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 IPXA2025012994882Door Frame · corrodedSEVERE CORROSION FOUND ON APU AIR INLET DOOR FRAME. INSTALLED NEW STRAP IAW B757-200, SRM 51-40-02. REVIEWEDSDR DALA2025012000452Window Post · crackedSHIP 3147 CRACK INDICATIONS WERE FOUND AT LHS (CENTER POST, LOWER RADIUS), RHS (CENTER POST, LOWER RADIUS AND LOWER NODE CONTINUITY FITTING), FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: COMPILED WITH ER/A 622155-14. (0769742)SDR DCGA2025081900557Canopy · crackedSERVERAL CRACKS FOUND IN FUSELAGE CANOPY ALONG THE INTERIOR LOWER FRAME FOR THE LEFT AND RIGH-HAND WINDOWS.SDR AALA202503268689Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 361440.SDR DALA2025012000448Fitting · crackedSHIP 3147 CRACK INDICATION FOUND ON CONTINUITY FITTING UPPER AREA RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 622156-14. (0769039)SDR JR2R20250119076Beam · corrodedLONG BEAM AT LBL 10 BETWEEN FRAMES 87 AND 88 IS CORRODED.SDR JR2R20250119072Shear Panel · corrodedRH SHEAR PANEL IS CORRODED.SDR JR2R20250119994Bonding Jumper · corrodedCENTER LOWER FUSELAGE, SKIN AND BONDING JUMPER CLIP CORRODED AFT OF FR31 STR27RSDR MAS2025F00000Bonding Jumper · corrodedCENTER LOWER FUSELAGE, SKIN AND BONDING JUMPER CLIP CORRODED AFT OF FR31 STR27RSDR JR2R20250119001Bonding Jumper · corrodedCENTER LOWER FUSELAGE SKIN AND BONDING JUMPER CLIP CORRODED AFRT OF FR 31, ON STR 27LSDR JR2R20250119078Gusset · corrodedTOP GUSSET AT FR90 LBL10 CORRODEDSDR JR2R20250119077Doubler · corrodedEXISITNG DOUBLER AT FRAME 87 ON LONG BEAM AT RBL 10 IS CORRODEDSDR SWI2025F00419Splice Strap · corrodedFS319 FRAME SPLICE STRAP (FWD SIDE OF THE SERVICE DOOR) IS CORRODED AT THE FLOOR LEVEL (C-CHECK RO 04/04/2025)BLENDED AND REMOVED CORROSION AT FS319 FRAME SPLICE STRAP (FWD OF SERVICE DOOR). FOUND TO BE ACCEPTABLE AT THIS TIME REF REO 670-53-21-2576 REV -- DASDR AALA202504040856Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 16 LEFT AND #7 DOOR STOP FITTING. REPAIRED FRAME PER EA 361714.SDR AALA202502034949Track · gougedAIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY SERVICE DOOR FUSELAGE CUTOUT AFT FRAME-MOUNTED LATCH TRACK FITTING HAS A GOUGE. REMOVED AND REPLACED, AND PERFORMED SATISFACTORY ADJUSTMENT ON FORWARED GALLEY SERVICE DOOR FUSELAGE CUTOUT AFT FRAME-MOUNTED LATCH TRASDR AALA202502034999Roller Track · gougedAIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY SERVICE DOOR FUSELAGE CUTOUT AFT FRAME-MOUNTED CENTER GUIDE ROLLER TRACK FITTING HAS A GOUGE AT LOWER EDGE. REMOVED AND RPLACED, AND PERFORMED SATISFACTORY ADJUSTMENT ON FORWARD GALLEY SERVICE DOOR FUSELAGE CUTOUT ASDR AALA202502038379Latch · gougedAIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY SERVICE DOOR FUSELAGE CUTOUT AFT FRAME-MOUNTED LOWER LATCH FITTING HAS A GOUGE. REMOVED AND REPLACED FORWARD GALLEY DOOR LOWER AFT LATCH FITTING. PER B737NG SRM 51-40-02-OG. AND PERFORMED SATISFACTORY ADJUSTMENT. PESDR DALA2025012100508Door Frame · crackedSHIP 3266 DISC: EXISTING REPAIR ON FR68 LH AT LEVEL DOOR STOP FITTING 1 ON OPEN HOLES H1= 0.280, H2= 0.280 , H3= 0.280 AND H4= 0.280 AA 5311-01216 AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT ENGINEERING EVALUATION REQUIRED, CONTACT LIAISON ENGINEERINGSDR DALA2025012100481Support Frame · corroded(LOG 0767345) CORROSION ON STA540 BULKHEAD FWD LOWER CORD, BILDGE AREA, RBL5-LBL5. ACCOMPLISHED REPAIR AT 540STA BULKHEAD FWD LOWER CHORD, BILGE AREA RBL5-LBL5 PER ER/A 623396-14 REV 0.SDR AALA202501197114Connector · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR CROSS BEAM SECTION CONNECTION AT FR 66 BETWEEN S23R AND S24R. REPLACED BEAM CROSS BEAM SECTION CONNECTION PER SRM 51-42-11.SDR DALA2025030401707Door Frame · corrodedSHIP 6707 FLC DOOR INTERNAL VERTICAL FRAME NO.4 IS CORRODED AT LOWER END. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW VERTICAL FRAME #4 ON FLC DOOR IAW B757 -200 SRM 51-40-02. (0766236)SDR SWAA2025021086866Pressure Deck · crackedCRACK IN LH HORIZONTAL PRESSURE DECK BS 672 WL 202 LBL35. CRACK IS .650 INCHES IN LENGTH. MARKED IN RED INK.<[01] REPAIRED LH HORIZONTAL PRESSURE DECK WEB AT BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REPAIR 2 FIG. 202.;[02] TASK CARD COMPLETED.;[SDR SWAA2025021086867Pressure Deck · crackedCRACK IN RH HORIZONTAL PRESSURE DECK BS 664.5 WL 202 RBL 43. CRACK IS .250 INCHES LONG AND MARKED IN RED INK.<[01] REMOVED THE DAMAGE PART OF THE WEB AT BS 663.75 - 6BS75; RBL38 - 60; WL 202; PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202.<BR><BR>INSTALLED REPAIR RSDR SWI2025F00072Structure · damagedDUE TO EXISTING PILOT HOLES THERE ARE TWO OVERSIZE HOLES COMMON TO THE LH PRESSURE BOX AND LBL18, MARKED. (FILED CLOSED) COMPLIED WITH ALL STEPS OF THIS REO 670-53-41-712 REV. - - DATED 2025-01-22 FOR INSTALLATION OF INSTALL TWO HI- LITE PIN AT FS838.00 SDR CALA2025012200170Stiffener · crackedRH FWD EMERGENCY EXIT HATCH AFT VERTICAL STIFFNER IS CRACKED. REMOVED AND REPLACED AFT VERTICAL STIFFENER ON RH FWD EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.SDR CALA2025012100164Stiffener · crackedLH AFT OVER WING EXIT AFT VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER ON L/H OVER WING EXIT IA W A320 SRM 51-72-911-001. ACMP BY MECH V934190 INSP BY V935513SDR YENA2025012100089Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.135 INCH APPROX; REF AEROMAN N/R 2024-755221 REMOVED AND REPLACED FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LHSDR YENA2025012100088Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.125 INCH APPROX; REF AEROMAN N/R 2024- 755213, REMOVED AND REPLACED FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD SDR YENA2025012100087Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.140 INCH APPROX; REF. AERO WO: 2024 423/1 NR 2024-755216 - R&R FR SEGMENTS 1 AT OVERWING EMERG. EXIT DOOR ( AFT LH EEH DOOSDR YENA2025012100086Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT RH EEH DOOR 844) CRACK L=0.129 INCH APPROX; REF. AERO WO: 2024 423/1 NR 2024-755222 - R&R FR SEGMENTS 1 AT OVERWING EMERG. EXIT DOOR (AFT RH EEH DOORSDR YENA2025012100085Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 RH SIDE, DOOR STOP FITTING 7. CRACK DIRECTION IS: 11 OCLOCK; CRACK DEPTH IS : 0 .118 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00026) REF AEROMAN N/R 2024-755200, PSDR YENA2025012100084Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H3 ON FRAME 16 RH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 11 OCLOCK; CRACK DEPTH IS : 0 .120 INCH APPROX; REF AEROMAN N/R 2024-755201, REMOVED AND REPLACED INTERCOSTAL FITTING LOC ASDR YENA2025012100083Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 20 LH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 8 OCLOCK; CRACK DEPTH IS : 0. 114 INCH APPROX; REF AEROMAN N/R 2024-755205, PERFORMED REPAIR AT HOLE H1 ON FRAME 20 LH SIDESDR YENA2025012100082Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 LH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 4 OCLOCK; CRACK DEPTH IS : 0. 114 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00027) FUR-A320-53-01952, REF AEROMASDR YENA2025012100081Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 20 RH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 3 OCLOCK; CRACK DEPTH IS : 0. 112 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00028) FUR-A320-53-01953, REF AEROMSDR YENA2025012100080Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE, AT AFT GALLEY AREA, DOOR STOP 1, INBOARD/LOWER HOLE, CRACK INDICATION LOCATED AT 4 OCLOCK VIEW LOOK ING FROM FWD, DEPTH IS 0.167 INCHES APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00032) FUR-A3SDR AALA202501217380Door Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU COMPARTMENT DOOR SURROUND STRUCTURE AT LBL 20. REPLAIRED PER EA 360699 AND AARD 51-00-05-1.SDR DALA2025012000465Door Frame · corrodedCORROSION ON CARGO DOOR JAMB BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: CORROSION LEVEL 2. CARGO DOOR JAMB CORROSION BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT WAS REPSDR SWIA20250430116Pressure Web · crackedPAX-CAB, EVIDENCE OF CRACK ON PRESSURE WEB (CRACK LINE 3" LONG-APROX) FS 459, WL 64 APROX - BETWEEN LBL 9 - LBL 14 (C-CHECK RO 04/30/2025)PERFORMED PRESSURE WEB FLOOR REPAIR AS REQ'D PER REO 601R-53-41-3286 REV. -- DATED: 2025-03-11. SEE ATTACHED RS-01'S FORSDR SIMA20250116002Seal Rest · corrodedFWD CARGO DOOR CUTOUT LWR SILL UPPER SECTION HAS CORROSION BELOW FIRST AND SECOND LOWER FRAME FITTINGS. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR FWD CARGO DOOR CUTOUT LWR SILL IAW EMB 175 SRM 51-40-08SDR ASAA2025011655705Angle · crackedFWD CARGO BAFFLE CLIP IS CRACKED STA 500K L/H SIDE. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW B737-900ER SRM 51-40-02-0G-0 & 51-40-05-0G-0.SDR IPXA2025012228979Spring · deformedFOUND MAIN ENTRY DOOR STOP PIN RETAINER SPRING DEFORM 1 EA.INSTALLED AND ADJUSTED F/O #2 SLIDING WINDOW PER AMM 56-11-02/401 AND 56-11-02/501. LEAK CHK PERFORMED PER 05-51-24/201.SDR VNAA20250116074Plate · corrodedMULTIPLE AREAS OF CORROSION R/H SILL PLATE F.S. 280 -333 RBL 34 CORRECTIVE ACTION: REMOVED AND REPLACED R/H SILL PLATE P/N SH670-32172-5 AT FS 280-333 RBL 34 IAW CRJ 700 SRM 51-42-13-001-001-A01SDR VNAA20250116068Splice · corrodedDISCREPANCY: FS 629 STGR 19L -27 ON WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGES FWD AND AFT HAVE MULTIPLE AREAS OF CORROSION AROUND THE FASTENER HOLES CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE SPLICE JOINT PLATE P/N SH670-39054-3 WITH SOLID RIVETS IASDR VNAA20250116047Window Post · crackedLH WINDSHIELD SIDE POST P/N 601R33223 IS CRACKED APPROX. 6" FROM TOP AND 2" LONG AT 100% FSH FAILING NDT. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24SDR VNAA20250116046Retainer · corrodedMAIN AVIONICS DOOR L/H FWD SEAL RETAINER IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.SDR J6B2025F00003Retainer · gougedCARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR UPPER AFT CORNER SEAL RETAINER WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CHILD CAMP FOR LEAKSDR SIMA20250115006Gusset · corrodedSSI 53-23-005 AFT GALLEY RH SPLICE AT FR 90 IS CORRODED. (LEVEL 2 CORROSION) RAR AFT GALLEY RH SPLICE AT FR90 IAW EMB 170 SRM 51-40-08.SDR VNAA20250121009Plate · corrodedCORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR YENA2025011600061Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 LH. CRACK DIRECTION 5 AND 11 OCLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00036) REF AEM WO 2024-413/1, NR 2024-749227, PERFOR
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