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 05FDEA04043Skin · crackedRIGHT WING FIXED LEADING EDGE FOUND CRACKED AT TELESCOPE DUCT UPPER CUTOUT. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT UPPER SKIN CUTOUT AS PER FEDEX EA 1-5730-90693, TITLE "WINGS - RT WING LEADING EDGE SKIN CRACKS AT TESDR 2005UALA01374Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 617.5 AT WBL 85.0 TO 87.0. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.SDR 2005UALA01373Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 626 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.SDR 2005UALA01372Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 626 TO 663.7 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTORED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.SDR 05FDEA04006Doubler · corrodedDURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.SDR 05FDEA04005Doubler · corrodedDURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.SDR 05FDEA03974Skin · crackedRT WING TIP WING CRACKED 1 INCH LONG ON LOWER SKIN. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER IAW SRM 57-00-01 FIG 4 AND SRM 51-35-01 PG 1/13. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160709/N00709 IAW SRM 57-00-01 FIG 4.SDR 05FDEA03979Repair · properRIGHT WING LOWER SURFACE FOUND DOUBLER REPAIR ON PANEL 8 X 5 INCHES. PERFORMED INSPECTION TAP TESTING, NO DELAMINATION FOUND IAW SRM 51-61-01 VOL 2 AND PERFORMED INSPECTION ON REPAIR IAW SRM 57-71-00 VOL 2 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-510SDR VNAA0511023Skin · ground damageTHE RIGHT WINGLET SUSTAINED LEADING EDGE DAMAGE AFTER HITTING A BAGGAGE CART WHILE AIRCRAFT WAS BEING MARSHALLED INTO THE GATE. MAINTENANCE REMOVED & REPLACED THE RIGHT WINGLET LEADING EDGE ASSEMBLY. NO FURTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FSDR UPS05445839Panel · delaminatedLEFT WING LOWER PANEL DELAMINATED OUTBOARD OF NR 3 CANOE. UNDER NR 5 SPOILER ACT, AREA MARKED. COMPLIED WITH EO B747-5720-23353A EXCEPT FOR INSTALLING FASTENERS ON LE OF PANE. REMOVED TEMP REPAIR PANEL SH 1199928 DRILLED UP NEW PANEL. INSTALLED RIVETS AND LSDR VNAA0511019Skin · unknownDURING AN FAA RAMP CHECK, THE INSPECTOR REPORTED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WINGTIP. MAINTENANCE COMPLIED WITH EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. NO DAMAGE OR EVIDENCE OF A LIGHTNING STRIKE WAS FOUND. THE AIRCRAFT WAS RELEASED FSDR A6WA200540334Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 540CB HAS MINOR CORROSION ON OB 5 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP AND IB 4 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIRED TO LT WING LOWER PLANK SDR ASAA0540692Skin · dentedOKC - FOUND DENT IN RIGHT L/E 15 FEET OUTBOARD FROM WING ROOT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR 2. (M)SDR DHL2005803517Repair · crackedRT WING OB STUB WING LWR EXTERNAL SKIN REPAIR DOUBLER CRACKED 0.500 IN XW 485.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG. 1 PG. 3. REMOVED EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLESDR 2005UALA01305Skin · bird strikeBIRD STRIKE TO RIGHT OUTBOARD WING L/E. REPAIRED NR 10 LE SLAT NOSE SKIN PER SRM 57-43-01.SDR 05FDEA03878Repair · properRIGHT WING INBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN L/E AT STA XIFH 155 DIMENS. 2.5 X 2 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3.SDR 05FDEA03892Repair · unknownLT WING INBOARD FLAP FOUND DOUBLER 5" BY 5" ON UPPER SKIN AT STA XIFH 177. PERFORMED AGVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2SDR 05FDEA03890Repair · unknownLT WING INBOARD FLAP FOUND A FLUSH DOUBLER 3" BY 5.25" ON LWR SKIN AT STA XIFH 177. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-SDR 05FDEA03889Repair · properLT WING OUTBOARD FLAP LOWER SKIN FOUND A FLUSH DOUBLER 40" BY 34" WITH A EXTERNAL SPLICE BTWN STA XOF 605 AND XOF 639. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 57-10-00 FIG 7 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3.SDR 05FDEA03886Repair · properFOUND LT WING L/E EXT SKIN FOUND A FLUSH DOUBLER DIMENSIONS 3" BY 2" AT STA XORS 512. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P.SDR 05FDEA03884Repair · properRIGHT WING TIP WING FOUND DOUBLER REPAIR ON LOWER SKIN DIMENS 10 X 10 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3.SDR 05FDEA03877Repair · properRIGHT WING INBOARD VANE FLAP, FOUND DOUBLER ON UPPER SKIN AT STA XIFH 256 DIMENS 4 INCH DIAM. PERFORMED INSPECTION FOUND NO DELAMINATION IAW SRM 51-61-01 VOL 2 TAP TEST. PERFORMED INSPECTION ON REPAIR IAW SRM 51-71-00 VOL 2 AND FOUND IN COMPLIANCE WITH CRITESDR 05FDEA03874Repair · properRIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XOF 458 DIMENS 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.SDR 05FDEA03869Skin · unsecureACCESS PANEL LT WING P/N 525 AT FOUND SKIN UNGLUED. REBONDED AND REPAIRED PANEL IAW SRM 57-10-00 FIG 71 VOL 1 AND DWG ARB1111 DPS 1.07- 2 TYPE 2. FABRICATED PART IAW DETAIL PART TRAVELER N02362 AND SRM 57-10-00 FIG 71 VOL 1.SDR ABXA050367Access Panel · leaking12 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 7 NEAR ACCESS PANEL 505F. REMOVED 12 BLIND FASTENERS ON STRINGER NR 7 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.SDR ABXA050368Access Panel · leaking16 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 5 NEAR ACCESS PANEL 505F. REMOVED 16 BLIND FASTENERS ON STRINGER NR 5 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.SDR 05FDEA03802Skin · crackedLT WING L/E FOUND 1 CRACK 1'' LONG ON SKIN AT STA XORS 670. REPAIRED CRACK ON SKIN IAW SRM 57-10-00 FIG 68 SHT 1 AND IAW SRM 51-33-01 PAGE 34-47.SDR QXEA200501531Panel · damagedPDX: LT WING AND LADDER PLATE FOR FUEL PANEL 522BT REQUIRES REPAIR. MAINTENANCE REPAIRED IAW QX EA 6-57-394, NDTM PART 6, 51-00-02 AND RD 8/4-57-577.SDR TIM2005F00014Skin · damagedTHE FASTENERS WERE DISCOVERED TO BE WORKING INTO THE LOWER SKIN WHILE DOING AN INSPECTION OF THE WING. IT APPEARS THAT THIS WAS CAUSED BY NORMAL WING FLEX IN THIS AREA. (K)SDR LR7A05194Panel · crackedDURING C-7 CHECK PER SB 382-57-85, FOUND CRACK AT CENTER WING LOWER SURFACE PANEL NR 3 AT FS 597, LBL60. REPAIRED PANEL IAW TASK 0044, DRG SK382-57-298, MEA 382-57-05-099, NR 0744.SDR QXEA200501539Skin · damagedPDX: TWO BLENDED AREAS ON FWD APERTURE AND 2 BLENDED AREAS ON AFT APERTURE FOR WING PANEL 523AT ARE OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND QX EO 6-57-317 AND RD 8/4-57-577.SDR QXEA200501538Skin · damagedPDX: 2 AREAS ON FWD APERTURE AND 2 AREAS ON AFT APERTURE FOR WING PANEL 522CT ARE BLENDED OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND RD 8/4-57-577.SDR QXEA200501537Skin · damagedPDX: ONE AREA ON AFT APERTURE FOR WING PANEL 522AT IS BLENDED OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND RD 8/4-57-577 AND QX EO 6-57-317.SDR VNAA0511005Skin · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE ON DESCENT INTO YYZ. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT WINGLET. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE COMPLIED WITH DETAILED LIGHTNING STRIKE INSPECSDR QXEA200501523Skin · out of limitsPDX: 7 AREAS OF FWD APERTURE AND 2 AREAS ON AFT APERTURE FOR WING PANEL 522BT ARE BLENDED OUT OF LIMITS. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394, RD 8/4-57-577 AND QX EA 6-57-317.SDR QXEA200501527Access Panel · corrodedPDX: LT WING FUEL ACCESS APPERTURE FOR PANEL 522AT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NTDM PART 6, 51-00-02, Q400 SRM 51-25-40 AND QX EO 6-57-317.SDR QXEA200501526Access Panel · corrodedPDX: LT WING FUEL ACCESS APERTURE FOR PANEL 522BT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-21-10, Q400 SRM 51-25-40 AND QX EO 6-57-317.SDR 05FDEA03742Repair · unknown"WINGS BASIC EXTISTING EXTERNAL DOUBLER ON RT WING UPPER SKIN. COMPLIED WITH EA8-5710-92352 WINGS BASIC EXISTING EXTERNAL DOUBLER ON RT WING UPPER SKIN.SDR QXEA200501525Access Panel · corrodedPDX: LT WING FUEL ACCESS APERTURE FOR PANEL 522CT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-21-10 AND QX EO 6-57-317.SDR QXEA200501524Access Panel · corrodedPDX: LT WING FUEL ACCESS APERTURE FOR FUEL PANEL 523AT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-25-40 AND QX EO 6-57-317.SDR COMA0570118Skin · corrodedMINOR CORROSION ON WING PLANK AT FUEL PANEL ACCESS CUTOUT FOR PANEL 541AB/BB. ACCOMPLISHED MINOR REPAIR IAW BRAS EO 601R-57-7672.SDR 05FDEA03648Skin · bulgedFOUND RHW IN SPAR UPPER SKIN AT APPROX XORS 280 STRINGER 13 FOUND WITH SKIN BULGE. CARRIED OUT REPAIR AS PER EA 1-5720-87644.SDR IXXA05RNG098SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AT RIGHT WING LOWER SKIN OF CENTER EXTENDED LEADING EDGE AROUND WING STATION XFS 360.250, RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUNDSDR UPS05M45815Skin · corrodedINSPECTION TYPE:C2 LEFT WING TIP LWR SURFACE SKIN CRACKED .5 INCH LONG AND HAS HEAVY CORROSION AT XW 998. THE CORRODED AREA WAS TRIMMED OUT AND A FILLER AND DOUBLER WERE INSTALLED IAW SAA SK 270-894256 UPS ENG FILE MD11-57-20035, BOEING MSG 1-139605558-2 BOEISDR IXXA05RNG097SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON UPPER SKIN AT CENTER EXTENDED LEADING EDGE AROUND STA XW 257.500-LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRSDR 05FDEA03598Panel · crackedRT WING UPPER LE PANEL 6-7830-7-5007-402 HAS 1 EA CRACK APPROX 3.5" LONG ON IB LE REF N00123. REPAIRED APPROX 3.5 CRACK ON RT WING UPPER LE PNL 6-7830-7-5007-402 USING EPOXY RESIN AND GLASS OVERLAY IAW A310 SRM 51-77-11 PAR 4D.SDR QXEA200501694Doubler · corrodedYYC - DURING C3 CHECK, LEFT WING LOWER SURFACE AT STATION 38, LOWER WING PLANK DOUBLER LEADING EDGE HAS SURFACE RUST. REMOVED RUST IAW CRJ-700 SRM 51-21-06-001-001-A01. RESTORED FINISH.SDR QXEA200501647Skin · damagedYYC - DURING C3 CHECK, LEFT WING UPPER SURFACE AT STATION 231.23 HAS 2 RIVET HEADS MISSING. REPLACED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01.SDR QXEA200501615Skin · chafedYYC - DURING C3 CHECK, RIGHT WING UPPER LEADING EDGE SKIN HAS A CHAFED AREA FROM WS 178. MAINTENANCE BLENDED AREA IAW CRJ-700 SRM 57-41-01-101-001-A01. FINISH RESTORED.SDR QXEA200501614Skin · damagedYYC - DURING C3 CHECK, RIGHT WING UPPER SKIN TRAILING EDGE OUTBOARD OF MULTIFUNCTION SPOILERS HAS LOOSE FASTENERS. MAINTENANCE REPLACED THE RIVETS AS REQUIRED IAW CRJ SRM 51-42-06-001-001-A01.
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