161Skin · crackedTHE UPPER SKIN OF THE LT WING WAS FOUND WITH A 2.5 INCH CRACK AT WBL 170 RUNNING FWD FROM THE AFT EDGE OF THE SKIN NEAR THE REAR SPAR. THE CRACK WAS REMOVED WITH A 3 INCH BY 2 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 ALUMINUM REPAIR DOUBLERS PSDR DHL2003804780Panel · delaminatedRT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA. XW5.000-32.000. R & R RT WING T/E UPPER PANEL IAW SRM 51-3-0 PG. 1.SDR DHL2003804913Panel · delaminatedLT WING UPPER SURFACE T/E UPPER ACCESS PANEL 510 SHOWS EXTERNAL SKIN DELAMINATED STA XA 475.000- XA 507.000. REMOVED AND REPLACED T/E UPPER ACCESS PANEL 510 ON LT WING UPPER SURFACE, STA XA 475.000- XA 507.000 IAW SRM 51-3-0 PG 1.SDR UPS03840231Skin · crackedINSPECTION TYPE: C1, AFTER REMOVAL OF LEAKING FASTENERS FOUND EXTERNAL DOUBLER AND UPPER WING SKIN CRACKED AT FASTENER HOLE AT XRS 22 AT STRINGER 5. REMOVED DOUBLER, OVERSIZED FASTENER HOLE, NDT VERIFIED NO CRACKS AT HOLE, FABRICATED FREEZE PLUG BUSHINGS, DOSDR DHL2003804888Skin · crackedRT WING T/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK STA XRS.285.000- 305.000. CUT OUT DAMAGED AREA IAW SRM 57-2-0 FIG 2. FABRICATED FILLER (2024-T3 0.032) AND DOUBLER (2024-T3 0.050) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW SDR DHL2003804781Skin · delaminatedLT WING LOWER ACCESS DOOR NR 540 WITH EXTERNAL SKIN DELAMINATED. R & R LT LOWER EXTERNAL ACCESS DOOR NR 540 IAW SRM 51-3-0 PG. 1SDR DHL2003804767Panel · crackedLT WING L/E OUTBD SLOT UPPER DOOOR SHOWS FOUR .250 CRACKS BTWN STA XS484.895 AND XS520.168 CORR: R & R LT WING OUTBD SLOT UPPER DOOR BETWEEN XS484.895 AND XS520.168 IAW MM.SDR DHL2003804552Skin · crackedRT WING T/E UPPER SKIN SURFACE WITH 1/2 INCH CRACK IN IT. (XRS285.000-305.000) CUT OUT DAMAGED AREA IAW SRM57-2-0 FIG. 2 FABRICATED FILLER (2024T3,032) & DOUBLER (2024T3.050) IAW SRM57-2-0 FIG. 2. CLEANED , TREATED AND PRIMED FILLER & DOUBLER INNER SURFACESDR DHL2003804895Skin · damagedRT WING CTR L/E LWR PART SHOWS ELONGATED HOLES AROUND STA XS 521.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030114, ED-3215. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DAMAGED AREA IAW EODHL-30114,ED-3215. FABRICATED DOUBLER (7075-T6AL-0SDR DHL2003804877Skin · corrodedLT WING L/E UPPER SKIN CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030103, ED-3213. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON LT WING L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57SDR DHL2003804662Vane · damagedLT WING OUTBOARD FLAP VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO67.000. PERFORMED MAJOR REPAIR IAW EO DHL 030109 , ED-3222 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLSDR DHL2003804540Skin · crackedITEM REF. N/R 2153 LH WING T/E UPPER SKIN WITH .5000 CRACK AT STA XW90.000 CORR: STOP DRILLED IAW SRM 57-2-0 FIG 2 FABRICATED DOUBLER ( 7075T6.050) IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B . INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2 , SRM5SDR 1206SSkin Panel · crackedDURING A PHASE 1-5 DISCOVERED CRACKS IN LT AND RT WING SKIN AT AFT OUTBOARD EDGE OF WHEEL WELL CUT OUT. LT WING CRACK WAS .50 IN. LONG RT WING CRACK WAS 0.40 IN. LONG. REPAIRED IN ACCORDANCE WITH CESSNA REPAIR DEFINITION S-550-0264/02RD DATED NOVEMBER 14, 2000SDR P5CA0300807Skin · corrodedRIGHT WING L/E LWR SURFACE STA 1380-1385 FOUND CORROSION IN LWR SURFACE. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH DOUBLERS PER SRM 57-30-03 FIG -9.SDR P5CA0300806Skin · corrodedRIGHT WING L/E LWR SURFACE CORROSION IN LWR SURFACE WAS 1280. DAMAGED AREA TRIMMED OUT, REINFORCED WITH DOUBLER PER SRM 57-30-03 FIG -9.SDR AUS20030121Skin · corroded(AUS) RT LOWER WING SKIN CHAFED ON WATER SCAVENGE PIPE DEBRIS GUARDS. CORROSION WAS ALSO FOUND IN THE SAME AREA BETWEEN FRAME 14 AND FRAME 15.SDR AUS20030120Skin · corroded(AUS) LT WING LOWER SKIN CORRODED BEYOND LIMITS. FOUND DURING X-RAY INSPECTION.SDR UPS03M40400Skin · corrodedINSPECTION TYPE: C, RT WING EXTERNAL SURFACE AT STA XORS 683-700 AFT STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MATERIAL REMOVED 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AS PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIESDR UPS03M40399Skin · corrodedINSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT XORS 740-745 AFT OF STRUCTURE 1 FOUND CORRODED AT 2 PLACES AS MARKED. REMOVED MATERIAL 0.023 INCH ORIGINAL THK:0.200 INCH FOUND OUT OF LIMIT AT XOR S 740-745 AS PER SRM 57-10-00 FIG 32 VOL 1 REV 32. REWORKSDR UPS03M40361Skin · corrodedINSPECTION TYPE: C, RT WING TOP EXTERNAL SURFACE AT STA XORS 683-700 AFT OF STRINGER 1 FOUND CORRODED AT 3 PLACES AS MARKED. AT STA XORS 685 MAT REMOVED 0.023 ORIGINAL THICK 0.200, FOUND OUT OF LIMIT PER SRM 57-10-00 VOL 1 FIG 32 REV 32. 10X MAGNIFIED VISUALSDR R2J2003F00003Skin · crackedDURING ANNUAL INSPECTION, INSPECTOR FOUND 2 EA .750 INCH CRACKS AT WS 124.6B RIVET. FURTHER INSPECTION FOUND 3 CRACKS IN PN 3743301 RIB AT SOME WS CRACKS EXCEEDED 1 INCH IN LENGTH, ALSO AT THE RIVET HOLES CRACKS REPAIRED IAW APPROVED DATA. CAUSE OF CRACKING,SDR 03FDEA00108Skin · corrodedLEFT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108, LT WING PANEL, AT STATION XIS 168.66 TO XORS 130.40, STRINGER 7L AND 19SDR 03FDEA00107Skin · corrodedRIGHT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108 RT WING SKIN PANEL AT STA XIS 168.66 TO XORS 130.40, STRINGER 1R AND 22SDR DHL2003804558Skin · corrodedLT WING L/E UPPER SKIN CORRODED BETWEEN STA 422.750 AND XFS 427.000 PERFORMED MAJOR REPAIR IAW SRM57-2-1 PAGE 2 FIG. 38 REMOVED CORROSION ON L/E UPPER SKIN IAW SRM51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. CUT OUT CORRODED AREA IAW SRM 57-2-SDR IXXA060478SPanel · chafedDURING ROUTINE C CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AFT OF TRUNNION PANEL CHAFED ON INBOARD UPPER SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER. IAW 57-2-0, 57-2-1, 57-3-SDR IXXA060486SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CRACKED AT STATION XW291. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW DC8 SRM 51-1-8, 51-2-1, 51-1-20D, AND 51-3-0.SDR IXXA060507SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LOWER LEADING EDGE OUTBOARD OF PANEL 522A EXISTING REPAIR CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SDR IXXA060506SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE OUT BOARD SKIN SPLICE REPAIR, OUTER SKIN CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM SDR UIEA200300005Skin · crackedDURING CURRENT C-CHECK AT SIA, FOUND BS 1241 L/S KICK FITTING AT BOLT HOLE NR 11 CRACKED IN WING SKIN ONLY. REAMED HOLE TO 1.169 INCH. NO CRACK INDICATION. FINAL REAMED HOLE TO 1.284 INCH IN WING SKIN AND CHORD. REAMED STRINGER SPLICE FITTING TO 1.126 INCHSDR 2003FA0000040Doubler · corrodedFUEL INTERCONNECT ACCESS PANEL CUT OUT DOUBLER IS CRACKED AT LT AND RT PANEL NUMBERS 53L AND 53R. LT AND RT UPPER CENTER WING BOX BEAM COVERS HAVE MODERATE TO MILD CORROSION ON THE UPPER HAT SECTIONS AND THE SKIN BETWEEN WING STATIONS 84.5 TO 192 LT AND RT. SDR AUS20030046Skin · corroded(AUS) WING CENTRE SECTION LOWER SKIN CORRODED AT BS 800 LBL20, WL168.1.SDR AUS20030042Skin · corroded(AUS) WING CENTRE SECTION LOWER SKIN CORRODED AT BS 840 LBL30, WL168.SDR P5CA0300731Panel · delaminatedDELAMINATION FOUND L/H WING LEADING EDGE TOP PANEL AT FSSD 1550 (O/B MOST). PANEL REPAIR CARRIED OUT PER SRM 51-40-12 & SRM 51-30-20.SDR DHL2003804546Skin · corrodedITEM REF>: N/R: 0237 LH WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS566.250 AND XFS585.000 ( MAJOR REPAIR)CORR: PERFORMED MAJORIAW SRM 57-2-1 PG. 2 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 REMOVED CORROSION ON LH WING UPPER SKIN ( STA. XFS566.250-585.000) IAW SSDR AUS20030029Wing · faulty(AUS) LH AILERON INBOARD FORWARD EDGE BINDING ON TRAILING EDGE OF LOWER WING SKIN. SUSPECT MANUFACTURING ERROR.SDR QXEA0300207Skin · crackedCKB- RIGHT WING CENTER LEADING EDGE INBOARD BOTTOM CORNER IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-107.SDR MDAS092002Skin · chafedBOEING 737-800 EXPERIENCED CHAFING DAMAGE TO THE LOWER SKIN AND FUEL ACCESS DOORS IN THE AREA OF THE PYLON BLADE SEAL CONTACT DURING MAINTENANCE VISIT. IT APPEARS THAT THE STRUT SEALS HAVE BEEN RIDING ON THE ACCESS PANELS, ACCESS PANEL RINGS, AND THE LOWER SUR
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