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 AALA202406262189Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT AREA LEFT HAND SIDE UPPER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 353883.SDR AALA202409068047Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT SIDE UPPER TENSION BOLT AREA CRACKED BETWEEN FR 4 AND FR 6 AT Y0. REPAIRED WINDSHIELD FRAME PER EA 355749.SDR AALA202409062412Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT SIDE UPPER TENSION BOLT AREA CRACKED BETWEEN FR 4 AND FR 6 AT Y0. REPAIRED WINDSHIELD FRAME PER EA 355749.SDR IXXA20240801001Support Beam · chafedR/H AFT MLG SUPPORT BEAM FWD EDGE OF THE LOWER FREE FLANGE HAS CHAFING DAMAGE DUE TO CONTACT WITH LOWER BULB SEAL ATTACH ANGLE APPROX 30" OTBD OF THE INBD END OF BEAMSDR CALA2024062801919Door Frame · crackedR/H O/W ESCAPE HATCH FWD VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED R/H O/W ESCAPE HATCH FWD VERTICAL FRAME IAW SRM 51- 72-11 AND 51-42-11.SDR CALA2024062801918Door Frame · crackedR/H O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED R/H O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A319 SRM 51 -72-11 AND 51-42-11.SDR CALA2024062801917Door Frame · crackedL/H O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED LH O/W ESCAPE HATCH AFT VERTICAL FRAME IAW SRM 51-72-11 AND 51-11-12.SDR CALA2024062801913Door Frame · crackedL/H O/W ESCAPE HATCH FWD VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED L/H O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A319 SRM 51 -72-11 AND 51-42-11.SDR CALA2024062501888Striker · missingCENTER SECTION SUPPORT BEAM MISSING STRIKER PLATE AND CHORD DAMAGED.LP CREATED FOR ESFR PURPOSE ESFR CREATED SFR NUMBER 1036615SDR SWAA2024072405249Tie Down · corrodedFWD. CARGO COMPARTMENT FLOOR TRACK HAS CORROSION ON 3EA TIE DOWN AT WL 156; LBL 18; BS 402/BS 436/BS 495.<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT FLOOOR TRACK TIE DOWN BS 396 TO BS 500D LBL 18 WL 146 IAW SRM 51-40-02 AND DWG 143A7500.;[02] VERIFIED CORSDR AALA202406254893Lock · out of adjustAIRCRAFT WAS GROUNDED: GATE AGENT REPORTS AIRCRAFT ENTRY DOOR IS VERY DIFFICULT TO OPEN FROM OUTSIDE. CHECKED ADJUSTMENT OF SECOND FROM LOWER DOOR STOP PIN AND INSTALLED LOCK CLIP, PER AMM 52-11-00. CHECKS GOOD.SDR DALA2024062506461Door Frame · crackedSHIP 3161 CRACK INDICATION FOUND ON OPEN FASTENER HOLE AT FR68RH DOOR STOP FITTI NG 1 LOWER INBOARD POSITION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. ON FR 68 RH AT LEVEL DOOR STOP FITTING #1, LOWER INBOARD POSITION HOLE AS PER A319 SRM53-41-12-300-SDR UIEA2024061400522Structure · corrodedCENTER SECTION AFT FACE CORROSION ( NEAR RH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED : REMAIN 0.755" ORG 0806, WIDTH 1.4" LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DASDR UIEA2024061700526Structure · crackedBS 2598 LH LOWER INNER CHORD 1EA CRACK FOUND ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) AT 2 O'CLOCK POSITION WITH THROUGH THICKNESS CRACK(<P>BS 2598 LH LOWER INNER CHORD 1EA CRACK ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) REPAIRED IAW RI-53-00-16937 RESDR DALA2024062506477Retainer · cracked(LOG 0409603) CRACK ON LH NO.1 WINDSHIELD RETAINER (LH UPPER CORNER) AT FWD FUSELAGE. CRACK ON LH NO.1 WINDSHIELD RETAINER (LH UPPER CORNER) AT FWD FUSELAGE WAS REPAIRED PER PRI 618217-14 REV 0 AND REV 1 AND ER/A 618217-14AD REV. ORIGINAL.SDR YENA2024062500912Beam · corrodedDURING HEAVY MAINTENANCE: CPCP FINDING INITIAL INSPECTION: CORROSION ON LONGITUDINAL BEAM BTW FR12 AND FR 17, Y= 270RH AT W1; (RESOLVED ON W/O: 1309155 TASKCARD: NR-00010) 355218 - VELAZQUEZ NEQUIZ, ANTON TONATIHU 10/JUN/24 69707 - CORONADO LOPEZ, JOSE DE JESUSDR YENA2024062500911Beam · corrodedDURING HEAVY MAINTENANCE: CPCP FINDING INITIAL INSPECTION: CORROSION ON LONGITUDINAL BEAM BTW FR12 AND FR 17 BEAM Y= 300LH. AT W1; (RESOLVED ON W/O: 1309155 TASKCARD: NR-00015) 355218 - VELAZQUEZ NEQUIZ, ANTON TONATIHU 10/JUN/24 69707 - CORONADO LOPEZ, JOSE DESDR YENA2024062500910Beam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON BEAM RH LOCATED BTW FR85/86 AND Y=280 AT AFT FLOOR STRUCTURE; (RESOLVED ON W/O: 1309155 TASKCARD: NR-00022) 359618 - CRUZ LARRIETA, EMMANUEL 12/JUN/24 10001841 - GUTIERREZ DIAZ, JESUS 12/JUN/24 WIP: SUMMARY: CORROSION ON SDR YENA2024062500909Beam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON CENTER RH LONGITUDINAL BEAM BTW FR 84-85 AND Y=200 AT AFT FLOOR STRUCTURE; (RESOLVED ON W/O: 1309155 TASKCARD: NR-00024) 359618 - CRUZ LARRIETA, EMMANUEL 12/JUN/24 10001841 -GUTIERREZ DIAZ, JESUS 12/JUN/24 WIP: SUMMARY: CSDR VNAA202406230008Window Post · crackedLH WINDSHIELD SIDE POST IS VISIBLY CRACKED ON THE FWD SIDE, APPROXIMATELY 5" FROM THE TOP OF THE POSTSDR VNAA202406230005Fitting · crackedLH OVERWING EMERGENCY EXIT UPPER AFT ALIGNMENT FITTING IS CRACKEDSDR AALA202408142799Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD RIGHT HAND LATERAL FRAME RIGHT AT FR 4 AND Y0. REPLACED WINDSHIELD FRAME PER EA 355670SDR AALA202408144392Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD LEFT HAND LATERAL FRAME RIGHT AT FR 4 AND Y0. REPLACED WINDSHIELD FRAME PER EA 355669.SDR K11A2024080900275Door Frame · crackedR1 DOOR CUTOUT FRAME NEAR UPPER HINGE CRACKED.SDR HNAA2024090500236Door Frame · corrodedRF1 BTW FR65-68, BEAM LOWER FRAME CARGO DOOR, FOUND CORRODED.SDR SWAA2024080704329Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.312 INCH 2024-404906<[01] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[02] STEP 8 TOOL USED EDDY CSDR SWAA2024080704480Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.375 INCH 2024-404930<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 210138503; DUE DATE: 21-JUL-24;[02] ON STEP 10; TOOL USED PSDR SWAA2024080504309Panel · corrodedPANEL 192F HAS FLAME SPRAY CORRODED AT ANTENNA MOUNT AREA. 8-22<[01] RECIEVED NEW PANEL. WORK WILL BE ACCOMPLISHED ON TTG8Q00U3UBG;[02] CORRECTION TO STEP 1: <BR>RECIEVED NEW PANEL; PART NUMBER 14A7755-1 192F. WORK WILL BE ACCOMPLISHED ON TTG8Q00TNXXE;[03] VERSDR SWAA2024071104302Pressure Panel · corrodedDOT A24-7 RH AFT NOSE W/W PRESSURE PANEL 114BW HAS SEVERAL AREAS OF FRETTING CORROSION ON INTERNAL SIDE.<[01] REMOVED FRETTING CORROSION ON PANEL 114BW IAW EA 24-153-01783-WIP1 AND EA 24-153-01783;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR DALA2024062406341Beam · crackedCRACK ON BEAM #2 STA Y=196 APROX IN PASSANGER DOOR (L1) AT CABIN PAX. SUMMARY OF NRC 00090: AREA ON BEAM #2 STA Y=196 IN PASSANGER DOOR L1 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0406350)SDR DALA2024062106306Beam · corroded(LOG 0404892) CORROSION ON BEAM STA 294 RBL 10 AT W1. BEAM STA 294 RBL 10 AT W1 WAS REPAIRED PER B737-800 SRM 53-10-51-2R.SDR SWIA202411040620Fitting · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED CLOSED) INSTALLED NEW FITTING IAW BOMBARDIER DRAWING SH670-33600 REV AD, CRJ700 SRM 51-42-22-001-001-A01 REV 38. DATE: JSDR AALA202409236246Splice Plate · damagedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING CENTER POST RIGHT HAND SPLICE PLATE HAS 2 HOLES WITH REJECTABLE DAMAGE INDICATION. MAINTENANCE REPLACED SPLICE PLATE PER EA 356606.SDR REXA2024090300676Post · corrodedFLOOR POST AT F.S. 280 LBL 11.16 IS HEAVILY CORRODED TOWARDS BOTTOM OF POST. REPLACED FLOOR POST AT FS 280.00 LBL 11.16 P/N: CC670-34180-7 IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01.SDR REXA2024081200655Door Frame · cracked"LH AFT EMERGENCY EXIT DOOR (SB1439) UPPER FORMER CRACKED AT LUG REMOVED SURFACE FINISH ON LH AFT EMERGENCY EXIT DOOR (SB1439) UPPER FORMER IAW CRJ 900 SRM 51-26-01-001-001-A01. REF ATTACHED EA CRJ952-16927, REF STEP 12 OF THE P1 COPY FOR WORK PERFORMED. PERSDR SWAA2024073003665Deck Plate · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+2 RBL 41 WL 203 (MARKED)<[01] REMOVED DAMAGE ON HORIZONTAL PRESSURE DECK AND REPAIRED BS663-BS675 RBL 30-LBL60 I.A.W SRM 53-40-51-2R-2 REPAIR 2;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024071903966Tie Clip · crackedFWD CARGO RH FRAME AT STA 500H HAS 1EA CRACKED CLIP DOT M339<[01] REMOVED AND REPLACED CLIP AT STA 500H WITH NEW PN:143A7502U158 PO:1094585.1 IAW B737-800 SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT).;[02] VERIFSDR UIEA2024061800545Seal · leakingEXTERNAL FUSELAGE, LEAK ON RH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF RH EMERGENCY EXIT DOOR </SPAN><SPAN>WAS REPLACED IAW AMM 52-09-06-404--</SPAN><SPAN>003 REV 142, APR 22, 2024; CHECK FOR LEAKS </SPAN><SPAN>WAS PERFORMED, NO LEAKS FOUND</SPAN></P>)SDR AALA202406219773Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406217713Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR DALA2024062006271Beam · damagedCRACK BEYOND STOP DRILL ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00174: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7 PAR. 6 FIGURE 2SDR DALA2024062006269Door Frame · corrodedCORROSION ON LOWER EDGE AND FWD EDGE DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00297: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0402912)SDR HNAA2024071800540Beam · corroded00073 MULTIPLE SPOTS OF CORROSION FOUND ON BOTTOM AREA OF BAGGAGE DOOR SURROUND STRUCTURE. REMOVED AND INSTALLED BEAM ASSY PN# 145-25480-603 (CARGO DOOR SILL) @ AFT CARGO DOOR LOWER SILL IAW EMB145-LR SRM 51-40-02-PRSDR J6BA2024081400008Structure · damagedAFT LOWER FUSELAGE DAMAGED FROM TAILSTAND; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REMOVED AND REPLACED 2 (EA) STRINGERS 25L AND STR 27 , 1 (EA) GUSSET AT STR 27 AND 1 (EA) LH LOWER AFT SKIN PANEL PART # 600-21032-5 THAT WERE ALL DAMAGED BETSDR SWAA2024071903064Doubler · corrodedMIDDLE FUSELAGE DRAIN DOUBLER HAS CORROSION AROUND FASTENERS AFT OF MLG WHEEL WELL DOT M334<[01] REMOVED CORROSION; ORIG. .063; REF BAC DWG 146A3239 REV -; MATERIAL LOSS .005; REMAINING .058 NO DAMAGED ALLOWED IN THIS AREA; REF B737-NG SRM 53-60-01-1A-1 TABLE SDR ASAA2024061850950Transition Panel · corrodedAFT PIT L/H TRANSITION IS CORRODED FROM STA 727C-787. GROUNDED - YES. REMOVED AND REPLACED AFT PIT L/H TRANSITION FROM STA 727F TO 727C IAW B737-800 SRM 51-40-02-0G-0, TRANSITION FROM STA 727G TO STA 787 FOUND TO BE IN LIMITS IAW B737-800 SRM 53-00-53-1A-2W= 1SDR AALA202406211215Fairing · corrodedAIRCRAFT IN BASE MAINTENANCE: TAIL SKID DRAG LEVER FAIRING LEADING EDGE INNER SURFACE HAS AREAS OF CORROSION. REMOVED CORROSION AT TAIL SKID DRRAG LEVER FAIRING LEADING EDGE INNER SURFACE. PER B7737 SRM51-10-02.SDR CALA2024061901867Fitting · cracked(SUPPORT TASK) DURING ROTO TEST AT LH FR16 DOOR STOP 7 LOWER INB OARD HOLE FOUND CRAKCED. "REPAIR BEFORE NEXT FLIGHT" W/C:93882 REPAIRED IAW EC/RA 5311-03221. W/C:93882 ALL REQUIRED INSPECTIONS COMPLIED ON WORKCARD # 93882SDR DALA2024061906216Window Frame · crackedCRACK ON UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW IN REF TO NRC 00027. SUMMARY OF NRC 00661: UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1 PROCEDURE 1, REPAIR 1. (LP #0400469)SDR DALA2024061906215Window Frame · crackedCRACK ON RETAINER AND FRAME AT LH SLIDING WINDOW A COCKPIT. SUMMARY OF NRC 00182: FRAME AT LH SLIDING WINDOW A COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1 AND RETAINER LH SLIDING WINDOW COCKPIT WAS REPLACED PER B717-200 SRM 51-41-02
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