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 VNAA202411090045Frame · corrodedPAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED FRAME FS313.56 BETWEEN DD4 AND DD5 IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR FRAME FS313.56 P/N # 601R318086-1 IAW CRJ 700 SDR VNAA2024111090041Frame · corrodedFOUND CORROSION ON FS 379 R/H FRAME BETWEEN STR 20R AND STR 25R. INSTALLED NEW FS 379 FRAME IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.SDR VNAA202411090011Frame · corrodedFRAME SECTOR 364.00 HAS AREA OF CORROSION ON LOWER FLANGE FWD SIDE AT STR 27. REMOVED DEFECTIVE FRAME SH670-32090-7 AND REPLACED WITH NEW FRAME SH670-32090-9 AT FS364.00 STR27.00 AND COMPLIED WITH MHI RJ REO 670-53-21-687 REV.- B DATED 2023-04-10.SDR AALA202412090380Frame · gougedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FRAME GOUGED AT BS 294.5 AND STR 2L. REPAIRED THE GOUGED MAIN CABIN FRAME AT BS 294.5 STR 2L. PER B737NG SRM 53-00-07-2R-1.SDR SWAA2024120558010Frame · crackedCRACK ON FRAME LOCATED BS312 AND BTW STR5L / STR6L AT PASSENGER CABIN 2024-686307<[01] PERFORMED REPAIR ON FRAME LOCATED BS312 AND BTW STR5L / STR6L AT PASSENGER CABIN IAW EA M-22-153-01244. LENGTH OF CRACK IS:0.320? TOOL USED DIGITAL CALIPER P/N: 500-197-30; SDR SWAA2024121257810Frame · crackedCRACK ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-701458<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON FRAME LOC BS 727B BTW STR 8L TO STR SDR SIMA20241107001Frame · damagedHOLE BURNED INTO FR 10 BETWEEN STRINGERS 12L-13L (MAJOR REPAIR) PERFORMED PERMANENT REPAIR TO FRAME 10 BETWEEN STRINGERS 12L ? 13L IAW ERS-EJ-53MR-5087SDR VNAA202412150004Frame · corrodedCORROSION ON FRAME FS1088.20 BTW STGR 24RH AND STGR 24LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). C2
CORRCTIVE ACTION: CORROSION WAS REMOVED ON FRAME FS=1088.20 BTW STGR 24RH AND STGR 24LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). C2, PER CRJ-900SDR YENA2024111201452Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 20 RH / DOUBLE JOGGLE AREA / DOOR STOP FITTING 7 HOLE 6 / CRACK - PERMANENT REPAIR (FRAME REPLACEMENT); REFERENCES: /1/ AEROMAN EA 53-9051-24 REV. 0 (COVER & PART 1 - 2) /2/ AIRBUS SB A320-53-1374 REVSDR YENA2024111201451Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9043-24 COVER REV.0 & PART 1-5 /2/ AIRBUS SB A320-53-1331 (REF. FAA ADSDR DALA2024111110790Frame · crackedSHIP 1708 HFEC INSPECTION FOUND 01 EA CRACK IN THE FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AT STATION 903.5, RBL 89, BELOW WL 200. CORRECTIVE ACTION: REPAIRED PER W/C 5311- 01195-09F (0646794)SDR DALA2024110810741Frame · corroded(LOG 0648858) CORROSION ON FRAME IN THE E/E BAY LOCATED AT STA 336, S-23L AND WL 167. REMOVED AND REPLACED FRAME IAW B737-800 SRM 51-40-02-0G, AND BOEING DWG 141A1180.SDR REXA2024120601555Frame · corrodedCORROSION FOUND ON FRAME 333 BETWEEN STRINGER 24R-23R REMOVED CORROSION AND COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER REO 670-53-21-2509 REV - - DATED 2024-12-02.SDR DALA2024110810744Frame · corroded(LOG 0648936) CORROSION ON FRAME IN THE E/E BAY LOCATED AT STA 320, S-23L AND WL 168. REMOVED AND REPLACED STUB FRAME IAW B737-800 SRM 51-40-02-0G AND BOEING DWG 141A1180.SDR DALA2024110810733Frame · corroded(LOG 0645364) FUSELAGE / MAIN FRAME / FRAME INNER CHORD / STA 291.5 & S-17R / CORROSION. REPAIRED PER ERA 621732-14.SDR CALA2024110802808Frame · corrodedCORROSION FOUND ON FWD SIDE OF FRAME AT STA 1360 BETWEEN STR 26-27R.SDR AAL2024F00008Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT PASSENGER / CREW DOOR CUTOUT AFT UPPER FRAME CORNER FITTING FORWARD FACE AT FR 68 AND S8R. REPLACED FRAME CORNER FITTING PER SRM 51-42-11.SDR REXA2024121601590Frame · corrodedFRAME 295 HAS CORROSION BETWEEN STR 19R - 20R PERFORMED CUTOUT AT FS295 STR19R AND 25R IAW CRJ-900 SRM 53-00-06-201-001-A03. PERFORMED EDDY CURRENT OF FS295 STR19R-25R CUTLINE EDGES IAW CRJ 700 NDTM PART 1 51-20-006-250-A01 NO INDICATIONS NOTED AT THIS TIMESDR SWAA2024121056510Frame · crackedCRACK FRAME LOCATED BS 259.5 AT LEVEL STRINGER 9L AT COCKPIT 2024-687094<[01] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED STA 259.5 BETWEEN STR 6R TO 11R AT PASSENGER CABIN IAW EA 24-153-03134-WIP1<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 <BR>PSDR DALA2024111110786Frame · crackedSHIP 1708 CABIN CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA927 LH. CORRECTIVE ACTION: REPAIRED PER SRM51-40-02 (0643319)SDR DALA2024111110785Frame · crackedSHIP 1708 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA852 LH. CORRECTIVE ACTION: REPAIRED PER SRM 51-40-02 (0643314)SDR DALA2024110810736Frame · corroded(LOG 0647259) FRAME IN THE FORWARD CARGO WAS FOUND TO BE DENTED AT STATION 500E AT STRINGER S-23L. REPAIRED FWD CARGO COMPARTMENT L/H STA 500E FRAME AT STR 23L IAW B737 SRM 53-30-07-2R-2.SDR DALA2024110810735Frame · corroded(LOG 0647247) FORWARD CARGO BAY FRAME DAMAGED AT STA 500B BETWEEN STR 24R AND STR 23R WL 165. REPAIRED FWD CARGO BAY R/H STA 500B FRAME BETWEEN STR 24R AND 23R WL 165 IAW B737 SRM 53-30-07-2R-2.SDR DALA2024110510648Frame · crackedSHIP 3160 CRACK FOUND IN HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 581727-14. (0644434)SDR VNAA20241213020Frame · corrodedCORROSION ON FRAME FS 265.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS 265.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CSDR SWAA2024121056323Frame · crackedCRACK FRAME ON BS 312 LOCATED BTW STR5L TO STR6L FWD GALLEY AND LAV 2024-685371<[01] PERFORMED REPAIR ON FRAME LOCATED STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN IAW EA M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] PERFORMED REPAIR ON FRAME LOCSDR YENA2024110501433Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE / AREA LH/RH CRACKS - PERMANENT REPAIR; REFERENCES: /1/ DOSSIER REFERENCE 81461224 /2/ AEM EA 53-9039-24 (COVER, P1 THROUGH P5) /3/ R53113672 ISSUE C /4/ R531134SDR SWAA2024121055855Frame · crackedTHERE IS CRACK ON UPPER CHORD OF FRAME ASSEMBLY ON FED CUTOUT BETWEEN S-5L AND S-6L AT BS 312 .<[01] REPAIRED UPPER CHORD OF FRAME ASSEMBLY ON FED CUTOUT BETWEEN S-5L AND S-6L AT BS 312 PER EA M-22-153-01244.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024120455953Frame · crackedCRACK FRAME LOCATED BS400 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680403<[01] REPAIRED FRAME LOCATED BS400 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03279-WIP1 AND EA 24-153-03279. <BR>SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPAIRED FRAME LOCATED BS4SDR SWAA2024120455954Frame · crackedCRACK FRAME LOCATED BS380 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680402<[01] REPAIRED FRAME LOCATED BS380 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03257-WIP AND EA 24-153-03257.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPAIRED FRAME LOCATED BS380SDR SWAA2024120455952Frame · crackedCRACK FRAME LOCATED BS440 AND STR8L TO STR9L AT PASSENGER CABIN 2024-680404<[01] PERFORM REPAIR FRAME LOCATED BS440 AND STR8L TO STR9L AT PASSENGER CABIN IAW EA 24-153-03262-WIP1 AND EA 24-153-03262 <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORM REPAIR FRAME SDR SWAA2024120455736Frame · crackedCRACK ON FRAME LOCATED BS 259.5 AT LEVEL STR9R AT PASSENGER CABIN 2024-680373<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 14-APR-25.;[02] PERFORMED REPAIR ON FRAME LOC. BS259.5 AT PASSENGER CABIN BETWEEN STR 5R TO STR 12R IAW EA 24-153-031SDR IPXA2024112615555Frame · crackedFAULT: CRACK FOUND ON LH FR40 LOWER RADIUS HOLE (FIRST LAYER). RAPAIRED LH FR40 LOWER RADIUS HOLE (FIRST LAYER) I.A.W. E.O.-64759-JIC003 REV. 1 (TASK CARD T3F18E005J6P4). (FILLER, P/N: UPR53810798200, BATCH: 0003044070, TRAVELER # T24/1786448; COVER PLATE, P/NSDR DALA2024110410589Frame · crackedCRACK ON MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00433: MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0639803)SDR HNAA2024112501132Frame · cracked53-2120 FR 59 CRACKED BTW STR15-16L. REPAIRED IAW EO1-53-24-0661SDR DALA2024110510646Frame · damagedR/H FRAME ON STATION Y1133 DAMAGED NEAR LONGERON R8. REMOVED DAMAGED FRAME REF B717 SRM 53-20-07-2R PROCEDURE 1. FABRICATED, ALODINE, PRIMED, AND PAINTED REPAIR FRAME SPLICE PARTS FOR SPLICE R4-R5 LONGERON. FRAME GOES DOWN TO PRODUCTION SPLICE RIGHT PER B717 SSDR DALA2024103010505Frame · corrodedCORROSION ON FRAME STA Y=1022 INTERSECTION WITH LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00752: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=1022 INTERSECTION WITH LONG 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 RESDR HNAA2024112501129Frame · cracked53-2047 FR25 CRACKED UNDER SILL BTW STR15-16R. REPAIRED IAW EO1-53-24-0663SDR DALA2024103110556Frame · damaged(LOG 0634725) AFT CARGO BAY FRAME DAMAGE AT STA 727J STR 25L WL 168. REPAIRED AFT CARGO BAY FRAME STA 727J AT STR 25L WL 168 IAW B737 SRM 53-60-07-2R-1.SDR R61A2024111800546Frame · crackedREF DEFECT: DMI R1008580/1: LH WHEEL WELL FR-52 CRACKED. LH WHEEL WELL FR-52 HAS BEEN REPLACED IAW SRM 51-41-01 AND SRM 51-43-03. THIS CLEARS DMI R1008580/1.SDR DALA2024103110540Frame · cracked(LOG 0631709) CRACK OF 0.625 IN LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 867 BTW S-8L & S-9L. FRAME STA 867 BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526- 01236-02A.SDR DALA2024103110539Frame · cracked(LOG 0631688) CRACK OF 0.562 IN LENGTH ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L. FRAME STA 380 BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02A.SDR DALA2024103110538Frame · cracked(LOG 0631679) CRACK OF 0.375 IN LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 827 BTW S-8L & S-9L. FRAME STA 827 BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02ASDR DALA2024103110537Frame · cracked(LOG 0631663) CRACK OF 0.281 IN LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 787 BTW S-8L & S-9L. FRAME STA 787 BTW S-8L & S-9L(REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02A.SDR DALA2024103110536Frame · cracked(LOG 0631655) CRACK OF 0.406 IN LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 500D BTW S-8L & S-9L. FRAME STA 500D BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02A.SDR DALA2024102910483Frame · gougedSHIP 6804 R/H FUSELAGE FRAME AT STA 1640 HAS A GOUGE AT STRINGER 16R ON FWD SIDE. (MARKED) REF 5311-01218-01B. CORRECTIVE ACTION: C/W ER/A 620661-14AD REV ORIGIANL SECTION I. (0632857)SDR 2024FA0000794Frame · crackedDURING HFEC INSPECTION OF FR40 LH SIDE FASTENER HOLE LOCATION, FOUND H260 WITH CRACK INDICATION.SDR DALA2024102810467Frame · crackedSHIP 3133 CRACK INDICATION WAS FOUND ON FR20LH AT HOLE IDENTIFIED AS HOLE A. CORRECTIVE ACTION: COMPLIED WITH ER/A 575137-14AD. (0631415)SDR DALA2024102810440Frame · cracked(LOG 0631268) CRACKS WERE FOUND OF 0.22IN AND 0.24IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 727B. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 727B WAS REPAIRED PER AMDS 2526-01236-02B.SDR DALA2024102810439Frame · cracked(LOG 0631106) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 867 WAS REPAIRED PER AMDS 2526-01236-02B.
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