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 WRLA2007005Skin · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND CORROSION UNDER LEFT WING T/E FIXED PANEL UPPER SURFACE NEAR NR 5 SPOILER OUTBOARD SIDE. REPAIR THE DAMGED AREA PER EGAT E1 NR W2007A57B-066 REV.OO & APPROVED DOCUMENT BOEING MESSAGE NR 1-277655111-2. 2.CONDITIONSDR 2007FA0000063Skin · mismanufacturedDURING AN RECEIVING INSPECTION OF NEW RT OB LEADING EDGE SKIN, IT WAS FOUND TO HAVE BEEN DRILLED UP INCORRECTLY SINCE NONE OF THE NOSE RIBS WOULD LINE UP AND THE SET UP WOULD HAVE LT INSUFFICIENT EDGE DISTANCE ON THE LOWER MAIN WING SPAR RIVET LINE. THIS IS ZSDR UPS07M49397Skin · chafedINSPECTION TYPE:C LEFT WING UNDERSIDE FIXED L/E SKIN ABOVE ENG PYLON I/B EDGE SKIN FOUND CHAFF MARK. LEFT WING UNDERSIDE FIXED L/E SKIN ABOVE ENG PYLON I/B EDGE SKIN CHAFF MARK REMOVED AND REPROTECTED PER SRM 51-21-01 V-II R38. FOUND EXCEED LIMIT PER SRM 57-SDR 07FDEA00055Doubler · corrodedRT WING UPPER SURFACE DOUBLER AT XORS 264 FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-105593, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00054Skin · corrodedRT WING UPPER SURFACE TRAILING EDGE MOST INBD FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-107764, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UPS07848942Skin · crackedINSPECTION TYPE:C3 LARGE DENT ON NOSE OF RT CTR L/E. CRACKED SKIN, BROKEN RIVETS XFS 392. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED CONICAL WASHERS, FILLER AND DOUBLER IAW SRM 57-02-01-0 FIG 0024, 51-1-21 AND 51-1-20D.SDR UPS07849109Skin · crackedINSPECTION TYPE:C3 LEFT UPPER WING SKIN POSSIBLE CRACKED AT XCW69 AFT SPAR VERY I/B SIDE. CUT OUT DAMAGE, FABRICATED 2 EA DOUBLERS, 1 EA FILLER AND 1 EA ANGLE AND INSTALLED IAW SRM 57-02-01-0 FIG 020 AND 51-1-21.SDR TRAX200700024Panel · crackedRIGHT WING PLANK CRACKED AT WS 148.19 APPROX (REF AD2002-03-14REP). REPAIRED IAW ALL SRMS.SDR 07FDEA00020Skin · corrodedRT WING UPPER SKIN LOWER SURFACE FOUND CORROSION AT XORS= 720 TO XORS= 726. COMPLIED WITH FEDEX E.A 1-5720-106578, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UPS07449153Panel · delaminatedINSPECTION TYPE:C LEFT WING INBOARD TRAILING EDGE MID FLAP LWR OUTBOARD AFT PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.SDR 07FDEA00017Skin · corrodedRIGHT WING UPPER SURFACE CORROSION AT XORS 1011. COMPLIED WITH FEDEX E.A.# 1-5710-105601, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR CA070115014Skin · cracked(CAN) DURING ANNUAL INSPECTION SEVERAL CRACKS WERE DETECTED AT THE RIVET HOLES WHERE THE FLAP BAY SKIN (PN 20438-2) ATTACH TO THE RIB FLANGES. CRACKS WERE STOP DRILLED AND PLATE INSTALLED OVER THE RIB FLANGE AREA IAW AIR TRACTOR INSTRUCTIONS (ATTACHED). THISSDR UPS07M48815Skin · crackedLEADING EDGE CRACK AFT OF NR 7 SLAT. FIXED L/E SKIN AFT OF NR 7 LT SLAT I/B SIDE AT STA X0S 906 REF 57-10-00 PG 104. DMG REMOVED. ROLLED DBLR & PICK UP HOLES FAB FROM 7075-76-063. DRILLED,TRIMMED, BEVELED & PRIMED SURFACE PER SRM 57-10-00. INSTALL DBLR. INSTSDR DLM88070419Skin · delaminatedLT FORWARD CENTER BUTE DOOR EXTERNAL SKIN REPLACEMENT - SEVERAL DELAMINATED AREAS ON SKIN P/N 5919586-35 BETWEEN STA XRS=170.746-XTE=251.996. EXTERNAL SKIN WAS REPLACED IAW BACG PRODUCTION DRAWING 5919586-505 AND ERA 458462-14.SDR 06FDEA04335Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT LOWER WING SURFACE CORNER OF ACCESS PANEL 581 AB, WS 663 AND RIB 11. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFSDR 06FDEA04339Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE OUTBD OF NR 7 SPOILER, WS 1604 AND RIB 26. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO SDR 06FDEA04300Skin · delaminatedRT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN IAW A310-200 SRM 57-52-12 FIG 204. THE REPAIR IS FOUND TO BE MAJOR IAW FED EX GMM 6-2-100.SDR 06FDEA04285Skin · gougedLWR SURFACE OF WING JUST O/B OF AFT PYLON HAS DEEP GAUGE FROM DEPARTURE OF PYLON "V" PANEL DURING FLIGHT NR 3 PYLON. GOUGE LOCATION ON RIGHT WING BOTTOM SKIN BETWEEN S41 AND S40 AT XORS 372.0. GOUGE MEASURES 5.5 IN LONG AND 0.060 DEEP AT DEEPEST POINT. GOSDR COMA0660713Skin · crackedWHILE PERFORMING EDDY CURRENT INSPECTION OF THE WING PLANK DRAIN HOLES, TASK CARD 002-57-540/640-603, A CRACK WAS FOUND AT SW 66.75 BETWEEN STRINGER 14L AND 15L. WING PLANK WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-57-21-770 DATED 12-15-06.SDR UIEA2006310Skin Panel · delaminatedLT WING UPPER L/E PANEL HAS A PREVIOUS REPAIR DELAMINATED AND CRACKED, 8.0 IN. BY 5.0 IN. ACCOMPLISHED PERMANENT REPAIR AS PER B747 SRM 51-40-09 FIG 1 AND B747 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO 4757A335.SDR UIEA2006309Skin Panel · delaminatedRT WING UPPER SURFACE T/E PANEL HAS 4.0 IN. BY 2.0 IN. AREA OF DELAMINATION LOCATED 30 INCHES I/B OF I/B AILERON. ACCOMPLISHED PERMANENT REPAIR AS PER B747 SRM 51-40-09 FIG 2 AND B747 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO 4757A334.SDR UIEA2006307Panel · tornRT WING LOWER PANEL 671AB INBOARD CORNER IS TORN, 2.0 INCH BY 2.0 INCH AREA. ACCOMPLISHED PERMANENT REPAIR AS PER B747 SRM 51-40-09 FIG 1 AND B747 SRM 51-40-12. ALSO REFERENCE ATLAS AIR EO 4757A334.SDR IXXA06SMN436SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS422.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATEDSDR IXXA06SMN435SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD AILERON SKIN DENTED AT STATION XA694.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED REPAIR PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSDR MASA200800040Skin · corrodedCORROSION DAMAGE (3 OFF AREAS), 0.026 INCH MAX DEPTH TO RT WING LOWER PLANK FUEL TANK ACCESS PANEL AT LOWER PANEL LOCATION 541AB. THE DAMAGE MEASURE 1/10" WIDE IN FWD AND AFT DAMAGED AREAS. REPAIRED DAMAGE.SDR QXEA200603275Skin · chafedC3 OKC - LEFT AILERON LOWER FORWARD EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 51-25-06, AND 51-21-16.SDR QXEA200603315Fastener · looseC3 - LEFT WING LOWER SURFACE HAS SMOKING RIVETS AT TRAILING EDGE WS147. REPLACED RIVETS IAW CRJ700 SRM 51-12-06-001-001-A01.SDR QXEA200603264Skin · gougedC3 OKC - LEFT WING LEADING EDGE IS GOUGED AT INBOARD SLAT SPLIT. REPAIRED IAW SRM 51-12-00 AND 57-41-01.SDR UIEA200600304Skin · crackedLT WING UPPER L/E PANEL AT WBL 450 SURFACE HAS AREA OF COMPOSITE CRACK. ACCOMPLISHED PERMANENT REPAIR OF AREA OF CRACK AS PER B747 SRM 51-40-09 FIG 18 AND 747 SRM 51-40-12. CRACK LENGTH IS 2.0 INCHES LONG AND REPAIR AREA IS 4.0 INCH BY 7.0 INCH. ALSO, REFERSDR UIEA200600303Skin · crackedRT WING UPPER L/E PANEL HAS 2 EACH AREAS WITH COMPOSITE CRACKS AT WBL 480, WBL 480 FORWARD CRACK IS 8.0 INCHES LONG. REPAIR AREA IS 3.0 INCH BY 12.0 INCH, WBL 480 AFT CRACK IS 6.0 INCHES LONG. REPAIR AREA IS 7.0 INCH BY 12.0 INCH. PERMANENT REPAIR WAS ACCOMSDR QXEA200603282Panel · wornC3 OKC - PANEL 684GB WORN BARE METAL AT CUTOUT. REPAIRED IAW SRM 57-41-01, 51-21-16, AND 51-21-00.SDR QXEA200603268Panel · damagedC3 OKC - LEFT WING PANEL 522AB IS SCRATCHED AND HAS BARE METAL. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603277Skin · scratchedC3 OKC - RIGHT WING INBAORD LEADING EDGES HAVE SEVERAL SCRATCHES. REPAIRED IAW SRM 51-21-01, 51-12-00.SDR QXEA200603314Skin · damagedC3 - LEFT WING UPPER SURFACE HAS SMOKING RIVET AT TRAILING EDGE WS 170. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR QXEA200603311Skin · damagedC3 - RIGHT WING TRAILING EDGE TOP SURFACE INBOARD AND OUTBOARD OF MFS, TRAILING EDGE SURFACE HAS SEVERAL LOOSE SOLID RIVETS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR UIEA200600298Skin Panel · delaminatedLT WING UPPER L/E PANELS AT ILES 675.50 AND ILES 651.50 HAS AREA OF DELAMINATION. ACCOMPLISHED PERMANENT REPAIRS AT LT WING L/E UPPER PANELS AS PER BOEING 747 SRM 51-40-09 FIG 18, SHEET 5 AND 747 SRM 51-40-12. ILES 675.50 REPAIR AREA IS 7.0 INCH LONG BY 7.0 SDR UIEA200600297Skin Panel · delaminatedLT WING UPPER FIXED TRAILING EDGE PANEL AT WBL 445.0 HAS A 2.O INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER BOEING 747 SRM 51-40-09 FIG. 2, SHEET 5 AND 747 SRM 51-40-12. REPAIR AREA IS 3.0 INCH LONG BY 4.0 INCH WIDE. ALSO, REFERENCE ATLAS AIR XEO NR 57-SDR 06FDEA04138Skin · corrodedCORROSION LEFT WING UPPER SKIN AT BUTT SPLICE 42" OTBD OF NR 4 SLAT INBD EDGE. REPAIRED PER FED EX EA 7-5730-105911.SDR 2006UALA02260Skin · damagedLEFT WING LEADING EDGE UPPER SURFACE HAS PREVIOUS REPAIR THAT IS CRACKED AND DELAMINATED AT NR 3 SLAT ACTUATOR CUTOUT. MAJOR REPAIR: REMOVED EXISTING REPAIR AND ACCOMPLISHED REPAIR REF AAR EA I060533.SDR 06FDEA04123Skin · crackedRIGHT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 3:30 POSITION (LOOKING FORWARD VIEW UP). RIGHT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUTOUT BETWEEN STASDR 06FDEA04122Skin Panel · crackedLEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 1:30 POSITION (LOOKING FORWARD VIEW UP). LEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS =SDR UIEA200600293Skin Panel · delaminatedRT WING UPPER FIXED TRAILING EDGE PANELS AT WBL 353 AND WBL 445 AND UPPER FIXED LEADING EDGE PANEL AT WBL 363 HAVE DEGRADED AND DELAMINATED EXISTING COMPOSITE REPAIRS. ACCOMPLISHED PERMANENT REPAIRS AT WBL 353 ON 12 INCH LONG BY 10 INCH WIDE SECTION, WBL 445,SDR UIEA200600295Skin · corrodedCORROSION FOUND BETWEEN UPPER WING SKIN REAR SPAR AREA AND FLYING PANEL AT STATION 406. REPAIR CARRIED OUT IAW XEO 57-112106 AND SRM 57-30-01 FIG 1.SDR UIEA200600294Skin · corrodedCORROSION FOUND ON RT WING REAR EDGE BETWEEN REAR SPAR UPPER SKIN AND FWD EDGE OF FLYING PANEL. PANELS AT STA 456 AND 586. LEVEL 1 CORROSION. REPAIR CARRIED OUT PER XEO 57-112206 AND SRM 57-30-01 FIG 1.SDR 06FDEA04062Skin · corrodedRT WING L/E DROOP FOUND CORROSION WITH EXF ON EXT SKIN. REMOVED SEAL IAW SRM 51-31-01 VOL 2 PAGE 36/41. REMOVED RUB STRIP IAW SRM 51-31-01 VOL 2 PAGE 36/41. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VOL 2 PAGE 1/13. CLEANED AREA IAW SRM 51-21-01 VOL 2 PAR 2SDR DHL2006807523Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED 8" (STA XA 566.000 - 613.000). REMOVED AND REPLACED RT WING UPPER PANEL IAW SRM 51-3-0, SRM 51-3-1.SDR QXEA200603385Skin · chafedPDX C4 - CHAFE DAMAGE ON RIGHT WING UPPER SKIN DOUBLERS AROUND AFT INBOARD AND OUTBOARD SCREW HOLES FOR PANEL 422ET. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-36 AND 51-20-51.SDR QXEA200603087Skin · wornC3 YYC - LEFT LOWER WING SURFACE HAS WEAR MARK ON SKIN AT NR 2 FLAP TRACK WS 128. REPAIRED IAW SRM 57-00-01 AND 51-25-16.SDR IXXA06SMN426SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD LEADING EDGE UPPER SLANT PANEL CORRODED FROM STATION XFS7.000 TO STATION XW751.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION SDR IXXA06SMN425SPanel · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING INBOARD LEADING EDGE SLANT PANEL UPPER CAP CORRODED AT STATION XFS7.000 TO STATION XFS195.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED SLANT PANEL UPPER CAP. CLEANED, TREATED AND PRIMED AREA. INSTA
Back to JASC 5730