JASC 5330

Service difficulty reports · 79,312

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 DALA2025092306957Skin · scratchedFOUND SCRATCHES AAFFECTING THE FUSELAGE SKIN PANEL BETWEEN FR 57 AND STR 26L-27L. COMPLIED WITH ER/A 629166-14AD. (1212433).Sep 22, 2025 · N319NB · Airbus A319114SDR DALA2025092306956Skin · scratchedSCRATCH ON EXTERNAL SKIN LOCATED BTW FR 57 TO FR 58 AND STR 26L TO ST R 27L AT LOWER FUSELAGE. COMPLIED WITH ER/A 629166-14AD. (1212626).Sep 22, 2025 · N319NB · Airbus A319114SDR DALA2025092306934Bear Strap · ground damageDUE TO IMPACT DAMAGE, FUSELAGE BEARSTRAP P/N 141A3522-3 FORWARD SECTION DAMAGED FROM STA 203.8 - 196.5. REPAIRED DAMAGED BEARSTRAP PER ER/A 628235-14 REV ORIGINAL COMPARED TO PRI 628235-14 REV 0 AND 1. IDENTIFIED REPAIR STEPS 10 AND 11 ADDED TO ER/A 628235-14 Sep 22, 2025 · N3742C · Boeing 737832SDR DALA2025092306933Skin · mechanic errorDURING THE LOCATION AND DRILLING OF SKIN P/N 141A3521Y33, 12 HOLES WERE MISDRILLED ON THE SKIN @ RBL 17 AND BS 178 - 188. TRIMMED OUT MINIMAL AMOUNT OF MATERIAL ONLY TO REMOVE MISDRILLED HOLES PER STEP 3 PN 628289-14 REV 0. REMOVED THE NECESSARY NUMBER OF FASSep 22, 2025 · N3742C · Boeing 737832SDR BAGA2025092300003Skin · damagedPREVIOUS SUBMISSION UPDATED WITH CORRECTIVE ACTION ---VERY LOUD BAND SOUND HEARD DURING CLIMB. UPON LANDING, FOUND EVIDENCE OF LARGE BIRD STIKE OVER FLIGHT DECK AREA. TEMP DOUBLER REPAIR TO BIRD STRIKE DAMAGE ON THE FUSELAGE CANOPY SKIN BETWEEN THE LT WINDSHIESep 21, 2025 · N221BZ · Airbus BD5001A11SDR CALA2025092409213Skin · damagedREF LOG PAGE 5420901 FOR REPAIR OF TAILSTRIKE DAMAGE TO AFT LOWER FUSELAGE. R & R SKIN ACCOMPLISHED. OK TO CLEAR.Sep 21, 2025 · N66831 · Boeing 737924ERSDR CALA2025092309167Skin · crackedEXTERNAL POWER DOOR CUTOUT CRACKED AT LOWER SIDE. INSTALLED DOUBLER AND FILLER TO REPAIR AREA AS PER REFERENCE SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204 SHEET 1 AND SRM SRM 514002-0G-0Sep 21, 2025 · N33284 · Boeing 737824SDR VNAA202511250003Doubler · corrodedCORROSION ON DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000. DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000.00 WAS REPLACED PER REO 670-53-00-290 REV -FSep 20, 2025 · N527EA · Cndair CL6002C10SDR R61A2025101700435Doubler · corrodedDURING HEAVY CHECK CF III FR 88-89 STR26R-28R FOUND CORRODED WASTE DOOR. REMOVED AND REPLACED WASTE DOUBLE IAW SRM 51-41-02Sep 20, 2025 · N810MD · Emb ERJ170100SUSDR JJBA20251014044Skin · corrodedCORROSION ON HEATED WATER DRAIN BETWEEN FRAMES 60 TO 61 LOWER EXTERNAL FUSELAGE. REMOVED CORROSION BY PERFORMING CUTOUT AND INSTALLING A DOUBLER AT HEATER WATER DRAIN BETWEEN FRAMES 60 AND 61 ON LOWER EXTERNAL FUSELAGE.Sep 20, 2025 · N17169 · Emb EMB145XRSDR CALA2025101309989Skin · corrodedPOSIBLE CORROSION ON UPPER SKIN STA 727G TO 727F BTW STR 2L TO 3L. PERFORMED INTERIM REPAIR ON FUSELAGE SKIN AT STA 727F AND STRG 3L TO STRG 4L, ALL WORK PERFORMED IAW EC/RA 5360-02016 REV ORIG AND EO 250327 REV IR.Sep 20, 2025 · N77525 · Boeing 737824SDR AALA202509279225Skin · corrodedAIRCRAFT WAS GROUNDED: AFT LAVATORY VACUUM VENT OUTLET APPEARS TO HAVE CORROSION. MAINTENANCE FERRY TO TLE FOR REPAIR (SEE AALA202509272720) CORROSION ON LOWER FUSELAGE SKIN AROUND AFT LAVATORY VACUUM VENT LOCATED AT BS 917 FROM S21L AND S22L. ACCOMPLISHED TSep 20, 2025 · N960AN · Boeing 737823SDR AALA202509259225Outlet · corrodedAIRCRAFT WAS GROUNDED, AFT LAVATORY VACUUM VENT OUTLET APPEARS TO HAVE CORROSION. (OPEN)Sep 20, 2025 · N960AN · Boeing 737823SDR DALA2025091906890Skin · dentedFOUND DENT BETWEEN FR10 AND FR11, AND APPR. 12" BELOW STR23 ON THE LEFT. CONFIRMED SURFACE PROTECTION ACCEPTABLE. EVALUATED PER A319 SRM 53-11-11-283-012. (7191121).Sep 19, 2025 · N369NB · Airbus A319114SDR SWIA2026032775575Skin · dentedCOMPLY WITH PERMANENT REPAIR ON RA ID: 94891PER TEMP REPAIR REO 601R-53-61-8247 REV-, DENT WITH BLENDED SCRATCH DAMAGE ON FUSELAGE SKIN BETWEEN FS605.00 - FS 621.00 NEAR STGR 19L IS STRUCTURALLY ACCEPTABLE FOR 1200 FH FROM THE TIME OF INCORPORATION OF THIS REOSep 18, 2025 · N246PS · Cndair CL6002B19SDR CALA2025101510112Skin · corrodedPOSIBLE CORROSION ON UPPER SKIN BS 727E BTW STR 3R TO 4R. REPAIRED SKIN, BS 727E S3R TO S4R IAW EC/RA 5360-02015 AND EO 250309 REV. IR, RSep 18, 2025 · N77525 · Boeing 737824SDR FDEA202509181854Skin · misrepairedEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR102~103,STGR 1~2L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,INSPECTION OF DOUBLERSep 18, 2025 · N690FE · Airbus A300F4605RSDR DALA2025092206929Skin · dentedWHILE PERFORMING DENT DOT MONITOR INSPECTION FOR LOG PAGE 6784736, FOUND ADDITIONAL DAMAGE AT DENT LOCATION 13" AFT OF STA 1197+66 AND 3" BELOW STR 35L. REPAIRED PER B767 SRM 53-00-01-2R-12 DETAIL I. REPAIR IS CAT B. (1205512)Sep 18, 2025 · N173DZ · Boeing 767332SDR R61A2025092200413Skin · dentedBIRD STRIKE CAUSING DENT ON FWD FUSELAGE BETWEEN FR. 5-6 STR 10R-12R. CUTOUT DAMAGE AND INSTALLED A 2 ROW DOUBLER.Sep 18, 2025 · N128HQ · Emb ERJ170200LRSDR CALA2025092209093Skin · dentedDAMAGE NOTED FWD OF D2LREF SRM 53-030-01-1A-2, VERTICAL DENT MEASURED AT 7.25" WITH A MAX MEASURED DEPTH OF 0.019". DENT LOCATION MEASURED TO BE 17" AFT OF STA 655. TOP OF DENT MEASURED TO BE 24" BELOW S24L. FOR 4X PREVIOUS DENTS, SEE LP 3269188 ADD EMP:U33028Sep 18, 2025 · N799UA · Boeing 777222SDR CALA2025101309983Skin · dentedDENT AT BS 188 BETWEEN STR 21 & 24 RT & CARD LP# 4423742 REF.AAR N/E:99950967. REMOVED DAMAGED AREA ON FUSELAGE SKIN AND INSTALLED REPAIR AT BS 177 TO 196.5, S17R-24R, REF AAR-MIA ESR-WI #2023803-17-12771 AND UNITED EC/RA 5310-08695. PERFORM AN INSPECTION OSep 17, 2025 · N33284 · Boeing 737824SDR DALA2025091806867Skin · corrodedCORROSION FOUND LWR SKIN AT STA 660 BETWEEN STR 26L AND 27L. REMOVED DAMAGED AREA IN SKIN BETWEEN STRINGERS S-26L AND S27L, FABRICATED REPAIR DOUBLER, FILLERS, AND SPLICE PALTE REPAIR DOUBLER AND INSTALLED PER ER/A 629135-14AD. (LP 1203519)Sep 17, 2025 · N692DL · Boeing 757232SDR CALA2025091809024Skin · dentedFUSELAGE BTWN BS 600 - 620 S16L. EXISTING REPAIR DOUBLER HAS A DENT. COMPLIED WITH UAL ECRA 5330-07610 AND V T MAE EA 757-5330-13-A41 09 REV-.Sep 17, 2025 · N14118 · Boeing 757224SDR 2025FA0000651Skin · damagedDURING THE STRUCTURE INSPECTION IT WAS FOUND THE FORWARD FUSELAGE, AT FR18+50MM, AND S27LH + 155MM (JUST 8.0MM FROM THESTR 28L FASTENER ROW), THE EXTERNAL SKIN WITHLIGHTNING STRIKE WITH EXISTING BLEND OUT. THE BLEND OUT WAS EVALUATED AND CLASSIFIED ASNON-SIGNISep 17, 2025 · N247JB · Emb ERJ190100IGWSDR EE4Y2025091723171Skin · damagedCUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE EXTERNAL SKIN OF THE FWD FUSELAGE, LOCATED AT FRAME 20+85MM, STRINGER 27RH+115MM. THE DAMAGE EXCEEDS 50% OF THE SKIN THICKNESS. A 3.97MM HOLE WAS DRILLED TO INSTALL A THROUGH DAMAGE REPAIR IN ACCORDANCE Sep 17, 2025 · N247JB · Emb ERJ190100IGWSDR EE4Y2025091723170Skin · damagedDURING STRUCTURE INSPECTION, FOUND FWD FUSELAGE, FR 18+50MM, & S27L + 155MM (JUST 8.0MM FROM STR 28L FASTENER ROW), EXTERNAL SKIN WITH LIGHTNING STRIKE WITH EXISTING BLEND OUT. BLEND OUT WAS EVALUATED & CLASSIFIED AS NON-SIGNIFICANT IAW SRM 51-75-16. LIGHTNSep 17, 2025 · N688DR · Emb ERJ190200LRSDR EE4Y2025091723168Skin · damagedCENTER FUSELAGE I SKIN HAS A LIGHTNING STRIKE DAMAGE AT FRAME 30+290MM AND STRINGER 27R. SEE FIGURE 1. THE DAMAGE WAS REMOVED BY BLENDING AND WAS FOUND BEYOND LIMITS PER SRM 53-21-01/AD 51. SINCE THE DAMAGE IS LOCATED IN THE NOT ALLOWED REPAIR AREA (GREY AREA)Sep 17, 2025 · N688DR · Emb ERJ190200LRSDR SWIA202512220916Skin · dented1 DENT LOCATED APRROXIMATELY 6" AFT OF FS 654.50 BETWEEN STRINGERS 22L AND 23L. (C-CHECK RO 12/19/2025)COMPLIED WITH REO 601R-53-61-8393 REV "--" DATED 2025-10-16. REPAIR FOR DENT AND GOUGE DAMAGE TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.20 AND STR21L - STR2Sep 16, 2025 · N944SW · Cndair CL6002B19SDR R61A2025092700414Skin · corrodedDURING HEAVY MAINTENANCE VISIT CORROSION ON LOWER FUSELAGE SKIN AT FR 97-98, STGR 28R-29L. REPAIRED LOWER FUSELAGE SKIN AROUND IDENTIFICATION PLACARD AT FR 97-98, STGR 28R-29L PER ETD2025-170-927947 REV. A .Sep 16, 2025 · N232JQ · Emb ERJ170200LRSDR AALA202509195003Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND AFT LAVATORY VENT LOCATED AT BS 1947, LBL 84. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-70-01-2R-1.Sep 16, 2025 · N762AN · Boeing 777223SDR YENA2025091800948Skin · ground damageDURING HEAVY MAINTENANCE: AC UNIT 12934 CAME IN CONTACT WITH AIRCRAFT AT RH FUSELAGE LOWER SKIN 1" FWD OF FR15 STR 35-36 RIGHT; (RESOLVED ON W/O: 1407010 TASKCARD: NR-00009) REF HAECO WO 440615 NR 42452 ACCOMPLISHED REPAIR OF FUSELAGE SKIN RH FR 15 STR 35-36 RSep 16, 2025 · N2016J · Airbus A321271NXSDR FDEA202509161706Skin · crackedFUSELAGE EXTERIOR SKIN APPROXIMATELY LEFT HAND STATION 475, FORWARD OF NOSE LANDING GEAR FORWARD DOOR FOUND CRACK APPROXIMATELY 1.5 INCHES. CRACK AT FUSELAGE EXTERIOR SKIN APPROXIMATELY LEFT HAND STATION 475, FORWARD OF NOSE LANDING GEAR FORWARD DOOR REPAISep 16, 2025 · N590FE · Doug MD11FSDR SWIA202512020915Doubler · scratchedWIFI FWD ATG ANTENNA CUTOUT HAS MULTIPLE SCRATCHES ON OUTER SKIN. INSTALLED NEW WIFI FWD ATG ANTENNA OUTER DOUBLER IAW DWG P13110-20110 REV M.Sep 15, 2025 · N897SK · Cndair CL6002D24SDR SWIA2025F01429Doubler · corrodedWASTE SERVICING ACCESS DOOR CUTOUT INTERNAL DOUBLER HAS CORROSION DAMAGE ON THE LEFT SIDE OF THE ACCESS DOOR HINGE. REMOVED AND REPLACED WASTE SERVICING DOOR CUTOUT INTERNAL DOUBLER REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED. PART REPLACED WITSep 15, 2025 · N174SY · Emb ERJ170200LRSDR N6WA2025091702Skin · corrodedCORROSION ON BELLY SKIN UNDER VHF2 ANTENNA. REPAIRED SKIN ON FUSELAGE UNDER VHF2 ANTENNA IAW EA 129-2025-194 REV IRSep 15, 2025 · N507GJ · Cndair CL6002C10SDR FDEA202509151703Skin · ground damageAFT CGO LOADER WENT UP (BY ITSELF PER RAMP) AND HITTED THE AFT FUSELAGE BELOW DOOR FRAME, LOADER STILL IN CONTACT CURRENTLY, BUT A HOLE IS VISIBLE ALREADY ABOUT 5 SQUARE INCHES. WILL EVALUATE WHEN LOADER IS REMOVED. OMPLIED WITH EA 1-5330-T0384834 PART 2 Sep 15, 2025 · N525FE · Doug MD11FSDR JR2R20250915753Skin · dentedLOWER AFT FUSELAGE SKIN BETWEEN FR97-FR97 AND STR27L-STR28L HAS A PROTUDING DENT. REPAIRED.Sep 15, 2025 · N82333 · Emb ERJ170200LRSDR SWIA2025100700914Skin · ground damageEXTERIOR DAMAGE FROM LAV SERVICING TRUCK NEAR AFT POTABLE WATER PANEL: UPON INSPECTION, FOUND DAMAGE TO FUSELAGE STRUCTURE BETWEEN FS574 €“ FS589.00 AND BTW STR 17R-18R. IMPACT (LAVATORY CART) CAUSED DAMAGE TO MULTIPLE PARTS. REFER TO REO 601R-53-61-8383 TABSep 14, 2025 · N929EV · Cndair CL6002B19SDR N6WA2025091703Skin · corrodedCORROSION ON FUSELAGE SKIN UNDER UPPER TCAS ANTENNA. REPAIRED FUSELAGE SKIN UNDER UPPER TCAS ANTENNA IAW REO-670-53-21-1250Sep 14, 2025 · N507GJ · Cndair CL6002C10SDR HNAA2025102100716Skin · dentedF069895 FUSELAGE EXTERNAL SKIN HAS A PROTRUSION BETWEEN FR 77/80 STR 18R/19R. INSTALLED FABRICATED REPAIR DOUBLER AND FILLER ON FUSELAGE EXTERNAL SKIN BETWEEN FR. 77-80, STRG. 18R-19R IAW ETD2025-145-928508 AND PIEDMONT EO1-05-25-0363.Sep 13, 2025 · N691AE · Emb EMB145LRSDR MASA20250930003Fastener · corrodedCORRODED FASTENERS (QTY 42) WERE REMOVED AND REPLACED IAW ERJ175 SRM 51-43-04 ON RH LOWER SKIN AT RIB 26, AND SPAR 2.Sep 13, 2025 · N80343 · Emb ERJ170200LRSDR DALA2025091606801Skin · damaged(LOG 1197892) AIRCRAFT TAIL NUMBER N3742C WAS SUBJECT TO IMPACT DAMAGE DUE TO HIGH WIND EVENT IN DENVER COLORADO. FUSELAGE SKIN PN 141A5321-11 WILL BE REPLACED AND SO IS THE BEARSTRAP PN 141A3522-3 FORWARD SECTION. WHILE THE SKIN PN 141A3521-11 IS RUNNING FROMSep 13, 2025 · N3742C · Boeing 737832SDR DALA2025091506789Skin · not reportedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BT W FR 5 TO FR 6 AT THE LAP SEAM AND 5 INCHES BELOW LH SIDE STRINGER L OWER FUSELAGE. COMPLIED WITH ER/A 574394-14. (1197223).Sep 13, 2025 · N352NB · Airbus A319114SDR AALA202512248147Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR 59 TO FR 60 AND BTW STRG 42L TO STRG 43L IN AFT CARGO COMPARTMENT L= 20.07 IN, W=3.569 IN, D=0.025.Sep 12, 2025 · N9002U · Airbus A319115SDR AALA202512085332Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR 59 TO FR 60 AND BTW STRG 41L TO STRG 42L IN AFT CARGO COMPARTMENT.MEASURE CORROSION ARE L=3.432 INCH W=2.122 INCH D=0.002 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON REAR FUSELAGE ISep 12, 2025 · N9002U · Airbus A319115SDR AALA202511288958Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR 61 TO FR 62 AND BTW STRG 43R TO STRG 44 IN AFT CARGO COMPARTMENT MEASURES OF CORROSION ARE: L=4.699 IN, W=3.89 IN, D=0.008 IN. MAINTENANCE ACCOMPLISHED INTERIM REPAIR AT LEVEL FR 62 BTW STRG Sep 12, 2025 · N9002U · Airbus A319115SDR AALA202511289667Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR 56 TO FR 57 AND BTW STRG 43L TO STRG 44 IN AFT CARGO COMPARTMENT L= 3.000 IN, W= 2.927 IN, D= 0.003 IN. MAINTENANCE INSTALLED DOUBLER ON SKIN.Sep 12, 2025 · N9002U · Airbus A319115SDR AALA202511247615Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL SKIN LOCATED BTW FR 58 TO FR 59 AND BTW STRG 42L TO STRG 43L IN AFT CARGO COMPARTMENT MEASURMENT OF CORROSION ARE: L= 1.494 IN, W=0.800IN D=0.002IN. MAINTENANCE REPAIRED SKIN PANEL IAW EA 369173.Sep 12, 2025 · N9002U · Airbus A319115SDR SWAA2025102114271Plate · corrodedCORROSION PLATE LOCATED STA 312 LBL 54 AND WL 208.1 AT FWD GALLEY AREA. REPLACED PLATE LOCATED STA 312 LBL 54 AND WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9. AND APPLIED TORQUE OF 150 LB-IN IAW SRM 51-40-04-0G-0.Sep 12, 2025 · N8619F · Boeing 7378H4SDR SWIA2025F01339Skin · scratchedUPON INSPECTION, FOUND THE DAMAGED AREA BETWEEN THE AFT CARGO DOOR AND AFT LAV SERVICE PANEL TO BE 15.5"L X 2.5" W WITH A SCRATCH 1/16" DEEP. DAMAGE IS OUT OF LIMITS PER SRM 53-23-01 (FLIGHT 4653 - FILED CLOSED)TRANSFERED FROM EAML 1702353 : REF AML# 1702303Sep 12, 2025 · N124SY · Emb ERJ170200LR
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