JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 ASAA2021113036898Floorbeam · corrodedFWD WET AREA STA 328 HAS CORROSION AT RBL 46. GROUNDED - YES. REPAIRED OUT OF LIMITS CORROSION AT STA 328 RBL 46 IAW EA# 800-53EA-24051 & B737-800 SRM 53-10-51-2R-8.W= 1.75" O= .0125" R= .105" L= 2.25" D= .020".SDR VNAA2021113099914Hinge Fitting · gougedFOUND SCRATCHING/GOUGING DAMAGE INSIDE L/H WING FUEL TANK AT WS 264.00 AROUND THE BOLT HOLES FOR THE FLAP FORWARD HINGE SUPPORT FITTING ASSEMBLY.SDR VNAA2021113099913Stringer · corrodedSTGR 21R AND CONNECTOR MOUNTING PLATE BETWEEN FS 349 AND FS 364 ARE CORRODED.SDR VNAA2021113099912Stringer · corrodedSTINGER 20R CORRODED BETWEEN FS 379 AND FS 394.SDR VNAA2021113099911Stringer · corrodedSTRINGER 19R CORRODED BETWEEN FS 394 AND FS 409.SDR VNAA202111309997Angle · bentFS280.00 BULKHEAD RH AFT FACE 2ND, 4TH, 5TH, AND 7TH FROM TOP REINFORCEMENT ANGLES BENT.SDR VNAA202111309996Angle · bentFS280.00 BULKHEAD LH AFT FACE TOP, 5TH AND 6TH FROM TOP, AND BOTTOM REINFORCEMENT ANGLES BENT.SDR VNAA202111309994Stringer · corrodedSTRINGER 20R CORRODED BETWEEN FS 421 AND FS 453.SDR VNAA202111309993Stringer · corrodedCORROSION AT FS 549.00 FROM STGR 26L TO STGR 26R (FRAME)SDR VNAA202111309992Door Sill · corrodedR/H FLOOR SILL UPPER SURFACE RBL 45.0 FS 287.00 HAS AREA OF MINOR CORROSION.SDR V0XD202112030003None · corrodedR/H FLOOR SEAT TRACK FROM F.S. 708 TO 830 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SEAT TRACK FROM F.S. 708-830 (PN: BA690-30000-6959A) IAW CRJ 900 SRM 51-21-06, 51-40-00, 51-40-11 CRJ 900 AMM 53-00-49, 51-21-01.SDR V0XD202112030002None · corrodedR/H FLOOR SEAT TRACK FROM F.S. 708 TO 830 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SEAT TRACK FROM F.S. 708-830 (PN: BA690-30000-597A) IAW CRJ 900 SRM 51-21-06, 51-40-00, 51-40-11 CRJ 900 AMM 53-00-49, 51-21-01.SDR FDEA202111302953Stringer Splice · corrodedAFT CARGO , STRINGER SPLICE CORRODED AT STA 1620 LBL28 REMOVED CORROSION ON STRINGER SPLICE IAW B757-200 SRM 53-00-03-1A . ORIGINAL MAT. THICKNESS IS .100 , MAT. REMOVED .004 , REMAINING THICKNESS IS .096 . IN LIMITS IAW B757-200 SRM 53-00-53 DETAIL I FIG SDR AALA202112229164None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.SDR ASAA2021112936926None · corrodedAFT CARGO DOOR SILL WEB HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED & REPLACED AFT CARGO DOOR SILL WEB IAW B737-800 SRM 51-40-02-0G-0W- 1" O- .050" R- .043" L- 36" D- .007".SDR ASAA2021112936925Scuff Plate · crackedAFT CARGO DOOR CUT-OUT, AFT SCUFF PLATE THRESHOLD IS CRACKED. GROUNDED - YES. LOCATED AND DRILLED NEW THRESHOLD SCUFF PLATE IAW B737-800 SRM 51-40-05-0G-0 TO BE INSTALLED ON W/O 1019736/1000/0124 S/N 8294525 C/N RS-2-GRP-25 (050).SDR FDEA202111293083None · corrodedAFT CARGO - STA 1902 R/H SIDE - SIDEWALL PANEL VERTICAL STANCHION HAS CORROSION ON LOWER SECTION I/B SIDE (MARKED) REMOVED AND REPLACE SIDE WALL PANEL VERTICAL STANCHION AT STA 1902 REF SRM 51-31- 01-OGSDR NACA2021112900001None · noneSUPPLEMENTAL INFORMATION: REMOVED CORROSION AT STA 654 BETWEEN S-15L & S-16L, AND STA 785 BETWEEN S-14L AND 2-16L AND TREATED IAW AMM 51-21-03, 51-21-04 AND AMM 51-24-21SDR AALA202112034630Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT UPPER DOOR STOP FITTING #6 OUTBOARD HOLE HAS CRACK INDICATION AT FR 68. REPLACED DOOR STOP FITTING PER EO 5317Y201.SDR CALA2021120102199Angle · noneTRANSCRIBED FROM HAECO GSO NRC# 9287273: SUPPORT TASK- MAIN CABI N STA 295-430 LBL65 CREASE BEAM ANGLE HAS ELONGATED AND OVERSIZE D ATTACHMENT HOLES.SDR CALA2021120102198Web · noneTRANSCRIBED FROM HAECO GSO NRC# 9287537: SUPPORT TASK- THE CREAS E WEB BETWEEN STA 395 AND 410 LBL65 HAS ELONGATED AND OVERSIZED HOLES. REMOVED AND REPLACED CREASE WEB FROM STA 395 TO STA 410 LBL-65 I AW B757-2 SRM 51-40-02 AND DWG 141N8322 REV F. REF HAECO GSDR R61A2021113000940Skin · dentedLH FOWARD FUSELAGE UNDER CAPTAINS WINDOW BETWEEN FRAMES 9 AND 10 AND STR 17L AND 18L DENTED. PERFORMED CUTOUT AND INSTALLED FILLER AND DOUBLER IAW ETD2021-170-040099-2021. REF VP-040252-2021 N/R #1. REF LP R864910 ITEM 1.SDR SWAA2022011148394Web · corrodedAFT CARGO DOOR CENTER THRESHOLD WEB HAS SEVERAL AREAS OF CORROSION ; / [01] INSTALLED NEW THRESHOLD PER SRM 51-40-02.SDR SWAA2022010454989Web · crackedCRACK WEB LOCATED BETWEEN BS 847 TO BS 867 LBL 24.75 AT AFT CARGO COMPARTMENT. REPAIRED WEB LOCATED BETWEEN BS 847 TO BS 867 LBL 18.92 & WL 202.6 AFT CARGO COMPARTMENT IAW EA 21-153-03680.SDR SWAA2021122748005Stub Frame · crackedCRACK FOUND ON FSD FWD UPPER COVE STRUCTURE BS 294.5+3', APPROX. WL 265. REMOVED ON FSD FWD UPPER COVE STRUCTURE IAW SRM 51-40-02. EVALUATED CRACK AT FSD FWD UPPER COVE STUB FRAME AND FOUND OUT LIMITS IAW SRM 53-10-15-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 ANDSDR SWAA2022010348085Web · crackedSUPPLEMENTAL INFORMATION: CRACK WEB LOCATED BTW BS 328 TO BS 344 AT LBL 45 AT FWD GALLEY AREA ; 2021-544508 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 11228551 DUE DATE: 25/SEP/22.; [02] REPLACED NEW WEB LOCATED BTW BS 328 TO BS 344 AT LBL 45 AT FWD GALLEY ASDR SWAA2022010348084Web · crackedSUPPLEMENTAL INFORMATION: CRACK WEB LOCATED BTW BS 312 TO BS 328 ON RBL 30 AT FWD GALLEY AREA ; 2021-544507 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 11228551 DUE DATE: 25/SEP/22.; [02] REPLACED NEW WEB LOCATED BTW BS312 TO BS328 ON RBL 30 AT FWD GALLEY ARESDR SWAA2022010347700Web · crackedSUPPLEMENTAL INFORMATION: CRACK WEB LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA ; 2021-544338 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A18234369 DUE DATE: 29-SEP-22; [02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES0000SDR SWAA2022010447727Structure · crackedCRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR17L LH SIDE AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BS303.9 AT LEVEL STR17L LH SIDE AT FWD GALLEY AREA IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A8110 SHEET 9, REV A . REPLACED INNER CHORD LOCATED BS 2SDR AALA202112019599Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND PRESSURE DECK SKIN AT BS 663 BETWEEN LBL 31.83 AND LBL 40. REPAIRED PRESSURE DECK PER SRM 57-10-10-2R-3.SDR FDEA202111243052Shear Tie · corrodedAFT CARGO - R/H SIDE - SHEAR TIE HAS CORROSION AT STA 1902 BETWEEN LONGERON 42 & 43 REMOVED, FABRICATED AND INSTALLED SHEAR TIE (P/N: AGA7009-7) AT STA 1902 BTWN L-42 AND L-43 RHS REF, DOUGLAS DWG AGA7009 AND MD11 SRM 51-31-01-0G.SDR SWAA2021121346771Web · crackedSUPPLEMENTAL INFORMATION: CRACK WEB LOC. BTW BS 927 TO BS 947 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT ; 2021-526047 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000SDR CALA2021112302161Fitting · crackedROTO PROBE OF LH FR16 #7 DOOR STOP FITTING FOUND THAT THE TOP I/ B AND BOTTOM I/B HOLES HAVE CRACK INDICATIONS. REPAIR BEFORE NEX T FLIGHT REPLACED INTERCOSTAL FITTING IAW SRM 51-72-11-911-001 AND SRM 51 -42-11/001. P/N D5311423620091 B/N: 0003867876. EMP: V93SDR SIMA20211121003None · noneL/H CENTER FLOOR BEAM CORRODED FR-16 MARKED-C/A-INSTALLED REPAIR DOUBLER/FILLER ON L/H CENTER FLOOR BEAM FR-16 IAW EMB 175 SRM 53-10-10 RE 01, FIGURE 202SDR SIMA20211121004None · noneR/H FLOOR DOUBLER CORRODED BETWEEN FR-12 AND FR-13 AND BETWEEN FR-13 AND FR-14 MARKED-C/A-REMOVED CORRODED AND INSTALLED SERVICEABLE R/H FLOOR DOUBLER BETWEEN FR-12 AND FR-14 IAW EMB 175 SRM 51-40-08 (SEE WIPS AND TASK PERFORMED FOR FURTHER DETAILS)SDR R61A2021120800988Shear Tie · corrodedCORROSION FOUND ON FWD FUSELAGE FRAME SHEAR TIE CLIP AT FR17, BETWEEN STGR 27R AND 28R. REPLACED IAW SRM 51-41-01 AND 51-41-02SDR CALA2021112202148Door Sill · noneL2 DOOR SILL HAS LIGHT SURFACE. PER HAECO LCQ NR 9292357/20357 G ENERATED BY V892442. CUT OUT CORRODED NUT PLATE HOLE AT FR66 DOOR SILL FLANGE, CUT A FILLER FOR REPAIR PRINCIPLE 6 AND ISNTALLED IAW A319 SRM 53-41-1 4-283-002, SRM 53-41-300-001. PERFORMED BY V9SDR CALA2021112202146Fitting · corrodedFR 68 RH LOWEST HOLE JUST ABOVE DOOR SILL PLATE IS CORRODED. PER HAECO LCQ NR 9292399/20399 GENERATED BY V892442 -1.1"SHIM AND FILLER INSTALLED. SRI 53-41-12-205-003 TABLE 1 REQ UIRES A DETAILED INSPECTION FROM FIRST FLIGHT 24,000FC (FH NOT R ELEVANT. SUBSEQUESDR SWAA2021121445939Angle · crackedA-061 DOT 003 AFT CARGO PIT WASTE TANK ENCLOSURE VERTICAL BEAM AT STA 847+18' LBL 10 LOWER ATTACH ANGLE CRACKED ; / [01] REMOVED CRACKED CLIP IAW SRM 51-40-02.; [02] LOCATED/DRILLED NEW CLIP; 149A8109U114; IAW SRM 51-40-05. A TAG # A94253.; [03] OK TO INSTALL SDR FDEA202111192904Frame · gougedEMPENNAGE INTERIOR BELOW CENTER SECTION BILGE AREA FRAME HAS A GOUGE AT BS 1844 RBL 5 REPAIRED PER B757 SRM 51-70-11-OGSDR VNAA202111199997Frame · corrodedF 310 CONTAINS CORROSION ON FRAME BETWEEN STR 25 L TO STR 25 RSDR WX0A1900010073970None · noneNRC 2000-0048: 031-9 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT LH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE, LOWER MAIN SILL AREA BTW FRAME 66-68, LH THRESHOLD BEAM PERMANENTLY REPAIRED AS PER SRSDR WX0A1900010073965None · noneNRC 2000-0049: 031-11 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT RH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE LOWER MAIN SILL AREA BTW FRAME 66-68, PERMANENTLY REPAIRED PERFORMED AT THRESHOLD BEASDR SWAA2021122245793Scuff Plate · corrodedL-2 DOOR INNER WEB STRUCTURE UNDER SCUFF PLATE CORRODED. REMOVED CORROSION UNDER SCUFF PLATE. FOUND OUT OF LIMITS IAW SRM 51-010-02-0G-0. REMOVED STRUCTURE UNDER SCUFF PLATE IAW SRM 51-40-02-0G-0. WEB STRUCTURE UNDER SCUFF PLATE INSTALLED WEB, INSTALLEDSDR SWAA2021120745739Web · crackedAFT CARGO DOOR CUTOUT FWD CLOSE OUT WEB PANEL#142KW HAVE MULTIPLE CRACKS. ; / [01] NO ALLOWABLE DAMAGE FOUND ON SRM; PART REQUIRED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR.9.C.; [02] VERIFIED PART CAN BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-SDR AALA202111298265None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF CREASE ANGLE BETWEEN STA 951 AND STA 997 AT STR 17R AND RBL 64, MEASURING L=3.0 IN, W=6.0 IN, D=0.08 IN. REPLACED CREASE ANGLE WITH NEW IAW SRM 51-40-02.SDR K11A2021111900095Beam · corrodedL/H WALKWAY BEAM AREA HAS CORROSIONSDR FDEA202111172873Beam · crackedLOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 FLOOR BEAM FOUND WITH CRACK. LOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 CRACKED FLOOR BEAM REPAIRED AS PER EA#1-5321-T0365615 PART 1. TITLE: FUSELAGE - CARGO COMP FLOORS - LOWER CENTER CARGO FLOOR BEAMSDR FDEA202111172870Beam · noneAGING AIRCRAFT - EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM . EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-00-2R FIGURE 203. EXISTISDR AALA202111297584Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR PANEL SUPPORT ANGLE AT STA 500H+21 BETWEEN LBL 24 AND RBL 24, MEASURING L=24.0 IN, W=2.0 IN, D=0.015 IN. REPLACED SUPPORT ANGLE WITH NEW IAW SRM 51-40-02.
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