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.

SDR USAA2012123100019Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING FUEL DOOR 640RB BETWEEN RIB 21 TO RIB 22 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640RB IAW A319 AMM 57-27-11-400-002-A.Dec 6, 2012 · N751UW · Airbus A319112SDR SWIA201232413Skin · crackedFOUND CRACK ON RIGHT LOWER WING PLANK IN THE AREA OF THE REAR SPAR AND WING STATION 148.019. (C-CHECK) REPAIRED CRACK ON RIGHT LOWER WING PLANK IN THE AREA OF THE REAR SPAR AND WING STATION 148.019 IAW REO.Dec 6, 2012 · N908SW · Cndair CL6002B19SDR IXXA2013020700006Skin · crackedRT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED DOUBLER 0.190", FILLER 0.200" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED FABRICATED PARTS AND Dec 5, 2012 · N41CX · Doug DC862SDR I5EA20121205001Skin · corrodedCORROSION WAS FOUND AT A WING FUEL HOLE COVER PANEL LANDING AREA. THE CORROSION WAS REMOVED, CAUSING THE AREA TO BE OUT OF LIMITS. CESSNA OBTAINED AN 8100-9 REPAIR APPROVAL AND MADE THE REPAIRS.Dec 5, 2012 · N147CX · Cessna 750SDR USAA2012123100018Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING FUEL DOOR 640LB BETWEEN RIB 16 TO RIB 17 & BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640LB IAW A319 AMM 57-27-11-400-002-A.Dec 5, 2012 · N751UW · Airbus A319112SDR USAA2012122800004Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER LEFT WING FUEL DOOR 540HB BETWEEN WS 7316 TO WS 7792, BETWEEN S8L TO S11L & BETWEEN RIB 13 TO RIB 14. REPLACED LOWER LEFT WING FUEL DOOR 540HB IAW A319 SRM 51-72-11 & 57-27-11 PARA 4B ITEM 4.Dec 5, 2012 · N751UW · Airbus A319112SDR ASOA20121205153Skin · crackedDURING A-CHECK INSPECTION THE RT WING SKIN WAS FOUND TO HAVE A .70" LOG CRACK AT THE CUT-OUT FOR THE SPOILER CENTER HINGE POINT. INSTALLED A REPAIR DOUBLER TO THE AFFECTED AREA AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 5, 2012 · N15926 · Emb EMB145EPSDR FDEA201212044238Skin · crackedRT WING SLAT TRACK NR 12 LOWER OTBD CUT-OUT CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11FSDR FDEA201212044234Slat Track · crackedLEFT WING NR 8 SLAT TRACK UPPER DOOR CUT-OUT CRACKED. REPAIRED AS PER E.A. 1-5730-163557. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Dec 4, 2012 · N599FE · Doug MD11FSDR AALA20121204001Skin · corrodedRIGHT WING INBOARD END JUST FORWARD OF AFT SPAR HAS CORROSION. REWORKED CORROSION AND INSTALLED SECOND OVER FASTENERS AS PER EA B767-57-0273449.Dec 4, 2012 · N376AN · Boeing 767323SDR QXEA2012120301549Access Panel · corrodedRT UPPER WING ACCESS PANEL 621BT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. MEASURED BLENDED AREAS BELOW MIN THICKNESS, MIN .215 ACTUAL .198 REF RD 8/4-57-425. PANEL OUT OF LIMITS, RECEIVED NEW PANEL FROM STOCK.Dec 3, 2012 · N433QX · Bombdr DHC8402SDR UHLA2012120200407Skin · crackedMAJOR REPAIR - LEFT WING LOWER SURFACE A3 HOLE HAS CRACK LIKE INDICATION. CRACK FOUND TO EXTEND BEYOND SB170-57-0053 LIMITS. PERFORMED MAJOR REPAIR ON SPAR II IAW ETD 2012-170-017538.Dec 2, 2012 · N638RW · Emb ERJ170100SESDR SWIA201232391Skin · damagedFOUND 3 EACH PREVIOUSLY OVERSIZED HOLES THRU RIGHT LOWER WING PLANK. (C-CHECK) REPAIRED IAW REO.Dec 1, 2012 · N909SW · Cndair CL6002B19SDR FDEA201211304219Skin · corrodedLT WING T/E PANEL 541JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11FSDR FDEA201211304217Skin · corrodedRT WING T/E PANEL 641JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11FSDR FDEA201211304209Duct · crackedLT WING TELESCOPIC DUCT UPPER DOOR CUT-OUT CRACKED. REPAIRED IAW SRM 57-40- 01 REPAIR 10 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Nov 30, 2012 · N599FE · Doug MD11FSDR QXEA2012113001495Access Panel · corrodedLT UPPER WING ACCESS PANEL 521AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. MEASURED BLENDED AREAS MIN .215 ACTUAL .183, REF 8/4-57-425 PG 41. PANEL FOUND TO BE OUT OF LIMITS IAW RD 8/4-57-425. RECEIVED NEW PANEL FROM STOCK.Nov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001493Skin · corrodedRH UPPER WING SKIN LANDING FOR ACCESS PANEL 624AT HAS AREAS OF CORROSION. BLENDED OUT CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .079" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. BLEND FOUND Nov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001492Skin · corrodedLT UPPER WING SKIN LANDING FOR ACCESS PANEL 624BT HAS AREAS OF CORROSION. BLENDED OUT CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. BLEND FOUND Nov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001491Skin · corrodedLT UPPER WING SKIN LANDING FOR ACCESS PANEL 524AT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .079" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHNov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001490Skin · corrodedLT UPPER WING SKIN LANDING FOR ACCESS PANEL 524BT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHNov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001489Skin · corrodedLT UPPER WING SKIN LANDING FOR ACCESS PANEL 524CT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-445. MIN THICKNESS REMAINING .080" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. FOUND TO BE WITHNov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001488Skin · corrodedLT UPPER WING SKIN LANDING FOR ACCESS PANEL 524DT HAS AREAS OF CORROSION. REMOVED CORROSION FROM LANDING IAW RD 8/4-57-441. MIN THICKNESS REMAINING .075" REF NTM 51-00-04-910-801 PT 1. VERIFIED BLENDS CRACK FREE IAW NTM 51-00-06-910-801 PT 1. REPAIR WITHIN LINov 30, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012113001473Panel · corrodedLT UPPER WING PANEL 522AT HAS AREAS OF CORROSION. REMOVED CORROSION FROM PANEL IAW RD 8/4-57-425. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1. FOUND WORKED AREA TO BE IN LIMITS IAW RD 8/4-57-425. APPLIED ALODINE, PRIMERAN DEPT TAPE IAWNov 30, 2012 · N433QX · Bombdr DHC8402SDR SWIA201232322Skin · crackedDURING WING SPLICE INSPECTION FOUND ONE CRACK ON WING SKIN, ORIGINATES FROM TRAILING EDGE OF RIVET AND IS PARALLEL TO WS 65.75. (SERVICE) WORK PERFORMED BY VENDOR IAW REO.Nov 29, 2012 · N408SW · Cndair CL6002B19SDR QXEA2012112901465Access Panel · corrodedLT UPPER WING ACCESS PANEL 524AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDS AND FOUND TO BE IN LIMITS RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. APPLIED ALODINE, PRIMER, REIDENTIFIED PANNov 29, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012112901462Access Panel · corrodedLT UPPER WING ACCESS PANEL 524CT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDS AND FOUND TO BE IN LIMITS RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. APPLIED ALODINE, PRIMER, REIDENTIFIED PANENov 29, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012112901461Access Panel · corrodedLT UPPER WING ACCESS PANEL 524DT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED BLENDED AREAS FOUND WITHIN LIMITS IAW RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. ALODINED, PRIMED, REIDENTIFIED PANELNov 29, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012112901460Access Panel · corrodedRT UPPER WING ACCESS PANEL 624AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. MEASURED IAW RD 8/4-57-442. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. PANEL FOUND WITHIN LIMITS IAW RD 8/4-57-442. APPLIED ALODINED, PRIMER ANov 29, 2012 · N433QX · Bombdr DHC8402SDR QXEA2012112901459Access Panel · corrodedRT UPPER WING ACCESS PANEL 622AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425. CORRODED PANEL WAS FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW.Nov 29, 2012 · N433QX · Bombdr DHC8402SDR SWAA2012121810753Panel · delaminatedLEFT WING L/E PANEL 521WB FWD I/B CORNER IS DELAMINATED. REPAIRED DELAMINATION ON FWD I/B CORNER OF LEFT WING L/E PANEL 521WB IAW SRM 51-70-05-2R-6, 57-40-01, 51-40-02, AND 51-70-14-2R-3 89215U 08DEC2012.Nov 28, 2012 · N552WN · Boeing 7377BXSDR DALA1257150183Skin · crackedRT WING AFT PITCH LOAD FITTING FWD TENSION BOLT AREA OTBD HOLE FOUND CRACKED. REPAIRED IAW ERA 507540-14AD, REV ORIG.Nov 28, 2012 · N183DN · Boeing 767332SDR SWAA2012121210521Panel · delaminatedRIGHT WING L/E PANEL 621CB DELAMINATED AT FWD I/B CORNER. REPAIRED RIGHT WING L/E PANEL 621CB I/B FWD CORNER IAW SRM 51-70-05.Nov 28, 2012 · N552WN · Boeing 7377BXSDR FDEA201211274186Skin · crackedONE FASTENER HOLE FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. REPAIR CARRIED OUT IAW SRM 57-20-02, FIGURE 201, REPAIR 5, REVISIONov 27, 2012 · N605FE · Doug MD11FSDR ABXA20121127333Skin · gougedLEFT WING LOWER SKIN IN ENGINE DRY BAY HAS TOOLING MARKS AT WING STATION 389 JUST AFT OF LOWER SPAR CAP MARKED. BLENDED AREA IAW B767 SRM 51-20-01. MAX MATERIAL REMOVED .046. ACFT WAS GROUNDED.Nov 27, 2012 · N795AX · Boeing 767281SDR SWAA2012120310162Panel · delaminatedRIGHT WING PANEL 6531R DELAMINATED AT SLAT TRACK CUTOUTS. FOUND EDGE BAND DELAMINATED ON RIGHT WING PANEL 6531R, BONDED EDGE BAND BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310161Panel · delaminatedRIGHT WING PANEL 6526R DELAMINATED AT SLAT TRACK CUTOUT. FOUND EDGE BAND DELAMINATED ON RIGHT WING PANEL 6526R, BONDED EDGE BAND BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310160Panel · delaminatedRIGHT WING PANEL 6541R CORNER DELAMINATED AT SLAT ACTUATOR CUTOUT. FOUND EDGE BAND ON RIGHT WING PANEL 6541R DELAMINATED AT SLAT ACTUATOR CUTOUT, BONDED EDGE BAND BACK TO PANEL USING EA934NA/A16511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310159Panel · delaminatedRIGHT WING PANEL 6541R CORNER CRUSHED. FOUND EDGE BAND DELAMINATED AND PULLED BACK ON PANEL 6541R, BONDED EDGE BAND BACK TO PANEL USING EA934NA/A60511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310158Panel · delaminatedLEFT WING PANEL 6223L DELAMINATED AT SLAT TRACK CUTOUT. FOUND EDGE BAND ON LEFT WING PANEL 6223L DISBONDED. BONDED EDGE BAND BACK TO PANEL USING EA934NA/A60511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310157Panel · delaminatedLEFT WING PANEL 6231L DELAMINATED AT CORNERS OF TRACK CUTOUTS. FOUND EDGE BAND DELAMINATED ON LEFT WING PANEL 6231C, BONDED EDGE BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.Nov 27, 2012 · N605SW · Boeing 7373H4SDR SWAA2012120310156Skin · crackedRIGHT WING LEADING EDGE SKIN CRACKED AT UPPER EDGE OF NR 6 SLAT INBOARD AUXILIARY TRACK CUTOUT. REPAIRED DAMAGE AT RIGHT WING LEADING EDGE NR 6 SLAT AUXILARY TRACK CUTOUT IAW EA 1-A57-273 REV 1.Nov 27, 2012 · N605SW · Boeing 7373H4SDR QXEA2012112701437Access Panel · corrodedRT UPPER WING ACCESS PANEL 624BT HAS AREAS OF CORROSION. LOCALLY BLENDED CORROSION IAW RD 8/4-57-442.Nov 27, 2012 · N433QX · Bombdr DHC8402SDR TRBA20121127002Skin · corrodedDURING MX INSPECTION, FOUND CORROSION AT RT WING BOTTOM T/E BETWEEN RIB 6 AND 10. ACFT REMOVED FROM SERVICE. INSTALLED RT WING T/E RIB 8-10 PANEL JIC 53-93-00 RAI-10000. ACFT RETURNED TO SERVICE.Nov 27, 2012 · N448AM · Aerosp ATR72212SDR ASOA2012121302642Skin · crackedLT WING LOWER SKIN PLANK CRACKED AT WS 148.019 FWD OF REAR SPAR. CRACK IS 1.025". UPON REMOVAL OF SKIN PANEL AT WS 127-25 -WS 148.019 FOUND JOINT STRAP AT WS 148.019 BROKEN. STRAP REQUIRES REPLACEMENT. LOCATED, DRILLED, SEALED AND INSTALLED A NEW JOINT STRNov 26, 2012 · N823AS · Cndair CL6002B19SDR TRBA20121126008Access Panel · corrodedDURING MX INSPECTION, FOUND CORROSION ON THE RT T/E ACCESS PANEL HINGE NEAR RIB 5-6. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING T/E ACCESS PANEL HINGE NEAR RIB 5-6. NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERNov 26, 2012 · N448AM · Aerosp ATR72212SDR TRBA20121126007Skin · corrodedDURING MX INSPECTION, FOUND CORROSION AT THE RT WING L/E BETWEEN RIB 4-5. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING L/E BETWEEN RIB 4-5 NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERVICE.Nov 26, 2012 · N448AM · Aerosp ATR72212SDR DALA1255350183Skin · crackedLT WING AFT PITCH LOAD FITTING FOUND TENSION BOLT HOLE AREA CRACKED AT WING LWR SKIN. FREEZE PLUG REPAIR IAW ERA 507539-14, REVO.Nov 26, 2012 · N183DN · Boeing 767332SDR ABXA20121125335Skin · corrodedSKIN BULGING AND POSSIBLE CORROSION AT RT WS 1025 UPPER SURFACE ABOVE OUTBOARD. AILERON, OUTBOARD OF PCA. REMOVED CORROSION AND REPAIRED AREA IAW REA B657-60384-MR. ACFT WAS GROUNDED.Nov 25, 2012 · N795AX · Boeing 767281SDR FDEA201211244147Skin · crackedLT WING L/E LOWER SURFACE ACCESS PANEL 518FB CUT-OUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 202, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.Nov 24, 2012 · N605FE · Doug MD11F
Back to JASC 5730