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 CA060927003Skin · cracked(CAN) PERIMETER WAS INFORMED FROM ANOTHER OPERATOR OF THE SAME AIRCRAFT OF POTENTIAL WING SKIN CRACKS EMINATING FROM THE LT AND RT BATTERY VENT SCOOPS INSTALLED IN THE LOWER WING SKIN BETWEEN THE NACELLE AND FUSELAGE. INITIAL VISUAL INSPECTION REVEALED NO CRACSep 27, 2006 · Swrngn SA227ACSDR USAA061196Skin · wornKG WING, PYLON I/B SKATE ANGLE WING ATTACH HAS WEAR. OVERSIZED THE AFFECTED FASTENER HOLES AND REASSEMBLED WITH NEW OVERSIZED FASTENERS IAW EA 98052, DEFECT SIZE: .187 INCH.Sep 26, 2006 · N532AU · Boeing 7373B7SDR IXXA06SMN320SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 ALTERNATE TANK CRACKED AT STATION XW485.000, CONFIRMED WITH NDT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PSep 25, 2006 · N825BX · Doug DC871FSDR DU4R2006642Skin Panel · corrodedCORROSION RT WING FUEL TANK UPPER ACCESS PANELS (9) MATING SURFACE AND COUNTERSINKS. REPLACED 1 PLATE P/N ARB0975-520, REWORKED 8 PLATES, IAW DC-9/MD-80 SRM 51-22-2A AS DIRECTED BY TIMCO RFTS 60005.Sep 25, 2006 · N921DL · Doug MD88SDR DU4R2006641Skin Panel · corrodedCORROSION LT WING FUEL TANK UPPER ACCESS PANELS (4 ) MATING SURFACE AND COUNTERSINKS. REWORKED PLATES, FABRICATED AND INSTALLED 2 BUSHINGS IAW DC-9/MD-80 SRM 51-22-2A AS DIRECTED BY TIMCO RFTS 60005.Sep 25, 2006 · N921DL · Doug MD88SDR CALA0600363Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 6 FIXED L/E SKIN AT WS 255-389. REPAIRED IAW SRM 51-70-17 AND 51-40-02.Sep 23, 2006 · N14341 · Boeing 7373T0SDR 06FDEA03398Skin · damagedFASTENER HOLES ELONGATED AT LANDING OF ACCESS PANEL 650LB (30 EA) RIGHT WING. COMPLIED WITH EA 6-5730-104952 PART 1 FOR ELONGATED HOLES IN PANEL LANDING 650LB.Sep 22, 2006 · N677FE · Airbus A300F4605RSDR UPS06848094Doubler · crackedINSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 597. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21,51-1-20D AND DWG 5769600.Sep 21, 2006 · N708UP · Doug DC871FSDR QXEA200602580Skin Panel · nickedC3 PDX - LEFT WING INBOARD FIXED LEADING EDGE PANEL 521AT HAS 2 NICKS. REPAIRED IAW SRM 57-41-01 AND SRM 51-21-11.Sep 21, 2006 · N608QX · Cndair CL6002C10SDR UIEA200600265Panel · crackedLT WING TOP T/E PANEL AT WBL 235.65 HAS A 1.750 INCH CRACK 17.0 INCHES FROM FORWARD EDGE OF PANEL. ACCOMPLISHED PREPREG LAYUP 250 DEGREES CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG. 2 AND SRM 51-40-12.Sep 21, 2006 · N517MC · Boeing 747243BSDR UIEA200600264Panel · delaminatedRT WING TOP L/E PANEL AT ILES 559.72 HAS AREA OF 4.0 BY 7.0 INCH OF DELAMINATION. ACCOMPLISHED PREPREG LAYUP 250 DEGREES F CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 AND 747 SRM 51-40-12.Sep 21, 2006 · N517MC · Boeing 747243BSDR QXEA200602577Skin · chafedC3 PDX - LEFT WING FIXED LEADING EDGE 522RL CHAFED IN 5 PLACES JUST BELOW CENTER LINE OF LEADING EDGE. REPAIRED IAW SRM 57-41-01 AND SRM 51-25-01.Sep 20, 2006 · N608QX · Cndair CL6002C10SDR QXEA200602584Skin · gougedC3 PDX - GOUGE IN RIGHT WING FIXED LEADING EDGE AT WS 180 BETWEEN INBOARD AND MID SLAT. REPAIRED IAW SRM 51-21-11 AND SRM 51-20-006, SRM 57-41-01.Sep 20, 2006 · N608QX · Cndair CL6002C10SDR 06FDEA03363Skin · tool damageFASTENER HOLES HAVE TOOLING MARKS AT LANDING OF ACCESS PANEL 650NB (7 EACH) RIGHT WING COMPLIED WITH EA 6-5730-104952 PART 1 FOR TOOLING MARKS ON PANEL LANDING FOR 650NB.Sep 19, 2006 · N677FE · Airbus A300B4622RSDR QXEA200602583Skin · gougedC3 PDX - GOUGES ON RIGHT WING LEADING EDGE PANEL 621AT. REPAIRED IAW SRM 57-41-01 AND SRM 51-20-004, SRM 51-20-006.Sep 16, 2006 · N608QX · Cndair CL6002C10SDR USAA061168Skin · crackedFOUND LOWER LT WING O/B OF ENGINE FWD OF FRONT SPAR. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW TR 57-41-02, DEFECT SIZE: 1".Sep 13, 2006 · N532AU · Boeing 7373B7SDR IXXA06SMN299SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN CRACKED AT STATION XFS360.000. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. APPLIED SEALANSep 12, 2006 · N825BX · Doug DC871FSDR QXEA200602540Skin · chafedC4 YYC - RIGHT WING OUTBOARD TRAILING EDGE FLAP TOP SKIN HAS A CHAFE MARK AT WING STATION YW 180.0. REPAIRED IAW RD8-57-3461.Sep 9, 2006 · N357PH · Dhav DHC8202SDR QXEA200602543Skin · damagedC4 YYC - LEFT WING LOWER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT STATION YW326. REPAIRED IAW SRM 51-40-11 AND SRM 51-20-51.Sep 8, 2006 · N357PH · Dhav DHC8202SDR EIA2006242Skin · corrodedRIGHT WING LEADING EDGE FRONT SPAR AND LOWER SKIN INTERFACES FOUND CORROSION AT FSSI 1430. CORROSION AREA REPAIRED IAW EA57-0511.Sep 7, 2006 · N485EV · Boeing 747212BSDR QXEA200602539Skin · damagedC4 YYC - LEFT OUTER WING LEADING EDGE BOTTOM SKIN HAS SMOKING FASTENERS. REPAIRED IAW SRM 51-40-00, 51-20-26.Sep 7, 2006 · N357PH · Dhav DHC8202SDR 06FDEA03225Skin · damagedLT WING L/E SLAT TRACK CUT OUT STA XOS 890 EXISTING REPAIR REPAIRED IAW SRM 57-10-00 FIG 49 AND 51-30-00 VOL II.Sep 7, 2006 · N567FE · Doug DC1010SDR 06FDEA03224Skin · damagedLT WING L/E SLAT TRACK CUT OUT STA XOS 610 EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 51-30-00 VOL II.Sep 7, 2006 · N567FE · Doug DC1010SDR 06FDEA03223Skin · damagedRT WING L/E SLAT TRACK CUT OUT STA XOS 890 EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 57-10-00 FIG 68 VOL 1.Sep 7, 2006 · N567FE · Doug DC1010SDR 06FDEA03218Skin · crackedLEFT WING, FIXED LEADING EDGE SKIN AT TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103504, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 6, 2006 · N608FE · Doug MD11FSDR MWEA060191Skin · damagedSKIN BENT DUE TO IMPACT DAMAGE FROM BAG CART. FABRICATED AND INSTALLED SKIN.Sep 5, 2006 · N927ME · Boeing 717200SDR 06FDEA03184Skin · crackedRIGHT WING, FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103503, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 5, 2006 · N608FE · Doug MD11SDR WRLA2006076Skin · corrodedDURING 2C+12A+150M CHECK FOUND CORROSION ON RIGHT WING UPPER SKIN AT XORS 97 TO XORS 1070 BETWEEN FRONT SPAR AND REAR SPAR.Sep 3, 2006 · N275 · Doug MD11FSDR WRLA2006075Skin · corrodedDURING 2C+12A+150M CHECK, FOUND CORROSION ON LEFT WING UPPER SKIN AT XORS 97 TO XORS 1070 BETWEEN FRONT SPAR TO REAR SPAR.Sep 3, 2006 · N275 · Doug MD11FSDR DU4R2006608Skin · gougedLT I/B FLAP LOWER SKIN GROUP OF NICKS AT 16 INCHES FROM I/B EDGE. BLENDED GOUGES OUT OF LT I/B FLAP LOWER SKIN. REMOVED AND REPLACED SKIN 22-3/4" BY 1-3/8", 24-7/8" BY 4" FROM 7075-T6 .063 AND 42-1/4" BY 25" FROM 7075-T6 .040" AND LOWER TEE REPAIR 41" BY 12.Sep 3, 2006 · N924DL · Doug MD83SDR UIEA200600221Skin · corrodedN415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINE 105 LEFT WING UPPER SURFACE WS 752-779 FIVE BLENDED & RESURFACED AREAS ON THE OUTER AREA. FWD MOST DEPTH TO BE CHECKED. FWD BLEND OUT CHECKED BETWEEN WS 752 - WS 779. MAX DEPTH OF BLEND OUT = 0.017 Aug 31, 2006 · N415MC · Boeing 74747UFSDR 06FDEA03137Skin · corrodedLT WING UPPER SURFACE FOUND CORROSION AT XORS 270 STR 2 AREA. REPAIR CARRIED OUT AT LH WING UPPER SURFACE XORS 270 STR 2 AREA AS PER FEDEX EA 1-5710-103499.Aug 29, 2006 · N580FE · Doug MD11SDR 06FDEA03134Doubler · crackedSNRM N00501: RT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 613. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-103491, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Aug 29, 2006 · N580FE · Doug MD11SDR 06FDEA03133Doubler · crackedSNRM N00500: RT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 639. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-103491, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Aug 29, 2006 · N580FE · Doug MD11SDR 06FDEA3088Skin · damagedRT WING UPPER SKIN AT STA XORS 160 HAS A DOUBLER REPAIR 19" BY 11". CUT OUT ORIGINAL DOUBLER IAW SRM 57-10-00 FIGURE 44 VOL 1 AND ACCOMPLISHED FEDEX EA 8-5710-99717.Aug 25, 2006 · N365FE · Doug DC1010SDR 06FDEA3087Skin · damagedLT WING CRACK 1" LONG AT STA 480 ON L/E SKIN. REPAIRED IAW SRM 57-10-00 FIG 68 VOL 1.Aug 25, 2006 · N365FE · Doug MD1010FSDR 06FDEA3086Skin · damagedLT WING FOUND 1 CRACK ON DOOR SKIN LONG.1.25". REPAIRED IAW SRM 57-10-00 FIGURE 8 VOL.1.Aug 25, 2006 · N365FE · Doug MD1010FSDR QXEA200602379Skin · chafedPDX - C3 CHECK, RIGHT WING INBOARD SLAT OUTER UPPER CORNER IS CHAFING ON UPPER LEADING EDGE SKIN. FOUND CORNER OF TRAILING EDGE CHIPPED, ROUNDED CORNER SMOOTH. MATERIAL LOSS WAS .001. POLISHED UPPER SKIN CHAFFE. WITHIN LIMITS OF SRM 57-42-01-101-001-A01. Aug 23, 2006 · N602QX · Cndair CL6002C10SDR TRAX200600649Skin · crackedRANRC NR 396, RT WING PLANK CRACKED AT RHWS 148.0. REPAIRED IAW ALL FAA APPROVED REPAIR MANUALS.Aug 22, 2006 · N823AS · Cndair CL6002B19SDR UPS06448146Skin · corrodedINSPECTION TYPE:C M/D CENTER SECTION UPPER SURFACE FOUND CORROSION AT BS 1180 RBL 98. CORROSION BLEND OUT 0.050" BY 2" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35603 AND UPS ENGINEERING FILE NUMBER 747-57-20115.Aug 21, 2006 · N682UP · Boeing 747121SDR 06FDEA03022Skin · crackedRIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED. RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT REPAIR CARRIED OUT PER FEDEX EA NR 1-5730-1013480, WINGS RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING Aug 21, 2006 · N621FE · Doug MD11SDR 06FDEA03021Skin · crackedLEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED, SNRM NR N00183. LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA NR 1-5730-103497, WINGS, LT WING LEADING EDGE SKIN CRACKAug 21, 2006 · N621FE · Doug MD11SDR UPS06247770Panel · delaminatedLEFT WING OUTBOARD PANEL DELAMINATED. REMOVED DAMAGED AREA OF SKIN PER SRM 51 40 24. MADE REPAIR PARTS TREATED WITH AC 130 SOLGEL. REF SRM 51 40 20, PG 42 46. APPLIED PRIMER BARED AFT 175* PER SRM 51 40 24 FIG 2.Aug 20, 2006 · N941UP · Boeing 72722CSDR A6WA200640326Panel · corrodedFOUND RIGHT WING PLANK ACCESS HOLE BETWEEN BL 0.00 AND WS 12.245 FUEL PANEL 610AB HAS MINOR CORROSION AT INBOARD RADIUS. MAINTENANCE BLENDED MINOR CORROSION, PERFORMED EDDY CURRENT, ROTOPEENED, SANDED AND APPLIED FINISH IAW REO 601R-57-21-030. (M)Aug 19, 2006 · N407AW · Cndair CL6002B19SDR UIEA200600213Panel · delaminatedRIGHT WING, INBOARD LEADING EDGE WING PANEL AT WING STATION 248.81 TO 268.81, INNER SKIN HAS AREA OF COMPOSITE DELAMINATION 20.0 INCH LONG BY 22.0 INCH WIDE. ACCOMPLISHED INTERIM REPAIR OF AREA AS PER ATLAS XEO 57-081706. REQUIRES REPEAT INSPECTIONS AT EVERYAug 18, 2006 · N512MC · Boeing 747230BSDR UIEA200600212Panel · crackedRIGHT WING FIXED TRAILING EDGE PANEL AT WBL 445.9 OUTBOARD AFT END OF PANEL HAS 1.0 INCH LONG CRACK AND LOWER AREA HAS AREA OF DETERIORATION. ACCOMPLISHED PREPREG 250 DEGREES PERMANENT REPAIR OF AREAS AS PER 747 SRM 51-40-09 AND 51-40-12.Aug 18, 2006 · N512MC · Boeing 747230BSDR UPS06448113Skin · corrodedFOUND BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.120" BY 5" BY 5" EXCEED SRM LIMIT. BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35591 AND UPS ENGINEERING FILE NUMBER 747-57Aug 17, 2006 · N682UP · Boeing 747121SDR EIA2006197Skin · gougedLOWER SKIN OF LEFT WING STA 1241 OUTBOARD OF BUTTERFLY FITTING, SKIN GOUGED IN 4 AREAS. FABRICATED AND INSTALLED REPAIR PER B747 SRM 57-30-01 AND ECRA 470-292-2 REV A.Aug 17, 2006 · N470EV · Boeing 747273CSDR DHL2006809519Skin · damagedRT WING CTR LE LWR EXTERNAL SKIN HAS AN INTERIM REPAIR AT STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060702 DATED 07-10-06. REMOVED FASTENERS FROM REPAIR AREA AND EXISTING DOUBLER IAW SRM 51-1-20D, SRMAug 17, 2006 · N809DH · Doug DC873FSDR DHL2006809521Doubler · crackedRT WING TOP PANEL NR 3 MAIN TANK ACCESS DOOR 505E, CRACK ON PREVIOUSLY REPAIRED DOUBLER CONTINUES 0.375" (STA XRS 107.000 - 139.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-16-06, EO NR AST060707 DATED 07-15-06. REMOVED EXISTING INTAug 17, 2006 · N809DH · Doug DC873F
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