- Registered owner
- Trans Executive Airlines Of Hawaii Inc
- Location
- Honolulu, HI
- Owner type
- Corporation
- Serial number
- SH3746
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- January 26, 1989
- Certificate issued
- June 10, 2004
- Expires
- September 30, 2027
- Mode S code
- AB4AFA
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 71
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1984 | 2 |
|---|---|
| 1985 | 1 |
| 1986 | 6 |
| 1987 | 5 |
| 1988 | 6 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 6 |
| 1994 | 5 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 7 |
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 4 |
| 2004 | 3 |
| 2005 | 6 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 2011 | 1 |
| 2015 | 1 |
Airframe · Short Bros SD3-60
AD 2015-16-04Fire ProtectionAD 2010-24-06FuelAD 2008-16-09 R1StabilizersInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Short Bros SD3-60
SAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsNTSB investigations
No NTSB investigations matched to N827BEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Short Bros SD3-60 aircraft
FAA incident reports
No FAA accident or incident reports matched to N827BEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Short Bros SD3-60 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TXHA201407296881Hydraulic System · underservicedDURING CLIMBED OUT, AFTER PERFORMING CLIMBING CHECKLIST, THE HYDRAULIC CONTENTS GAUGE WAS IN THE MIDDLE OF THE RED ARC. THERE WERE NO CWP OR OTHER INDICATIONS. PILOT RAN THROUGH LOSS OF HYDRAULIC CONTENTS CHECKLIST. THE FIRST ITEM ON THE CHECKLIST WAS TO CLSDR TXHA2011090900001Wheel · crackedON REPOSITIONING THE ACFT, THE LT MAIN TIRE BLEW AND RIM WAS DAMAGED.SDR TXH2005F00000Skin · crackedDEFECT WAS NOTED DURING INSPECTION OF HORIZONTAL AND VERTICAL STABILIZERS. SKIN AND RIB, TOP SIDE OF RUDDER BALANCE WEIGHT ATTACHMENT AND STRUCTURAL AREA CRACKED AND CORRODED. (WP13200509006) (K)SDR TXHA6881Blade · looseON 11/5/02, POST FLIGHT INSPECTION WAS CARRIED OUT. FOUND 2 BLADES ON RIGHT PROP SN-AP37 TO HAVE EXCESSIVE FORWARD AND ACT PLAY. PROP MFG O/H FACILITY CONSULTED AND CONFIRMED PLAY TO BE EXCESSIVE. PROP REMOVED AND REPLACED. PREVENT RECURRENCE IS NOT TO USE
STCs that may be installed · 6
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Pratt & Whitney Canada PT6A-60A
STC SE01624WIConversion of Pratt & Whitney Canada, Model PT6A-60A to a North Star Aviation PT6A-60AG turboprop engine.
Data required:
1. A copy of this certificate
2. North Star Aviation document, NSA No. 1200, Turboprop Engine Conversion of PT6A-60A Model to PT6A-60AG Configuration per FAA Approved STC , dated March 15, 2011, or later FAA approved revision
3. The ICA supplement for North Star Aviation PT6A-60AG models, Instructions for Continued Airworthiness, NSA No. 1200-ICA, Rev NC, dated March 9, 2011 or later applicable revision.STC SE00014ENInstallation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models.STC SE00020ENInstallation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1STC SE01805NYInstallation of Fuel Nozzle Adapters using studs and nuts.STC SE09257SCConvert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration.STC SE659NEInstallation of oil tank filler neck check valve, P/N TSA-76A.