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 DALA2024072307397Frame · cracked(LOG 0455961) CRACK (0.250 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 867 BTW S-8L & S-9L. FUSELAGE FRAME STA 867 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024072307396Frame · cracked(LOG 0455951) CRACK (0.125 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C. BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024072307395Frame · cracked(LOG 0455944) CRACK (0.796 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L AND CRACK (0.125IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L. FUSELAGE FRAME STA 380 BTW S-8L & S-9L WAS REPAIRED UNDER ASDR DALA2024072307394Frame · cracked(LOG 0455202) CRACK (0.250 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024072307393Frame · cracked(LOG 0455181) CRACK (0.500 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500D. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 500D BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024072307392Frame · cracked(LOG 0455149) CRACK (0.625 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R AND CRACK (0.125IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R. RH FUSELAGE FRAME STA 380 BTW S-8R & S-9R WAS REPAIRED USDR YENA2024072301027Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE HOLE 6 AT LEVEL DOOR STOP 7. CRACK AT 1. O CLOCK. D1-D2= 0.079 INCH. CONFIRM INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-00; REF AEROMAN N/R 2024-348897, PERFORMED PERMANENT REPAIR OF CRSDR YENA2024072301026Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE HOLE C AT LEVEL DOOR STOP 7 . CRACK AT 1. O CLOCK. D1-D2= 0.118 INCH. CONFIRM INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-0; REF AEROMAN N/R 20240348898, PERFORMED PERMANENT REPAIR OF CRSDR YENA2024072301024Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / RHS FR16 DOUBLE JOGGLE AREA HOLE C AND #6 / CRACKS - PERMANENT REPAIR; REFERENCES: AEROMAN EA 53-9015-24 REV. 0 (COVER + PARTS 1-3) AIRBUS SB A320-53-1373 REV. 01 AIRBUS RDAF 81411276/028/2024#A AIRBUS SDR N6WA2024072201Bracket · crackedANGLE BRACKET LOCATED ON AFT SIDE OF FS220.00 STRINGER 13A ON RH SIDE IS CRACKED. REPAIRED RH INTERCOSTAL AT FS220.00 IAW CRJ REO 670-53-11-1979 AND EO C550-53MR-24.SDR DALA2024072207363Frame · cracked(LOG 0455956) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B. BTW S-8L & S-9L. FUSELAGE FRAME STA 727B BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024072207362Frame · cracked(LOG 0455948) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 400 BTW S-8L & S-9L. FUSELAGE FRAME STA 400 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024072207361Frame · cracked(LOG 0455208) CRACK (0.125 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 867 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR SWIA202411151241Frame · damagedFRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WSDR SWI2024F01098Frame · damagedFRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WSDR SWIA20240718Frame · crackedFRAME 682.00 HAS 1 CRACK ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMENT BAY DOOR OPENING. (FILED CLOSED) REPAIRED CRACK IN FRAME 682.00 ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMENSDR SWI2024F00910Frame · damagedFRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED OPEN)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WATSDR SWIA20240809718Frame · crackedFRAME 682.00 HAS 1 CRACK ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMENT BAY DOOR OPENING. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR UIEA2024071300652Frame · damagedM/D LH STA 940 FRAME FASTENER HOLE BTN STR 8L-9L FOUND PREVIOUSLY FREEZE PLUG HOLE REPAIR.(<P>FRAME REPLACEMENT CARRIED OUT AS PER SRM 51-10-02, NEW FRAME HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTSDR UIEA2024071300653Frame · crackedLEFT BS 2231 STR 16L FRAME FWD INNER CHORD 1EA FASTENER HOLE CRACK. FRAME FWD INNER CHORD REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071300655Frame · crackedRIGHT BS880 UPPER DECK TENSION TIE ATTACHED TO FRAME FOUND 2EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 9F AND SRM 53-20-07-2R-5 REPAIR 5 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071300656Frame · crackedRIGHT BS 840 UPR DECK TENSION TIE ATT FRAME FOUND 4EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 7F AND SRM 53-20-07-2R-3 REPAIR 3 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR A6WA202407168779Frame · damagedCORROSION DAMAGED FRAME AT FS 605.00 BETWEEN STR 24L AND 20R. AIRCRAFT REMOVED FROM SERVICE. DAMAGED FRAME WAS REPAIRED BY CREATING A DOUBLER PER REO 601R-53-61-8207 REV --.SDR DALA2024071707225Cusp Web · damagedMISSING MATERIAL ON CUSP WEB MEMBRANE STA 527 X=-59 AT PAX CAB. SUMMARY OF NRC 00501: CUSP WEB MEMBRANE STA 527 X=-59 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #0450942)SDR DALA2024071607173Frame · crackedCRACK ON FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00468: FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ER/A 619238-14 REV ORIGINAL AND PRI REV 1. ASSOCIATED ER/A 14-619238 ADDED FOR AC 9502. (LP #SDR SWAA2024082212187Frame · corrodedCORROSION FRAME ON BS 303.9 LEVEL STRINGER 17L AND WL 208.1 FWD GALLEY AND LAV. REPAIRED FRAME ON BS 303.9 LEVEL STRINGER 17L AND WL 208.1 FWD GALLEY AND LAV IAW EA 24-153-02062-WIP1 AND EA 24-153-02062 SUMMARY. REPAIRED FRAME ON BS 303.9 LEVEL STRINGER 17L SDR DALA2024071807251Frame · cracked(LOG 0447566) L/H FUSELAGE FRAME CRACKED AT 827, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED PER CUSTOMER CARD #2526-01236-02A.SDR DALA2024071607186Frame · cracked(LOG 0447569) (L/H) FUSELAGE FRAME CRACKED AT 500F, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED REPAIR PER CUSTOMER CARD #2526-01236-02A.SDR DALA2024071607185Frame · cracked(LOG 0447563) (L/H) FUSELAGE FRAME CRACKED AT 500C, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED REPAIR PER CUSTOMER CARD #2526-01236-02A.SDR DALA2024071607184Frame · cracked(LOG 0447559) (L/H) FUSELAGE FRAME CRACKED AT 867, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED REPAIR PER CUSTOMER CARD #2526-01236-02A.SDR DALA2024071507162Frame · crackedCRACK ON UPPER EDGE FRAME, 2 FROM UPPER EDGE AND 38 FROM FWD EDGE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00107: UPPER EDGE AND FWD EDGE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1.SDR SWIA20240920031Frame · crackedFRAME CRACKED AT FS333.00 BETWEEN STGR 1R AND STGR 2R (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO FRAME SECTOR FS333 BETWEEN STR 1R & STR 2R REF REO 670-53-21-2437 REV -- 2024-07-24. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWAA2024082612113Stub Frame · crackedCRACK ON STUB FRAME LOCATED ON BS 294.5 LOCATED BTW STR S-8R TO S- 9R AT PASSENGER CABIN 2024-421058<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-7R AND STR-10R FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM B737-700SDR SWAA2024082212163Stub Frame · crackedCRACK LOWER STUB FRAME BS 294.5 AT LEVEL STRINGER 17R FWD GALLEY AREA 2024-443599<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 220272712; DUE DATE: 28-NOV-24.;[02] STEP 7 ET TOOL USED PN: NORTEC 600D ; SN: 210138003. DUE DATE: 11-JUN-25;SDR DALA2024071507158Frame · cracked-AD- CRACK OF 1.00 IN LENGTH APPROX ON UPPER RADIUS OF THE LH OVERWING FRAME TAB STA Y=715.00 (IN REF. CARD 5310-01436-01B STEP 7). SUMMARY OF NRC 000333: THE LH OVERWING FRAME TAB STA Y=715.00 WAS REPLACED AMDS 5310-01436-03A JOB 165-0001. (LP #0444425)SDR NACA2024071200001Frame · corrodedMAIN DECK COMP'T FUSELAGE FRAME CORRODED ON STA847R WL208. FABRICATED SHEAR TIE AND INSTALLED PER NAC EO 737-57-0355SDR VNAA202409010022Frame · corrodedCORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PESDR SWAA2024081611811Frame · crackedPASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] VERIFIED COMPLIED WITH THE TASK CARD.;[02] ALL STEPS COMPLETED;[03] ALL STEPS COMPLETED/CARD COMPLETED.SDR SWAA2024081311958Frame · crackedAFT CARGO BAY FRAME IS CRACKED ON INBOARD FLANGE; BS 747; RBL 20<[01] PARTIALLY COMPLETED STEP-9;[02] AFT CARGO BAY FRAME IS CRACK ON INBOARD FLANGE; BS 747; RBL 20 WAS REPAIRED IAW SRM 53-60-07-2R-2-A01771;[03] VERIFIED CORRECTIVE ACTION 2SDR YENA2024071601014Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT GALLEY AREAA, DOOR STOP 1 INBOARD LOWER HOLE. CRACK INDICATION LOCATED A 5 OCLOCK VIEW LOOKING FROM FWD. DEPTH IS 0.067 INCHES; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00053) ACCOMPLISHED REPSDR DALA2024071507157Frame · crackedCRACK ON FRAME STA Y=1037 AND STR 17 LH AT C. PAX. SUMMARY OF NRC 00361: FRAME AT STA Y=1037 AND STR 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4 PAR 5 A. (LP #0444212)SDR FDEA202407120989Frame · crackedAFTER INSPECTION PER EO F-5310-E0329085 D P6 STEP: 3 CRACK WAS FOUND AT FRAME 1640, S-14 RT. COMPLIED WITH FEDEX E.A.#: F-5310-T0379544 (P1), TITLE: FUSELAGE-MAINFRAME- STA 1640 RH - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9R AND S-20R.SDR FDEA202407120988Frame · crackedAFTER INSPECTION PER EO F-5310-E0329085 D P5 STEP: 3 FIG: 1 CIRCLE: 1 CRACK WAS FOUND AT FRAME BS 1640 LH S-14. COMPLIED WITH FEDEX E.A. #: F-5310-T0379541(P1), TITLE: FUSELAGE-MAINFRAME-LH STA 1640- TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9L AND S-2SDR DALA2024071207076Frame · dentedSHIP 684 DENT ON FRAME STA. 1260 ABOVE S-26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00543: DENT ON FRAME STA. 1260 ABOVE S-26R AT AFT CARGO COMPARTMENT.WAS REPAIRED PER ER/A 618976-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (0442411)SDR IXXA202400712002Frame · corrodedALC HAS SURFACE CORROSION AT STA. 1197+66 RBL-8.SDR NACA2024071100001Frame · crackedMAIN DECK COMP'T FUSELAGE FRAME INNER CHORD CRACK ABOUT 0.5" STA 616L ADJACENT TO LBL 70.85 UNDER FLOOR PANEL. REPAIRED CHORD IAW NAC EO 737-53-0265-04SDR AALA202408208467Frame Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME 71 ANGLE LOCATED BETWEEN STR 26 AND STR 31. REPLACED WITH NEW ANGLE PER SRM 51-42-11-801.SDR DALA2024071607182Frame · cracked(LOG 0447487) (R/H) FUSELAGE FRAME CRACKED AT 867, S-8R A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024071607181Frame · cracked(LOG 0447475) (R/H) FUSELAGE FRAME CRACKED AT 827, S-8R. A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024071607180Frame · cracked(LOG 0447470) (R/H) FUSELAGE FRAME CRACKED AT 500F, S-8R A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.
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