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 VNAA202405130019Doubler · corrodedCORROSION WAS FOUND ON AFTER ATG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS BTW STA: 1007. STG 25R TO 26R. TG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WERE REPLACED PEApr 18, 2024 · N574NN · Bombdr CL6002D15SDR IPXA2024052246418Skin · corrodedMAIN CABIN CTR WING BOX AREA HAS CORROSION ON R/H SIDE BETWEEN STA 1199 - 1219 AND 106 INCH. ACCOMPLISHED REPAIR PER EO-90345-REQ1 AND VT-SAA EA 011-5730-01-B0194, REV I/R.Apr 17, 2024 · N276UP · Doug MD11FSDR DALA2024041904577Frame · crackedSHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED ER/A 616797-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616797-14AD REV 0 THRU REV. 5. IT HAS Apr 17, 2024 · N353NW · Airbus A320212SDR YENA2024041800645Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FR 35 / STR 38-40R / DENTS-PERMANENT REPAIR; ACCOMPLISH REPAIR OF DENTS ON FWD FUSELAGE SKIN BETWEEN FR 35.3 - 35.4 & STGR 37R -39R IAW AEROMAN EA 53-0080-24 COVER & PART 1, AND AIBUS RDAF 81024769 / 2024 ISSApr 17, 2024 · N950JT · Airbus A321231SDR YENA2024041800644Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN BTW FR 35 TO FR 35.1 AND BTW STR 39L TO STR 40L AT LOWER FUSELAGE;(RESOLVED ON W/O: 1279338 TASKCARD: NR-00020) PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR 35 TO FR 35.1 AND BTW STR 39L TO STR 40L AT LOWER FApr 17, 2024 · N950JT · Airbus A321231SDR SWIA20240621416Skin · dentedADM# N742SK-8061(CRJ700) MULTIPLE DENTS AND SCRATCHES FOUND AT UPPER FUSELAGE SKIN JUST BEHIND COCKPIT BULKHEAD ON TOP OF ENTRANCE STORAGE COMPARTMENT JUST BEHIND FS 280 LH SIDE OF FUSELAGE. .765" LONG .0625 WIDE SCRATCH. 0.004" DEEP. 4" AFT OF FS280.2. 2" BELApr 16, 2024 · N742SK · Cndair CL6002C10SDR NACA2024041600001Skin · crackedFOUND CRACK INDICATION BELOW STRINGER 2R @ BS 400 + 1/38. FOUND INTERNAL NICK ON SKIN. REPAIRED NICK @ BS400 + 1 3/8 STR 2R PER NAC EO 737-53-0341-01 AEI EO 233-49Apr 16, 2024 · N360WA · Boeing 737330SDR DALA2024041804531Skin · damagedREF LOG #0286119: C/W ER/A 617263-14 REV ORIG. C/W ER/A 617263-14 REV ORIG SECTION II STEPS 1 AND 2. NO FURTHER DEFECTS NOTED. CUT OUT DAMAGED SKIN AND DRILLED REPAIR DOUBLER PER ER/A 617263-14 REV ORIG SECTION II STEP 3. C/W DVI OF DENTS REF STEP 4 SECTION IIApr 16, 2024 · N947AT · Boeing 717200SDR CALA2024041701115Skin · damagedNOSE FUSELAGE SKIN BETWEEN STA 333 TO STA 350 AND NEXT TO S23R WITH LIGHTNING STRIKE MARK. ACCOMPLISH PERMANENT REPAIR IAW B757-200 SRM 53-00-01-2R-28, REP AIR 28 FIG 202, NOSE FWD FUSELAGE SKIN, BETWEEN STA 333 TO STA S TA 350, AT S23R.Apr 16, 2024 · N17128 · Boeing 757224SDR SWAA2024041975440Skin · crackedMULTIPLE CRACKED HOLES @ STA 114.55<[01] ACCOMPLISHED CUTOUT OF DAMAGED HOLES IAW SRM 55-10-01-2R-1.;[02] PREFORMED HFEC ON SKIN PER BOEING NDT PART 6 51-00-00 PROCEDURE 23 NO DEFECTS FOUND AT SKIN CUTOUT;[03] ACCOMPLISHED PERMANENT REPAIR IAW SRM 55-10-01-2R-Apr 15, 2024 · N438WN · Boeing 7377H4SDR YENA2024041600622Doubler · corrodedDURING HEAVY MAINTENANCE: CORROSION ON DOUBLER AND MISSING COLLARS FOR ATTACHMENT OF WASTE SERVICE PANEL. LOCATED BTW STRG 27R/28R AND FR 88/89; REF: TOMX W/O 2527 N/R 00234 REPLACED DOUBLER IAW EMB190 SRM 51-41-02.Apr 15, 2024 · N329JB · Emb ERJ190100IGWSDR YENA2024041600615Finger Doubler · corrodedDURING HEAVY MAINTENANCE: CORROSION IN FWD FINGERPLATE LOCATED OVER STR 27R AND FR 77 AT INTERNAL STRUCTURE OF AFT CARGO DOOR CUTOUT; CORROSION IN FWD FINGER PLATE LOCATED OVER STR 27R AND FR 77 AT INTERNAL STRUCTURE OF AFT CARGO DOOR CUTOUT WAS REMOVED & REPLApr 15, 2024 · N329JB · Emb ERJ190100IGWSDR DALA2024041604490Skin · corrodedSHIP 180 AFT CARGO INTERNAL SKIN FOUND CORROSION AT STA1197+ 110 BETWEEN S33R TO S34R. CORRECTIVE ACTION: THE DAMAGE AREA REPAIRED AS PER PRI 566933-14 REV 0.COMPARED AND COMPLIED WITH ER/A 566933-14 (0294385)Apr 15, 2024 · N180DN · Boeing 767332SDR DALA2024041604482Skin · damagedEXTERNAL POWER DOOR CUTOUT AFT SIDE REPAIR CRACKED AND DAMAGED. REPAIRED EXTERNAL POWER DOOR CUTOUT AFT SIDE PER ER/A 617174-14 REV O.Apr 14, 2024 · N391DA · Boeing 737832SDR DALA2024041504403Skin · gougedPCS ANTENNA- EXTERNAL SURFACE OF THE UPPER FUSELAGE HAS GOUGES/ TOOLING DAMAGE IN SEVERAL AREAS WHERE THE ANTENNA IS MOUNTED. REPAIRED FUSELAGE SKIN PER A320 SRM 53-22-11-300-087. REQUIRES SUBSEQUENT INSPECTION.Apr 13, 2024 · N317US · Airbus A320211SDR SWIA2024053000412Skin · mechanic errorWHILE SHOOTING RIVETS FOR THE INCORPORATION OF SB 670-32-056 THE TECHNICIANS RIVET SET SLIPPED AND DENTED THE FUSELAGE JUST OUTBOARD OF THE LEFT AFT NLG WHEEL WELL CUT OUT. (C-CHECK RO 5/25/2024) REPAIRED DENT PER REO 670-53-11-1944 REV -- DATED 2024-05-10Apr 12, 2024 · N750SK · Cndair CL6002C10SDR JJBA20240418047Skin · cracked8 CRACKS SUSPECTED ON RH SKIN FR77-81 AND STR 3R-9R. SKIN REPAIRED WITH A DOUBLER ON RH REAR FUSE 2 AT FR 78 BTW STR 5R-7R AND 6 BUSHINGS ON RH REAR FUSE SKIN AT FR 77 & 79 BTW STR 3R-9RApr 12, 2024 · N14186 · Emb EMB145XRSDR JJBA20240418046Skin · cracked8 CRACKS SUSPECTED ON LH SKIN FR77-81 AND STR 3L-9L. 9 CRACKS FOUND. SKIN REPAIRED WITH A DOUBLER ON LH REAR FUSE 2 AT FR78 BTW STR 5L-7L AND 7 BUSHINGS ON LH REAR FUSE 2 SKIN AT FR 77,79 & 80 BTW STR 3L-9LApr 12, 2024 · N14186 · Emb EMB145XRSDR NACA2024041200001Skin · crackedPOSSIBLE SKIN CRACK FOUND AT STATION 1210 STRINGER 37R. CUTOUT DAMAGE, INSTALLED REPAIR DOUBLER IAW NAC EO 767-53-004Apr 12, 2024 · N565NC · Boeing 7673BGSDR YENA2024041600608Access Panel · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR BARREL / FR 75-76 AND STGR 32-36LH / WASTE ACCESS PANEL CUTOUT DOUBLER / CORROSION - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 12, 2024 · N519JB · Airbus A320232SDR FDEA202404120457Skin · damagedDURING HMV 1 AT INDY, A PRIOR LIGHTNING STRIKE WAS DISCOVERED AND ONE FASTENER LOCATION AT STA 452, ON STRINGER 30L WAS BLENDED TO 0.040 THICK FROM A 0.063 MATERIAL THICKNESS AT THIS LOCATION. THIS AREA WILL BE REPAIRED WITH A SRM 53-00-01-2R REPAIR 29 DOUApr 12, 2024 · N297FE · Boeing 76732LFSDR DALA2024041504422Angle · corrodedCORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00072: CORROSION LEVEL 2. FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 FIG 201. (LApr 12, 2024 · N988AT · Boeing 717200SDR DALA2024041504441Skin · damaged(LOG 0290573) DURING ROUTINE INSPECTIONS, DAMAGE WAS FOUND COMMON TO AN EXISTING REPAIR ON THE AFT EDGE OF THE EGPR CUTOUT DOUBLER, INSTALLED PER DAL ER/A 467662-14. DAMAGE REPAIRED PER ERA 617174-14.Apr 12, 2024 · N391DA · Boeing 737832SDR DALA2024041304397Skin · damagedAIRCRAFT 3094, LIGHTNING STRIKE DAMAGE FWD FUSELAGE 52" ABOVE COPILOTS FIXED WINDOW. APPROX. 1.3" AFT OF FRAME 11, STA 5794. 4"X5.3" HOLE. CORRECTIVE ACTION: REMOVED DAMAGE PER A321 SRM 53-11-11-300-041, PERFORMED HFEC AT CUT OUT PER A321 SRM 53-11-11-300-041.Apr 12, 2024 · N394DX · Airbus A321211SDR JR2R20240412748Skin · damagedFUSELAGE SKIN AT FR34 STR17R HAS DRILL START UNDER FWD WING TO BODY FAIRING LANDING. REPAIREDApr 12, 2024 · N87337 · Emb ERJ170200LRSDR SWI2024F00461Skin · corrodedFORWARD BAGGAGE BAY DOOR SURROUND LOWER INNER SKIN CORRODED BETWEEN JOINT PLATES FS519.64 - FS562.64, STGR25L (MARKED) (C-CHECK RO 5/28/2024) BLENDED-OUT CORROSION, INSTALLED (41 EA) NEW FASTENERS AND RESTORED FINISH REWORKED AREAS AT FORWARD BAGGAGE BAY Apr 11, 2024 · N692CA · Cndair CL6002D24SDR SWI2024F00459Skin · damagedFORWARD BAGGAGE BAY FORWARD DOOR SURROUND LOWER INNER SKIN HAS EDGE DAMAGE AT THE FORWARD AND AFT DOOR HINGE. (MARKED) (C-CHECK RO 5/28/2024) BLENDED OUT EDGE DAMAGE ON FWD BAGGAGE BAY FWD DOOR LOWER INNER SKIN AT FWD AND AFT DOOR HINGE REF CRJ 900 SRM 51Apr 11, 2024 · N692CA · Cndair CL6002D24SDR SWI2024F00446Skin · corrodedFORWARD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN HAS CORROSION FS562.36 STGR25L - STGR19L. (MARKED) (C-CHECK RO 5/28/2024) REPAIRED FWD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN IAW REO 690-53-31-830 REV. -- DATED 2024-04-22. COMPLIED WITH SKYWEST TASK CARDApr 11, 2024 · N692CA · Cndair CL6002D24SDR HNAA2024051400391Skin · crackedE031667 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 79. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 79 STR 3L-4L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303Apr 11, 2024 · N653AE · Emb EMB145LRSDR HNAA2024051400390Skin · crackedE031665 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUNDRIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 4L-5L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303Apr 11, 2024 · N653AE · Emb EMB145LRSDR HNAA2024051400389Skin · crackedE031613 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 80. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 80 STR 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302Apr 11, 2024 · N653AE · Emb EMB145LRSDR HNAA2023051400388Skin · crackedE031612 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 78. ABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 78 STR 4R-5R AND 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302Apr 11, 2024 · N653AE · Emb EMB145LRSDR HNAA2024051400387Skin · crackedE031611 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 5R-6R IAW EMB 145 SRM 53-32-01. ITEM 9, FIGURE 213 AND EO1-53-24-0302Apr 11, 2024 · N653AE · Emb EMB145LRSDR JJBA20240418051Skin Splice · corrodedRH SKIN SPLICE BTW FR 23-24 AND STR 19-20 FOUND CORRODED. CIRCUMFERENTIAL STRAP SPLICED ON CENTER FUSE 1 & 2 BTW FR 23-24 AND BTW STR 20L-19RApr 11, 2024 · N14186 · Emb EMB145XRSDR SWAA2024041773611Access Panel · looseACCESS PANEL 192DR LATCHES LOOSE<[01] 01 - REMOVED AND REPLACED PER [AMM 52-48-42-400-802-NG (ENVIRONMENTAL CONTROL SYSTEMS (ECS) HIGH PRESSURE DOOR - INSTALLATION - PERMANENT)]Apr 11, 2024 · N938WN · Boeing 7377H4SDR YENA2024041600605Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION: CORROSION: FUSELAGE SKIN FR81-82 STR27-28R; (RESOLVED ON W/O: 1300462 TASKCARD: NR-00020) DEEMED OUT OF LIMITS IAW SRM 51-12-01, 51-10-03, AND 53-23-01/AD51. ACCOMPLISHED REPAIR FUSELAGE SKIN FR81-82 STR27/28R IAW SRM 53-23Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600600Doubler · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION CPCP FINDING, CORROSION ON DOUBLER LOCATED BTW FR88/FR89 AND STGR 28R/25R AT AFT CARGO COMPARTMENT; REF.TOMX WO N249JB/2525/E190/BRIDGE N/R 00102-DOUBLER WAS REPAIRED PER EMB190 SRM 53-23-60/REP 51P.REPAIR INSPECTIOApr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600572Skin · mechanic errorDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / UPPER SKIN ABOVE WINDSHIELD FRAME BTWN STGR 4R-5R / MISDRILLED HOLES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600568Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / SKIN BETWEEN FR82-84 & STGR 21L023L / DENT - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600551Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / LOWER SKIN / STGR 29R / FR 89-90 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600539Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II / LOWER SKIN / AT STR 29R BETWEEN FR73 – FR74 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600536Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN / BTW FR 23-24 & STGR 15L-16L / PREVIOUS DOUBLER / DENT - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600531Skin · gougedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER SKIN / BTWN FR20-21 & STR 27LH-28LH / GOUGES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600524Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FWD LOWER SKIN BETWEEN FR1-7 & STGR 24R-25R AND 24L-25L / HAIL DAMAGE - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600523Skin · unknownDURING HEAVY MAINTENANCE: FUSELAGE- FWD/ EXTERNAL SKIN FR22 STGR 24L-25L/ DENTTEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600519Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR BARREL / FR 75-76 AND STGR 32-36LH / WASTE ACCESS PANEL CUTOUT DOUBLER / CORROSION - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR JJBA20240415040Skin · corrodedCORROSION FOUND ON INNER SKIN UNDER FR 67 BTW STR 21L-21R. SKIN REPAIRED WITH A DOUBLER AT FR 67 BTW STR 20L-20R. CORROSION LEVEL 1.Apr 11, 2024 · N14186 · Emb EMB145XRSDR DALA2024041204360Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0273: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PERApr 11, 2024 · N996AT · Boeing 717200SDR EE4Y2024041119894Skin · corrodedDURING THE INSPECTION ACCORDING TO ALLEGIANT WORK CARD: 532180-01-2-001, THE FASTENER HEADS OF THE EXISTING EXTERNAL DOUBLERS WERE FOUND WITH CORROSION AND AFTER REMOVAL WERE FOUND ELONGATED HOLES. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND THE CORRODED AREA WAS Apr 11, 2024 · N297NV · Airbus A320214SDR HNAA2024052200432Skin · cracked53-2021 2 CRACKS BTW STR6R-8R AND FR77-78. REPAIRED IAW EO1-53-24-0247Apr 10, 2024 · N664MS · Emb EMB145LR
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