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 AALA202404261651Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT UPPER CORNER AFT FACE AT FR 68 AND S8R. REPAIRED FRAME PER SRM 53-41-12-300-012.SDR DALA2024031503375Frame · crackedCRACK ON FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W. SUMMARY OF NRC 00705: FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1. (LP #0245021)SDR DALA2024031503367Frame Angle · crackedSHIP 188 FOUND CABIN L/H FRAME END FITTING CRACK AT STA 915. CORRECTIVE ACTION: FUSELAGE FRAME FITTING AT STA 916.4, LBL 97.42 CRACK. FABRICATED AND REPLACED AS PER PRI: 616386-14 (0243896)SDR SWIA202404290313Frame · chafedFS1144.00 STRG 9RH FRAME IS CHAFFED BY THE WATER INJECTION LINE (MARKED) (C-CHECK RO 4/26/2024) REPAIRED CHAFFE ON FRAME AT FS 1144.00 STRG 9R REF REO 670-53-61-2251 REV -- DATED 2024-04-10. ALL STEPS OF REO COMPLIED WITH. M337 AND SKYWEST TASK CARD 51-90SDR CALA2024041101029Frame · crackedLH FR 20 UPPER DOUBLE JOGGLE AREA HOLE C & 6 HAS CRACK INDIC ATIONS IN FRAME LAYER 12 OCLOCK 100% S.H AND 3 & 9 OCLOCK, 40% S. H. #C AND #D PER PART 2 OF LATEST REVISION OF EC/RA 5311-03164 ON CYCLES. REPEAT INSPECTIONS INTERVALS NOT TO EXCEED 7,300 OR BEFORESDR CALA2024040200923Frame · crackedLH FR 20 UPPER DOUBLE JOGGLE AREA HOLE C & 6 HAS CRACK INDIC ATIONS IN FRAME LAYER 12 OCLOCK 100% S.H AND 3 & 9 OCLOCK, 40% S. H. REPEAT INSPECTIONS INTERVALS NOT TO EXCEED 7,300 OR BEFORE THE AIRCRAFT REACHES 41,855 TOTAL ACFT FLT CYCLES, PERFORMED INTERIMSDR SWI2024050800379Frame · corrodedCORROSION ON FRAME FS 574.00 BETWEEN STGR 26R - 21L (C-CHECK RO 5/6/2024) REPLACED FRAME AT FS574 REF BOMBARDIER DWG 601R36024 REV N, BOMBARDIER DWG 601R35005 REV AG, BOMBARDIER DWG 601R35031 REV AG, CRJ200 SRM 51-42-06 AND SRM 51-42-21 DRAWING 601R35226SDR SWI2024050800378Frame · corroded* FRAME AT FS319 HAS CORROSION ON FORWARD SIDE BETWEEN STR27 AND STR26L. (C-CHECK RO 5/6/2024) REPAIRED FRAME AT FS319 BETWEEN STR 27 - STR 26L REF REO 601R-53-21-3684 REV - DATED 2024-03-28 AND CRJ-200-SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSSDR SWIA20240508312Frame · corroded* FRAME AT FS310 HAS CORROSION ON AFT SIDE BETWEEN STR27 AND STR26L. (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS 310 REF DRAWING 601R32002 REV AD , CRJ-200-SRM 51-42-06 AND CRJ-200-SRM 51-42-21 . COMPLIED WITH 51-900-1003-SKY AND PSDR DALA2024031303279Frame · crackedCRACK ON CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE. SUMMARY OF NRC 00232: CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #0241299)SDR IXXA2024041802Frame · corrodedALC STA 1153 RT SIDE FRAME CAP CORRODEDSDR IPXA2024041502252Frame · damagedHOLES A & S HAVE DAMAGE INDICATIONS. HOLES B, F, AND P HAVE CRACK INDICATIONS ON FR 47 LH HORIZONTAL JUNCTION. COMPLIED WITH UPS EO: EO-90000-REQ1 AND VT MAE FINAL EA 300-5710-27-A3547 REV.SDR SWAA2024040961745Stub Frame · crackedCRACK SERVICE DOOR CUT OUT STUB FRAME BS 294.5, STRINGER 17R. PERFORMED REPAIR ON SERVICE DOOR CUT OUT STUB FRAME BS 294.5 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.SDR YENA2024031200407Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND HOLE 6 AT FRAME 20RH DOUBLE JOGGLE AREA STOP FITTING N7. CRACK DIRECTION IS 10 O'CLOCK AND CRASCK DEPTH IS 0.100 INCH; (RESOLVED ON W/O: 1284156 TASKCARD: NR-00022) REF AEROMAN W.O. 2024 41/1 NR 2024- 54655 - PESDR YENA2024031200406Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND HOLE 6 AT FRAME 16LH DOUBLE JOGGLE AREA, DOOR STOP FITTING N7 CRACK DIRECTION IS 10 OCLOCK AND CRACK DEPTH IS 0.155 INCH; (RESOLVED ON W/O: 1284156 TASKCARD: NR-00023) REF AEROMAN W.O. 2024 41/1 NR 2024- 54656 -SDR YENA2024031200405Frame · damagedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND HOLE B AT FRAME 16LH DOUBLE JOGGLE AREA, DOOR STOP FITTING N7. CRACK DIRECTION IS 9:00 & CRACK DEPTH IS 0.100 INCH; (RESOLVED ON W/O: 1284156 TASKCARD: NR-00024) PERFORMED REPAIR ON HOLE B FRAME 16LH DOUBLE JOGGSDR CALA2024031200692Frame · corrodedLH FR 16 UPPER DOUBLE JOGGLE AREA HOLE ''A'' HAS CRACK INDICATION IN FRAME LAYER, 5 OCLOCK, 100% S.H GENERATED BY V892444 ON HAECO LCQ NR 9296308/32308SDR SWAA2024040961301Frame · crackedCRACK FRAME ON BS 312 AT UPPER CHORD AND LBL 33 AND BETWEEN S-5L TO S-6L FWD GALLEY . PERFORMED REPAIR ON FRAME ON BS 312 AT UPPER CHORD AND LBL 33 AND BETWEEN S-5L TO S-6L FWD GALLEY IAW EA M-22-153-01244.SDR CALA2024031300709Frame · damagedUPON REMOVAL OF CLEVIS FITTING AT 500C L/H SIDE, FOUND 1 EA. DRILL START AT LOWER OUTBOARD FASTENER HOLE.SUPPORT TASK NSA EMX N/R 00156.SDR YENA2024031200386Frame · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FRAME 80 BTW STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; CMOR:REMOVE CORROSION, EVALUATE AND IF IT IS NECESSARY REPAIR PER EMB-190 SRM 51-12-01, SRM 51-10-03, ETI-190-24-036. REV. 2SDR YENA2024031200372Frame · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTWN STR 27R-28R / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)SDR DALA2024031103205Frame · crackedSHIP 6821 AA/AD 03 CRACKS WERE FOUND OF: 1) 1.400 IN. 2) 0.100 IN. AND 3) 0.180 IN. LENGTH ON FRAME STA 1380 INNER CHORD BTW STRINGER 27 RH AND 26 RH AT AFTER CARGO COMPARTIMENT (IN REFERENCE JOB# 027- 0001. CARD. 5311-01217-03). CORRECTIVE ACTION: SUMMARY OF SDR SWAA2024041160921Frame · crackedCRACKED FRAME LOCATED BS 259.5 BETWEEN S-10L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW LBL 20 AND LBL 50 IAW EA# 24-153-00698-WIP1 AND EA# 24-153-00698.SDR SWAA2024041160922Frame · crackedCRACKED FRAME ON BS 907 BETWEEN S-25R TO S-26R AFT CARGO COMPARTMENT. REPLACED FRAME AND FASTENER LOC. BS 907 BTW STRINGER 25R TO STRINGER 24L AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 147A1007 SHEET 42 REV:D AND DWG 147A0002 SHEET 87 REV-.SDR SWAA2024041160925Frame · crackedCRACK FRAME ON BS 947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT. REPLACED THE FRAME LOC. BTW STRINGER 25L TO STRINGER 26R BS 947.5 AND FASTENERS LOC. BS BS 947.5 BTW STRINGER 24R TO STRINGER 24L IAW SRM 51-40-02 AND DWG 147A8110 SHEET 41 REV:A AND DWG 147A004SDR SWAA2024040960789Stub Frame · crackedCRACK SERVICE DOOR FWD UPPER CORNER STUB FRAME AT STA 294 AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED SERVICE DOOR FWD UPPER CORNER AT STA 294 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A8370 SHEET 10 REV SDR SWAA2024040460492Frame · crackedSTATION 312 FRAME IS CRACKED IN RADIUS ABOVE L1 DOOR CUT-OUT.<[01] VERIFIED STEP 1 COMPLETE.;[02] REPAIRED BS 312 FRAME IAW EA: M-22-153-01244;[03] VERIFIED STEPS 1;2 COMPLETE; CORRECTION ACTION ITEM 2 AND MEASUREMENT TABLE; CARD COMPLETE.SDR HNAA2024032700230Frame · crackedE026728 FR 66 CRACKED STGR 17L-18L BELOW CARGO DOOR SILL. RAR LOWER FR 66 IAW EMB 145 SRM 51-40-02.SDR DALA2024031103204Frame · crackedSHIP 5645 LEFT HAND SIDE STA 1640 FRAME AT STR 14L LOWER I/B OPEN HOLE HAS (2) INDICATIONS OF DEFECTS NOTED AT THE 3 OCLOCK (OUTBD) AND 9 OCLOCK (INBD) POSITION LOOKING AFT. INDICATION (CRACK) IS ESTIMATED IN THE FRAME LAYER AT OVER .100" IN LENGHT IN BOTH DIRSDR 2024F00059Frame · crackedL/H FUSELAGE FRAME AT STA 840 BETWEEN STR8L AND STR9L HAS A CRACK.SDR 2024F00058Frame · crackedR/H FUSELAGE FRAME AT STA 800 BETWEEN STR8R AND STR9R HAS A CRACK.SDR 2024F00057Frame · crackedL/H FUSELAGE FRAME AT STA800 BETWEEN STR8L AND STR9L HAS A CRACKSDR 2024F00056Frame · crackedR/H FUSELAGE FRAME AT STA760 BETWEEN STR8R AND STR9R HAS A CRACKSDR 2024F00055Frame · crackedL/H FUSELAGE FRAME AT STA 760 BETWEEN STR8L AND STR9L HAS A CRACK.SDR 2024FA0000208Frame · gougedR/H FUSELAGE INTERIOR FRAME AT STA 1280 STR14R HAS 3 GOUGE MARKS POSSIBLE INTERIOR BINS NOT PROPERLY INSTALLED.SDR 2024F00054Frame · gougedL/H FUSELAGE INTERIOR FRAME AT STA440 STR8L HAS A GOUGE FROM IMPROPER OVERHEAD BIN INSTALLATION.SDR SWIA202404250318Frame · corroded(MX# 27918611) MULTIPLE SPOT OF CORROSION ON FS280.00 FRAME AFT WEB BETWEEN STGR 25L TO 25R. (MARKED) (C-CHECK RO 4/24/2024) REPAIRED FS280.00 FRAME AFT WEB BETWEEN STGR 25L TO 25R (2EA SPOTS). COMPLIED WITH ALL STEPS OF REO 670-53-11-1931 REV -- DATE 2024SDR SWAA2024041160195Frame · crackedCRACK ON FRAME BS 259.5 BETWEEN STRINGERS 9R - 10R IN THE PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME IAW EA 24-153-00687-WIP1 AND EA 24-153-00687.SDR IPXA2024040846502Frame · damagedDAMAGE FOUND ON BOTTOM HOLE ON FR 40 RH LOWER JUNCTION FASTENERS. COMPLIED WITH UPS EO-89994-REQ1 AND VTMAE FINAL EA 300-5710-27-A3542 REV-.SDR GTIA2024030837974Frame · crackedCRACK FOUND ON FR 43 RH STR 22 MEASURING .2465" L X .2465" W X RAF 01.-ACCOMPLISHED REPAIR OF FR43 FOOT RH CRACKED HOLE PER REO L24904 EA 5331-2430 INSTRUCTIONS CAT A NO REINSPECT PER RDAS 81356958/004/2024 #A REF NR 122190-34252 FOR RFTS 60005SDR DALA2024030803166Frame · crackedFUSELAGE FR 16 RH, DOUBLE JOGGLE CRACK HOLES #15, #16, AND #17. REPAIRED BY ERA 611708-14AD. (0234452)SDR DALA2024030803165Frame · crackedFUSELAGE FR 16 RH, DOUBLE JOGGLE FR 2 TO FR 3 CRACK HOLES #7, #8, #9, AND #10. REPAIRED BY ERA 611708-14AD. (0234440)SDR DALA2024030803164Frame · crackedFUSELAGE FR 16 RH, DOUBLE JOGGLE CRACK HOLES #5 AND #6. REPAIRED BY ERA 611708-14AD. (0234429)SDR VNAA202403070014Frame · corrodedFS 319.70 FRAME IS CORRODED BETWEEN STGR 25L AND STGR 27. REPAIRED FS 319.70 FRAME IAW CRJ-900 SRM 53-00-06-201-001-A03 SH670-31355-1SSDR 2024F00052Frame · crackedFRAME 5 FOUND CRACKED AT MOUNTING LOCATIONS FOR METRO AFT MED WALLSDR VNAA202404150004Frame · corrodedCORROSION ON FRAME FS= 319.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 349.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PSDR SWAA2024041059857Frame · crackedCRACK FRAME STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN 2024-165776<[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 LOCATEDSDR GRTA20240315003Frame · crackedFRAME CRACKED CENTER LINE ABOVE BELLY SKIN @ APPROXIMATE F.S. 167.625. REPAIRED IAW SIRM 20-10-34.SDR GRTA20240315002Frame · crackedFRAME CRACKED AT FS 236.5 BETWEEN STRINGERS 12L AND 13L. REPAIRED IAW KING AIR SIRM 20-10-34.SDR DALA2024030803152Frame · corroded(LOG 0232684) AFT CARGO COMPARTMENT STA 767 BETWEEN STGR 28R AND STGR 29R, FRAME WITH CORROSION. AFT CARGO COMPARTMENT STA. 767 BATEEN STG. 28/29RH ON THE FRAME WAS PERFORMED TO REWORK AND TO NDT INSPECTION NTM PART 6 51-00-00 PROCEDURE 23 REV.142 NOV. 01, 202
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