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 DALA2026031801872Skin · puncturedPUNCTURE TO LH SIDE FUSELAGE SKIN BETWEEN FR69-FR70 AND BETWEEN STR 33L AND 34L. REPAIRED DAMAGE SKIN ON L/H SIDE FUSELAGE BETWEEN FR69-FR70 AND BETWEEN STR 33L AND 34L PER ER/A# 633137-14AD REV-ORIGINAL. ASSOCIATED ER/A 14-633137 ADDED FOR AC 8136. (LP# 14956Mar 15, 2026 · N136DQ · Airbus BD5001A10SDR SWIA2026031575512Skin · not reportedLIGHTNING STRIKE ON CLIMB OUT THOUGH 9000 FT. POSSIBLE ENTRY POINT BELOW RIGHT WINDSHIELD (FLIGHT 5783) REPAIRED.Mar 15, 2026 · N120SY · Emb ERJ170200LRSDR DALA2026031601794Skin · damagedFR 62-63, STRINGER 3R, VIASAT FEEDTHROUGH DOUBLER, ADDITIONAL HOLES ON SKIN. MAJOR REPAIR PER ERA 632576-14. (1496171)Mar 15, 2026 · N858NW · Airbus A330223SDR IXXA20260315001Skin · corrodedFOUND SKIN CORROSION COMMON TO RT FILLET PANEL @ STA 793, 805, 825 ALL ON SKIN PANEL 143N3561-4Mar 15, 2026 · N752CX · Boeing 7572G5SDR CALA2026042915831Skin · crackedNDT CRACK INDICATION IDENTIFIED AT FS500A +20, .35" OTBD OF S2L IN PROXIMITY TO EA 5330-04336 CHEM MILL STEP INSPECTION AND PREVENTATIVE MOD SERVICE BULLETIN AREA FWD LH DOUBLER AND FILLER. WORKING DEFECT ON LAUNCH NON ROUTINE 5310-08359/006.THIS WILL BE A MAJMar 14, 2026 · N77258 · Boeing 737824SDR DALA2026031901908Skin · ground damageGROUND EQUIPMENT PUNCTURED SKIN AT BS 1480-1502 BETWEEN STRINGERS 23L AND 24L. COMPLIED WITH ER/A 632978-14 REV 0, REV 1, REV 2 AND REV 3. (LP 1495132)Mar 14, 2026 · N169DZ · Boeing 767332SDR AALA202603181519Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM FIRST LOWER HOLE LOCATED FWD OF FR35 AND STR 30L LEVEL AT FWD CARGO COMPARTMENT, CRACK DIRECTIONS AT 5 OCLOCK. LOOKING FROM AIRCRAFT EXTERIOR. CRACK DEPTH IS 0.098 INCHES. MAINTENANCE ACCOMPLISHED TIME LIMITEMar 14, 2026 · N125UW · Airbus A320214SDR DALA2026031701818Skin · ground damageGROUND EQUIPMENT PUNCTURED SKIN IN TWO PLACES BETWEEN STATION 1502-1518 BETWEEN STRINGERS 24L AND 26L. C/W PRI 632934-14. (1495125)Mar 14, 2026 · N169DZ · Boeing 767332SDR VNAA2026041500008Skin Panel · scratched2650 FH PERM REPAIR - TEMPORARY REPAIR FOR SCRATCHES TO FUSELAGE SKIN PANEL BETWEEN STRG19L - STRG20L & BETWEEN FS333 - FS349 THIS TEMPORARY REPAIR IS VALID FOR 2650 FLIGHT HOURS FROM THE TIME OF INCORPORATIONMar 13, 2026 · N521AE · Cndair CL6002C10SDR REXA2026033000277Skin · chafed"FUSELAGE OUT SKIN IS CHAFED AT FS 913.00 STGR 27 STRIPPED PAINT AT AREA OF DAMAGE FS 913.00 STGR 27 OUTER SKIN IAW CRJ 900 SRM 51-26-01-001-001-A01. REMOVED 2 RIVETS AND BLENDED OUT DAMAGE IN SKIN AT FS 913.00 STGR 27 IAW STEP A. OF BOMBARDIER REO 670-53-00-2Mar 13, 2026 · N937XJ · Cndair CL6002D24SDR MASA2026032019024Skin · dentedDURING THE STRUCTURAL INSPECTION, A DENT WITH CREASE WAS FOUND ON THE FORWARD FUSELAGE LOWER SKIN AT FRAME 06 AND BETWEEN STRINGERS 23RH-24RH: DAMAGE WAS TEMPORARY REPAIRED IAW ETD 2026-170-003825 VALID UNTIL MARCH 2,2027 AS IT WILL REQUIRE A DETAILED STRUCTURMar 13, 2026 · N89321 · Emb ERJ170200LLSDR DALA2026031701847Doubler · corrodedWHILE PERFORMING DVI OF ER/A 610625-14 REV ORIGINAL SECTION II OF CC JOB#136-2882877 CORROSION WAS FOUND AT INTERNAL DOUBLER AFT EDGE CORNERS OF WASTE BOX CUTOUT. C/W ER/A 610625-14 REV A ASSOCIATED ER/A 14-610625 ADDED FOR AC 8136. LOG TO REFLECT SDR YES. (LPMar 13, 2026 · N136DQ · Airbus BD5001A10SDR AALA202603169895Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: LEFT SIDE FUSELAGE SKIN HAS AREAS OF LIGHT CORROSION AROUND AFT LAVATORY OVERBOARD VENT AT BS 915 BETWEEN STRINGER 21L AND STRINGER 22L. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-70-01-2R-3.Mar 12, 2026 · N871NN · Boeing 737823SDR DALA2026031301770Skin · damagedFUSELAGE / FR26 TO FR26.1 / STR50L TO STR50R / IMPACT DAMAGE. REPAIRED DAMAGE PER ERA 624866-14. (1491497)Mar 12, 2026 · N826NW · Airbus A330302SDR SWIA2026031176883Skin · crackedCRACK FOUND IN FUSELAGE SKIN AT BS 235 AT AFT LEFT CORNER OF NLG CUTOUT. REPAIRED THE SKIN IAW REO 601R-53-11-048 REV-D, & REO 601R-53-11-4076, REV-.Mar 11, 2026 · N207PS · Cndair CL6002B19SDR DALA2026041502390Skin · corrodedER/A 610625-14 REV A; A220 / LOWER AFT FUSELAGE / FR75-76 / WASTE SERVICE COMPARTMENT/CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 610625-14 REV A, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 14,667 TOTAL AIRCRAFT FMar 11, 2026 · N136DQ · Airbus BD5001A10SDR 2026F00042Skin · crackedTHE MECHANIC WAS COMPLYING WITH THE ZONE 3 TRANSMISSION INSPECTION WHEN HE FOUND THE CRACK. IT WAS FOUND BECAUSE OF BLACK OIL AROUND THE AREA. HE CLEANED THE AREA AND COMPLETED A DYE PENETRANT INSPECTION TO VERIFY THE CRACK. THE CRACK LENGTH IS 2", LOCATED ATMar 11, 2026 · N403PH · Bell 407SDR SWIA2026031175511Skin · dentedDENT DAMAGE FOUND TO FORWARD FUSELAGE SKIN BETWEEN FR 11 AND STRG 15L-18L. (FLIGHT 4004) COMPLIED WITH REPAIR OF DAMAGE ON FWD FUSELAGE SKIN BETWEEN FR 11 AND STRG 15L-18L IAW SRM 53-10-01/REP 15.Mar 11, 2026 · N289SY · Emb ERJ170200LLSDR ABXA202603131097Skin · corrodedDURING C1 CHECK, PERFORMED DVI OF FUSELAGE SKIN INTERNALLY ON AREAS EXPOSED BY REMOVAL OF THE SIDE FRAME FITTING HAS CORROSION. REPAIR ACCOMPLISHED ON WORK ORDER# 47008ORD09. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETED.Mar 11, 2026 · N312AA · Boeing 767223SDR IXXA20260311001Skin · corrodedFUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2Mar 11, 2026 · N752CX · Boeing 7572G5SDR SWIA2026031077431Skin · corrodedRIGHT CENTER FUEL PUMP ACCESS HOLE BS 225 STR 30, HAD CORROSION ON SURROUND SKIN, BLENDED DAMAGE ON RT CENTER FUEL PUMP ACCESS HOLE AND FOUND OUT OF LIMITS REPAIRED PER REO 670-57-11-258 REV -.Mar 10, 2026 · N611SK · Cndair CL6002C10SDR BAGA2026043000009Doubler · corrodedHVY CHECK SUBMISSION - CORROSION FOUND ON WASTE DOUBLER CUTOUT AT REAR BARREL FRAME 75-76. REPAIRED IAW AIRBUS REO.Mar 10, 2026 · N227BZ · Airbus BD5001A11SDR SWIA2026031075903Skin · damagedSIGNS OF LIGHTENING DAMAGE BETWEEN RIVET AND SKIN FWD OF BS 453 ABOVE STR 2L. REPAIRED DAMAGE ON EXTERIOR FUSELAGE SKIN BS 453, STR 2L IAW REO 690-53-21-2117, REV - (P1), AND SRM 51-42-06, 53-00-00, 51-12-00, 51-25-01, AMM 21-31-00. NDT PERFORMED.Mar 10, 2026 · N816SK · Cndair CL6002D24SDR DALA2026031101672Skin · misrepairedDURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE) BETWEEN FR1 AND FR2 / LBL12 TO RBL 12. SEVERAL FASTENERS (3EA) ARE LOCATED IN THE CHEM MILLED RADIUS AREA THAT ARE NOT SPOT FACED. REFERENCE DELTA AIR LINES ER/A 548858-14Mar 10, 2026 · N365NB · Airbus A319114SDR DALA2026031101671Skin · misrepairedDURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE). ONE FASTENER LOCATED 11 ROWS OUTBOARD (LEFT) OF THE FILLER CUTOUT AND 3 ROWS AFT OF FORWARD BULKHEAD IS SPOT FACED BUT DOES NOT MEET THE SRM REQUIREMENTS (EDGES ARE NOT BMar 10, 2026 · N365NB · Airbus A319114SDR IXXA20260310001Skin · corrodedFUSEELAGE LEFT SIDE STA 785-855 LEVEL 2 CORROSION2 BODY TO WING PANELSMar 10, 2026 · N752CX · Boeing 7572G5SDR SWIA2026030975624Skin · damagedEVALUATE PREVIOUS DOUBLER REPAIR AT FRAME 11, STRINGERS 18L AND 19L FOR SERVICABILITY. PERFORMED SKIN REPAIR ON SKIN AT FR 11 STR 18L AND STR 19L. REF ETD2026-170-004397 REV B.Mar 9, 2026 · N139SY · Emb ERJ170200LRSDR AALA202603250927Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON ACCESS DOOR 312AR CUTOUT DOUBLER AT FR 71 BETWEEN S28R AND S29R. REPLACED DOUBLER PER SRM 51-72-11.Mar 9, 2026 · N418AN · Airbus A321253NXSDR CALA2026032314795Skin · damagedFOUND EXISTING REPAIR FASTENER AT THE FUSELAGE SKIN BTW STA 500A AND STA 500B STRG- 3L AND 2L. REQUIRE ENG SUPPORT ON HOW TO PROCEED, REF TO EA 5330-04336 REV A OPS 007. FOUND EXISTING REPAIR FASTENER AT THE FUSELAGE SKIN BTW STA 500A AND STA 500B STRG- 3L ANDMar 9, 2026 · N27246 · Boeing 737824SDR AALA202603128057Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT STABILIZER STA 98 ALONG AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.Mar 9, 2026 · N990AN · Boeing 737823SDR R61A2026030900058Skin · gougedDEEP GOUGE FR 21-22 ABOVE STR 16L. CUT OUT GOUGE BETWEEN FR 21-22 ABOVE STR 16L AND PERFORMED REPAIR USING DOUBLER AND FILLER IAW ETD2026-170-004205.Mar 9, 2026 · N778YX · Emb ERJ170200LRSDR REXA2026031000235Skin · chafedRIVETS ON FUSELAGE OUTER SKIN ARE CHAFED AND SHEARD OFF AT FS 913.00 STGR 27. RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA: CRJ-953-21545 REV IR DATED 2/15/2026.Mar 9, 2026 · N917XJ · Cndair CL6002D24SDR EE4Y2026030924076Skin · damagedCUSTOMER REPORTS TWO LIGHTNING STRIKE DAMAGES AFFECTING THE CENTER FUSELAGE I SKIN, LOCATED AT FR33 + 242 MM (DAMAGE #1) AND FR33 + 394 MM (DAMAGE #2) ON STR 26L. DAMAGE #1 WAS COMPLETELY REMOVED BY BLEND-OUT. DAMAGE #2, DEPTH EXCEEDED 50% OF THE SKIN THICKNESMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR EE4Y2026030924075Skin · damagedDURING THE STRUCTURAL INSPECTION, DAMAGE CAUSED BY A LIGHTNING STRIKE WAS FOUND ON THE EXTERNAL SKIN OF THE CENTER FUSELAGE I, AT FR24 + 327MM, STR-27LH + 8MM. AFTER PERFORMING A LIGHT BLEND-OUT, IT WAS DETERMINED THAT IN A POINT, THE DAMAGE EXCEEDED 50% OF THMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR EE4Y2026030924073Doubler · misinstalledDURING STRUCTURAL INSPECTION, THE CUSTOMER FOUND AN EXTERNAL REPAIR DOUBLER AT FR74 + 105 MM AND STR 24L + 85 MM, REPORTEDLY INSTALLED IN ACCORDANCE WITH EMB IC2009-190/05358C DATED 09-JUL-2009. ONCE THE AVAILABLE DOCUMENTATION LACKED ESSENTIAL INFORMATION, THMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR EE4Y2026030924072Skin · damagedWAS REPORTED THAT DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR32 AND JUST ABOVE STR-26LH. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR EE4Y2026030924071Skin · damagedDURING THE STRUCTURAL INSPECTION, AN EXISTING BLEND-OUT WAS FOUND IN THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 86-87 AND STRINGERS 27R-28R. SINCE NO PREVIOUS RECORD OF THIS BLEND-OUT EXISTS, IT WAS INSPECTED AND EVALUATED. THE CONDITION WAS FOUND TO BEMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR EE4Y2026030924069Skin · damagedCUSTOMER REPORTS LIGHTNING STRIKE DAMAGE AFFECTING THE CENTER FUSELAGE III SKIN, LOCATED AT FR74 AND STR 28L. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR SWIA2026030877397Skin · damagedICE DETECTORS SURROUND HAD TOOLING MARKS, ON BOTH LT & RT. REMOVED SCRATCHES ON FUSELAGE EXTERIOR SKIN ICE DETECTOR SURROUNDS, BOTH RT & LT SIDES IAW SRM 51-12-00-001-001-A01, REWORKED AREAS ARE WITHIN LIMITS PER REO 670-53-11-2295, REV -.Mar 8, 2026 · N611SK · Cndair CL6002C10SDR IPXA2026031775549Skin · crackedCRACKED PANEL, RT BODY MLG WW INNER LONGERON BOX AREA ,BS 1372. REPAIRED THE DAMAGE IAW EO-96831,REQ1, REV 1, AND EGAT EI F2026A53M-503, REV 1.Mar 8, 2026 · N574UP · Boeing 74744AFSDR VNAA202603140006Skin · scratchedRIGHT FUSELAGE SKIN SCRATCHED. WITHIN 661 FLIGHT HOURS FROM REVISION REQUEST, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: SUBMIT AN RFTS WITH UPDATED DAMAGE REPORT.Mar 8, 2026 · N635NN · Cndair CL6002D24SDR CALA2026090119140Skin · damagedWHILE PERFORMING PHASE 2 GVI, IAW AMM 05-51-19-210-805, FOUND LIGHTNING STRIKE DAMAGE ON LT SIDE OF ACFT FUSELAGE SECTION 41. DAMAGE LOCATED BS 219, ABOVE STR 24, HOLE THROUGH SKIN. HOLE MEASURES 0.265". ACTUAL DAMAGE AROUND HOLE MEASURES 0.451". CLOSEST FAMar 7, 2026 · N68821 · Boeing 737924ERSDR SWIA2026030776886Skin · wornSKIN PANEL AT BS 550, LBL47 WORN. REPAIRED THE LT APRON SKIN PANEL BTWN BS 516.85 - 559 IAW REO 601R-53-41-3423, REV -.Mar 7, 2026 · N207PS · Cndair CL6002B19SDR SWIA2026030776881Skin · wornSKIN PANEL AT BS 550, RBL47 WORN. REPAIRED THE RT APRON SKIN PANEL BETWEEN BS 516.85 - 559 IAW REO 601R-53-41-3423 REV -, SKYWEST CONTINUE CARDS, ITEMS 1-32; 1-22; 1-22,Mar 7, 2026 · N207PS · Cndair CL6002B19SDR AALA202603104724Skin · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE OF FUSELAGE SKIN HAS CREASED AREA WITH MULTIPLE SMALL DENTS AT BS 365 BETWEEN STR 15L AND STR 16L. ACCOMPLISHED SKIN REPAIR BETWEEN BS 360 AND BS 380, STR 13L AND STR 17L. PER AA EA 372415.Mar 7, 2026 · N989AN · Boeing 737823SDR DALA2026031001653Skin · ground damage(LOG 1484200) CATERING TRUCK HIT A/C RESULTING IN DAMAGE IN SECTION 41, AT BS 340-360, LOCATED ON STRINGER 20R. DAMAGE CONSISTS OF AN 8 IN X 4 IN DENT WITH A MAXIMUM DEPTH OF 0.147 INCHES. THE DENT IS ON THE FUSELAGE SKIN AND UNDERLYING STRINGER 20R. REMOVED DMar 7, 2026 · N849DN · Boeing 737932ERSDR DALA2026031001652Skin · damaged(LOG 1484180) FUSELAGE SKIN DAMAGE AT STR 20R STA 360. C/W ERA 632727-14 ORIGINAL SECTION 1. C/W RII OF ERA 632727-14 ORIG SECTION 1.Mar 7, 2026 · N849DN · Boeing 737932ERSDR CALA2026031014483Skin · corrodedEVEALUATE CORROSION ON THE WASTE TANKS AREA PAN ASSY. PERFORMED REPAIR ON EXTERNAL SKIN OF THE VACUUM LAVATORY SERVICE DOOR CUTOUT BTW BS 847 - 867, S23L - 25L, MAJOR REPAIRMar 7, 2026 · N75410 · Boeing 737924SDR DALA2026030801591Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR 13 TO FR 14 RH SIDE LEVEL Z=1330 UPPER FUSELAGE (REFERENCE AA CA RD 5100-01821-01A). C/A: COMPLIED WITH ER/A 520355-14 REV.B MATCHES WITH ALL STEPS ON PRI 520355-14 PRI REV 0,1,2,3 ITS Mar 7, 2026 · N377NW · Airbus A320211SDR DALA2026031001641Skin · crackedSHIP 9523 CRACKS (2EAS) ON UPPER EXTERNAL FUSELAGE SKIN APPROX Y=1087 BTW LONG 13R-14R. CORRECTIVE ACTION: REPAIRED PER ER/A 632448-14 (1482120)Mar 6, 2026 · N964AT · Boeing 717200
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