JASC 5311
Service difficulty reports · 61,549
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 SWAA2020030642203Frame · corroded***CORROSION*** ON FRAME BS 887 LBL 25 BETWEEN STR 24L AND 25L WL 156 DUE TO BLUE WATER SPILL REPAIRED PER: EA 1-753-36628 REV IR AND ATS ER 20-01497 REV IRSDR SWAA2020030642202Frame · corroded***CORROSION*** ON FRAME BS 887 LBL 11 AFT SIDE OF FRAME WL 156 DUE TO BLUE WATER REPAIRED PER: EA 1-753-36628 REV IR AND ATS ER 20-1497 REV IRSDR SIMA2020021830006Frame · crackedIN COCKPIT ZONE 225 (TOP L.H SIDE ABOVE PILOT HEAD), ONE FRAME IS CRACKED-C/A-OVERHEADCIRCUIT BREAKER PANEL REMOVED FOR SHEET METAL ACCESS IN COCKPIT ZONE 225 (TOP L/H SIDE ABOVE PILOT HEAD) ONE FRAME REPLACED IAW SRM 51-40-02. OVERHEAD CIRCUIT BREAKER PANEL RSDR REXA202002050166Frame · corroded"FRAME IS CORRODED AT F.S. 319 BETWEEN STR 25R AND 25L.
""REMOVED AND REPLACED FRAME AT F.S. 319 BETWEEN STR 25L AND 25R IAW CRJ900 SRM 53-00-06-201-006-A01. WVAC STAMP EMP# 771 MTC
"SDR DALA2020020130773Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 943 LH SIDE. (CPAX) RING PAN UPPER FWD EDGE AT STA Y= 943 LH WAS REPAIRED PER MD-90 SRM 56-20-02 VOL. I PAR. 3 FIG. 2 (1468779)SDR SWIA2020030348967Frame · corrodedCORROSION ON FS349.00 FRAME LOWER FLANGE FROM 25L TO 25R (C-CHECK) RO 2/28/2020 REPLACED FRAME SECTION PN:601R32005-69 AT FS349 REF DWG, CRJ200 SRM. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD.SDR RAIA202002060001Frame Angle · crackedCRACKED SIDEWALL VERTICAL FRAME IN COCKPIT AREA AT ATTACHMENT TO WINDOW LOWER HORIZONTAL FRAME COUPE RAIL AT RIVET LOCATION----REMOVED AND REPLACED VERTICAL FRAME WITH NEW ITEMSDR DALA2020020300805Frame · dented(AIRCRAFT 5655, L/P 1467164) DENT ON FRAME STA 1400 BTW STGR 27L AND 26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-07-2R REPAIR. 5.SDR DALA2020013000702Frame · damagedFRAME 35 COLDWORK HOLE A AND HOLE B REPAIR IN ACORDENCE WITH WORD CARD 5311-01171-03A TO FURTHER FLIGHT AA5311-01171, SB A320 -53-1264, AD-2018-06-04 LOG-PAGE UPDATED @ 29JAN20 1705 UTC 02 CORR BY VASQUEZ DO 00691739 SAL 29JAN20 ATA 5311 ENTR 00527653 W LOG-PASDR DALA2020020390802Frame · dented(AIRCRAFT 5655, L/P 1465980) DENT ON FRAME STA 1580 BTW STGR 25R AND 26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-07-2R REP. 5.SDR DALA2020020390801Frame · dented(AIRCRAFT 5655, L/P 1465976) INITIAL INSPECTION: DENT ON FRAME STA 1420 BTW STGR 27L AND 26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-00-07-2R REP. 5.SDR DALA2020013190748Frame · dentedDURING INSPECTION, FOUND A DENT ON FRAME BS 727I, STRINGER 25R IN THE AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-60-07-2R.SDR SWAA2020022641690Frame · crackedFRAME INBOARD RADIUS CRACKED AT BS. 312, STRINGER 5L. / REPAIRED FRAME IAW IR & EA.SDR FDEA202001270229Frame · corrodedR/H SIDE LOWER HOLE AT FR40 HAS CRACK INDICATION, IN BORE, SHOWING AT THE 3 O'CLOCK POSITION LOOKING OUTBOARD, HOLE DEPTH MEASURES FROM 0.921" TO 0.990" FROM EDGE OF RECESS REAMED HOLE TO .6324 PER A300-600 SRM 51-40-44. INSTALLED BUSHES(3EA), WASHERS (2EASDR DALA2020012800636Frame · crackedINITIAL INSPECTION: CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE. (CPAX) . SUMMARY OF NRC 00283:RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE WAS REPAIRED PER MD90-SRM VOL I 56-20-02 PAR. 3 FIG. 2. (LP# 1463818)SDR R61A202002140170Frame · corrodedMAJOR: CORROSION FWD WET AREA FRAME 17 RH SIDE COMPLIED WITH CUTOUT AND PERMINANT REPAIR OF FR17 RH SIDE REF. SRM 53-00-10/REPAIR03P RESTORED SURFACE PROTECTION REF. SRM 51-23-06SDR DALA2020020370799Frame · cracked(AIRCRAFT 5801, L/P 1462772) INITIAL INSPECTION: CRACK ON FRAME STA 780 + 20 BTW S-8R AND S-9R AT PAX CABIN. CORRECTIVE ACTION: REPAIR ACCP PER B757-300 SRM 53-00-07 REP 8.SDR DALA2020020370798Frame · cracked(AIRCRAFT 5801, L/P 1462538) CRACK ON FRAME STA 780 + 20 BTW S-8L AND S-9L AT PAX CABIN. CORRECTIVE ACTION: REPAIR ACCP PER B757-300 SRM 53-00-07 REP 8.SDR CALA2020020200281Frame · dentedB757-06-3-0230 DENT ON FWD CARGO FRAME UPPER FLANGE STA 660BETWE EN STRINGER 24 AN STRINGER 25 (034-038) LH SIDE REF ST ENG N/R 0 085668 FOUND DENT OUT OF LIMITS IAW B757-200 SRM 53-00-07 FIG 101 L=1.1 0, W=.90, D=.047. CUT OUT DAMAGE AND ACCOMPLISHED CATEGORYSDR DALA2020012960672Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE. (CPAX) SUMMARY OF NRC 00293: RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE WAS REPAIRED PER MD 90 VOL I SRM 56-20-02 TYPE C FIGURE 3SDR SIMA202001276001Frame · crackedDURING HMBV INSPECTION, QA FOUND FRAME 66 IS CRACKED AT STRINGER 16R. -C/A-REMOVED AND REPLACED FRAME 66 IAW EMB 145 SRM 51-40-02.SDR SWIA2020030549013Frame · corrodedEVIDENCE OF CORROSION ON FRAME AT STR 21 TO 20 AT FS 319 (C-CHECK) RO 3/3/2020 REMOVED AND INSTALLED NEW FRAME P/N SH670-31891-3 REF CRJ900 SRM AND BOMBARDIER DWG. NO LEAK NOTED. COMPLIED WITH TASK CARD AND MAJOR REPAIR M-337SDR DALA2020012960671Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1231 RH SIDE. (CPAX) SUMMARY OF NRC 00284: RING PAN UPPER AFT EDGE AT STA Y= 1231 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2SDR DALA2020012960670Frame · crackedCRACK ON RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH SIDE. (CPAX) RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461639)SDR DALA2020012960669Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1250 RH SIDE. (CPAX) SUMMARY OF NRC 00294 RING PAN UPPER AFT EDGE AT STA Y= 1250 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461632)SDR DALA2020012960668Frame · crackedCRACK ON LOWER AFT RING PAN STA Y= 332 AND 636 AT PAX CABIN SUMMARY OF NRC 00135 LOWER AFT RING PAN STA Y= 332 AND 636 WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 LOG-PAGE UPDATED (1461624)SDR CALA2020020210270Frame · corrodedCORROSION ON AFT CARGO FRAME FWD SIDE AT STA 1560 BETWEEN STR 27 R-29R. REF ST-SAA NR 0084433. REMOVED AND CHECKED LIMITS TO CORROSION AT AFT CARGO FRAME, FWD SIDE AT STA 1560 BETWEE S-27R AND S-29R; L= 5.0", W= 2.0" D= .01 2". ORIGINAL MATERIAL THICKNESS IS .SDR DALA2020012500594Frame · crackedCRACK DETECTED ON UPPER CANTED FRAME AT 2 0'CLOCK. REMOVED UPPER CANTED FRAME AND DRILLED REPLACEMENT CANTED FRAME. (398826). INSTALLED REPLACEMENT FRAME IAW BOEING DRAWING 9911843. (LP1460279)SDR DALA2020012500593Frame · crackedCRACK DETECTED ON LOWER CANTED FRAME AT 7O'CLOCK. REMOVED LEFT CANTED FRAME. DRILLED UP REPLACEMENT CANTED FRAME. BEGAN INSTALLING LEFT CANTED FRAME. COMPLETED LEFT CANTED. (LP1460270)SDR SWIA2020031049228Frame · corroded*FRAME 513.00 HAS HEAVY CORROSION PITTING FROM APPROXIMATELY STGR 4RH €“ STGR 7RH (MARKED) (C CHECK) RO 3/7/2020 BLENDED OUT CRROSION ON FS 513 FRAME RH AT STRINGER 4R TO 7R AND FOUND ACCEPTABLE TO ENGINEERING REF REO.SDR DSCR2020022713438Frame · crackedTHE FRAME 5A HAS CRACK ON THE RH SIDE, UPPER DOUBLER EXTENDING FROM EDGE TO RIVET HOLE.SDR REXA2020012820074Frame · corroded"INITIAL INSPECTION. CORROSION ON FRAME FS 319, STRG 25L-25R AT MAIN AVIONICS COMPARTMENT.(TCI 100-09).
"FRAME FS 319, STRG 25L-25R, WAS REPAIRED PER EA NO: CRJ953-10198 REV IR. (LEVEL CORROSION 2) SDR DALA2020012300567Frame · crackedDURING INSPECTION FOUND CRACK ON FWD FRAME OF FWD SERVICE DOOR CUTOUT STA 294 AND LONGERON PROJECTION 17RH AT PASSENGER CABIN. FRAME OF FWD SERVICE DOOR CUTOUT STA 294 AND LONGERON PROJECTION 17RH AT PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-10-15 REPAISDR VNAA2020012299906Frame · corrodedFS 349 FRAME CORRODED AT STR 27 AFT SIDE. REMOVED CORRODED FRAME SEGMENT AT FS 349.00 FROM STRINGER L23 TO R24 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE FRAME SEGMENT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-ASDR VNAA2020012299903Frame · corrodedFS 310 STR 26L - 26R CORRODED ON FWD AND AFT SIDES OF FRAME. RMEOVED DAMAGED SECTION OF FS 310 IAW SRM 53-00-06-201-006-A01. INSTALLED NEW SERVICEABLE FRAME SECTION IAW SRM 53-00-06-201-006-A01. PERFORMED EDDY CURRENT OF FS 310 FRAME CUTLINE EDGES IAW SDR SWIA2020031049214Frame · corroded*FS605.00 FRAME IS CORRODED FROM LH STGR25 TO RH STGR24. FAGGED & CIRCLED WITH GREASE PENCIL. (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON FS 605 LOWER FRAME AS MARKED BETWEEN STRINGER 25L TO 24R REF CRJ 200 SRM. ORIGINAL THICKNESS OF FS 605 LOWER FRAMSDR DALA2020012720603Frame · crackedCRACK FOUND ON FRAME AT BS 1540, BETWEEN STRINGERS 8R AND 9R IN THE PASSENGER CABIN. REPAIRED IAW SRM 53-00-07-2R-8. AND PERFORM REPETITIVE DETAIL VISUAL INSPECTION AT INTERVAL EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, OR 50,000 AIRFRAME FLIGHT CYSDR DALA2020012720602Frame · crackedCRACK FOUND ON FRAME AT BS 1520, BETWEEN STRINGERS 8R AND 9R IN THE PASSENGER CABIN. REPAIRED IAW SRM 53-00-07-2R-8. AND PERFORM REPETITIVE DETAIL INSPECTION AT INTERVAL EVERY 12,000 FLIGHT CYCLES OR 50,000 AIRFRAME CYCLES, WHICHEVER COME FIRST PER B757-200 SDR CALA2020012600237Frame · dentedTWO DENTS FOUND ON THE AFT CARGO FRAME UPPER FLANGE AT BS 1400 BETWEEN STRINGERS 25L - 26L. DENTS NOT PERMITTED ON FLANGE IAW SRM 53-00-07, FIG 101. ACCOMPLISHED ECRA NO. 5311-02371 PART 1, INTERIM REPAIR. ECRA NO 5311-002371 PART 2, INSEPCTION REQUIREMENT SDR DALA2020012410547Former · corrodedFORMER AT FRAME 1002 AND FRAME 1002 CUT AND REMOVED DUE TO CORROSION. REPLACED FRAME 1002 BETEEN STRINGER L21-30 AND SPLICE AT L21 IAW B717 SRM 53-20-07-2R-3. RII COMPLETED BY QC2037. (LP #1455181)SDR DALA2020012200507Frame · crackedCRACK FRAME 3 RACK 10VU CENTER LUG IN COCKPIT WORK CARD 2511-01146-01, AD 2019-07-05, REPAIRED IN ACCORDANCE WITH AD 2019-07-05 AND AIRBUS SB A320-92-1087 REV.3 CRACK LENGTH 0.532SDR DALA2020012210483Frame Angle · damagedAT BS 1002 BETWEEN STRINGER 29 AND 30L, THERE IS A FRAME SPLICE ANGLE WITH DAMAGE BEYOND LIMITS. REPLACED FRAME ANGLE IAW SRM 51-41.SDR VNAA2020022999910Frame · corrodedIB AND ATTACH ANGLES ON BOTTOM OF KEEL BEAM FOUND TO BE CORRODED.REPAIR OR REPLACEMENT REQUIRED.SDR SWIA2020030348959Angle · corroded*CORROSION ON ANGLE ON THE FORWARD SIDE OF FRAME FS394.00, STGR25L - STGR25R. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED NEW ANGLE PN: 601R32011-45. REMOVED AND INSTALLED NEW ANGLE REF SRM, DWG, CRJ200 SRM. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK SDR VNAA202002299999Frame · corrodedKEEL BEAM IN MLG WHEEL WELL HAS CORROSION ON THE BOTTOM AND NICKS ON EDGE.REMOVED CORROSION ON KEEL BEAM ASSY IAW CRJ 700 SRM 51-21-06-001-001-A01,SDR VNAA202002299995Frame · crackedFLIGHT DECK FLOOR BEAM AT LBL 11 IS CRACKED WHERE F.S. 280 CROSSBEAM ANGLE ATTACHES. LOCATED, DRILLED & INSTLLED NEW SERVICABLE ANGLE IAW CRJ 700 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01.SDR DALA2020012000387Frame · crackedCRACK INDICATION ON FRAME 36 THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35L AND FR36L. ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. AA 5311-01171. SB A320-53-1263. AD-2018-06-04. IN FWD CARGO CSDR DALA2020012000386Frame · crackedCRACK INDICATION ON FRAME 36 LT SIDE IN OPEN O/B HOLE A. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT, AA 5311-01171, SB A320-53-1264, AD-2018-06-04 IN AIR CONDITIONING BAY (2 EA) D=0.135 INCH. (CRACK DIRECTIONS 6 AND 12 O CLOCK VSDR DALA2020012000402Pickle Fork · not reportedC/W LT AND RT PICKLE FORK FITTING REPLACEMENT SUPPORT AND ACCESS REF ERA 584218-14 PRI REV 1. C/W PRI 584218-14 REV 0,1 AND 2. RECEIVED ERA 584218-14 REV ORIGINAL AND REV A. PRI 584218-14 REV 0,1 AND 2 AND ERA 584218-14 REV ORIGINAL AND REV A MATCH. REPAIRED PSDR DALA2020012000397Pickle Fork · crackedWHILE PERFORMING J/C 5300-01157-01B INSPECTION OF RT PICKLE FORK FOUND CRACK EXTENDING THRU FASTENER. NO VISIBLE CRACK ON FAIL SAFE STRAP. LEFT AND RIGHT PICKLE FORK REPLACEMENT COMPLIED WITH REF ERA'S 584218-14AD REV ORIGINAL, 584219-14AD REV A, 584220-14AD R
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