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 DHL2005782530Skin · crackedR/WING UPPER SURFACE CRACKED AT NR 12 SPOILER HINGE CUTOUT. STOP DRILLED CRACK SIZE .250 IAW B72 SRM 51-10-1. FABRICATED DOUBLER REPAIR USING 7075T6 .071 PO# 9002012 DIM. 6" BY 3 3/4" IAW B727 SRM 57-30-4 FIG 10. ALODINE AND PRIMED PART AND AREA IAW B727 51Mar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782529Skin · crackedR/WING UPPER SURFACE CRACKED OUT AT NR 11 SPOILER HINGE CUTOUT. REMOVED SPOILER PANEL FOR ACCESS IAW 727 MM 27-61-1. STOPPED DRILLED CRACK IAW 727 SRM 51-10-1. FABBED DOUBLER FROM 7075T6 .071 PO NR 9001737 DIM 5" BY 4" IAW 727SRM 57-30-4 FIG10. DOUBLER TREMar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782524Skin · crackedCRACK IN RT WING ROOT UPPER SKIN LE STA 95. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024T3 .050 DIM. 7.5 INCH BY 7.5 INCH PO NR 9002012, DOUBLER FROM 2024T3 .040 DIM. 3.7 INCH BY .75 INCH PO NR 9001938 IAW 727 SRM 57-30-4 FIG 5. REPAIR PARTS TREATED Mar 11, 2005 · N782DH · Boeing 727227SDR QXEA200500498Skin · corrodedPDX - 623AT HAS FRETTING CORROSION IN COUNTER SINKS. REPAIRED IAW DHC-8 200 RD 8-57-1715.Mar 9, 2005 · N366PH · Dhav DHC8202SDR 05FDEA00439Panel · damagedRT WING PANEL 650JB HAS 4 EA ELONGATED REF N00522. REPAIRED PANEL 650JB IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00438Panel · damagedRT WING PANEL 650KB HAS 4 EA ELONGATED HOLES REF N00521. REPAIRED PANEL IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00437Panel · damagedLT WING PANEL 550HB HAS 2 EA ELONGATED HOLES REF N00520. REPAIRED HOLES IAW EA 6-5710-85051.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00436Panel · damagedRT WING PANEL 650HB HAS 3 EA ELONGATED HOLES REF N00523. REPAIRED PANEL 650HB IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00423Skin · crackedRT WING T/E SKIN HAS A .4 CRACK ON IB CORNER OF CUTOUT FOR PANEL 681 AB REF N00265. REPAIRED SKIN IAW EA 6-5710-86028.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00418Panel · crackedUPON REMOVAL OF LANDING AT RT WING HINGE PANEL ON L/E FOUND PANEL LANDING CRACKED REF N00915. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A572-434548.Mar 8, 2005 · N446FE · Airbus A310222SDR 05FDEA00404Panel · damagedLEFT WING PANEL 550GB HAS ONE ELONGATED HOLE (LANDING). REPAIRED PANEL 550GB LANDING IAW TD/JI/SI/00339/2005 AS PER FEDEX EA 6-5710-86051.Mar 7, 2005 · N446FE · Airbus A310222SDR 05FDEA00403Panel · damagedLEFT WING PANEL 550PB HAS 2 EA ELONGATED HOLES (LANDING). REPAIRED PANEL 550PB LANDING IAW TD/JI/SI/00339/2005 AS PER FEDEX EA 6-5710-86051.Mar 7, 2005 · N446FE · Airbus A310222SDR 2005F00061Skin · crackedDURING MAINTENANCE WORK ON THE RIGHT CENTER WING LOCKER BAY COMPARTMENT FUEL TANK, MAINTENANCE FOUND TWO WING SKIN .5 INCH SURFACE CRACKS AT APPROX WING STATION 60.0 AND FUSELAGE STATION 54.0. SIMILAR DAMAGE WAS FOUND IN THE LEFT WING SAME LOCATION. A DAMAGEMar 7, 2005 · N134J · Cessna 310ASDR QXEA200500478Access Panel · corrodedYYC - LEFT HAND, FUEL PANEL 55100 REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96.Mar 6, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500479Access Panel · corrodedYYC - LEFT HAND, FUEL PANEL 551EB REBATE IS CORRODED. REPAIRED IAW CRJ700 SRM 51-24-11-001-001-A01, REO 670-57-00-010, AND HORIZON AIR EA R-57-96.Mar 6, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500477Access Panel · corrodedYYC - LEFT HAND WING, FUEL PANEL 551BB REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96.Mar 6, 2005 · N605QX · Cndair CL6002C10SDR IXXA0500149SPanel · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AROUND STA XRS 71.000, S-7 TO S-8. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS FROM REPAIR AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER Mar 3, 2005 · N821BX · Doug DC871FSDR IXXA0500122SRepair · improperDURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER AFT PLATING INTERIM REPAIR AROUND STA XF 385.00. MAJOR REPAIR ACCOMPLISHED BY REMOVING EXISTING REPAIR IAW DC8 SRM 51-1-11 PG1, DC8 SRM 51-3-0 PG1. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-5N FIG Mar 3, 2005 · N821BX · Doug DC871FSDR QXEA200500480Access Panel · scratchedYYC - RIGHT HAND LOWER WING LEADING EDGE ACCESS PANEL 622DB FORWARD SECTION, SKIN HAS A SCRATCH AND CHAFE MARK. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01.Mar 3, 2005 · N605QX · Cndair CL6002C10SDR 05FDEA00357Panel · delaminatedRT WING PANEL 641NB HAS AN AREA DELAMINATED. REPAIRED PANEL 641NB IAW EA 8-5710-83988, WINGS - RIGHT WING PANEL 641NB - REPAIR.Mar 3, 2005 · N361 · Doug MD1010FSDR 05FDEA00355Panel · dentedLT WING, LOWER TRAILING EDGE PANEL OVER LEFT MAIN LANDING GEAR IS DENTED AND PUNCTURED. REPAIRED PANEL ARC0269 IAW EA 8-5710-8393, WINGS - LT HAND MLG FITTING TO FUSELAGE AFT UPPER PANEL - REPAIR.Mar 3, 2005 · N361FE · Doug MD1010FSDR 05FDEA00341Panel · delaminatedLEFT WING PANEL 541 NB HAS AREAS OF DELAMINATION. REPAIRED DELAMINATION PANEL 541NB BY FABRICATING AND BONDING NEW SKINS, DOUBLER AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5610-83986, WINGS - LEFT HAND WING PANEL 541NB- REPAIR.Mar 3, 2005 · N361FE · Doug MD1010FSDR 05FDEA00339Skin · corrodedRT WING PANEL INBOARD OF OUTBOARD AILERON ISLAND ABOVE FLAP OUTBOARD TRACK HAS CORROSION AND DELAMINATION. REPAIRED TRAILING EDGE WING PANEL PART NUMBER ARC0616 IAW FEDEX EA 8-5710-83980, WINGS-RIGHTHAND UPPER SK9N, TRAILING EDGE PANEL-REPAIR.Mar 3, 2005 · N361FE · Doug MD1010FSDR QXEA200500472Skin · chafedYYC - LEFT HAND WING LEADING EDGE SKIN HAS CHAFFED MARK FROM LEADING EDGE AT STATION 22. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01 AND SRM 51-12-00-001-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR 05FDEA00329Panel · delaminatedRIGHT WING FIRE BOTTLE ACCESS PANEL TRAILING EDGE DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-83990, WINGS - LEADING EDGE, ACCESS FIREX BOTTLE DOOR-REPAIR.Mar 2, 2005 · N361FE · Doug MD1010FSDR ASAA0580161Skin Panel · elongatedHV- CHECK - LT WING ACCESS PANEL 1392C HAD ELONGATED FASTENER HOLES. REPLACED PANEL. (K)Mar 1, 2005 · N965AS · Doug DC983SDR IXXA0500148SFastener · missingDURING A ROUTINE C CHECK INSPECTION, FOUND WING TO FUSELAGE LOWER PLATING DRAIN HOLE REPAIR MISSING ONE ROW OF FASTENERS AT STA FS 620.000, L-35R TO L-35R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING DOUBLER AND FASTENERS WITHIN REPAIR AREA AND REMOVED DAMAFeb 28, 2005 · N821BX · Doug DC871FSDR IXXA0500145SSkin · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING FORWARD TOP PANEL PLATING CRACK DAMAGE AT STA XRS 144.00 FRONT SPAR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOUBLER AND FILLER PLUG. Feb 25, 2005 · N821BX · Doug DC871FSDR IXXA0500134SPanel · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AT STA XRS 74.869, S-2. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREFeb 24, 2005 · N821BX · Doug DC871FSDR IXXA0500125SRepair · improperDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP AFT LOWER PANEL INTERIM REPARI AT STA XW 34.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION, FABRICATED NEW PLATING SEGMENT, INTEFeb 24, 2005 · N821BX · Doug DC871FSDR IXXA0500124SRepair · improperDURING A ROUTINE C CHECK, INSPECTION FOUND LT WING INBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIRS BETWEEN STA XW 87.000 AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR, AND REMOVED PLATING SEGMENT. PERFORMED NDT INSPECTION AND FABRICAFeb 23, 2005 · N821BX · Doug DC871FSDR CALA0500059Skin · delaminatedINSPECTION FOUND THE LT WING O/B FIXED LEADING EDGE SKIN TOP SURFACE DELAMINATED AT WS 380. REPAIRED IAW SRM 51-40-02, 51-70-07, 51-70-17 AND EA 5731-01010.Feb 23, 2005 · N57111 · Boeing 757224SDR AALA20050169Skin · wornAFW - LEFTHAND LOWER WING OF SKIN HAS TWO AREAS OF WEAR CAUSED BY WING TO BODY PANELS AT WING BUTTLINE 103 AND 105. WEAR IS BEYOND SRM LIMITS. AREA IS 36 BY 2.0 INCHES WITH A DEPTH OF 0.023 INCHES. BLEND THE WORN AREA PER SRM 51 20 01 AND DYE PENETRANT INSPFeb 22, 2005 · N39364 · Boeing 767323SDR EIA2005013Skin · crackedRIGHT WING EXTERIOR, L/E NOSE IS CRACKED AT FASTENER HOLE 10 INCHES LONG AT WS 200.0. HOT BONDED METAL TO METAL REPAIR MADE TO RT WING L/E NOSE AT WS 200.0 PER ECRA 471-57-241-2 AND 747 SRM 51-40-06 PG 23.Feb 21, 2005 · N471EV · Boeing 747273CSDR MASA200500141Skin · erodedIN C-CHECK LEADING EDGE II ON RT WING IS ERODED OUT OF LIMITS. DAMAGE HAS BEEN BLENDED IAW SRM 57-40-00, REMAINING MATERIAL IS ACCEPTABLE IAW EMBRAER ENGINEERING DOCUMENT IC2005-145/0934.Feb 21, 2005 · N851MJ · Emb EMB145LRSDR UPS05844064Skin · corrodedINSPECTION TYPE: C2 LT L/E AT APPROX 660 HAS CORROSION AND FLAKING. REPAIRED LT L/E WING UPPER SKIN REPAIR AT XFS 710-824 IAW UPS EO DC8-57-20127, SAA SK 811-933.Feb 15, 2005 · N811UP · Doug DC873FSDR 05FDEA00290Skin · damagedELONGATED HOLES IN THE RT LWR WING SKIN AT 1 FASTENER HOLE FOR MANHOLE COVER 650KB.Feb 15, 2005 · N431FE · Airbus A310203SDR USAA050290Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, RT WING LEADING EDGE WBL 204 AT LOWER WING SURFACE. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER T/R 57-41-02. (M)Feb 14, 2005 · N438US · Boeing 7374B7SDR IXXA0500128SRepair · damagedDURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD FLAP AFT UPPER PLATING INTERIM REPAIRS AND DENT DAMAGE BETWEEN STA XW 2.00 CANT AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREFeb 13, 2005 · N821BX · Doug DC871FSDR DHL2005781510Skin · gougedDURING A "C" CHECK, RT WING TIP LOWER INBD EDGE IS GOUGED BY NR 8 SLAT AND WEB IS DENTED SLAT STA 434.5. REMOVED R/WING TIP AND WEB SLAT STA 434.5 IAW B727 SRM 51-30-2. REMOVED AREA TO ORIGINAL CONTOUR IAW B727SRM 51-40-1. ACCOMPLISHED NOT HFEC AT REMOVED Feb 13, 2005 · N781DH · Boeing 727227SDR DHL2005751500Skin · corrodedLEFT WING L/E STA 644.5 HAS CORROSION. CUT OUT CORROSION DAMAGE IN LT WING L/E AT STA 644.5. FABRICATED -1 FILLER USING .040 2024T3 PO 0442771, -2 DOUBLER USING .050 2024T3 PO 0440785. DRILLED DEBURRED, ALODINED, PRIMED AND INSTALLED DOUBLER & FILLER IAW B7Feb 13, 2005 · N751DH · Boeing 727264SDR 05FDEA00280Skin Panel · corrodedOVERWING BOX, TANK TOP, HAS CORROSION AT BODY STATION 840 RIGHT BUTT LINE 12.0. REPAIRED OVERWING BOX FUEL TANK, STATION 840 AT RIGHT BUTT LINE 12.0 IAW FEDEX EA 7-5730-83992, WINGS-UPPER SKIN PANEL, CENTER TANK CORROSION-REPAIR.Feb 12, 2005 · N258FE · Boeing 727233SDR DHL2005781523Skin · gougedDURING A "C" CHECK, LT WING UPPER SURFACE GOUGED 1 INCH AFT OF NR 2 SLAT O/B SLAT HOOK RETAINER. REMOVED PAINT AT AFFECTED AREA IAW B727 B772 51-20-1. INSPECTED AREA USING C/3 ULTRSONIC THICKNESS GOUGE ORIGINAL THICKNESS OF 0.040 MATERIAL LOSS OF 0.0102 INCHFeb 11, 2005 · N781DH · Boeing 727227SDR QXEA200500283Access Panel · chafedYYC - RIGHTHAND WING AILERON ACCESS PANEL HAS CHAFE MARKS FROM SEAL. REPAIRED IAW CJR700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01.Feb 11, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500261Skin · nickedYYC - LT WING LOWER SKIN INBOARD HAS A SHARP NICK AT STATION 25. REPAIRED IAW CRJ 700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01.Feb 11, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500260Fastener · looseYYC - LEFTHAND WING UPPER SKIN SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION 231.23 AND 172. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND SRM 51-42-06-001-001-A01.Feb 10, 2005 · N609QX · Cndair CL6002C10SDR UPS05443922Skin · crackedINSPECTION TYPE:C, RHW REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND CRACKED AT HOLE NR 7 AT SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123SDR UPS05443921Skin · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND HOLE NR 12 CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123SDR UPS05443920Skin · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123SDR ASOA05118Skin · crackedDURING A C-CHECK IN MCN, THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS IAW ASA EO 600-57-0134A. (M)Feb 9, 2005 · N828AS · Cndair CL6002B19
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