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 DALA2025080505875Skin · corrodedLOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW DELTA ERA 627451-14. REMOVESDR DALA2025080505874Skin · corrodedLOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35. S36R - 36L. SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/SDR DALA2025080505873Skin · corrodedLOWER FWD WTBF AT LWR FUSELAGE, 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R -36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/ASDR AALA202508042106Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY VENT AT BS 920 BETWEEN S21L AND S22L. ACCOMPLISHED REPAIR PER EA 366657.SDR JJBA20250731129Doubler · corrodedCF4, EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R FOUND CORRODED. CF4 EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R REMOVED FOR ACCESS, CORROSION BLENDED WITHIN LIMIT. AFTER INVESTIGATION, INTERNAL SKIN BTW FR 57-59 ANSDR JJBA20250731128Skin · damagedSCREWS HOLES ELONGATED ON BOTH STARKE SPLICE SKIN. STARKE SPLICE SKIN (2X) FABRICATED.SDR FDEA202507311344Skin · crackedFUSELAGE EXTERIOR SKIN APPROXIMATE X= 18.955 LEFT HAND STATION 475, FORWARD OF NOSE LANDING GEAR FORWARD DOOR FOUND CRACKED. CRACKED SKIN AT FUSELAGE EXTERIOR APPROXIMATE X= 18.955 LEFT HAND STATION 475 FORWARD OF NOSE LANDING GEAR FORWARD DOOR REPAIRED ASSDR SWI2025F01810Skin · dentedFUSELAGE SKIN HAS PROTRUDING DENTS AT FS 299 BETWEEN STRS 20R AND 21R. REPAIRED FUSELAGE SKIN FS299 STGR 20R-21R IAW REO# 670-53-21-2667 REV - AND SRM 51-23-00-001-001-A01 REV 38SDR SWIA2025102000730Skin · chafedL/H WING, LOWER WING PLANK HAS CHAFE DAMAGE FROM CONTACT WITH FLAP FAIRING 586AB. (C-CHECK RO 10/19/2025)REPAIRED LH WING LOWER PLANK CHAFE DAMAGE FROM CONTACT WIT FLAP FARIING 586AB IAW REO 601R-57-21-3961 REV--, DATED 2025-08-06 COMPLETED TASK CARD 51-900-SDR SWAA2025080196449Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER CRACKED ON LOWER EDGE. REPAIRED ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER AT LOWER EDGE IAW SRM 53-10-15-2R-4. PERFORMED A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE TRIM OUT AT THE LOSDR YENA2025073100789Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE SKIN HAS CORROSION AT LAV VENT FR69-70 STR 32R-31R. RESOLVED ON W/O: 1428515 TASKCARD: NR-00002. REF HAECO WO 440633 NR 40009. PERFORMED REPAIR IAW SRM 53-41-11-300-004. TO BE REINSPECTED AT 60000FC FROM ACFT FIRST FLIGHT PSDR IXXA20250730003Skin · crackedCRACK INDICATION IN THE 2ND HOLE FROM THE BOTTOM AT FORWARD ENTRY DOOR LOWER AFT CORNER, SKIN LAYERSDR IPXA2025082873361Stringer · crackedMAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S35R. PERFORM EO-94926-REQ1 REV.1 AND EI F2025A53M-1729, REV.2 2.SDR CALA2025081407754Skin · corrodedAFT PIT LT SIDE, FUSELAGE SKIN CORRODED AROUND THE LAVATORY EXHAUST VENT ATTACHMENT BETWEEN BS 907 AND BS 927 AND BETWEEN STRINGERS S19L AND S22L. ACCOMPLISHEDD INTERIM REPAIR OF THE AFT PIT LT SIDE, FUSE SKIN IAW ECRA 5370-01182 PT1.SDR IPXA2025080870685Skin · corrodedCORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-94636-REQ1 REV1.SDR IPXA2025080670685Skin · corrodedCORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. RESPECTIVELY PART MARK THE REPAIR PART(S) PER BAC5307 CODE M AS BELOW. REPAIR FILLER: F2025A53M-1650-1, REPAIR DOUBLER: F2025A53M-1650-2; REPAIR TRIPLER: F2025A53M-1650-3. INSTALL THE REPAIR PARTS WSDR DALA2025080105779Skin · damagedTAIL SECTION RH FUSELAGE SKIN AT STA 1730 UNDER SEAL PANEL 314CRX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-01.SDR DALA2025080105778Skin · damagedTAILCONE RH FUSELAGE SKIN AT STA1783 UNDER SEAL PANEL 314CRX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-01.SDR DALA2025080105777Skin · damagedTAILCONE LH FUSELAGE SKIN AT STA1783 UNDER SEAL PANEL 313CLX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-01-2R.SDR DALA2025080105776Skin · damagedTAIL SECTION RH FUSELAGE SKIN AT STA 1730 UNDER SEAL PANEL 314CRX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-01.SDR DALA2025080105775Skin · damagedTAIL SECTION LH FUSELAGE SKIN AT STA 1730 UNDER SEAL PANEL 313CLX FOUND ABRASION. DAMAGED AREA REPAIRED PER B767-400 SRM 53-80-01.SDR SIMA20250729001Doubler · corrodedINNER REINFORCEMENT SKIN AT LAV SERVICE PANEL IS CORRODED. (LEVEL 2 CORROSION). REPAIRED IAW ERJ SRM 53-23-60.SDR SWIA2025102000728Skin · corrodedMID. FUSELAGE SKIN UNDER FORWARD WING - TO - FUSELAGE FAIRING SEALANT BED HAS NUMEROUS AREAS OF CORROSION AROUND NUTPLATE HOLES. MARKED WITH TAPE. (C-CHECK RO 10/19/2025)REPAIRED FUSELAGE SKIN UNDER FORWARD WING TO FUSELAGE FAIRING SEALANT BED AROUND NUTPLATESDR JJBA20250825055Skin · dentedDENT/CREASE WAS IDENTIFIED IN THE FORWARD FUSELAGE 1 AREA, LOCATED BETWEEN FRAMES 1A AND 2 AND BETWEEN STRINGERS 15R AND 13R. NO STRUCTURAL DEFORMATION OR ADDITIONAL ANOMALIES WERE OBSERVED. PERMANENT REUNFORCING REPAIR PERFORMED ON RF FWD DUSELAGE SKIN AT FRASDR SWIA2025F01382Skin · gougedFOUND GOUGE ON PAX DOOR SURROUND EXTERIOR SKIN AT FS 345.0 APPROX. NEXT TO PAX DOOR PIANO HINGE. (C-CHECK RO 09/24/2025)REPAIRED GOUGE ON PAX DOOR SURROUND EXTERIOR SKIN APROX @FS345.0 IAW REO 601R-53-21-3763 REV -- DATE: 2025-07-30 AND COMPLIED WITH TASK CASDR SWIA2025F01376Skin · gougedAPU EXHAUST CUTOUT AFT VERTICAL CUT LINE HAS EVIDENCE OF GOUGING. (S/N#00482) (C-CHECK RO 09/24/2025)REMOVED DAMAGE IN APU EXHAUST CUTOUT AFT VERTICAL CUT LINE REF. CRJ200 SRM 51-12-00. COMPLIED WITH REO 601R-53-61-8365 REV -- DATE 2025-08-04 STEP 1-4. FOUND SDR CALA2025091208833Skin · crackedTYPICAL CRACK FOUND AT R1 DOOR BEAR STRAP AT FASTENER ADJACENT TO FITTING LATCH. CRACK AT 10 O'CLOCK POSITION WITH CRACK LENGTH : 0.156". ACCOMPLISHED REPAIR AT R1 DOOR BEAR STRAP REFERENCE B737-800 SRM 53-10-01-2R-6 FIGURE 202SDR CALA2025080507318Doubler · crackedEXTERNAL POWER RECEPTACLE DOOR CUTOUT INNER DOUBLER FWD CENTER AREA CRACKED. APPLIED TOP COAT EXTERNAL POWER RECEPTACLE DOOR CUTOUT IAW AMM 51-21-73-370-803. REMOVED AND REPLACED EGPR INNER DOUBLER AS REQUIRED IAW SRM 51-40-02-0G-0, DWG 141A3702 AND DWG 141SDR AALA202508038861Skin Panel · corrodedAIRCRAFT WAS GROUNDED: WASTE OVERBOARD VENT SHOWS SIGNS OF CORROSION. MAINTENANCE REPAIRED SKIN PANEL PER EA 366767.SDR AALA202508030264Skin Panel · corrodedAIRCRAFT WAS GROUNDED: WASTE OVERBOARD VENT SHOWS SIGNS OF CORROSION. REPAIRED SKIN PANEL PER EA 366767.SDR AALA202507310264Skin · corrodedAIRCRAFT WAS GROUNDED: WASTE OVERBOARD VENT SHOWS SIGNS OF CORROSION. (OPEN)SDR DALA2025072805670Skin · damagedSHIP 3119 FWD FUSELAGE DAMAGE FR 1-4. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1108228).SDR DALA2025080405839Skin · ground damageSHIP 3119 GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR 2-4 AND ABOVE Y=330 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1107429).SDR DALA2025080405836Skin · dentedSHIP 3119 FOUND DENT ON THE CROWN SKIN AFT OF FR 53 BETWEEN STR 3L-4L. CORRECTIVE ACTION: COMPLIED WITH ER/A 626580-14. (1107420).SDR DALA2025072905683Skin · damaged(LOG 1107254) FUSELAGE / SKIN / BTW BSTA 178 AND BSTA 188 AND BTW LBL 10 AND LBL 20 / LIGHTNING STRIKE. REPAIRED PER ERA 627647-14.SDR GTIA2025072839018Skin · no discrepancyEXISTING RE-WORK EXTERNAL SKIN LOCATED FR23 TO FR24 BTW STR 41L TO STR 42L AT LOWER FUSELAGE. RAF-01 3336958-01-PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED FR.23 TO FR.24 BTW STR 41L TO STR 42L AT LOWER FUSELAGE IAW EA #53-00-45-25 AIRBUS PROVIDED AN ISDR GTIA2025072839017Skin Panel · dentedDENTS ON EXTERNAL FUSELAGE BTW FR. 8 - 9 AND LH SIDE STRINGER TO LOWER STRINGER RAF-01 3551196-01 CREATED-EVALUATED DENT 1 AND 2 BTW FR8-9 LOWER STRG 28 LH AND FOUND WITHIN LIMITS I.A.W A321 SRM 53-00-11-283-005, THIS REPAIR IS CATEGORY B, INSPECTION THREHOLD SDR DALA2025072805645Skin · mechanic errorSHIP 3360 WHILE DISBONDING STGR 3R, TOOLING MARKS WERE CREATED ON SKIN AT FR 61. CORRECTIVE ACTION: REPAIRED PER PRI 627795-14 REV 1. (1106308)SDR HALA20250728040Skin · corrodedINFO TO MX CORROSION AROUND THE AFT WASTER OVEBOARD VENT. REPAIR ACCOMPLISHED ON TASK CARD E105-370017-INI2 OK FOR SERVICESDR 9WGA2025092054664Panel · corrodedCENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX. STA 1173, SDR 9WGA2025092054663Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPSDR 9WGA2025092054662Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED UT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEEN CLSDR 9WGA2025092054661Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWSDR DALA2025073005716Skin · damagedSHIP 3360 STRINGER 3R AND FUSELAGE SKIN REWORK, FR 60-62. REPAIRED PER ERA 627795-14.SDR DALA2025072905675Skin · crackedSHIP 9572 INITIAL INSPECTION: CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 BTW. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN STA 1076 BTW LONG 13-14 LH WAS REPAIRED PER REPAIR ERA PRI 626436-14AD (1105456)SDR DALA2025072805650Skin · damagedSHIP 3360 DAMAGE FOUND ON INTERNAL SIDE SKIN AT FASTENER HOLE INBOARD OF STR 3L BETWEEN FR 61 AND FR 62. CORRECTIVE ACTION: REPAIRED PER ERA 627562-14 REV O. (1105056)SDR DALA2025072805631Skin · damagedSHIP 3360 TOOLING DAMAGE FOUND ON THE SKIN ADJACENT TO STR R1 AT FR 63. CORRECTIVE ACTION: REPAIRED PER ERA 627916-14 REV ORIGINAL. (1105858)SDR DALA2025072805630Skin · mechanic errorSHIP 3360 WHILE DISBONDING STR 1R, TOOLING MARKS WERE CREATED ON SKIN 8" AFT OF FR60 1" OB OF STR 1R. CORRECTIVE ACTION: REPAIRED PER ERA 627744-14 REV O. (1105844)SDR 2025FA0000524Support Strap · corrodedCORROSION WAS FOUND ON THE LOWER FAIRING SUPPORT STRUCTURE FOR THE AFT WING TO FUSELAGE FAIRINGS ON THE LH & RH SIDES AT FS 618-FS6358. THIS IS A NON-PRESSURIZED AREASDR SWAA2025090395117Bear Strap · crackedCRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BETWEEN BS 291-BS 294.5 AND BETWEEN S-8R AND S-9R .CRACK LENGTH 0.125 IN.APPROX. AT PASSENGER CABIN REPAIRED FUSELAGE BEAR STRAP FWD GALLEY DOOR LOCATED BTW BS 277 TO BS 320 AND BTW STR 5R TO STR 10R IAW EA M-
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