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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 08FDEA01835Panel · corrodedRIGHT WING FUEL PANEL ASSY NR 650 CB CLAMP RING HAS AREAS OF FRETTING. BLENDED AREA SMOOTH IAW SRM 51-73-10. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-16. REMOVED AND REPLACED THE CLAMP RING.SDR 08FDEA01834Panel · corrodedRIGHT WING FUEL PANEL ASSY NR 650 FB CLAMP RING HAS AREAS OF FRETTING. BLENDED AREA SMOOTH IAW 57-73-10. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-16. REMOVED OLE CLAMP RING AND REPLACED WITH A NEW RING.SDR 08FDEA01833Skin · damagedEXISTING EXTERNAL REPAIR DOUBLER AT FIXED L/E STA XIS 150 REMOVE REPAIR AND ACCOMPLISH A NEW IAW SRM 57-10-00 FIG 40 BECAUSE REPAIR DETECTED WAS FOUND WITH A SIGNIFICANT LOSS OF MATERIAL DUE TO A LIP CONTACT.SDR NWAA082185514Panel · inflt separationCLIMBING THROUGH FL 230 PANEL 651, ON THE UPPER SURFACE OF THE RIGHT WING ABOVE THE RIGHT LANDING GEAR RETRACT CYLINDER, DEPARTED FROM THE AIRCRAFT. WHEN THE PANEL DEPARTED THE AIRCRAFT IT TORE TWO HYDRAULIC LINES FOR THE RETRACT CYLINDER AND DRAINED THE LEFTSDR UIEA200800204Access Door · corrodedNR 1 MAIN TANK ACCESS DOOR 552CB CUT OUT LOWER SURFACE CORROSION EVIDENT. BLENDED OUT CORROSION IAW SRM 57-30-03 AND REPROTECTED AREA IAW SRM 51-10-02.SDR 08FDEA01808Skin · cracked06 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-122445. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100SDR 08FDEA01807Skin · cracked15 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LHW LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 690 AND STA XORS = 700. REPAIR CARRIED AS PER EA 1-5710-122444 REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100SDR UIEA200800181Skin Panel · delaminatedRT WING UPPER FIXED T/E PANEL HAS LOOSE AND WORKING FASTENERS, PANEL IS DELAMINATED. PANEL LOCATED INBOARD OF INBOARD AILERON, AT WBL STA 445.0, DELAMINATION AFT EDGE OF PANEL. AREA OF DELAMINATION IS 9.0 INCH LONG BY 1.5 INCH WIDE. PERMANENT REPAIR ACCOMPLSDR UIEA200800180Skin Panel · delaminatedRT WING UPPER FIXED L/E PANEL DELAMINATED, 6.0 FEET OUTBOARD OF NR 3 ENGINE, 12 INCHES FROM AFT EDGE OF PANEL AT ILES STA 772.5. AREA OF DELAMINATION IS 14.0 INCH LONG BY 3.0 INCH WIDE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEESDR UIEA200800179Skin Panel · crackedRT WING UPPER FIXED TRAILING EDGE PANEL HAS COMPOSITE CRACK, 3.5 INCHES FROM FORWARD EDGE OF PANEL AT WBL STA 515. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR ESDR UIEA200800178Skin Panel · delaminatedLT WING UPPER FIXED L/E PANEL DELAMINATED, INBOARD OF NR 2 ENGINE, 8.0 INCHES FROM AFT EDGE OF PANEL AT ILES STA 545.56. AREA OF DELAMINATION IS 2.0 BY 2.0 INCHES. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250SDR UIEA200800177Skin Panel · crackedLT WING UPPER FIXED LEADING EDGE PANEL CRACKED AND DELAMINATED, ILES 833.00, 20 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR SDR 08FDEA01804Skin · corrodedLEFT WING TIP INBD SIDE SKIN HAS CORROSION AROUND THE STATIC WICK BASE. REMOVED STATIC WICK BASE AND REMOVED THE CORROSION. ORIGINAL THICKNESS 0.056 IAW AA300-600 SRM 57-30-11. REMOVED MATERIAL 0.014. REMAINING THICKNESS 0.042 AND IS OUT OF LIMITS IAW A300SDR 08FDEA01798Skin · wornRT WING L/E EXT SURFACE FOUND WEAR ON SKIN. REPAIRED L/E WITH DOUBLER IAW SRM 57-10-00 FIG 40 VOL I.SDR 08FDEA01797Skin · looseRT WING UPPER SURFACE FOUND 8 EA RIVETS LOOSE ON UPPER SKIN OF OUTBD AILERON. REPAIRED AREA IAW SRM 57-10-00 FIG 85 VOL I.SDR 08FDEA01796Skin · crackedRT WING EXT L/E CRACK ON SKIN (NEAR OLD REPAIR). REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 68 SHT 2.SDR 08FDEA01795Skin · dentedRIGHT WING FIXED LEADING EDGE SKIN IS DENTED IN 4 PLACES AT STA XFS 627 TO XFS 653. DEPTH OF THE DENTS ARE0.045 TO 0.120. DENTS ARE OUT OF LIMITS IAW SRM 57-00-01 VOL I FIG 1B. FABRICATED REPAIR IAW SRM 52-00-01 VOL I FIG 4. ALODINED IAW SRM 51-21-01 SDR UPS08M52323Skin · crackedINSPECTION TYPE:2C RIGHT WING LEADING EDGE ACCESS PNL LANDING CRACKED XOS 550. FABRICATED AND INSTALLED STIFFENER IAW DWG ARB 2918 AND MD-11 SRM 51-31-01.SDR UG8A08P050601Skin · corrodedMISSING PAINT WITH MINOR CORROSION ON MIDDLE RT WING, UNDER THE SLAT, AT THE WING LIFTING POINT. CORROSION IS LOCATED ON WING PLANK AT LIFT POINT IN MACHINED CUTOUT. CUTOUT IS FILLED WITH SEALANT. CORROSION LOCATED UNDER SEALANT ON WING PLANK. REMOVED CORRSDR 08FDEA01760Panel · chafedRIGHT WING T/E PANEL NR 645 BB L/E IS CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. RECEIVED NEW PART. DRILLED, DEBURRED AND COUNTERSUNK IN REF TO SRM 51-31-01; VOL II.SDR 08FDEA01754Skin · damagedRIGHT SKIN LEADING EDGE SKIN LOWER SURFACE IS KNIFE EDGED AT THE CUTOUT FOR THE ANTI-ICE "T" DUCT. BLENDED DAMAGED AREA. ORIGINAL MATERIAL 0.063 IAW DWG ARB1284, REV "AC". MATERIAL LOSS 0.045. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATEDSDR USAA920081120Skin Panel · corrodedMCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE LEFT WING LOWER SURFACE INNER SPAR SKIN, WBL 583, STRINGER 6. REPAIRED THE LEFT WING LOWER SURFACE INNER SPAR SKIN, WBL 583, STRINGER 6 IAW USAIRWAYS EA 130024.SDR ASAA0892956Skin · damagedBIRD STRIKE TO LT WING JUST INBOARD OF NR 1 ENGINE. REPAIRED PER SRM 57 41 01 REPAIR NR 5.SDR ASAA0892955Skin · damagedBIRD STRIKE TO RT WING LEADING EDGE ROOT. REMOVED & REPLACED RT LEADING EDGE SKIN.SDR 2008UALA02604Panel · missingTEN INCH SQUARE SECTION OF PANEL MISSING FROM UNDER LT WING ABOVE MAIN GEAR. ACP TEMP REPAIR PER EVA 71522 .100 FILLER AND .100 DOUBLER. ACCOMPLISH INSPECTION OR RECHECK AS REQUIRED IN CF0477. AC OK FOR SERVICE.SDR 08FDEA01739Skin · crackedFOUND ON LT ASA BOOSTER DOOR A CRACK IN HOLE FOR RUBBER STRIP ATTACHMENT. REPAIR PERFORMED BY CUT OUT AND INSTALLING A FILLER AND DOUBLER IAW, RAS/BAE/1006711/2008 ISS A, APPROVED BY EA 6-5751-117144.SDR 08FDEA01953Access Door · chafedRIGHT WING PANEL HAS NUMEROUS CHAFED SPOTS ON PANEL 675 CB. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-51-12, PG 101. REMOVED PANEL IAW A300-600 SRM 51-40-21, PARA 5. REMOVED FASTENERS FROM PANEL IAW EA 6-5750-118484 AND A300-600 SRM 5SDR 08FDEA01731Skin · crackedRIGHT WING FIXED LEADING EDGE CAVITY UPPER SKIN DOUBLER IS CRACKED AT STA XFS 669, OUTBD OF THE NR 10 SLAT TRACK. FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00; FIG 71; VOL I. PRIMED REPAIR DOUBLER IAW SRM 51-21-01; VOL II AND 51-35-01; VOL II.SDR 08FDEA01729Access Panel · chafedLEFT WING LEADING EDGE FIRE BOTTLE COMPARTMENT ACCESS PANEL IS CHAFING AROUND THE CONTACT SURFACE. REPAIRED PANEL BY BLENDING CHAFED AREA & CHECKING LIMITS IAW SRM 57-00- 01; VOL I. BLENDED AREAS FOUND TO BE OUT OF LIMITS. REMOVED PANEL IAW SRM 51-31-01;SDR 08FDEA01782Panel · damagedLEFT WING T/E PANEL 590 AB AFT CORNER IS BROKEN, BLENDED CORNER ON THE LEFT T/E PANEL, SEALED EDGE AND PAINTED IAW A300-600 SRM 51-42-20.SDR 08FDEA01696Panel · delaminatedRIGHT WING L/E LWR PANEL 6402 HAS 2 INCH BY 6 INCH AREA OF DISBOND CORE FROM INNER AND OUTER SURFACES. REPAIRED PANEL 6402 REF SRM 51-40-9 PARAGRAPHS 3D, 4B, 4E, 4F AND AMM 51-20-051-7, 51-20-151-7 TAP TEST GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01694Skin · wornFOUND ELONGATED HOLES ON RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS/BAE/1006364/2008 ISS A AND EA 6-2900-114925.SDR 08FDEA01693Skin · wornFOUND ELONGATED HOLES ON LT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS /BAE/1006364/2008 ISS A AND EA 6-2900-114925.SDR 08FDEA01692Skin · wornFOUND ELONGATED HOLES ON LT/RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-29-6057, APPROVED BY EA 6-2900-114925.SDR 08FDEA01616Skin · cracked14 FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113138, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.SDR 08FDEA01615Skin · cracked16 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113137, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.SDR 08FDEA01619Skin · damagedRIGHT WING UPPER I/B L/E PANEL 618AT INNER SKIN IS DAMAGED. REMOVED DAMAGED SECTION INNER SKIN IAW SRM 57-10-00. FABRICATED FILLERS 2 EA AND A REPAIR DOUBLER IN REF TO SRM 57-10-00. PRIMED REPAIR PARTS IN REF TO SRM 51-21-01. INSTALLED FILLERS AND REPAIR COUBSDR 08FDEA01618Panel · dentedRIGHT WING LOWER I/B T/E PANEL 641EB HAS SEVERAL DENTS. REPAIRED ( 3 EA ) DAMAGED AREAS BY FABRICATING & BONDING A CORES; FILLERS & DOUBLERS IAW SRM 51-71-00 VOL II.SDR 08FDEA01567Panel · wornRIGHT WING LEADING EDGE PANEL NR 612 BB INNER SKIN LAMINATE IS WORN/TORN AROUND THE FASTENERS. APPLIED ANTI-ERROSION TAPE 7 PRIMED IAW A300-600 SRM 51-75-10; PG 213.SDR 08FDEA01607Skin Panel · damagedLEFT WING LOWER INBD L/E PANEL 517 AB HAS DAMAGED ATTACHED HOLES. FABRICATED DOUBLER & FILLER IAW SRM 57-00-01 VOL I. ALODINED; PRIMED AND TOPCOAT PAINTED SRM REPAIR IAW SRM 51-21-01 VOL II. INSTALLED SRM REPAIR DOUBLER & FILLER IAW 57-31-01 VOL II.SDR 08FDEA01576Panel · erodedPANEL 612 CB MATING SURFACES ARE ERODED. REPLACED ERRODED FOIL ON PANEL 612 CB MATING SURFACE IAW SRM 57-41-12.SDR 08FDEA01574Panel · crackedPANEL 612 CB LEADING EDGE IS CRACKED AND ERODED. REPAIRED CRACK & ERROSION ON PANEL 612 CB L/E WITH WET LAY UP IAW SRM 57-41-12.SDR 08FDEA01566Panel · wornRIGHT WING LEADING EDGE PANEL NR 612 DB HAS LANDING AREA INTERIOR LAMINATE WORN/TORN. REPAIRED THE DAMAGED AREA BY APPLYING ALUMINUM FOIL IAW SRM 57-41-12. REMOVED & REATTACHED THE PANEL RESTRAINING CORDS REF AMM 57-41-41-4. PREPPED THE BONDING SURFACE FOR THSDR 08FDEA01565Panel · wornRIGHT WING LEADING EDGE PANEL NR 612 GB HAS LANDING AREA SKIN LAMINATE WORN/TORN. REPAIRED DAMAGED AREA IAW SRM 57-41-12; FIG 208. REMOVED & RE-ATTACHED THE PANEL RESTRAINT CORDS REF AMM 57-41-41-4; PG 1.PREPARED THE BONDING SURFACE FOR THE FOIL APPLICASDR 08FDEA01564Panel · erodedRIGHT WING LEADING EDGE PANEL NR 623 HB IS ERODED AT THE FWD EDGE. REPAIRED ERRODED AREAS BY APPLYING FIBREGLASS OVERLAYS IAW SRM 57-41-12 & 51-77-12. REAPPLIED FOIL IAW SRM 57-41-12; FIG 208. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. RESTORED PAINSDR HALA0800542Skin · dentedUNDER SIDE OF WING PANEL P/N 5912161-4512 ABOVE NR 3 MLG TIRE AREA HAS DENT APPROX 1.5 INCH DIAMETER AND .25 DEEP. OK TO CONTINUE PER GMM43.1. OK TO CONTINUE PER HAL M105 FILE NR 475127 INSPECTION FIRST FLIGHT EACH DAY, TAP TEST MARKED BOUNDARY OF DENT ENSURSDR QXEA200800447Panel · chafedRFD C4 CHECK PANEL 584HT HAS CHAFFING. BLENDED PANEL 584HT FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .004 MATERIAL FROM PANEL 584HT IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584HT IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WITH 8003/B707 PAINT ISDR QXEA200800446Panel · chafedRFD C4 CHECK PANEL 584ET HAS CHAFFING. BLENDED PANEL 584ET FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .005 MATERIAL FROM PANEL 584ET IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584ET IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WITH 8003/B707 IAW CRJSDR UPS08852282Skin · corrodedINSPECTION TYPE:C3 LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN GOUGED AND CORRODED AT CORNER SCREW HOLES. REPAIRED LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN IAW EO DC8-5720- -A AND SRM 57-03-03-0 FIG 005.SDR UPS08852223Skin · corrodedINSPECTION TYPE:C3 LEFT WING CENTER L/E 4 EA SCREWS PULLING AND HAVE CORROSION ON SKIN INBOARD LOWER CORNER OF SLOT VANE. REPAIRED LEFT WING CENTER L/E INBOARD LOWER CORNER OF SLOT VANE IAW EO DC8- 5720-7767-A.
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