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 ASAA2023122947511Skin · dentedLESSOR ITEM 100; (73875) 1 OFF DENT L/H REAR FUSELAGE LOWER APPROX FR 79. GROUNDED - YES. EVALUATED DENT 7.2" AFT OF FR 76, 1.8" DOWN OF STGR 26LH. D/A LESS THAN OR EQUAL TO 0.1 DENT IS .018/1 LESS THAN OR EQUAL TO 0.1 FOUND TO BE WITHIN LIMITS IAW ASA A320 SRSDR CALA2024010200016Skin · damagedFOUND FIVE LIGHTNING STRIKES ON LEFT HAND OF FUSELAGE BETWEEN ST. 218 AND ST. 237, WL 192 AND WL 187. REPAIR REQUIRED ON OR BEFORE 50,000 FLIGHT CYCLES, REPETITIVE REPAIR 8 STEP 5. TABLE 202. INSPECTION EVERY 9,000 CYCLES THERAFTER. REF. SRM 53-10-01-2R-8 REPASDR MAS2024F00000Skin · dentedAFT LH LOWER FUSELAGE SKIN DENTEDSDR DALA2023122910729Unknown · unknownAIRCRAFT 1603, AD / EM-EO TASK -ON S13AR HFEC INSPECTION FOUND 01 EA CRACK AT STA 1659, IT IS ABOUT 0.2 INCH LONG AS MARKED. CORRECTIVE ACTION: THE CRACK LENGTH IS 0.2 INCH. REPAIRED THE CRACKED SKIN AT STA 1659: S-13AR AS PER B767-300 SRM53-80-01-2R-7 FIG201 SDR JR2R20231229592Doubler · corrodedTEXAS DOUBLER ON FR90 CORRODED. REMOVED AND REPLACEDSDR ASAA2023122848261Skin · dentedLESSOR ITEM: DENT LOCATED LH SKIN PANEL 1" FWD OF FRAME 9, 14" BELOW CAPTFIXED WINDOW CUT OUT. NEED PERMENANT REPAIR ACCOMPLISHED. ALSO, REFERENCE DB CHART ITEM 10 GROUNDED - YES. STRIPPED AREA IAW SRM 51-75-11/001, REV 146-01AUG2023 DENT DEPTH .031, LENGTH 2SDR SWIA2024021931228Skin · gougedLEFT SIDE PITOT STATIC SKIN CUT OUT HAS GOUGING AROUND NUT PLATE HOLES BETWEEN STGR 14L AND STGR 15L (C-CHECK RO 2/18/2024) REMOVED AND INSTALLED NEW LEFT SIDE PITOT STATIC MOUNTING PLATE BETWEEN STGR 14L AND STGR 15L REF CRJ 700 SRM 51-40-11-001-001-A01. SDR R61A2024012900054Skin Panel · dentedAIRCRAFT DAMAGED ON FWD NOSE FROM FRA 1 TO FRA 6 AND STR 6L TO STR 6R . REPAIRED A/C IAW ETD2023-170-032803,ETD2024-170-002628 AND EMB SRM 51-41-01,51-41-02 AND 51-43-00. ALSO REF VP-055456-2023 NR 1 THRU 6 ,13,15,23 THRU 29 AND 49.SDR IPXA2024010381409Unknown · unknown*SDR FILED OPEN* FAULT - DENT, FUSELAGE EXTERNAL SKIN, STA 718, S-38R~S-39R. (EVALUATE) 1. MEASURED THE DENT ON FUSELAGE STA 718 S-38R~S-39R LENGTH=0.9" WIDTH(A)=0.9" DEPTH(Y)=0.009" AND A/Y = 100, FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL ISDR DALA2024010210744Unknown · unknownSHIP 3251 DISC: DENT EXTERNAL SKIN LOCATED BTW FR 29 TO FR 30 AND STR 36R TO STR 37R A T LOWER FUSELAGE. C/A: EVALUATED DENT LOCATED ON EXTERNAL SKIN BTW FR 29 TO FR 30 AND STRG 36R TO STRG 37R LOWER FUSELAGE AND FOUND WITHIN LIMITS AS PERA320 SRM 53-00-11-283SDR EE4Y2023122819073Skin Panel · burnedFORWARD FUSELAGE, FR06, STRINGER 24RH+40MM, EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030843 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER COO-EO-2023-18932-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILSDR EE4Y2023122819071Skin Panel · burnedFORWARD FUSELAGE, AT X=2743.5 STRINGER 15RH+120MM, AT FR10 STRINGER 17RH, AND AT FR11+260MM STRINGER 17RH EXTERNAL SKIN WITH LIGHTNING STRIKES. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030848 GUIDELINES AS STATED IN COOPESA ENGINEERING OSDR HNAA2024013000039Doubler · improper partE015153 FLUSH DOUBLER REPAIR AT FR 73 STGR 18L HAS NO DTI INFORMATION. REMOVED DOUBLER AND FILLER, FABRICATED SERVICEBLE DOUBLER AND FILLER AND INSTALLED REPAIR AT FR 73 AND STGR 18L IAW EMB 145 ETD2024-145-000911 AND EO1-53-24-0046.SDR DALA2024010210751Unknown · unknownGOUGES FOUND AT FUSELAGE BELLY SKIN FOR #1 RAD ALT TRANS ANTENNA. SUMMARY NRC 003-0001:0514-2001/001 00011: C/W ERA 614660-14 REV ORIG REPAIR INSTRUCTIONS. CHECKED TO ENSURE ALL PRI'S MATCH ERA 614660-14 REV ORIG. REPAIRED SKIN PER ERA 614660-14 REV ORIG. (LP SDR DALA2024010210749Unknown · unknownSHIP 3242 DISC: SCRATCH ON EXTERNAL SKIN ON STATIC PORT LOCATED BTW FR 23 TO FR 24 LEV EL STR 32L AT LOWER FUSELAGEE. C/A: EVALUATED REWORK ON EXTERNAL SKIN JOINED POINT 1 AND POINT 2, JOINED POINT 3 AND POINT 4 LOCATED STATIC PORT FR23 TO FR 24 LEVELSTR 33L ASDR DALA2024010210748Unknown · unknownSCRATCH EXTERNAL SKIN STATIC PORT LOCATED BTW FR 23 TO FR 24 AT LEVEL STR 33R AT LOWER FUSELAGE. C/A: EVALUATED REWORK ON EXTERNAL SKIN JOINED POINT 1 AND POINT 2, JOINED POINT 3 AND POINT 4,POINT 5, POINT 6 AND POINT 7 LOCATEDSTATIC PORT LOCATED BTW FR 23 TO SDR DALA2024010210746Skin · dentedDENTS ON EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 & STR 16L TO STR 1 7L ON UPPER FUSELAGE (5 EA). EVALUATED DENTS (5 E/A) EXTERNAL SKIN LOCATED BTW FR69 TO FR70 AND STR16L TO STR17L ON UPPER FUSELAGE FOUND WITHIN LIMITS IAW SRM 53-00-283-005 PARA 2.A.(1) FIG SDR DALA2024010210745Unknown · unknownSHIP 3242 DISC: DENT EXTERNAL SKIN LOCATED BTW FR 84 TO FR 85 AND STR 10R TO STR 11R T AIL CONE AT LOWER FUSELAGE. C/A: EVALUATED DENT EXTERNAL SKIN LOCATED BTW FR 84 TO FR 85 AND STR 10R TO STR 11R TAIL CONE AT LOWER FUSELAGE AND FOUND WITHINLIMITS AS PER A32SDR DALA2023122810697Unknown · unknownSHIP 6817 CORROSION ON EXTERNAL STRAP AT FUSELAGE SKIN STA BTW 1787.45-1795 APROX AND STGRS 3R-6R AROUND APU AIR INLET. CORRECTIVE ACTION: SUMMARY OF NRC 00046: EXTERNAL STRAP AT FUSELAGE SKIN STA BTW 1787.45-1795 APROX AND STGRS 3R-6R AROUND APU AIR INLET WASSDR DALA2023122810690Unknown · unknownAIRCRAFT 1705, FOUND RH FUSELAGE TO H/STAB CUTOUT FORWARD FAIRING SKIN WORN AT STA1725 S20R. CORRECTIVE ACTION: RH FUSELAGE TO H/STAB CUTOUT FORWARD DAMAGED FAIRING SKIN. REMOVED AND REPAIRED AS PER B767-300 SRM53-80-01-2R-3 FIGURE 201 REV121.00 APR-25-2023. (SDR DALA2023122810689Unknown · unknownAIRCRAFT 1705, FOUND LH FUSELAGE TO H/STAB CUTOUT FORWARD FAIRING SKIN WORN AT STA1725 S20L. CORRECTIVE ACTION: LH FUSELAGE TO H/STAB CUTOUT FORWORD DAMAGED FAIRING SKIN REMOVED AND REPAIRED AS PER B767-300 SRM53-80-01-2R-3 FIGURE 201 REV121.00 APR-25-2023. (LSDR EE4Y2023122719070Skin Panel · misrepairedPER CUSTOMER REQUEST REPLACE THE FASTENER INSTALLED ON CENTER FUSELAGE I, FR26+94MM, STRINGER 11RH+105MM, EXTERNAL SKIN WITH THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2018-190-086940 GUIDELISDR EE4Y2023122719069Skin Panel · misrepairedPER CUSTOMER REQUEST REPLACE THE FASTENER INSTALLED ON CENTER FUSELAGE III, AT FR90+140MM, STRINGER 27RH+17MM, EXTERNAL SKIN WITH EXISTING THROUGH DAMAGE REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2011-190-SDR EE4Y2023122719068Skin Panel · misrepairedCENTER FUSELAGE III, FROM FR81+95MM TO FR82+85MM, BETWEEN STRINGER 23LH+35MM AND STRINGER 26LH+105MM, EXTERNAL SKIN WITH EXISTING REPAIR WITHOUT TRACEABILITY OF MATERIALS. FURTHERMORE, FROM FR80+70MM TO FR81+70MM, BETWEEN STRINGER 23LH AND STRINGER 24LH EXTERNSDR EE4Y2023122719067Skin Panel · damagedCENTER FUSELAGE I, AT FR25+235MM, STRINGER 26LH+17MM, EXTERNAL LOWER SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030721 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18924-R00 INSTRUCTIONS ( FSDR EE4Y2023122719066Skin Panel · burnedCENTER FUSELAGE I, FROM FR33+40MM TO X=11035.0, BETWEEN STRINGER 24LH AND STRINGER 25LH, LOWER EXTERNAL SKIN WITH LIGHTNING STRIKES. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030701 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COSDR EE4Y2023122719065Skin Panel · misrepairedFORWARD FUSELAGE, BETWEEN FR16+250MM AND FR18+80MM, AND BETWEEN STRINGER 20RH AND STRINGER 21RH, EXISTING SKIN REPAIR EVALUATION. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030699 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-ESDR EE4Y2023122719064Skin Panel · burnedLOWER FUSELAGE, AT FR01+150MM, STRINGER 24RH+130MM, EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030945 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18945-R00 INSTRUCTIONS ( FOR ADDITSDR EE4Y2023122719063Skin Panel · burnedLOWER FUSELAGE, AT FR76+365MM, STRINGER 26LH+142MM EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030547 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18904-R00 INSTRUCTIONS ( FOR ADDITISDR IPXA2023122648565Unknown · unknown*SDR FILED OPEN* FAULT - FUSELAGE SKIN AT STA 1050.25 BETWEEN S21L AND S22L FOUND WITH BLEND MARK RECOMMENDED ACTION TO MEASURE BLEND OUT MARKSDR DALA2023122810682Unknown · unknownSHIP 1706 FUSELAGE DRAIN VALVE HOLE AT STA 1543.1 FOUND CORROSION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 614196-14 (0125131)SDR DALA2023122810675Unknown · unknownSHIP 1706 FUSELAGE DRAIN VALVE HOLE AT STA 1420.1 FOUND 1EA CORROSION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 614196-14 (0125140)SDR DALA2023122610573Unknown · unknownSHIP 3217 DISC: ON WALK AROUND FOUND CREASE & DENTS FR 3, 12" ABOVE LOWER LAP OF SKIN D5311340220600. C/A: TRANSFERRED TO N/R #1 (WIP174073). NON-REOUTINE LOG # 0124665.. (LP 4595639)SDR DALA2023122610572Unknown · unknownSHIP 3217 DISC: TRANSFERRED FROM LP 4595639. ON WALK AROUND FOUND CREASE & DENTS FR3 12" ABOVE LOWER LAP OF SKIN D5311340220600. C/A: REMOVED EXISTING FASTENERS IN THE REPAIR AREA. CUT OUT DAMAGED SKIN AND DEBARR EDGES OF CUTOUT (WIP 174075) PERFORMED HFEC OF SDR IPXA2024020724315Skin · damagedSCRATCH MARK FOUND AT FUSELAGE EXTERNAL SKIN STA 368 TO STA 390, S-10L REFER TO FAULT T3F18E003NRT7 FOR DETAILS. REVIEWD FAULT MOVED TO REFERENCED BAR CODESDR R61A2024011800002Skin · dentedDENT FOUND ON FUSE SKIN BTWN FR9-10 AND BTWN STR 15L-16L. MX REPAIRED IAW ETD2024-000369.SDR IXXA20240103Skin · damagedLH FUSELAGE LIGHTNING STRIKE DAMAGE AT STATION 387 STRINGER33LSDR DALA2023122610600Unknown · unknownSHIP 0670 FUSELAGE / EXTERNAL SKIN / BSTA 767 / AT S-26R / TOOL DAMAGE. CORRECTIVE ACTION: REF ERA 614283-14AD. (0122329)SDR DALA2023122610584Unknown · unknownSHIP 3407 WHILE ON THE LINE IN AMS, MTC DISCOVERED GOUGE DAMAGE COMMON TO THE LOWER AFT EDGE OF THE FWD CARGO DOOR SURROUND SKIN, PN: F5327060020000. FOLLOWING CLEANUP, THE DAMAGE MEASURES 0.150IN FWD/AFT, 0.125IN DEEP, AND IS 2.5IN CIRCUMFERENTIALLY. THE DAMASDR IPXA2023122624315Unknown · unknown*SDR FILED OPEN* FAULT - SCRATCH MARK FOUND AT FUSELAGE EXTERNAL SKIN STA 368 TO STA 390, S-10L OK TO WORKSDR AALA202403305542Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE INTERNAL SKIN IN AFT CARGO COMPARTMENT BETWEEN FE 63 AND FR 64, BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER SRM 53-00-11-300-042.SDR R61A2024011200788Skin Panel · damaged30+ TOTAL LIGHTNING STRIKE DAMAGE IN BAY FR 18-19 AND STR 27-28R. REPAIRED LIGHTNING STRIKE DAMAGEAT FRAME 18-21 STRINGER 27L-27R WITH DOUBLER TRIPLER,FILLER REPAIR IAW WITH ETD2023-170-032470 REV.: ASDR R61A2024011200787Skin · damaged"LIGHTNING STRIKE DAMAGE ON SKIN EDGE NEXT TO GPS ANTENNA. A FR 43-45, STR1L-STR 1R WITH DOUBLER ,FILLER REPAIR IAW WITH IAW EMB 175 SRM 53-22-01 REPAIR 11P"SDR R61A2024011200786Skin Panel · damagedLIGHTNING STRIKE DAMAGE ON 2 FASTENERS STR 1L-1R FWD OF SKIN SPLICE ON 3RD ROW FR 34. REMOVED LIGHTNING STRIKE DAMAGE FR 34 SKIN SPLICE BETWEEN STRG. 1L -1R, BY REMOVE AND REPLACING RIVET IN AREA 1 FREEZE PLUG BUSHING PER ETD2023--170-032829 REV.:B.SDR R61A2024011200785Skin · burnedLIGHTNING STRIKE DAMAGE ON FASTENER ON FR 32 BETWEEN STR 1L-1R. : REMOVED LIGHTNING STRIKE DAMAGE ON FASTENER ON FR 32 BETWEEN STR 1L-1R BY INSTALLING FREEZE PLUG REF EMB 175 SRM 53-00-00 REPAIR 03P.SDR R61A2024011200784Skin · damagedLIGHTNING STRIKE DAMAGE ON FASTENER ON STR 1L BETWEEN FR 28-29. REMOVED LIGHTNING STRIKE DAMAGE ON FASTENER ON STR 1L BETWEEN FR 28-29 AND INSTALLED FREEZE PLUG REF EMB 175 53-00-00/REPAIR 03P.SDR DALA2024010200028Unknown · unknown(LOG 5511959) FOUND DAMAGE OT STA 218 BETWEEN STRINGER 23-24 AND STA 500C +15 BETWEEN STR 22-21. COMPLIED WITH ERA 614705-14.SDR DALA2023122610604Unknown · unknownSHIP 0670 FUSELAGE / EXTERNAL SKIN / BSTA 767 / AT S-26R / TOOL DAMAGE. CORRECTIVE ACTION: REF ERA 614286-14AD. (0121725)SDR DALA2023122610567Unknown · unknown(LOG 0121715) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 727 TO 727B BETWEEN STR 1 AND STR 2R. C/W ER/A 614245-14 REV ORIGINAL.SDR DALA2023122610566Unknown · unknown(LOG 0121712) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 663 TO 706 BETWEEN STR 1 AND STR 2R. C/W ER/A 614216-14 REV ORIGINAL.
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