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 DL76L100675Skin · crackedLT WING, AFT PITCH LOAD FITTING AREA OTBD FWD BOLT HOLE CRACKED AT SKIN LOWER EDGE RUNNING FWD APPROX .0625" IN LENGTH. REPAIRED IAW ERA 479965-14AD REV 0.Feb 18, 2010 · N172DN · Boeing 767332SDR FDEA201002180448Skin · wornLT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.Feb 18, 2010 · N315FE · Doug DC1030FSDR 22AA201000038Skin · crackedDURING "C" CHECK, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN FOUND CRACK. NON-ROUTINE NR 372, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN REPAIR IAW EN 1003-10 AND FAA APPROVED FORM 8110-3 DATED 24 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 2010F00047Skin · corrodedREPAIRED SURFACE AND INNER GRANULAR CORROSION LOCATED FWD WING PLANK IN AREA OF FUEL ACCESS DOOR. REF: GDAS-BAF W/O SC3925 FOR FURTHER DETAILS. RECEIVED ENGINEERING DISPOSITION DATED 02/05/2010, W/O CS197059 STATING REPAIR IAW BLUE PRINT SE45803171-1 REV.-, PFeb 12, 2010 · N255GA · Gulstm GIVSDR UALA2010021200527Skin · crackedUPR WING PANEL ABOVE NR 19 L-E VARIABLE CAMBER FLAP HAS A 18 INCH CRACK APPROX 8 IN OTBD OF INBD END. PREPPED SURFACE FOR REPAIR, FABRICATED PATCH. NEEDS APPLIED & BAGGED, CURED. ACCOMPLISHED 250 DEG. OVER LAY REPAIR, PRIMED AND PAINTED.Feb 11, 2010 · N119UA · Boeing 747422SDR FDEA201002110381Skin · corrodedSURFACE CORROSION - LT WING UPPER SKIN AFT OF NR 3 SLAT AT XORS 361 STR NR 6. REPAIR CARRIED OUT IAW EA NR1-5730-137587, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.Feb 11, 2010 · N579FE · Doug MD11FSDR UALA2010021100524Skin · damagedLT WING PANEL 540 PB WING SKIN BOLT HOLES HAS GOUGES. REPAIRED REF MAE EA 520-57 21-13-A1927 AND UAL EVA.Feb 10, 2010 · N446UA · Airbus A320232SDR AALA20100209TUL01Panel · damagedTRAILING EDGE PANEL AT WING STATION 91 RIGHT TO 99 RIGHT DAMAGED. REPLACED DAMAGED TRAILING EDGE PANEL.Feb 9, 2010 · N494AA · Doug DC982SDR TRBACPCP2010019Skin · corrodedAN AERA OF CORROSION WAS FOUND AT RT WING LOWER SKIN T/E BETWEEN RIBS 6-7. C/A: CORROSION WAS BLENDED OUT IAW SRM AND ATR SRI, MINIMUM REMAINING THICKNESS IS 0.287 IN FOR A NOMINAL THICKNESS OF 0.318 IN. REF SRI NR DO/TS-1345/10-13152, SRAS NR DO/TS-3929/09, 5Feb 9, 2010 · N377AT · Aerosp ATR72212SDR TRBACPCP2010017SUSkin · corrodedAREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN AROUND JACK POINT AT RIB 10. CORROSION WAS BLENDED OUT IAW SRM 51-21-42 AND NDT ASSURING THERE IS NOT MORE CORROSION. CORROSION DOES NOT REACH ANY FASTENER SEATING, FASTENERS WERE NOT REMOVED. REF SRI NR DO/TFeb 9, 2010 · N377AT · Aerosp ATR72212SDR TRBACPCP2010018Skin · corrodedCORROSION WAS FOUND DURING INSP AT C-CHECK AROUND THE SECTION OF THE RT WING, LOWER SKIN SURROUNDING THE RT BOOST PUMP AREA BETWEEN RIBS 4-5. CORROSION WAS REPAIRED IAW SRI INSTRUCTIONS AND EO. REF SRI NR DO/TS-1341/10-13139, SRAS NR DO/TS-3929/09, 5349 ISSUFeb 9, 2010 · N377AT · Aerosp ATR72212SDR TRBACPCP2010007Skin · corrodedCORROSION AROUND RT WING FUEL PUMP CUT-OUT. COMPLIED WITH SRI-DO/TS-OS67/10-12887. RT WING FUEL PUMP CUT-OUT. NO DEFECTS NOTED. COMPLIED WITH SRAS DO/TS-127/08..4458 TO BE INSPECTED IN 2YR INTERVALS. TASK 571402/DVI 10000. OK FOR SERVICE. COMPLIED WITH EO E2-Feb 9, 2010 · N369AT · Aerosp ATR72212SDR TRBACPCP2010006Skin · corrodedCORROSION AROUND LT WING FUEL PUMP CUT-OUT. COMPLIED WITH SRI-DO/TS-0618/10-12888 REF NDT REPORT AMS100121-33 FOR UT & HFEC RESULTS. NO DEFECTS NOTED AT THIS TIME. LT WING SRAS DO/TS-128/08, 4450. AROUND LT WING FUEL PUMP CUTOUT. COMPLIED WITH. OK FOR SERVFeb 9, 2010 · N369AT · Aerosp ATR72212SDR TRBACPCP2010005Wing · corrodedRT WING HAS CORROSION AT RIB 8 BETWEEN STIFFENERS 8-9 UNDER FLAP HINGE FAIRING. COMPLIED WITH SRI DO/TS-0623/10-12890 REF NDT REPORT AMS100121-32 FOR UT AND HFEC RESULTS. NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH EO E2-57MR-365. RT WING LOWER SKIN PNL AT Feb 9, 2010 · N369AT · Aerosp ATR72212SDR TRBACPCP2010004Skin · corrodedLT WING HAS CORROSION AROUND JACK POINT AT RIB 10. COMPLIED WITH SRI-DO/TS-0634/10-1288. REF AMS100121-19. FOR UT VALUES & HFEC RESULTS, NO CRACKS NOTED AT THIS TIME. COMPLIED WITH ATR-SRAS DO/TS-129/08.4451. COMPLIED WITH AE-EO E2-57MR-363 TDMI OPENED FOR 2 Feb 9, 2010 · N369AT · Aerosp ATR72212SDR IPXA10558592Skin · chafedINSP TYPE:C2 LT WING UPPER SKIN IS CHAFED FROM FRONT SPAR TO REAR SPAR AT BL 70. REPAIRED LT WING UPPER SKIN IAW ATS ER NR 10-1520.Feb 9, 2010 · N405UP · Boeing 75724APFSDR UALA2010021100525Skin · gougedPANEL 540PB, WING SKIN BOLT HOLES HAS GOUGES. INSTALLED REPAIR REF MAE EA320-5721-13-A1927 AND EVA.Feb 9, 2010 · N446UA · Airbus A320232SDR GUUA93757020710ASkin · puncturedDURING SCHEDULED ROUTINE INSP DISCOVERED RT STUB WING TOP OF L/E HAS A DENT AND PUNTURED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.Feb 7, 2010 · N38537 · Beech 1900DSDR IPXA10M58617Skin · gougedINSPECTION TYPE:1C, LT WING FIXED L/E APPROX BETWEEN STA XOS 1185-1191 WELD REPAIR GOUGE. GAINED ACCESS, DETERMINED THAT NOTED DAMAGE WAS ADJACENT TO INCOMING WELD REPAIR. REPAIRED NOTED DAMAGE BY WELDING REF STA SA EA 011-5740- 01-A2191 AND EO MD11-5730-36Feb 5, 2010 · N282UP · Doug MD11FSDR IPXA10M58564Skin · gougedINSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W4-01 RT WING FIXED L/E APPROX BETWEEN STA XIS 154-168, PREVIOUS DOUBLER GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER REF STASA EA NR 011-5730-01-A2174, REV IR & EO MD11-5730-36706-A.Feb 5, 2010 · N282UP · Doug MD11FSDR IPXA10M58528Skin · gougedINSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W3-03 LT WING BETWEEN STA XIS210-229 FIXED L/E PREVIOUS REPAIR DOUBLE GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED REPAIR IAW EA 011- 5730-01-A2172 & EO 5730-36689-A.Feb 5, 2010 · N282UP · Doug MD11FSDR IPXA10M58508Skin · gougedINSP TYPE:C1, REPAIR SURVEY SEQ NR 282-W4-02 RT WING FIXED L/E UPPER SKIN, APPROX BETWEEN STA XIS 240-253 PREVIOUS REPAIR DOUBLER IS GOUGED. REMOVED OLD REPAIR DOUBLER, ENLARGED DAMAGE CUT-OUT, FABRICATED AND INSTALLED DOUBLER AND FILLER REF SRM 57-40-02 FIGFeb 5, 2010 · N282UP · Doug MD11FSDR ZZDA2010095Skin Panel · crackedRIGHT WING T/E LOWER SKIN PANEL, STA XRS189, CRACKED. ACCOMPLISHED T/E LOWER SKIN PANEL DOUBLER REPAIR PER B717 SRM 51-41-01 AND B717 SRM 51-41-02.Feb 5, 2010 · N930AT · Boeing 717200SDR IPXA10M58545Skin · crackedINSP TYPE:1C LT WING TELESCOPIC DUCT SPRING DOOR CUT-OUT CRACKED AT BOTH UPPER CORNERS. GAINED ACCESS TO AREA, CUT-OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLERS REF SRM 57-40-01, REPAIR 10, FIG 201, RESTORED AREA.Feb 4, 2010 · N282UP · Doug MD11FSDR ASOA201000160Skin · crackedRT WING FUEL DRAIN HOLE AT APPROX WS 50.00 HAS A 60 PERCENT FSH HFEC INDICATION NOTED 0.100" LONG APPROX 0125" OTBD OF DRAIN HOLE. INDICATION MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-57-21-1230 AND REO 601R-57-21-1230.Feb 3, 2010 · N843AS · Cndair CL6002B19SDR A6WA201040223Skin · gougedLT WING OTBD L/E INNER SKIN AT INBD END GOUGED. TRIMMED EDGE IAW SRM 57-00-31.Feb 2, 2010 · N431AW · Cndair CL6002B19SDR A6WA201040094Skin · crackedINNER SKIN OF RT OTBD WING L/E CRACKED. REPLACED WEB IAW SRM 51-42-10.Feb 2, 2010 · N431AW · Cndair CL6002B19SDR EPUA1553692Skin · chafedABRASION ON LT INBOARD WING SKIN CAUSED FROM LT INBOARD WING/FUSELAGE FAIRING. LOCATED LEFT WING STATION 35 TO 35.5 INCHES FROM TRAILING EDGE, EXTENDING FORWARD 11 INCHES.Feb 1, 2010 · N208SD · Cessna 208BSDR ABXR201002010001Skin · tornWHILE ACCOMPLISHING ROUTINE SCHEDULED MX, THE LT WING-TIP WAS FOUND TO HAVE A TEAR OUT IN THE AREA OF THE AFT LOWER MOUNTING FASTENER HOLE. CUT DAMAGED AREA OUT AND PERFORMED HFEC TO ENSURE DAMAGE WAS REMOVED IAW NDT MANUAL PART 6 51-00-00 FIG. 23. REPAIR INFeb 1, 2010 · N308AS · Boeing 727227SDR FOTR20006NR5287Skin · chafedLT WING STA 574 UPPER LE SURFACE HAS A DEEPLY CHAFED AREA 13" IN LENGTH. REPAIRED ON FASI WO 20006. N/R 05287- REPAIRED LT WING UPPER L/E SURFACE AT STA 574 IAW SRM 57-30-4 FIG 4, REV 102 MATERIAL USED: DOUBLER; 2024-T3, 0.050", DIM: 10.90", 4.10". FILLER; 20Jan 30, 2010 · N286SC · Boeing 7272A1SDR FOTR20006NR5289Skin · crackedLT WING, STA 549, UPPER L/E SLAT TRACK CUTOUT IS CRACKED IN UPPER RADIUS. REPAIRED ON FASI WO 20006. N/R 05289- REPAIRED LT WING UPPER L/E SLAT TRACK CUTOUT AT WS 549 IAW SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 9.50" X 10.0Jan 30, 2010 · N286SC · Boeing 7272A1SDR FOTR20006NR5293Skin · crackedLT WING STA 474 SLAT TRACK CUTOUT UPPER L/E CUTOUT IS CRACKED IN THE RADIUS. REPAIRED ON FASI WO 20006, N/R 05293. REPAIRED LT WING LEADING EDGE AT SLAT TRACK CUTOUT AT WS 474 IAW B727 SRM 57-30-4 FIG 11, REV 102. MATERIAL USED: DOUBLER- 2024-T3, 0.063, DIMJan 30, 2010 · N286SC · Boeing 7272A1SDR FOTR20006NR5351Skin · crackedNR 11 SPOILER 2ND HINGE CUTOUT IS CRACKED AT WS 460. REPAIRED ON FASI WO 20006. N/R 05351- REPAIRED NR11 SPOILER 2ND HINGE CUTOUT AT WS 460 IAW SRM 57-30-4 FIG 10, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.071", DIM: 6.0" X 4.50".Jan 30, 2010 · N286SC · Boeing 7272A1SDR IPXA10M58455Skin · crackedINSPECTION TYPE:2C, LT WING FIXED L/E LWR T/E SKIN CRACK AT STA XOS 610 REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW 57-40-02 REPAIR 7, FIG. 201.Jan 30, 2010 · N288UP · Doug MD11FSDR IPXA10M58432Skin · gougedINSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 288-W3-02 LT WING TELESCOPIC DUCT CUTOUT PREVIOUS REPAIR DOUBLER GOUGED 2 PLACES BTWN XTA XOS 459-475. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-40-01 REPAIR 10, FIG. 20Jan 29, 2010 · N288UP · Doug MD11FSDR AALA20100128TUL18Skin · damagedLEFT INBOARD TRAILING EDGE AFT FLAP HAS A HOLE IN THE LOWER SKIN. REMOVED 2.75 INCH DIAMETER DAMAGED BOTTOM SKIN AND CORE. TOP SKIN UNDAMAGED. FABRICATED NEW CORE AND INSTALLED PER SRM 51-70-17-0G PARAGRAPH 4C FIGURE 11 SECTION B-B.Jan 28, 2010 · N643AA · Boeing 757223SDR IPXA10M58529Skin · crackedINSP TYPE:4C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED ON UPPER INBD AND OTBD CORNERS. CUT OUT DAMAGE AREA AND FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.Jan 28, 2010 · N279UP · Doug MD11FSDR ZZDA2010087Rub Strip · corrodedRIGHT WING UPPER ACCESS PANEL 620CT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 620CT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01.Jan 28, 2010 · N951AT · Boeing 717200SDR SWAA100527Skin · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING L/E SKIN CRACKED AT STA 213. REPAIRED SKIN PER EA.Jan 28, 2010 · N617SW · Boeing 7373H4SDR UALA2010012800339Panel · damagedRT WING L/E: SECOND PANEL INBD OF NR 3 ENGINE HAS 1 RIVET MISSING ON INBD EDGE OF PANEL. REPLACED 1 DAMAGED RIVET ON L/E PNL NR 10, RT 302 ILES, IAW UA-EVA-72940 A.Jan 27, 2010 · N174UA · Boeing 747422SDR UALA2010012800338Panel · damagedRT WING LE SECOND PANEL INBD OF NR 4 ENG HAS 1 RIVET MISSING FROM INBD EDGE OF PANEL. REPLACED 3 DAMAGED RIVETS ON LE PANEL NR14 AT RT 822 ILES, IAW UA-EVA-72940 A.Jan 27, 2010 · N174UA · Boeing 747422SDR UALA2010012800337Panel · damagedLT WING L/E PANEL JUST INBD OF NR 2 ENGINE HAS 3 MISSING RIVETS ON INBD EDGE OF PANEL. REPLACED 3 DAMAGED RIVETS ON L/E PNL NR 5 LT 630 ILES, IAW UA-EVA-72940A.Jan 27, 2010 · N174UA · Boeing 747422SDR IPXA10M58530Skin · crackedINSP TYPE:C4, RT WING FIXED L/E TELESCOPING DUCT INBD AFT CUTOUT CRACKED AT CORNER. CUT OUT DAMAGED AREA FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.Jan 26, 2010 · N279UP · Doug MD11FSDR IPXA10M58485Skin · crackedINSPECTION TYPE:C4 RT WING FIXED L/E SLAT TRACK NR 14 SKIN CUT-OUT CRACKED AT AFT END. CUT OUT DAMAGE AT XOS891, FABRICATED AND INSTALLED FILLER AND DOUBLER REF MD11 SRM 57-40-02 FIG 201 REPAIR 7.Jan 26, 2010 · N279UP · Doug MD11FSDR SIMA201002702Skin · puncturedDURING MAINTENANCE BASE INSPECTION FOUND THAT THE LEFT WING LOWER MAIN LANDING GEAR SKIN WAS DAMAGED DURING JACKING PROCEDURES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE LEFT WING LOWER MAIN LANDING GEAR SKIN IAW EO EM-57MR-460Jan 26, 2010 · N621AE · Emb EMB145LRSDR IXXA10SMN24SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND RT WING NR 3 INBD SLOT VANE HOLES ELONGATED AT STA XW 257.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS, INTERNAL DOUBJan 25, 2010 · N603AL · Doug DC873FSDR FDEA201001250258Skin · crackedDURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND STA XORS 700, 05 EACH FASTENER HOLES FOUND CRACKED INDICATION. REPAIR IAW EA1-5710-132339.Jan 25, 2010 · N574FE · Doug MD11FSDR FDEA201001250257Skin · crackedDURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS 690 AND STA XORS 700, 07 EACH FASTENER HOLES FOUND CRACKED INDICATION. REPAIR IAW EA1-5710-132338.Jan 25, 2010 · N574FE · Doug MD11FSDR IXXA10SMN023SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 505F DOUBLER CRACKED AT STA XRS 22.270 STR 6. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL, INTJan 23, 2010 · N603AL · Doug DC873FSDR 2010FA0000068Skin · corrodedCORROSION FOUND AROUND FASTENERS ON RT WING, L/E AT WING STA 320.Jan 23, 2010 · N422BN · Boeing 727227
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