- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 34030
- Year built
- 2005
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 25, 2020
- Certificate issued
- April 27, 2020
- Expires
- April 30, 2030
- Mode S code
- AAE810
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-7B model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1998 | 3 |
|---|---|
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 4 |
| 2019 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
Engine · CFM International CFM56-7B series
AD 2023-05-05Turbine Engine Compressor SectionAD 2022-02-03Turbine Engine Accessory DriveAD 2021-16-08Turbine SectionInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · CFM International CFM56-7B series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairNTSB investigations
No NTSB investigations matched to N8011AMatched 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 Boeing 737-84P aircraft
FAA incident reports
No FAA accident or incident reports matched to N8011AMatched 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 Boeing 737-84P aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SCNA20260504182Retainer · out of limits-FWD ENTRY EMERGENCY ESCAPE SYSTEM COMPARTMENT RETAINER CLIPS WITH MEASUREMENTS OUT OF LIMITS.SDR SCNA20260504181Girt Bar · bentUPPER FUSELAGE, FWD GALLEY EMERGENCY ESCAPE SLIDE PACK, GIRT BAR RETAINER CLIPS (2EA) BENT AND WITH DEFORMATION. WORK ACCOMPLISHED: WO 90084 NR13: REPLACED GIRT BAR RETAINER CLIPS (2EA) LOCATED AT FWD GALLEY EMERGENCY ESCAPE SLIDE PACK IAW BCF SRM 51-10-02SDR SCNA20260504180Door Frame · damagedFWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING WITH SHARP EDGES. DEBURRED SHARP EGES LOCATED AT FWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING IAW AC5300-1 SECTION 11-2-2 REV K DATED 05-11-2018SDR SCNA20251205462B-Nut · leakingDURING POST FLIGHT INSPECTION NR 2 WHEEL AND BRAKE ASSY WAS COATED WITH FLUID & WAS SMOKING. REQUEST INSPECTION OF NR 2 MLG. PERFORMED A HYDRAULIC SYSTEM EXTERNAL LEAKAGE CHECK IAW AMM 29-00-00, FOUND ALT BRAKE SELECTOR VALVE B-NUT LOOSE, TIGHTENED THE B-SDR SCNA20250811315Brake · leakingGROUND CREW STATED WHEEL SMOKING DURING TAXI IN. LOOKS LIKE BRAKES ARE LEAKING FLUID CAPTAIN SIDE MAIN LANDING GEAR. R&R #2 BRAKE ASSY LEAK AND OPS CHECK GOOD IAW AMM 32-41-41 OK FOR SERVICE.SDR SCNA20240806291Channel · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE LBL 25.2. ZEE CHANNEL SIDEPLATE WITH CORROSION AT SEVERAL PLACES. REPLACED FLOOR ZEE CHANNEL LH SIDE PLATE PN BAC 1496-377 FROM STA727+4" TO STA 847" LBL 21 WITH TWO REPAIR SPLICES INSTALLED FORM STA 727+6.SDR SCNA20240702260Access Panel · wornPERFORMED PERMANENT CATEGORY A REPAIR ON CENTER SECTION LOWER CHORD I/B FLANGE FROM STA 543.250" TO STA 565.250" RBL 40" I/A/W SUN COUNTRY A. ENGINEERING AUTHORIZATION 53-0204 REV. 00, AND SRM 57-10-13-2R-3 REPAIR 3 TABLE 201 FIGURE 201 AND 202. NOTE: ALSO RE
STCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56-7B series
STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineSTC SE03036CHApplication of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision.
Earlier aircraft with this N-number · 1
This aircraft carried N8011A before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.