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.
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 SWAA2024112549948Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-645554<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. IAW B737-800. SRM 51-40-02-0G. AND DWG 141A8SDR CALA2024102202701Skin · damagedREF LOG PAGE 9352203 AND ENGINEERING REQUEST REMOVE PAINT AND BLIND FASTENER AT PREVIOUS LIGHTNING STRIKE REPAIR STATION 2018. REMOVED PAINT, BLIND FASTENER AND CREATED GRID MAP STA 2018 REF CONFIRMED HOLE SIZE IS .199" MEASURED DISTANCES FROM FRAMES AND STRINSDR CALA2024102102688Skin · damagedTHERE ARE OLD SCRIBE MARKS ON EXTERNAL SKIN OF FUSELAGE, LOCATED BETWEEN STA 654 PLUS 110/STA 785.9 AND BETWEEN STR20LH/36LH. FOR REFERENCE SEE SRM 53-30-01-0I-1 FIG 1, SHEET 2(ITEM 3) AND SHEET 4(ITEM 6). IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS TSDR DALA2024101810200Skin · mechanic errorSHIP 5651 WHILE REMOVING LEFT (UPPER) VHF ANTENNA, DAMAGED FWD MOST RIGHT-SIDE BOLT HOLE. CORRECTIVE ACTION: ACCOMPLISHED FREEZE PLUG REPAIR ON EXTERNAL FUSELAGE SKIN BTW STA 740-760 STR 1L-STR 1R IAW ER/A 621330-14 REV ORIG. SECTION I PERMANENT REPAIR. (06137SDR YENA2024101701349Skin · gougedDURING HEAVY MAINTENANCE: GOUGE ON LH FUSELAGE, OUTER SKIN, AT FR 25+ 18" AND 1" ABOVE STGR 42; REF MEXICANA WO # 1318489 , 1327754, 1328846 NR # 00349 AND JB WO # 1318489 NR # 00020 : GOUGE ON LH FUSELAGE, OUTER SKIN, AT FR 25 + 18" AND 1" ABOVE STGR 42 WAS SDR BJNA2024101701Skin · corrodedDURING A HEAVY CHECK MAINTENANCE VISIT OF A N708VL AIRCRAFT, A CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 847.00 TO STA 867, S-24L TO S-25L LOCATIONS. THE DAMAGE WAS BLENDED OUT AS PER SRM, AND THE CONDITION WAS RULED OUT OF LIMITS SINCE THE REMAININSDR DALA2024101710163Skin · damagedSHIP 3305 DAMAGE AROUND AFT CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ERA 620921-14 REV.A. (0613444)SDR DALA2024101710162Skin · damagedSHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P3 AND STR P2 FROM STA C53.7 TO C53.8. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612957)SDR DALA2024101710161Skin · damagedSHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P'3 AND STR P'2 FROM STA C53.7 TO C53.8. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612948)SDR DALA2024101710160Skin · damagedSHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P3 AND STR P2 FROM STA C53.6 TO C53.7. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612944)SDR DALA2024101710159Skin · damagedSHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P'3 AND STR P'2 FROM STA C53.6 TO C53.7. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612936)SDR IXXA20241017003Bear Strap · corrodedFLC FLOOR CORROSION FOUND AT DOOR THRESHOLD UNDERSIDE OF LONGITUDINAL BEAR STRAP AT BOLTHOLE OF THE MOST AFT CARGO LOCK @ STA 590 RBL 46.SDR DALA2025100607261Skin · damagedDTE - ER/A 620860-14 REV A. FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R / FWD LOWER ATG4 ANTENNA / REMOVAL CORRECTIVE ACTION: REF ERA 620860-14. (0611998)SDR BAGA2024111400287Skin · corrodedHEAVY CHECK- RELEASE DATE 11/14/2024-AFT SERVICE DOOR LWR SKIN UNDERNEATH SCUFF PLATES CORROSION AROUND ATTACHMENT HOLES. CORROSION LEVEL 2. REPAIRED PER REO.SDR BAGA2024111400285Skin · corrodedHEAVY CHECK- RELEASE DATE 11/14/2024- FWD FUS LH LWR SKIN CORROSION, UNDERNEATH SCUFF PLATE CORROSION AROUND HOLES. REPAIRED WITH DOUBLER PN C01342310-111S. LEVEL 2 CORROSION.SDR IPXA2024102850625Bear Strap · crackedFOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR). REMOVE ADJACENT FASTENERS AROUND CRACKED HOLE TO SEPARATE STRUCTURE I.A.W SRM 51-40-02-0G REV.90 IN ORDER TO HAVE NDT DOUBLE CHECK. INSTALL REMOVED FASTENERS I.A.W SRM 51-40-02-0SDR DALA2024101710174Skin · mechanic errorSHIP 5651 DTA MONITOR INSPECTION LOG REF ERA 621330-14 FUSELAGE / SKIN / BETWEEN BSTA 740 AND 760 AND BETWEEN S-1L AND S-1R / MISSDRILL. CORRECTIVE ACTION: REF ERA 621330-14. (0612903)SDR DALA2024101710168Skin · ground damageSHIP 3305 AFT CARGO DOOR SURROUND / C59A & STR-40RH TO STR-42RH / GROUND DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 620921-14, REV B. (0611670)SDR DALA2024101710167Skin · gougedSHIP 3305 GOUGES WERE FOUND ON THE FUSELAGE SKIN BETWEEN FR 53.6 AND FR 53.7, STR 2R TO STR 2L. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14. (0611415)SDR DALA2024101710151Skin · nickedAIRCRAFT 3066, NICK @ EXTERNAL SKIN LOC. FR 51 AT LEVEL STR 28 RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOC. FR 51 AT LEVEL STR 28 RH SIDE AT LOWER FUSELAGE AS PER A321 SRM53-41-11-300-109 STEP 2A TOOK INITIASDR IPXA2025073138042Skin · damagedMAJOR REPAIR, BEFORE INSTALLATION OF TAIL STAND NOTED AREA AFT OF TAIL STAND BALL IS DAMAGED WITH 2 SCRATCHES AND CREASE. VERIFIED ALL STEPS OF EO-91694- REQ 4 PERMANANT REPAIR COMPLIED WITH.SDR SWAA2024112649233Bear Strap · crackedCRACK ON BEAR STRAP LOCATED BTW BS291.5 TO BS294.5 STR8R AND STR9R AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON BEAR STRAP LOCATED BETWEEN BS 277 TO BS 312 AND STR 6R TO STR 11R IAW EA-24-153-03005 WIP1 AND EA-24-153-03005 SUMMARY SEE INDIVIDUAL SIGN OFSDR SWAA2024112048879Tail Cone · debondedTAILCONE EXTERNAL SKIN DISBOND AT 9' FROM FWD EDGE 5 O'CLOCK POSITION<[01] TAILCONE EXTERNAL SKIN DISBOND AT 9' FROM FWD EDGE AT 5 O'CLOCK POSITION; WAS REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024111448836Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-634539<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A5400 SHEET 3SDR BAGA2024111400286Doubler · corrodedHEAVY CHECK- RELEASE DATE 11/14/2024- REAR BARREL FR 75/76 WASTED AREA CORROSION INNER DOBLER CORRODED. INNER DOUBLER REPAIRED. CORROSION LEVEL 2....STATION 75 TO 76.SDR ASAA2024101553660Skin · damagedEXTERIOR SKIN HAS AREA OF PITTING BS. 360+5 STR.5L. GROUNDED - YES. REMOVED AND REINSTALLED CABIN SIDEWALLS AND #1, #2 STOWBINS L/H SIDE IAW B737-900 AMM 25-24-31-000-804-001, AMM 25-21-46, AMM 25-24-31. DISPLACED AND RESECURED INSULATION AT STR 5L STA 360-380SDR SWAA2024110548568Skin · debondedPANEL 191D INNER SKIN HAS MULTIPLE DISBONDS. (MARKED)<[01] PANEL 191D WITH MULTIPLE DISBONDS ON INNER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2024110548569Skin · debondedPANEL 191HL OUTER SKIN IS DISBONDED. (MARKED)<[01] DISBOND ON OUTER SKIN OF PANEL 191HL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2024110548570Skin · debondedPANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194CR OUTER SKIN WAS DISBONDED AND REPAIRED IAW SRM 53-60-70-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR DALA2024101610138Skin · damagedAIRCRAFT 3021, FOUND LIGHTENING STRIKE DAMAGE @ FRAME 24 STRINGER 6 BURN ON SKIN. CORRECTIVE ACTION: INSPECTED DAMAGE AS PER A321 SRM 53-00-11. PERFORMED PERMANENT REPAIR AS PER A321 SRM 53-21-11-300. (LP 5785554)SDR DALA2024101610126Doubler · corrodedWASTE BOX HAS CORROSION ON INNER SIDE OF DOUBLER ON FWD R/H CORNER. CORRECTIVE ACTION: COMPLIED WITH PRI 621280-14. (0610881) - ERA 621280-14 IS CONNECTED TO SHIP 8142 WHICH IS AN A220-100 NOT SHIP 3142 WHICH IS AN A319. THE CROSS-REFERENCE LOG NUMBER IS 06039SDR FDEA202410151505Doubler · chafedCENTER CARGO DOOR - AFT DOOR JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 1781, LONGERON -39 RIGHT TO LONGERON -42 RIGHT. CENTER CARGO DOOR - AFT DOOR JAMB AT STATION 1781, LONGERON -39 RIGHT TO LONGERON -42 RIGHT CHAFFED EXISTING REPAIR DOUBLER RSDR FDEA202410151504Doubler · chafedFORWARD CARGO DOOR FORWARD JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 895.7, LONGERON -40 RIGHT TO LONGERON -41 RIGHT. FORWARD CARGO DOOR FORWARD JAMB AT STATION 895.7, LONGERON -40 RIGHT TO LONGERON -41 RIGHT CHAFFED EXISTING REPAIR DOUBLER REPSDR FDEA202410151503Doubler · chafedFORWARD CARGO DOOR AFT JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 1002.3, LONGERON -39 RIGHT TO LONGERON -44 RIGHT. FORWARD CARGO DOOR AFT JAMB AT STATION 1002.3, LONGERON -39 RIGHT TO LONGERON -44 RIGHT CHAFFED EXISTING REPAIR DOUBLER REPAIRED SDR DALA2024101510105Skin · corrodedCORROSION ON INTERIOR OF FUSELAGE JUST FORWARD OF AFT PRESSURE BULKHEAD FRAME 79 BETWEEN STRINGER 36L AND 35L.-M- SEE ATTACHED PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 143-0001:5300-2110/001 00426 ER/A 620821SDR DALA2024101510100Skin · corrodedSHIP 3133 CORROSION EXTERNAL SKIN LOC. FR 69 TO FR 70 BTW STR 31 TO STR 32 RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC. FR69 TO FR70 BTW STR31 TO 32 RH SIDE AT LOWER FUSELAGE AS PER A319 SRM 53-41-11-300-004. (SDR VNAA2024100300013Skin · dentedFS893.00 - FS909.00 STRG 5RH - 7RH, 2 EA, EXTERIOR SKIN DENTS. COMPLIED WITH ALL STEPS OF REO 670-53--51-308 REV -- DATED 2024-09-24. AND COMPLIED WITH ALL STEPS OF REO 670-53-51-309 REV --, DATED 2024-10-02.SDR DALA2024101510114Skin · damagedSHIP 665 BIRDSTRICK TO FUSELAGE SKIN FWD OF STA 215, 16" BELOW STR 20L. CORRECTIVE ACTION: DAMAGE FOUND TO BE OUT ALLOWABLE LIMITS PER B757-200 SRM 53-00- 01-1A-1, CUT OUT DAMAGE PER B757 SRM53-00-011-2R REPAIR 29. PERFORMED HFEC INSP, NO DEFECTS. TREATED, PRISDR SWIA2024101400013Skin · dentedDENTED/GOUGED AREA AFFECTING THE EDGE OF FUSELAGE SKIN PANEL (DWG: SH670-31187, 0.135" THK AT DAMAGE LOCATION, REF). DAMAGE AREAS ARE LOCATED ALONG FS349.00 & STR5L. DAMAGE ON FUSELAGE SKIN MEASURES 1.0" LENGTH X 0.125" WIDTH X APPROX 0.081" MAX DEPTH. SEE CSDR SWAA2024120647719Support Angle · crackedCRACK SUPPORT ANGLE DODY FAIRING BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE 2024-633745<[01] REPLACED SUPPORT ANGLE LOCATED BODY FAIRING BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE IAW B737-700 SRM 51-40-05; SRM 51-10-02 Ï¿½TEM 9 AND DWG #: 116A3010; SHEET:SDR SWAA2024120547718Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-633743<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 146A7901 SHEET 19 REV.?;[02] TASK COMPLETEDSDR SWAA2024111447724Angle · crackedCRACK ANGLE LOCATED BS 291.5 TO BS 294.5 AND S-17R AT FWD GALLEY AREA 2024-634333<[01] REPLACED ANGLE (CLIP) LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02-0G; SRM-51-10-02-0G-0 Ï¿½TEM 9 AND DWG:141A8310 SHEET:25 REVSDR SWAA2024111447921Strap · corrodedCORROSION ON STRAP LOCATED BETWEEN BS 787 AND BS 793.5; STRINGER 25; WL 156 AFT CARGO COMPARTMENT 2024-634339<[01] TOOL USED: MULTIMETER P/N: FLUKE-289 S/N:61180136 DUE DATE: 10-JUL-25; TOOL USED: THERMOMETER P/N: FLUKE 566 S/N: 65900104WS DUE DATE: 17-OCT-25 SDR SWAA2024111447922Angle · corrodedCORROSION ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT 2024-634340<[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 767 AND BS 787; STRINGER 25R; WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 14SDR SWAA2024111447923Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B AND BS 727D STRINGER 25L WL 156 AFT CARGO COMPARTMENT 2024-634341<[01] REPLACED SUPPORT ZEE; [2] SPLICE SIDE PLATE (3 E/A) AND FASTENERS LOCATED BETWEEN BS 727 TO BS 847 STRINGER 25L WL 156 AFT CARGO COMPARTMENT IASDR JR2R202410120000Skin · gougedELONGATED HILITE HOLE AT FR45 1 INCH BELOW STR17LSDR SWAA2024111447520Angle · crackedCRACK ANGLE LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-634319<[01] REPLACED ANGLE (BRACKET) AND FASTENERS LOCATED BS867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G AND DWG: 146A7901 SHEET:66 SDR DALA2024111410943Skin · deformedSHIP 3236 DISC: SKIN DEFORMATION FOUND BETWEEN FRAME 72-74 AND STRINGER 33L-32L. C/A: PER ERA 621564-14 REV ORIG, C/W SECT II REP DETAILED INSPECTION W/ NO DAMAGE FOUND THE TABLE THERE BY YOUR, NO OTHER STRUCTURE HAS BEEN DAMAGED AS WELL AS ALL FANERS HAVE REMSDR DALA2024111410942Skin · dentedSHIP 3236 DISC: A DENT WAS FOUND IN THE FUSELAGE SKIN AT FR 72-74 / STR 33L-32L. THE DENT WAS REPAIRED PER ER/A 621564-14 AND NOW REQUIRES A DTE WITHIN 12 MONTHS. C/A: ER/A 621564-14 HAS BEEN REVISED, CURRENT REVISION IS 'B'. SECTION III PERMANENT REPAIR ACCOMSDR R61A2024102900520Skin · dentedREF DEFECT DMI R1038588/1 DURING LOGBOOK REVIEW REF L/P R949811/1 FOR DENT ON R/H RVSM AREA SYSTEM NOT QUALIFIED FOR RVSM OPERATION, ACFT MUST BE DOWNGRADED TO NON RVSM STATUS
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