JASC 5730

Service difficulty reports · 27,262

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 JGVR20181210002Access Panel · corrodedFUEL PANEL LANDS 511AB, 511BB, 511DB, AND 511EB HAVE AREAS OF CORROSION. BLENDED AREAS OF CORROSION ON FUEL PANEL LANDS 511AB, 511BB, 511DB, AND 511EB IAW CITATION 560XL SPM: 51-10-00. PERFORMED REPAIR TO BLENDED AREAS PER TEXTRON LETTER REF. DQ16664M1 RRL DATDec 10, 2018 · N579QS · Cessna 560XLSDR JGVR20181210001Panel · corrodedUNDER-WING PANELS 510DB AND 610DB HAVE SMALL AREAS OF CORROSION. FOUND DURING COMPLIANCE OF TASK A570000. REPLACED CORRODED FUEL ACCESS PANELS 510DB AND 610DB WITH NEW FUEL ACCESS PANELS PN:9912514-22 AND 9912514-21.Dec 10, 2018 · N579QS · Cessna 560XLSDR SWAA2022022822978Seal · crackedLEFT HAND HORIZONTAL STAB; FORWARD LOWER SLIDER SEAL TEFLON RUNNER CRACKED / REPLACED L/H HORIZONTAL STAB; FORWARD LOWER SLIDER SEAL IAW AMM 53-31-31-000-803 AND AMM 53-31-31-400-803 AND IPC 53-31-31-02A ATAG #UK1490; AA9777Dec 8, 2018 · N269WN · Boeing 7377H4SDR DALA2018121187148Access Panel · missingACCESS PANELS 522MB, 522PB, 622MB, 622PB MISSING ON LEFT AND RIGHT WING. COVERED AREAS WITH SPEED TAPE AND DEFERRED. LP 5263059Dec 8, 2018 · N803NW · Airbus A330323SDR SWAA2022022815387Panel · elongatedR/W T/E PANEL 671BB HAS A ELONGATED HOLE. ( MARKED ) / REPAIRED ELONGATED HOLE ON R/W T/E PANEL 671BB IAW SRM 51-70-05-2R-6 59278U 12/17/18Dec 6, 2018 · N7851A · Boeing 7377Q8SDR DALA2018121067124Skin · damagedDAMAGE ON LWR AFT TRAILING EDGE OF WING TIP L/H SIDE. C/W PERMAMENT REPAIR PER SRM 57-31-01. (LP 5263140)Dec 5, 2018 · N845MH · Boeing 767432ERSDR AALA201812269004Skin · corrodedCORROSION FOUND ON THE SKIN BETWEEN RIBS 5 - 6 ON THE LEFT WING. REPAIRED THE SKIN IAW EA 105103A.Dec 4, 2018 · N165US · Airbus A321211SDR AALA201812075003Skin · crackedDURING ACCOMPLISHMENT OF ECO F2326AA-001, AND HFEC ROTARY HOLE PROBE INSPECTION, ON THE LEFT WING DIAGONAL BRACE, FASTENER HOLE NR 9, FOUND A CRACK INDICATION IN THE SKIN LAYER ONLY AT THE AFT INBOARD SIDE OF HOLE. REPAIRED IAW EA 287209.Dec 4, 2018 · N195AN · Boeing 757223SDR DALA2018120407032Skin · damagedRT LOWER WING SKIN STRINGER L-6.5. BETWEEN WSTA990.2 AND WSTA1018.2. DIAMETER:0.625" HOLE REPAIRED PER ER/A 572984-14.Dec 4, 2018 · N183DN · Boeing 767332SDR DALA2018120407031Skin · crackedLT WING LOWER SKIN, STRINGER L-9.5 WSTA906.20 TO WSTA934.20. ONE CRACKED HOLE REPAIRED PER ER/A 572983-14.Dec 4, 2018 · N183DN · Boeing 767332SDR DALA2023011300272Doubler · not reportedSHIP 183 RH LOWER WING SKIN EXTERNAL DOUBLER REPAIR AT STR 6.5 AND STA 990. CORRECTIVE ACTION: ER/A 572984-14AD REVISED TO REV. A. ACCOMPLISH ER/A 572984-14AD REV A SECTION II INSPECTIONS. (0850550)Dec 3, 2018 · N183DN · Boeing 767332SDR SWAA2022022858659Panel · delaminatedFWD OUTB'D CORNER OF PANEL 621SB DELAMINATED. / REPAIRED PANEL PER SRM 57-41-01Dec 3, 2018 · N488WN · Boeing 7377H4SDR FDEA201812030123Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, 22" AFT OF FRONT SPAR AT WS 204.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND Dec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030122Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 269 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TODec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030121Skin · corrodedRT WING, CORROSION ON UPPR SURFACE, ABOVE REAR SPAR AT WS 361 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO Dec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030120Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE FRONT SPAR, WS 642 TO WS 654 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 ANDec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030119Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, AS OF REAR SPAR WS 289-293 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TDec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030118Skin · corrodedRT WING CORROSION ON UPPR SURFACE AFT OF REAR SPAR, WS312 TO WS316 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUNDec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030112Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 215 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FDec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030111Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 300 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FODec 3, 2018 · N915FD · Boeing 757236SDR FDEA201812030110Skin · corrodedLT WING UPPER TE, EVIDENCE OF CORROSION ADJACENT TO FASTENER HEADS AT AREA 5 INCHES AFT OF REAR SPAR AND 67 INCHES OUTBOARD OF WING ROOT FAIRING 195AL REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DADec 3, 2018 · N915FD · Boeing 757236SDR ASOA2018121935345Skin · crackedREF: CO# 7496618 JOB# 7749665 OP# 35: LOWER WING PLANK CUTOUT FOR R/H BOOST PUMP HAS AN INDICATION NOTED ON THE LOWER SURFACE OF THE WNG PLANK ON THE AFT SIDE OF CUT OUT. INDICATION IS .150" LONG BY 100% FSH. FAILED NDT INSPECTION.C/A: REPAIRED DAMAGE I.A.W. Dec 3, 2018 · N881AS · Cndair CL6002B19SDR YENA2018120730817Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB 4-5 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 4-5 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB MDec 3, 2018 · N509JB · Airbus A320232SDR YENA2018120730816Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB1-2 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 1-2 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB MUDec 3, 2018 · N509JB · Airbus A320232SDR YENA2018120730815Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE AT LEVEL RIB 7 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BETWEEN RIB 7 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AEDec 3, 2018 · N509JB · Airbus A320232SDR YENA2018120730814Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED BTWN RIB 8-9 UPPER SURFACE ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 8-9 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AEROMDec 3, 2018 · N509JB · Airbus A320232SDR FDEA201812033418Finger Doubler · detachedRIGHT WING TRAILING EDGE INBOARD ISLAND UPPER SKIN FINGER DOUBLER AT XORS 449 FOUND DETACHED. RIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER AT XORS 449 DAMAGED SKIN AREA REPAIRED AS PER SRM 57-50-01-2R FIGURE 202 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER Dec 3, 2018 · N599FE · Doug MD11FSDR FDEA201811300155Skin · corrodedLT WING, UPPER SURFACE RSS 170 TO RSS 200 AT WING SKIN AND TRAILING EDGE PANEL JOING SUSPECT CORROSION. COROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1 REV 125. REPAIR CARRIED OUT IAW EA #F-573Nov 30, 2018 · N915FD · Boeing 757236SDR FDEA201811300109Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS.748 TO WS761, 2 INCHES FWD OF REAR SPAR AND TRILING EDGE PANEL JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 ANNov 30, 2018 · N915FD · Boeing 757236SDR FDEA201811300108Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101 TABLE Nov 30, 2018 · N915FD · Boeing 757236SDR FDEA201811300107Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125 EVALUATED BLEND OUT AND FOUND AREA TO BE OUT OF LIMITS IAW DUE TO LOCATION OF DAMAGE IAW Nov 30, 2018 · N915FD · Boeing 757236SDR ASOA2018121435341Skin · corrodedREF: CO# 7476718 JOB# 7747675 OP# 57 LOWER WING PLANK CUTOUT FOR RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORZ AND VERTICAL SURFACE 50% FSH. FAILED NDT INSP. C/A: PERFORMED MAJOR REPAIR CARD NO: REO 601R-57-21-2908 BLENDED TONov 30, 2018 · N862AS · Cndair CL6002B19SDR AALA201812039001Skin · crackedA CRACK WAS FOUND ON THE LOWER SKIN, OTBD FIXED LEADING EDGE RIB 15 ON THE RT WING. REPAIRED THE SKIN IAW SRM 57-41-11-300-013, AND DRAWING D574-59073.Nov 30, 2018 · N977UY · Airbus A321231SDR JGVR20181130001Access Panel · corrodedCENTER WING FUEL QUANTITY DIPSTICK PANEL 172BZ HAS LEVEL 2 CORROSION AROUND SEVERAL SCREWS REQUIRING REPLACEMENT OF OUTER PANEL. FOUND WHILE PERFORMING C750 BASE CHECKLIST.Nov 30, 2018 · N906QS · Cessna 750SDR FDEA201811290068Skin · corrodedLT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. REV 125 ALLOWABLE MINIMUM REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.145" REPAIRNov 29, 2018 · N915FD · Boeing 757236SDR FDEA201811290066Skin · corrodedRT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. ALLOWABLE MINIMUN REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.148 REPAIR CARRIED OUNov 29, 2018 · N915FD · Boeing 757236SDR SWIA2018121245310Skin · dentedDENT ON RH WING LEADING EDGE. (FLT#3110) FO: 11/30/2018. CLOSED C/W REO.Nov 29, 2018 · N930EV · Cndair CL6002B19SDR SWIA2018113045310Skin · dentedDENT ON RT WING LEADING EDGE. FLIGHT 3110. FO: 11/30/2018. CARRIED FORWARD FOR RESCHEDULING, TIME REMAINING UNTIL NEXT RE-INSPECTION IS DUE OR UNTIL PERMANENT REPAIR IS REQUIRED.Nov 29, 2018 · N930EV · Cndair CL6002B19SDR R61A201812181242Skin · cracked*** WHILE THE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** MAJOR... A 0.465 INCH CRACK WAS FOUND ON LH WING LOWER SKIN @ RIB 17 AND STR 19. CRACK WAS REPAIRED IAW ETD2018-170-125321 REV A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECKNov 28, 2018 · N646RW · Emb ERJ170100SESDR ASOA2018121475339Skin · crackedREF: CO#7476718 JOB# 7747675 OP#43 R/H LOWER WING PLANK AND STRAP JOINT CRACKED AT RWS 148.00. C/A REPAIRED DAMAGE IAW EXPRESSJET ECTC REO 601R-57-21-130 01.Nov 27, 2018 · N862AS · Cndair CL6002B19SDR DALA2018112766842Skin · corrodedLEFT WING LOWER SKIN WSTA 962.2-900.2 HAS A CRACKED FASTENER HOLE AT L-9.5. C/W ERA 573238-14. (LP 5141061)Nov 25, 2018 · N156DL · Boeing 7673P6SDR FDEA201811233355Finger Doubler · detachedRIGHT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT ON STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-Nov 23, 2018 · N618FE · Doug MD11FSDR FDEA201811233354Finger Doubler · detachedLEFT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT AT STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-Nov 23, 2018 · N618FE · Doug MD11FSDR DALA2018112626781Skin · damagedSKIN FOUND THE NO.66 HOLE DIAMETER :0.624" REPAIRED PER ERA 573161-14. (LP 0836480)Nov 22, 2018 · N176DN · Boeing 767332SDR DALA2018112626780Skin · crackedHFEC SURFACE INSPECTION FOUND 01 EA CRACK APPROX 0.080"IN LENGTH AT THE FWD DIRECTION OF THE MOST O/B HOLE AND REPAIRED. (LP 0836471)Nov 22, 2018 · N176DN · Boeing 767332SDR ASOA201811185325Skin · damagedREF: CO# 7654518 JOB# 7765456 OP# 6: WHILE PERFORMING SB 601R-57-046, FOUND (1EA) FASTENER TO BE OVERSIZE IN R/H LOWER BUTTSTRAP AND WINGPLANK.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-57-21-2900 REV.--, DATED 2018-11-12 AND EXPRESSJET EC/TC REO 601R-57-Nov 18, 2018 · N908EV · Cndair CL6002B19SDR FDEA201811183273Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPLACED WITH NEW RIB DOUBLER AS PER SRM 51-33-01-0G. FABRICATED RIB DOUBLER AS PER DWG ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Nov 18, 2018 · N599FE · Doug MD11FSDR K11A2020010302Skin · corrodedLEFT WING UPPER SURFACE WBL 72 APPROX S-19C HAS CORROSIONNov 17, 2018 · N332CK · Boeing 737375SDR AALA2018121989019Skin · wornWEAR FOUND ON THE INBOARD SKIN ON THE FIXED LEADING EDGE RIB UNDER THE ROOT FILLER FAIRING BETWEEN STATION 0 - 700, RIB 1 TO 2, LT WING. REPAIRED THE SKIN IAW EA 287405.Nov 17, 2018 · N815AW · Airbus A319132SDR DALA2018121307165Skin · crackedRIGHT WINGS UPPER SKIN PANEL OUTBOARD UPPER LINK PITCH LOAD FITTING AREA CRACKED FASTENER LOCATIONS C/W ERA 507538-14 (LP 0829134)Nov 16, 2018 · N183DN · Boeing 767332
Back to JASC 5730