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 SWI2025F01290Skin · corrodedCORROSION ON FS1000.00 BETWEEN STGR24R - STGR22L AS MARKED (C-CHECK RO 09/07/2025)REMOVED CORROSION AT FS1000 BETWEEN STR 24R - STR22L. REWORK AREA FOUND TO BE STRUCTURALLY ACCEPTABLE PER REO 690-53-61-1628 REV -- 2025-06-11. COMPLIED WITH SKYWEST TASK CARD SDR SWI2025F01283Cover · corrodedLH SILL VENT COVER CORRODED BETWEEN FS1088.20 TO FS1098.20 OUTBOARD OF LBL27 AS MARKED (C-CHECK RO 09/07/2025)BLENDED OUT CORROSION ON LH SILL VENT COVER AND THEN COMPLIED WITH REO 690-53-61-1537 REV -- DATE 2025-04-07. COMPLIED WITH SKYWEST TASK CARD 51-900-SDR SWI2025F01272Cover · corrodedRH SILL VENT COVER CORRODED BETWEEN FS1088.20 TO FS1098.20 OUTBOARD OF RBL27 AS MARKED (C-CHECK RO 09/07/2025) BLENDED OUT CORROSION ON RH SILL VENT COVER CORRODED BETWEEN FS1088.20 TO FS1098.20 OUTBOARD OF RBL27 AND COMPLIED WITH REO 690-53-61-1538 REV -- DSDR DALA2025032602235Skin · corrodedCORROSION FOUND ON FWD AND AFT WASTE BOX PREVIOUS REPAIR DOUBLER AT WASTE SERVICE DOOR OPENING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 063-0001:10-0653-8- 7228/001 00153 CMOR: REPAIRED PER PRI 602195-14 REV 0, PRI 602195-14 REV 1, PRI 602195-14 REV 2, AND FSDR 2025FA0000199Skin Panel · corrodedCORROSION FOUND AT FS 779 THAT WAS CLASSIFIED AS LEVEL 2 AND A REPAIR WAS REQUIRED.SDR HNAA2025051200316Skin · crackedF035594 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0146SDR HNAA2025051200315Skin · crackedF035593 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 3R-4R. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 3R-4R IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0146.SDR HNAA2025051200314Skin · crackedF035592 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 3L-4L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 3L-4L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.SDR HNAA2025051200313Skin · crackedF035591 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 6L-7L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 6L-7L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.SDR HNAA2025051200312Skin · crackedF035590 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 8L-9L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 79 BETWEEN STRINGERS 8L-9L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.SDR HNAA2025051200311Skin · crackedF035589 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 8L-9L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 8L-9L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.SDR HNAA2025051200310Skin · crackedF035588 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 78 BETWEEN STRINGERS 6L-7L. PERFORMED SKIN BUSHING REPAIR ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FRAME 78 BETWEEN STRINGERS 6L-7L IAW EMB 145 SRM 53-32-01RE AND PIEDMONT EO1-53-25-0147.SDR IPXA2025040777721Skin · cracked**SUPPLEMENTAL SDR** STR- FOUND BENT FUSELAGE SKIN ABOVE RADOME RH HINGE. INSTALLED REPAIR DOUBLER AND REPAIR FILLER AT FUSELAGE SKIN ABOVE RADOME R/H IAW MD11 SRM 51-33-01 AND SRM 51-35-01 AND APPLIED TOP COAT IAW MD11 SRM 51-21-02 PROCESS B. / REMOVED PROTECSDR IPXA2025040277721Skin · cracked**SDR FILED OPEN** STR- FOUND BENT FUSELAGE SKIN ABOVE RADOME RH HINGE. ATA 53 OUT OF SEQUENCE VERIFIED STEP 2 AND 6 AND 7 RIISDR R61A2025033000162Doubler · corrodedWHILE IN BRIDGE CHECK - SUSPECTED CORROSION ON FWD LOWER CORNER OF WASTE DOUBLER. REMOVED AND REPLACED WASTE DOUBLER ON CENTER FUSELAGE III BTW FR88-FR89 STRGR 26R-28R. REF: EMB SRM 51-40-08.SDR DALA2025032602233Skin · corrodedFUSELAGE SKIN AT AFT SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLES 2OL, 4OL , 5OL, 6OL, 8OL, 9OL,10OL, 11OL, 12OL, 13OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/001 00260 REPAIREDSDR DALA2025032602232Scuff Plate · corrodedFUSELAGE SKIN AT FORWARD SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLE 7OL, 8OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 018-0001:5331-01297- 01B/001 00268 REPAIRED PER PRI 624621-14 REV 0, PRI 624621-14 RSDR SIMA20250321001Skin · dentedPROTRUSION ON FUSELAGE SKIN BTW FR 97-98 STGR 25R-27R. (MAJOR REPAIR) INSTALLED REPAIR DOUBLER AND FILLER ON FUSELAGE SKIN BTW FR 97-98 STGR 25R-27R IAW EMB 175 SRM 53-30-01 REPAIR 12P.SDR CALA2025032503184Bear Strap · crackedCRACK FOUND AT FWD GALLEY DOOR BEARSTRAP AT INTERNAL FUSELAGE STA.294.5 BETWEEN STR 8R AND 9R. CRACK LENGTH : 1"SDR CALA2025032503180Bear Strap · crackedEA5330-04213 REV D OP004: THE L1 DOOR SURROUND STRUCTURE HAS 1EA FASTENER HOLE WITH A CRACK INDICATION AT THE BOTTOM OF BEAR STR AP LAYER ONLY. DISCREPENT FASTENER MARKED IN RED. ESFR COMPLETED. PERFORMED REPAIR I.A.W B757-300 UAL EC/RA 5330-07485 AND VTMAE E SDR CALA2025032403146Skin · dentedRAMP REPORT DENT AT 48" FWD OF DOOR L1 BETWEEN STA 277 & STA 285 , APPROXIMATELY BETWEEN S-7L & S-8LMEASURED THE DENT W= 1.15" , Y( DEPTH) = 0.07" . W/Y RATIO = 16.42. REFERENCE: SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 - FUSELAGE SKIN TABLE 102 DENT AND SCRATCSDR 2025F00071Skin · corrodedMECHANICALLY REMOVED 12 LARGE AREAS OF CORROSION LOCATED ON TAIL CONE SERVICE DOOR OUTER FRAME SKIN IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FOR NOMINAL THICKNESS IAW C680 SRM 51-70-02.SDR SIMA20250320003Skin · damagedREAR FUSELAGE EXTERNAL SKIN AT FR 94 -4? AND STR 27R HAS LIGHNING STRIKE. (MAJOR REPAIR). BLENDED AREA ON REAR FUSELAGE IAW EMB 175 SRM 51-10-03, AREA MEASURES L=0.60 W=0.57 D=0.032. PERFORMED UT THICKNESS CHECK IAW EMB 175 NDTM 51-04-00 PART 4, REMAINING MATESDR AALA202504042604Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: EXTERIOR FUSELAGE SKIN AND SEVERAL FASTENERS UNDER RIGHT AFT RAM AIR INLET MODULATION PANEL HAS CORROSION. REMOVED CORROSION AT EXTERIOR FUSELAGE SKIN BS 500I TO 520 RIGHT AFT RAM AIR INLET MODULATION. PER B737 NG SRM 51-10-02-0G.SDR AALA202504042393Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: EXTERIOR FUSELAGE SKIN AND SEVERAL FASTENERS UNDER LEFT AFT RAM AIR INLET MODULATION PANEL HAS CORROSION. REMOVED CORROSION LOCATED AT BS 500I TO 520, PER B737NG SRM 51-10-02-0G.SDR DALA2025032502212Doubler · damagedTOILET SERVICE DOOR CUTOUT DOUBLER, FWD EDGE DAMAGED. WORK ACCOMPLISHED ON ER/A # 624822-14 AD REV - ORIGINAL ASSOCIATED ER/A 14-624822 ADDED FOR AC 8108. (LP# 0868332)SDR DALA2025032402166Doubler · corroded(LOG 0868202) RH LOWER FUSELAGE JUST AFTER WHEEL WHEEL BODY DRAIN DOUBLER CORRODED. FABRICATED AND INSTALLED NEW DOUBLER IAW BOEING DWG 146A3239, REV. - AND C.SDR JGVR20250320002Skin · corrodedBLENDED AREAS OF CORROSION LOCATED ON UPPER EXTERIOR FUSELAGE SKIN IN ZONE 254, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.SDR JGVR20250320001Skin · corrodedBLENDED 5 AREAS OF CORROSION LOCATED ON EXTERIOR FUSELAGE SKIN ALONG THE SEAM NEXT TO THE PILOT DV WINDOW IN ZONE 243 ALONG SEAM, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, SDR IPXA2025050946776Skin · damagedMAJOR REPAIR. DAMAGE ON RH SIDE NOSE CARGO DOOR STA 200 BETWEEN STRINGER S20 AND S21 PERFORMED PROTECTIVE TREATMENT OF SKIN SURFACE IAW. SRM 51-20-01-0G-0 REV. 45 WITH PRIMER. DEFERRED DAMAGE IAW. SRM 53-00-01-1A-2 FIGURE 101 CHART AREA B FOR 50 FLIGHT CYCLESSDR SWI2025F00634Skin · chafedFWD BAG BAY FUSELAGE SKIN CHAFING UNDER DOOR TOP AFT CORNER (C-CHECK RO 05/08/2025)REPAIRED DAMAGE TO FUSELAGE SKIN AT FWD BAG BAY TOP AFT CORNER IAW REO 670-53-31-1028 REV-- DATE 2025-04-18 AND CRJ700 SRM 51-12-00, 53-31-01, AMM 21-31-00. NDT PERFORMED BY BASDR SWIA202504090319Skin · dentedDENT FOUND ON FWD FUSELAGE LH SIDE ABOVE SKYWEST LOGO. EVALUATE AND REMOVE EVIDENCE OF DENT. (C-CHECK RO 04/08/2025)PERFORMED REPAIR ON FWD FUSELAGE EXTERNAL SKIN BETWEEN FRAMES 21-22 AND STRINGERS 14L-15L REF EMB SRM 53-10-01/REPAIR 12P. SEE CONTINUATION CARDSDR SWIA20250407319Skin · damagedFWD FUSELAGE UPPER SKIN HAS LIGHTNING STRIKE AT FRAME 3 BETWEEN STRINGERS 2L/2R. (C-CHECK RO 04/05/2025)PERFORMED PLUG REPAIR ON FWD FUSELAGE UPPER SKIN AT FR3, STGR CTL REF ETD2025-170-904818 REV.B. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WSDR SWIA202503270019Skin · dentedFOUND VERTICAL DENT ON AFT PART OF R/H FUSELAGE BELOW R/H ENGINE ASSY. DAMAGE LOCATION FOUND TO BE APPROXIMATELY 0.5" INCHES AFT OF THE AFT RIVET LINE OF FRAME 1051.3. DENT SPANS VERTICALLY APPROXIMATELY 6 INCHES AND INTERSECTS STGR 14R AT THE DENT MID-POINT. SDR IPXA2025032332357Skin · damagedMAJOR REPAIR, L/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28 PERFORMED REPAIR IAW EO-93137-REQ1.SDR VNAA20250320105Skin · dentedHN00198229 DISCREPANCY: FUSELAGE EXTERNAL SKIN IS DENTED BETWEEN F.S. 1015 TO F.S. 1031 STGR 26R TO STGR 25R. CORRECTIVE ACTION: REPAIRED THE EXTERNAL SKIN OF THE FUSELAGE BETWEEN FS1015 AND FS1031, STGR 25R TO STGR 26R IAW REO 670-51-00-085 REV: A DATED: 2017SDR VNAA20250320075Skin · ground damageHN00198891 SN: 00194 DISCREPANCY:DURING REMOVAL OF RH ENGINE BY PSA ENGINE REMOVAL TEAM BACKED LIFT INTO RIGHT SIDE OF FUSELAGE JUST AFT OF PYLON TRAILING EDGE AND TWO FOOT BELOW PYLON TRAILING EDGE. THE SKIN IS PUNCTURED. CORRECTIVE ACTION: REPAIRED PUNCTUREDSDR VNAA20250320051Doubler · corrodedHN00203627 SN: 00589 DISCREPANCY: INTERNAL ANTENNA DOUBLER BETWEEN FS 295.00 TO FS 310.00 STR 27 IS CORRODED CORRECTIVE ACTION: REMOVED CORRODED/UNSERVICEABLE TCAS OMNIDIRECTIONAL ANTENNA INTERNAL DOUBLER P/N SH670-32364-7S IAW CRJ 700 SRM 51-42-06-001-001-A01SDR IPXA202503212357Skin · damagedL/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28.SDR YENA2025032000293Skin · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE C FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 3 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00019) FUR-A320-53-02089, REF AEROMAN N/R 2025- 125698, PERFORMED PERMANENTE RESDR YENA2025032000287Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE LOC. BTW FR64 TO FR 65 AND BTW STR 30R T O STR 31R IN AFT CARGO COMPARTMENT. (SKIN); (RESOLVED ON W/O: 1353243 TASKCARD: NR-00025) REF AEROMAN W/O:2025 84/1 NR 2025 - 125815; PERFORMED PERMANENT REPAIR LOCSDR YENA2025032000280Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE LOC. BTW FR64 TO FR 65 AND BTW STR 30R T O STR 31R IN AFT CARGO COMPARTMENT. (SKIN); REF AEROMAN W/O:2025 84/1 NR 2025 -125815; PERFORMED PERMANENT REPAIR LOC. BTW FR64 TO FR 65 AND BTW STR 30R TO STR 31R SDR SWI2025F01172Skin · damagedFORWARD BAGGAGE BAY SURROUND STRUCTURE JOINT PLATE ON THE INNER SKIN AT FS533 STGR25L HAS A FASTENER HOLE WITH DAMAGE AROUND THE INNER EDGE OF THE HOLE. REMOVED AND INSTALLED NEW FORWARD BAGGAGE BAY SURROUND STRUCTURE JOINT PLATE ON THE INNER SKIN AT FS533 STSDR SWI2025F01171Skin · damagedFORWARD BAGGAGE BAY SURROUND STRUCTURE INNER SKIN FS533.00 BETWEEN STGR22L & 23L FASTENER IS PULLED INTO THE HOLE. REPAIRED FORDWARE BAGGAGE BAY SURROUND STRUCTURE INNER SKIN FS533 BETWEEN STGR22L & 23L IAW REO 670-53-31-1019, REV -A, DATED 2025-06-18. COMPLISDR SWI2025F01170Skin · gougedAFT FUSELAGE EXTERIOR PROTECTION PLATE GOUGED BETWEEN FS977.00 - FS985.00 STGR27. REPAIRED AFT FUSELAGE PROTECTOR PLATE SKIN FS977-FS985 STGR 27 IAW REO 670-53-00-290 REV F DATE 2019-04-26, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.SDR SWI2025F01168Skin · corrodedFORWARD BAGGAGE BAY SURROUND STRUCTURE INNER SKIN HAS SPOT OF CORROSION FS533.00 - FS549.00 STGR25L - 24L. REMOVED DAMAGE AREAS AT FORWARD BAGGAGE BAY SURROUND STRUCTURE INNER SKIN FS533.00 - FS549.00 STGR25L - 24L. AND COMPLIED WITH ALL STEPS OF REO 670-53-3SDR SWIA2025090200016Doubler · corrodedTCAS ANTENNA UNDERFLOOR DOUBLER HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS.295.00 AND FS.310.00 AT STR.27. REPLACED LOWER TCAS ATTACH DOUBLER BETWEEN FS295 - FS310 IAW SRM 51-42-06-001-001-A01 AND DWG: SH670-30023 REV G. LEAK CHECK GOOD. COMPLIED WITH TASK CSDR IPXA2025071516005Skin · gougedDENT AND GOUGE FOUND ON LEFT SIDE OF AIRCRAFT AT STATION 1794.5, JUST ABOVE STRINGER 8. REMOVED THREE FASTENERS IN BLEND OUT AREA PER ENGINEERING REQUEST. TAPE AND MEASUREMENTS AT AFFECTED LOCATION REF [T3F18E006A182] ALL STEPS OF EO-93108-REQ3 COMPLETED ON SHSDR HNAA2025043000780Skin · corrodedF034712 : FUSELAGE SKIN PREVIOUS REPAIR FILLER BETWEEN FR 67/68 STR21L/21R CORRODED. REPAIRED FUSELAGE SKIN PREVIOUS REPAIR FILLER BTW FR 67-68 AND BTW STR 21L-21R IAW PIEDMONT EO1-53-25-0119 AND EMB 145 SRM 53-31-01 RE ITEM C TYPE A, TABLE 209SDR AALA202503288480Skin · tornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE EXTERNAL POWER PANEL ACCESS DOOR CUTOUT HAS TORN SKIN AT LOWER EDGE. REPAIRED AREA AT RIGHT HAND SIDE OF FUSELAGE EXTERNAL POWER PANEL ACCESS DOOR CUTOUT. PER B737-NG SRM 53-10-15-2R PROCEDURE 4 REPAIR
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