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 DHL2008F00008Skin · crackedLT WING UPPER LEADING EDGE WS 507 AFT CORNER OF HOOK CUT OUT IS CRACKED. REMOVED HOOK SEAL IAW B727 SRM 51-30-2. STOP DRILLED CRACK DIMENSION .250 IAW B727 SRM 51-10-1. CUT OUT STRAP DIMENSION 7.875" X 1.875" IAW B727 SRM 57-30-4 FIG 9. FABRICATED PLATE REJun 10, 2008 · N750DH · Boeing 7272M7SDR QXEA200800640Skin · corrodedPDX C4 CHECK FUEL PANEL 524AT APERTURE HAS SLIGHT CORROSION AROUND SCREW HOLES. CLEANED LIGHT CORROSION USING SCOTCH BRITE PAD AS PER -8 400 RD 8/4-57-445 PG 1 THRU 4 STEP 1 THRU 3. MAX MAT REMOVED .002" WITHIN LIMITS PER D8-400 RD8/4-57-445. HFEC INSPECTEDJun 9, 2008 · N424QX · Bombdr DHC8402SDR IXX2008F00082Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00081Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00072Skin · misrepairedDURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00068Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OTBD SLOT VANE LEADING EDGE AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CJun 9, 2008 · N721CX · Doug DC872FSDR IXX2008F00061Skin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WIND OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEWJun 9, 2008 · N721CX · Doug DC872FSDR 08FDEA02154Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3, MEASURING 4.0 IN BY 4.7 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON RT WINJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02141Panel · chafedLEFT WING INBD LOWER L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW DC/MD-10 SRM 57-00-01; VOL I; FIG 1-A. ORIGINAL MATERIAL THICKNESS IS 0.090 IAW DC/MD-10 SRM 57-31-01; VOL III; FIG 1. MATERIAL LOSS IS 0.028. REMAINING THICKNESS IS 0.062. FOUND TO BE OUTJun 3, 2008 · N357FE · Doug MD1010FSDR 08FDEA02135Panel · delaminatedLEFT WING L/E PANEL 6220, CORNER SKIN DISBONDED REPAIRED PANEL 6620 REF SRM 51-20-9 PAR 3D AND 7 PG 3-11 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG1, THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 3, 2008 · N487FE · Boeing 727227SDR 08FDEA02131Skin · damagedFOUND 2 NICKS ON TOP SKIN C 46-47, TRACK 4-5 RT REPAIR PEFORMED BY SMOOTH BLEND OUT, SPOTFACING AND NDT FOR CRACK FREE CONDITION IAW RAS 70507169/004/2008, APPROVED BY EA 6-5710-120053.Jun 3, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA02090Panel · chafedLEFT WING INBD LOWER L/E PANEL 516 DB IS CHAFED AT THE CONTACT SURFACE. REMOVED PANEL. BLENDED OUT CHAFFED AREA. FABRICATED; PRIMED & BONDED THE REPAIR DOUBLER IAW SRM 57-00-01 VOL II PG 31 & EA 8-5720-118511. EDGE SEALED, PRIMED & PAINTED IAW SRM 51-7Jun 2, 2008 · N357FE · Doug MD1010FSDR 08FDEA02088Panel · chafedLEFT WING INBD LOWER L/E PANEL 518 FB IS CHAFING AROUND THE CONTACT SURFACE. REPAIRED LEFT WING INBD LOWER PANEL ARB 1268-23 BY FABRICATING AND BONDING THE PAN DOUBLER IAW FEDEX EA 8-5720-116990; TIMCO TPS - 1001, REV E, AND DAC DWG ARB 1268. FEDEX EA 8-5720Jun 2, 2008 · N357FE · Doug MD1010FSDR 08FDEA02086Skin · wornLEFT WING INBD FLAP HINGE PANEL 541 BR HAS A WORN AREA. REPAIRED BLENDED AREA BY REMOVING FINISH ON INNER SKIN AREA OF LEFT WING INBD FLAP HINGE PANEL 541 BR; FABBING A DOUBLER; HOT BONDING THE DOUBLER IN PLACE AND REFINISHING IAW DC/MD-10 SRM 51-71-00; VOLJun 2, 2008 · N357FE · Doug MD1010FSDR 08FDEA02082Skin · crackedCRACK FOUND QUANTITY 13 FASTENER HOLES ON RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 13 FASTENER HOLES CRACKED. ARJun 2, 2008 · N624FE · Doug MD11FSDR 08FDEA02081Skin · crackedCRACK FOUND QUANTITY 3 FASTENER HOLES ON LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND XORS=713.6. LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND XORS=713.6 03 FASTENER HOLES CRACKED. AREAJun 2, 2008 · N624FE · Doug MD11FSDR 08FDEA02093Panel · wornLEFT WING LOWER TRAILING EDGE PANEL NR 551 BB INBD UPPER EDGE IS WORN FROM FRETTING. REPAIRED LEFT WING T/E PANEL NR 551 BB BY REMOVING THE DAMAGED AREA, FABRICATING A NEW FILLER AND DOUBLER. PERFORMED BONDING, CURE AND SEALING IAW DC/MD-10 SRM 51-71-00; VOLJun 2, 2008 · N357FE · Doug MD1010FSDR GLBA20061109Skin · damagedMAJOR REPAIR - DURING ROUTINE MX INSPECTION A REPORT OF A FUEL LEAK WAS REPORTED ON THE LEFT LEADING EDGE NEAR THE FUEL BARRIER BOX AT WS 194.8 WING SKIN. ALSO REMOVED TO FACILITATE REPAIR AT WS 177.8 - WS 226.8. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED UJun 2, 2008 · N220GL · Beech 1900DSDR 08FDEA02077Skin Panel · gougedRIGHT WING T/E O/B FLAP NOSE SKIN TOP SIDE HAS GOUGE. REMOVED RIGHT WING T/E FLAP NOSE SKIN IAW SRM 51-40-02. RECEIVED NEW PART P/N 113N3500Y28. INSTALLED NEW SKIN IAW SRM 51-40-02.Jun 1, 2008 · N903FD · Boeing 7572B7SDR CALA0800510Skin · crackedLEFT WING LEADING EDGE SKIN UPPER SURFACE CRACKED AT THE NUMBER 3 SLAT ACTUATOR. REPAIRED CRACK AT LEFT WING LEADING EDGE AT NUMBER 3 SLAT ACTUATOR CUT OUT PER CONTINENTAL EC/RA 5720-02060 AND PACE EA644-57-001 CAL.May 31, 2008 · N17644 · Boeing 737524SDR QXEA200800594Skin · chafedRFD-C4 CHECK - CHAFING ON RT WING CUTOUT AT LEADING EDGE WS 220.00. BLENDED CHAFED AREA IAW REO 670-57-41-059. TREATED IAW CRJ-700 SRM 51-21-11. PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-06 AND 51-25-01. (S)May 30, 2008 · N610QX · Cndair CL6002C10SDR 08FDEA02092Skin · corrodedLT WING, WING TOP SKIN FOUND WITH CORROSION NEXT TO REAR SPAR, BETWEEN RIBS 27 AND 28. REPAIRED AS PER EA 6-5710-121647.May 28, 2008 · N721FD · Airbus A300B4622RSDR 08FDEA02011Skin · crackedRT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT TOP INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 28, 2008 · N529FE · Doug MD11FSDR 08FDEA02007Doubler · crackedLEFT WING, LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01, VOL. II. FABRICATED NEW RIB DOUBLER AS PER DRAWING ARB3954. INSTALLED NEW RIB DOUBLER AT LT WING LEADING EDGE AT XOS 667 AS PER SRM 51-33-01, VOMay 28, 2008 · N529FE · Doug MD11FSDR 08FDEA02006Skin · crackedLEFT WING ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER FOUND CRACKED AT STATION XOS 464 AND XOS 470. REPAIR CARRIED OUT AS PER SRM 57-10-00, FIG.43, VOL.I AND EA 1-5710-122715, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 28, 2008 · N529FE · Doug MD11FSDR P5CA0801565Panel · crackedLEFT WING INBOARD FIXED PANEL FORWARD OF THE INBOARD FUELING PANEL CRACKED 3 INCHES LONG. ACCOMPLISHED PART 1 OF EO 4457A142. STOP DRILLED CRACK AND APPLIED SPEED TAPE OVER AFFECTED AREA.May 25, 2008 · N451PA · Boeing 74746NFSDR UPS08M52372Doubler · crackedINSPECTION TYPE:2C HAIRLINE CRACK 2 PLACES ON RT WING TOP OF ANTI-ICE TELESCOPIC DUCT CUT OUT CORNER. REMOVED DAMAGE IN 2 PLACES, FABRICATED FILLERS AND DOUBLER AND INSTALLED IAW MD-11 SRM 57-10-00, 51-31-01, AND 51-21-01F.May 24, 2008 · N255UP · Doug MD11FSDR C2XA08TY052Skin · crackedLEFT WING SKIN CENTER CUTOUT AT I/B SPOILER HAS A CRACK. CUT OUT DAMAGE AREA, FABRICATED FILLER, DOUBLER AND TRIPLER. ALODINED, PRIMED AND PAINTED IAW EC 5740-01158. AIRCRAFT RELEASED AND RETURNED TO SERVICE.May 23, 2008 · N26545 · Emb EMB145LRSDR UPS08M52451Structure · crackedINSPECTION TYPE:2C LT WING OUTBOARD L/E FIXED PANEL, SLAT ANTI-ICE DUCT ACCESS CUTOUT AREA FOUND UPPER CORNER CRACKED. CUT OUT TWO EACH AREAS, FABRICATED 2 EA DOUBLERS AND FILLERS, AND INSTALLED IAW MD11 SRM 57-10-00, 51-35-01, 51-21-01, AND 51-21-02.May 22, 2008 · N280UP · Doug MD11FSDR DHL2008764519Skin · damagedSKIN DAMAGE ON LT WING T/E AT NR 2 SPOILER NR 3 HINGE CUTOUT. ROUTER OUT SKIN AT LT WING T/E NR 2 SPOILER NR 3 HINGE CUTOUT FOUND OUT OF LIMITS IAW B727 SRM 51-10-1 AND 57-20-1 FIG 2. FAB DOUBLER REPAIR WITH 7075-T6. DIMENSION: 4" X 7" AND PO 9006522 IAW B72May 22, 2008 · N764AT · Boeing 727264SDR 08FDEA01954Panel · delaminatedRIGHT WING PANEL 635 BL HAS DELAMINATION AND A PUNCTURE. REPAIRED PANEL BY FABRICATING A NEW INNER SKIN IAW E.A. 8-5720-118490 & TPS 1001, REV E. DURING POST CURE CLEAN UP FOUND 4 CRACKS IN THE PANEL. HEAT TREATED IAW TPS 1003, REV A. FABBED REPAIR DOUBLEMay 22, 2008 · N367FE · Doug MD1010FSDR 08FDEA01937Panel · corrodedLEFT WING FUEL TANK PLATE / PANEL 534 CT; INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION; NICKS & GOUGES. REMOVED DAMAGE FROM THE PANEL & FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; VOL I; PG 217. MACHINED A NEW 534 CT PANEL IAW DAC DWG ARB0872May 21, 2008 · N567FE · Doug DC1010FSDR 08FDEA01936Panel · corrodedRIGHT WING RUEL TANK TANK PLATE/PANEL 634 BT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVED CORROSION FROM THE FLANGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I; PG 217. MACHINED A NEW 634 BT PANEL IAW DMay 21, 2008 · N567FE · Doug MD1010FSDR 08FDEA01935Panel · corrodedRIGHT WING FUEL PLATE/PANEL 635 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVED DAMAGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL II, PG 217. MACHINED A NEW 635 AT PANEL IAW DAC DWG ARB0872, REV "AV". May 21, 2008 · N567FE · Doug MD1010FSDR 08FDEA01934Panel · wornLEFT WING FUEL TANK PLATE/PANEL 535 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS, GOUGES AND TWO FASTENER HOLES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I, PG 217. MACHINED A NEW PANEL IAW DAC DWG ARB0872, REMay 21, 2008 · N567FE · Doug MD1010FSDR 08FDEA01932Panel · corrodedLEFT WING FUEL TANK PLATE/PANEL 531 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED NEW FUEL PANEL IAW DAC DWG ARB0872, REV "AV".May 21, 2008 · N567FE · Doug MD1010FSDR 08FDEA01931Panel · corrodedRIGHT WING FUEL TANK PLATE/PANEL 633 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED NEW FUEL PANEL IAW DAC DWG ARB0872, REV "AV".May 21, 2008 · N567FE · Doug MD1010FSDR 08FDEA01929Panel · wornRIGHT WING TANK PLATE/PANEL 639 CB HAS ELONGATED FASTENER HOLE AND FOUND TO BE OUT OF LIMITS IAW DC/MD SRM 57-10-00, VOL I. MACHINED A NEW PANEL IAW DAC DWG ARB0975-33, REV "AY". FPI IAW DPS 4.707 AND DAC DWG ARB0975, REV "AY". NO CRACKS NOTED. APPLIED AMay 21, 2008 · N567FE · Doug MD1010FSDR UPS08M52448Skin · crackedINSPECTION TYPE:2C RIGHT WING OUTER ACCESS PNL LANDING HAS CRACK. CRACK BETWEEN UPPER AND LOWER HINGE. VIEWED WITH MIRROR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 SRM 57-10-00 FIG 18.May 20, 2008 · N280UP · Doug MD11FSDR 08FDEA02622Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING, RIB 4-5, AT SHROUD BOX TOP SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR INSTMay 19, 2008 · N721FD · Airbus A300B4622RSDR 08FDEA01879Skin · crackedFOURTEEN FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. REPAIR CARRIED OUT AS EA 1-5710-122451, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.May 19, 2008 · N590FE · Doug MD11FSDR 08FDEA01878Skin · cracked08 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-122452, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 18, 2008 · N590FE · Doug MD11FSDR HALA0800590Skin · damagedRIVETS SHEARED ON RIGHT WING FIXED T/E UPPER SURFACE (9). REMOVED AND REPLACED SHEARED RIVETS ON RIGHT WING FIXED T/E UPPER SURFACE PANEL IAW SRM 51-40-04-OG-O.May 16, 2008 · N581HA · Boeing 76733ASDR HALA0800589Panel · looseATB - ON CLIMB APPROX 16,000, A BANG SOUND WAS HEARD AND A/C AIRFRAME VIBRATION OCCURRED. SLOWED A/C FROM 330 KTS TO 270 KTS VIB DECREASED. ALL OTHER INDICATIONS NORMAL. RETURNED TO SEA. REDUCED SPEED TO 250 KTS IN DESCENT. F/A CONFIRMED BANG AND VIBRATIOMay 16, 2008 · N581HA · Boeing 76733ASDR 08FDEA01866Skin · dentedRIGHT WING NR 2 SLAT L/E HAS A DENT. CUT OUT DAMAGED AREA OF SLAT. FABRICATED DOUBLER AND FILLER IN REF TO DC/MD-10 SRM 57-10-00, FIG 43 VOL II. REMOVED RUB STRIP FROM THE NR 2 SLAT IAW DC/MD-10 SRM 51-35-01, VOL II. REMOVED NR 3 SLAT TRACK IN REF TO DC/MDMay 16, 2008 · N567FE · Doug MD1010FSDR 08FDEA01869Skin · crackedLT WING LEADING EDGE TELESCOPIC DUCT CUT OUT OUTBOARD UPPER CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 16, 2008 · N590FE · Doug MD11FSDR UPS08M52316Strap · crackedINSPECTION TYPE:2C RT LEADING EDGE FIXED SKIN SPLICE STRAP STA XORS 562 CRACKED. REMOVED, FABRICATED, AND INSTALLED SKIN SPLICE STRAP IAW MD-11 SRM 51-33-01, 51-21-01, AND DWG ARB3954-1.May 15, 2008 · N255UP · Doug MD11FSDR UPS08M52315Angle · crackedINSPECTION TYPE:2C RT WING LEADING EDGE SKIN SPLICE STRAP ANGLE CRACK XOS 475. REMOVED CRACKED ANGLE, FABRICATED ANGLE, AND INSTALLED IAW DWG ARM2931, MD-11 SRM 51-33-01, 51-21-01, AND 51-21-00.May 13, 2008 · N255UP · Doug MD11FSDR UPS08M52314Strap · crackedINSPECTION TYPE:2C LEFT FIXED LEADING EDGE SKIN SPLICE STRAP CRACKED STA XORS 683. REMOVED, FABRICATED, AND INSTALLED SKIN SPLICE STRAP IAW MD-11 SRM 51-31-01, 51-33-01, AND DWG ARB3954.May 13, 2008 · N255UP · Doug MD11FSDR 08FDEA01839Panel · chafedLT WING FUEL PANEL ASSY 550 AT CLAMP RING HAS AREAS OF FRETTING. REMOVED & REPLACED THE CLAMP RING IAW SRM 57-20-16.May 13, 2008 · N815FD · Airbus A310
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