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 IXXA20241107004Skin · crackedR1 DOOR CUTOUT LOWER AFT CORNOR STA 335 JUST ABOVE STRINGER 20R LOWER FASTERNER HOLE HAS CRACK INDICATION IN SKIN ONLY.SDR SWIA202501300002Skin · dentedFS1015.00- 1031.00 STRG 23LH - 24LH, 2EA DENTS ON FUSELAGE EXTERIOR SKIN (MARKED) (C-CHECK RO 1/29/2025) DENT #1- LENGTH: 3.745", WIDTH: 0.854", DEPTH: 0.003". DENT #2- LENGTH: 3.670", WIDTH: 0.795", DEPTH- 0.002". USED CALIBRATED TOOL 101030TUC CAL DUESDR SWAA2024120657274Angle · crackedCRACK ON ANGLE LOCATED AT LEVEL STR 8L AND BS 312 AT FWD GALLEY AREA 2024-633958<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] REPLSDR ABXA202411086214Skin · dentedDURING CURRENT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED A DENT ON THE FUSELAGE SKIN BETWEEN STATIONS 1395-1417 AND BETWEEN S-28L AND S-29L. THE DENT WAS FOUND TO BE OUT OF SRM ALLOWABLE LIMITS. 767-200 SRM 53-00-01 REPAIR 1 REQUIRES THE DOUBLER REPASDR DALA2024110610683Skin · corrodedSHIP 3160 CORROSION SKIN LOWER EXTERNAL AREA AFT WALL LAVATORY A. CORRECTIVE ACTION: REPLACED PER ER/A 621147-14. (0646441)SDR MES2024F00005Doubler · corrodedAFT TEXAS DOUBLER CORRODEDSDR SWIA202501300001Skin · crackedRH TRU DOOR CUT OUT, THE LOWER AFT CORNER OF THE FUSELAGE SKIN HAS POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 1/29/2025) VERFIFIED CRACK ON RH FWD LOWER FUSELAGE SKIN UNDER TRU DOOR CUTOUT. REMOVED FWD SKIN PANEL ADG AT RIGHT SIDE REF CRJ700 SRMSDR VNAA20241213017Skin · corrodedCORROSION AND WEAR ON INTERNAL SKIN CUT OUT (SEAL SEATLEMENT AREA) DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT. CORROSION AND WEAR ON INTERNAL SKIN CUT OUT (SEAL SEATLEMENT AREA) DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND ESDR VNAA202412131012Bracket · corrodedCORROSION ON MACHINED BRACKETS (5 E/A'S) AND FWD PLATE AT FWD CARGO COMPARTMENT. MACHINED BRACKETS (5 E/A'S) AND FWD PLATE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001SDR HNAA2024121101185Skin · crackedF005671 RH SIDE SKIN CRACKED ON RIVET HOLE AT FR77 BTW STR3-4R. REPAIRED IAW EO1-53-24-0696SDR HNAA2024120301149Skin · cracked53-2212 FUSELAGE SKIN BLEND IS CRACKED AT BTW FR26-27 AT STR21L. REPAIRED IAW EO1-53-24-0700SDR HNAA2024120101143Skin · cracked53-2211 CRACK ON BLEND OF FUSE SKIN BTW FR23-24 BTW STR20-21L. REPAIRED IAW EO1-53-24-0271SDR ASAA2024110553642Skin · corrodedBUTT JOINT AT STA 360 FROM STR 25L TO STR 27L HAS SIGNS OF CORROSION. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON LH FUSELAGE SKIN BUTT JOINT AT STA 360 FROM STGR 25L TO STGR 27L P/N 141A3571-18 IAW EA# 800-53EA-27805 REV 00SDR A6WA202411058839Skin · gougedTEMPORARY REPAIR TO THE DAMAGE TO THE FUSELAGE SKIN AT FS607 AND STR17L- GOUGE. AIRCRAFT REMOVED FROM SERVICE. CUT AWAY EXISTING DOUBLER VISUAL INSPECTED FUSELAGE SKIN AT FS605 TOFS608 STR17L. NO ADDITIONAL DAMAGE FOUND. FABRICATED AND INSTALLED DOUBLER P/NSDR JR2R20241105142Doubler · chafedEXT SKIN DOUBLER AROUND MID AVIONICS BAY CHAFEDSDR SWIA20250130104Skin · dentedEVALUATE DENT ON EXTERNAL AIRCRAFT EXTERNAL SKIN AT FASTENER ON STGR 25R, FS 549.00 - 533.00 (C-CHECK RO 1/29/2025) PERFORMED ALL STEPS REO 670-53-31-974 REV--DATED 202412-03 FOR REPAIR. COMPLIED WITH TASK CAD 51-900-1002-SKY. THIS REO REPAIR ADRESSES 2SDR SWI2025F00098Skin · dentedEVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- DSDR SWI2025F0000098Skin · dentedEVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- DSDR SWAA2024120656747Stiffener · crackedCRACK STIFFENER ASSY LOCATED BS540 BETWEEN BL0 TO RBL 24.75 AT CENTER WING BOX 2024-686152<[01] REPLACED STIFFENER ASSY DUE TO NO FOUND ALLOWABLE DAMAGE IN B737-800 SRM LOCATED BS540 BETWEEN BL0 TO RBL 24.75 AT CENTER WING BOX IAW B737-800 SRM 51-10-02 ITEM 9 SDR SWAA2024120656750Angle · crackedCRACK ANGLE LOCATED 380 TO BS 400 AND LBL 13 AT PASSENGER CABIN 2024-686169<[01] REPLACED ANGLE AND FASTENER LOCATED 380 TO BS 400 AND LBL 13 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400; SHEET 142 REV-.<BR><BR>SEE INDIVIDSDR SWAA2024120556748Stiffener · crackedCRACK STIFFENER ASSY LOCATED BS540 BETWEEN BL0 TO LBL 24.75 AT CENTER WING BOX 2024-686153<[01] REPLACED STIFFENER ASSY LOCATED BS540 BETWEEN BL0 TO LBL 24.75 AT CENTER IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9<BR>LENGTH CRACK 0.509?<BR>TOOL USED: DIGISDR SWAA2024112156313Doubler · crackedEGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[02] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[0SDR CALA2024110601036Skin · damagedLIGHTNING STRIKE AT STA. 690 STR. 36REMOVED RIVET REF SRM 51-40-02 BLENDED OUT THE DAMAGE REF SRM 53-00-01-R-8. REMOVED FASTENERS FOR DOUBLER REPAIR AND REMOVED THE DAMAGED SKIN REF SRM 53-00-01-2R-4 REQUEST NDT OPEN HOLE INSPECTION FOR FASTENERS REMOVED REF.SDR DALA2024110510675Skin · ground damageAIRCRAFT 3821, BELT LOADER IMPACTED AIRPLANE NEAR REAR CARGO DOOR. CORRECTIVE ACTION: FOUND DENT ON AFT CARGO DOOR CENTER SCUFF PLATE DIMENSION 9/32 WIDE 15/32 LONG .134 DEE PER B737 SRM 53-60-15-1A PROC 3. DAMAGE LOCATED IN ZONE 1. REMOVED & INSTALLED AFT CASDR 2024FA0000815Skin · corrodedREPAIRED THE CORRODED AREAS OF THE FUSELAGE SKIN LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING (WING-TO FUSELAGE FAIRING) BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDSDR DALA2024110410608Skin · dentedSHIP 3303. FUSELAGE LOWER SKIN FOUND DENT BETWEEN FR67 TO FR68, STRG50R TO STRG57R. CORRECTIVE ACTION: COMPLIED WITH ERA 612856-14. (0643343)SDR SWIA202412231103Skin · gougedAFT LOWER EXTERNAL SKIN GOUGED BETWEEN FS977.00 & FS985.00 (C-CHECK RO 12/20/2024) PERFORMED REPAIR OF AFT LOWER EXTERNAL SIN GOUGE BETWEEN FS977.00 AND FS985.00 BY COMPLYING WITH ALL STEPS OF REO 670-53-00-290 REV -F DATE 2019/04/26. PRESSURE LEAK CHECSDR YENA2024110501432Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / STR 30LH / FASTENER HOLES / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9040-24 REV. 0 (COVER + PARTS 1-4) /2/ AIRBUS RDAF 81463325/004/2024 ISSSDR DALA2024110410590Skin · gougedGOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A, FIG 202. (LP #0642594)SDR DALA2025040102464Skin · damagedLIGHTNING STRIKE FASTENER FRAME 20 STRINGER 43 AND 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. PREVIOUS ITEM FOR MON REF ENTERED IN ERROR. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER SDR DALA2025040102463Skin · damagedLIGHTNING STRIKE FASTENER FRAME 20 STRINGER 41LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (430SDR DALA2025040102462Skin · damagedLIGHTNING STRIKE FASTENER FRAME 21 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350 -A-53-00-61-01001-661A-A FOUND TEMP ALLOWABLE LSDR DALA2025040102461Skin · damagedLIGHTNING STRIKE OFF FASTNER FRAME 19 STRINGER 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350 -A-53-00-61-01001-661A-A FOUND TEMP ALLOWABSDR DALA2025040102460Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSP. PER A350-A-53 -00-61-01001-661A-A , FOUND TEMP ALLOWABLE LIGHSDR DALA2025040102459Skin · damagedLIGHTNING STRIKE FRAME 18 STRINGER 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. PREVIOUS STEP MON REF ENTERED IN ERROR, REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSP. PER A350-A-53-00-61-01001-661SDR DALA2025040102458Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 41LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (478SDR DALA2025040102457Skin · damagedLIGHTNING STRIKE FRAME 17 BELOW STRINGER 45 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR PITTING AT FASTENER WITHIN LIMITS. RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. QA, PLESDR DALA2025040102456Skin · damagedLIGHTNING STRIKE FRAME 28 STRINGER 44LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (478884) PLEASSDR DALA2025040102455Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 43LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . PREVIOUS ITEM FOR MON REF ENTERED IN ERROR. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350-A-53SDR DALA2025040102454Skin · damagedLIGHTNING STRIKE FRAME 17 ABOVE STRINGER 45 L/H . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR DAMAGE/PITTING AT FASTENER TO BE WITHIN LIMITS PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (458844) PSDR DALA2025040102453Skin · damagedLIGHTNING STRIKE FASTENER FRAME 25 STRINGER 44LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (430SDR DALA2025040102452Skin · damagedLIGHTNING STRIKE FRAME 16 STRINGER 45 L/H . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR PITTING AT FASTENER TO BE WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (45884SDR DALA2025040102451Skin · damagedLIGHTNING STRIKE FASTENER FRAME 24 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10. FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (4788SDR DALA2025040102450Skin · damagedLIGHTNING STRIKE AT FRAME 14 STRINGER 45 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REMOVED TAPE FROM LIGHTNING STRIKE AREA. FOUND DAMAGE AREA PITTING WITHIN LIMITS PER ASR A350-A-53-00-61-01001-661A-ASDR DALA2025040102449Skin · damagedLIGHTNING STRIKE FASTENER FRAME 23 STRINGER 42LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10. FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (47888SDR DALA2025040102448Skin · damaged.LIGHTNING STRIKE 5" AFT FRAME 13 BETWEEN STRINGERS 44 AND 45. PERFORMED TEMP. SKIN PROTECTION USING HIGH SPEED TAPE. REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REMOVED TAPE FROM LIGHTNING STRIKE AREA. FOUND DAMAGED AREA/ BURN MARK < 15.7MM. REPAIR OF PAINT CSDR SWIA20250130102Skin · dentedRHS OF FWD. FUSELAGE AT APPROXIMATELY FS202, ABOVE WL79.50, (ABOVE RVSM RED CORNER MARKING), THE SKIN APPEARS TO BE DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RSDR R61A2024110900535Skin · dentedBIRD STRIKE FOWARD FUSELAGE BETWEEN FRAME 1 TO FRAME 2 AT STR 10L TO 12L. REMOVED AND REPLACED SKIN IAW EMB 170/175 SRM 51-43-02 AND 51-41-02. ALSO REF VP-045924-2024 N/R #1,#11,#12 FOR WORK ACCOMPLISHED.SDR DALA2024110410611Skin · misrepairedSHIP 3303 AN EXISTING DOUBLER REPAIR WAS FOUND IN AN EXCLUDED AREA PER A330 SRM AT FR 66 TO FR 67, STR 53R TO 54R. CORRECTIVE ACTION: REMOVED AND NEW REPAIR INSTALLED PER SECT I OF ERA 621856-14. (0641236)SDR DALA2024110410607Doubler · mislocatedSHIP 3410 DURING VIASAT ANTENNA MOD, #7 DOUBLER WAS MISLOCATED AT FR64 AND STRINGERS BETWEEN P1 TO P'1. CORRECTIVE ACTION: COMPLIED WITH ERA 621698-14. (6157121)
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