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 SWIA20250602506Skin · damagedADM#9188 EVALUATE AND IMPROVE APPEARANCE OF DAMAGE AT FR 9 -10 STGR 18L - 19L (C-CHECK RO 5/30/2025) REPAIRED FUSELAGE SKIN BETWEEN FR 9-10 STGR 18L-19L WITH DOUBLER REPAIR. REF ETD2025-170-921639 REV F. SEE CONTINUATION FOR WORK PERFORMED. REPAIR PARTSMay 6, 2025 · N605UX · Emb ERJ170200LLSDR BAGA2025051400007Skin · corrodedFOUND DURING HEAVY CHECK - REAR BARREL FR 79 STGR 34L FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062.May 6, 2025 · N215BZ · Airbus BD5001A11SDR BAGA2025051400005Skin · corrodedFOUND DURING HEAVY CHECK - AFT CARGO DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062May 6, 2025 · N215BZ · Airbus BD5001A11SDR BAG2025F00000Skin · corrodedFWD PASSENGER DOOR UNDERNEATH SCUFF PLATES FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062May 6, 2025 · N215BZ · Airbus BD5001A11SDR BAGA2025051400003Skin · corrodedAFT SERVICE DOOR UNDERNEATH SCUFF PLATES, FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062May 6, 2025 · N215BZ · Airbus BD5001A11SDR BAGA2025051400002Skin · corrodedFWD SERVICE DOOR UNDERNEATH SCUFF PLATES, FOUND CORROSION ON LWR SKIN, REPAIRED IAW AIRBUS REO, DVI INSPECTIONS EVERY 1,000 FH, REPAIR VALID FOR 10,000 FH, CURRENT FH 8062May 6, 2025 · N215BZ · Airbus BD5001A11SDR DALA2025051203658Skin · damaged(LOG 0951753) GROUND DAMAGE TO THE RH SIDE OF THE A/C BETWEEN STA 500 AND STA 500A. REPAIRED DAMAGE PER ERA 626231-14.May 6, 2025 · N934DZ · Boeing 7379GPERSDR DALA2025050903636Skin · ground damage(LOG 0952052) WHILE ON THE LINE IN SDF, A BELT LOADER STRUCK THE RH SIDE OF THE A/C BETWEEN STA 500 AND STA 500A. REPAIRED DAMAGE PER ERA 626220-14.May 6, 2025 · N934DZ · Boeing 7379GPERSDR DALA2025050903634Skin · dented(LOG 7037449) DENT ON RT SIDE OF A/C AFT OF FWD CARGO DOOR. C/W ERA 626220-14 REV ORIGINAL.May 6, 2025 · N934DZ · Boeing 7379GPERSDR DALA2025050903593Skin · damagedREF LOG#7170928, FUSELAGE DAMAGE FWD OF DOOR 2L. C/W PRI 626076-14 REV 0 (251784) C/W PRI 626076-14 REV 1 (251784) C/W PRI 626076-14 REV 2 (251784) C/W PRI 626076-14 REV 3 (252784) C/W ERA 626076-14 REV ORIG. ENSURED ERA 626076-14 REV ORIG MATCHES ERA 626076-1May 6, 2025 · N518DZ · Airbus A350941SDR JGVR20250506001Skin · corrodedREPAIRED THE CORRODED FUSELAGE SKIN AT THE LOWER TCAS ANTENNA CABLE FEED-THROUGH BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH AVIATION QUALITY RESEARCH AND DEVELOPMEMay 6, 2025 · N305QS · Cessna 680CESDR SWIA20250616505Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA79960-ETD2022-170-026072 MXCODEID63557-PR - DENT FOUND ON THE LH NOSE OF AIRCRAFT FWD OF #3 PROBE IN THE FWD UPPER CORNER OF RVSM AREA MEASURING WIDTH 4.0'' X LENGTH 3.375'' X DEPTH 0.125'' LOCATED BETWEEN STRG-12L TOMay 5, 2025 · N168SY · Emb ERJ170200LRSDR IPXA2025060719081Skin · dentedFUSELAGE SKIN AT LOWER RIGHT SIDE AT FRAME 92-93 HAS THREE PROTUDING DENTS. NOT ON ADM. DOT AA024 VERIFIED EA 300-5319-27-A3965 PRELIMINARY 2 STEP #9 C/W<BR>VERIFIED SURFACE PROTECTION RESTORED. NOTE: DAMAGE NEEDS TO BE ADDED TO UPS MAPPING.May 5, 2025 · N139UP · Airbus A300F4622RSDR CALA2025050904585Skin · corrodedCORROSION FOUND ON BULK CARGO COMPARTMENT FUSELAGE SKIN AT LAP SPLICE STRINGER 36LH BETWEEN STA 1540 AND 1540 PLUS 7". CLASSIFIED AS MAJOR REPAIR. FILLED OUT ESFR INFORMATION, IT'S NECESSARY QC REVIEW AND APPROVAL TO GENERATE ESFR NUMBER. VERIFIED THE ESFR AMay 5, 2025 · N644UA · Boeing 767322SDR DALA2025050703548Skin · broken(LOG 0950240) GROUND POWER RECEPTACLE CUTOUT FWD LOWER CORNER SKIN BROKEN OFF. ACCOMPLISHED REPAIR AT EXTERNAL POWER RECEPTICAL DOOR IAW B737 SRM 53-10-15-2R REPAIR 5.May 5, 2025 · N3755D · Boeing 737832SDR CALA2025050604508Skin · damagedREF L/P4559461. RH FUSELAGE DAMAGE BETWEEN STA. 609+240 AND 632 ABOVE STR23L.COMPLIED WITH STEPS 1 THRU 4 AND 6A IN REF TO AVO14615 COMPLIED WITH STEP 5A-B OF AVO14615 NO OTHER DAMAGE NOTED AT THIS TIME COMPLIED WITH STEPS 6A-C OF AVO14615, .5"X.5" GRID ON INTMay 5, 2025 · N12003 · Boeing 78710SDR JR2R20250505244Skin · damagedRH SIDE OF LOWER FUSELAGE AT FR15 BETWEEN STR23R AND STR24R AIRCRAFT SKIN HAS A WAVY APPEARANCEMay 5, 2025 · N88325 · Emb ERJ170200LLSDR WRXR20250505003Skin · dented15EA. DENTS ON THE FUSELAGE UNDER THE L/H VENTRAL FIN FAIRING. RE-HAND DRESSED ALL DENTS ON FUSELAGE UNDER THE L/H VENTRAL FIN FAIRING TO REFORM TO ORIGINAL SKIN CONTOUR AND TO BE WITHIN AERODYNAMIC LIMITS PER REO 670-51-00-085 REV--, IAW MHI RJ REO 690-53-00-May 5, 2025 · N638NN · Cndair CL6002D24SDR WRXR20250505002Skin · dented15EA. DENTS ON THE FUSELAGE UNDER THE L/H VENTRAL FIN FAIRING. RE-HAND DRESSED ALL DENTS ON FUSELAGE UNDER THE L/H VENTRAL FIN FAIRING TO REFORM TO ORIGINAL SKIN CONTOUR AND TO BE WITHIN AERODYNAMIC LIMITS PER REO 670-51-00-085 REV--, IAW MHI RJ REO 690-53-00-May 5, 2025 · N638NN · Cndair CL6002D24SDR WRXR20250505001Skin · dented5EA. DENTS ON THE FUSELAGE UNDER THE R/H VENTRAL FIN FAIRING. RE-HAND DRESSED ALL DENTS ON FUSELAGE UNDER THE R/H VENTRAL FIN FAIRING TO REFORM TO ORIGINAL SKIN CONTOUR AND TO BE WITHIN AERODYNAMIC LIMITS PER REO 670-51-00-085 REV--, IAW MHI RJ REO 690-53-00-May 5, 2025 · N638NN · Cndair CL6002D24SDR VNAA20250602016Skin · corrodedEROSION AND CORROSION WAS FOUND ON ANTENNA AND SETTLEMENT AREA EXTERNAL FUSELAGE SKIN. CORROSION ON SETTLEMENT AREA EXTERNAL FUSELAGE SKIN WAS REMOVED PER CRJ-900 SRM 53-00-01-201-017-A01. AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-201-017-A01 AND AMay 4, 2025 · N598NN · Cndair CL6002D24SDR SWI2025F01240Skin · chafedPREVIOUS REPAIR TO THE EXTERNAL SKIN IS CHAFED, FS975.00 STGR27. (MARKED) (C-CHECK RO 09/07/2025)COMPLIED WITH REO 670-53-00-290 REV -F DATTED 2019-04-26 DOUBLER REPAIR FOR EXTERNAL SKIN FS975.00 STGR27, LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-90May 3, 2025 · N701SK · Cndair CL6002C10SDR SWAA2025052366807Splice · corrodedCORROSION L SHAPE STRINGER SPLICE ON STR28L LOC BS 360 AT EQUIPMENT ELECTRONIC COMP 2025-296187<[01]. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26; P/N P3015GOES00000 S/N 112820025 DUE DATE 28 JAN 26.; [02] REPLACED SPMay 3, 2025 · N440LV · Boeing 7377H4SDR SWAA2025052367145Plate · crackedCRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 229 TRAILING EDGE AT RT WING 2025-296204 <[01]. REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 229 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 115A2001; SHEET 30 ; REV A.; [02]May 3, 2025 · N440LV · Boeing 7377H4SDR ASAA2025050357996Skin · corrodedBUBBLING PAINT AT STR 23L STA 727I+2. GROUNDED - YES. REPAIRED SKIN AT LAP SPLICE STR 23L STA 727G-727J IAW ALASKA EA# 800-53EA-28682 REV 00. CAT B REPAIR INSPECTION REQUIREMENTS MUST BE ISSUED PRIOR TO THRESHOLD OF 50,000 TOTAL FLIGHT CYCLESW= 2" O= .080" R= May 3, 2025 · N537AS · Boeing 737890SDR DALA2025050703532Skin · corroded(LOG 0946135) WHILE ACOMPLISHING DOT INSP LOG 1202873 FOUND CORROSION AT AFT FUSELAGE SKIN AT LAV EXAUST PORT STA 907+10, STR20-21. COMPLIED WITH DELTA ER/A 626201-14 REV: ORIGINAL.May 3, 2025 · N802DN · Boeing 737932ERSDR DALA2025050603505Skin · corroded(LOG 0946865) DURING REMOVAL OF STR28L SO A REPAIR COULD BE PERFORMED, A CORROSION SPOT WAS ENCOUNTERED IN THE INNER SURFACE OF SKIN, SPECIFICALLY BETWEEN BSTA380 AND BSTA400 AT STR28L. REPAIRED PER ERA 625661-14.May 3, 2025 · N3746H · Boeing 737832SDR ASAA2025050357692Skin · corrodedCORROSION ON FUSELAGE SKIN AT STGR 23R FROM STA 967 TO STA 847 IN SEVERAL PLACES SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR ON FUSELAGE SKIN P/N 146A3251-32, 146A3231-49, 147A3110-4, AND 147A3400-4 AT STGR 23R BETWEEN STA 847 AND STA 967 IAW EA#8May 3, 2025 · N594AS · Boeing 737890SDR ASAA2025050357691Skin · corrodedSIGNS OF CORROSION FOUND BETWEEN STA 480 AND STA 500G AT STGR 24R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR ON FUSELAGE SKIN P/N 143A3252-29 AT STGR 24R BETWEEN STA 480 AND STA 500G IAW EA#800-53EA-28642 REV 00 SRXR430X.May 3, 2025 · N594AS · Boeing 737890SDR ASAA2025050357690Skin · corrodedCORROSION AROUND SERVICE INTERPHONE CONNECTION BELOW STGR 23L BETWEEN STGR 24L-25L STA 1040 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR ON FUSELAGE SKIN P/N 148A3321-13 AT STGR 24L-25L STA 1040 IAW EA#800-53EA-28635 REV 00 SRXR430X.May 3, 2025 · N594AS · Boeing 737890SDR DALA2025050503415Skin · damagedGROUND DAMAGE ON FUSELAGE BOTTOM AT APPROX STATION 412-420, BETWEEN STRINGERS LBL 537 AND RBL 537. REF NR LOG #0921831 FOR PRI COMPLIANCE ERA 625864-14 REV O. REPAIRED DAMAGE IAW PRI/ERA 625902-14 REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. VERIFIED PRI 625902-14 REV May 3, 2025 · N197DN · Boeing 767332SDR DALA2025050503414Skin · damagedFOUND SEVERAL HOLES OUT OF ROUND AND UNINSPECTABLE. 7 HOLES AT S-37L, 2 HOLES AT S-37R, AND 1 HOLE AT STA 421 ABOVE S-37R. MARKED. COMPLIED WITH E/RA 625902-14 REV A. PRI REVREV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625May 3, 2025 · N197DN · Boeing 767332SDR DALA2025050503413Skin · damagedAT STR 37R STA 421 (MARKED). SUMMARY SEE NRC 003-0001:0520-8130/013 00013: COMPLIED WITH E/RA 625902-14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9, REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902 -14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9 REPAIR May 3, 2025 · N197DN · Boeing 767332SDR DALA2025050503412Skin · ground damageGROUND DAMAGE. COMPLIED WITH E/RA 625902-14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9 REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902-14 REV A. PRI REV. 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL.May 3, 2025 · N197DN · Boeing 767332SDR SWIA2025080600502Doubler · wornON BELLY UNDER FAIRING FS-969, BL -0, DEEP WEAR MARK ON DOUBLER. REMOVED AND REPLACED DOUBLER UNDER BELLY FAIRING FS969 BL 0 IAW REO 670-53-00-290 REV. -F DATED: 2019-04-26May 2, 2025 · N748EV · Cndair CL6002C10SDR HNAA2025061600436Skin · gougedF043987 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR8L / 9L. REMOVED THE CRACKED SKIN AND INSTALLED BUSHING WITH A RIVET AT REAR FUSELAGE SKIN FR 77BETWEEN STGR 8L/9L IAW EMB 145 SRM 53-32-01 ITEM 9, FIG 213, SRM 53-32-01 ITEM 9, FIG 2May 2, 2025 · N663AR · Emb EMB145LRSDR HNAA2025061600435Skin · gougedF043864 FUSELAGE EXTERNAL SKIN DOUBLER BELOW GPU DOOR GOUGED. RE-ACCOMPLISHED FUSELAGE EXTERNAL SKIN DOUBLER BELOW GPU DOOR IAW EMB 145 SRM 53-12-01, ITEM 2, FIG 201 AND EO1-53-25-0173.May 2, 2025 · N663AR · Emb EMB145LRSDR DALA2025050603506Skin · corroded(LOG 0946117) WHILE ACCOMPLISHING DOT INSPECTION (PREVIOUSLY BLENDED AREA PER LOG# 1202873), CORROSION WAS DISCOVERED ON THE EXTERIOR SURFACE OF THE FUSELAGE SKIN (PN 147A3110-43) AT THE LOWER FORWARD SURFACE OF THE LAV EXHAUST PORT, BS 927, BETWEEN S-21L AND May 2, 2025 · N802DN · Boeing 737932ERSDR CALA2025050504460Bear Strap · crackedR1 FWD SERVICE DOOR AFTER CORNER - DURING HFEC OPEN HOLE INSPECTION WAS FOUND HOLES WITH CRACK INDICATION.UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT CLASSIFIED AS MAJOR REPAIR. (CHANGE ATTRIBUTES). UPDATE GENERATED DUE REPAIR ACCOMPLISHMENT CLASSIFIED AS MAJORMay 2, 2025 · N652UA · Boeing 767322SDR CALA2025050504459Bear Strap · crackedL1 FWD ENTRY DOOR AFTER CORNER - THERE ARE TWO CRACKS AT 10 AND 4 O'CLOCK IN THE LOWER ON THE AFTER CORNER. UPDATE GENERATED DUE REPAIR TO BE ACCOMPLISHED CLASSIFIED AS MAJOR. THE FUSELAGE SKIN 1R DOOR CUTOUT AFTER LOWER CORNER BEAR STRAP WAS REPAIRED AT GIMay 2, 2025 · N652UA · Boeing 767322SDR SWI2025F01219Skin · gougedTHE FWD CARGO DOOR SURROUND FUSELAGE SIDE LOWER CLOSING SKIN BETWEEN FS533 AND FS581 HAS MULTIPLE LOCATIONS OF GOUGES AND CORROSION. (C-CHECK RO 09/07/2025)REMOVED GOUGES AND CORROSION ON FWD CARGO DOOR, SURROUND FUSELAGE SIDE LOWER CLOSING SKIN BETWEEN FS53May 1, 2025 · N701SK · Cndair CL6002C10SDR SWIA202507140501Skin · crackedFORWARD LOWER FUSELAGE SKIN AT THE NLG AFT DOOR CUTOUT HAS A SUSPECTED CRACK AT THE AFT RIGHT CORNER. APPROX. FS235.00. CAMP 30064121 (C-CHECK RO 07/11/2025)REPAIRED FWD LWR FUSELAGE SKIN AT THE NLG AFT DOOR CUTOUT APPROX FS235 PER REO 601R-53-11-048 REVMay 1, 2025 · N223JS · Cndair CL6002B19SDR DALA2025050803566Skin · damagedSHIP 1006 WHILE SEARCHING FOR L/L MON OF LIGHTNING STRIKE FOUND UNDOCUMENTED LIGHTNING STRIKE FWD OF FR 52 NEAR STGR 6R. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:00-0505-8-8536/005 00024 May 1, 2025 · N106DN · Airbus A321211SDR DALA2025050803565Skin · damagedSHIP ER/A 626079-14 SECTION I REPAIRED LIGHTNING STRIKE DAMAGE ON LAP SPLICE S-6R, BETWEEN FR\47.5 AND FR57. CORRECTIVE ACTION: ER/A 626079-14 SECTION II REPAIR TO BE ACCOMPLISHED WITHIN 200 FLIGHT CYCLES FROM SECTION I ACCOMPLISHMENT. (0943413)May 1, 2025 · N106DN · Airbus A321211SDR CALA2025050604507Skin · scratchedREF LP 4621073. WORK WITH AVO14672. USE THE LOG PAGE TO UPDATE ACCOMPLISHMENT OF AVO STEPS. COMPLETED THE DAMAGE INSPECTION AND EVALUATION INSTRUCTIONS UP TO STEP A.4.A). NO INTERNAL DAMAGE VISUAL OR TACTILE INDICATIONS OR FOUND AT THIS TIME. INSPECTION UPDAMay 1, 2025 · N14019 · Boeing 78710SDR IXXA20250502001Skin · dentedEXTERIOR FUSELAGE SHIN HAS SEVERAL OUTWARDLY PROTUDING DENTS BETWEEN STA 654+44 - STA 654+68, AT STRINGERS S-R1 THOUGH S-4L. 8110-3 ISSUED.May 1, 2025 · N229AZ · Boeing 767323SDR CALA2025050204416Skin · crackedL/H HOLE #2 AT FR 35 HAS BEEN PREVIOUSLY WORKED. ACCOMPLISHED REPAIR PER HAECO RCO-L25396 WITH NO DEVIATIONS. ACCOMPLISHED A PERMANENT REPAIR AT LH FR35 STA R30LH HOLE #2 PER PART 3 OF THE LATEST REVISION OF ECRA 5320-07500 ON OR BEFORE 22OCT2025. INTERIM REMay 1, 2025 · N460UA · Airbus A320232SDR ASAA2025050157666Skin · corrodedCORROSION ON SKIN BETWEEN STA 887 AND STA 927 BETWEEN STGR 24L AND STGR 27L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3400-4 BETWEEN STA 887 AND STA 907 STGR 24L-26L IAW EA 800-53EA-28620 REV 00 SRXR430X.May 1, 2025 · N594AS · Boeing 737890SDR ASAA2025050157665Skin · corrodedSIGNS OF CORROSION FOUND BETWEEN STA 787 AND STA 867 AT STGR 14L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 146A3201-32 BETWEEN STA 787 AND STA 867 STGR 14L IAW EA 800-53EA-28621 REV 00 SRXR430X.May 1, 2025 · N594AS · Boeing 737890SDR FDEA202505010702Skin · chafedFWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM FOUND CHAFFED. FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM CHAFFED AREA REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-10-02-0G, SRM53-10-01-2R REPAIR 1, SRM 51-40-05-0G, SRM 51- 40-08-0G, SRM 51May 1, 2025 · N890FD · Boeing 777FS2
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