JASC 5330

Service difficulty reports · 79,329

Reports filed under 5330 · Fuselage Main, 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 = '5330'
  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 DALA2024100909894Skin · dentedSHIP 693 IN REFERENCE TO NRC 00036: DENT (1 EA) ON FUSELAGE SKIN BWT STA. 1941 TO 1963 AND BTW S-3L TO S-6L AT AFT FUSELAGE BODY SECTION 48 "DENT #4; A=850" Y=0.050" A/Y=17. AREA IS OUT OF LIMITS PER B757-200 SRM 53-80-01-1A AD. CORRECTIVE ACTION: SUMMARY OF NOct 5, 2024 · N693DL · Boeing 757232SDR CALA2024100702593Panel · corrodedCORROSION VACCUME WASTE TANK PAN ASSY INNER SKIN AT LOWER OF DRAIN AND THE AFT LOWER CORNER REF AAR N/R 9909822 REMOVED VACUUM WASTE TANK PAN ASSY AND INSTALLED NEW VACUUM WAST E TANK PAN ASSY P/N 146A7401-21 AS PER SRM 51-40-02-0G-0 AND BOE ING DWG 146A7400 SOct 5, 2024 · N37408 · Boeing 737924SDR SWI2025F00090Skin · scratchedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA77491-690-53-21-1499 170PQ MXCODEID74254-PR - FOUND SCRATCH DAMAGE JUST AFT OF MCD 3/32" AFT OF FS 349 AND 3/16" ABOVE STGR 6L. COMPLIED WITH REO 690-53-21-1499 REV A DATED 2024-04-29. PERMANENT REPAIR DUE WITHIN 695Oct 4, 2024 · N170PQ · Cndair CL6002D24SDR R61A2024102700486Skin · damagedREAR FUES FR100 STR STR 21R-23R FOUND LIGHTNING STRIKE ON EXTERNAL SKINOct 4, 2024 · N864RW · Emb ERJ170100SESDR FDEA202410041421Skin · crackedACCIDENTAL DAMAGE BY FOD AT LH FUSELAGE STA 1175, BETWEEN STGR 10-11, REPAIR AS REQUIRED ACCIDENTAL DAMAGE BY FOD AT LH FUSELAGE STA 1175, BETWEEN STGR 10-11 WAS REPAIRED IAW E.A.#: H-5330-T0380846 AND SRM 53-00-01-2R REPAIR 29 FIGURE 201 SHEET 1-12 TABLE Oct 4, 2024 · N147FE · Boeing 7673S2FSDR CALA2024100702594Skin · corrodedINITIATE DIP PER ECRA 5331-03128 STEP 2, A/C 0408, FUSELAGE SKIN STA 847 ? 867, STR 24L ? 26L INTERIM REPAIR. BETWEEN STA 847 - 867, STR 24L - 26L ON AIRCRAFT N37408 IN 5331-03128. ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA AFTER THE ACCUMULATION OFOct 4, 2024 · N37408 · Boeing 737924SDR CALA2024100702572Skin · no discrepancyREMOVE UPPER FUSELAGE SKIN FR1-3 TO F.O.M. (CONTINUITY FITTING R EPLACEMENT). REMOVED AND REINSTALLED FUSELAGE UPPER SKIN TO FOM CONTINUITY FI TTING REPLACEMENT AT FR1-FR3 IAW A319 SRM 51-72-11-911-001.Oct 4, 2024 · N882UA · Airbus A319132SDR JR2R20241004191Doubler · corrodedINSIDE WASTE WATER CUTOUT CORRODED. REPAIRED.Oct 4, 2024 · N87303 · Emb ERJ170200LRSDR SWIA202411271292Skin · gougedLOWER EXTERNAL SKIN PANEL HAS 4 DEEP GOUGES FORWARD AND AFT OF FS977 (C-CHECK RO 11/26/2024) COMPLIED WITH ALL STEPS OF SOLUTION 2 OF REO 670-53-00-290 REV - F 2019/04/26. LEAK CHECK GOOD, COMPLIED WITH TASK CARD 51-900-1002-SKYOct 3, 2024 · N706SK · Cndair CL6002C10SDR AALA202411066097Skin · corrodedAIRCRAFT WAS GROUNDED: LARGE AREA OF SEVERE CORROSION APROX 2" X 1" AT BS 887 STR 27L. RIVET HEAD MISSING AN D SKIN CRACKED APROX 1" LENGTHWISE OF AC. MX FOUND CORROSION ON FUSELAGE SKIN UNDER SPLICE STRAP AT BS 887, FROM S24L TO S27R. ACCOMPLISHED DOUBLER REOct 3, 2024 · N922AN · Boeing 737823SDR CALA2024102300906Skin · damagedREF LP 9356893 LIGHTING STRIKE FOUND ON FRAME 54 BETWEEN STR 36L AND STR 37L LENGHT IS .2 BY WIDE 1.7 IAW SRM 53-21-11-283-004 FIG 1,SPEED TAPED DISCREPANT AREA AS PER SRM 51-75-12-911-022. UNLOCKING ACCOMPLISHED GVI OF REMOVED DAMAGED AREA PER SRM 53-21-11-30Oct 3, 2024 · N433UA · Airbus A320232SDR IPXA2024101240887Strap · corrodedREMOVED AFT LWR. SKIN STRAP AT STA. 1885.20 FOR ACCESS. FOUND CORROSION ON LWR. SKIN STRAP. INSTALLED REPLACEMENT SKIN PLATE ON AFT LOWER FUSELAGE 313AL CUT OUT STA. 1885.20 REF B757 SRM 51-40-02-0G-0. PRODUCTION AUDIT C/WOct 3, 2024 · N453UP · Boeing 75724APFSDR CALA2024100900798Skin · damagedREF LP 9356893 LIGHTING STRIKE FOUND BETWEEN FRAME 31 AND FRAME 32. BETWEEN STR 39L AND 38L. LENGHT IS .5" BY WIDE .5"... CLOSEST FASTNER IS 28"STRIKE IS 6.8" FROM FR 31. FOUND STRIKE TO BE BURNED THRU SKIN. IAW SRM 53-21-11-283-004 LOCKING LOG PAGE FOR FERRY Oct 3, 2024 · N433UA · Airbus A320232SDR DALA2024100709752Skin · corrodedSHIP 693 CORROSION ON INNER SKIN ON FWD CARGO DOOR CONTROL PANEL AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00051: CORROSION ON INNER SKIN BEAR STRAP ON FWD CARGO DOOR CONTROL PANEL AT FUSELAGE WAS REPAIRED PER ER/A 621144-14 REV. ORIGINAL SECTION I: PERMAOct 3, 2024 · N693DL · Boeing 757232SDR CALA2024100702569Skin · damagedREF ELB LP 5384043 PERFORM PART 3 OF ECRA 5370-01085 REF AAR N/R 9909483 PERFORMED CAT B REPAIR TO DAMAGE FUSELAGE SKIN I.A.W ECRA 5331-03126 PART 1 PARA 1 BETWEEN ST907 TO 947 AFT WATER SERVICE AREA REVISED LP 5384043 AND DIP MADE ON LP 9446226 WORK ACCOMPLISOct 3, 2024 · N37408 · Boeing 737924SDR R61A2024100100442Skin Panel · damagedACFT WAS PARKED AT THE GATE. THE JETBRIDGE MADE CONTACT W/ FUSELAGE AT AN ANGLE W/ THE BACK CORNER OF THE JETBRIDGE MAKING CONTACT W/ ACFT FIRST CAUSING ACFT TO HEEL. THE NOSE WHEELS HAD TURNED TO THE RIGHT AFTER THE JETBRIDGE HIT. REPAIRED LH FUSELAGE SKIN BEOct 3, 2024 · N217JQ · Emb ERJ170200LRSDR VNAA2024100300010Skin · corrodedCORROSION NOTED AROUND WATER DRAIN HOLES EXTERNAL SKIN AT APPROX. FS946.00 BETWEEN STRG26L-STRG26R. BLENDED CORROSION ON EXTERNAL SKIN AROUND WATER DRAIN HOLES AT FS946.00 BETWEEN STGR 26L - 26R REF CRJ700 SRM 51-21-06-001-001-A01 AND FOUND ACCEPTABLE TO ENGINOct 3, 2024 · N708PS · Cndair CL6002C10SDR VNAA202410030009Skin · corrodedCORROSION NOTED ON EXTERNAL SKIN AROUND DOME NUT SCREW HOLE FOR R/H196DR BODY FAIRING BETWEEN FS923-FS939. REPAIRED AREA AND COMPLIED WITH ALL STEPS REO 670-53-51-306 REV-- DATEOct 3, 2024 · N708PS · Cndair CL6002C10SDR VNAA202410030008Skin · scratchedSCRATCHES NOTED ON EXTERNAL SKIN AT APPROX FS847-FS977 BTWN STRG17L-20L, MATING SURFACE FOR L/H BODY FAIRING 196DL AND 195AL. REPAIRED AREA AND COMPLIED WITH ALL STEPS OF REO 670-53-00-748 REV-- DATED:Oct 3, 2024 · N708PS · Cndair CL6002C10SDR VNAA20241103022Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH/RH TO STGR 21LH/RH. DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGHT VENTRAL FIN FAIRING BTW FS Oct 2, 2024 · N587NN · Bombdr CL6002D15SDR IPXA2024100218767Skin · damagedE/E CUTOUT EXISTING TEMP REPAIR ACCOMPLISH REPAIR PER VT-SAA EA 011-5330-01-B0283, REV. I/R, PRIOR TO FURTHER FLIGHT. MAJOR REPAIR.Oct 2, 2024 · N293UP · Doug MD11FSDR VNAA202410080007Skin · damagedFORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE INNER SKIN HAS CORROSION AROUND FASTENERS IN MULTIPLE AREAS FS533.00 - 581.00 STGR 26L - 25L. REMOVED CORROSION ON FWD BAGGAGE BAY DOOR SURROUND STRUCTURE, INNER SKIN REF SRM 51-21-06-001-001-A01 AND FOUND ACCEPTAOct 2, 2024 · N708PS · Cndair CL6002C10SDR DALA2024101009934Skin · dentedSHIP 5807 FUSELAGE SKIN DENTS AT STA 610, S-17L, REPAIR. ER/A 500142-14AD. CORRECTIVE ACTION: REF ERA 500142-14AD. (0586612)Oct 1, 2024 · N587NW · Boeing 757351SDR DALA2024100409703Skin · damagedSHIP 5808 FUSELAGE/ CROWN SKIN/ FS 780 + 85, S-4R / LIGHTNING STRIKE DAMAGE. ER/A 516342-14AD REV B. CORRECTIVE ACTION: REF ERA 516342-14. (0587206)Oct 1, 2024 · N588NW · Boeing 757351SDR CALA2024100402563Skin · crackedFOUND CRACK AND CORROSION EXFOLIATION AT THE FUS EXTERNAL SKIN STA 917 BTW STRG 21L AND STRG 22L AT BOTTOM HALF OF THE VACUUM WASTE VENT CUTOUT REQUIRE REPAIR PER SRM 53-70-01-2R-3. (REF: AAR NR 1000021409) ION, INSPECTION THRESHOLD 50,000 CYCLE METHOD (LFEC)Oct 1, 2024 · N76526 · Boeing 737824SDR CALA2024100302544Skin · corrodedFOUND CORROSION ON OUTER SKIN LOWER SIDE LOCATED UNDER LAV SERVICE PANEL. BETWEEN STA 884 AND STA 867 AND STR 23L AND 26L. PART 2 OF EC/RA 5331-03125 ON OR BEFORE 24 MARCH 2026. ?ON THE FUSELAGE SKIN BETWEEN BS 847-867 AT S-25 COMMON TO LAVATORY SERVICE PAN, AOct 1, 2024 · N28457 · Boeing 737924ERSDR DALA2024100209635Skin · cracked(LOG 0587433) CRACK ON INTERNAL SKIN STA 1121 TO 1129 BTW S4L AND S5L AT AFT ACCESSORY COMPARTMENT. INTERNAL SKIN STA 1121 TO 1129 BTW S4L AND S5L AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ERA 620803-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.Oct 1, 2024 · N3733Z · Boeing 737832SDR 21GA20241001019Skin · crackedDURING HEAVY CHECK, FOUND CRACKED SKIN CRACKED 1 INCH FWD AND 2.5 INCHES AFT OF IAI PG STRAP. REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC EO #24151-3.Oct 1, 2024 · N999YV · Boeing 767241SDR 21GA20241001018Skin · dentedDURING HEAVY CHECK, A DENT AND CREASE WERE FOUND AT FUSELAGE SKIN STA 1279.53 BETWEEN STR 33R AND 35R. WAS REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC. EO # 24151-2.Oct 1, 2024 · N999YV · Boeing 767241SDR 21GA20241001017Skin · dentedDURING HEAVY CHECK, DENTS AND CRACKS WERE FOUND BETWEEN FUSELAGE SKIN STA 347 AND 390 AT STR 19R TO 21R. WAS REPAIRED IAW FLIGT VEHICLES CONSULTING INC. EO# 24151-1.Oct 1, 2024 · N999YV · Boeing 767241SDR DALA2024100109577Skin · dentedSHIP 3303 DTE, ER/A 614093-14 REV B REQUIRES STAGE 3 DTA APPROVAL. A330-300 / FUSELAGE / SKIN / FWD CARGO DOOR SURROUND / FR 20A, S -40R / DENT DAMAGE. CORRECTIVE DAMAGE: COMPLIED WITH ERA. (0585118)Sep 30, 2024 · N803NW · Airbus A330323SDR SWAA2024102943155Access Panel · crackedLOWER FUSELAGE MID FWD ACCESS PANEL 191D INNER SURFACE SKIN 3EA CRACKS MKD DOT<[01] ACCOMPLISHED REPAIR AT PANEL #191D PER B737 SRM 53-30-70-2R-1; SRM 51-70-04-2R-1 AND TOP COATED REPAIR AREA PER AMM 51-21-73-370-803;[02] VERIFIED STEP 1Sep 29, 2024 · N498WN · Boeing 7377H4SDR UIEA2024092400938Skin · crackedDOUBLER INSTALLED ON EMERGENCY LIGHT OF THE MCD SURROUND SKIN CIRCUMFERENTIAL SPLICE STA 654+22 AT AFT FASTENER ROW IN THE SECOND LOWER FASTENER HOLE WITH CRACK INDICATION.(<P>THE SECOND LOWER FASTENER HOLE WAS ENLARGE UP TO SECOND OVERSIZE AND WAS REPAIRED IASep 29, 2024 · N1619A · Boeing 7673Y0SDR UIEA2024092400939Skin · crackedAT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER ONE HOLE WITH CRACK INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK.(<P>HOLE INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK. CRACK WAS REPAIREDSep 29, 2024 · N1619A · Boeing 7673Y0SDR UIEA2024092400940Skin · crackedAT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER TWO HOLES WITH CRACK INDICATION ON FUSELAGE SKIN APPROX 10 O´CLOCK.(<P>AT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER ON FUSELAGE SKIN APPROX 10 O´CLOCK DAMAGES WERE REPAIRED IAW FVCI #24153-2 A FAA FORM 8110-3 (09/20Sep 29, 2024 · N1619A · Boeing 7673Y0SDR UIEA2024092500949Access Panel · wornSYST LH HYD BAY, (ACCESS PANEL: 437BL) INNER RIGHTSIDE, LOWER REAR CORNER AREA, PLATE-STRICKER WITH WORN.(<P>LOWER REAR CORNER AREA, PLATE ASSY WAS REPLACED SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0SDR IPXA2024092851725Skin · damagedFOLLOW ON ACTION, ON FUSELAGE SKIN DAMAGE AND STRINGER DAMAGE STA 1417 TO STA 1439 S-38R TO S-38L AFTER ADDITIONAL CUTOUT PERFORMED, FOUND SKIN AT AFT SIDE OF CUTOUT TO BE .063" THICK. OPENSep 28, 2024 · N377UP · Boeing 767300SDR REXA2024100700854Skin · chafedTHE OUTER LOWER SKIN IS CHAFED BETWEEN FS 897 AND FS 913 STGR 27. UPON FURTHER INVESTIGATION DAMAGE WAS FOUND TO BE ON AN EXISTING DOUBLER AT F.S. 897 - F.S. 913 INSTALLED TO ENDEAVOR EA CRJ953-11279 REV IR. DAMAGE WAS FOUND TO BE OUT OF LIMITS PER ENGINEERINSep 28, 2024 · N325PQ · Cndair CL6002D24SDR DALA2024100209623Skin · crackedSHIP 1806 HFEC INSPECTION FOUND 1EA CRACK UNDER THE 7TH RIVET OF THE STRINGER14 COUNT FROM FRONT TO BACK, THE LENGTH OF CRACK IS 0.3 INCH, AS MARKED. CORRECTIVE ACTION: REPAIRED AS PER B767-400 SRM 53-80-01 (0580491)Sep 28, 2024 · N830MH · Boeing 767432ERSDR DALA2024100209618Skin · corroded-AD- CORROSION ON UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL. SUMMARY OF NRC 00216: CORROSION LEVEL 2. UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL WAS REPAIRED PER PRI 620162-14 REV 8 AND ER/A 620162-14AD REV ORIGINAL SECTION I: PERMSep 28, 2024 · N951AT · Boeing 717200SDR DALA2024092909497Skin · ground damageAIRCRAFT 3518, RIGHT NOSE OF AIRCRAFT STRUCK BY CATERING TRUCK DAMAGE TO SKIN. CORRECTIVE ACTION: CUT AND REMOVED THE DAMAGED SKIN BETWEEN FR8 AND FR6, STGR 33 RH AND STGR 35 RH PER A350 ASR A350-A-53-11-61-00001-662A-A STEP 4A HEFC INSPECTED CUT OUT PER A350 Sep 28, 2024 · N518DZ · Airbus A350941SDR JR2R20240927456Doubler · corrodedFRAME 90 AT RBL 20 "TEXAS DOUBLER" CORRODED. REPLACEDSep 28, 2024 · N86311 · Emb ERJ170200LRSDR HNAA2024102101014Skin · cracked53-2339 FUSE SKIN CRACKED ABOVE FWD RH WINDSHIELD BTW FR12 -12A. REPAIRED IAW EO1-53-24-0618Sep 27, 2024 · N673AE · Emb EMB145LRSDR CALA2024100702578Skin · crackedAD 2008-16-12 - EA 5300-01986 REV A OP 004 - 1EA FASTENER HOLE FOUND 2EA CRACK APPROX 0.125" AND 0.060" IN LENGTH AT RH STA 2195.75 BETWEEN S6-S7 TRANSFER REF. NON-ROUTINE HX NRC WO.3766628. SKIN REPAIRED AS PER EA 5300-01986 REV A OP 010 RH STA 2195.75 STR 5Sep 27, 2024 · N771UA · Boeing 777222SDR CALA2024100702577Skin · crackedAD 2008-16-12 - EA 5300-01986 REV A OP 002 - 1EA FASTENER HOLE FOUND 3EA CRACK APPROX 0.125", 0.060" AND 0.060" IN LENGTH AT LH STA 2221.65 BETWEEN S9-10 TRANSFER REF. NON-ROUTINE HX NRC WO.3766615. SKIN REPAIRED AS PER EA 5300-01986 REV A OP 008 SKIN REPAISep 27, 2024 · N771UA · Boeing 777222SDR DALA2024100209616Skin · cracked-AD- CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH (FUS). SUMMARY OF NRC 00348: CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH WAS REPAIRED PER ER/A 619986-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 23-SESep 27, 2024 · N951AT · Boeing 717200SDR DALA2024093009526Bear Strap · damaged(LOG 0581058) DAMAGED BEAR STRAP 27R AT STA 312 RBL 10. ACCOMPLISHED ERA 583828-14 REV-B FOR DAMAGE FOUND ON PREVIOUS REPAIR TO FUSELAGE SKIN STA 312 STR 27R.Sep 27, 2024 · N848DN · Boeing 737932ERSDR FDEA202409271377Skin · crackedFUSELAGE SKIN STATION 585 #1 AIRCON PACK EXHAUST OUTLET CUTOUT SUSPECT CRACK. CRACKED FUSELAGE SKIN STATION 585 #1 AIRCON PACK EXHAUST OUTLET CUTOUT, REPAIR ACCOMPLISHED PER E.A.#: 1-5320-T0380781 P1. TITLE: FUSELAGE AUXILIARY STRUCTURE REPAIR FOR CRACSep 27, 2024 · N595FE · Doug MD11FSDR VNAA20241103006Skin · corrodedIN REFERANCE TO RC TRFKE001DESZ CORROSION ON INTERNAL SKIN CUTOUT SEAL SETTLEMENT AREA DOOR STRUCTURE AT MAIN AVIONICS COMPARTMENT. INTERNAL SKIN CUTOUT DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER 690-53-21-032 REV --.Sep 26, 2024 · N587NN · Bombdr CL6002D15SDR R61A2024102300476Skin · dented****MAJOR****REF DMI R1212594/1 DENT ABOVE CPTS DV WINDOW BTWN FR11-12 & STR 05L-06L DENTS ARE IN SAME BAY 15MM APART. MX REPAIRED IAW ETD2024-170-026800*****MAJOR*****Sep 26, 2024 · N638RW · Emb ERJ170100SE
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