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 IXXA06SMN423SDoubler · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING NR 2 STUB WING SLOT DOUBLER HAS ELONGATED HOLES AT STATION XS 250.000. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FNov 17, 2006 · N799AL · Doug DC862FSDR IXXA06SMN407SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 4 STUB WING UPPER SKIN CORRODED AT STATION XF520.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED RENov 17, 2006 · N799AL · Doug DC862FSDR IXXA06SMN398SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING REPAIR OUTBOARD LEADING EDGE UPPER SKIN HAS A NON STANDARD REPAIR AT STATION XFS566.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND ANov 17, 2006 · N799AL · Doug DC862FSDR IXXA06SMN384SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD LEADING EDGE UPPER SKIN DOUBLER CORRODED AT STATION XFS195.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED PANEL WITH EXISTING DOUBLER. FABRICATED NEW PANEL. CLEANED, TREATED AND PRIMNov 17, 2006 · N799AL · Doug DC862FSDR IXXA06SMN397SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING HAS A NON STANDARD REPAIR ON THE LOWER SKIN AT STATION XFS566.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FNov 17, 2006 · N799AL · Doug DC862FSDR IXXA06SMN381SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING LOWER SKIN DRAIN HOLE CRACKED AT STATION XFS597.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMANov 17, 2006 · N799AL · Doug DC862FSDR QXEA200603029Panel · damagedC3 OKC - LEFT WING PANEL 522CB HAS DAMAGE ON TABS. REPAIRED IAW SRM 57-52-01, 51-20-00.Nov 17, 2006 · N612QX · Cndair CL6002C10SDR DHL2006807522Skin · crackedRT OUTER WING INBD EXTENDED L/E LWR SKIN 0.750" CRACK STA XFS 610.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-15-06 DWG AC24-57-R05 REV. IR DATED 11-03-06. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21. CUT OUT DAMAGED SECTION IANov 17, 2006 · N807DH · Doug DC873FSDR DHL2006807520Skin · corrodedLT WING L/E UPPER SKIN CORROSION AT STA XS 250.080 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED NOV 15/06, DWG AC24-57-R06 REV IR DATED 11-03-06. REMOVED EXISTING REPAIR DOUBLER NEAR AFFECTED AREA IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CNov 17, 2006 · N807DH · Doug DC873FSDR QXEA200603023Panel · chafedC3 OKC - PANEL 684JB IS CHAFED. REPAIRED IAW SRM 57-61-01, 51-13-00, ND 51-25-06.Nov 16, 2006 · N612QX · Cndair CL6002C10SDR DHL2006807513Skin Panel · delaminatedRT WING UPPER PANEL SKIN DELAMINATED 7" (STA XRS 435.000 - 475.000). REMOVED AND REPLACED RT WING UPPER PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE).Nov 16, 2006 · N807DH · Doug DC873FSDR QXEA200603504Skin · corrodedC2 PDX - FRETTING AROUND BOLT HOLES ON WING SKIN FOR PANEL 624CT. REPAIRED IAW RD8/4-57-0445.Nov 15, 2006 · N416QX · Bombdr DHC8402SDR QXEA200603062Panel · corrodedC2 PDX - LEFT WING FUEL PANEL LANDING FOR 524CT HAS FRETTING AND SIGNS OF CORROSION AT SEVERAL SCREW HOLES. REPAIRED IAW RD8/4-57-445.Nov 15, 2006 · N416QX · Bombdr DHC8402SDR QXEA200603061Panel · corrodedC2 PDX - PANEL 624CT FRETTING AROUND NUMEROUS BOLT HOLES. REPAIRED IAW RD8/4-57-0443.Nov 15, 2006 · N416QX · Bombdr DHC8402SDR DHL2006363552Skin · corrodedBOTTOM OF L/W SKIN HAS CORROSION AT DRAIN HOLE FWD OF NR 6 FLAP TRACK. CORROSION BLEND OUT TO A MAJOR REPAIR AT L/W BOTTOM SKIN SLAT TRACK NR 9 DRAIN HOLE FWD OF NR 6 FLAP TRACK ASSEMBLY, FOUND TO BE OUT OF LIMITS AS PER ATTACHED AIRBUS REPAIR APPROVAL SHEETNov 14, 2006 · N363DH · Airbus A300B4203SDR 06FDEA04006Skin · corrodedLT WING INT AILERON FOUND CORROSION UNDER SKIN AILERON LOWER SIDE SKIN AT STA 300 XIA. CUT DAMAGED SECTION OF LOWER SKIN. REPAIRED IAW SRM 57-10-00 FIG 86 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027611/N02611.Nov 14, 2006 · N554FE · Doug DC1010SDR DHL2006807521Skin · damagedRT WING CTR L/E LWR SKIN HOLES ELONGATED STA XFS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-10-06, DWG AC24-57-R03 REV IR DATED 11-01-06. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DWG AC24-57Nov 13, 2006 · N807DH · Doug DC873FSDR 06FDEA03992Skin · crackedRT WING L/E AT NR 9 CUT OUT SLAT TRACK LWR AREA, EXISTING DOUBLER REPAIR XOS 602. EXISTING REPAIR REMOVED, AREA ASSESSED TWO CRACKS TRIMMED OUT AND FILLERS FABRICATED, NEW DOUBLER PLATE FABRICATED AND FITTED IAW SRM 57-10-00 PAGES 215-216A FIG 68 (SHT 1,2,3) Nov 13, 2006 · N554FE · Doug DC1010SDR 06FDEA03990Skin · misrepairedRT WING L/E SKIN AT NR 10 CUTOUT SLAT TRACK, EXISTING DOUBLER REPAIR STA XOS 659. RT WING L/E SKIN AT SLAT TRACK NR 10 EXISTING DOUBLER REPAIR STA XOS 659 REMOVED IAW SRM 51-30-00 VOL 2 AS NONE CONFIRMING REPAIR. REPLACED WITH DOUBLER IAW SRM 57-10-00 FIG 68Nov 13, 2006 · N554FE · Doug DC1010SDR 06FDEA03989Skin · crackedRT WING L/E XOS 550 1 CRACK ON ATTACHED PANEL STRAP. LOWER LEADING EDGE STRINGER DOUBLER REPAIRED IAW SRM 57-10-00 FIG 49, PAGE 163 VOL1. FAB PART IAW DETAIL PART TRAVELER N02724 AND SRM 57-10-00 FIG 49 VOL 1.Nov 13, 2006 · N554FE · Doug DC1010SDR 06FDEA03979Skin · corrodedRT WING LWR SKIN TANK AT XORS 250 ON DOUBLER BEAVER TAIL FOUND SEVERE CORROSION WITH EXFOLIATION. REMOVED CORROSION IAW SRM 57-00-01 FIG 8 SHT 3 4 VOL 1. REMOVED FASTENERS IAW SRM 51-34-01 PAGE 1/7 VOL 2. RECORDED RESIDUAL MTL. THK AND VERIFIED REWORK LIMITNov 13, 2006 · N567FE · Doug DC1010SDR QXEA200603097Skin · damagedC3 YYC - RIGHT LOWER WING LEADING EDGE SKIN HAS LOOSE AND MISSING RIVETS AT WS 88. REPAIRED IAW SRM 51-42-06, 51-42-02.Nov 12, 2006 · N613QX · Cndair CL6002C10SDR IXXA06SMN355SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD STUB WING UPPER SKIN CORRODED AT STATION XFS246.000 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER FILLERS AND STRAP. TREATED REPAIR AREA AND REPANov 10, 2006 · N799AL · Doug DC862SDR IXXA06SMN354SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND RIGHT WING INTERNAL LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS157.000 TO STATION XFS163.750. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERNov 10, 2006 · N799AL · Doug DC862FSDR IXXA06SMN353SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORRODED STATION XF195.500 UPPER SIDE. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED NEW SKIN Nov 10, 2006 · N799AL · Doug DC862FSDR DHL2006807512Skin Panel · delaminatedLT WING UPPER PANEL SKIN DELAMINATED 7" (STA XA 613.000 - 681.000). REMOVED AND REPLACED LT WING UPPER PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Nov 10, 2006 · N807DH · Doug DC873FSDR ASAA0641186Skin · nickedLT OB AFT FLAP TE IS NICKED AND SEPARATING JUST OB OF IB TRACK FAIRING. REMOVED DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 10.Nov 8, 2006 · N772AS · Boeing 7374Q8SDR DHL2006807503Doubler · crackedRT WING OTBD L/E INBD SECTION INTERNAL DOUBLER 1" CRACK APPROX STA XFS 572.000 (LWR PART). REMOVED CRACKED DOUBLER IAW SRM 51-1-21. FABRICATED DOUBLER (AL7075T6 0.050") IAW SRM 57-3-3 PG 16. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSNov 6, 2006 · N807DH · Doug DC873FSDR UPS06448692Skin · corrodedINSPECTION TYPE:C RIGHT WING WS 402 CORROSION REVEAL AT MATTING SURFACE BETWEEN CHORD AND EXTENSION SKIN (DEFECT FOUND AFTER EXTENSION SKIN LIFT UP) FOR CHORD REPAIR. CORROSION BLEND OUT 0.124" X 2" X 2" & 0.137" X 1.5" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS, Nov 5, 2006 · N677UP · Boeing 747123FSDR 06FDEA03894Skin · corrodedLEFT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.430", MATERIAL REMOVED = 0.041", REMAINNov 5, 2006 · N619FE · Doug MD11SDR 06FDEA03893Skin · corrodedLEFT WING TOP SKIN SURFACE AFT AT XORS 779 FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT XORS 792 CORROSION REMOVED AS PER SRM 51- 21-01 VOLUME II. ORIGINAL THICKNESS = 0.175", MATERIAL REMOVED = 0.046", REMAINED THICKNESS = 0.129" AND FOUND ENov 5, 2006 · N619FE · Doug MD11SDR IXXA06SMN339SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORROSION AT STATION XF803.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS, Nov 4, 2006 · N799AL · Doug DC862SDR IXXA06SMN352SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS341.500. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO Nov 4, 2006 · N799AL · Doug DC862SDR IXXA06SMN341SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CRACKED AT STATION XW74.000, STRINGER 11. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND FINov 4, 2006 · N799AL · Doug DC862SDR IXXA06SMN340SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORRODED FROM STATION XF422.520 TO STATION XOLDI6.225 UPPER SIDE. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVNov 4, 2006 · N799AL · Doug DC862SDR 06FDEA03866Skin · misrepairedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. PREVIOUS COMPOSITE REPAIR LOCATED ON RT WING LEADING EDGE, WS 1182, RIB 19, REPAIR LOCATED BETWEEN NUMBER 2 AND 3 SLAT. REPAIR REQUIRES EVNov 4, 2006 · N431FE · Airbus A310203SDR QXEA200602980Access Panel · chafedC1 OKC - LEFT WING ACCESS PANEL 584JB IS CHAFED. REPAIRED IAW SRM 51-21-00 AND 51-12-00, 51-25-06.Nov 3, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602975Access Panel · chafedC1 OKC - RIGHT WING ACCESS PANEL 684GB IS CHAFED. REPAIRED IAW SRM 51-12-00 AND 57-52-01.Nov 3, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602974Access Panel · chafedC1 OKC - RIGHT WING ACCESS PANEL 684EB IS CHAFED. REPAIRED IAWSRM 51-12-00 AND 57-52-01.Nov 3, 2006 · N618QX · Cndair CL6002C10SDR 06FDEA03833Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 643. REPAIRED AS PER FEDEX EA NR 1-5730-104824, PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11SDR 06FDEA03832Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 698 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 698. REPAIRED AS PER FEDEX EA NR 1-5730-105537, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11SDR 06FDEA03831Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 728 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE AT XOS 728 REPAIRED AS PER FEDEX EA 1-5730-105538, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11SDR DHL2006780107Skin · crackedLEFT WING TIP UPPER SURFACE, WBL 638, AFT OF NAV LIGHT LENS COVER, PREVIOUS REPAIR CRACKED. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FAB DOUBLER FROM 7075-T6, 0.050, PO NR 6149108, DIM 4 BY 3. FILLER FROM 7070-T6 0.040, PO NR 9003839, DIM. 2.50 BY 1.50Nov 2, 2006 · N780DH · Boeing 727223SDR DHL2006780007Skin · crackedNR 077407, LT WING TIP UPPER SURFACE, WBL 638, AFT OF NAV LIGHT LENS COVER, PREVIOUS REPAIR CRACKED. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FAB DOUBLER FROM 7075-T6, 0.050, PO NR 6149108, DIM. 4 BY 3. FILLER FROM 7070-T6 0.040, PO NR 9003839, DIM. 2.50 BY Nov 2, 2006 · N780DH · Boeing 727223SDR QXEA200602977Access Panel · chafedC1 OKC - RIGHT WING ACCESS PANEL 684LB IS CHAFED. REPAIRED IAW SRM 51-12-00 AND 57-52-01.Nov 2, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602976Access Panel · chafedC1 OKC - RIGHT WING ACCESS PANEL 684JB IS CHAFED. REPAIRED IAW SRM 51-12-00 AND 57-52-01.Nov 2, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602983Access Panel · gougedC1 OKC - LEFT WING ACCESS PANEL 584LB IS GOUGED. REPAIRED IAW SRM 57-52-01AND 51-21-11.Oct 31, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602982Access Panel · gougedC1 OKC - LEFT WING ACCESS PANEL 584EB IS GOUGED. REPAIRED IAW SRM 57-52-01 AND 51-21-11.Oct 31, 2006 · N618QX · Cndair CL6002C10SDR QXEA200602981Access Panel · chafedC1 OKC - LEFT WING ACCESS PANEL 584GB IS GOUGED. REPAIRED IAW SRM 57-52-01 AND 51-21-11.Oct 31, 2006 · N618QX · Cndair CL6002C10SDR 06FDEA03818Skin · corrodedCORROSION ON WING LOWER SKIN SURFACE, AT NR 2 AFT FLAP TRACK MOUNT. REMOVED CORROSION ON WING LWR SURFACE AT NR 2 FLAP TRACK MOUNT AND REPAIRED IAW FED EX EA 7-5710-100598.Oct 31, 2006 · N241FE · Boeing 727200
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