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 R61A2021091200731Doubler · corrodedWHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON AFT FUSELAGE WASTE BOX INNER SKIN DOUBLER PN 170-86668-403 FWD INNER SURFACE AFT OF FR88. MX REPLACED SKIN DOUBLER PN IAW SRM 53-23-60 SEE AAT NRC# 45000949-1000-0008 FOR WORK PERFORMED. AC WAS RTS.SDR A6WA202109087870Skin · gougedSCRIBE MARKS ON LH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128 AND S17L TO S27L ALONG SEALANT LINE OF WING TO BODY FAIRING 191BB. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRIBE MARKS ON LH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128SDR R61A2021081700649Skin · gougedUNDER BELLY SKIN GOUGED BETWEEN FRAMES 27-28 STR 28R AS MARKED. REPAIRED UNDER BELLY SKIN BETWEEN FRAMES 27-28 STR 28R BY COMPLYING WITH ETD2021-170-025911SDR FDEA202108162020Skin · chafedLOWER CONTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT AFT LOWER EDGE FOUND WITH CHAFE MARK. LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT AFT LOWER EDGE CHAFE MARK CARRIED OUT REPAIR AS PER EA # 1-5330-T0362780 PART 1 AND PART 2. TITLE: FUSELAGE - PLSDR IPXA2021081672780Skin · crackedINSPECTION TYPE:N/AFUSELAGE SKIN CRACK AT RIGHT SIDE AIR CONDITIONING DOOR OPENINGACCOMPLISH FUSELAGE SKIN REPAIR IAW EO 80909-BSDR A6WA202109087872Skin · dentedDENT ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S18R TO S19R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENTED SKIN TO ORIGINAL CONTOUR ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S18R TO S19R TO ORIGINAL CONTOUR. P/N 601R35005. DENT MEASUREMENT L = 0.8SDR A6WA202109087873Skin · dentedDENT ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S24R TO S25R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENTED SKIN ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S24R TO S25R TO ORIGINAL CONTOUR. P/N 601R35005. DENT MEASUREMENTS L = 0.500Ï¿½ X W = 0.450ÏSDR A6WA202108307864Skin · dentedDENT AFT FUSELAGE SKIN AT FS656 S20R - S21R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO AFT FUSELAGE SKIN AT FS656 S20R - S21R. DENT DIMENSIONS L = 0.900Ï¿½ X W = 0.800Ï¿½ X D = 0.010Ï¿½. CUTOUT DIMENSIONS L=7.50Ï¿½ X W = 4.50Ï¿½. FSDR IPXA2021091173801Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN IS CORRODED AT XCW -91 AND STRINGER 18.REPAIRED CORRODED CENTER WING UPPER SKIN BETWEEN XCW -70 TO XCW -110 AND BETWEEN STRINGER 17 & 19 IAW EA 011-5730-01-A9306 REV. IR AND UPS EO MD11-5730-81382-A. (MAJOR)SDR IPXA2021091173798Skin · corrodedINSPECTION TYPE:3C CENTER WING UPPER SURFACE SKIN AT STRINGER 15 BETWEEN XCW -104 TO XCW 49.25 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SURFACE SKIN AT STRINGER 15 BETWEEN XCW -104 TO XCW 49.25 IAW VT-SAA EA 011-5730-01-9330 REV. IR AND UPS EO MD11-5730SDR SWAA2021090307285Skin · corrodedCORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES. BS 694; RBL 4.8 WL 308.25. ; / [01] REMOVED CORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES L=1 W=1 PER REF SRM 53-00-01-1A -1 AND ARM90-7023-01; [02] VERIFIED DAMAGE REMOVED; L=32.5 W=1; PER SRM 53-SDR IPXA2021083173377Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN BETWEEN XCW 45 TO XCW 48 AT STRINGER 19 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN BETWEEN XCW 45 TO XCW 48 AT STRINGER 19 IAW VT-SAA EA 011-5730-01-A9303 REV. IR AND UPS EO MD11-5730-81391-A. (MINOR)SDR IPXA2021082873235Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN BETWEEN XCW -76 TO XCW -79 AT STRINGER 21 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN BETWEEN XCW -76 TO XCW -79 AT STRINGER 21 IAW VT-SAA EA 011-5730-01-A9313 REV IR AND UPS EO MD11-5730-81383-A. (MINOR)SDR IPXA2021082873234Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN BETWEEN XCW -101.5 TO XCW -104.5 AT STRINGER 21 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN BETWEEN XCW -101.5 TO XCW -104.5 AT STRINGER 21 IAW VT-SAA EA 011-5730-01-A9309 REV. IR AND UPS EO MD11-5730-81419-A. SDR REXA2021082500638Doubler · corrodedLOWER TCAS ANTENNA INTERNAL DOUBLER CORRODED AT FS 300 STR 27. - REMOVED & REINSTALLED TCAS ANTENNA IAW CRJ 900 AMM 34-43-01-001-400-801-A03, REMOVED AND REPLACED ANTENNA DOUBLER IAW SRM 51-42-06-001-A01, 51-40-11-001-001-A01, OPS CHECK IAW AMM 34-43-00-710-80SDR DALA2021081604695Door Frame · crackedDURING INSPECTION FOUND CRACK AND BENT ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NBR 114AR. CRACK ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NBR 114AR (FUS) WAS REPAIRED PER ER/A 593393-14 REV ORIGINAL SECTION 1 PERMASDR SWAA2021091547128Panel · crackedPANEL 193AL HAS 3EA CRACKED FASTENER HOLES ON AFT EDGEBAND; 12.5' FROM UPPER EDGE TO 18.4' FROM UPPER EDGE ; / [01] IDENTIFIED PANEL #193AL IAW SRM 53-40-70-0I-1; FIGURE 2; TABLE 2; ITEM 7. <BR> <BR>REMOVED FINISH IAW AMM 51-21-11-150-815 PARA. 17. C. AND D. <SDR DALA2021081704775Skin · damagedLUG LOCATION #1 FROM THE GOGO DEMOD HAS SKIN DAMAGE AROUND THE MOUNTING FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:2330-01347-16D/001 00002 REPAIRED PER PRI/ERA 593409-14 REV ORG. (LP# 1910465)SDR DALA2021081704774Skin · damagedLUG LOCATION #2 FROM THE GOGO DEMOD HAS SKIN DAMAGE AROUND THE MOUNTING FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:2330-01347-16D/002 00003 REPAIRED PER PRI/ERA 593409-14 REV ORG. (LP# 1910464)SDR DALA2021081704773Skin · damagedLUG LOCATION #3 FROM THE GOGO DEMOD HAS SKIN DAMAGE AROUND THE MOUNTING FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:2330-01347-16D/003 00004 REPAIRED PER PRI/ERA 593409-14 REV ORG. (LP# 1910463)SDR DALA2021081704772Skin · damagedLUG LOCATION #5 FROM THE GOGO DEMOD HAS SKIN DAMAGE AROUND THE MOUNTING FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:2330-01347-16D/005 00006 REPAIRED PER PRI/ERA 593409-14 REV ORG. (LP# 1910460)SDR AALA202108164925Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND LOWER FUSELAGE INTERNAL SKIN AIR INLET DUCT FLANGE BETWEEN FR 21 AND FR 22. REPLACED FLANGE PER SRM 51-72-11.SDR DALA2023091307517Unknown · unknownSHIP 0692 DENT ON FUSELAGE SKIN BTWN STA 640/STA 660 AND BTWN S-24L/S-25L. CORRECTIVE ACTION: REF ERA 611161-14 (1909118)SDR DALA2022081605572None · noneERA 593409-14 SECTION I ACCOMPLISHED IN MSP 12AUG21. FOLLOW ON A CTION IS REQUIRED. ACCOMPLISH ERA 593409-14 SECTION II WITHIN 60,000 FC OR 120,000 FH OF SECTION I. ASSOCIATED ER/A 30-593409 ADDED FOR AC 3025. (LP# 1909626)SDR DALA2021081304669Fastener · damagedSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND DAMAGE FASTENER APPROXIMATELY AT FRAME 1 26 L/H SIDE OF FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 599821-14 REV. PERFORMED PERMANENT REPAIR SIDEWALL SKIN PANEL AT FR. 1 ABOVE LOWSDR DALA2021081304670None · noneSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND PIN HOLE PITTING IN SKIN FWD OF FRAME 1 STRINGER 26 APPROXIMATELY. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR FOR LIGHTNING STRIKE LOCATED BTW FRO TO FR1 AT 15.500 INCHES UP OF LOWESDR DALA2021081304674None · noneSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND DAMAGED FASTENER APPROXIMATELY AT FRAME 5 L/H SIDE OF FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR FOR LIGHTNING STRIKE LOCATED FR5 AT 8 INCH BELOW OF LOWER STRINGER L/H SIDSDR DALA2021081304673None · noneSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND DAMAGED FASTENER APPROXIMATELY AT FRAME 9 L/H SIDE OF FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR FOR LIGHTNING STRIKE LOC. FR9 AT 18 INCH BELOW OF LOWER STRINGER L/H SIDE SDR DALA2021081304672None · noneSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND DAMAGED FASTENER APPROXIMATELY AT FRAME 11A STRINGER 43 L/H SIDE OF FUSELAGE. CORRECTIVE ACTION: PERFORMED PERAMANENT REAPIR FOR LIGHTNING STRIKE LOCATED AT FR 11A AND STR 43 L/H SIDE SDR DALA2021081304671None · noneSUPPLEMENTAL INFORMATION SHIP 3304 DURING LIGHTNING STRIKE INSPECTION FOUND DAMAGE FASTENER APPROXIMATELY AT FRAME 15A STRINGER 45 L/H SIDE OF FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR FOR LIGHTNING STRIKE LOCATED AT FR 15A STR 45 L/H SIDE. AS PESDR SWAA2021092106267Gusset · crackedRH GUSSET CRACKER AT STA 500D; WL 200; STR 19R ; / [01] REMOVED RH GUSSET AT STA 500D WL 200 STR 19R. REF. BOEING 737-700 SRM 51-40-02-0G--; [02] VERIFIED 1; [03] LOCATED AND DRILLED NEW GUSSET AT STA 500D STGR 19R. REF. BOEING 737-700 SRM 51-40-05-0G-0; [04] SDR DALA2021081604715Skin · corrodedSHIP 650 CORROSION FUSELAGE SKIN BTW STA 760 TO 780 AND S-27L TO S-27R WITH ON STR 28 LH +4 IN THEREFORE AREA IT IS OUT OF LIMITS IN REF NRC 00812. (1907569)SDR DALA2021081204650Skin · dentedSHIP 3158 - DENT EXTERNAL SKIN AT FR 18 BTW STR 37/38 LH LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED SECTION 1 PART A AND PART B ON FRAME 18 AT LEVEL STR37LH AND STR38LH LOWER FUSELAGE AS PER ERA 593178-14 REV ORIGINAL.(1908190)SDR DALA2021081204643Skin · damagedSHIP 3158 - CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 58 AND BTW STR 42R TO STR 43R LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR EXTERNAL SKIN LOCATED FR 58 TO FR59 AND BTW STR 42R TO STR 44 LOWER FUSELAGE AS PER ESDR DALA2021081104614Skin · corroded(LOG 1907567) DURING INSPECTION FOUND CORROSION ON EXTERNAL FUSELAGE SKIN BTW S-20LH AND S-21LH, STA 917. ORROSION ON EXTERNAL FUSELAGE SKIN BTW S-20LH AND S-21LH, STA 917 WAS REPAIRED PER B737-800 SRM 53-70-01-2R-3.SDR FDEA202108112001Skin · dentedFUSELAGE SKIN @ STA 1730, BETWEEN STR 29L - STR 29R, HAS 2EA DENTS. REPAIRED SKIN IAW FEDEX EA # F-5330-146539-P3SDR 2021F00244Skin · chafedLWR SKIN CHAFE FROM ANTI - ICE CROSSFLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/15/2019, STANDARD REPAIR - 680A ALL S/N LWR SKIN CHAFE FROM ANTI - ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 DATED 07/19/2019. COMPLETESDR DALA2022080805401None · none(LOG 1906288) ELONGATED HOLES AND MISDRILLS FOUND DURING IDTV REMOVAL. DAMAGE REPAIRED PER ERA 593376-14.SDR SWAA2021090705872Doubler · corrodedCORROSION ON DOUBLER AT FWD CARGO BAY BS500A+12 BL0 WL148. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NSDR SWAA2021090705864Doubler · corrodedCORROSION ON DOUBLER AT FWD CARGO BAY BS500+8 BL0 WL148. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO SDR JJBA20210810041Skin · dentedDENT WITH RIVET PLUGS ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PERFORMED CUT-OUT ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PREDRILLED DOUBLER RIVETS LAYOUT IN SKIN ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. FSDR V0XD20210810008Skin · dentedTHERE IS A DENT ON THE FWD R/H FUSELAGE BETWEEN FS 177.00 AND F.S. 185 AT STGR 23R. CORRECTIVE ACTION: BLENDED DISCREPANT AREA IAW STS ENGINEERING SOLUTIONS ENGINEERING AUTHORIZATION 69-2021-124 IR DATED 8/6/2021. ***DTE REQUIRED WITHIN 12 MONTHS OF RTS.SDR SWAA2021092105414Doubler · crackedFWD FUSELAGE EXTERNAL POWER SUPPLY COMPARTMENT CUTOT AFT EDGE DOUBLER CRACKED MKD DOT ; / COMPLETED INSTALLATION OF NEW EGPR DOUBLER PER B737-700 SRM 51-40-02-0G-0 AND DRAWING # 141A0640SDR SWAA2021090205450Panel · corrodedPANEL 192F SHOWS SURFACE CORROSION AROUND THE BEACON ANTENNA HOLE ; / [01] RECEIVED SERVICEABLE PANEL P/N 149A7755-1. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q005EBPQ.; [02] VERIFIED WILL BE INSTALLED ON TASK TTG8Q005EBPQ.SDR DALA2021081104610Skin · corrodedSHIP 650 REF. ER/A 593188-14; FUSELAGE / SKIN / STA 760 TO STA 780, S-28L TO S-28R / CORROSION; TIME LIMITED REPAIR REQUIRES ADDITIONAL DTE. CORRECTIVE ACTION: REFER TO ER/A 593188-14. (1905908)SDR FDEA202108092002Skin · dentedFUSELAGE EXTERIOR SKIN DENT/CREASE - AFT OF CENTER CARGO AT APPROX STA.1850 BETWEEN LONGS 38-39. CUT OUT DAMAGED SKIN AT STA. 1850 BETWEEN LONGERONS 38R AND 39R AND INSTALLED REPAIR PER SRM 53-20-00 FIG. 6 SH.12-15 VOL.1. "MAJOR REPAIR"SDR FDEA202108091997Skin · chafedRH FWD PAX DOOR UPR CUTOUT SKIN FOUND CHAFE MARKS REPAIRED THE CHAFE MARKS AT RH FWD PAX DOOR UPR CUTOUT SKIN (FAIL SAFE RING) PER EA 6-5310-T0363353 A P1. TITLE: FUSELAGE MAINFRAME - RH FWD CREW/COURIER DOOR FAIL SAFE RING CHAFE/WEAR DAMAGE - BLEND REPAIRSDR CALA2021080901302Skin · corrodedPOSSIBLE INTERIOR SKIN CORROSION ON WASH, SKIN AND RIVETS BUCKLED FROM STA 360 TO STA 400 AROUND S-26 LEFT APPROX. [EXTERIOR SKIN CIRCLED] FLEET CYCLE LOG PAGE 9780955. INITIATE A 2ND DTA DIP FOR "PLANNING TO CONTACT ENGINEERING AFTER 16 MONTHS, BUT BEFORE 17 SDR ASMF202110009None · noneDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL LIGHTNING STRIKES ON NEAR LEFT SIDE RADOME AND RH WINGLET TIP. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-19, DETECTING SEVERAL LIGHTNING STRIKES ON NEAR LEFT SIDE RADSDR SWIA202161461None · bentFUSELAGE SKIN CUT-OUT FOR NOSE LANDING GEAR AT AFT EDGE HAS INTERNAL ANGLES THAT ARE BENT. (C-CHECK RO 9/27/2021) PERFORMED DOUBLER REPAIR TO LOWER FUSELAGE SKIN BETWEEN FS220-280, STGRS 25L - 25R REF MHIRJ REO 670-53-11-1720 REV -- DATED 2021-08-24 AND
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