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 DHL2007804519Panel · delaminatedLT WING T/E LWR PANEL DELAMINATED (STA XW 0.000 - 90.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL (STA XW 0.000 - 90.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873FSDR DHL2007804518Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XRS 162.000 - XF 219.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANEL (STA XRS 162.000 - XF 219.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873FSDR DHL2007804517Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XW 0.0000 - 47.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANEL (STA XW 0.000 - 47.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873FSDR DHL2007804516Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XW 97.000 - XRS 162.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873FSDR A6WA200740468Skin · corrodedLEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 HAS CORROSION IN NON-CRITICAL AREA MEASURING 3.5 INCH BY .35 NCH BY .004 INCH DEEP ALONG INBOARD LIP LANDING. MAINTENANCE BLENDED CORROSION ON LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 IAW BOMBARDIER REO 6Aug 7, 2007 · N466AW · Cndair CL6002B19SDR DHL2007804523Skin · damagedRT OUTER WING INBD L/E HOLES ELONGATED STA XW 485.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D857-0009 REV IR DATED 06-13-07, DWG AD79-57-102 REV IR DATED 07-13-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUAug 6, 2007 · N804DH · Doug DC873FSDR 07FDEA02770Skin · damagedLT WING, LEADING EDGE EXTERIOR SKIN BETWEEN SLAT TRACK NR 10 AND NR 11 FOUND CHIPPED. [08-17-07] CHIPPED AREA SMOOTHENED OFF AS PER SRM 51-21-01 VOLUME II. EXCEEDED LIMIT AS PER SRM 57-00-01 FIGURE 2 VOLUME I. REWORKED AREA REPAIRED AS PER SRM 57-10-00 FAug 6, 2007 · N612FE · Doug MD11FSDR 07FDEA02769Skin · crackedWITH REFERENCE TO EA NR 1-5710-90773 DURING ACCOMPLISHMENT OF ALI 57.23.01.2. TWO MOUNTING BORES THE TANKS ACCESS PLATE AT STA XORS = 713.6 GAVE A CRACK INDICATION. THE BORES WERE INCREASED TO 0.310" WHERE CRACK INDICATION CEASED. COMPLIED WITH FEDEX EA NR Aug 5, 2007 · N602FE · Doug MD11FSDR 07FDEA02765Skin · crackedCRACK INDICATIONS REVEALED IN 06 EA FASTENER HOLES TOWARDS EDGE OF ACCESS C/OUT IN LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS= 683.400 TO XORS= 713.600. REPAIRED AS PER FEDEX EA 1-5710-112375, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Aug 4, 2007 · N612FE · Doug MD11FSDR 07FDEA02766Skin · crackedCRACK INDICATIONS REVEALED IN 09 EA FASTENER HOLES TOWARDS EDGE OF ACCESS. C/OUT IN RT WING LWR SKIN ACCESS DOOR C/OUT (BETWEEN STA XORS= 683.400 TO XORS= 713.600). [08-17-07] REPAIRED AS PER FEDEX EA 1-5710-112376, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-Aug 4, 2007 · N612FE · Doug MD11FSDR DHL2007804508Skin · crackedRT WING UPPER SKIN CRACKED 1 1/4" AT STA XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 20 SHEET 1. PERFORMED NDT INSPECTION IAW DAug 3, 2007 · N804DH · Doug DC873FSDR TAMF20070012SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 57-666-00) WAS FOUND A LIGHTNING STRIKE ON WING UPPER SKIN STA 1018.2 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-490432776 AND EWO 767 57-023. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISAug 2, 2007 · N767QT · Boeing 767200SDR DHL2007804505Panel · corrodedLT WING T/E UPPER SURFACE PANEL CORRODED, STA XRS 74.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED CORRODED PANEL ASSY IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEAug 1, 2007 · N804DH · Doug DC873FSDR DL75E070979Skin · damagedDAMAGE LED TO A 0.500" OVERSIZED WING SKIN HOLE AND A 0.310" OVERSIZED STRINGER U-9.5 HOLE AT A COMMON FASTENER LOCATION JUST INBD OF WING STATION 537 (3RD NEW FASTENER FROM RIB NR 17). REPAIR CONSISTED OF A COUNTERSUNK FREEZE PLUG AND AN OVERSIZED FASTENER. Aug 1, 2007 · N702TW · Boeing 7572Q8SDR 07FDEA02677Skin · dentedLT WING, I/B FLAP LOWER SKIN (I/B HALF) FOUND WITH NUMEROUS DENTS. [08-15-07] REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 31, 2007 · N612FE · Doug MD11FSDR 07FDEA02675Panel · corrodedPNL 486BR HAS FRETTING CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10.Jul 30, 2007 · N405FE · Airbus A310203SDR 07FDEA02674Panel · corrodedPNL 486BR HAS FRETTING CORRSION AND BARE METAL EXPOSED REMOVED CORRSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10.Jul 30, 2007 · N405FE · Airbus A310203SDR 07FDEA02673Panel · corrodedPNL 438BL HAS SURFACE CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM 7-1-1001. ALODINED AND PRIMED PER 51-23-10 AND 51-21- 10.Jul 30, 2007 · N405FE · Airbus A310203SDR DHL2007804504Skin · damagedLT OUTER WING INBD L/E SKIN HOLES ELONGATED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-25-07, DWG NR AD79-57-101 REV IR DATED 07-13-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWGJul 28, 2007 · N804DH · Doug DC873FSDR A6WA200740428Skin · corrodedLT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19SDR A6WA200740427Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19SDR A6WA200740426Skin · corrodedRT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19SDR UPS07450346Panel · delaminatedRT WING LEADING EDGE, TOP FILLER PANELS OF NR 3 ENGINE 4 INCH X 10 INCH DELAMINATED. DISCOVERED ADDITIONAL DELAM OF INNER SKIN OPPOSITE EXTERIOR SOFT SPOT. REMOVED PANEL FROM AIRCRAFT XZ 1227688, TRIMMED AND PICKED UP HOLES IN NEW PANEL IAW INSTALLED NEW PANEJul 27, 2007 · N677UP · Boeing 747123FSDR UPS07M50728Skin · dentedINSPECTION TYPE:C LEFT WING INBOARD FLAP UPPER SURFACE SKIN DENT. LEFT WING I/B FLAP UPPER SURFACE SKIN DENT AREA TRIMMED OUT. HFEC INSP C/OUT ON TRIMMED OUT FOUND NO CRACK. REPAIR DOUBLER FABRICATED USING MAT'L 2024T3-0.040" & HOLES PICKED UP. REPAIR PARTJul 25, 2007 · N290UP · Doug MD11FSDR 07FDEA02582Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 636AB). [08-09-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112366, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 23, 2007 · N603FE · Doug MD11FSDR 07FDEA02581Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 536AB). [08-09-07] REPAIR CARRIED OUT IN FASTENER HOLE TOWADS EDGE OF ACCESS CUTOUT IN LT WING LOWER SKIN ACCESS DOOR CUTOUT (PANEL 53Jul 23, 2007 · N603FE · Doug MD11FSDR 07FDEA02532Skin · crackedCRACK INDICATIONS REVEALED IN 04 FASTENER HOLES TOWARDS EDGE OF ACCESS, CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112360, REPAIR CLASSIFIED AS MAJOR PER GJul 20, 2007 · N602FE · Doug MD11FSDR 07FDEA02531Skin · crackedCRACK INDICATIONS REVEALED IN 04 EACH FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112359, REPAIR CLASSIFIED AS MAJOR PER Jul 20, 2007 · N602FE · Doug MD11FSDR 2007FA0000872Skin · corrodedLT AND RT WING UPPER SKINS UNDER THE NACELLE FUEL BLADDER TANKS HAD CORROSION PRESENT TO THEM AND RELATED AREA AROUND THE BLADDER BAYS. WO NR 10688. (K)Jul 19, 2007 · N648SB · Cessna 421CSDR USAA070571Access Panel · corrodedRIGHT OUTER WING AT FUEL SHUTOFF VALVE ACCESS PANEL HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER IPC 28-22-11; CORR TASK C57-300-01, DEFECT SIZE: .1875 INCH.Jul 19, 2007 · N417US · Boeing 737401SDR UPS07850339Skin · gougedINSPECTION TYPE:C2 LH INBD UPPER SURFACE SKIN EXSISTING REPAIR DOUBLER HAS DEEP GOUGE AT STA 100 REMOVED DAMAGED DOUBLER AT L/WING STA 100 IAW SRM 51-01-21-0 FABRICATED AND INSTALLED REPAIR DOUBLER AT LH WING INBD UPPER SURFACE STA 100 IAW SRM 57-07-01-0 AJul 18, 2007 · N851UP · Doug DC873FSDR USAA070556Skin · crackedLEADING EDGE JUST O/B OF LEFT PYLON WING STA 157 HAS CRACK. STOP DRILLED CRACK, INSTALLED DOUBLER PER TR 57-41-02, DEFECT SIZE: 0.5 INCH.Jul 18, 2007 · N417US · Boeing 737401SDR 07FDEA02489Skin · corrodedUPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.Jul 16, 2007 · N556FE · Doug DC1010FSDR 07FDEA02488Skin · corrodedUPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II.Jul 16, 2007 · N556FE · Doug DC1010FSDR 07FDEA02486Panel · delaminatedRT WING OB TE PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-02 PG 1 AND PG 13-14.Jul 16, 2007 · N481FE · Boeing 727227SDR UPS07M50447Skin · crackedINSPECTION TYPE:C RIGHT WING L/E CORRUGATED SKIN FOUND CRACKED AT 04 EA PLACES AROUND RIVETS AT 14 INCHES O/B OF REFUEL PANEL I/B EDGE AS MARKED. CRACKED AREA TRIM OUT PER SRM TEMP REV 57-10-00 FIG 25B R38. HFEC INSP C/O PER DAC NDT SPM REV13 PART6 06-10-01.Jul 15, 2007 · N289UP · Doug MD11FSDR UIEA200700264Panel · delaminatedRT WING FUELING BAY ACCESS PANEL NR 621BB, INNER SKIN HAS 2 EACH AREAS OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 18, SHEET 1, 3, AND 5, TABLE 1, PREPEG 250* F CURE. ALSO, REFERENCE ATLAS AIR XEO NR 57-071207.Jul 13, 2007 · N526MC · Boeing 7472D7BSDR 07FDEA02450Panel · delaminatedRT WING O/B T/E PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-2 PG 1 & PG 13-14.Jul 13, 2007 · N481FE · Boeing 727227SDR 07FDEA02479Skin · wornLT WING L/E ON EXTERNAL SKIN DROPPED FOUND DEEP WEAR. REPAIRED AREA IAW SRM 57-10-00 FIG 39 VOL 1.Jul 13, 2007 · N68052 · Doug DC1010FSDR 07FDEA02472Skin · crackedLT WING L/E EXTERNAL SURFACE LWR SIDE ON SKIN FOUND CRACK 0.40" LONG. REPAIRED SKIN IAW SRM 57-10-00 VOL 1 FIG 68.Jul 13, 2007 · N68052 · Doug DC1010FSDR 07FDEA02469Skin · wornRT WING SLATS DEEP WEAR ON EXT SKIN ON DROOPED L/E OUTBOARD SIDE. REPAIRED AREA IAW SRM 57-10-00 VOL 1 PAG 39.Jul 13, 2007 · N68052 · Doug DC1010SDR 07FDEA02462Skin · unknownEXISTING REPAIR LT WING I/B FLAP LOWER SKIN. REPAIRED IAW SRM 57-00-01 VOL 1 FIG 1A SHT 2.Jul 13, 2007 · N68051 · Doug DC1010FSDR 2007FA0000683Skin · crackedCRACK IN THE TOP SKIN OF THE RT WING AT THE LANDING GEAR SIDE BRACE ATTACHMENT LOCATION, APPROX WS 63.45. THE SKIN IS 2024-T3 ALUMINUM, .032 THICK. THE CRACK IS ABOUT 4.5 INCHES LONG. (K)Jul 12, 2007 · N5152J · Cessna 340CESSNASDR 2007FA0000675Skin · crackedCRACK IN THE TOP SKIN OF THE LT WING AT THE LANDING GEAR SIDE BRACE ATTACHMENT LOCATION, APPROXIMATELY WS 63.45. THE SKIN IS 2024-T63 ALUMINUM, .032 THICK. THE CRACK IS ABOUT 3 INCHES LONG OR LONGER. CANNOT DETERMINE THE TOTAL LENGTH OF THE CRACK. (K)Jul 12, 2007 · N8647K · Cessna 340ASDR AMWA15036CSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 6772-1 REV 1R.Jul 10, 2007 · N155ZV · Beech 1900DSDR AMWA15036BSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 677201 REV 1R.Jul 10, 2007 · N155ZV · Beech 1900DSDR KCSA071209Skin · corrodedLOWER RIGHT WING SKIN FWD OF FRONT SPAR WS 1308.00 IS CORRODED AT STIFFENER PAD.Jul 10, 2007 · N702CK · Boeing 747146SDR A6WA200740366Skin · corrodedRT WING PLANK ACCESS HOLE R 2 (610AB) WS 12.245 HAS PITTING ALONG FWD HALF OF HOLE, APPROX .007 DEEP LOCATED IN CRITICAL AREA. (K) MAINTENANCE REMOVED MINOR PITTING, NDT, ROTO-PEENED AND TREATED AREA. (M)Jul 9, 2007 · N409AW · Cndair CL6002B19SDR A6WA200740365Skin · corrodedLT WING PLANK ACCESS HOLE NR 11, (550CB) WS 209.040 HAS PITTING ON IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON CRITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO PEENED AND PROTECTED TREATED AREA. (M)Jul 9, 2007 · N409AW · Cndair CL6002B19SDR A6WA200740364Skin · corrodedLT WING PLANK ACCESS HOLE NR 2, (510AB) WS 12.245 HAS PITTING AT IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON-CRITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO-PEENED AND PROTECTIVE TREATED. (M)Jul 9, 2007 · N409AW · Cndair CL6002B19
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