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 N6WA2020112302Doubler · corrodedCORROSION ON TCAS ANTENNA DOUBLER AT FS 295-FS 310 STRG 27. REMOVED AND REPLACED TCAS ANTENNA DOUBLER AT FS 295-FS 310 STG 27, IAW CRJ 700 SRM 51-42-06. Nov 23, 2020 · N502GJ · Cndair CL600*SDR VNAA202011239994Skin · chafedREPAIR DOUBLER BETWEEN FS 969.00-958.00 AND STRINGER 26L-26R IS CHAFED.Nov 23, 2020 · N500AE · Cndair CL6002C10SDR SWIA202055597Skin · corrodedEXTERNAL SKIN APPROXIMATELY 6 EA RIVETS SHOW SIGNS OF CORROSION STGR 25R BETWEEN FS 939/969, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM LOWER EXTERNAL SKIN, IAW CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND REPLACED RIVETS, IAW CRJ700 SRM 51-42-Nov 22, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055560Skin · dented2 EA DENTS IN EXTERNAL FUSELAGE STGR 27 JUST AFT OF FS 969, AS MARKED. C-CHECK RO 1/17/2021. THE BLENDS ON THE EXTERNAL SKIN AT STRG 27 JUST AFT OF FS 969 IS STRUCTURALLY ACCEPTABLE, REF MHIRJ REO 670-53-00-644 REV- DATE 2020-12-02. THE 2 EA DENTS IN EXTERNNov 22, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055559Skin · dentedEXTERNAL SKIN DENT AND GOUGE AT STGR 27 JUST FWD OF FS 985, AS MARKED. C-CHECK RO 1/17/2021. BLENDED GOUGE TO SMOOTH CONTOUR, REF CRJ700 SRM 51-12-00-001-001-A01. DAMAGE IS OUT OF LIMITS, REF CRJ700 SRM 53-61-01-101-003-A01. FABRICATED AND INSTALLED REPAIRNov 22, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055558Skin · gougedEXTERNAL SKIN 1.5" GOUGE AT STGR 27 JUST AFT OF FS 985. C-CHECK RO 1/17/2021. BLENDED GOUGE AT STRG 27 JUST FWD OF FS 985, REF CRJ 700 SRM 51-12-00-001-001-A01. THE BLEND ON THE EXTERNAL SKIN AT STRG 27 JUST FWD OF FS 985 IS STRUCTURALLY ACCEPTABLE, REF MHINov 22, 2020 · N758EV · Cndair CL6002C10SDR SWAA2020121431822Skin · crackedRIGHT FWD LOWER FUSELAGE EXTERNAL POWER COMPARTMENT CUTOUT CRACKED BELOW ACCESS DOOR LOWER HINGE, MARKED. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE BETWEEN STA 227 & STA 235 WL 176. ELECTRICAL GROUND POWER RECEPTACLES SURROUND DOUBLER BELOW ACCESS DOOR LOWERNov 22, 2020 · N7717D · Boeing 73776NSDR SWIA202055955Skin · damagedRH FUSELAGE SKIN HAS HOLE BELOW STRINGER 11 AT APPROX FS 1151. VISABLE FROM WITHIN AEB (EXTERIOR SKIN IS COVERED BY RH PYLON). (C-CHECK) RO 2/5/2021 FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO # T-52592 AND FABRICATED SHIM FROM 2024-T3 .080 PO # T-55Nov 21, 2020 · N716EV · Cndair CL6002C10SDR SWIA202055543Doubler · corrodedTCAS OMNIDIRECTIONAL ANTENNA DOUBLER IS CORRODED AROUND THE CONNECTOR PENETRATION, LOCATED AT STGR 27, BETWEEN FS 295 TO FS 310. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM THE TCAS ANTENNA DOUBLER "OUT OF LIMITS". REMOVED AND REPLACED THE TCAS ANTENNA AT Nov 21, 2020 · N758EV · Cndair CL6002C10SDR JJBA20201121020Skin · dentedDENT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L. LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L, SKIN REPAIRED.Nov 21, 2020 · N13124 · Emb EMB145XRSDR JJBA20201120015Doubler · damaged2 REPAIR DOUBLER ON LOWER REAR FUSE 1, BETWEEN FR 64-66 AND BETWEEN STR 19L-20R. 2 EXISTING DOUBLER REMOVED FOR ENGINEER REVIEW. AFTER FURTHER INVESTIGATION, MORE DAMAGE FOUND UNDERNEATH FWD DOUBLER AND CUT OUT ENLARGED TO REMOVED ALL DAMAGE FOR ENGINEERING Nov 20, 2020 · N11137 · Emb EMB145XRSDR JGVR20201120003Skin · corrodedFOUND 17 AREAS OF VERIFIED CORROSION ALONG FUSELAGE AFT CHIN FAIRING. FOUND ADDITIONAL 120 AREAS OF CORROSION UNDER AFT CHIN FAIRING. REPAIRED BLENDED AREAS OF LEVEL 2 CORROSION ON LOWER FUSELAGE SKIN UNDER AFT CHIN FAIRING BY INSTALLING REPAIR DOUBLERS. ALNov 20, 2020 · N375QS · Cessna 680ASDR ASAA2020111934513Skin · damagedREF LOG PAGE 60063891 - DURING A/C LOADING FOUND DAMAGE TO A/C AT STA 811 AND AT STRINGER S26R & S27R JUST BELOW AFT CARGO DOOR THRESHOLD GROUNDED - YES. (RESOLVED ON W/O: 1855193 TASKCARD: N/R-00001 ) REPAIRED DAMAGE AT STA 811 BETWEEN STR 26R AND 27R BELOW ANov 19, 2020 · N609AS · Boeing 737790SDR R61A2020122100916Skin · dentedDOUBLER APPEARS TO BE OIL CANNED OR DENTED BETWEEN FR 1/FR 2 AND STGR 2R. FOUND TO BE ALLOWABLE, IAW ETD2020-170-033556.Nov 19, 2020 · N241JQ · Emb ERJ170200LRSDR JJBA20201119014Skin · damagedMULTIPLE DAMAGES ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L. ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L SKIN STRIPES. ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETNov 19, 2020 · N11137 · Emb EMB145XRSDR DALA2020112003801Skin · dentedDURING INSPECTION FOUND DENTED FUSELAGE SKIN ON PREVIOUS REPAIR RIVET REPAIR AREA AT STA 417 STR 26R. FUSELAGE SKIN AT STA 417 STR 26R WAS REPAIRED, PER ETI-37-20-356 REV ORIGINAL AND ERA 588727-14.Nov 19, 2020 · N383DN · Boeing 737832SDR ASMF202101011Skin · corrodedREVISION, DETECTING A BULGE OF 2.00" LENGTH, 0.875" WIDTH AND 0.1875" DEPTH AND A DENT OF 1.3125" LENGTH, 1.0625" WIDTH AND 0.021" DEPTH WITH THREE FASTENERS DAMAGES IN FUSELAGE SKIN RIGHT COUNTER FRAME APU ACCESS DOOR. APU COWL DOOR WAS REMOVED, IAW AMM 52-4Nov 18, 2020 · N950AM · Boeing 737852SDR SWIA202054657Skin · dentedEXTERNAL SKIN HAS DENT LOCATED APPROXIMATELY AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L. C-CHECK RO 12/14/2020. CUT DAMAGE OUT AND INSTALLED DOUBLER AT EXTERNAL SKIN AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L, REF CRJ 700 SRM.Nov 18, 2020 · N750EV · Cndair CL6002C10SDR MASA20201119087Skin · corrodedC-CHECK SKIN CORROSION FS 280-FS 295 STGR 25L-26L. R & R SKIN PANEL PN SH670-31633-7S BETWEEN FS 280-FS 333, IAW SRM 51-42-06 & 51-40-11.Nov 18, 2020 · N918FJ · Cndair CL6002D24SDR 2020F00450Skin · corrodedRT NOSE SKIN CORROSION ENGINEERING LETTER DQ27848M1.Nov 18, 2020 · N642QS · Cessna 560XLSDR 2020F00449Skin · corrodedLT NOSE SKIN CORROSION ENGINEERING LETTER DQ27848M1.Nov 18, 2020 · N642QS · Cessna 560XLSDR SWAA2020112330861Skin · cracked7' CRACK FROM FASTENER TO FASTENER AT RBL 54.0, JUST ABOVE HYDRAULIC SERVICE PUMP IN GFRP WEB MATERIAL. PERFORMED INTERIM REPAIR, IAW SRM 57-10-10-1A-2 2C (3)(A). SPEED TAPE TO BE REINSPECTED FOR CONDITION EVERY 600 FLT CYCLES, REF EA OTHER 57 EA 03738, REF Nov 17, 2020 · N8600F · Boeing 7378H4SDR MASA20201117081Floor Support · corrodedC-CHECK CORROSION ON LONGITUDINAL FLOOR BEAM BOTTOM OF UPPER CORD. REMOVED AND REPLACED FLOOR BEAM.Nov 17, 2020 · N918FJ · Cndair CL6002D24SDR SWIA202055954Skin · damagedEVALUATE CREASE @ FS 409 ABOVE STGR 20L. (C-CHECK) RO 2/5/2021 INSTALLED REPAIRED DOUBLER-1 AND REPAIR SHIM-2. REF: REO 670-53-21-1888 REV. -- DATE: 2020-12-14. PRESSURE CHECK GOOD. / COMPLIED WITH ALL STEPS OF REO 670-53-21-1888 REV -- DATED 2020-12-14. CNov 16, 2020 · N716EV · Cndair CL6002C10SDR SWIA202054726Lap Joint · corrodedCORROSION FOUND AT AT STR 21L AT FS 333.00 ON CIRCUMFERENTIAL JOINT. C-CHECK RO 12/24/2020. REPAIRED CORROSION AT STR 21L AT FS 333.00 CIRCUMFERENTIAL JOINT, IAW MHIRJ REO & SKY CARD NOTE DTA REQUIREMENTS WILL BE PROVIDED WITHIN 12 MONTHS. NO WIEGHT CHANGESNov 16, 2020 · N754EV · Cndair CL6002C10SDR JJBA20201116019Skin · deformedFWD FUSELAGE LT SIDE, THE SKIN IS DEFORMED AROUND THE TAT PROBE. ON FWD FUSELAGE LT SIDE SKIN, AROUND TAT PROBE, PAINT STRIPPED FOR INVESTIGATION. TAT PROBE INNER BASE REMOVED FOR INVESTIGATION. AFTER INVESTIGATION, THE TAT PROBE INNER BASE FOUND WITH DEFORNov 16, 2020 · N13124 · Emb EMB145XRSDR ASAA2020111633587Skin · dentedDURING A/C LOADING FOUND DAMAGE TO A/C AT STA 811 AND AT STRINGER S26R & S27R, JUST BELOW AFT CARGO DOOR THRESHOLD. GROUNDED-YES. REPAIRED DAMAGE AT STA 811 BETWEEN STR 26R AND 27R BELOW AFT CARGO DOOR, IAW ALASKA AIRLINES EA 700-53EA-23054.Nov 16, 2020 · N609AS · Boeing 737790SDR JJBA20201116011Doubler · damagedREPAIR DOUBLER ON LEFT HAND CENTER FUSE I, BETWEEN FR 19-20 AND STR 11L-13L. ON LEFT HAND CENTER FUSE 1 BETWEEN FR 19-20 AND STR 11L-13L REPAIR DOUBLER REMOVED FOR INVESTIGATION ON LEFT HAND CENTER FUSE 1 BETWEEN FR 19-20 AND STR 11L-13L DAMAGE FOUND UNDERNEANov 16, 2020 · N11137 · Emb EMB145XRSDR SWIA202055400Skin · dentedFS 169.0 EXTERNAL SKIN ON UPPER LEFT SIDE HAS SEVERAL DENTS. C-CHECK RO 1/16/2021. INSTALLED NEW LT NOSE SKIN P/N 600-33052-113, REF CRJ 200 SRM 51-42-06, CRJ200 SRM 51-42-13, DWG 600-33052 REV -W. COMPLIED WITH 51-900-1003-SKY.Nov 15, 2020 · N868AS · Cndair CL6002B19SDR DALA2020111603731Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR 3 TO FR 4 AND 5 INCH ABOVE OF LT LOWER STRINGER LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOCATED EXTERNAL SKIN BETWEEN FR 3 TO FR 4 AND 5 INCH ABOVE OF LT LOWER STRINGERNov 15, 2020 · N369NB · Airbus A319114SDR TIPR2020121444717Skin · not reportedFUSELAGE SKIN PN 65C35785-44 BS 360 TO BS 540, S4R TO S10R REQUIRES REPLACEMENT, REPLACED SKIN.Nov 14, 2020 · N303KH · Boeing 737319SDR REXA2020111800755Skin · dentedSKIN DAMAGE MEASURING .750" L LOCATED AT FWD FS 672 BETWEEN STGR 27 &26L. REPAIRED SKIN DAMAGE LOCATED FWD OF 672, IAW ENDEAVOR EA CRJ253-10934 REV IR DATED 10-31-2020 THIS IS A MAJOR REPAIR.Nov 14, 2020 · N8839E · Cndair CL6002B19SDR JJBA20201113010Skin · crackedREAR FUSE 1, LOWER SKIN CRACKED AT FR 75A BETWEEN STR 21P-21S. REPAIRED DOUBLER AND TRIPLER INSTALLED AND FRAME BOTTOM SECTION REPLACED.Nov 13, 2020 · N11106 · Emb EMB145XRSDR A6WA202011137418Skin · crackedTRANSFORMER RECTIFIER SUPPORT SKIN CRACKED BETWEEN FS 193.00 AND HYDRAULIC SYSTEM 2 & 3 ACCUMULATOR SUPPORT BRACKET. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RECTIFIER SUPPORT SKIN AT FS 193, IAW REO 601R-53-11-111.Nov 13, 2020 · N454AW · Cndair CL6002B19SDR SWAA2020121433735Strap · corrodedCORROSION EXTERNAL SKIN STRAP AT TOILET SERVICE CUT OUT AT LOWER FUSELAGE WL 152.5 AND BS 847 TO BS 867 BETWEEN S-24L AND 25L. BLENDED EXTERNAL SKIN STRAP AT TOILET SERVICE CUT OUT AT LOWER FUSELAGE WL 152.5 AND BS 847 TO BS 867 BETWEEN S-24L AND S-25L MEASURNov 12, 2020 · N932WN · Boeing 7377H4SDR DALA2020111203694Doubler · damagedDURING INITIAL INSPECTION MAINTENANCE FOUND A DENT AND NICK ON PREVIOUSLY REPAIRED DOUBLER STA 620 BETWEEN STGR 16L-17L. REPAIRED PER 588549-14.Nov 12, 2020 · N588NW · Boeing 757351SDR SWAA2020113032528Skin · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER ACCESS DOOR ON FUSELAGE SKIN AT LOWER FUSELAGE. PERFORMED REPAIR EXTERNAL SKIN GROUND ELECTRICAL POWER ACCESS DOOR LOWER FUSELAGE, IAW SRM B737-700 53-10-15-2R-5 REPAIR 5. REPAIR IS CATEGORY B FOR INSPECTION REQUIREMENTNov 11, 2020 · N203WN · Boeing 7377H4SDR FDEA202011112832Skin · crackedFWD CARGO DOOR CUT OUT, AFT LOWER CORNER, SKIN HAS MINOR GOUGES ON EDGE OF REPAIR. REPAIRED LOWER AFT CORNER OF FWD CARGO DOOR FRAME, REF SRM 53-50-00 FIGURE 26 SHEETS 2, 3, 4, 5, AND 9 VOL 1 REF SRM 53-50-00 FIGURE 27 SHEET 2 VOL 1. SRM 51-31-01 VOL 2 SRM 5Nov 11, 2020 · N562FE · Doug MD1010FSDR UO2R2020111101Skin · corrodedRAZOR TOOL MARKS PRESENT ON FUSELAGE SKIN BELOW THE TOP FWD TCAS ANTENNA. DISCREPANCY FOUND DURING COMPLIANCE OF THE 72 CALENDAR MONTH SCHEDULED INSPECTION TASK 539005-UPPER ANTENNA AND PENETRATION INTERFACE-DETAILED INSPECTION. THE DAMAGE EXCEEDED MAXIMUM TNov 11, 2020 · N528QS · Gulstm GVSPG550SDR SWIA202055778Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54568-690-53-21-1168 MXCODEID49801-PR - DAMAGE TO FUSELAGE LOWER SKIN PANEL AND UPPER SKIN PANEL. PERFORMED TEMPORARY REPAIR PER REO 690-53-21-1168 REV -- DATED 2019-11-17. PERMANENT REPAIR DUE IN 2000 FLIGHT HOURS. Nov 10, 2020 · N161PQ · Cndair CL6002D24SDR SWIA202055538Skin · damagedFS 1031.00-FS 1051.00 STRG 23-24RT EXTERIOR SKIN PITTING DAMAGE, MARKED. C-CHECK RO 1/17/2021. REPAIRED AREA ON FUSELAGE SKIN BETWEEN FS 1031.00 TO FS 1051.00 BETWEEN STRINGER 23R TO STRINGER 24R TO COMPLY WITH REO 670-53-61-1778 REV- DATE 2020-12-02. SEE CNov 10, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055537Panel · erodedLEADING EDGE OF PANEL 341BR ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 341BR, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV -- DATE 2020-12-01.Nov 10, 2020 · N758EV · Cndair CL6002C10SDR SWIA202055536Panel · erodedLEADING EDGE OF PANEL 331BL ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 331BL, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV DATE 2020-12-01.Nov 10, 2020 · N758EV · Cndair CL6002C10SDR SWIA202054548Skin · damagedWHILE REMOVING PANEL 132AL FOUND EXISTING DAMAGE AROUND SCREW HOLE. C-CHECK RO 12/05/2020. BLENDED OUT TOOLING DAMAGE ON SKIN RING AT PANEL 132AL, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED AND RECEIVED ENGINEERING REF REO, ALL STENov 10, 2020 · N939SW · Cndair CL6002B19SDR SWAA2020113029754Skin · corrodedCORROSION ON FUSELAGE SKIN BS 886-888 BETWEEN STRS 2L-2R WL 308 RBL10-LBL10. REMOVED DAMAGE AT BS 886-888 BETWEEN STRS 2L-2R WL 308.5 RBL 10-LBL 10. DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-01-1A-1. REPAIRED AREA PER ATS ER 20-03531 REV IR AND SWA EANov 10, 2020 · N569WN · Boeing 7377CTSDR AALA202011179015Skin · wornAIRCRAFT IN BASE MAINTENANCE. BLEND OUT PREVIOUSLY ACCOMPLISHED TO REPAIR GOUGES ON FUSELAGE SKIN BELOW CAPTAIN WINDSHIELD AT BS 200 AND LBL 20 AT WL 246.1. DURING THE CURRENT MAIN BASE VISIT ADDITIONAL WEAR DAMAGE WAS FOUND, WHICH EXCEEDED LIMITATIONS. REPNov 10, 2020 · N983NN · Boeing 737823SDR HNAA2020111200317Skin · crackedLT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 4 EA FR 79. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 78, IAW PIEDMONT EO1-53-20-0407. 2 LOCATIONS WERE FOUND NOT TO BE CRACKED.Nov 10, 2020 · N906AE · Emb EMB145LRSDR HNAA2020111200316Skin · crackedLT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 79. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 79, IAW PIEDMONT EO1-53-20-0407.Nov 10, 2020 · N906AE · Emb EMB145LRSDR HNAA2020111200315Skin · crackedLT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 2 EA FR 77. REPAIRED LT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT 2 EACH RIVETS AT FR 77, IAW PIEDMONT EO1-53-20-0407.Nov 10, 2020 · N906AE · Emb EMB145LRSDR HNAA2020111200314Skin · crackedRT EXTERNAL UPPER FUSELAGE SKIN CRACKED AT RIVETS 5 EA FR 77. INSTALLED SERVICEABLE RIVET AND REPAIR SKIN BUSHING AT FR 77 BETWEEN STR 8R-9R, IAW EO1-53-20-0406. SEE WIPS AND TASKS FOR DETAILS.Nov 10, 2020 · N906AE · Emb EMB145LR
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