N3737C

Service difficulty reports · 131

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N3737C' AND registry_match = 'registration'
  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 DALA2026080504524Unknown · smokeON LIFTOFF, AFT FLIGHT ATTENDANT SAID SMOKE IN THE MID TO AFT CABIN. R & R HEAT EXCHANGERS, ACM, TEMP CONTROL VALVE, SENSE LINE AND RECIRCULATION FILTER. (5930822) AIRCRAFT WAS GROUNDEDAug 2, 2026 · N3737C · Boeing 737832 · Air Distribution SystemSDR DALA2026063003856Fan · out of balanceATB/DE- DUE TO RIGHT ENGINE FAN VIBRATION 4.2 AND HAD TO REDUCE THROTTLE TO KEEP VIB BELOW LIMITS. PERFORMED FAN TRIM BALANCE VIB NOW AT 1.8. (LOG 8365005 - AIRCRAFT WAS GROUNDED).Jun 29, 2026 · N3737C · Boeing 737832 · Engine (Turbine/Turboprop)SDR DALA2025031802032Mount · corroded(LOG 0855497) VERTICAL STAB MOUNTING POINTS CORROSION PRI 624280 ISSUED. C/W VERTICAL STAB/MOUNTING POINTS/CORROSION FINDINGS ERA 624280-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. VERIFIED ERA 624280-14 HAS BEEN COMPLETED.Mar 13, 2025 · N3737C · Boeing 737832 · Fuselage, Stabilizer Attach FittingsSDR DALA2025031702014Rudder · ground damage(LOG 0855976) A/C HIT IN RUDDER BY JAL 787. C/W ERA 624172-14 SECTION 1 PERMANENT REPAIR. R/R RUDDER ASSY, REF LOG 0853320. REPAIRED VERTICAL STAB ASSY IAW ERA 624172-14,624294-14,624280-14,624522-14,624701-14 ALL REV ORIGINAL.Mar 13, 2025 · N3737C · Boeing 737832 · Rudder, Plate/SkinSDR DALA2025031702016Rudder · damaged(LOG 0853320) DAMAGED RUDDER BY TAIL STRIKE. REMOVED RUDDER PER AMDS #2721-4912 STEPS 1-3. C/W RUDDER REPLACEMENT IAW AMDS 2721-4912 (R.GROSS 436426) ALL RII ITEMS C/W.Mar 12, 2025 · N3737C · Boeing 737832 · Rudder, Plate/SkinSDR DALA2025030301616Stabilizer · ground damageAIRCRAFT 3737, WHILE PARKED ON DE-ICE PAD IN SEA, AIRCRAFT WAS STRUCK BY THE RIGHT WINGTIP OF A TAXIING JAL B787. AIRCRAFT VERTICAL STABILIZER WAS STRUCK ON THE RIGHT SIDE CAUSING SUBSTANTIAL DAMAGE. IN ORDER TO ACCESS THE BOLTS FOR THE REAR SPAR PRIMARY FITTIFeb 27, 2025 · N3737C · Boeing 737832 · Vertical StabilizerSDR DALA2025030301627Mount · corrodedAIRCRAFT 3737, ON VERTICAL STAB AFT MOUNT OUTBOARD LT FITTING LUG CORROSION ON FACE OF BUSHING. CORRECTIVE ACTION: REPLACED VERTICAL STAB AFT MOUNT OUTBOARD LT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS. REF ERA 624280-14 REV 0 PRI REV5. (LP 0829461)Feb 26, 2025 · N3737C · Boeing 737832 · Fuselage, Stabilizer Attach FittingsSDR DALA2025030201584Bushing · not reported(LOG 0829464) ALL 8 BUSHINGS ON AFT PRIMARY AND FAIL SAFE FITTING MUST BE REPLACED. R/R ALL 8 BUSHINGS ON AFT PRIMARY AND FAILSAFE FITTINGS PER PRI 624280-14, C/W ALL RII ITEMS, REF ERA 624280 REV 0, PRI REV 5.Feb 25, 2025 · N3737C · Boeing 737832 · Empennage StructureSDR DALA2025030201577Structure · damaged(LOG 0828481) ACCESS HOLE CUTOUT IN LWR CLOSURE RIB WEB (P/N 172A3104-1) IS MADE FOR REAR SPAR PRIMARY FITTING BOLTS INSPECTION. HOLE CUTOUT IS REPAIRED BY DOUBLER IAW PRI 624294-14 REV 1.Feb 25, 2025 · N3737C · Boeing 737832 · Vertical StabilizerSDR DALA2025030201589Mount · corroded(LOG 0829460) ON VERTICAL STAB AFT MOUNT OUTBOARD RT FITTING LUG CORROSION ON FACE OF BUSHING. R/R VERT STAB AFT MOUNT OUTBOARD RT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS, REF ERA 624280-14 REV 0, PRI REV 5.Feb 25, 2025 · N3737C · Boeing 737832 · Fuselage, Stabilizer Attach FittingsSDR DALA2025030401688Bushing · corroded(LOG 0824717) ON FWD MOUNT OF VERTICAL STAB, FOUND CORROSION ON RIGHT BOLT ATTACH BUSHING AND FRAME. REMOVED AND REPLACED R/H FWD ATTACH BUSHING REF PRI 624280-14.Feb 23, 2025 · N3737C · Boeing 737832 · Vertical StabilizerSDR DALA2025030401689Bushing · corroded(LOG 0824702) FOUND CORROSION ON FWD MOUNT OF VERTICAL STAB ON LH FWD BUSHING AND FRAME AROUND BUSHING ATTACH BOLT. REMOVED AND REPLACED L/H FWD MOUNT BUSHING REF PRI 624280-14.Feb 22, 2025 · N3737C · Boeing 737832 · Vertical StabilizerSDR DALA2024122411993Seal · failedSHIP 3737 -MISC- DECLARED EMERGENCY INTO ATL DUE TO ABNORMAL FLIGHT CONTROL FEEL DURING ROLL MANEUVERS. CHECKED AILERON SPRING CARTRIDGE, RATIO CHANGER INPUT ROD, VERIFIED CABLE TENSIONS, GREASED AILERON POWER LEVER. FOUND UPPER AILERON POWER CONTROL UNIT B Dec 23, 2024 · N3737C · Boeing 737832 · Aileron Control SystemSDR DALA2024121211682Gearbox · inoperativeSHIP 3737 -UFC/DE- DECLARED EMERGENCY INTO ATL DUE TO FLAP LOCKOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED TEE ANGLE GEARBOX PER B737 AMM 27-51.Dec 11, 2024 · N3737C · Boeing 737832 · Trailing Edge Flap Control SystemSDR DALA2024101610123Door Frame · cracked(LOG 0610929) CRACK ON UPPER/FWD CUTOUT JAMB OF AFT ENTRY DOOR AT PAX CABIN. UPPER STUB FRAME ON FWD CUTOUT JAMB OF AFT ENTRY DOOR AT PAX CABIN WAS REPAIRED PER ER/A 620875-14.Oct 15, 2024 · N3737C · Boeing 737832 · Fuselage Main, StructureSDR DALA2024101410035Floor Support · corroded(LOG 0604725) CORROSION ON FLOOR SUPPORTS BTW STA=727 D TO 727 E, LBL=8.1 AND STA= 767 TO 787 RBL= 3.0, RBL=8.1 AT AFT CARGO COMPARTMENT. FLOOR SUPPORTS BTW STA=727 D TO 727 E, LBL=8.1 AND STA= 767 TO 787 RBL= 3.0, RBL=8.1 AT AFT CARGO COMPARTMENT WERE REPAIREOct 12, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101109987Plate · corroded(LOG 0602237) CORROSION ON SIDE PLATES FROM STA 727 TO STA 727G ALSO FROM STA 727G TO STA 787 LH SIDE AT AFT CARGO COMPARTMENT. SIDE PLATES STA 727G TO STA 787 LH SIDE AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.Oct 10, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101109984Stringer · corroded(LOG 0600655) CORROSION ON STRINGER 26LBL & FROM STA 802 TO STA 827 AT AFT CARGO COMPARTMENT. STRINGER 26LBL & FROM STA 777 TO STA 887 AT AFT CARGO COMPARTMENT WAS REPAIRED PER 53-00-03-2R PROCEDURE 1 REPAIR 1.Oct 9, 2024 · N3737C · Boeing 737832 · Fuselage Main, Longeron/StringerSDR DALA2024101109978Plate · corroded(LOG 0599360) CORROSION ON LH SIDE PLATE BTW STA 510 TO STA 500H AT FWD CARGO COMPARTMENT. LH SIDE PLATE BTW STA 510 TO STA 500H AT FWD CARGO COMPARTMENT WAS REPLACED PER PER B737-800 SRM 51-40-02-0G.Oct 9, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101009927Plate · corroded(LOG 0600722) CORROSION ON SIDE PLATES FROM STA 727 TO 727G+10 AND FROM STA 727G+10 TO STA 787 ALSO FROM STA 887 TO STA 947.5 RH SIDE AT AFT CARGO COMPARTMENT. SIDEPLATE RH BTW STA 727 AND STA 767 WAS REPLACED PER B737-800 SRM 51-40-02-0G.Oct 9, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101009926Pressure Deck · gouged(LOG 0598896) GOUGES IN HOLES WERE FOUND ON VERTICAL PRESSURE DECK WEB, VERTICAL STIFFENERS, ATTACH ANGLE AND UPPER COMPRESSION CHORD. VERTICAL PRESSURE DECK WEB, VERTICAL STIFFENERS, ATTACH ANGLE AND UPPER COMPRESSION CHORD BTW BS 663 RBL 30-40 WERE REPAIRED Oct 8, 2024 · N3737C · Boeing 737832 · Fuselage Main, StructureSDR DALA2024101009924Plate · corroded(LOG 0598818) CORROSION ON LH SIDE PLATE BTW STA 400 TO STA 510 ATFWD CARGO COMPARTMENT. LH SIDE PLATE BTW STA 400 TO STA 510 ATFWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR. 4. AND SRM.51-40-05-0G.Oct 8, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101009921Plate · corroded(LOG 0598552) CORROSION ON RH SIDE PLATE BTW 500B +10 TO 500H AT FWD CARGO COMPARTMENT. RH SIDE PLATE BTW 500B + 10 TO 500H AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-05-0G AND SRM 51-40-02-0G.Oct 8, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101009912Support Fitting · corroded(LOG 0597577) CORROSION ON RH/LH FITTING SUPPORT STA=951- 972, RBL=50 AND LBL=50 AT CPAX. RH/LH FITTING SUPPORT STA=951-972, RBL=50 AND LBL=50 AT CPAX (W2) WERE REPLACED PER B737-800 SRM 51-40-02-0G.Oct 8, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024101009906Floor Support · corrodedCORROSION ON FLOOR SUPPORTS 294.5-344 AT FLOOR SRTUCTURE OF PASSERNGER CABIN. LEVEL 2-FLOOR SUPPORTS BTW STA 312 TO 328 LBL 11, STA 328 TO 344 LBL 11 AND INTERCOSTAL BTW STA 312 TO 294.5 LBL 11 WERE REPLACED PER B737-800 SRM 51-40-02-0G.Oct 7, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024100809807Shield · corroded(LOG 0597233) CORROSION ON SHIELD BTW STA767 TO STA 790 AFT CARGO COMPARTMENT. SHIELD BTW STA767 TO STA 790 AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4 , SRM 51-40-02-0G PAR 7 AND SRM 51-40-02-0G PAR 5 AND DWG: 146A8127.Oct 7, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024100409689Floorbeam · corroded(LOG 0591048) CORROSION ON FLOOR SUPPORT STA 887 BTW STRINGERS 25RH-25LH AT AFT CARGO COMPARTMENT. FLOOR SUPPORT STA 887 BTW STRINGERS 25RH-25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.Oct 4, 2024 · N3737C · Boeing 737832 · Fuselage Main, Floor BeamSDR DALA2024100409688Floor Support · corroded(LOG 0591035) CORROSION ON FLOOR BEAM STA=977-981, LBL=17. STA= 951-961, RBL=26 AND STA 951 RBL 19, STA 951 RBL 40. AND ANGLES STA=992.8, LBL/RBL=41, AT PAX CABIN. FLOOR BEAM STA=977-981, LBL=17. STA= 951-961, RBL=26 AND STA 951 RBL 19, STA 951 RBL 40 AND ANGLOct 4, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024100209629Plate · corroded(LOG 0586565) CORROSION ON RH SIDE PLATE BTW STA 500 TO STA 500A AT FWD CARG COMPARTMENT. RH SIDE PLATE BTW STA 500 TO STA 500A AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.Oct 1, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024100109574Seat Track · worn(LOG 0585465) WEAR RH INB/OUTBD SEAT TRACKS STA520 AT CPAX. RH INB/OUTBD SEAT TRACKS STA 520 WERE REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 4. REPAIR 4.Oct 1, 2024 · N3737C · Boeing 737832 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024100109573Floor Support · cracked(LOG 0584614) CRACK ON INTERCOSTAL BTW STA 345 AND STA 360 AT FLOOR STRUCTURE OF PASSERNGER CABIN. INTERCOSTAL BTW STA 345 AND STA 360 AT FLOOR STRUCTURE OF PASSERNGER CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.Sep 30, 2024 · N3737C · Boeing 737832 · Fuselage Miscellaneous StructureSDR DALA2024093009524Seat Track · worn(LOG 0579458) WEAR ON LH IN'BD & OUT'BD SEAT TRACKS AT STA 500I TO 520. SEAT TRACK SECTION PREVIOUS REPAIR LH IN'BD & OUT'BD AT STA 500I TO 520 WERE REPLACED PER B737-800 SRM 53-00-52-2R PROCEDURE. 4.Sep 27, 2024 · N3737C · Boeing 737832 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024093009519Seat Track · corroded(LOG 0577624) CORROSION ON RH INBOARD SEAT TRACKS STA462 AT CPAX. RH INBOARD SEAT TRACKS STA462 AT CPAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.Sep 26, 2024 · N3737C · Boeing 737832 · Fuselage, Seat/Cargo Attach FittingsSDR 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 737832 · Fuselage Main, FrameSDR 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 737832 · Fuselage Main, FrameSDR 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 · Fuselage Main, FrameSDR DALA2024093009513Frame · cracked(LOG 0575887) CRACK WAS FOUND OF 0.11IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024093009512Frame · cracked(LOG 0575883) CRACK WAS FOUND OF 0.28 IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024093009511Frame · cracked(LOG 0575872) CRACK WAS FOUND OF 0.26IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 480. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 480. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609462None · none(LOG 0576123) "A.A IN REF AMDS 5732-01015-01B-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC: 00599 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01B-01.Sep 25, 2024 · N3737C · Boeing 737832 · Standard Practices/StructuresSDR DALA2024092609461None · none(LOG 0576156) " A.A IN REF AMDS 5732-01015-01A-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC:00598 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01A-01.Sep 25, 2024 · N3737C · Boeing 737832 · Standard Practices/StructuresSDR DALA2024092609460Frame · cracked(LOG 0576096) CRACK WAS FOUND OF 0.19IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609459Frame · cracked(LOG 0575891) CRACK WAS FOUND OF 0.310IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609458Frame · cracked(LOG 0575884) CRACK WAS FOUND OF 0.1IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609457Frame · cracked(LOG 0575882) CRACK WAS FOUND OF 0.22IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500D. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500D. BTW S-8L & S-9L WAS REPIARED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609456Frame · cracked(LOG 0575871) CRACK WAS FOUND OF 0.21IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609455Frame · cracked(LOG 0575867) CRACK WAS FOUND OF 0.12IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609454Frame · cracked(LOG 0575863) CRACK WAS FOUND OF 0.200IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609453Frame · cracked(LOG 0575860) CRACK WAS FOUND OF 0.8IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 440. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 440. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, FrameSDR DALA2024092609452Frame · cracked(LOG 0575820) CRACK WAS FOUND OF 0.7IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.Sep 25, 2024 · N3737C · Boeing 737832 · Fuselage Main, Frame
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