JASC 5311
Service difficulty reports · 61,540
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 SWAA2024112753520Frame · crackedCRACK FRAME BS 312 AT LEVEL STRINGER 5L AT PASSENGER CABIN 2024-672290<[01] REPAIRED FRAME BS 312 AT LEVEL STRINGER 5L AT PASSENGER CABIN IAW B737-700 EA M-22-153-01244 SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BESDR R61A2024110700530Frame · corrodedFR 88 LOWER SIDE IS CORRODED BETWEEN STGR 27R-28R. REMOVED AND REPLACED FR 88 BETWEEN STGR 25R-23L. REF SRM 51-40-08.SDR DALA2024103110551Stub Frame · cracked(LOG 0634531) CRACK DAMAGE FOUND ON RH STUB FRAME OF FWD GALLEY DOOR SURROUND STRUCTURE AT STA 296.4. R/H STUB FRAME OF FWD GALLEY DOOR SURROUND STRUCTURE AT STA 296.4 WAS REPAIRED IAW B737-800 SRM 53-10-12-2R-7.SDR DALA2024102510407Frame · crackedSHIP 1708 HFEC INSPECTION FOUND 01 EA CRACK IN THE FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AT 883.5 RBL89. CORRECTIVE ACTION: THE CRACK IN THE FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AT STA883.5 RBL89 BELOW WL200 REPAIRED AS PER W/C 5311-01195-SDR REXA2024121601588Frame · corrodedFRAME AT FS 379.00 IS CORRODED BETWEEN STGR 24R TO 20R. LOCATED AND DRILLED NEW SERVICEABLE FRAME P/N: SH670-32118-1S, AT FS379 BETWEEN STR 20R TO STR25R IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE FRAME FS 379 P/N: SH670-32118-1S, BETWEEN SDR REXA2024120901564Frame Splice · corrodedFS333 CIRCUMFERENTIAL SPLICE IS CORRODED BETWEEN STGR 20R-21R. COMPLIED WITH MHIRJ REO# 670-53-21-2517 REV. - - DATED 2024-12-04.SDR HNAA2024120401156Frame · cracked53-2009 CRACK ON FR4 IN BATTERY COMPARTMENT BTW STR19-20L. REPAIRED IAW ETD 2024-145-030671 AND EO1-53-24-0680SDR IPXA2024112010471Frame · dentedFRAME 1500 RIGHT SIDE IN AFT PIT IS DENTED. DOT AA007. REQUIRED SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF, REV 121, 53-00-07-2R-5, TABLE #3 FOR ZONE #1.SDR IPXA2024112510405Frame · dentedFRAME 1460 RIGHT SIDE BETWEEN S-25R AND S-27R, IN AFT PIT IS DENTED. DOT AA006. CORRECTION TO LAST STATEMENT REPAIR PER DETAIL #1SDR DALA2024102410385Frame · crackedSHIP 3133 FUSELAGE FRAMES CROSSBEAM JUNCTION AREA AT FR16 RH CRACKED HOLE 3. CORRECTIVE ACTION: REPAIRED PER ER/A 620268-14AD. (0624050)SDR REXA2024112501507Frame · corrodedFRAME AT FS 661.00 IS CORRODED BETWEEN STGR 26L AND 26R. RECEIVED ENDEAVOR AIR EA# CRJ753-17805 REV. IR DATED 11/21/2024 AND COMPLIED WITH STEPS 1 AND 3. PERFORMED H.F.E.C. ON FRAME AT FS661 BETWEEN STRINGER 26L-26R REWORK AREAS IAW ENDEAVOR AIR EA CRJ753-1780SDR SWAA2024112152064Frame · crackedFRAME ASSEMBLY CRACKED IN PAX CABIN AT BS312; 11INCHES BELOW S-4L.<[01] ACCOMPLISHED REPAIR PER EA#M-22-153-01244 REV B;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR FDEA202410221573Frame · crackedAFTER INSPECTION PER FEDEX EO, F-5310-E0329085 P-6 STEP 3A CRACK WAS FOUND AT FRAME 1640 R/H S-14R. COMPLIED WITH EA # F-5310-T0380850 P1 TITLE; FUSELAGE - MAIN FRAME - RH STA 1640 - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9R AND S-20R, THIS IS A MSDR REXA2024122301602Frame · corrodedAFT SIDE OF F.S. 1031 FRAME IS CORRODED BETWEEN STGR 21L TO 22L, AND FWD SIDE IS CORRODED BETWEEN STGR 26L TO STGR 25L. REMOVED CORROSION ON AFT SIDE OF FS1031 BETWEEN STGR 21L AND 22L FOUND TO BE OUT OF LIMITS DUE TO 50% REMOVED PLUS EXCESSIVE PITTING IAW SDR SWAA2024112651397Frame · crackedCRACK FRAME ON BS 947.5 BETWEEN S-26R TO S-27R AFT CARGO COMPARTMENT 2024-651056<[01] REPLACED FRAME ON BS 947.5 BETWEEN S-23L TO S-23R AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 ITEM 9 AND DWG# 147A1047; SHEET 107; REV.?; SEE INDIVIDSDR SWAA2024112551348Frame · crackedFWD SERVICE DOOR FRAME BS 294 CRACKED AT LOWER END RBL 56 WL 208.<[01] REFER TO FAULT TTG8Q00WJ92N FOR REPAIR RESOLUTION;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024112551351Frame · crackedCRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282.<[01] REMOVED CRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282 PER M-22-153-01244 ON FAULT# TTG8Q00WKNT8.;[02] VERIFIED CORRECTIVE ACTION 1SDR DALA2024102410364Frame · cracked(LOG 0621991) CRACK FOUND AT FRAME STA 440 STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410363Frame · cracked(LOG 0621985) CRACK FOUND AT FRAME STA 380 STR 8L AT OUTBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410362Frame · cracked(LOG 0621981) CRACK FOUND IN FRAME AT STA 827 STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410361Frame · cracked(LOG 0621977) CRACK FOUND IN FRAME AT STA 727B STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410360Frame · cracked(LOG 0621967) CRACK FOUND IN FRAME AT STA 500F STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410358Frame · cracked(LOG 0622115) CRACK FOUND AT FRAME STA 867 STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410357Frame · cracked(LOG 0622096) CRACK FOUND AT FRAME STA 827 STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410356Frame · cracked(LOG 0622084) CRACK FOUND AT FRAME STA 727B STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410355Frame · cracked(LOG 0622077) CRACK FOUND AT FRAME STA 500D STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410354Frame · cracked(LOG 0622046) CRACK FOUND AT FRAME STA 440 STR 8L AT INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410353Frame · cracked(LOG 0622042) CRACK FOUND IN FRAME AT STA 500F STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410352Frame · cracked(LOG 0622036) CRACK FOUND IN FRAME AT STA 727B STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410351Frame · cracked(LOG 0622029) CRACK FOUND IN FRAME AT STA 827 STR 8R INBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410350Frame · cracked(LOG 0622022) CRACK FOUND AT FRAME STA 380 STR 8L AT OUTBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102410349Frame · cracked(LOG 0622015) CRACK FOUND AT FRAME STA 380 STR 8L AT OUTBD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA2526-01236.SDR DALA2024102210315Frame · crackedCRACK ON FRAME BTW STA Y=1037 AND LONG 14L AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 14L AT AFT PAX CABIN WAS REPAIRED PER ER/A 621344-14 REV ORIG SECTION I, PERMANENT REPAIR. ASSOCIATED ER/A 00-621344 ADDED FOR AC 9529. (LP #062103SDR VNAA202410210008Frame · corroded"CORROSION ON FRAME FS364.00 NEAR STGR 27 BEHIND OF SENSOR PX41 AT MAIN AVIONICS COMPARTMENT. FRAME FS364 WAS RE INSPECTED PER CRJ900 NDTM PART 01 51-20-009-210-A01 AND ONLY NUTPLATE BRACKET WAS FOUND WITH CORROSION, WAS FABRICATED PER DWG SH670-32456 REV. NCSDR VNAA202410210006Frame · corroded"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900SDR VNAA202410210005Frame · corroded"DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON FRAME FS 295.00 BTW STGR 24RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. SUMMARY CORROSION ON FRAME FS 295.00 BTW STGR 25RH AND STGR 26LH THIS WAS FOUND ITS OUT LIMITS PER CRJ-900SDR SWAA2024120551162Web · crackedCRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-633925<[01] REPLACED HORIZONTAL WEB LOC. BS 294.5 TO BS 332.1 AT LEVEL STR 17R FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:141A8310 SDR SWAA2024112651066Stub Frame · crackedCRACK ON STUB FRAME LOCATED BS 294.5 BETWEEN S-10R TO S-6R AT PASSENGER CABIN 2024-651034<[01] REPLACED STUB FRAME LOCATED BS 294.5 BETWEEN S-10R TO S-6R AT PASSENGER CABIN AND FASTENER IAW B737-700 SRM: 51-40-02 AND DWG: 141A8370 SHEET 10 REV? SEE INDIVIDUAL SDR UIEA2024101601041Frame · corrodedAFT AREA BULK CARGO ON THE STA 1540 AND STG 36LH FRAME WITH CORROSION.(<P>SHEAR TIE WAS REPLACED BY NEW ONE PER DWG 146T1222. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202410201564Frame · dentedMAIN DECK CARGO COMPARTMENT LEFT HAND FRAME AT STATION 1741 L12 FOUND DENTED. CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT DENT AT LEFT HAND FRAME STATION 1741 LONGERON 12 LEFT REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQSDR SWAA2024112150854Stub Frame · crackedCRACK ON R1 DOORWAY FWD STUB FRAME IB SURFACE; BS 295 STR 17R<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; VERIFIED 1 INCH LONG CRACK FOUND; MARKED. <BR>EQUIP ID IS000680 DUE 07/25;[02] REMOVED DAMAGE PART OF THE R1 DOORWAY FWD STUB SDR YENA2024102201393Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE THE FRAME SEGMENTS (1) THE EEH 833 CRACK LENGTH IS 0.330 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EEH 833 (1EA) IAW EC. A320-52-1144 A320 SRM 51-72-11. FOR INSTALLATION SEE TASK CSDR YENA2024102201392Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 844 PASSENGER CABIN CRACK LENGTH IS 0.350 INCHES; CORRECTIVE ACTION: REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EMERGENCY EXIT DOOR 844 I.A.W EC. A320-52-SDR YENA2024102201390Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 834 PASSENGER CABIN CRACK LENGTH IS 0.280 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EEH 834 (1EA) IAW EC. A320-52-1144 A320 SRM 51-72-11. FOR INSTASDR YENA2024102201391Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 843 PASSENGER CABIN CRACK LENGTH IS 0.315 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EMERGENCY EXIT DOOR 843 I.A.W EC. A320-52-1144 AND A320 SRM 51-SDR ASAA2024101853379Frame Splice · corrodedAFT CARGO RH FRAME SPLICE AT STA 727I IS CORRODED GROUNDED - YES. SPLICE EVALUATED AND FOUND W/ NO ALLOWABLE LIMITS IAW B737-900 SRM 53-00-07-1A-1 REMOVED IAW B737-900 SRM 51-40-02, LOCATE AND DRILLED HOLES IN SPLICE IAW B737-900 SRM 51-40-05 AND BAC DWG 146A1SDR DALA2024102110283Frame · corrodedCORROSIONS ON FRAME STA Y=870 BTW L-29L AND L-29R AT AFT CARGO. SUMMARY OF NRC 00206: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=870 BTW L-29L AND L-29R AT AFT CARGO WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM AN INITIAL INTERNAL ASDR ASAA2024101753697Frame · crackedSTA 328 FRAME WEB CRACKED BETWEEN STR 20R & 21R. GROUNDED - YES. REMOVED & REPLACED STA 328 FRAME WEB FROM STR 27R TO STR 10R IAW BOEING 737-700 SRM 51-40-02-0G-0.SDR 2A6R2024101771704Frame · crackedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND FRAME 5 CRACKED ON THE RIGHT AND LEFT BEAM NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE CRACKS ARE NE MORE THAN 1.50 INCHES IN LENGTH.SDR 2A6R2024101771703Frame · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FRAME 1 HAS EXTENSIVE CORROSION ON THE LOWER FLANGE OF THE FRAME ON THE LEFT AND RIGHT SIDE AS WELL AS CORROSION IN THE WEB OF THE FRAME.
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