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.

SDR DALA2023030101544None · noneSHIP 5640 COMPLY WITH ERA 606327-14AD REV. A SECTION 1 FRAME HARDWARE INSTALLATION. CORRECTIVE ACTION: COMPLIED WITH ERA 606327-14AD REV. A SECTION 1. (2648245)Feb 27, 2023 · N540US · Boeing 757251SDR DALA2023030101534None · none(LOG 2647730) DURING INSPECTION FOUND REAR SERVICE DOOR HAS CORROSION ON MOP SILL, STA 967-992, RBL 45. ACCOMPLISHED REPAIR TO REAR SERVICE DOOR MOPSILL STA 967-992 RBL 45 IAW DELTA ER/A 606187-14 REV ORIGINAL.Feb 27, 2023 · N952DJ · Boeing 7379SDR SWIA20230200025Unknown · damaged2 MISS DRILLED HOLES IN THE FWD I/B CORNER OF THE R/H WEB FR 12 (C-CHECK RO 3/11/2023) REMOVED AND REPLACED FWD I/B BEAM BETWEEN FR12-13. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.Feb 25, 2023 · N211SY · Emb ERJ170200LRSDR SWIA2023011225None · corroded*CORROSION IN THE RADIUS OF STGR20L UPPER END CLIP JUST AFT OF FS559.00+112 (MARKED) (C-CHECK RO 3/7/2023) REMOVED AND REPLACED STRINGER 20L CLIP AFT FS 559+112 REF CRJ 200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31057 REV. J. COMPLIED WITH 51-90Feb 25, 2023 · N461SW · Cndair CL6002B19SDR SWIA20230201025None · corroded*CORROSION IN THE RADIUS OF STGR19L UPPER END CLIP JUST AFT OF FS559.00+112 (MARKED) (C-CHECK RO 3/7/2023) REMOVED AND REPLACED STRINGER 19L CLIP AFT FS 559+112 REF CRJ 200 SRM 51-42-06 , AND CRJ 200 SRM 51-42-21 AND DWG 601R31057 REV. J. COMPLIED WIFeb 25, 2023 · N461SW · Cndair CL6002B19SDR CALA2023022700557Nut Plate · corrodedFR68 LH FWD FACE AT NUT PLATE HOLE HAS CORROSION PER HAECO LCQ N R 9298794/20794 GENERATED BY V061680 SPEC: A3NB-53-3-6222. = .030", REM''ING MTL = .068", MAX ALLOWABLE REM''ING MTL = .050", HFEC AND ROTO INSPECTED AREA AND NUT PLATE HOLE IAW 51-10-08 REPAIR FFeb 25, 2023 · N892UA · Airbus A319132SDR CALA2023022700555Frame · dented(B757-06-3-0230) FWD PIT RH SIDEWALL AREA,FUSELAGE FRAME UPPER FLANGE IS DENTED IN 2EA LOCATIONS AT STA 680 BETWEEN S24R AND S25R (MARKED).TRANSCRIBED BY HAECO GSO NR9284523. DOT: X366Feb 25, 2023 · N13110 · Boeing 757200SDR DALA2026021701089Frame · dentedON WALKAROUND, FOUND TWO DENTS ON THE FRAMES OF AFT OF RADOME ON RT SIDE OF FUSELAGE. REPAIRED PER ER/A 606387-14 REV A, PRI REV .1, WAITING ON ABC RVSM SKIN CONTOUR RESULTS AND FINAL ER/A. ( 00127702 10FEB26 07:45 UTC) (ETS WIP) MECHANIC : ACCOMPLISHED ERA 60Feb 24, 2023 · N308DU · Airbus BD5001A11SDR DALA2026021701088Frame · dentedTWO DENTS ON FRAMES AFT OF RADOME ON RT SIDE OF FUSELAGE. C/W ERA 606387-14, REV ORIG, SECTION 1, OMITTED STEP 4 FOR TIME. ER/A PERMANENT REPAIR MUST BE DONE PRIOR TO CLOSING LOG 23 FEB, 2023 FLT 2477, REP 850 TER 8500 APPROVED PER DAL P.S. 900-5-1 NO 4. ACCOFeb 24, 2023 · N308DU · Airbus BD5001A11SDR DALA2023022801498None · noneSHIP 3265 FR 68 DOOR-STOP FITTING HAS CRACK INDICATION AT HOLE #2. CORRECTIVE ACTION: COMPLIED WITH ER/A 606329-14AD, REV. ORIGINAL. (2643120)Feb 24, 2023 · N365NW · Airbus A320212SDR DALA2023022801497None · noneSHIP 3265 AFT RIGHT DOOR, AFT FRAME 68, BOTTOM DOOR STOP LOOSE WITH SHEARED BOLTS. CORRECTIVE ACTION: COMPLIED WITH ERA 606329-14AD, REV. ORIGINAL. (2643102)Feb 24, 2023 · N365NW · Airbus A320212SDR DALA2023022801495None · noneSHIP 3265 RH FR68 #1 DOOR-STOP FITTING, HOLE #4 HAS A CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 6060329-14AD, REV. ORIGINAL. (2643131)Feb 24, 2023 · N365NW · Airbus A320212SDR DALA2023022801494None · noneSHIP 3265 RH FR 68 #1 DOOR-STOP FITTING, HOLE #3 HAS A CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 606329-14AD. (2643127)Feb 24, 2023 · N365NW · Airbus A320212SDR DALA2023022801493None · noneSHIP 3265 HOLE #1 HAS CRACK INDICATIONS DURING ROTARY SCAN AT #2 DOOR-STOP FITTING FR68. CORRECTIVE ACTION: COMPLIED WITH ERA 606329-14AR, REV. ORIGINAL. (2643114)Feb 24, 2023 · N365NW · Airbus A320212SDR V0XD20230406003Frame · chafedCHAFFING AND ARCING DAMAGE TO FRM 3 BETWEEN STGR 15R-17R, FWD ELECTRONICS BAY. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR DOUBLER AT FRM 3 BETWEEN STGR 15R-17R IAW ETD2023-145-007395 REV 1. SEE AVMAX WO: 81033 WC: 1109.Feb 23, 2023 · N15986 · Emb EMB145LRSDR DALA2023022401387None · noneSHIP 3265 AFT FUSELAGE / FR68 RH / DOOR-STOP FITTING #1 / HOLE DAMAGE / AD 2018-03-12. CORRECTIVE ACTION: COMPLIED WITH ERA 606329-14 AD. (2642329)Feb 23, 2023 · N365NW · Airbus A320212SDR SWAA2023040509431Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 LT SIDE CENTER SECTION 2023-142557<[01] REPLACED ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 BL 0 LT SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: AFeb 22, 2023 · N212WN · Boeing 7377H4SDR DALA2023022301374None · noneAIRCRAFT 3122, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA LH SIDE IN INBOARD VERTICAL FLANGE FROM UPPER TENSION BOLT TO UPPER RADIUS, CRACK LENGTH IS 0.180 INCH APPROX, IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 6Feb 22, 2023 · N322NB · Airbus A319114SDR DALA2023022401393Web · corroded(LOG 2638967) DURING INSPECTION FOUND CORROSION CORROSION ON FWD CARGO COMPARTMENT SUB THRESHOLD WEB STA 440-500 LBL 29 WL 156. REMOVED AND REPLACED FWD CARGO COMPARTMENT SUB THRESHOLD WEB STA 440-500 LBL 29 WL 156 PER B737 S.R.M 51-40-02-0G PARA 5B AND DWG# 1Feb 21, 2023 · N952DJ · Boeing 7379SDR DALA2023022201324None · noneSECONDARY IN REF TO AMDS 5310-01436-01A: CRACK ON CUSP MEMBRANE WEB AT STA 674 L-18 LH. SUMMARY NRC 00198: CUSP MEMBRANE WEB AT STA 674 L-18 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2637942)Feb 21, 2023 · N952AT · Boeing 717200SDR DALA2023022201335None · noneSHIP 5639 VIASAT SYSTEM INSTALLATION AT FS 1280 FRAME. CORRECTIVE ACTION: REF ERA 606173-14. (2637435)Feb 20, 2023 · N539US · Boeing 757251SDR DALA2023022201323None · noneCORROSION ON CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55. SUMMARY OF NRC 00519: CUSP WEB WAS FABRICATED PER DWG 9936535 REV CS AND CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55 WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4, 51-41-05-0G PFeb 20, 2023 · N893AT · Boeing 717200SDR DALA2023022201321None · noneSECONDARY NRC, IN REF NRC 00618: CORROSION ON MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH. SUMMARY OF NRC 00650: CORROSION LEVEL 2. REPAIR OF MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH WAS PERFORMED PER B-717 SRM 53-00-55-2Feb 19, 2023 · N893AT · Boeing 717200SDR DALA2023022001259None · noneSECONDARY NRC IN REF NRC #00493: SEVERAL DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)=15 TO (-X)=42. SUMMARY OF NRC 00660: DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)= 15 TO (-X)=42 WERE REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2636349)Feb 19, 2023 · N893AT · Boeing 717200SDR DALA2023022001258None · noneCRACK ON CUSP MEMBRANE WEB AT STA 696 L-18 LH. SUMMARY OF NRC 0209: CUSP MEMBRANE WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2636060)Feb 19, 2023 · N952AT · Boeing 717200SDR DALA2023022001257None · noneA.A. A.D. CRACK WAS FOUND OF 0.437" LENGTH ON FRAME STA Y=715 RH SIDE IN REF CARD 5310-01436-04D JOB #074-0004 STEP: 13. SUMMARY OF NRC 00329: FRAME STA Y=715 RH SIDE WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G IN REF. A.A. WORK CARD: 5310-01436-03B.Feb 18, 2023 · N893AT · Boeing 717200SDR ABXA2023051195Frame · dentedDURING THE MAINTENANCE AIRCRAFT INSPECTION, A DENT DAMAGE WAS FOUND ON THE WTB UNDERWING STRUCTURE FAIRING FRAME (19T7300-5) APPROXIMATELY AT BS 779. THE DENT DAMAGE IS ON AREA WHERE NO DAMAGE IS ALLOWED. FOR DENT DETAILS SEE FIGURE 2 AND FIGURE 3. CPZ AND ABXFeb 17, 2023 · N362CM · Boeing 767338SDR SWIA20230217None · corrodedFWD FUSELAGE HAS LIGHTNING STRIKE ABOVE STGR 19R AFT OF FR 04 AS MARKED (C-CHECK RO 3/6/2023) REPAIRED DAMAGE AT STGR 19R AFT OF FR 04, BY DRILLING HOLE AND INSTALLING REPAIR FASTENER AND WASHER. REF EMB ETD2023-170-004756 REV.A NO WEIGHT INCREASE DUE TFeb 17, 2023 · N176SY · Emb ERJ170200LRSDR AALA202302206208Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FOOT COUPLING FASTENER HOLE AT FR 43 BETWEEN S21R AND S22R. MAINTENANCE REPLACED FRAME PER EA 341803.Feb 17, 2023 · N109UW · Airbus A320214SDR DALA2023022101286None · noneSHIP 5812 AFTER COCKPIT WINDSHIELD NO. 3 RH REMOVAL, CORROSION WAS FOUND IN CUTOUT OF WINDSHIELD (FRONT UPPER AREA). IN REF NRC 028. CORRECTIVE ACTION: SUMMARY OF NRC 00260: CUTOUT OF WINDSHIELD (FRONT UPPER AREA) WAS REPAIRED PER PRI 606122-14 REV 0, REV 1 ANFeb 16, 2023 · N592NW · Boeing 757351SDR DALA2023021701231None · noneA.A. A.D. CRACK WAS FOUND OF 0.250" LENGTH ON FRAME STA Y=737 RH SIDE IN REF CARD 5310-01439-01D JOB# 094-0004 STEP: 4. SUMMARY NRC 00154: OVER WING FRAME STA Y=737 BTW LONG 8 TO 18 RH WAS REPLACED PER WORK CARD 5310-01439-02B. ASSOCIATED AA 5310-01439 ADDED FFeb 16, 2023 · N894AT · Boeing 717200SDR DALA2023021701229None · noneCRACK ON INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22, PASSENGER CABIN. SUMMARY OF NRC 00442: INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1. (LP #2631096)Feb 16, 2023 · N894AT · Boeing 717200SDR DALA2023021701228None · noneSEVERAL HIDDEN CRACKS ON RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 IN REF NRC 00154. SUMMARY OF NRC 00514: RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2 R REP 4 PAR 5 FIFeb 15, 2023 · N894AT · Boeing 717200SDR DALA2023021501184Unknown · unknownCORROSION ON SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT. SUMMARY OF NRC 00331: CORROSION LEVEL 2. SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2629599)Feb 15, 2023 · N893AT · Boeing 717200SDR DALA2023021501196None · noneSHIP 3236 LHS AT S-22L (DOOR STOP #1) CRACK. CORRECTIVE ACTION: COMPLIED WITH AA 5311-01244. OK FOR SERVICE. (2628034)Feb 14, 2023 · N336NW · Airbus A320212SDR VGCA20230213002Stub Frame · damagedMISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95Feb 13, 2023 · N215WE · Boeing 7272S2FSDR VGCA20230213001Frame · scratchedDAMAGED HOLE / DEEP SCRATCH AT THE LOWEST HOLE OF THE INBOARD CHORD OF THE LH FRAME PART NUMBER 65-16326-139 AT STATION 783.95Feb 13, 2023 · N215WE · Boeing 7272S2FSDR DALA2023021501181None · noneSECONDARY NRC, IN REF NRC 00488 CORROSION ON LH CUSP WEB BTW STA Y=560 - 579 AND BTW Y=609 TO 617. SUMMARY OF NRC 00612: CUSP WEB LH BTW STA Y=560 TO 579 AND BTW Y=609 TO 617 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP. 4 AND 51-41-02-0G. (LP #2Feb 13, 2023 · N893AT · Boeing 717200SDR CALA2023021400433Unknown · cracked(B757-53-3-0571) AFT CABIN LH SIDE FRAME 1620 INTERCOSTAL SUPPOR T CRACKED. (LOCATED JUST ABOVE THE AFT CABIN WINDOW) TRANSCRIBED FROM HAECO GSO NR 9282500. REMOVED AND REPLACED LH STA 1620 INTERCOSTAL SUPPORT CHORD IAW B AC DWG 146NN3700 REV A AND B757-200 SRFeb 13, 2023 · N17139 · Boeing 757200SDR CALA2023021400432Frame · unknown"THE REPAIR INCORPORATED VIA ECRA 5360-01687 IS APPROVED AS TIME -LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE AU GUST 01, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING AP Feb 13, 2023 · N17139 · Boeing 757200SDR DALA2023021401172None · noneSHIP 5636 VIASAT SYSTEM INSTALLATION AT FS 1260 & FS 1280 FRAMES. CORRECTIVE ACTION: REF ERA 606050-14. (2627217)Feb 13, 2023 · N536US · Boeing 757251SDR CALA2023021300426Stop · crackedLEFT FR66 DOORSTOP #1 INBD LOWER HOLE HAS CRACK INDICATIONS IN F RAME 1 POSITION. GEN BY V061671 ON HAECO LCQ NR 9298406/42406 CRACKS NOTED.REQUIRES INSP AT 31,600 FC FROM RPR EMBODIMENT WITH 53-41-12-205-010 TABLE 001.THIS IS A CLASS B RPR. ALL WORK ACMP SUBSFeb 13, 2023 · N427UA · Airbus A320232SDR SWIA20230212None · damagedFRAME 73 LH CROSSBEAM HAS TOOLING MARKS AS MARKEDFeb 12, 2023 · N132SY · Emb ERJ170200LRSDR DALA2023021301097Unknown · unknown(LOG 2626129) DURING INSPECTION FOUND BENT FRAME STA. 500K BTW STR 26L TO STR 22L AT FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON FRAME STA 500K BTW STR 22LTO STR 26L AT FWD CARGO COMPARTMENT AS PER ERA 603433-14.Feb 12, 2023 · N956DD · Boeing 7379SDR CALA2023021300417Stop · crackedLEFT FR66 DOORSTOP #1 OTBD UPPER HOLE HAS A CRACK INDICATION IN FRAME AT 8:30 POSITIONS. GEN BY V061671 ON HAECO LCQ NR 9298407( 42407) AMED BUSHING TO FINAL ID OF .2815? IAW SRM 53-41-12-300-010. LEF UIRES INSPECTION AT 33,000 FC AND SUBSEQUENT INSPECTION AT Feb 12, 2023 · N427UA · Airbus A320232SDR DALA2023021501192None · noneAIRCRAFT 3132, CRACK INDICATION FOUND ON FR 16RH DOORSTOP#7 HOLES#1 AND HOLE#3 ON FRAME AND FITTING. CORRECTIVE ACTION: CRACK WAS REPAIRED ON FR 16 RH DOOR STOP #7 HOLE #1 ON FRAME AND INTERCOSTAL WAS REPLACED I.A.W. PRI 605872-14 REV 0 AND ERA 605872-14 REV 0Feb 11, 2023 · N332NB · Airbus A319114SDR DALA2023021501191None · noneAIRCRAFT 3132, CRACK INDICATION FOUND ON FR 20 RH DOORSTOP#7 ON FRAME AND FITTING. CORRECTIVE ACTION: CRACK WAS REPAIRED ON FR 20 RH DOOR STOP #7 HOLE #1 ON FRAME AND INTERCOSTAL WAS REPLACED I.A.W. PRI 605874-14 REV 0 AND ERA 605874-14 REV 0. (LP 2627622)Feb 11, 2023 · N332NB · Airbus A319114SDR DALA2023021501190None · noneAIRCRAFT 3132, CRACK INDICATION FOUND ON FR 16RH DOORSTOP HOLES#1 AND HOLE#3 ON FRAME AND FITTING. CORRECTIVE ACTION: CRACK WAS REPAIRED ON FR 16 RH DOOR STOP #1 HOLE #3 ON FRAME AND INTERCOSTAL WAS REPLACED I.A.W. PRI 605872-14 REV 0 AND ERA 605872-14 REV 0. Feb 11, 2023 · N332NB · Airbus A319114SDR DALA2023021501189None · noneAIRCRAFT 3132, CRACK INDICATION FOUND ON FR 16LH DOORSTOP HOLES#1 AND HOLE#3 ON FRAME AND FITTING. CORRECTIVE ACTION: CRACK WAS REPAIRED ON FR 16 LH DOOR STOP #1 HOLE #3 ON FRAME AND INTERCOSTAL WAS REPLACED I.A.W. PRI 605885-14 REV 0 AND ERA 605885-14 REV 0. Feb 11, 2023 · N332NB · Airbus A319114SDR DALA2023021401136Unknown · unknownCORRODED DIAPHRAGM ON STA Y=200 X=-22. ORIGINAL THICKNESS WAS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.012 IN, THEREFORE IT IS OUT LIMITS IN REF NRC 00424 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00510: CORROSION LEVEL 2. DIAPHRAGM (WEB) ON STA Y=200 X=-22Feb 11, 2023 · N894AT · Boeing 717200
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