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 HNAA2021050400167Skin · dentedDMT 23 DENT ON LH FUSELAGE BETWEEN FRAMES 58 AND 59 AND STRG. 7L AND 8L REPAIRED PER EO1-53-20-0126 WITHIN 1700 FLIGHT HOURS ACCOMPLISH A PERM. REPAIR....FABRICATED, PREPPED AND INSTALLED SERVICEABLE REPAIR DOUBLER AND FILLER ON LH FUSELAGE BETWEEN FR 58-59 ATApr 22, 2021 · N646AE · Emb EMB145LRSDR A6WA202105037766Skin · corrodedCORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L, 2.5Ï¿½L X 1.0Ï¿½W X .003Ï¿½D. ORIGINAL MATERIAL 0.045Ï¿½, LOSS 0.003Ï¿½ REMAINING 0.042Ï¿½. PERFORMED HFEC WITH NO INDICAApr 21, 2021 · N462AW · Cndair CL6002B19SDR A6WA202105037767Skin · corrodedCORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R, 4.0Ï¿½L X 5.0Ï¿½W X .005Ï¿½D. ORIGINAL MATERIAL 0.058Ï¿½, LOSS 0.005Ï¿½ REMAINING 0.053Ï¿½. PERFORMED HFEC WITH NO Apr 21, 2021 · N462AW · Cndair CL6002B19SDR JJBA20210420036Skin · crackedLH FUSELAGE FR 75 BTW STR 1-3, SKIN CRACKED. LH FUSE, FR 75 BTW STR 1L-3L SKIN REPAIRED.Apr 20, 2021 · N14179 · Emb EMB145XRSDR 2021F00120Skin · scratchedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SCRATCH ON RIGHT FUSELAGE SKIN SECTION 43. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A SCRATCH OF 0.004" DEPTH, 1.5" LENGTH ON RIGHT FUSELAGE SKIN SECTION 43 AT BS 500D + 12.5" AND RIGHT STRIApr 19, 2021 · Boeing 7378SDR A6WA202104287758Skin · dentedAFT FUSELAGE SKIN DENT FS 672.20+2 AND S23+3R ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS672.20+2 AND S23+2R IAW ASAP EA# AWAC CRJ253-01606 REV IR DATED 4/27/2021.Apr 19, 2021 · N462AW · Cndair CL6002B19SDR A6WA202104267757Skin · dentedAFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT AFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L IAW CRJ SRM 53-00-31 REPAIR #3 REV 38.Apr 19, 2021 · N462AW · Cndair CL6002B19SDR A6WA202104267755Skin · dentedAFT FUSELAGE SKIN DENT AT FS 691.0 STR 23+2L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FUSELAGE DENT AT FS 691.0 STR 23+2L TO ORIGINAL CONTOUR IAW ASAP EA# AWAC-CRJ253-01607 REV IR DATED 4/21/2021.Apr 19, 2021 · N462AW · Cndair CL6002B19SDR A6WA202104267756Skin · dentedAFT FUSELAGE SKIN DENT FS 636-638 STR 26+1.5 TO 26+3L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED 2 DENTS TO ORIGINAL CONTOUR AT FS636-638 STR 26+1.5 TO 26+3L IAW ASAP EA# AWAC CRJ253-01609 REV IR DATED 04/21/2021.Apr 19, 2021 · N462AW · Cndair CL6002B19SDR A6WA202104237754Skin · dentedAFT FUSELAGE SKIN DENT LH FS692.5 STR 23+4L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT LH FS693.5 AND STR 23+4L IAW ASAP ENGINEERING REV IR DATED 4/21/2021Apr 19, 2021 · N462AW · Cndair CL6002B19SDR A6WA202104237753Skin · dentedAFT FUSELAGE SKIN DENT AT FS580.0 AND STR L20+2.5. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS580 LEFT HAND AT STR 20+2.5, PERFORMED HFEC NO INDICATIONS NOTED. REPAIR WITHIN LIMITS REF ASAP EA# AWAC-CRJ253-01608 REV A DATED 4/22/2021.Apr 19, 2021 · N462AW · Cndair CL6002B19SDR KCSA202104191046Skin · damagedSKIN DAMAGE AT APPROX STR 37 L AND APPROX STA 750 ON EXTERNAL SIDEApr 19, 2021 · N700CK · Boeing 7474R7FSDR SWIA2021070759317Skin · gougedGOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R (C-CHECK RO 7/5/2021) REPAIRED GOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R REF REO 670-53-00-290 REV -F DATED 2019/04/26 SOLUTION 2 ALL STEPS COMPLIED WITH. COMPLIED WITH 51-900-1002-SKY RApr 18, 2021 · N612QX · Cndair CL6002C10SDR SWIA202158892Skin · dented*DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 265.00 - 250.00, STGR 24L - 23L. MARKED. (C-CHECK RO: 6/20/21) / REPAIRED DENT IN THE EXTERNAL SKIN BETWEEN FS 265.00 - 250.00, STGR 24L - 23L REF MHIRJ REO 670-53-11-1686 REV-- DATED: 2021-05-25. LEAK CHECK GOOD AApr 18, 2021 · N603SK · Cndair CL6002C10SDR HNAA2021051900213Skin · damagedPREVIOUS REPAIR OF FR 19 BETWEEN STGR. 2R-4R IS DAMAGED. RE-ACCOMPLISHED REPAIR OF FR19 BETWEEN STRINGER 2R - 4R IAW PIEDMONT EO1-53-21-0107.Apr 18, 2021 · N644AE · Emb EMB145LRSDR SWIA2021080960128Skin · corrodedEXTERIOR LOWER SKIN JUST AFT OF PNL 195 BB HAS CORROSION (C-CHECK RO 8/5/2021) REMOVED CORROSION ON EXTERIOR SKIN AFT OF PANEL 195BB IAW MHIRJ REO 601R-53-61-7653 REV -- DATED 2021-06-01 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED FApr 17, 2021 · N693BR · Cndair CL6002B19SDR AALA202105183796Skin · gougedAIRCRAFT IN BASE MAINTENANCE: EXISTING REWORK AT EXTERNAL SKIN OF FUSELAGE FOR A GOUGE, FR 53 + 1.0 INCHES AT S25L + 4.1 INCHES. REPAIRED SKIN PER SRM 51-73-00-801 AND EA 327397.Apr 17, 2021 · N523UW · Airbus A321231SDR AALA202105181758Skin · gougedAIRCRAFT IN BASE MAINTENANCE: EXISTING REWORK AT EXTERNAL SKIN OF FUSELAGE FOR A GOUGE, FR 53 +5.30 INCHES AT S25L + 3.50 INCHES. REPAIRED SKIN PER SRM 53-41-11-300-019 AND EA 327397.Apr 17, 2021 · N523UW · Airbus A321231SDR YENA2021042100256Finger Doubler · corrodedDURING HEAVY MAINTENANCE, CORROSION OVER FINGER PLATE ON AFT CARGO COMPARTMENT FR 77; CORROSION OVER FINGER PLATE ON AFT CARGO COMPARTMENT FR 77 WAS REMOVED BLEND OUT IS OUT OF LIMITS FINGER PLATE WAS REPLACED PER EMB -190 SRM 51-43-02 STEP 5 FIG 2 AND SRM 51-Apr 17, 2021 · N373JB · Emb ERJ190100IGWSDR P5CA2021041900098Skin · not reportedDEVIATION FOUND DURING PERFORM 747-8F SRM 53-00-01 REPAIR 1 ON FUSELAGE SKIN NEAR STA 680 BETWEEN S-31R AND S-33R.(<P>ACCOMPLISHED EI NO T2021A53M-1021 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Apr 17, 2021 · N855GT · Boeing 74787UFSDR DALA2021042002299Skin · damagedSHIP 5811 BURNED RIVET AT FS 230, A/C RIGHT, 5" OUTBOARD FROM BLO, 2" FWD OF FWD ELECRICAL BAY. CORRECTIVE ACTION: BLENDED PNL PER 757 SRM. (1784240)Apr 17, 2021 · N591NW · Boeing 757351SDR SWIA2021090360654Skin · chafedEXTERNAL SKIN CHAFED BETWEEN FS969.00 AND FS985.00 AT STRGR 27 (C-CHECK RO 8/31/21) REPAIRED EXTERNAL SKIN IAW MHI REO 670-53-00-661 REV.--, DATED 6/2/21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CApr 16, 2021 · N703SK · Cndair CL6002C10SDR SIMA20210416005Skin · crackedFUSELAGE SKIN HAS 4 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 79 BETWEEN STR 6R-7R. -C/A-REPAIRED SKIN AT FRAME 79 BETWEEN STR 6R-7R IAW SRM 53-32-01.Apr 16, 2021 · N668HH · Emb EMB145LRSDR SIMA20210416008Skin · crackedFUSELAGE SKIN HAS 13 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 77 BETWEEN STR 3L-7L. E854459, E854460, E854461, AND E854462-C/A-REPAIRED SKIN AT FRAME 77 BETWEEN STR 3L-4L IAW SRM 53-32-01.-REPAIRED SKIN AT FRAME 77 BETWEEN STR 4L-5L IAW SRM 53-32Apr 16, 2021 · N668HH · Emb EMB145LRSDR SIMA20210416007Skin · crackedFUSELAGE SKIN HAS 9 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 78 BETWEEN STR 5L-7L. (E854463, E854464) -C/A-REPAIRED SKIN AT FRAME 78 BETWEEN STR 6L-7L IAW SRM 53-32-01. AND REPAIRED SKIN AT FRAME 78 BETWEEN STR 5L-6L IAW SRM 53-32-01.Apr 16, 2021 · N668HH · Emb EMB145LRSDR SIMA20210416006Skin · crackedFUSELAGE SKIN HAS 4 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 77 BETWEEN STR 3R-4R. -C/A-REPAIRED SKIN AT FRAME 77 BETWEEN STR 3R-4R IAW SRM 53-32-01.Apr 16, 2021 · N668HH · Emb EMB145LRSDR HALA2021041900067Skin · corrodedSHIP 393 FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV FWD EXHAUST PORT. CORRECTIVE ACTION: BLENDED AND CHECKED LIMITS PER A330 SRM 53-41-11. REMOVED CORROSION. REMOVED .008. REMAINING SKIN THICKNESS IS .090 WITHIN LIMITS PER A330 SRM 53- 41-11. PERFORMED UT. Apr 16, 2021 · N393HA · Airbus A330243SDR HALA2021041900066Skin · corrodedSHIP 393 LWR FUSELAGE- FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV AFT EXHAUST PORT. CORRECTIVE ACTION: REMOVED .022 MATERIAL REMAINING SKIN THICKNESS IS .076 WITHIN LIMITS PER A330 SRM 53-41-11. PERFORMED UT. TREATED, PRIMED, AND PAINTED AREA.(1783498)Apr 16, 2021 · N393HA · Airbus A330243SDR JJBA20210416037Skin · corrodedLH EXT FUSE SKIN BTW FR 61 AND JOINING OF SKIN AND BTW STR 20L-19L AT HEATED WATER DRAIN CORROSION. SKIN REPAIRED.Apr 16, 2021 · N14179 · Emb EMB145XRSDR DALA2021041902283Filler · corrodedDURING INSPECTION MAINTENENACE FOUND CORROSION LEVEL 2 ON SKIN FILLER FWD SIDE OF LAV SERVICE DOOR HINGE SIDE OUT OF LIMITS. FILLER REPLACED. (LP 1783482)Apr 16, 2021 · N199DN · Boeing 767332SDR CALA2021041900488Skin · crackedFUSELAGE 1EA HOLE FOUND CRACK ON WING SKIN RUNNING 11 O/C WITH APPROX 3/32" DEPTH PER EA 5310-06900 REV C OP 002 INSPECTION. (REFER NR LP 9131741, ZONE 100 SEQ 0357) DURING RH UNDERWING LONGERON REPLACEMENT PER EA, 1EA FASTENER HOLE CRACKED ON WING SKIN. HAECOApr 16, 2021 · N776UA · Boeing 777222SDR 2A6R2021041960201Skin · crackedTHERE IS A CRACK IN THE LOWER SKIN(PN:350A23-4218-21) AND THE EXISTING BATTERY DOOR DOUBLER(PN:350A23-4281-20) THE CRACK IS 2.0" IN LENGTH.Apr 16, 2021 · N139HN · Urocop EC130B4SDR CALA2021041600487Skin · corrodedFUSELAGE 2EA CRACKS FOUND ON THE FUSELAGE BS 1035 RH BUILT-UP UNDERWING LONGERON PER EA 5310-06900 REV C OP 002 INSPECTION. (REFER NR LP 9131740, ZONE 100 SEQ 0356) FX SKIN STA 993-1035 S35R - S38R SKIN REPAIRED AS PER ECRA 5331-02714 REV- PART 1 INTERIM REPAIApr 16, 2021 · N776UA · Boeing 777222SDR CALA2021041600486Skin · corrodedBELLY SKIN AT STRINGER 40R BETWEEN FR56 AND FR64 IS BULGING/DIMPLING AT FASTENER HEADS DUE TO CORROSION FROM MATING SURFACES OF INTERNALLY CORRODED AREAS. PHOTO IS ATTACHED TO ADD VISUAL CONTEXT. NO EVIDENCE THAT THE BELLY SKIN IS CORRODED. ALL OTHER FASTENER Apr 16, 2021 · N494UA · Airbus A320232SDR CALA2021041600485Skin · corrodedVACUUM BLOWER EXHAUST VENT PORT AT STA1968 FUSELAGE SKIN FOUND CORROSION. STA1968 FUSELAGE SKIN VACUUM BLOWER EXHAUST VENT PORT CORROSION AREA REPAIRED AS PER SRM 53-70-01 REV 85 AND ECRA 5331-02712 REV -.Apr 16, 2021 · N78002 · Boeing 777224SDR SWIA2021072259675Skin · dented*(DENT W/GOUGE) DETECTED R/H FUSELAGE SKIN, APROX 6" (FWD) F.S. 969.00 AND APROX 1" ABOVE STGR 17R/ WL 72.50. REQUIRES EVALUATION (MARKED). (C-CHECK RO 7/20/2021) (C-CHECK RO 7/20/2021) PERFORMED CUT-OUT DOUBLER REPAIR ON THE RH FUSELAGE SKIN BEApr 15, 2021 · N790SK · Cndair CL6002C10SDR QMLA2021041520032Skin · crackedDAMAGE TO THE LH STA5025 FRAME INNER SKIN PANEL (PN: B533K5606-211) IN THE FORM OF 2EA CRACKS ON THE UPPER END OF THE PART AND A CHAFE ON THE LOWER END OF THE PART. THE CRACKS WERE MEASURED TO BE APPROXIMATELY 0.19” AND 0.20” IN LENGTH EMANATING FROM A FASTENEApr 15, 2021 · N984ME · Bolkms BK117C2SDR SCNA20210514032Skin · dentedPANEL 192AL OUTER SURFACE DENTED MULTIPLE SPOTS. REPAIRED MULTIPLE DENTS ON OUTER SURFACE ON PANEL 192AL IAW SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-0Apr 15, 2021 · N815SY · Boeing 7378BKSDR SCNA20210514031Skin · puncturedPANEL 194DL INNER SURFACE PUNCTURED 6" FROM CENTER VENT. REPAIRED PUNCTURE 6" FROM CENTER VENT ON INNER SURFACE OF PANEL 194DL PER 737-800 SRM 53-60-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-1Apr 15, 2021 · N815SY · Boeing 7378BKSDR CALA2021041600478Skin · corrodedVACUUM BLOWER EXHAUST VENT PORT AT STA1968 FUSELAGE SKIN FOUND CORROSION. STA1968 FUSELAGE SKIN VACUUM BLOWER EXHAUST VENT PORT CORROSION AREA REPAIRED AS PER SRM 53-70-01 REV 85 AND ECRA 5331-02712 REV -.Apr 15, 2021 · N78002 · Boeing 777224SDR SWAA2021052464098Bear Strap · crackedSUPPORT TASK AD 2021-02-13 STA. 294.5 S-8R+4' (BELOW STRINGER) FASTENER HOLE AT BEAR STRAP EXHIBITS CRACK INDICATION (MARKED) INTERNALLY. /Apr 14, 2021 · N7815L · Boeing 73776QSDR HNAA2021051900205Skin · crackedREAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 78 BTW STRINGERS 4L-5L.REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 78 BETWEEN STRINGERS 4L-5L IAW PIEDMONT EO1-53-21--0110.Apr 14, 2021 · N644AE · Emb EMB145LRSDR HNAA2021051900204Skin · crackedREAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 78 BTW STRINGERS 6L-7L. REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 78 BETWEEN STRINGERS 6L-7L IAW PIEDMONT EO1-53-21--0110.Apr 14, 2021 · N644AE · Emb EMB145LRSDR HNAA2021051900202Skin · crackedREAR FUSELAGE II SKIN HAS POSSIBLE CRACKS AROUND 1 RIVET AT FR 77 BTW STRINGERS 8L-9L. REPAIRED REAR FUSELAGE II SKIN CRACKS AROUND 1 RIVET AT FR 77 BETWEEN STRINGERS 8L-9L IAW PIEDMONT EO1-53-21--0110.Apr 14, 2021 · N644AE · Emb EMB145LRSDR DALA2021041902270Doubler · bentSHIP 660 1640 FRAME REPAIR NOTICE SKIN DOUBLER BENT. CORRECTIVE ACTION: REMOVED FABRICATED AND INSTALLED SKIN DOUBLER. (1781654)Apr 14, 2021 · N660DL · Boeing 757232SDR DALA2021041602231Skin · dentedSHIP 672 DENTS ON FUSELAGE EXTERNAL SKIN BTW STA= 1375 AND STA= 1385 STRINGERS 28 AND 29 RH SIDE. CORRECTIVE ACTION: SUMMARY OF NRC 00183: DENTS ON FUSELAGE EXTERNAL SKIN BTW STA= 1375 AND STA= 1385 STRINGERS 28 AND 29 RH SIDE WERE REPAIRED PER ETI-57-21-146 RApr 14, 2021 · N672DL · Boeing 757232SDR SWIA202158745Skin · corrodedMULTIPLE AREAS OF CORROSION AND CHAFF DAMAGE BETWEEN F.S. 559+80 & 559+112 FROM STGR 21R TO 24R (C-CHECK RO 6/11/2021) REMOVED DAMAGE FROM FUSE EXTERIOR SKIN FS 559+80- FS 559+112 FROM STR 21R 24R IAW REO 601R-53-51-582 REV -- DATED 2021-04-27. COMPLIEDApr 13, 2021 · N904EV · Cndair CL6002B19SDR DALA2021041602226Doubler · dentedSHIP 658 AWR. TRANSFERRED FROM LOG #1100871: 2 DENTS REPORTED ON DOUBLER REPAIR OF 553127-14 REV ORIGINAL AT STA 620 ABOVE STRINGER 16L. DENT #1 LOCATED 0.560 AFT OF THE FRAME AND 0.870 ABOVE THE STRINGER. DENT #2 LOCATED 0.750 AFT OF THE FRAME AND 2.560 ABOVEApr 13, 2021 · N658DL · Boeing 757232SDR DALA2021041302168Skin · gougedSHIP 3238 GOUGE 6.25 AFT OF 2R DOOR, 1.5" BELOW STRINGER 15. MEASURES APPROX 3/8 X 1/4 X 0.011. CORRECTIVE ACTION: BLENDED DAMAGED AREA PER A320 SRM 53-41-11. OK FOR SERVICE. (7424822)Apr 13, 2021 · N338NW · Airbus A320212SDR SWIA2021082060544Skin · dentedWITHIN 10 FLIGHT CYCLES, COMPLY WITH PERMANENT REPAIR OF FOUND DENT ON LH NOSE BETWEEN FS193.25 AND FS202.75 STRGR 19 LH AND 21 LH, MEASURING 7.82 IN IN LENGTH BY 4.53 IN WIDE AND .155 AT ITS DEEPEST. COMPLIED WITH TEMPORARY DISPOSITION PER REO 670-53-11-165Apr 12, 2021 · N724EV · Cndair CL6002C10
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