N349PH1997 Dehavilland DHC-8-202
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply220 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Bam Leasing LLC
- Owner type
- LLC
- City, state
- California, MD
- Certificate issued
- Jan 10, 2012
- Expires
- Jan 31, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- Aug 9, 2016
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Dehavilland
- Model
- DHC-8-202
- Year
- 1997
- Serial number
- 486
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 40
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A3E00A
Engine
- Make and model
- P&W Canada Pw123
- Type
- Turbo-prop
- Power
- 2142 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2012 – nowBam Leasing LLCCalifornia, MD · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (3)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-15-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Sep 17, 2013 | Engine (PW123)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW123)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2004-20-01 | Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B… | Nov 5, 2004 | Engine (PW123)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (220)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Hydraulic power · hydraulic line · failedOct 30, 2008
PDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3/4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN. REPLACED CRACKED NOSE GEAR DOWN LINE, CHECK GOOD. PERFORMED EDP HYD FLUID LOSS INSP IAW MM 05-50-33-280-801, NO DEFECTS. CLEANED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · pressure switch · malfunctionedOct 20, 2008
PDX- NR 2 ENG HYD PUMP CAUTION ILLUMINATED. CAUTION REMAINED ILLUMINATED THROUGHOUT LANDING. TAXI AND PARKING. NO LOSS OF HYD PRESS OR QTY. PERFORMED ALTERNATE GEAR EXTENTION. UNEVENTFUL LANDING. REMOVED AND REPLACED NR 2 HYD PRESSURE SWITCH, GROUND RAN NR 2 ENGINE. OPS CHECK AND LEAK CHECK GOOD.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Propellers · switch · malfunctionedMay 31, 2008
PDX - FLIGHT 2193, AUTOFEATHER ARM LIGHT FLICKERING AND SHOWING AS "ARM" WITHOUT THE BUTTON BEING SELECTED. DURING CLIMB AND CRUISE. MAINTENANCE REPLACED THE AUTOFEATHER SELECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine · servo · inoperativeMar 3, 2008
PDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND NR 1 ENGINE IBV SERVO INOPERATIVE, REMOVED AND REPLACE IBV SERVO COMPLETED GROUND RUNS, ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support angle · corrodedJan 14, 2008
PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X553.00 AT DOOR THRESHOLD HAS CORROSSION ON NUTPLATES AND MOUNTING SURFACE. REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND WITHIN LIMITS NO CRACKS FOUND. ALODINED PRIMED AND PAINTED INSTALLED NUTPLATES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support angle · corrodedJan 14, 2008
PDX - C CHECK - SUPPORT ANGLE AT APPROX STA X569.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS NO CRACKS NOTED. ALODINED, PRIMED AND PAINTED. INSTALLED NUTPLATES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support angle · corrodedJan 14, 2008
PDX - C CHECK - SUPPORT ANGLE AT APPROX X586.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support angle · corrodedJan 14, 2008
PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X594.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION. INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support angle · corrodedJan 14, 2008
PDX - C1 CHECK - SUPPORT ANGLE AT APPROX STA X600.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · nut plate · corrodedJan 14, 2008
PDX - C1 CHECK - NUTPLATE AND MOUNTING SURFACE AT STA X599.00 Y21.00 LT IS CORRODED. MAINTENANCE REMOVED NUTPLATE AND REMOVED CORROSION. INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER, AND PAINT. INSTALLED NEW NUTPLATE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 220 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026