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 DALA2024101310015Frame · crackedSHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE / CRACK. C/A: ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 97,200 TOTAL AIRFROct 8, 2024 · N353NW · Airbus A320212SDR DALA2024101310014Frame · crackedSHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE / CRACK. C/A: ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 73,600 TOTAL AIRFROct 8, 2024 · N353NW · Airbus A320212SDR DALA2024101009937Frame · corrodedSHIP 3144 CORROSION WEB FRAME 16 AT LEVEL STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB FR16 AT LEVEL STR23R AT FWD GALLEY AREA AS PER A319 SRM 51-42-11-801 AND A319 SRM 51-72-11-911-001. (0598661)Oct 8, 2024 · N344NB · Airbus A319114SDR AALA202410098894Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 66 RIGHT AND #7 DOOR STOP FITTING. REPAIRED FRAME PER SRM 53-41-12-300-011Oct 8, 2024 · N118US · Airbus A320214SDR AALA202410098108Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN STUB FRAME ABOVE CENTER WING BOX AT BS 616, FROM RBL 70 TO RBL 85. ACCOMPLISHED REINFORCING REPAIR PER EA 357998.Oct 8, 2024 · N905AN · Boeing 737823SDR DALA2024100909865Frame · corrodedSHIP 1806 DURING HCK AT STAG, CORROSION WAS FOUND AT STA 1562 FRAME WEB, S37L-39L. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER ER/A 621214-14. (0597265)Oct 7, 2024 · N830MH · Boeing 767432ERSDR FDEA202410071439Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPILED WITH EA: 6-5710-T0381007 P1. REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGEOct 7, 2024 · N665FE · Airbus A300F4605RSDR FDEA202410071438Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO: 6-5710-E0342809 D P1. REPAIRED THE CRACKED HOLE "I" OF CENTER WING BOX - REAR SPAR AND BOTTOM PANEL ATOct 7, 2024 · N665FE · Airbus A300F4605RSDR R61A2024102200471Frame · corrodedCORROSION ON CABIN FLOOR STRUCTURE RH INBD SEAT TRACK BEAM AT FR12-13, 13-14. INSTALLED REPAIRED FILLER/DOUBLER REF ETD2024-170-027084Oct 5, 2024 · N403YX · Emb ERJ170200LRSDR DALA2024100709733Frame · crackedCRACK ON FRAME BTW STA Y=1037 AND LONG 17R AT PAX CABIN RH SIDE. SUMMARY OF NRC 00287: FRAME BTW STA Y=1037 AND LONG 17R AT PAX CABIN RH SIDE WAS REPAIRED PER B717 SRM 53-20-07-2R-4. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK PER B717-200 SRM 53-20-07-2Oct 5, 2024 · N991AT · Boeing 717200SDR DALA2024100909848Frame · crackedSHIP 1806 SURFACE HFEC INSPECTION OF THE FWD OUTER CHORD BETWEEN STRINGERS 3R AND 10R,FOUND 2EA CRACKS IN THE CORNER OF THE STRINGER 7R,THE LENGTH OF CRACK ARE 0.5IN AND 0.2IN.AS MARKED. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER B767-400 SRM 53-80-08. (0591Oct 4, 2024 · N830MH · Boeing 767432ERSDR DALA2024100709739Frame · cracked(LOG 0591941) CRACK WAS FOUND OF 0.23IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.Oct 4, 2024 · N3735D · Boeing 737832SDR DALA2024100709738Frame · cracked(LOG 0591870) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. WAS REPAIRED PER CARD AD 2526-01236-02B.Oct 4, 2024 · N3735D · Boeing 737832SDR DALA2024100709737Frame · cracked(LOG 0591808) CRACK WAS FOUND OF 0.32IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.Oct 4, 2024 · N3735D · Boeing 737832SDR VNAA202410030021Frame · corrodedHN00175058 FUSELAGE CIRCUMFERENTIAL JOINT AT FS280.00 SHOWS SIGNS OF CORROSION BETWEEN STRINGERS L23-L24. CORRECTIVE ACTION: REPAIRED FUSELAGE CIRCUMFERENTIAL JOINT AT FS280.00 BETWEEN STRINGERS L23-L24 IAW REO 670-53-21-2446 REV -- DATED 2024-08-19.Oct 4, 2024 · N716PS · Cndair CL6002C10SDR DALA2024100409686Frame · cracked(LOG 0590743) CRACK WAS FOUND OF 0.500IN OF LENGTH ON RH FUSELAGE FRAME AT INBD FASTENER HOLE ON STA 500F BTW S-8R & S-9R. FRAME AT INBD FASTENER HOLE ON STA 500F BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100409685Frame · cracked(LOG 0590237) CRACK WAS FOUND OF 0.28IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100409683Frame · cracked(LOG 0589533) CRACK WAS FOUND OF 0.21IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 827 BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100409682Frame · cracked(LOG 0589476) CRACK WAS FOUND OF 0.31IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 727B. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 727B BTW S-8L & S-9L.. WAS REPAIRED PER AMDS 2526-01236-02A.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100409681Frame · cracked(LOG 0589342) CRACK WAS FOUND OF 0.25IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L . WAS REPAIRED PER AMDS 2526-01236-02A.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100409692Frame · cracked(LOG 0590309) CRACK WAS FOUND OF 0.12IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F. BTW S-8L & S-9L. NO CRACKS WERE FOUND PER B737 NDT MANUAL PART 6 ASSOCIATED AA 2526-01236 ADDED FOR AC 3735.Oct 3, 2024 · N3735D · Boeing 737832SDR DALA2024100709741Frame · cracked(LOG 0592097) FOUND CRACK IN FRAME AT BS 440 STR 8L INBD FASTENER HOLE. REPAIRED PER WORK CARD 2526-01236-04A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.Oct 2, 2024 · N3730B · Boeing 737832SDR DALA2024100409675Frame · cracked(LOG 0589206) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 500C BTW S-8R & S-9R. WAS REPAIRED PER AMDS 2526-01236-02B.Oct 2, 2024 · N3735D · Boeing 737832SDR IXXA2024111301Frame · crackedR/H 1809.5 BULKHEAD FWD OUTER CHORD INBOARD FLANGE IS CRACKED AT FASTENER HOLE JUST ABOVE HORIZ STAB PIVOT PIN FITTINGOct 1, 2024 · N761CX · Boeing 767223SDR SWAA2024103144059Frame · crackedFWD ENTRY DOOR CUTOUT; BS 312 FRAME IS CRACKED IN RADIUS JUST ABOVE CUT OUT HEADER FRAME<[01] FWD ENTRY DOOR CUTOUT BS 312 FRAME BELOW STR 5L REPAIRED PER EA # M-22-153-01244;[02] VERIFIED CORRECTIVE ACTION; TASK COMPLETE.Oct 1, 2024 · N272WN · Boeing 7377H4SDR AALA202410027495Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FATENER HOLE AT FR 68 LEFT AND #1 DOOR STOP FITTING. REPAIRED FRAME PER SRM 53-41-12-300-011.Oct 1, 2024 · N118US · Airbus A320214SDR TLLA2050314000137Frame · crackedDURING 300 HOUR AF INSPECTION FOUND A CRACK AT STATION 142 R/H SIDE ON THE UPPER FRAME. NOT RELATED TO ANY INCIDENT OR ACCIDENTSep 30, 2024 · N249TH · Bell 206L1SDR 2025FA0000137Frame · crackedDURING 300 HOUR A/F INSPECTION FOUND A CRACK AT STATION 142 R/H SIDE ON THE UPPER FRAME NOT RELATED TO ANY INCIDENT OR ACCIDENT.Sep 30, 2024 · N249TH · Bell 206L1SDR IPXA2024103079737Frame · crackedCRACKS FOUND IN TOP AND MIDDLE HOLES ON LH FR40 UPPER TENSION. ACCOMPLISED REPAIR IN ACCORDANCE VT-MAE EA 300-5710-27-A3702, REV -.Sep 30, 2024 · N170UP · Airbus A300F4622RSDR UIEA2024092400943Frame · corrodedFWD CARGO COMPARTMENT, EVIDENCE OF CORROSION ON WEB FRAME AT BS 764 BTW S37L AND S38L.(<P>WEB FRAME AT BS 764 BTW S37L AND S38L. PAINT WAS REMOVED, REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND. ALLODINE, PRIMER AND PAINT WAS RESTORED IAW SRM 53-00-07-1A-1. NSep 29, 2024 · N1619A · Boeing 7673Y0SDR COEA2024110613807Frame · damagedWO 257175 NR 6 HEAVY CHECK COE/MAJOR REPAIR: DRILL STRIKE ON FRAME 33 ON THE R/H OUTER FLANGE BELOW THE OUTBOARD MOST RIVET OF FLOORBEAM 33. CORRECTIVE ACTION: REPAIRED PER ATR72 SRM 51-25-01.Sep 28, 2024 · N807FX · Aerosp ATR72212SDR VNAA20241102016Frame · corrodedCORROSION ON FRAME FS1088.20 BTW STGR 24RH AND STGR 23LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). FRAME FS1088.20 BTW STGR 24RH AND STGR 23LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-06-101-003-A02 ANSep 28, 2024 · N587NN · Bombdr CL6002D15SDR COEA2024110111807Frame · damagedWO 257175 NR 5 HEAVY CHECK COE/MAJOR REPAIR: DRILL STRIKE ON FRAME 33 L/H OUTER FLANGE BELOW THE OUTBOARD MOST RIVET. CORRECTIVE ACTION: REPLACED L/H SIDE FRAME SEGMENT PER ATR72 SRM 51-25-01.Sep 28, 2024 · N807FX · Aerosp ATR72212SDR SWAA2024102942833Frame · crackedPASSENGER COMPARTMENT LEFT SIDE FOUND CRACK AT FRAME STA 312; STR#5L DOT#001<[01] ACCOMPLISHED REPAIR AT FRAME STA 312; STR#5L PER M-22-153-01244;[02] ACCOMPLISHED REPAIR AT FRAME STA 312; STR 5L PER EA NO: M-22-153-01244;[03] ACCOMPLISHED REPAIR AT FRAME STA Sep 28, 2024 · N498WN · Boeing 7377H4SDR JR2R20240928348Frame · corrodedFR88 HAS CORROSION BETWEEN STR27R THRU STR28R. REPAIREDSep 28, 2024 · N86311 · Emb ERJ170200LRSDR JR2R20240928458Strap · corrodedDOUBLER / FRAME STRAP AT FR90 AND LBL10 CORRODED. REPLACEDSep 28, 2024 · N86311 · Emb ERJ170200LRSDR SWIA2024120301326Frame · corrodedFRAME FS295.00 HAS CORROSION ON THE LOWER FLANGE STGR25L - 24R. (MARKED) (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM LOWER FLANGE COMMON TO BELLY SKIN, AT FS295.00 BETWEEN STGR25L - STGR24R, AND EVALUATED AS 'OUT-OF-LIMITS'. REPAIRED FRAME FLANGE. RESep 27, 2024 · N744EV · Cndair CL6002C10SDR SWIA2024120301325Frame · corrodedFRAME FS310.00 HAS CORROSION ON THE UPPER FLANGE FROM STGR24L - STGR26R. (MARKED) (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM FRAME UPPER FLANGE AT FS310.00 STGR24L-STGR26R PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED FRAME PESep 27, 2024 · N744EV · Cndair CL6002C10SDR VNAA20241102014Frame · corrodedCORROSION ON FRAME FS= 319.70 BTW STRG 26LH TO 26RH AT MAINAVIONICSCOMPARTMENT. (E/E) CORROSION ON FRAME FS= 319.70 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERCRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED, THEREFORE IS WHITHIN OF LSep 27, 2024 · N587NN · Bombdr CL6002D15SDR VNAA20241102013Frame · corrodedCORROSION ON FRAME FS= 310.00 BTW STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BTW STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERCRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ 90Sep 27, 2024 · N587NN · Bombdr CL6002D15SDR VNAA20241102012Frame · corrodedCORROSION ON FRAME FS295.00 BTW STGR 26LH TO STGR 26RH. CORROSION ON FRAME FS295.00 BTW STGR 26LH TO STGR 26RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-06-101-002-A04Sep 27, 2024 · N587NN · Bombdr CL6002D15SDR DALA2024093009555Frame · corrodedSHIP 3148 CORROSION FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FRAME 20 AS PER ER/A 620187-14. (0579927)Sep 27, 2024 · N348NB · Airbus A319114SDR DALA2024093009548Frame · crackedSHIP 3148 CRACK INDICATION FOUND AT HOLE 4 HOLE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FR 68 ON STR 22R AT HOLE 4 LOWER INBOARD POSITION LOCATED AT DOOR STOP FITTING 1 AS PER ER/A 620540-14AD. (0579914)Sep 27, 2024 · N348NB · Airbus A319114SDR VNAA20241103009Frame · corrodedCORROSION ON FRAME FS 349.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS 349.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRJ90Sep 26, 2024 · N587NN · Bombdr CL6002D15SDR VNAA20241103008Frame · corrodedCORROSION ON INTERCOSTAL BTW FS349.00 TO FS364.00 STGR 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL BTW FS349.00 TO FS364.00 STGR 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITSSep 26, 2024 · N587NN · Bombdr CL6002D15SDR AALA202409276319Frame · crackedAIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR CUT OUT UPPER AFT CORNER FRAME FITTING CRACKED AT FR68 AND S8R. REPLACED UPPER AFT CORNER FRAME FITTING PER SRM 51-72-11.Sep 26, 2024 · N751UW · Airbus A319112SDR SWIA20240925Floorbeam · corrodedCORROSION ON AFT WET AREA RH BEAM AROUND RIVETS AT FR 87 STGR27R/28R (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED THE AFT WET AREA RH BEAM AT FR 87 STGR27R/28R. REF EMB SRM 51-40-08. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.Sep 25, 2024 · N116SY · Emb ERJ170200LRSDR DALA2024093009516Frame · cracked(LOG 0576124) CRACK WAS FOUND OF 0.15IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832SDR DALA2024093009515Frame · cracked(LOG 0576118) CRACK WAS FOUND OF 0.12IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8R & S-9R.RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832SDR DALA2024093009514Frame · cracked(LOG 0575896) CRACK WAS FOUND OF 0.14IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832
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