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 07FDEA01860Skin · crackedLEFT WING TELESCOPIC DUCT CUT-OUT FOUND WITH 0.3125 INCH CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I , FIGURE 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UPS07M50207Skin · damagedINSPECTION TYPE:C LEFT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO BE REPLACED. NEW SKIN FAB PER BOEING DWG ARC2736 R.B. NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V2 R38. NEW SKIN PROTECTED PER SRM 51-21-01 V2 R38. NEW SKIN INSTALLED PER SRM 51-31-01 VSDR UPS07M50201Skin · damagedINSPECTION TYPE:C RIGHT WING - I/B FLAP LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01 V2R38. NEW SKIN FAB USING MATL 2024T3-0. 040" TK PER DWGARB2444. NEW SKIN HOLES DRILLED & REPROTECTED PER SRM 51-21-01V2R38. OK TO INSTALL NESDR UPS07M50200Skin · damagedINSPECTION TYPE:C LEFT WING - I/B FLAP, LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01V2R38. NEW SKIN FAB PER SRM 51-31-01V2R3 8. NEW SKIN HOLE P/UP PER 51-31-01V2R38. NEW SKIN PROTECTED PER SRM 51- 31-01V2R38. NEW SKIN PAINTEDSDR 2007UALA01546Skin · gougedLEFT WING LWR SKIN FASTENER HOLE -B- AT SIDE LINK FITTING ATTACH AREA HAS 3 EA DEEP GOUGES. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN, REPLACED PRODUCTION SLICE AND REPAIRED HOLE PER UA ENGINEERING SPECIFICATIONS.SDR 07FDEA01823Skin · corrodedRIGHT WING TRAILING EDGE UPPER SURFACE CLOSE OUT PANEL IS BULGED AT SEVERAL LOCATIONS BETWEEN NR 2 AND NR 5 SPOILER AREA. REMOVED CORROSION IAW DC/MD10 SRM 51-21-01 VOLII AND FEDEX EA 8-5710-109151 WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733-REPAIRSDR A6WA200740257Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 9 FOR PANEL 550AB HAS FRETTING/ CORROSION DAMAGE 1 INCH AREAS AT IB END NOT IN CRITICAL AREA. (K) [07-17-07] MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 9 PANEL 550AB IAW BOMBARDIER REO 601R-57-21-030 REV A. (SDR A6WA200740256Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 FOR PANEL 540BR HAS FRETTING/ CORROSION DAMAGE AREA ABOUT 2 INCHES LONG AT FWD/ OB QUADRANT, NO IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 1 PANEL 540BB IAW BOMBARDIER REO 601R-57-21-030SDR A6WA200740255Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 3 FOR PANEL 510BR HAS FRETTING/ CORROSION DAMAGE AT IB END 1 INCH LONG NOT IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 3 PANEL 510BB IAW BOMBARDIER REO 601R-57-21-030 REV A. (K)SDR A6WA200740254Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 2 FOR PANEL 510AB HAS FRETTING/ CORROSION DAMAGE AT IB END, ALL ALONG FWD SIDE AND OB END, IN AND OUT OF CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 PANEL 510AB IAW BOMBARDER REO 601R-57-21-SDR 07FDEA01820Skin · corrodedRIGHT WING T/EDGE UPPER SURFACE CLOSE-OUT PANEL IS BULGED AT SEVERAL LOCATIONS, BETWEEN NR 2 AND NR 5 SPOILER AREA.SDR WRLA2007068Panel · damagedFLT 8129/LEJ/ATL 05/15/2007. ON POST FLIGHT INSPECTION WORLD AIRWAYS MAINTENANCE FOUND LEFT WING REFUEL PANEL DAMAGED AND PINCHED BY NR 4 LEADING EDGE SLAT. REMOVED LEFT WING FUELING PANEL DOOR, TRIMMED OUT DAMAGE, INSPECTED PER DELTA AIR LINES ERA 461879-14SDR PAI52007S4573Skin · crackedWHILE PERFORMING PHASE 2 INSPECTION NOTED AN 8 INCH LONG SPANWISE CRACK ON LOWER SURFACE OF WING LEADING EDGE SKIN P/N 000-110133-33. ALSO FOUND CHANNEL P/N 101-910119-147 INSIDE THE ABOVE MENTIONED SKIN BROKEN IN TWO. REPLACED BOTH PARTS WITH NEW PARTS FROMSDR 07FDEA01773Skin · crackedLT WING LOWER EXT SKIN L/E SLAT TRACK NR 10 FOUND CRACK .50" LONG CUT OUT CRACK AREA AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM 57-10-00 FIG 68 VOL 1.SDR UPS07449798Panel · crackedLEFT WING LOWER T/E PANEL HAS 5 FT CRACK. A/C IS OOS. [SUP 05-21-07] REMOVED PANEL FROM A/C. SENT TO SHEETMETAL SHOP. PANEL REINSTALLED IAW EO B747-5720-6416E.SDR 2007UALA01481Skin · corrodedRIGHT UPPER WING SKIN HAS NUMEROUS AREAS OF EXFOLIATION CORROSION FROM FRONT SPAR TO AFT SPAR C-T FUSELAGE. [SUP 06-06-07] RT WING UPPER SURFACE AT FILLET FAIRING MATING SURFACES BETWEEN FRONT SPAR TO REAR SPAR HAS NUMEROUS AREAS BLENDED EXCEEDING SRM. WORK SDR 2007UALA01480Skin · corrodedLEFT UPPER WING SKIN CORRODED AT MID SPAR C-T FUSELAGE. [SUP 06-06-07] PERFORMED DETAILED VISUAL INSPECTION OF THE LT FWD TRUNNION FUSE PINS FOR LOOSE FUSE PINS AND CORROSION ON ADJACENT STRUCTURE. WORK ACCOMPLISHED PER UA ENGINEERING EVALUATION AND RECOMMESDR QXEA200700852Skin · gougedC4 OKC - PANEL 671AB GOUGED ON OUTER SURFACE. REPAIRED IAW SRM 57-31-01, 57-32-32.SDR 07FDEA01724Skin · crackedMD 10-10 ACF MODIFICATION AND REPAIR ASSESTMENT RT WING LEADING EDGE STA XORS 506 LOWER SIDE CLOSE TO PANEL FUEL PANEL, SKIN WITH CRACK OF ABOUT 2 INCH REMOVED ACCESS DOOR, REPAIRED FIXED L.E IAW SRM 57-10-00 FIG 68 SHEETS 2 AND 3. INSTALLED ACCESS DOOR. SDR CA070517007Winglet · separated(CAN) IT WAS FOUND THAT THE SHEET METAL SCREWS HOLDING THE TIP ON THE WING HAD ALL COME LOOSE. THE WING TIP THEN VIBRATED FOR A PERIOD OF TIME ,ELONGATING THE SCREW HOLES IN THE WING UNTIL ALL OF THE SCREWS FELL OUT AND THE WING TIP DEPARTED THE WING IN FLIGHTSDR QXEA200700858Panel · chafedC4 OKC - PANEL 584ET CHAFED AT LEADING EDGE. REPAIRED IAW SRM 53-00-01, 51-12-00, AND 53-00-01.SDR MWEA070100Skin Panel · looseREPORTED FUEL SEEPAGE FROM THE LEFT WING. RESECURED INBOARD FUEL TANK PANEL.SDR 07FDEA01692Skin · crackedRIGHT WING, LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER FOUND 5/8 INCH CRACK AT XOS 607. [SUP 05-22-07] REPAIR CARRIED OUT AT RIGHT WING - LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER, XOS 607 AS PER SRM 57-10-00 FIGURE 21 VOSDR 07FDEA01670Skin · crackedRIGHT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH) REVEALED IN SIX (6) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS DOOR CUTOUT LOWER SKIN (BETWEEN XOR=683.4 AND XOR=713.6). [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109877, REPAIR CLASSIFIED ASDR 07FDEA01669Skin · crackedLEFT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH ) REVEALED IN FIVE (5) EACH FASTENER HOLES TOWARDS THE EDGE OF ACCESS CUTOUT LOWER SKIN ACCESS DOOR (BETWEEN XOR=683.4 AND XOR=713.6). REPAIRED AS PER FEDEX EA 1-5710-109878, REPAIR CLASSIFIED AS MAJOR SDR UIEA200700213Panel · dentedLT WING LEADING EDGE HAS A 6.5 INCH LONG BY 3.0 INCH WIDE DENT AT ILES 207.0. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 1 THRU 5 AND B747-200 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A357.SDR UIEA200700214Panel · delaminatedRT WING UPPER L/E PANEL AT WS 440.0 HAS AN AREA OF 24.0 INCH LONG BY 12.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 1 THRU 5 AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A358.SDR 07FDEA01649Skin · crackedL-WING TE BOTTOM SKIN AT PANEL 581AB CUTOUT HAS CRACK ON LOWER SKIN RIB 11 WITH APPROX 0.75 IN LONG REF N00166 STOP DRILLED CRACK, DRILLED UP DOUBLER AND COLDWORKED AND INSTALLED IAW EA 6-5710-107726 AND SB A310-57-2066.SDR COMA0760341Skin · chafedRIGHT WING FUEL PANEL 640BB MATING MATERIAL SURFACE ON WING IS CHAFED. REWORKED AREA IAW REO 601R-57-21-030 REV F.SDR COMA0760340Skin · chafedLEFT WING FUEL PANEL 540BB MATING SURFACE ON WING IS CHAFED. REWORKED AREA IAW REO 601R-57-21-030.SDR UPS07849748Doubler · crackedINSPECTION TYPE:C3 CRACK ON INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE UPPER SURFACE I/B EDGE OF SLOT DOOR. REMOVED INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT WING LEADING EDGESDR 07FDEA01630Fairing · crackedA 200 MM CRACK IN INNER FACE NEAR PIVOT POINT AT NR 4 LT MOVEABLE FAIRING BONDING REPAIR PERFORMED IAW EA 6-5720-99195 AND RAS/FOK/069/2006 ISS A.SDR UPS07M50157Doubler · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 550 APPROX FOUND UPPER SKIN DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RIGHT WING L/E COMPT AT STA XORS 550 APPROX, UPPER SKIN DOUBLER AREA TRIMMED OUT AS PER SRM 57-10-00 V.I FIG 27 IAW EN 1294-07. HFSDR 2007UALA01288Skin · crackedRT WING L/E AFT OF NR 9 SLAT CRACKED OUT FROM RESTORATION SEAL CUTOUTS. [SUP 05-18-07] RT WING L-E AFT OF NR 9 SLAT CRACKED OUT FROM RESTORATION SEAL CUTOUTS. REPAIRED PER OV WRITE-UP W1682T AND R&R R41952.SDR A6WA200740214Skin · corrodedRT WING PLANK AT ACCESS HOLE 640DB HAS CORROSION ON LOWER IB SIDE MEASURES APPROX .5 X .25 X .002 IN NON-CRITICAL AREA. REPAIRS ACCOMPLISHED IAW EO E06/021/457. (K)SDR SWIA200718202Skin · damagedRIGHT INBOARD WING LEADING EDGE IS DENTED FROM A BIRD STRIKE. REMOVED AND REPLACED LEADING EDGE SKIN AND THREE DAMAGED RIBS IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-13.SDR 07FDEA01567Skin · corrodedRT WING T/E LWR SKIN FOUND SEVERE CORROSION ON BEAVER TAIL AT STA XORS 231. REPAIR IAW EA FEDEX 8-5710-108070.SDR F3LA200700110Skin · gougedDURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING INBD UNDER WING AREA. SEVERAL GOUGES AND SCRATCHES WERE FOUND BETWEEN RIBS 4 AND 6 AND STRINGERS 2 THRU 7.SDR DHL2007788505Skin · crackedRIGHT WING FIXED L/E NR 5 SLAT, INBD TRACK CUTOUT FOR SLAT TRACK SEAL, AFT INBD RADIUS, .5"-.75" LONG CRACK W/S 383.5. CUTOUT DAMAGED AREA 7" BY 2.25" IAW B727 SRM 57-30-4. FABRICATED NEW DOUBLER 7" BY 5.375 BY .040, 301 1/2 HARD AND FILLER 7" BY 2.25 BY .04SDR 07FDEA01548Skin · corrodedRIGHT WING UPPER SURFACE HAS CORROSION JUST O/B OF TRUNNION DOUBLER. [SUP 05-21-07] REMOVED COROSION FROM WING SKIN,ORIG THICKNESS .495,AMOUNT REMAINING.476,MATERIAL LOSS .019 FOUND TO BE WITHIN LIMITS IAW DC/MD SRM 57-10-00 FIG.61 VOL I,51-20-00 FIG2 VOL SDR 07FDEA01540Skin · crackedLEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-11-07] CRACK AT LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57- 10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01539Skin · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-09-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01537Skin · chafedELONGATED HOLES ON PYLON SUPPORT BRACKET AND WING BOTTOM SKIN, RIB 8-9 RT. REPAIR PERFORMED BY OVERSIZING AND INSTALLING BUSHES IAW DRW R572-49184, APPROVED BY EA 6-5720-99169 AND RAS/BAE/1002502/2006 ISSUE "A".SDR IXXA07SMN146SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP CRACKED ON UPPER PART EXTERNAL COATING AT STATION XW 104.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANTSDR IXXA07SMN157SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAD A NON STANDARD REPAIR AT STATION XFS 426.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER NDT TEST. SDR DXTA200702126Access Panel · misinstalledIN FLIGHT ABOVE 200 KTS THERE IS A RUMBLING VIBRATION THAT VIBRATES THE WHOLE AIRPLANE. IT CHANGES PITCH OR SEVERITY WITH INCREASE IN SPEED, 250 KTS IS THE SPEED THAT IT IS MOST PRONOUNCED. FOUND ACCESS PANEL ON LOWER LT STUB WING NR 313AL TO BE OVERLAPPING SDR 07FDEA01531Skin · damagedELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN, LT/RT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW EA 6-5720-66169 AND RAS/BAE/1002502/2006.SDR ASAA0741591Skin · crackedRIGHT WING O/B LEADING EDGE AT WS 290 FIXED LEADING EDGE SKIN CRACKED. FIXED LEADING EDGE SKIN REPAIRED IAW SRM 51-70-17.SDR CALA0700185Skin · crackedRT WING LEADING EDGE SKIN CRACKED AT RIB STA 471, BEHIND NR 8 SLAT AT I/B DRIVE TRACK. REPAIRED IAW ECRA 5731-1303 AND SRM 51-70-07.SDR AWXA200700634Skin · crackedMCN - C-11 CHECK - RIGHT WING NR 9 SLAT COVE PANEL CRACKED, WS 639.1. REPLACED RIGHT WING NR 9 SLAT COVE PANEL, WS 639.1 IAW B757-200 SRM 51-40-02.
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