N351JB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
17 reports on file, 2013-03-03 – 2022-01-18.
Part: FMU — FAILED (NR 1 ENGINE) · airframe 24,870 hrs · 16,827 cycles
FLT # 716,BUF-BOS.(EMERGENCY DECLARED). DURING CLIMB AT APPROX 12000FT ENGINE 1 BEGAN SURGING BETWEEN 56% - 79% N1 . UPON LEVEL OFF AT 19,000 FEET, THE SURGE STOPPED. ONCE WE BEGAN DECENT IT SURGED ONE MORE TIME, THEN WAS NORMAL THROUGHOUT LANDING ROLL.; SEE DEFECT # 3287925 FOR FMU REPLACEMENT. ENG #1 FADEC CONNECTORS P3 + P4 DISCONNECTED FOR TROUBLESHOOTING. RECONNECT P3+ P4 ON #1 ENG FADEC . REMOVED #1 ENG FMU REF DEFECT LP 3287923 ITEM #1. INSTALLED #1 ENG FMU LEAK CHECKS OK REF 73-00-00-050-804 LMM
Earlier reports · 2013–2021 · 16 reports
2021
Part: HEAT EXCHANGER — LEAKING (BLEED 1) · airframe 24,730 hrs · 16,737 cycles
FLT 468, FLL-ATL (AIR TURN BACK TO FLL). BLEED 1 LEAK ON EICAS AFTER TAKEOFF AT ABOUT 13K FT ; ACCOMPLISHED FIM TASK 36-21-00-810-813-A FOUND DC4 GREASE (INCREASES CAPACITANCE CHANGES IMPEDANCE) ON LOOP3 L/H PACK CERAMIC PINS CHA & B . CLEANED & REPLACED CERAMIC PINS LOOP3 & FOUND SMALL LEAK AT HEAT EXCHANGER COUPLING REPLACED O-RINGS LEAK CK GOOD. OPS CK LOOPS 3 CHA &B & ENG IDLE RUN GOOD ALL LOOPS CONTINUITY CK GOOD 7.3 OHMS NO SHORTS.
2020
Part: PIN — MISINSTALLED (R1 DOOR SLIDE) · airframe 22,485 hrs · 15,261 cycles
DURING HEAVY MAINTENANCE, SAFETY PIN CANNOT BE FULLY INSERTED IN THE SLIDE ON R1 DOOR. PERFORMED CONTROLLED SLIDE DEPLOYMENT OF DERVICE DOOR 821 PER MAD 25-03-12-006A IAW GMM PROCEDURE 6.25. REMOVED AND REPLACED EMERGENCY EVACUATION ESCAPE SLIDE FWD SERVICE DOOR IAW 25-65-01-000-801-A & 25-65-01-400-801.
Part: SEAL — LEAKING (PRECOOLER) · airframe 21,934 hrs · 14,892 cycles
FT # 490, MCO-JFK. RETURNED TO FIELD. BLEED 1 LEAK MSG CLIMBING THROUGH 17,000 FT. BLEED 2 WAS ALREADY ON MEL; FOUND # 1 ENG PRECOOLER OUTLET SEAL LEAKING SEE LG PAGE 2739138 ITEM # 1 FOR CORRECTIVE ACTION. REMOVED #1 ENG PRECOOLER OUTLET & SKIRT AND PRECOOLER OUTLET SEAL. INSTALLED ENG-1 PRECOOLER SEAL IAW 36-11-08. ACCOMPLISHED PERMANENT REPAIR IN ACCORDING WITH JB EC E20-060-01. LEAK AND OPS CK GOOD.
2017
Part: STRUT — LEAKING (NLG) · airframe 15,329 hrs · 10,142 cycles
DECLARED EMERGENCY. DUIRNG CLIMB OUT, LG WOW SYS FAIL MESSAGE ON EICAS. COMPLIED W/QRH. ALL COMPONENTS FUNCTIONED NORMALLY ON LANDING ROLLOUT; FOUND NLG LEAKING FLUID FROM LOWER SLIDING TUBE. STRUT EFLATED. NLG SPARE SEAL ACTIVATED IAW AMM 32-21-02. SERVICED NLG STRUT IAW AMM 12-12-09. NO LEAKS NOTED. PSEM 1 AND 2 CHECK OK WITH NO FAULTS. NO EICAS MESSAGES. ACFT OK TO CONTINUE SERVICE.
2016
Part: SEAL — FAILED (NLG STRUT) · airframe 12,380 hrs · 8,058 cycles
SHORTLY AFTER TAKEOFF, AFTER GEAR RETRACTION, CREW RECEIVED A LG WOW SYS FAIL EICAS MESSAGE. EMERGENCY DECLARED, DECISION WAS MADE TO RETURN TO DEPARTURE. ACFT LANDED UNEVENTFULLY. AFTER TROUBLESHOOTING FOUND THAT THE NLG STRUT SEAL FAILED. R & R NLG STRUT SEALS.
Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM CORROSION FRAME 14, RBL 31-31.75"; FLOORBEAM REPAIR IAW E16-064-01.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM FRAME 17 CORROSION FROM RBL 17.0-42.0"; REPAIR CROSSBEAM IAW E16-056-01.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM AT FRAME 17 CORROSION FROM RBL 17.0-42.0"; REPAIR FLOORBEAM IAW E16-056-01.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM FRAME 17 CORROSION FROM RBL17.0-42.0"; REPAIR CROSSBEAM IAW E16-056-01.
Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM CORROSION FRAME 14, RBL 13.5-13.75"; REPAIR FLOORBEAM IAW E16-064-01.
Part: SEAT TRACK — CORRODED (FRAMES 13-17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
RIGHT SEAT TRACK CORRODED FROM 4" AFT FRAME 13 TO 4" AFT FRAME 17, RBL 12.5"; R & R NEW SEAT TRACK IAW SRM 51-41-01, 53-10-10, FIG 56A, ITEM 270.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM FRAME 17 CORROSION FROM RBL 17.0 -42.0"; REPAIR CROSSBEAM IAW E16-056-01.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM AT FRAME 17 CORROSION FROM RBL 17.0-42.0"; REPAIRED IAW E16-056-01.
Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 10,841 hrs · 6,967 cycles
FLOORBEAM CORROSION FRAME 17 FROM RBL 17.0 -42.0"; CROSSBEAM REPAIR IAW E16-056-01.
2013
Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 4,670 hrs · 2,937 cycles
CREW DECLARED AN EMERGENCY, EICAS SLAT FAIL MESSAGE LEVELING AT CRUISE 340. PERFORMED FIM TASK 27-83-00-810-814-A, R & R OTBD SLAT SKEW SENSOR AT SLAT PANELS 2/3 IAW AMM 27-83-01. OPS CHECK NORMAL.
Part: I/O MODULE — FAILED (MAU) · airframe 2,160 hrs · 1,283 cycles
FLT 1731 JFK-BDA, AIR RETURN TO JFK DUE TO HF INOP. HF RADIO VERY GARBLED AND UNREADABLE TRANSMIT FUNCTIONS. READABLE ON THE OTHER END (HIGH FREQUENCY (HF) COMMUNICATION SYS). REMOVED AND REPLACED CONTROL I/O MODULE IN MAU NR 1 CARD 6 IAW AMM 31-41-05. PERFORMED OPS TEST OF HF SYSTEM, OPS CHECK GOOD.