JASC 5330

Service difficulty reports · 79,281

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 CALA2026072617990Skin · scratchedTHREE SCRATCHES ON RT PRIMARY STATIC PORT (A-73). BLENDED AND EVALUATED SCRATCHES ON THE RT PRIMARY STATIC PORT, BLEND NR 1 LOCATED BTW BS 417 AND 4" ABOVE OF THE S16R ORIGINAL THICKNESS: 0.080" MATERIAL LOSS: 0.002" MATERIA L REMAINING: 0.078", BLEND NR 2 Jul 11, 2026 · N37319 · Boeing 7378SDR CALA2026071217702Skin · corrodedL/H EXTERIOR FUSELAGE SKIN HAS CORROSION AROUND LAV EXHAUST VENT BETWEEN BS907 AND BS927 AND BETWEEN STR S-21L AND STR S-22L. REMOVED DAMAGE REF SRM 53-00-01-1A-1. ORIG .125, REMOVED .012, REMAINING .113 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A FIG 103 DJul 11, 2026 · N87507 · Boeing 737824SDR CALA2026071417747Skin · damagedLIGHTNING STRIKE DAMAGE LOCATED AT STATION 214 AND 7" BELOW FLOOR LINE STRINGER 17R. DAMAGE IS AWAY FROM FASTENER.BLENDED AREA REMOVED .017" OF MATERIAL ORIGINAL THICKNESS IS .040". BLEND IS OUT OF LIMITS. A REPAIR IS NEEDED FOR THIS AREA. REQUESTING A THICKNEJul 11, 2026 · N78501 · Boeing 737824SDR DALA2026071304094Skin · crackedHOLE H378 CRACKED AT THE FITTING LAYER OF FR 40 LOWER SHELL PANEL JUNCTION ON THE LH SIDE. IT IS AT THE 11 O`CLOCK DIRECTION. AND HOLE H362 CRACKED AT THE SKIN LAYER OF FR 40 LOWER SHELL PANEL JUNCTION ON THE LH SIDE. IT IS AT THE 5 O`CLOCK DIRECTION. CORRECTIJul 11, 2026 · N801NW · Airbus A330323SDR HNAA2026081400721Skin · crackedRIGHT EXT SKIN CRACKED AT FR75 BTW 2R-3R. REPAIRED IAW SRM 53-31-01Jul 10, 2026 · N939AE · Emb EMB145LRSDR SWIA2026071076734Doubler · corrodedWASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER CORRODED. REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER. IAW SRM 51-40-08. O.E.M. PART INSTALLED.Jul 10, 2026 · N146SY · Emb ERJ170200LRSDR CALA2026072117934Skin · corrodedPOSSIBLE CORROSION UNDER VACUUM WASTE PAN SKIN. (REF. AAR NR 1000079184). PERFORMED REPAIR AT VACUUM WASTE PAN SKIN AREA BTW STA 847 TO STA 867 AND S-23L TO S-25L IAW EO 260347 REV. P1, EO 260347 REV. P2, EO 260347 REV. IR AND EC/RA 5360-02179.Jul 10, 2026 · N38257 · Boeing 737824SDR FDEA202607100893Skin Panel · dentedUPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I.A.W B757 SRM 53-80-01-1A, TABLE I, NOTE 'C', FIG 101, SHEET 2 AND SRM 51-70-10-2R REP '4'Jul 10, 2026 · N935FD · Boeing 7572T7SDR FDEA202607100891Skin · dentedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DJul 10, 2026 · N140FE · Boeing 767300SDR R61A2026080200216Skin · damagedLIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R.MECHANIC REMOVED DAMAGE AND PERFORMED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R IAW ETD2026-170-012519 REV. AJul 9, 2026 · N865RW · Emb ERJ170100SESDR R61A2026080200214Skin · damagedLIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 3-4 STRINGERS 22R-24R.MECHANIC CUT OUT LIGHTNING STRIKE DAMAGE,FABRICATED, DRILLED AND INSTALLED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 3-4 AND STRINGERS 22R-24R IAW ETD2026-170-012124Jul 9, 2026 · N865RW · Emb ERJ170100SESDR YENA2026071500578Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN ON CUTOUT OF ACCESS PANEL 351AL LOWER FUSELAGE. (RESOLVED ON W/O: 1494820 TASKCARD: NR-00001 ) REF AEM WO 2026 303/1 NR 2026-348233. ACCP REPAIR CORROSION AND CRACKS ON TAIL CONE EXTERNAL SKIN BETWEEN FR81-8Jul 9, 2026 · N809JB · Airbus A320232SDR DALA2026071304114Floor Support · corrodedCORROSION ON FWD CARGO COMPARTMENT LOWER SILL AROUND FASTENER HOLES. COMPLIED WITH ER/A 635498-14 REV ORIGINAL ASSOCIATED ER/A 14-635498 ADDED FOR AC 8132. (LP# 1690635; AIRCRAFT WAS GROUNDED)Jul 9, 2026 · N132DU · Airbus BD5001A10SDR DALA2026071304084Skin · scratchedFWD UPPER FUSELAGE AROUND PCS/TIMING ANTENNA CUTOUT AT FR29+ 195MM AND BETWEEN STRINGER 1L-1R SKIN PANEL WITH SCRATCH. C/A: PERFORMED FUSELAGE SKIN REPAIR BETWEEN FR 29 AND FR 30 AT STGR 1R IAW DELTA ER/A # 635410-14 REV: ORIGINAL DATED 03-JUL-26. NOTE: PERFORJul 9, 2026 · N352NW · Airbus A320212SDR DALA2026071304083Skin · nickedFWD FUSELAGE FR13+65MM AND 400MM ABOVE OF LEFT SIDE STRG SKIN PANEL WITH NICK. PERFORMED PERMANENT FUSELAGE SKIN REPAIR AT FWD FUSELAGE FROM FR 12 +238MM TO FR 13 +155MM, BETWEEN Z-520 AND Z-742 L/H SIDE I.A.W A320 SRM 53-11-11-300-041 PARAG 1 AND PARAG 2A FIJul 9, 2026 · N352NW · Airbus A320212SDR FDEA202607090869Skin · dentedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DENT WAS MEASURED AJul 9, 2026 · N140FE · Boeing 7673S2FSDR FDEA202607090868Skin · crackedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DJul 9, 2026 · N140FE · Boeing 7673S2FSDR HNAA2026081400716Skin · crackedPOSSIBLE CRACK AROUND RIVET AT FR79 STRINGER 8R-9R. REPAIRED CRACKED SKIN AROUND RIVET AT FR79 BETWEEN STGR 8R-9R IAW EMB 145 SRM 53-32-01RE, ITEM 9, FIG 213, SHEETS 1,2,3 AND EO-1-53-26-0373.Jul 8, 2026 · N942LL · Emb EMB145LRSDR HNAA2026081400715Skin · crackedPOSSIBLE CRACK AROUND RIVET AT FR77 STRINGER 8R-9R. REPAIRED CRACKED SKIN AROUND RIVET AT FR77 BETWEEN STGR 8R-9R IAW EMB 145 SRM 53-32-01RE, ITEM 9, FIG 213, SHEETS 1,2,3 AND EO-1-53-26-0373.Jul 8, 2026 · N942LL · Emb EMB145LRSDR HNAA2026081400714Skin · crackedPOSSIBLE CRACK AROUND RIVET AT FR79 STRINGER 7L-8L. REPAIRED CRACKED SKIN AROUND RIVET AT FR79 BETWEEN STGR 7L-8L IAW EMB 145 SRM 53-32-01RE, ITEM 9, FIG 213, SHEETS 1,2,3 AND EO-1-53-26-0372Jul 8, 2026 · N942LL · Emb EMB145LRSDR HNAA2026081400713Skin · crackedPOSSIBLE CRACK AROUND RIVET AT FR78 STRINGER 7L-8L. REPAIRED CRACKED SKIN AROUND RIVET AT FR78 BETWEEN STGR 7L-8L IAW EMB 145 SRM 53-32-01RE, ITEM 9, FIG 213, SHEETS 1,2,3 AND EO-1-53-26-0372.Jul 8, 2026 · N942LL · Emb EMB145LRSDR R61A2026070800186Doubler · corrodedDOUBLER AT FR82-83 STGR28R-29R - LFEC INSPECTION DETECTED POSSIBLE CORROSION IN FASTENERS OR BETWEEN SKIN AND DOUBLER, AS MARKED EXTERNALLY. UPON VISUAL INSPECTION FROM INSIDE AFT CARGO. CORROSION NOTED AROUND ADDITIONAL FASTENERS OF DOUBLER REPAIR.Jul 8, 2026 · N133HQ · Emb ERJ170200LRSDR SWIA2026070777753Skin · damagedDENT & TOOL DAMAGE ON SKIN SURFACE BTWN BS 654 - 672, S26R. THE DAMAGED SKIN WAS REPAIRED IAW REO 601R-53-61-8613, REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.Jul 7, 2026 · N943SW · Cndair CL6002B19SDR DALA2026070804007Skin · corrodedERA 604935, REV A: FUSELAGE SKIN - FWD LEFT PASSENGER DOOR CUTOUT CORROSION. REF ERA 604935. (1687210) AIRCRAFT WAS GROUNDEDJul 7, 2026 · N3771K · Boeing 737832SDR DALA2026070803994Skin · crackedFOUND CRACK AT INBOARD OF XSR 164 AND THE LOWER WING SKIN BETWEEN STRINGER S-11 AND THE REAR SPAR, COMPLIED WITH ER/A 634526-14AD. (1686898) (AIRCRAFT GROUNDED).Jul 7, 2026 · N951AT · Boeing 717200SDR SWAA2026081792024Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-2, REPAIR 2.Jul 6, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081781900Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE. REPAIRED HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.Jul 6, 2026 · N8651A · Boeing 7378H4SDR FDEA202607060845Skin · damagedFOUND 1EA LIGHTNING STRIKE DAMAGE AT LOWER FUSELAGE AT SECTION 43 (STA654"88 - STA654"110 S37R-S38R) REPAIRED THE LIGHTNING STRIKE DAMAGE ON THE LOWER FUSELAGE SKIN AT STA654"88 - STA654"110, S37R - S38R PER SRM 53-00-01-2R REPAIR29, THIS IS A CATEGORY B Jul 6, 2026 · N103FE · Boeing 7673S2FSDR YENA2026070900558Skin · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 R H SIDE, CRACK DIRECTION: 07 OCLOCK, D1-D2= 0.165 INCH APPROX, AD RELAT ED TASK CARD NO. A320-Jul 5, 2026 · N568JB · Airbus A320232SDR MASA20260709175Skin Splice · corrodedCIRCUMFERENTIAL SKIN SPLICE FRM 74 BETWEEN S29L - S29R BLENDED IAW SRM 51-10-03, REV 53 AND FOUND WITHIN LIMITS IAW SRM 53-04-02 REV 46.Jul 5, 2026 · N85354 · Emb ERJ170200LRSDR DALA2026070703945Skin · corrodedAFTER REMOVAL WASTE PAN AT LOWER FUSELAGE WAS FOUND CORROSION ON EXTERNAL FUSELAGE SKIN. REPAIRED PER PRI 635303-14. (1682936) (AIRCRAFT GROUNDED)Jul 5, 2026 · N693DL · Boeing 757232SDR SWIA2026070476616Skin · dentedLARGE DENT FOUND BELOW CAPT WINDSHIELD DURING BIRD STRIKE INSPECTION, DENT MEASUREMENTS LENGTH-11.75IN, WIDTH 7.75IN, DEPTH 0.3125IN, AND STGR 02L UNDERNEATH DENT WAS FOUND TO BE BENT. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-01 FIG 101 SHEET 3. IAW GJul 4, 2026 · N505SY · Emb ERJ170200LRSDR YENA2026070900541Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN IN FROM O FFR28 PLUS1.487 IN AT LEVEL STR32 PLUS 1.795 INCH UNDER,LH LOWER FUSELAGE. ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON FR28 PLUS 1.487 IN AT LEVEL STR32 PLUS 1.795 INCH UJul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900540Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PLUS1.681 IN AT LEVEL STR 32 PLUS 2.567 IN UNDER, LT LOWER FUSELAGE. REF AEROMAN WO 2026-196/1NR 299252.ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PLJul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900539Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR27 TO FR28 AT LEVEL STR32 TO STR33 LH LOWER FUSELAGE;(RESOLVED ON W/O: 1457737 TASKCARD: NR-00047 ) REF AEROMAN WO 2026 196/1 NR 299041.ACCOMPLISHED REPAIR ON EXISTING REWORK ON EXACTJul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900538Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR 28 TO FR 29 AT LEVEL STR 32 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00048 ) REF AEROMAN WO 2026 196/1 NR 299042 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON Jul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900537Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 TO FR 27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00049 ) REF AEROMAN WO 2026-196/1 NR 299039 ACCOMPLISHED REPAIR ON EXISTING REWORK ONJul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900536Skin · damagedDURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN FR27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE IAW AEROMAN WO 2026-196/1 NR 299040 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN FR27 BTW STR 32LH AND STR 33LH IAW EA 53-Jul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900532Skin · damagedDURING HEAVY MAINTENANCE, EA A26-514-01. FUSELAGE FWD FUSELAGE EXTERNAL SKIN BTWN FR26-FR29 & STGR 32LH-33LH, EXISTING REWORKS – TIME LIMITED REPAIR(CONSIDERED MAJOR REPAIR)Jul 4, 2026 · N568JB · Airbus A320232SDR MASA20260709173Skin · corrodedFWD PASSENGER DOOR CUTOUT, SKIN EDGE IN CONTACT WITH SCUFFPLATE FR 17 TO 19 STGR 17L CORROSION IN SOME SPOTS. CORROSION REMOVED BY BLEND OUT IAW SRM 51-10-03 AND WAS FOUND WITHIN ALLOWABLE LIMITS IAW SRM 51-75-16, TABLE 101, REV 53. CORROSSION LEVEL 1Jul 4, 2026 · N85354 · Emb ERJ170200LRSDR DALA2026070703944Skin · damagedTWO ELONGATED HOLES LOCATED AT LOWER AFT CORNER AND LOWER FORWARD CORNER OF NR 1 CARGO DOOR CUTOUT IN REF CARD 5331 -01293-02A-01 STEP 6 & 7. REPAIRED PER ERA 635128-14 REV. (1681745) (AIRCRAFT GROUNDED)Jul 4, 2026 · N693DL · Boeing 757232SDR DALA2026070603930Skin · damagedDIVERTED TO IND DUE TO LIGHTNING STRIKE AFTER TAKEOFF FROM ORD. CORRECTIVE ACTION: PERFORMED LIGHTNING STRIKE INSPECTION AND PERMANENT REPAIR ON CROWN SKIN PER SRM. (8758506) AIRCRAFT WAS GROUNDEDJul 4, 2026 · N901DN · Boeing 737932ERSDR DALA2026070303902Skin · corrodedAIRCRAFT 3301, FOUND CORROSION LEVEL 2 ON LOWER FUSELAGE SKIN NEAR BTW FRAME 76 TO FRAME 77 AND BTW STR 40L TO 41L LOWER FUSELAGE CORRECTIVE ACTION: CORROSION REMOVED BY BLEND OUT, THE REWORKED AREA MEASURED AND EVALUATED: THE REMAIN THICKNESS IS 1.60MM<1.80MMJul 3, 2026 · N801NW · Airbus A330323SDR CALA2026070217528Skin · damagedLIGHTNING STRIKE BS 275 AND STR 6 LH AT FUS. SKIN. FOUND TO BE OUT OF LIMITS, REQUIRE REPAIR. PERFORMED THE REPAIR TO FUSELAGE SKIN P/N 141A3112-1 IAW EC/RA 5310-08955. (REF AAR NR 1000081138) PERFORMED THE REPAIR TO FUSELAGE SKIN P/N 141A3112-1 IAW EC/RA 5310Jul 2, 2026 · N17565 · Boeing 7379SDR SWIA2026070176984Skin · dentedMULTIPLE DENTS & GOUGES AT BS 589 - 605, BTWN STRINGERS 21R AND 27R. COMPLETED REPAIR WITH THE REO 601R-53-61-8591.Jul 1, 2026 · N982SW · Cndair CL6002B19SDR LR7A2026070103894Skin · corrodedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5701, FOUND LT CENTER WING LOWER TRAILING EDGE SKIN CORRODED AT CWS178-220L. REPAIRED IAW LAC MEA 382-55-26-090. NR# 1001392002.Jul 1, 2026 · N407LC · Lkheed 382GSDR LR7A2026070103891Doubler · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5305, FOUND FWD FUSELAGE DOUBLER CRACKED AT FS204, LBL80, WL195. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001390883.Jul 1, 2026 · N407LC · Lkheed 382GSDR CALA2026070117503Plate · corroded(EA 3830-01422 REV Q) AFT CARGO COMPT. AT STA. 1681.8 BILGE AREA, UPON REMOVAL BLADDER FOUND PLUG SKIN EXFOLIATED. REMOVED AND REPLACED PLATE ASSY-MOUNTING SUMP BLADDER, FLOOR DRA IN AT STA 1690 BTW STRG 29L TO 29R. IAW SRM 51-40-02- 0G0, DWG 417N2715 AND DJul 1, 2026 · N67134 · Boeing 757224SDR 1Q2R2026070100001Skin · damagedSCREW HOLE ELONGATED ON FUSELAGE SKIN AT BS 1005.2 BETWEEN S22R AND S23R. PERFORMED PERMANENT REPAIR IAW REO 670-53-61-2722, REV-.Jul 1, 2026 · N545PB · Cndair CL6002C10SDR VNAA202609010001Skin · corrodedLIGHTNING STRIKES (14 EA) FROM BS 594 - 661+32.00, BTW STRS 19L TO 26R AT FUSELAGE EXTERNAL SKIN. LIGHTNING STRIKES (14 EA) FROM BS 594 - 661.00+32, BTW STRS 19L TO 26R AT FUSELAGE EXTERNAL SKIN WERE REPAIRED PER REO 690-53-31-1159 REV -.Jun 30, 2026 · N642NN · Cndair CL6002D24
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