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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR EE4Y2025111323447Skin · damagedDURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE WITH SRM 51-10-03 (BLEND-OUT TYPES A AND D). THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-93SDR EE4Y2025111323445Skin · damagedDURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. SIX (6) LSDS WERE REMOVED BY DRILLING THE SKIN. THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-930784 ANDSDR EE4Y2025111323442Skin · damagedDURING A STRUCTURAL INSPECTION, CUSTOMER IDENTIFIED AN EXISTING SKIN REPAIR LOCATED BETWEEN FR23 AND FR24, AND BETWEEN STRINGERS 16L AND 17L. ACCORDING TO DOCUMENTATION PROVIDED BY THE PREVIOUS OPERATOR, THE REPAIR WAS PERFORMED IN ACCORDANCE WITH ETD2014-190-SDR FDEA202511122166Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 698 AND STGR 32/33L. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 32L AND STGR 33L AT STA 698 WAS REPAIRED IAW SRM 53-00-01-2R, REPAIR 29, REV 93 AUG 15, 2025.SDR FDEA202511122165Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 676 AND STGR 32/33 LH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 32 LT AND STGR 33 LT AT STA 676 WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 29 REV. 93 AUG 15,2025.SDR YENA2025111301099Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE/ VENT OUTLET SKIN / BTW FR69/70 & STGR31/33 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ STS EA 160-2025-02 REV IR_DRAFT /2/ AIRBUS RDAF 81686597/003/2025#A. ENGINEERING FERRY CONCURRENCE ECA-321. DESCRIPTSDR JGVR20251112002Skin · corrodedBLENDED CORRODED AREAS LOCATED ON THE NUTPLATE-SIDE OF THE FUSELAGE STRUCTURE WHERE THE SPADE DOOR (MAIN ENTRY DOOR LOWER FAIRING DOOR) ATTACHES TO THE AIRCRAFT, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS AS REQSDR DALA2025121009035Skin · damagedER/A 629290-14 ISSUED FOR DOUBLER REPAIR TO THE WASTE BOX AREA. FOLLOW-ON ACTION REQUIRED. ER/A 629290-14 SECTION I ACCOMPLISHED IN MSP NOV 2025. SECTION II REPEAT INSPECTION REQUIRED EVERY 1,000 FH UNTIL SECTION III IS ACCOMPLISHED WITHIN 10,000 FH OF SECTIONSDR ASAA2025111162583Web · corrodedAFT CARGO PIT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. EVALUATED AFT CARGO THRESHOLD WEB, ORIGINAL THICKNESS .045, REMOVED .024, REMAINING .021, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED DAMAGED THRESHOLD WEB IAW SRM 51-40-02 LOCATED AND DRILSDR DALA2025111308329Skin · dentedON ARRIVAL, RAMP REPORTED DENT 32.5 INCHES AFT OF L2 DOOR. DAMAGE EVALUATED & MEASUREMENTS SENT TO ENGINEERING. SIDEWALL PANELS 19A & 20A REMOVED FOR EXCESS 785626. REINSTALLED SIDEWALL PNLS 19A & 20A 715532. C/W SECTIOIN 1 FERRY FLT PREP PER ER/A 630409-14 SDR DALA2025111208283Skin · dentedDENTS ON EXISTING REPAIR EXTERNAL SKIN LOCATED BTW FR 62 TO FR 64 AND BTW STR 36R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD. (1299184).SDR DALA2025111208272Skin · gougedDURING LIGHTNING STRIKE INSPECTION FOUND GOUGE AT LOCATION ON RT FWD FUSELAGE. 6.25" FWD OF FR 18 & 15.5 INCHES BELOW S32R. DEPTH OF THE GOUGE IS 0.0130" WITH A LENGTH OF 1/4 INCH. REWORKED GOUGE IAW SRM 53-11-11-283-026. OK FOR SERVICE. (1298883)SDR DALA2025111108234Skin · ground damageCATERING TRUCK DAMAGED SKIN LOCATED BETWEEN FR 62-64 AND BETWEEN S 37-41R. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD (1298120).SDR DALA2025111108252Skin · dentedWHILE ON THE LINE IN LAX, MAINTENANCE REPORTED A DENT AND GOUGE ON THE FUSELAGE SKIN AT THE STR-14L LAP SPLICE, JUST FORWARD OF STA 1016. THE DENT AFFECTED BOTH THE UPPER SKIN (147A3110-1) AND LOWER SKIN (147A3110-3), CROSSING THE LAP JOINT. MAINTENANCE REPAIRSDR DALA2025111308328Skin · dentedER/A 630449-14 REV ORIGINAL: FUSELAGE SKIN, BS 760, S14L - S15L, DENTED AND GOUGED. REPAIRED IAW ERA 630449-14. (1298266)SDR DALA2025111208278Skin · corrodedEVIDENCE OF CORROSION FOUND ON LWR FUSELAGE SKIN BETWEEN FR34 AND FR35 JUST AFT OF DRAIN BETWEEN S36L AND S36R. REMOVED CORROSION ON LWR FUSELAGE SKIN FR34-FR35, S36L-S36R, NO DAMAGE PERMITTED IN THIS AREA IAW A220 ASRP J51-21-06, J53-31-01 . RESTORED FINISH ASDR DALA2025111108247Skin · damagedRAMP REPORTS DAMAGE AT AFT CARGO SURROUNDING SKIN LOWER AFT SIDE. REPAIRED PER SRM 63-41-11. OK TO CONTINUE. (8149048)SDR 2025F00268Skin · corrodedFOUND 43 AREAS OF CORROSION UNDER AFT BELLY PANEL 316CBC. MECHANICALLY REMOVED CORROSION WHERE 36 NUTPLATES WERE REMOVED AND 4 ADDITIONAL AREAS IN BAY 316CBC IAW SRM 51-70-03. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-03 EXCEEDING .002" OF MATERSDR DALA2025111008197Skin · dentedDENT EXTERNAL SKIN LOCATED FR 3 AND 17 INCHES BELOW -Y675 LOWER FUSELAGE. COMPLIED WITH ER/A 629682-14. (1295801).SDR SWIA2026070676545Skin · gougedPANEL 642AT IS GOUGED AT FASTENER HOLE. REMOVED GOUGE ON PANEL 642AT AT FASTENER HOLE PER SRM 51-12-00-001-001-A01. PERFORMED REPAIR ON DAMAGED FASTENER HOLE ON PANEL 642 AT BY PERFORMING ALL STEPS OF REO 690-57-22-116 REV--. COMPLIED WITH SKYWEST TASK CARD SDR DALA2025111208295Skin · crackedCRACK WAS FOUND DURING NDT INSPECTION AT FASTENER NR 3 & 4. REPAIRED FWD SERVICE DOOR CUTOUT AFT LOWER CORNER IAW B767-300 SRM 53-10-01 (1294240)SDR DALA2025111208294Skin · crackedCRACK WAS FOUND DURING NDT INSPECTION AT FASTENER NR. 3 & 4. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03. REPAIRED FWD SERVICE DOOR CUTOUT AFT LOWER CORNER IAW B767-300 SRM 53-10-01-2R-1 REPAIR 1 (1294213)SDR AALA202511107503Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN, AT ELECTRICAL GROUND POWER RECEPTACLE DOOR LOWER CUTOUT SURROUND DOUBLER AT BS 225, S22R. REPAIRED SKIN PER SRM 53-10-15-2R-4.SDR 2025FA0000750Skin · chafedWHILE REMOVING CRACKED STINGER DEBRIS SHIELD, FOUND CHAFING ON THE LT AND RT STINGER SKINS.SDR 2025FA0000749Skin · chafedWHILE REMOVING CRACKED STINGER DEBRIS SHIELD, FOUND CHAFING ON THE LT AND RT STINGER SKINS.SDR VNAA202601170002Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH. DENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH WAS REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-31-1091 REV - -SDR SWAA2025121532683Bear Strap · crackedCRACK INDICATION FOUND LOCATED AT BS 291.5 PLUS 10 INCHES, S7R BELOW 4.200 INCHES. PERFORMED REPAIR ON BEAR STRAP HOLE IAW EA 25-153-03090-WIP1, & 25-153-03090-WIP2.SDR SWAA2025120832821Skin · crackedCRACK FOUND AT FED SURROUND STRUCTURE BS 291.5+4, STR 16L. REMOVED AND REPLACED FED SURROUND STRUCTURE BS 291.5+4 S16L, IAW SRM 51-40-02-0G-0 AND DWG 141A8180 REV C.SDR JJBA20251120065Skin · corrodedFUSELAGE EXTERNAL LOWER SKIN LH AT FR 61, STR 18L, HAS CORROSION. COMPLIED WITH REAR FUSELAGE I - PERMANENT REINFORCING REPAIR OF SKIN AT FRAME 61 AND STRINGER 18LSDR ASAA2025110762312Skin · dentedFUSELAGE SKIN DENT AFT OF STA 867 MARKED WITH RED TAPE REQUIRES RE - EVAULUATION REF L/P 60831633. GROUNDED - YES. FOUND DENT TO BE OUT OF LIMITS PER B737-800 SRM 53-00-01-1A-1 (STA 876) PERFORMED REPAIR PER EA# 800-53EA-29586. FOUND DENT AT STA 867 TO BE IN LSDR ASAA2025110762311Skin · dentedFUSELAGE SKIN DENT L/H SIDE STA 807 + 3.5' 2' ABOVE S-22L GROUNDED - YES. REPAIRED FUSELAGE SKIN AT LH STA 807 + 3.5" ABOVE STR-22L IAW B737-800 SRM 53-00-01-2R-3, REPAIR IS CATERGORY B PERMANET REPAIR WITH INSPECTION THRESHOLD OF 50,000 CYCLES AFTER AIRCRAFT SDR DALA2025111008171Skin · damagedSTRINGERS 25-26 AND BS 7942-7662 LIGHTNING STRIKE DAMAGE. REPAIRED PER ERA 630330-14 REV A REV 0. (1293332)SDR DALA2025111008170Skin · damagedFUSELAGE / STR 25-26 AND STA 7942-7662 / LIGHTNING STRIKE DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 630330-14 REVISION B. (1293132)SDR SWIA2025110676534Skin · gougedMULTIPLE NICKS AND GOUGES ON EXTERIOR SKIN BETWEEN FS1000.00 TO FS1051.30 STGR21R AND STGR26R. REPAIRED NICKS AND GOUGES ON EXTERIOR SKIN BETWEEN FS1000.00 TO FS1051.30 STGR21R AND STGR26R IAW REO 690-53-61-1714 REV -- DATED 2025-12-29. COMPLIED WITH ALL STEPSSDR AALA202512189776Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL SKIN PANEL AT FR 56, BETWEEN S41L AND S42L. REPAIRED SKIN PANEL PER EA 370128.SDR SWAA2025111332453Filler · brokenEGPR DOOR CUT OUT REPAIR FILLER LOWER SIDE IS BROKEN. FABRICATED NEW FILLER FOR EXISTING REPAIR AND INSTALLED ON EGPR ACCESS DOOR SURROUND DOUBLER LATCH LANDING IAW SRM 53-10-15-2R-4. INSPECTED IAW SRM 53-10-15-2R-4-B00449, REPAIR 4.SDR DALA2025111108258Skin · crackedCRACK ON EXTERNAL SKIN, BS 1087, BTW L-13R AND L-14R AT AFT FUSELAGE. PERMANENT REPAIR AND PRI 630164-14 REV. 3. (1291355)SDR DALA2025110708127Skin · damagedSHIP 3163 NICK ON EXTERNAL SKIN LOCATED FR27 PLUS 8.5 INCHES BETWEEN STR41RH AN D STR42RH AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-21-11-283-018. (1291822)SDR SWAA2025121032242Web · corrodedCORROSION SHIELD WEB LOCATED BTW BS 492.4 - 500A, S26R, WL 156 IN FWD CARGO COMPARTMENT. REPLACED THE SHIELD WEB AND FASTENERS BS 492.4 - 500A, S26R, WL 156 IAW SRM 51-40-02, AND DWG 143A0080, SHEET 39, REV-.SDR JJBA20251125092Access Panel · wornACCESS PANEL #412 CL SHOWS BARE METAL. RECEIVED NEW PANEL AND PAINTED.SDR DALA2025110508076Skin · damagedPREVIOUS SKIN BLEND-OUT REWORK HAS DIAMETER LARGER THAN .346 INCHES SEE AMDS CARD 5331-01297-02C STEP 5. ACCOMPLISH DVI OF THE FUSELAGE BOTTOM SKIN BEHIND THE SCUFF PLATE FOOTPRINT PER AND TP BD500-A-J51-00-900-1AAA-018A-A AND VERIFY NO CORROSION REMAINS ON SDR CALA2025110510922Skin · dentedRAMP REPORTED A DENT UNDER CAPT WINDOW. UPON FURTHER INVESTIGATION FOUND TO BE 2 DENTS. UPPER DENT FOUND TO BE OUT OF LIMITS, DAMAGE IS LOCATED ON STRINGER AND FRAME REF SRM 53-11-11-283-012. ACCOMPLISHED DOUBLER REPAIR IAW ECRA 5311-03412, SRM 53-11-11-283SDR ASAA2025110463110Skin · dentedDENT ON BELLY SKIN AT STATION 400. GROUNDED - YES. (RESOLVED ON W/O: 2071370 TASKCARD: N/R-00026 ) ACCOMPLISHED REPAIR IAW EA 700-53EA-29631.SDR SWAA2025121531736Bear Strap · crackedCRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BETWEEN BS 291 TO BS 294.5 AND BETWEEN S-8R TO S-9R. CRACK LENGTH 0.250 IN. APPROX. REPAIRED BEAR STRAP EXTERNAL SKIN IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.SDR ASAA2025110462414Transition Panel · corrodedAFT CARGO COMPARTMENT-STA 727I-767-RIGHT SIDEPLATE WITH CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, R/H TRANSITION PANEL AT STA 727I-767 IAW B737-800 SRM 53-00-53-1A-2.2.D. 100% MAT LOSS AND IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-0SDR R61A2025111200491Skin · dentedRH FWD FUSELAGE DENTED FROM BIRD STRIKE BETWEEN FRA 3 TO FRA 5 AND STR 20R TO 21R. REPAIRED DENTS IAW EMB 170/175 ETD2025-170-931943. ALSO REF VP-047843-2025 N/R 1,2,10 FOR WORK ACCOMPLISHED.SDR DALA2025110708141Skin · crackedSHIP 9507 FUSELAGE / SKIN / STA Y=1087, L=13R & L=14R / CRACK. CORRECTIVE ACTION: ACCOMPLISH ER/A 630164-14 (1290083)SDR DALA2025110508070Skin · wornWEAR ON EXTERNAL SKIN LOC. BTW FR73 TO FR74 AND STR17/18 LH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A 630030-14. (1288502).SDR 2025FA0000740Skin · corrodedCORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAISDR 2025FA0000739Skin · corrodedCORROSION FOUND ON TAIL AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATA PLATE. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON BLENDED AREAS LOCATED ON AFT FUSELAGE AROUND AIRCRAFT DATA PLATE AND JUST AFT OF DATE PLATE. PERFORMED ULTRASONIC REMAI
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