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 R61A2025082000356Seal Rest · corrodedAFT SERVICE DOOR (R2) CUTOUT LOWER BEAM UPPER SURFACE SEAL REST FOUND CORRODED. MX REPLACED SUPPORT IAW SRM 51-41-01.SDR DALA2025080705924Door Frame · corrodedEVIDENCE OF CORROSION AT FWD R/H EMERGENCY EXIT CUT-OUT. COMPLIED WITH ER/A 628114-14 REV ORIGINAL SECTION 1 TEMPORARY REPAIR.SDR FDEA202508011354Access Panel · puncturedFLOOR ACCESS PANEL 242 VFF WITH SEVERAL PUNCTURE ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 242 VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 2 REV. 92 APR 15,2025SDR SWIA2025073175149Door Sill · corrodedAFT BAGGAGE DOOR SILL CORRODED AS MARKED (C-CHECK RO 02/01/2026)AFT BAGGAGE DOOR SILL. P/N MM670-35655-003, NO DAMAGE IS ALLOWED ON THE SURROUND STRUCTURE OF THE AFT BAGGAGE BAY DOOR. IAW. CRJ900 SRM 53-61-23-101-001-A01REMOVED AND REPLACED AFT BAGGAGE DOOR SSDR AALA202512014262Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLIGHT DECK WINDSHIELD LEFT HAND LATERAL FRAME BETWEEN FR 4 AND FR 8. REPAIRED WINDSHIELD FRAME PER EA 366681.SDR SWIA202509250731Channel · crackedCRACK FOUND IN WEB CHANNEL OF COPILOT'S SIDE WINDOW FRAME SUPPORT STRUCTURE CAMP#30584259 (C-CHECK RO 09/24/2025)REMOVED AND INSTALLED CLIP ATTACHED TO WEB CHANNEL AT LOWER SECTION REF. CRJ200 SRM 51-42-06 AND DWG 601R34032 REV. -V. AND COMPLIED WITH TASK CARSDR VNAA202509250015Door Frame · wornWEAR ON SURROUND OF HANDLE OF AFT COMPARTMENT DOOR. WEAR ON SURROUND OF HANDLE OF AFT COMPARTMENT DOOR WAS REPAIRED PER REO 670-52-31-031 REV BSDR AALA202508189668Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR ENTRY WAY LOWER SILL INNER CHORD (CREASE ANGLE) LOCATED AT BS 980, LBL 47. REPLACED CHORD PER AARD 51-00-05-1.SDR IPXA2025081524093Pressure Panel · corrodedMAIN CABIN AT CENTER WING L/H TUNNEL AT THE PRESSURE PANEL HAS CORROSION. VERIFIED STEP 7 C/W IAW UPS RII GMM 04-02.SDR CALA2025080807489Structure · corrodedAFT WET AREA. EXFOLIATION CORROSION ON SEVERAL SPOTS OF RT INNER CHORD BETWEEN BS 947.5 -1006. REMOVED AND REPLACED INNER CHORD AT RT AFT WET AREA BETWEEN STA 890 TO STA 1006 PER SRM 51-40-02-0G-0, 51-40-03-0G-0 AND DWGS 147A8501, 147A0004.SDR CALA2025080407235Stub Beam · damagedSTA 616 LH STUB BEAM HAS AN ELONGATED HOLE. REPAIRED BS616 L/H STUB BEAM AS REQ IAW REO-G25531 REV IR AND ECRA NO. 5311-03385 REV-.SDR AALA202510084915Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 366931.SDR AALA202509265046Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK INDICATION FOUND ON WINDSHIELD FRAME LOWER ATTACHMENT AREA INTERNAL SIDE. LOCATED ON LOWER RADIUS LH SIDE IN COCKPIT. CRACK LENGTH=0.400 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR, REPAIR ON CENTER POST LT AND RT SIDE SDR 9WGA2025092454671Panel · corrodedCENTER WING UPPER PANELCORRODED AT RH APPROX STA 1219, XCW 16.0, S-16. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WING UPPER PANEL RH APPROX STA 1219, XCSDR 9WGA2025092454670Panel · corrodedDURING HEAVY MAINTNENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. STA 1204, XCW 2SDR AALA202509237127Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING RADIUS AREA. LOCATED ON WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE. IN COCKPIT. CRACK LENGTH= 0.250 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR REPLACED CONTINUITY FITTING SDR 9WGA2025090954652Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RT APPROX. STA. 1219, XCW 16.0 S-16. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WINGSDR 9WGA2025090954651Panel · corrodedDDURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. SSDR CALA2025082808244Pressure Deck · crackedVERTICAL PRESSURE DECK WEB OF THE WING CENTER SECTION REAR SPAR HAS TWO CRACK SIGNAL INDICATION, AT RBL 25.00, AND RBL 40. REPAIRED VERTICAL PRESSURE DECK WEB AT WING CENTER SECTION RBL 25.00 AND RBL 40.00 IAW SRM 57-10-10-2R-3 ALTERNATIVE REPAIR 3. THIS IS SDR AALA202508110058Stop Fitting · undertorquedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND AFT EMERGENCY ESCAPE DOOR CUT OUT, UPPER AFT DOOR STOP LOOSE (ROTATES BY HAND). RETIGHTENED RIGHT HAND AFT EMERGENCY ESCAPE DOOR CUT OUT, UPPER AFT DOOR STOP. PER B737 NG SRM 51-40-02.SDR AALA202508119850Stop Fitting · undertorquedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT EMERGENCY ESCAPE DOOR CUT OUT, UPPER AFT STOP LOOSE (ROTATES BY HAND). RETIGHTENED LEFT HAND AFT EMERGENCY ESCAPE DOOR CUT OUT, UPPER AFT STOP. PER B737NG SRM 51-40-02.SDR AALA202508054391Stop Fitting · out of positionAIRCRAFT IN BASE MAINTENANCE: LEFT HAND OVERWING EXIT HATCH, FORWARD LOWER DOOR STOP IS CROOKED. MAINTENANCE POSITIONED LOWER DOOR STOP IN PROPER POSITION PER AMM 52-22-01.SDR CALA2025080107212Window Frame · crackedL3 WINDOW FRAME E-F POST REPAIRED PER ECRA 5310-08654. PERFORM AN INSPECTION OF LT WINDOW FRAME E-F POST REPAIR ON AIRCRAFT IAW PART 2 OF THE LATEST REVISION OF ECRA 5310-08654. MAJOR REPAIR. ACCOMPLISHED ESFR AND PERMANENT REPAIR COMPLIED WITH.SDR DALA2025073105751Fitting · damagedDAMAGE ON FITTING OB SIDE - FORWARD SIDE OF 62 STRINGER 3L. REMOVED AND REPLACED BRACKET PER ERA 627461-14 REV A.SDR CALA2025073107146Window Frame · damagedREPAIR THE RH #3 WINDOW FRAME E-F POST REF TO ECRA 5611-01314 R EV C PART 3. REPAIRED PER ECRA 5310-08655 REPAIR THE R3 WINDOW FRAME E-F POST REF TO ECRA 5611-01314 R EV C PART 3.SDR IXXA20250730002Skin · crackedCRACK INDICATION IN THE 2ND HOLE FROM THE BOTTOM AT FORWARD SERVICE DOOR LOWER AFT CORNER, SKIN LAYERSDR JJBA20251024072Door Frame · corrodedZONE 132, 232, AND 234 FOUND CORROSION AT THE RH SILL SERVICE DOOR AT FRAMES 20 AND 22. REMOVED AND REPLACED RH SILL SERVICE DOOR LOWER FRAME BETWEEN FRAME 20 AND 22.SDR 9WGA2025090954650Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 96.0 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WINSDR 9WGA2025090954649Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1233, XCW 76.5 AT S-14. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1233, XCW 76.5 AT S-14, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR ISDR 9WGA2025090954648Panel · corrodedDURING HEAVY MAINTENENACE CHECK CENTER WING UPPER PANEL CORRDODED AT LH APPROX STA 1205, XCW 7.0 S-18. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1205, XCW 7.0AT S-18, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MSDR CALA2025081307687Door Sill · corrodedAFTER FURTHER EVALUATION FOUND L1 DOOR LOWER MAIN SILL INNER CHORD OUT OF LIMITS - REQUIRE REPLACEMENT (REF: AAR NR 1000045910) L-1 DOOR LOWER MAIN SILL INNER CHORD REPLACED IN RFD DURING D CHECK. REMOVED AND REPLACED INNER CHORD LOCATED AT L1 DOOR LOWER MAIN SDR ASAA2025072960011Door Frame · damagedAFT WEB OF E&E BAY DOOR SURROUND STRUCTURE HAS DAMAGED FASTENER HOLES AND 1 EA DENT. GROUNDED - YES. REPAIRED PER EA M9-53EA-29111 REVISION 03.SDR REXA2025080600795Housing · crackedCRACK ON AFT LATCH HOUSING CUTOUT FS188.00 OF ACCESS DOOR 212AR AFT LATCH HOUSING CUTOUT FS188.00 OF ACCESS DOOR 212AR WAS FABRICATED PER EA CRJ953-19660 REV. IR AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01SDR CALA2025073107136Door Sill · corrodedAFT CARGO DOOR BOTTOM CUTOUT HAS CORROSION SPOTS ON DOOR SILL UP PER SURFACE. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW A320 DWN E534705000 08 AND SRM 51-72-11-911.SDR JJBA20250730110Door Sill · corrodedZONE 132, 232, AND 234 FOUND CORROSION AT THE RH SILL SERVICE DOOR AT FRAMES #20 AND #22 (LOWER BEAM AND SCREW HOLES UNDER FLOOR BOARD). REMOVED AND REPLACED RH SILL SERVICE DOOR LOWER FRAME BETWEEN FR20 AND 22.SDR DALA2025072905701Door Sill · corrodedAIRCRAFT AFT SERVICE DOOR SILL, BOLT HOLE #4 HAS CORROSION EMITTING FROM IT. (P)(M). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0546:5360-2024/002 00539 REMOVED AND REPLACED FORWARD CORNER STRIKER REF A220 ASRP 52-42-21. (LP# 1112326)SDR DALA2025072905693Angle · damagedSHIP 3416 TOOLING DAMAGE ON CLIP LH FR62. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-11. (1112353)SDR DALA2025072905692Angle · damagedSHIP 3416 TOOLING DAMAGE ON CLIP FR62 RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-11. (1112350)SDR SWIA2025F01374Panel · corrodedLANDING FOR PANEL 312DZ HAS POSSIBLE CORROSION WHERE THE PAINT IS REMOVED. (S/N#00521) (C-CHECK RO 09/24/2025)BLENDED OUT CORROSION LANDING FOR PANEL 312DZ AND RESTORED FINISH. FOUND WITHIN LIMITS. REF. REO 601R-53-61-8370 REV.-- ISSUED 2025-08-18.COMPLIED WISDR SWIA2025F01371Door Frame · chafedPAX DOOR SURROUND AFT LOWER STOP PIN FITTING HAS EVIDENCE OF CHAFFING. (S/N#00519) (C-CHECK RO 09/24/2025)BLENDED OUT CHAFE ON PAX DOOR SURROUND AFT LOWER STOP FITTING REF. CRJ-200 SRM 51-12-00. COMPLIED WITH STEPS 1-4 OF REO 601R-53-21-3764 REV -- DATE: 202SDR SWIA202509250728Door Frame · chafedPAX DOOR SURROUND FWD LOWER STOP PIN FITTING HAS EVIDENCE OF CHAFFING. (S/N#00518) (C-CHECK RO 09/24/2025)BLENDED OUT CHAFE ON PAX DOOR SURROUND FWD LOWER STOP FITTING REF CRJ-200 SRM 51-12-00 REV 39 MAR 10/21, COMPLIED WITH STEPS 1-4 OF REO 601R-53-21-3764 RSDR IPXA2025081416434Retainer Seal · crackedFWD CREW DOOR SCUFF PLATE RETAINER WITH CRACK.REMOVED AND REPLACED RETAINER SEAL P/N A5361155631802 B/N 0004417335, INSTALLED USING EXISTING FASTENERS IAW A300-600 SRM 51-40-21. NO FURTHER ACTION REQUIREDSDR CALA2025073107141Seal · missingUPON REMOVAL OF PANEL 191DT FOUND BOTTOM SEAL MISSING, WILL BE REPLACING BOTTOM SEAL WHEN PANEL GETS REPLACED.SDR NACA20250728001Plug · corroded#4 WINDOW PLUG OF MCD HAS LARGE PIECE OF EXFOLIATED MATERIAL FALLING OFF AT ITS FORWARD LOWER CORNER. REMOVED AND REPLACED #4 WINDOW PLUG IN MCD PER ANCRA INTL WINDOW PLUG INSTALLATION KIT DWG 86734 REV KSDR JJBA20250728102Rack · crackedREAR FUSELAGE I AVIONIC COMPARTMENT, AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK CRACKED. REAR FUSE I AVIONIC COMPARTMENT AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK REMOVED AND REPLACEDSDR AALA202509298757Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON RH SIDE WINDSHIELD CENTER POST (AROUND UPPER BOLT) . CRACK LENGTH 0.080 INCHES. CRACK DIRECTION 11 OCLOCK. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON RH SIDE WINDSHIELD CENTER POST IAW EA 3667SDR AALA202509295633Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON RH SIDE CONTINUITY FITTING. CRACK LENGTH 0.200 INC HES. CRACK DIRECTION VERTICAL REPLACE LH SIDE PER EA 366758. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON CONTINUITY FITTING LH IAW EA 366758.SDR AALA202509299056Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON RH SIDE CONTINUITY FITTING CRACK LENGTH 0.200 INCHES, CRACK DIRECTION VERTICAL. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTION ON CONTINUITY FITTING RH IAW EA 366758.SDR AALA202509290811Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LH SIDE WINDSHIELD CENTER POST (AROUND UPPER BOLT) . CRACK LENGTH 0.100 INCHES. CRACK DIRECTION 1 OCLOCK. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON LH SIDE WINDSHIELD CENTER POST IAW EA 3667SDR CALA2025081407753Window Frame · crackedRIGHT NR 3 WINDOW FRAME WITH CRACKED FASTENER HOLE (3RD FROM BOTTOM). REPAIRED R3 WINDOW FRAME IAW ESR-WI NO:2023573-13-12408 REV.IR & EC/RA 5310-08660 REV.ORIGINAL,INTERIM REPAIR.
Back to JASC 5310