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 CALA2025093009430Skin · ground damageLOADER CAME IN CONTACT WITH THE ACFT AT THE AFT CARGO DOOR, DAMAGE IS LOCATED APPROX. BS 1373, ABOVE STRINGER 29R ON FUSELAGE SKIN WITH PULLED FASTENERS ON SKIN. INSPECTION OF UNDERLYING STRUCTURE REVEALED BOWED FRAME. DAMAGE DEMENSIONS ARE 3.6"X 1.1". BLENSep 28, 2025 · N641UA · Boeing 767322SDR DALA2025093007104Skin · corrodedSHIP 3318 FUSELAGE SKIN / FR 74 TO FR 75 / S-40L TO S-42L / WATER WASTE VENT / CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 629544-14 REV ORIGINAL. (7074981)Sep 28, 2025 · N818NW · Airbus A330323SDR DALA2025093007098Vent · corrodedCORROSION ON LAV VENT BEYOND SRM LIMITS. REPAIRED PER ERA 629544-14 REV ORIGINAL. (7074980)Sep 28, 2025 · N818NW · Airbus A330323SDR DALA2025093007091Skin · damagedSHIP 3318 DAMAGE ON FUSELAGE SKIN AT FR74 TO FR75/S-40L TO S- 42L WASTEWATER VENT. CORRECTIVE ACTION: REPAIRED PER ERA 629544-14 REV ORIGINAL. (1222800)Sep 28, 2025 · N818NW · Airbus A330323SDR SWAA2025110318785Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL AT FUSELAGE EXTERIOR, REPAIRED THE ACCESS PANEL 193AL IAW SRM 51-70-05-2R-6, REPAIR 6.Sep 27, 2025 · N915WN · Boeing 7377H4SDR SWIA2025101700927Skin · chafedFWD FUSELAGE INTERNAL SIDE, FWD SERVICE DOOR CUTOUT FROM FR17-18, STGR 11 IS CHAFFED. REMOVED AND REPLACED RIB AT FWD SERVICE DOOR CUTOUT FROM FR17-18, STGR 11 REF EMB SRM 51-40-08.RESTORED SURFACE PROTECTION REF EMB SRM 51-23-04, 51-23-05, & 51-23-06. CIC RSep 27, 2025 · N616UX · Emb ERJ170200LLSDR CALA2025101309942Skin · bulgedFOUND BULDGE IN THE SKIN ALONG WITH PULLED RIVET HEADS ON STRINGER 26L BETWEEN STA 360-380. AFTER FURTHER INSPECTION, FOUND CORROSION BETWEEN STRINGER & SKIN AT THE STRINGER SPLICE. REMOVED STRINGER 26L IAW SRM 51-40-02 & AVO719-25-09-26-01. REMOVED STRINGSep 27, 2025 · N17719 · Boeing 737724SDR CALA2025101309941Skin · corrodedSKIN BULGED AROUND RIVETS LWR AFT CORNER OF LAV SERVICE PANEL. REMOVED LOCK FASTENERS ON LOWER AFT AND FWD OF LAV SERVICE PANEL IAW SRM 51-40-02. REMOVED LAV SERVICE PANEL IAW SRM 51-40-02. REMOVED CORROSION ON LOWER AFT CORNER OF LAV SERVICE DOOR CUTOUT ON Sep 27, 2025 · N17719 · Boeing 737724SDR AALA202510024602Skin · gougedAIRCRAFT IN BASE MAINTENANCE: GOUGE IN SKIN BS 116 AND STR 5-21R. COMPLIED WITH REPAIR, PER SRM 53-80-01-2R REPAIR 5 AND PER AARD 51-40-00-5.Sep 27, 2025 · N887NN · Boeing 737823SDR YENA2025093000983Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED BTW FR 79 AND FR 80 AND BTW STRINGER 2LH A ND STRINGER 2RH ON UPPER FUSELAGE; (RESOLVED ON W/O: 1409303 TASKCARD: NR-00057) REF AEROMAN W/O 2025 282/1 NR 2025-505895. PERFORMED PERMANENT REPAIR LOCATED ON EXSep 27, 2025 · N618JB · Airbus A320232SDR DALA2025092907027Skin · damagedAIRCRAFT 3034, DAMAGE FOUND ON SKIN FWD OF L-1 DOOR. REPAIRED DAMAGE REF A321-200 SRM 53-11-11-300-006. (LP 7866387)Sep 27, 2025 · N334DN · Airbus A321213SDR EE4Y2025092723172Repair · misinstalledDURING STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND ON THE FUSELAGE SKIN AT FR19 BETWEEN STR-27R. ACCORDING TO PREVIOUS OPERATOR DOCUMENTATION, THE REPAIR WAS PERFORMED UNDER ETD2025-190-000892 GUIDELINES. DUE TO ITS CONDITION (TOOL MARKS AND POORLY DRISep 27, 2025 · N247JB · Emb ERJ190100IGWSDR VNAA202510300006Skin · corrodedCORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR. CORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV -Sep 26, 2025 · N630NN · Cndair CL6002D24SDR IPXA2025100857008Skin · damagedRIGHT EXTERNAL UPPER FUSELAGE, STA 700-720 BETWEEN STR 6R-7R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN PREVIOUS REPAIR. REMOVED 1 EA RIVET AT RH EXTERNAL UPPER FUSELAGE, STA 700-720 BETWEEN STR 5R-6R IAW B757-200PF SRM 51-40-02. INSTALLED REPAIR DOUBLESep 26, 2025 · N457UP · Boeing 75724APFSDR IPXA2025100955989Skin · damagedEXTERIOR RT FUSELAGE STA 1320-1340, BETWEEN STR 7R-8R HAS (1EA) HOLE AT SKIN CAUSED BY LIGHTNING STRIKE. EVALUATED DAMAGE: ORIGINAL TICKNESS: 0.045 IN, 100% MATERIAL LOSS FOUND IT OUT OF LIMITS IAW SRM 53-00-01-1A-1. INSTALLED RIVET IAW SRM 51-40-02 AND SRM 5Sep 26, 2025 · N457UP · Boeing 75724APFSDR IPXA2025100857342Skin · damagedRIGHT EXTERNAL UPPER FUSELAGE, STA 540-560 BETWEEN STR 7R-8R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN.PERFORMED HFEC SURFACE INSPECTION ON EXTERNAL SKIN ONLY AT STA 540-560 BTW STR 7R-8R IAW. NTM 51-00-19 PART6.INSTALLED FASTENER ON. RH EXTERNAL UPPERSep 26, 2025 · N457UP · Boeing 75724APFSDR DALA2025100807328Skin · damagedSHIP 9540 DUE ER/A 628896-14 REV. ORIG. SECTION II PERMANENT REPAIR INSTRUCTION FOR RIGHT SIDE FUSELAGE SKIN DAMAGED AT STA. 237"- STA. 294". COMPLIED WITH PERMANENT REPAIR PER B717-200 SRM 53-00-01 (1219111)Sep 26, 2025 · N995AT · Boeing 717200SDR DALA2025092907062Skin · delaminatedDELAMINATED LOWER SKIN COMPARTMENT 510, 511, 512 ON GALLEY 5 AT AFT GALLEY AREA. COMPLIED WITH A.A WORK CARD 2530-01591-02D. (1220081).Sep 26, 2025 · N353NB · Airbus A319114SDR DALA2025092907047Skin · crackedFWD PAX DOOR CUTOUT AFTER LOWER CORNER HOLE NO. 4 IS CRACKED. REPAIRED FWD PAX DOOR CUTOUT AFTER LOWER CORNER IAW B767 SRM 53- 10-01-2R REPAIR 1. (1219987)Sep 26, 2025 · N173DZ · Boeing 767332SDR DALA2025092907046Skin · crackedSHIP 1703 FWD SERVICE DOOR CUTOUT AFT LOWER CORNER HOLE NO. 4 IS CRACKED. CRACK WAS FOUND DURING NDI INSPECTION. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REFER TO AA 5331-01288. CORRECTIVE ACTION: REPAIRED FWD SERVICE DOSep 26, 2025 · N173DZ · Boeing 767332SDR R61A2025092700417Skin Panel · dentedMULTIPLES DENTS ON RH FUSEALGE SKIN FRAME 5 THROUGH 13 STRG 12R TO 15R. REMOVED AND REPLACED BOTH SKINS FROM FR 5 TO FR 13, STR 12R - 15R IAW SRM 51-40-08Sep 26, 2025 · N767YX · Emb ERJ170200LRSDR DALA2025092607018Skin · ground damageFWD CARGO SURROUND SKIN / FR19 STR 37R-39R / IMPACT DAMAGE. COMPLIED WITH ERA 628935- 14 REV ORIG. (1218334)Sep 26, 2025 · N810NW · Airbus A330323SDR R61A2025101700467Skin · corrodedDURING C-CHECK FWD FUSELAGE EXTERNAL SKIN BETWEEN FR-10-11 STR 17L - 18L FOUND TOLLING MARKS AND DENT AROUND FASTENERS. REPAIRED IAW ETD 2025-170-929153Sep 25, 2025 · N810MD · Emb ERJ170100SUSDR GTIA2025092939097Skin Panel · crackedCRACK INDICATION FOUND IN FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR 68 DOOR STOP FITTING 1 RH SIDE. RAF 3589624-01 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #1 RH SIDE SRM 53-41-12-300-0Sep 25, 2025 · N623NK · Airbus A320232SDR GTIA2025092939096Skin Panel · crackedCRACK INDICATION FOUND IN FASTENER HOLE ( LOWER INBOARD POSTION) LOCATED AT FR 68 DOOR STOP FITTING 6 LT SIDE. RAF 3589623-02 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #6 LH SIDE IAW SRM 53-41-12-3Sep 25, 2025 · N623NK · Airbus A320232SDR DALA2025092907038Skin · damaged(LOG 1216613) LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BS708, S-6L. LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BS708 S-6L WAS REPAIRED IAW ER/A 629393-14AD REV ORIGINAL.Sep 25, 2025 · N938DZ · Boeing 7379GPERSDR DALA2025092607021Skin · ground damageFWD CARGO SURROUND SKIN, FR19, STR 37R - 39R, IMPACT DAMAGE. REPAIRED PER ERA 628935-00. (1217760)Sep 25, 2025 · N810NW · Airbus A330323SDR DALA2025092607020Repair · not reportedFWD FUSELAGE, FR18 & 19, STGR 39RT, LOWER SKIN PANEL, DOUBLER REPAIR. COMPLIED WITH ERA 629171-14. (1217643)Sep 25, 2025 · N810NW · Airbus A330323SDR DALA2025092607017Skin · damagedSHIP 3310 LOWER SKIN PANEL P/N F5327060020000 DAMAGED BELOW STRG 39 R/H AT FR 19. REPAIRED PER ERA 629171-14 REV. ORIG. (1218232)Sep 25, 2025 · N810NW · Airbus A330323SDR SWAA2025103017806Bear Strap · crackedCRACK INDICATION ON BEAR STRAP FWD GALLEY DOOR AREA, BS 291-294.5, S8 - 9R .CRACK LENGTH 0.187 IN. REPAIRED IAW SRM 53-10-01-2R-6 AND EA M-25-153-01539.Sep 24, 2025 · N907WN · Boeing 7377H4SDR CALA2025101309979Skin · corrodedPOSSIBLE CORROSION ON UPPER SKIN STA 727E BTW STR 3L TO 4L. PERFORMED INTERIM REPAIR ON FUSELAGE SKIN AT STA 727E BETWEEN STRG 3L TO STRG 4L, ALL WORK PERFORMED IAW EC/RA 5360-02016 REV ORIG AND EO 250328 REV IR. REPAIR REQUIRE REPETITIVE INSPECTIONS PERFORMSep 24, 2025 · N77525 · Boeing 737824SDR ASAA2025092461321Skin · damagedREF LOG 60949227, BIRD STRIKE FWD LH FUSLAGE AND NOSE AT APPROX 7,500 MSL. MIG-2C # 40-0058301 INITIATED. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MAJOR REPAIR AT FWD LH FUSELAGE NOSE SKIN PANEL 141A3521 BETWEEN STA 178-188 JUST BELOE STGR 24L IAW B737-700 SRSep 24, 2025 · N619AS · Boeing 737790SDR DALA2025100207168Skin · damaged(LOG 1215720) WHILE PERFORMING LIGHTNING STRIKE INSPECTIONS, MAINTENANCE OBSERVED LIGHTNING DAMAGE AROUND COMMON TO 2/EA FASTENERS LOCATED ON THE FUSELAGE SKIN (P/N 141A3521-38) AT APPROX. STA 278 AND 285 JUST BELOW STR26R. MAINTENANCE REPAIRED DAMAGE PER ERA Sep 24, 2025 · N828DN · Boeing 737932ERSDR DALA2025092907024Skin · no discrepancyDAMAGE TOLERANCE EVALUATION (DTE) REQUIRED. ER/A 629295-14 SECTION I ISSUED FOR A FUSELAGE SKIN REPAIR AT FR 69-FR 70, S- 28R TO S-32R. SECTION I, ACCOMPLISHED DURING MSP LINE VISIT 23SEP25. FOLLOW ON ACTION IS REQUIRED. REPAIR APPROVAL IS LIMITED TO 200 FCSep 24, 2025 · N325US · Airbus A320211SDR DALA2025092907023Skin · corrodedWHILE WALKING PAST THE ACFT, NOTICED CORROSION AROUND THE WASTE TANK VACUUM GENERATOR EXHAUST PORT. REMOVED EXISTING FASTENERS IN REPAIR A320 SRM 53-41-11 WIP .145518. WORKING REPAIR ON ERA 629295-14. -728756. COMPLETED REPAIR ON ERA 629295-14. OPS CHECK OF LSep 24, 2025 · N325US · Airbus A320211SDR AALA202509272720Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE SKIN AROUND AFT LAVATORY VACUUM VENT LOCATED AT BS 917 FROM S21L AND S22L. ACCOMPLISHED TRIPLER REPAIR PER SRM 53-70-01-2R REPAIR AND EA 368349.Sep 24, 2025 · N960AN · Boeing 737823SDR CALA2025092609298Skin Panel · gougedGOUGES FOUND ON EXTERIOR SKIN BETWEEN BS 727G AND 727H OTBD OF STRINGER 1. REPAIRED IAW EC/RA 5331-03181.Sep 24, 2025 · N37273 · Boeing 737824SDR FDEA202509241785Skin · misrepairedUPON EVALUATION FOUND EXISTING DOUBLER REPAIR ON FUSELAGE SKIN STATION 999 TO 1009 BETWEEN RIGHT HAND LONGERON 31 TO LONGERON 33 DOES NOT COMPLY TO CURRENT SRM 53-00-15-2R REPAIR 8 FIGURE 202. FUSELAGE SKIN AT STATION 999 TO STATION 1009 BETWEEN RIGHT HAND Sep 24, 2025 · N583FE · Doug MD11FSDR FDEA202509241781Skin · crackedNR 1 AIR-CON RAM AIR EXHAUST CUTOUT SUSPECT CRACK AT SKIN LEFT HAND STATION Y= 587. CRACKED SKIN AT NR 1 AIR-CON RAM AIR EXHAUST CUTOUT AT LT BS 587 AREA. REPAIRED IAW SRM 53-20-15-2R REPAIR 3, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIASep 24, 2025 · N574FE · Doug MD11FSDR FDEA202509241780Doubler · crackedNR 1 AIRCON RAM AIR EXHAUST ASSEMBLY CUTOUT PRODUCTION DOUBLER FOUND CRACKED AT LEFT HAND STATION 561.667. CRACKED DOUBLER AT FUSELAGE #1 AIRCON RAM AIR EXHAUST ASSEMBLY CUTOUT AT LEFT HAND STATION 561.667 REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PESep 24, 2025 · N574FE · Doug MD11FSDR JR2R20250924210Doubler · corrodedTEXAS DOULBER AT FRAME 90, RBL 24, IS CORRODED. OUT OF LIMITS. REPLACEDSep 24, 2025 · N85355 · Emb ERJ170200LRSDR REXA2026052600632Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH WAS REPAIRED PER REO 670-53-00-290 REV -ESep 23, 2025 · N228PQ · Cndair CL6002D24SDR DALA2025092907035Skin · ground damage(LOG 7472984) AIRCRAFT SUSTAINED IMPACT DAMAGE; SECTION 41 LOWER LOBE FORWARD OF E&E DOOR. PERFORMED FRAME REPAIRS PER BOEING DRAWINGS 141A1501, 141A1502 AND 141A1503. SKIN INSTALLATION PER BOEING DRAWING 141A0650, 141A3501 AND 141A3502. ASSOCIATED REPAIRS C/WSep 23, 2025 · N3742C · Boeing 737832SDR DALA2025092907032Skin · cracked(LOG 1213937) GROUND POWER RECEPTACLE SURROUND STRUCTURE TAB BETWEEN DOOR HINGES IS CRACKED. REMOVED AND REPLACED DOUBLER AND TRIPPLER PER ER/A 585833-14 REV A SECTION II. COMPARED TO PRI REV 1, 2, 3, 4 AND 5. ALL WORK STEPS COMPLETE.Sep 23, 2025 · N3742C · Boeing 737832SDR DALA2025092506984Skin · ground damageA GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RT. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1213648).Sep 23, 2025 · N319NB · Airbus A319114SDR DALA2025092506981Skin · ground damageA GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RH. COMPLIED WITH ER/A 628044-14. (1213814).Sep 23, 2025 · N319NB · Airbus A319114SDR BAGA2025092400006Skin · corrodedHEAVY CHECK, REAR FUSELAGE AT FR 79 LOWER SKIN FOUND CORRODED, REPAIRED PER REO.Sep 23, 2025 · N216BZ · Airbus BD5001A11SDR R61A2025101700468Skin · corrodedDURING C-CHECK FWD FUSELAGE EXTERNAL SKIN BETWEEN FR-05 -FR-06 STR 23L -24L FOUND UNRECORDED RIVET PLUG. REPAIRED IAW ETD 2025-170-929403Sep 22, 2025 · N810MD · Emb ERJ170100SUSDR CALA2025101510111Skin · corrodedFR 34 AREA I STRG 42L HAS CORROSION. REPAIRED STR 42L BETWEEN FR34-29 IAW SRM 53-21-13-300-018.Sep 22, 2025 · N832UA · Airbus A319131SDR CALA2025092409216Skin · nickedLEFT FUSELAGE AFT STATIC PORT CABIN PRESSURE HAS EVIDENCE OF SMALL NICKS. REPAIRED PER ECRA 5360-02022.Sep 22, 2025 · N14118 · Boeing 757224
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