# N273WA: 1993 Mcdonnell Douglas MD-11, registration cancelled 2017-02-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 16, 2017
- Status when cancelled: First renewal notice
- Airframe: [Mcdonnell Douglas MD-11](https://openairdocs.org/model/mcdonnell-douglas-md-11) (registry code 3023602)
- Engine: [Pratt & Whitney PW4000 series](https://openairdocs.org/engine/pratt-whitney-pw4000-series) (registry code 52119)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs)
- Serial number: 48519
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 15, 1993
- Certificate issued: April 21, 2014
- Last registry action: April 21, 2014
- Mode S code: A2B396
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N273WA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=273WA
- Page: https://openairdocs.org/deregistered/N273WA-2017-02-16

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas MD-11: https://openairdocs.org/model/mcdonnell-douglas-md-11.md

## Service difficulty reports (195, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR WRLA20130224579](https://openairdocs.org/sdr/WRLA20130224579), Feb 24, 2013: UNKNOWN. SMOKE. AIR RETURN - SMOKE IN COCKPIT. REMOVED ALL DU'S, GLARESHIELD, AND OPENED ALL CB PANELS FOR INSPECTIONS. FOUND NO CHAFING WIRES OR BURN INDICATIONS. PERFORMED RT
- [SDR WRLA20121229577](https://openairdocs.org/sdr/WRLA20121229577), Dec 29, 2012: BATTERY PACK. FAILED. DURING PRE-FLIGHT INSPECTION FOUND NR 2 EMERGENCY BATTERY PACK FAILED TEST (NOTE: NR 2 BATTERY PACK REMOVED). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 
- [SDR WRLA20120524545](https://openairdocs.org/sdr/WRLA20120524545), May 24, 2012: STRUCTURE. CORRODED. CORROSION ON TOP OF CENTER WING BOX AT STA 1249 BETWEEN X=75.25 AND X=709.25 RT.
- [SDR WRLA20120521544](https://openairdocs.org/sdr/WRLA20120521544), May 21, 2012: FITTING. CRACKED. CRACK - FOUND NOSE LANDING GEAR TRUNNION FITTING ON LEFT SIDE HAD CRACK STA Y=595 L=0.5". IAW AMM 32-21-01-000-801 REV B REMOVED NOSE LANDING GEAR ASSY. REPAIR 
- [SDR WRLA20110806499](https://openairdocs.org/sdr/WRLA20110806499), Aug 6, 2011: VENT. CORRODED. AFT RT FUSELAGE FWD LAV EXH VENT CORRODED AND POPPED RIVET AT 6 O'CLOCK POSITION. FWD VENT STA 1895 BETWEEN LONGERON 39 AND 40 RT.
- [SDR WRLA20100907451](https://openairdocs.org/sdr/WRLA20100907451), Sep 7, 2010: STANCHION. BROKEN. BROKEN-- STA 6-70 X=42 STANCHION A6A7094-11 BROKEN. NRC U05087 ISSUED.
- [SDR WRLA20100907450](https://openairdocs.org/sdr/WRLA20100907450), Sep 7, 2010: STANCHION. DEFORMED. DEFORM--STA 6-70 X=29 STANCHION A6A7094-7 DEFORM. NRC U05086 ISSUED.
- [SDR WRLA20100907449](https://openairdocs.org/sdr/WRLA20100907449), Sep 7, 2010: STANCHION. DEFORMED. DEFORM-- STA6-70 X=-29 STANCHION A6A7094-15 DEFORM. NRC U05090 ISSUED.
- [SDR WRLA20100907448](https://openairdocs.org/sdr/WRLA20100907448), Sep 7, 2010: STANCHION. BROKEN. BROKEN-- STA 6-70 X=-47 STANCHION A6A7094-11 BROKEN. NRC U05089 ISSUE.
- [SDR WRLA20100907447](https://openairdocs.org/sdr/WRLA20100907447), Sep 7, 2010: STANCHION. DEFORMED. DEFORM-- STA6-70 X=57 STANCHION A6A7094-13 DEFORM. NRC U05088 ISSUED.
- [SDR WRLA20100907446](https://openairdocs.org/sdr/WRLA20100907446), Sep 7, 2010: STANCHION. DEFORMED. DEFORM- STA 6-70 X=57 STANCHION A6A7094-5 DEFORM. NRC U05085 ISSUED.
- [SDR WRLA20100907445](https://openairdocs.org/sdr/WRLA20100907445), Sep 7, 2010: SKIN. CRACKED. CRACK AND CHAFING ON LT WING DROOP SLAT SKIN AT XDLE308.
- [SDR WRLA20100824443](https://openairdocs.org/sdr/WRLA20100824443), Aug 24, 2010: BATTERY PACK. DISCHARGED. NR 2 & NR 3 EMERGENCY BATTERY TEST LOW. REPLACED NR 2 EMER BATTERY PACK, NR 3 PACK CHARGED BACK TO NORMAL.
- [SDR WRLA20100120332](https://openairdocs.org/sdr/WRLA20100120332), Jan 20, 2010: SLIDE. DAMAGED. R4 EVAC SLIDE FELL FROM CONTAINER AND IS DAMAGED. REMOVED AND REPLACED R4 SLIDE.
- [SDR WRLA2009060](https://openairdocs.org/sdr/WRLA2009060), Feb 14, 2009: ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND NR 3 ENGINE PYLON PRECOOLER LT SIDE UPPER STRUCTURE ANGLE CRACKED (REF EGAT N/R U05114). REPLACED WITH NEW PART 1EA ON NR
- [SDR WRLA2009058](https://openairdocs.org/sdr/WRLA2009058), Feb 14, 2009: STIFFENER. CRACKED. DURING C-CHECK INSPECTION, FOUND CRACK ON STIFFENER ON RIGHT MLG DOOR AFT O/B JAMB ASSY Y=1472 X=115.1. REPLACED WITH NEW STIFFENER 1EA PER SRM VOL 2 51-35-01 R
- [SDR WRLA2009059](https://openairdocs.org/sdr/WRLA2009059), Feb 11, 2009: STIFFENER. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND LT MAIN GEAR W/W AFT LOWER SIDE HAS STIFFENER CRACKED TOTAL 1 EA AT STA Y=1461. REPLACED THE STIFFENER 2EA IAW SRM VOL 2 
- [SDR WRLA2009055](https://openairdocs.org/sdr/WRLA2009055), Feb 10, 2009: FITTING. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT WING T/E LOWER PANEL I/B SIDE CLIP AT XOHF453. REF EGAT N/R U05059. REMOVED AND REPLACED THE SUPPORT BRACKET 
- [SDR WRLA2009054](https://openairdocs.org/sdr/WRLA2009054), Feb 9, 2009: SUPPORT ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND LT AFTER BODY INTERCOSTAL APU DRAIN CAN SUPPORT ANGLE CRACKED AT Y: 2080 (REF EGAT N/R U05033). REPLACED WITH NEW ANGLE I
- [SDR WRLA2009051](https://openairdocs.org/sdr/WRLA2009051), Feb 9, 2009: DOUBLER. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER RT WING FIXED LEADING EDGE AT STA XOS605 (REF EGAT N/R U05122). REPLACE WITH NEW DOUBLER ON RT WING FIXE
- [SDR WRLA2009041](https://openairdocs.org/sdr/WRLA2009041), Feb 9, 2009: HINGE BRACKET. BROKEN. DURING C-CHECK IN TPE INSPECTION FOUND LT O/B FLAP INBOARD FORWARD HINGE BRACKET BROKEN. REPLACED WITH NEW BRACKET IAW SRM VOL 2 51-31-01 REV 40.
- [SDR WRLA2009048](https://openairdocs.org/sdr/WRLA2009048), Feb 8, 2009: SUPPORT ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND PANEL 15AZ - LT STA 463 X:+10 ANGLE CRACKED FORWARD AVIONICS COMPARTMENT. (REF EGAT N/R U05132). REPEAT INSPECTION AT AVI
- [SDR WRLA2009039](https://openairdocs.org/sdr/WRLA2009039), Feb 8, 2009: SUPPORT BRACKET. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND RT FUSELAGE BODY FAIRING 154GB PANEL SUPPORT BRACKET CRACKED AT STA 1521. REPLACED WITH NEW FABRICATED PART IAW EGAT EI N
- [SDR WRLA2009037](https://openairdocs.org/sdr/WRLA2009037), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 2 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 2 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009036](https://openairdocs.org/sdr/WRLA2009036), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 2 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 2 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009035](https://openairdocs.org/sdr/WRLA2009035), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 3 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 3 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009034](https://openairdocs.org/sdr/WRLA2009034), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 3 RT SPOILER PANEL UPPER SURFACE. REMOVED PANEL PER AMM 27-60-30-000-801. REPLACED UPPER SKIN PA
- [SDR WRLA2009033](https://openairdocs.org/sdr/WRLA2009033), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 4 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 4 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009032](https://openairdocs.org/sdr/WRLA2009032), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 4 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 4 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009031](https://openairdocs.org/sdr/WRLA2009031), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 5 LT SPOILER PANEL UPPER SURFACE. REMOVED NR 5 LT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009030](https://openairdocs.org/sdr/WRLA2009030), Feb 8, 2009: SKIN. DAMAGED. DURING C-CHECK IN TPE INSPECTION FOUND DENTS WITH DISBOND ON NR 5 RT SPOILER PANEL UPPER SURFACE. REMOVED NR 5 RT SPOILER PANEL PER AMM 27-60-30-000-801. REPLAC
- [SDR WRLA2009044](https://openairdocs.org/sdr/WRLA2009044), Feb 7, 2009: TEE FITTING. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND LT WING I/B AILERON LEADING EDGE O/B SIDE HAD TEE CHORD CRACKED AT XORS 412.369. REPLACED WITH NEW TEE CHORD IAW SRM VOL 
- [SDR WRLA2009045](https://openairdocs.org/sdr/WRLA2009045), Feb 7, 2009: TEE FITTING. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND TEE CHORD AT RT WING OUTBOARD FIXED T/E AT STA 412.329 NEAR I/B AILERON L/E LOCKOUT CRACKED (REF EGAT N/R U5037). REPLACE
- [SDR WRLA2009046](https://openairdocs.org/sdr/WRLA2009046), Feb 7, 2009: SUPPORT ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND PANEL SUPPORT ANGLE FOR RT WING TO BODY UPPER FAIRING CRACKED AT STA 1341 L31L (REF EGAT N/R U05040). REMOVE SUPPORT AT L
- [SDR WRLA2009047](https://openairdocs.org/sdr/WRLA2009047), Feb 7, 2009: SUPPORT ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND PANEL SUPPORT ANGLE FOR RT WING TO BODY UPPER FAIRING CRACKED AT STA 1341 L31R (REF EGAT N/R U05041). REMOVE SUPPORT AT R
- [SDR WRLA2009052](https://openairdocs.org/sdr/WRLA2009052), Feb 7, 2009: RIB. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT WING FIXED L/E PANEL RIB AT STA XORS 441. REPAIRED CRACK AREA IAW SRM 57-00-01 FIG 11 REV 40.
- [SDR WRLA2009049](https://openairdocs.org/sdr/WRLA2009049), Feb 7, 2009: SUPPORT. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND SUPPORT CRACKED BETWEEN LT FWD AND AFT AIR CONDITIONING BAYS AT STA Y =533 L33L. REF EGAT N/R U05004. REPAIRED CRACKED SU
- [SDR WRLA2009050](https://openairdocs.org/sdr/WRLA2009050), Feb 7, 2009: SUPPORT ANGLE. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT STA 420 PNL 1152AZ. REF EGAT N/R U05049. REPAIRED CRACK AREA IAW SRM 
- [SDR WRLA2009038](https://openairdocs.org/sdr/WRLA2009038), Feb 7, 2009: CHANNEL. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND AFT FUSELAGE BODY STATION YID = 310.3 X = 0.00 CHANNEL CRACK (REF EGAT N/R U05126). REPAIRED CHANNEL CRACK AREA AT BODY S
- [SDR WRLA2009053](https://openairdocs.org/sdr/WRLA2009053), Feb 6, 2009: HINGE BRACKET. BROKEN. DURING C-CHECK IN TPE INSPECTION FOUND RT O/B FLAP I/B FORWARD FAIRING HINGE BRACKET BROKEN (REF EGAT N/R U05125). REPLACED BRACKET AT RT O/B FLAP I/B FWD FAIRI
- [SDR WRLA2009043](https://openairdocs.org/sdr/WRLA2009043), Feb 6, 2009: DOOR. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND CRACK ON RT MLG DOOR AT FWD END (REF EGAT N/R U050007). REPAIRED RT FLIPPER DOOR CRACK AREA IAW SRM VOL 1 52-10-00 FIG 18
- [SDR WRLA2009042](https://openairdocs.org/sdr/WRLA2009042), Feb 6, 2009: DOOR. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND CRACK ON LT MLG FLIPPER DOOR AT FWD EDGE. REPAIRED CRACKED AREA IAW SRM VOL 1 52-10-00 FIG 18 REV 40.
- [SDR WRLA2009040](https://openairdocs.org/sdr/WRLA2009040), Feb 6, 2009: INTERCOSTAL. CRACKED. DURING C-CHECK IN TPE INSPECTION FOUND LT FORWARD AIR CONDITIONING ACCESS DOOR HAS CRACKED INTERCOSTAL (INTERNAL) AT CENTER LINE UPPER END (REF EGAT N/R U05002)
- [SDR WRLA2009057](https://openairdocs.org/sdr/WRLA2009057), Feb 5, 2009: SUPPORT FITTING. CORRODED. DURING C-CHECK IN TPE INSPECTION FOUND LT MLG RETRACT ACTUATOR SUPPORT FITTING LOWER SIDE CORROSION. FOUND DURING HEAVY LANDING INSP AS PER MANUFACTURER LETTER.
- [SDR WRLA2009056](https://openairdocs.org/sdr/WRLA2009056), Feb 5, 2009: SUPPORT FITTING. CORRODED. DURING C-CHECK IN TPE INSPECTION FOUND RT MLG RETRACT ACTUATOR SUPPORT FITTING LOWER SIDE CORROSION. FOUND DURING HEAVY LANDING INSP AS PER MANUFACTURER LETTER.
- [SDR WRLA2009029](https://openairdocs.org/sdr/WRLA2009029), Feb 3, 2009: LONGERON SPLICE. CRACKED. DURING C-CHECK INSPECTION IN TPE - FOUND AFT CARGO LONGERON SPLICE CRACKED AT STA 1521-1541, 5-44L, 5-51L & 5-47R. FABRICATED LONGERON SPLICE, REPLACED LONGERON
- [SDR WRLA2009028](https://openairdocs.org/sdr/WRLA2009028), Feb 3, 2009: LONGERON SPLICE. CRACKED. DURING C-CHECK INSPECTION IN TPE - FOUND AFT CARGO STA 5-113, 5-38L, & 5-37R LONGERON SPLICE CRACKED. REMOVED CRACKED SPLICES IAW SRM VOL 2 51-33-01. FABRICATED
- [SDR WRLA2009027](https://openairdocs.org/sdr/WRLA2009027), Feb 1, 2009: LONGERON. CRACKED. DURING C-CHECK INSPECTION IN TPE - FOUND THE FORWARD CARGO STRUCTURE LONGERON L45L CRACKED AT STA 755, .5 INCH. REPLACED WITH NEW FABRICATED SPLICE 1EA IAW SRM 
- [SDR WRLA2009026](https://openairdocs.org/sdr/WRLA2009026), Feb 1, 2009: LONGERON. CRACKED. DURING C-CHECK INSPECTION IN TPE - FOUND THE CARGO STRUCTURE LONGERON L46L CRACKED AT STA 1119 6-10. REPLACE WITH NEW FABRICATED SPLICE IAW EGAT EI W2009P53B-07
- [SDR WRLA2009025](https://openairdocs.org/sdr/WRLA2009025), Feb 1, 2009: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, FOUND SEAT TRACK CORROSION AT STA 824 + 859 X= -74.5. REPAIR THE DAMAGE SEAT TRACK PER SRM VOL I 53-70-00 PAGE 2 REV 40. REF EGAT N/R

All 195: https://openairdocs.org/deregistered/N273WA-2017-02-16/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110107002729I](https://openairdocs.org/incident/20110107002729I), Jan 7, 2011: Mcdonnell D MD-11 (N273WA), Victorville, CA, Minor damage. Captain [privacy data omitted]the PICWOA8504 and was the pilot flying (pf) during the approach and landing in vcv. According to the first officer [privacy data…

## Other aircraft with N273WA

- [Registered now](https://openairdocs.org/aircraft/N273WA): DJI AGRAS T20P, S/N 64UBL81002006B

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