JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 A6WA202110137899Skin · dentedMULTIPLE DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION P1- L = 7SDR A6WA202110137898Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 5.300Ï¿½ X W = 0SDR JJBA20210929017None · noneAFTER NDT INSPECTION, RH FUSE SKIN FOUND CRACKED AT FR 75 BTW STR 2R-3R. RH FUSE SKIN AT FR 75 BTW STR 2R-3R CRACK REMOVED. RH FUSE SKIN AT FR 75 BTW STR 2R-3R REPAIREDSDR CALA2021100101734Plate · noneFORWARD CARGO DOOR SILL HAS CORROSION IN MULTIPLE PLACES PER NR 9292224 / 26224 A3NB-53-36105 GEN BY V077960 RMVD AND RPLD FORWARD CARGO DOOR SILL FROM FR24 TO FR28 STR34 IA W DWG C2D53231725 AND A320 200 SRM 51-42-11/001 BY MECH V061680 INSP BY V077960.SDR CALA2021100101733Plate · noneAFT CARGO AT LWR DOOR OPENING SILL WEB AT FWD CORNER HAS 3 EA GO UGES.(A3NB-53-4-6179). GENERATED BY N078592 AT HAECO LCQ PER NR. 9294563 (28563) REMOVED AND REPLACED AFT CARGO LWR DOOR SILL WEB IAW A320 SRM 51 -42-11. PERFORMED BY V052030 AND INSP BY V061334.SDR CALA2021100101728Stringer · corrodedAFT CARGO FR59 STRGR43LT STRINGER CORRODED. (A3NB-53-4-6199). GE NERATED BY N078592 AT HEACO LCQ PER NON-ROUTINE 9294543. (28453) INSPECTED BY V061334. REMOVED AND REPLACED STRINGER AT FR.59 STRGR 43L. IAW A320 SRM 5 1-72-11-911-001. PERFORMED BY V052030 INSP SDR R61A2021101900811Finger Doubler · corrodedWHILE AT HEAVY CHECK FOUND CORROSION ON FWD CARGO DOOR CUTOUT FWD FINGER DOUBLER. REMOVED AND REPLACED FWD CARGO FWD FINGER DOUBLER REF: EMB SRM 51-40-02,51-23-04. INSTALLED
REF.EMB 175 SRM 51-
40-08 APPLIED SURFACE PROTECTION AS REQUIRED FWD
CARGO FWD FINGSDR JJBA20210928026None · noneUNRECORDED PATCH NEEDS TO BE REMOVED FOR INVESTIGATION BTW FR 19-20, STR 11-12. UNRECORDED REPAIR PATCH REMOVED BTW FR 19-20 PAINT STRIPPED BTW FR 19-20, STR 11-12 AT UNRECORDED PATCH LOCATION. PERMANENT REPAIR DOUBLER PERFORMED BTW FRAME 19-20 AND STR 10L-12LSDR SWIA202162771None · corrodedEVIDENCE OF CORROSION ON BRACKET PLATE AT STGR 27, FS549.00 OF INTERNAL SURROUND STRUCTURE OF THE FORWARD BAGGAGE BAY DOOR. (C-CHECK RO 11-24-21) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW PSDR SWIA202162769None · chafed* EXTERNAL LOWER FUSELAGE TRIPLER BETWEEN FS 969.00 AND FS 985.00 HAS SEVERAL CHAFES AT APPROX. STGR 27. (C-CHECK RO 11-24-21) REMOVED AND REPLACED THE FUESELAGE TRIPLER BETWEEN FS969.00 AND FS985.00 REF. CRJ700 SRM 51-42-21-001-001-A01 AND REO 670-53-00-2SDR SWIA202162768None · corrodedEVIDENCE OF CORROSION ON BRACKET PLATE IN BETWEEN STGR 27 AND STGR 26L, AT FS535.00 OF INTERNAL SURROUND STRUCTURE OF THE FORWARD BAGGAGE BAY DOOR. (C-CHECK RO 11-24-21) REMOVED AND REPLACED MACHINED BRACKET IN FORWARD BAGGAGE BAY AT FS535.00 STRINGER27L TSDR A6WA202111037950None · noneCRACK INDICATIONS (2 TOTAL) AT FS 621 AFT PRESSURE BULKHEAD. CRACKS AT THE FOLLOWING LOCATIONS: FS 621 WL 107-WL 110 AT BL 0 CRACK IS 3"LENGTH; FS 621 WL 112.5-WL 115.5 AT LBL 27.5 CRACK IS 3" LENGTH. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON SSDR A6WA202111017949Seat Track · corrodedSEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE. ALL WORK WITHIN LIMITS IAW CRJ200 ASDR A6WA202110197912Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS. ALL WORK WITHIN LIMITS WAS PESDR A6WA202110197913Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW SDR A6WA202110187911Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 10Ï¿½ Ï¿½ FS449.83 HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAW SDR A6WA202110187910Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 16Ï¿½ Ï¿½ FS409.00 + 112Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFSDR JJBA20210927024None · noneCRACK FOUND RH FRAME 25 AT JOINTING OF FLOOR STRUCTURE (RH SILL #1) IN CF2. DAMAGE SECTION OF RH FRAME 25 CUT BTW STR 16R-17R SPLICED U-SHAPE FABRICATED. RH FRAME 25 BTW 15R-17R IN CF II REPAIRED.SDR FDEA202109272425None · noneLMLG W/W SUB STRUCTURE IS CRACKED AT THE FASTENER HOLE, APPROX STA 1147 LBL 70 WL 200 REMOVED, FABRICATED, LOCATED AND DRILLED NEW SUPPORT ANGLE IAW B757-200 DWG 149N7222 REV AC, INSTALLED IAW B757-200 DWG 149N7222 REV HSDR SWIA202162757None · corroded* GALLEY SERVICE DOOR FWD FLOOR SUPPORT FITTING ATTACHED TO FS 319.70 FRAME CORRODED. (C-CHECK RO 11-24-21) BLENDED OUT CORROSION FROM GALLEY SERVICE DOOR FWD. FLOOR SUPPORT FITTING ATTACHED TO FS 319.70 FRAME. REF: CRJ-700 SRM 51-21-06-001-001-A01. FOUND SDR JJBA20210926002None · noneAFT FUSELAGE, UNDER TOILET AREA, RH GUSSET BEAMS, FROM FR 61 TO 59, BOTH HAT BEAMS HAS SIGNS OF CORROSION AT BOLT HOLES 4 EACH. BLENDED OUT CORROSION AND EVALUATED AT RH GUSSET FROM FR 59 - FR 60 FOUND TO BE OUT OF LIMITS. REMOVE DAMAGE GUSSET, LOCATE AND DRILSDR MASA20211004460Plate · noneSACRIFICIAL PLATE OF THE LAVATORY WASTE SERVICING SURROUND STRUCTURE WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23, FIGURE 53-51-23-991-802, ITEM 6, EA 81-2021-075.SDR WX0A2021092773843Unknown · vibration(EMERGENCY DECLARED) RHYTHMIC VIBRATION FELT THROUGHOUT AIRFRAME DURING CLIMB WITHOUT CONFIGURATION CHANGES. F/CTL PAGE DISPLAYED ALL SURFACES STOWED. LAND LIGHTS RETRACTED. AUTO PILOT WAS ON. FLIGHT ATTENDANTS REPORTED STRANGER VIBRATION ON THE AFT SECTION. VSDR TAMF20210927015None · noneDURING AIRCRAFT LOADING PROCEDURE THE AFT CARGO COMPT DOOR CUT-OUT WAS FOUND WITH A SCRATCH BETWEEN STGR 42RH AND STGR 42A RH ON FR 65. //////// ACTION TAKEN: IN ACCORDANCE WITH AIRBUS A330-200F SRM TASK 53-41-11-283-006 FIGURE 002 (SHEET 1) THE DAMAGE WAS EVASDR EE4Y2021092513904Fitting · crackedPER CUSTOMER INSPECTION TASK, IT WAS FOUND ON LH AND RH WINDSHIELD SIDE POST UPPER ATTACHMENT FITTING - 2 EA HOLES WITH CRACK INDICATION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.SDR SWIA202162755None · corroded*AFT BAGGAGE-BAY DOOR SILL ANGLE / FLOOR SUPPORT IS CORRODED. (C-CHECK RO 11-24-21) REMOVED AND REPLACED AFT CARGO DOOR SILL PER DWG# MM670-35085 REV.L, REF CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42SDR R61A2021102000816Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 CENTER SHEAR WEB BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-65928-001 IAW SRM 51-42-01. SEE AAR NRC # 4500970-1000-0052 FOR WORK PERFORMED. AC WAS RTS.SDR R61A2021102000815Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 RH SHEAR WEB BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-42-01, 51-43-03 SEE AAR NRC# 45000970-1000-0053 FOR WORK PERFORMED. AC WAS RTS.SDR SWIA202163049None · dentedADM 7321 - L/H FWD FUSELAGE 1.3" AFT OF FS235 AND 1" ABOVE STRINGER 21L HAS DENT WITH GOUGE DAMAGE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 12/07/2021) PERFORSDR EE4Y2021112614436Skin Panel · dentedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FORWARD FUSELAGE BETWEEN FR09 AND FR11, BETWEEN STRG-11L AND STRG-13L WITH DENT, THE DAMAGE
WAS REPAIRED INSTALLING REPAIR DOUBLER AS PER E.O. # COO-EO-2021-14069 R00 - WOA1K276 ÍTEM 21-4, ETD2021-190-034419 ANSDR A6WA202111017946None · gougedGOUGE FOUND ON FWD SIDE OF I/B FLANGE OF FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. GOUGE DIMENSIONS ARE: .200"L X .200" W X .032"D. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND OUT ON FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. BLEND DIMENSSDR JJBA20210924035None · noneCOCKPIT UPPER FRAME 10 CRACKED. REMOVED AND REPLACED COCKPIT UPPER FRAME 10 OVERHEAD PANEL.SDR JJBA20210924020None · noneCENTER FUSE I, UNDER FLOOR SKIN CORRODED BTW FRAME 17-19 AND STR 21R-21L. CENTER FUSE I, UNDER FLOOR SKIN BTW FRAME 17-18 AND STR 21R-21L BLENDED FOR INVESTIGATION. AFTER INVESTIGATION, CORROSION ON LOWER SKIN BTW FR 17-19 AND BTW STR 21L-21R FOUND OUT OF LIMISDR JJBA20210924015None · noneAT FF, COCKPIT AT STA X3010 CENTER UPPER WEB HANDLE FOUND CRACK 2 PLACE AROUND ANCHOR NUT. PERFORMED CUTOUTS IN COCKPIT AT STA X3010 CENTER UPPER WEB AT HANDLE LOCATION. FABRICATED REPAIR DOUBLERS IN COCKPIT AT STA X3010 CENTER UPPER WEB AT HANDLE LOCATION. ATSDR JJBA20210924010None · noneM/D CABIN RH SIDE, AT FRAME 53 - 34 FR SIGNS OF CORROSION ALONG FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON MID CABIN RH SIDE FR 56-41 AND FR 48-52. PERFORMED UTT BY NDT OF BLENDED AREA ON FR 41-48 MID RH CABIN FOUND TO BE WITHIN LIMITSSDR DALA2021092805841None · noneSHIP 649 CORROSION ON UPPER SURFACE OF LOWER SILL FROM STA 1380 TO 1440 AT AFT CARGO COMPARTMENT.(CCT). CORRECTIVE ACTION: SUMMARY OF NRC 00361: THE LOWER SILL FROM STA 1380 TO 1440 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (1960557)SDR 2A6D2021092409002Deck Plate · chafedDENT AND CHAFING WAS DISCOVERED ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE DENT WAS MEASURED TO BE 0.20” X 0.10” AND 0.040” DEEP, AND THE CHAFE WAS MEASURED TO BE 1.0” X 0.40” AND 0.005” DEEPSDR SWIA202162713None · corroded*CORROSION ON ATTACHING ANGLE AT FS 319.00/STGR23R (C-CHECK RO 11-20-2021) REMOVED AND REPLACED ANGLE P/N SH670-35625-1 ON FS319 AND STRINGER 23R REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-31950 REV Y. COMPLIED WITH ST 51-900-1002-SKYSDR HNAA2021101800519None · noneSTRINGER 17R CORRODED BETWEEN FRAMES 19A - 20 AND FRAMES 22- 22A .... REMOVED, PREPPED, AND INSTALLED STRINGER 17R REPAIR SECTION, STRINGER SPLICE, AND JSHAPE IAW EMB 145 SRM 53-00-03 ITEM 7. 51-40-02 AND EO1-53-21-0282SDR HNAA2021101800518None · corrodedCORROSION ON RH LAV-TO-CARGO BULKHEAD SUPPORT (BANANA PANEL) LOWER END AT FRAME 61 .... REMOVED CORROSION ON LOWER END OF RH LAV-TO-CARGO BULKHEAD SUPPORT (BANANA PANEL) AT FRAME 61 IAW EMB145 SRM 51-10-03. FOUND CORROSION ON RH LAV-TO-CARGO BULKHEAD SUPPORT (SDR HNAA2021101800517None · noneSERVICE DOOR CUTOUT FR 22 CORRODED UNDERNEATH LOWER AFT SERVICE DOOR STOP .... INSTALLED FR-22 BETWEEN STGR 8R-17R, AND DOUBLER REPAIR PARTS IAW ETD2021-145-031861 AND PIEDMONT EO1-53-21-0278SDR MASA20211008475None · noneLOWER FUSELAGE SKIN BETWEEN FS485.00 - FS501.00 & STGR26R - STGR26L WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1C, EA 72-2021-169.SDR JJBA20210923022None · noneINSPECT FOR AND TREAT AS NEEDED ANY CORROSION UNDER THE REAR FUSELAGE II NAMEPLATES. ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 RIB DAMAGED. SPLICE REPAIR ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 REPAIRED. AT FR 78 NAMEPLATES REMOVED FOR INVESTIGATSDR JJBA20210923014None · noneCENTER FUSE IV, UNDER FLOOR, SHEAR CLIP FRAME 60 BTW STR 18R-20R CORRODED. CENTER FUSE IV, UNDERFLOOR, SHEAR CLIP FRAME 60 BTW 18R-20R OUT OF LIMITS. CENTER FUSE IV, POST FR60 REMOVED FOR ACCESS AND SHEAR CLIP FR 60 STR 18R-20R REMOVED FOR REPLACEMENT. CENTER SDR JJBA20210923006None · noneHAT BEAM RH AFT OF FR 59 FOUND TO HAVE CORRODED AREA AT NUT PLATE AREA. CUTOUT DAMAGE AREA. FABRICATED REPAIR DOUBLER. APPLIED ALODINE, PRIMER, TOP COAT AND INSTALLED REPAIR DOUBLER. CORROSION LEVEL 2SDR HNAA2021100600491None · noneE879831 - RH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN). .... REPAIRED RH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE IAW SB 145-54-0008 AND EO1-54-21-0258. SEE WIPS AND TASKS FOR DETAILS.SDR HNAA2021100600490None · noneE881864 - FOUND ADDITIONAL CORROSION ON L/H #1 CABIN FLOOR SILL (MARKED. .... RAR L/H #1 CABIN FLOOR SILL IAW EMB145 SRM 51-40-02.SDR JJBA20210922008None · noneCF2, RH SIDE, FR25 AT FLOOR LEVEL BEHIND SILL, FRAME FOUND CRACKED. FRAME SPLICED.SDR CALA2021092401656Stiffener · crackedAD 2017-17-16 - EA 5310-07143 REV D ,RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 1" IN LENGTH. PLS PRINT AND ACCOMPLISH REPAIR PER OP004 TRANSFER REF. NON-ROUTINE LP 9130574 AND ORIGINATED BY SDR CALA2021092401655Stiffener · crackedAD2017-17-16 - EA5310-07143 REV D - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 OT 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 1" IN LENGTH. PLS PRINT AND ACCOMPLISHED REPAIR PER OP003 TRANSFER REF. NON-ROUTINE LP 9130578 AND ORIGINATED BY
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