# N381WA: 1992 Mcdonnell Douglas MD-11F, registration cancelled 2018-04-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 19, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600)
- 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: 48523
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 7, 2005
- Certificate issued: October 2, 2014
- Last registry action: October 2, 2014
- Mode S code: A460F6
- Owner when cancelled: [Mobility Air LLC](https://openairdocs.org/faa-owner/MOBILITY%20AIR%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7612° N, 80.1308° W: Placed by OpenAirDocs at the center of ZIP code 33109, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N381WA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=381WA
- Page: https://openairdocs.org/deregistered/N381WA-2018-04-19

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-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (48)

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

- [SDR WRLA20131118603](https://openairdocs.org/sdr/WRLA20131118603), Nov 18, 2013: SPINNER. FAILED. SPINNER CAME APART AND DAMAGED 15 C-1 FAN BLADES AND ENGINE INLET COWL. FOUND FOD TO NR 3 ENG. BLADES, SPINNER & ENG. INLET COWL. REPLACED ENG. INLET COWL, SPIN
- [SDR WRLA20130225581](https://openairdocs.org/sdr/WRLA20130225581), Feb 25, 2013: CARGO TRACK. CRACKED. DAMAGE AT SEAT TRACK IN MAIN CARGO COMPARTMENT STA 630 LBL 8. SEAT TRACK REPLACED ACC SRM 53-00-52 REV 51.
- [SDR WRLA20130225580](https://openairdocs.org/sdr/WRLA20130225580), Feb 25, 2013: CARGO TRACK. CRACKED. DAMAGE AT SEAT TRACK IN MAIN CARGO COMPARTMENT STA 630 RBL 8. SEAT TRACK REPLACED ACC SRM 53-00-52 REV 51.
- [SDR WRLA20120717551](https://openairdocs.org/sdr/WRLA20120717551), Jul 17, 2012: SKIN. CORRODED. REPAIR - CORROSION ON RIGHT WING UPPER SKIN AT XORS 163.8, STR NR 1 ~ STR NR 2. REPAIRED PER EGAT EI: W2012A57B-1780 R00 AND R01. JOB COMPLETED AND CONDITION CH
- [SDR WRLA20120716550](https://openairdocs.org/sdr/WRLA20120716550), Jul 16, 2012: SKIN. CORRODED. REPAIR - CORROSION ON RIGHT WING UPPER SKIN AT XORS 151, STR 6. REPAIRED PER EGAT EI: W2012A57B-1773 R00, R01, AND R02. JOB COMPLETED AND CONDITION CHECK NORMAL
- [SDR WRLA20120715553](https://openairdocs.org/sdr/WRLA20120715553), Jul 15, 2012: SPAR CAP. CORRODED. CORROSION ON RIGHT WING REAR SPAR UPPER CAP AT XORS 1044. REPAIRED PER EGAT EI: W2012A57B-1778 R00, R01, AND R02. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA20120715549](https://openairdocs.org/sdr/WRLA20120715549), Jul 15, 2012: SKIN. CRACKED. CRACK ON FASTENER HOLES OF THE LOWER WING SKIN AT 536AB ACCESS DOOR CUTOUT. REPAIRED PER MD-11 SRM 57-20-02 REPAIR 5 REV 50 IAW BOEING SR: 1-2256229965. CONDITI
- [SDR WRLA20120715548](https://openairdocs.org/sdr/WRLA20120715548), Jul 15, 2012: SKIN. CRACKED. CRACK ON FASTENER HOLES OF THE LOWER WING SKIN AT 636AB ACCESS DOOR CUTOUT. REPAIRED PER MD-11 SRM 57-20-02 REPAIR 5 REV 50 IAW BOEING SR: 1-2256229965. CONDITI
- [SDR WRLA20120714547](https://openairdocs.org/sdr/WRLA20120714547), Jul 14, 2012: SKIN. CORRODED. CORROSION ON RIGHT WING UPPER SKIN LEADING EDGE AT XORS 942, AFT OF FRONT SPAR. REPAIRED PER EGAT EI: W2012A57B-1729 R00 AND R01. JOB COMPLETED AND CONDITION CH
- [SDR WRLA20120710552](https://openairdocs.org/sdr/WRLA20120710552), Jul 10, 2012: SKIN. CORRODED. CORROSION ON RIGHT WING UPPER SKIN AT XORS 1060 ~ 1099. REPAIRED PER EGAT EI: W2012A57B-1776 R00, R01, AND R02. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR WRLA20110131471](https://openairdocs.org/sdr/WRLA20110131471), Jan 31, 2011: PANEL. CRACKED. UPPER TORQUE BOX PLANE PANEL STRUCTURE CRACKED STA 2020, X=-38 Z=56. REPAIRED THE DAMAGED AREA IAW MD-11 XFM 53-70-02 REV 45. CONDITION CHECKED SATISFACTORY.
- [SDR WRLA20110131470](https://openairdocs.org/sdr/WRLA20110131470), Jan 31, 2011: SKIN. CRACKED. LEFT WING INBD FLAP UPPER SKIN CRACKED. REPAIRED THE CRACK AREA IAW SRM 57-00-01 REPAIR 1 FIG 201 REV 45. CONDITION CHECKED SATISFACTORY.
- [SDR WRLA20110131469](https://openairdocs.org/sdr/WRLA20110131469), Jan 31, 2011: SEAT TRACK. WORN. M/D CARGO SEAT TRACK WORN OUT AT STA 1410 X=5.5. REPAIRED THE WORN AREA IAW SRM 53-00-52 FIG 201 REPAIR 1 REV 45. CONDITION CHECKED SATISFACTORY.
- [SDR WRLA20110129466](https://openairdocs.org/sdr/WRLA20110129466), Jan 29, 2011: FITTING. CRACKED. NOSE GEAR RT TRUNNION FITTING P/N ACA7017-502 CRACKED, NRC U05002 ISSUED. REPAIRED THE CRACK AREA IAW MD-11 SRM 53-10-14 FIG 202 REV 45 AND EI W2011A53B-232 REV
- [SDR WRLA20110129467](https://openairdocs.org/sdr/WRLA20110129467), Jan 29, 2011: TRUNNION. CRACKED. NOSE GEAR LT TRUNNION FITTING P/N ACA7017-501 CRACKED, NRC U05003 ISSUED.
- [SDR WRLA20110129465](https://openairdocs.org/sdr/WRLA20110129465), Jan 29, 2011: FITTING. CRACKED. FOUND THE FWD FITTING CRACKED AT LT WING LOWER WINGLET. NRC U01005 ISSUE.
- [SDR WRLA2009192](https://openairdocs.org/sdr/WRLA2009192), Jul 9, 2009: ACCESS PANEL. DAMAGED. DURING C-CHECK AT TPE, MAINTENANCE DISCOVERED A WORN HOLE AT FUEL TANK ACCESS DOOR PANEL 638CB. REFERENCE EGAT NRC U05066. REPAIRED HOLE PER EGAT EI NUMBER W200
- [SDR WRLA2009191](https://openairdocs.org/sdr/WRLA2009191), Jul 9, 2009: SEAT TRACK. CRACKED. DURING C-CHECK AT TPE, MAINTENANCE DISCOVERED A CRACK IN THE SEAT TRACK AT STA 755 AND X=+75.5. REFERENCE EGAT NRC NUMBER U05055. REPAIRED SEAT TRACK IN ACCORDA
- [SDR WRLA2009190A](https://openairdocs.org/sdr/WRLA2009190A), Jul 9, 2009: VANE. DEBONDED. DURING C-CHECK AT TPE, MAINTENANCE DISCOVERED TWO DISBOND AREAS ON THE RT INBOARD FLAP VANE LOWER SKIN MEASURING 21 X 15 INCHES BETWEEN XIFH 190.8 AND 205.8 AND
- [SDR WRLA2009190](https://openairdocs.org/sdr/WRLA2009190), Jul 9, 2009: FUEL TANK. CORRODED. DURING HEAVY MAINTENANCE AT EGAT, MAINTENANCE DISCOVERED CORROSION ON THE UPPER SKIN OF THE CENTER WING TANK BETWEEN STA 1229 AND 1381. REPAIR IN ACCORDANCE WIT
- [SDR WRLA2009188](https://openairdocs.org/sdr/WRLA2009188), Jun 23, 2009: LONGERON SPLICE. CORRODED. DURING C-CHK IN TPE INSP/MX FOUND CORROSION ON CTR CARGO LONGERON SPLICES HAVE CRACK AT STA 5-113-1541 L44R & L45R. A TOTAL OF 2 EA. (REF EGAT NRC U5101).
- [SDR WRLA2009187](https://openairdocs.org/sdr/WRLA2009187), Jun 22, 2009: DOUBLER. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK. CRACK ON CLG RT WHEEL WELL DOUBLER. (REF EGAT NRC U05113).
- [SDR WRLA2009186](https://openairdocs.org/sdr/WRLA2009186), Jun 22, 2009: DOUBLER. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK CRACK ON CLG LT WHEEL WELL DOUBLERS. (REF EGAT NRC U05069).
- [SDR WRLA2009185](https://openairdocs.org/sdr/WRLA2009185), Jun 20, 2009: SKIN. CORRODED. DURING C-CHK IN TPE MX/INSP FOUND CORROSION M/D CARGO FUEL TANK UPPER SKIN CORROSION LOCATION STA 1229 TO 1381 WING CENTER SECTION. PERFORMED EI W2009A57B-704 R
- [SDR WRLA2009184](https://openairdocs.org/sdr/WRLA2009184), Jun 20, 2009: LONGERON. CORRODED. DURING C-CHK IN TPE MX/INSP FOUND CORROSION CENTER CARGO LONGERON 46R HAS CORROSION AT STA 5-73. REPAIRED CORRODED AREA IAW EGAT EI W2009A53B-697 REV 00. CONDIT
- [SDR WRLA2009183](https://openairdocs.org/sdr/WRLA2009183), Jun 20, 2009: DOUBLER. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK RIGHT WING FIXED L/E XOS 546 NOSE LWR CHORD DOUBLER HAS CRACKED FROM FASTENER AREA. REMOVED CRACKED DOUBLER IAW MD11 SRM
- [SDR WRLA2009182](https://openairdocs.org/sdr/WRLA2009182), Jun 20, 2009: SEAT TRACK. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND WORN M/D CARGO SEAT TRACK WORN BEYOND LIMITS LOCATION STA 635, X=-8.5. REMOVED DAMAGED SEAT TRACK AT M/D CARGO STA 635 X=-8.5 
- [SDR WRLA2009181](https://openairdocs.org/sdr/WRLA2009181), Jun 20, 2009: SEAT TRACK. WORN. DURING C-CHK IN TPE MX/INSP FOUND WORN M/D CARGO SEAT TRACK WORN BEYOND LIMITS LOCATION STA 635, X=+27.5. REMOVED SEAT TRACK IAW SRM VOL II 51-35-01 REV 40. REP
- [SDR WRLA2009180](https://openairdocs.org/sdr/WRLA2009180), Jun 20, 2009: SEAT TRACK. WORN. DURING C-CHK IN TPE MX/INSP FOUND WORN M/D CARGO SEAT TRACK WORN BEYOND LIMITS LOCATION STA 635 X=+8.5. REMOVED DAMAGED SEAT TRACK AT M/D CARGO STA 635, X=+8.5;
- [SDR WRLA2009179](https://openairdocs.org/sdr/WRLA2009179), Jun 20, 2009: SEAT TRACK. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK FWD CARGO OVER CEILING PNL HAD SEAT TRACK CRACK STA 635 X=+47.5. REMOVED DAMAGED SEAT TRACK AT M/D CGO STA 63.5, X=+47.5
- [SDR WRLA2009178](https://openairdocs.org/sdr/WRLA2009178), Jun 20, 2009: SEAT TRACK. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK FWD CARGO OVER CEILING PNL HAD TRACK CRACK AT STA 635, X=-27.5. REMOVED SEAT TRACK IAW MD11 SRM 51-35-01 REV 40; REPAIRE
- [SDR WRLA2009177](https://openairdocs.org/sdr/WRLA2009177), Jun 20, 2009: SEAT TRACK. CRACKED. DURING C-CHK IN TPE MX/INSP FOUND CRACK FWD CARGO OVER CEILING PNL HAD SEAT TRACK CRACK AT STA 635 X-47.5. REMOVED THE DAMAGED SEAT TRACK AT M/D CGO STA635, X=-
- [SDR WRLA2009165](https://openairdocs.org/sdr/WRLA2009165), Jun 15, 2009: STIFFENER. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE ZEE STIFFENERS OF LEFT WING FIXED L/E UPPER PNL 516 ET HAVE CRACKED. PERFORMED REPAIR FOR CRACKED AREA ON STIFFENE
- [SDR WRLA2009164](https://openairdocs.org/sdr/WRLA2009164), Jun 15, 2009: STIFFENER. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE ZEE HAS CRACKED STIFFENER OF RIGHT WING FIXED L/E UPPER PNL 616FT. PERFORMED REPAIR FOR CRACKED AREA ON STIFFNER A
- [SDR WRLA2009163](https://openairdocs.org/sdr/WRLA2009163), Jun 14, 2009: SKIN. DEBONDED. DURING C-CHK IN TPE, INSP/MX FOUND DISBOND. RIGHT INBOARD FLAP VANE LOWER SKIN DISBOND 21X15 INCHES AT XIFH 190.8-205.8 AND 39X12 INCHES AT XIFH 216.8-255.8. RE
- [SDR WRLA2009162](https://openairdocs.org/sdr/WRLA2009162), Jun 14, 2009: TEE FITTING. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. AT LEFT WING FIXED T/E STRUCTURE XORS 412.329 TEE CHORD HAS CRACKED FROM JOGGLE. REPLACED LEFT WING FIXED T/E STRUCTUR
- [SDR WRLA2009161](https://openairdocs.org/sdr/WRLA2009161), Jun 14, 2009: STRAP. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE RIB STRAP AT RIGHT WING FIXED L/E NOSE CAVITY XOS 906, HAS CRACKED. REPLACED CRACKED RIB STRAP AT RT WING FIXED L/
- [SDR WRLA2009160](https://openairdocs.org/sdr/WRLA2009160), Jun 14, 2009: SKIN. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. LEFT AIR CONDITIONING BAY DOOR UPPER SKIN CRACK AT DOOR 113AL, STA 495. REMOVED THE LT FWD AIR CONDITIONING BAY DOOR; 
- [SDR WRLA2009159](https://openairdocs.org/sdr/WRLA2009159), Jun 14, 2009: RIB. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE STOP RIB OF RIGHT WING OUTBOARD T/E FLAP L/E HAS CRACKED (REF EGAT NRC U05014).
- [SDR WRLA2009158](https://openairdocs.org/sdr/WRLA2009158), Jun 14, 2009: RIB. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. STOP RIB OF LEFT WING OUTBOARD T/E FLAP L/E HAS CRACKED (REF EGAT NRC U05013).
- [SDR WRLA2009157](https://openairdocs.org/sdr/WRLA2009157), Jun 14, 2009: STRAP. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. NR 2 ENGINE EXHAUST NOZZLE FRONT STRAP CRACK 2.5 INCHES AT 6 O'CLOCK. IAW AMM 78-11-00-000-868 REV 64 AND AMM 78-11-00
- [SDR WRLA2009156](https://openairdocs.org/sdr/WRLA2009156), Jun 14, 2009: DOOR. CRACKED. DURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE LEFT MLG FLIPPER DOOR HAS CRACKED FROM THE FWD HINGE AREA. REMOVED LEFT MLG FLIPPER DOOR, PERFORMED DOOR CRACK REP
- [SDR WRLA2009155](https://openairdocs.org/sdr/WRLA2009155), Jun 14, 2009: BRACKET. CRACKED. DURING C-4 CHECK IN TPE, INSP/MX FOUND CRACK. THE BRACKET THAT FIXES THE HYD PIPING AYK7550-551 AND AYK7550-530 HAS CRACKED THE BRACKET JUST LOCATED ABOVE THE L
- [SDR WRLA2009010](https://openairdocs.org/sdr/WRLA2009010), Jan 16, 2009: STOP FITTING. CRACKED. DURING INSPECTION, FOUND DOOR R3 DOOR PLUG STOP FITTING CRACKED. REF SRT N/R 68. REPLACED FRAME PER SRM 52-12-01 REV 40 6/01/07 EDWG ADA3752-1.
- [SDR WRLA2009009](https://openairdocs.org/sdr/WRLA2009009), Jan 16, 2009: BEAM. BROKEN. DURING INSPECTION, FOUND DOOR L3 DOOR PLUG STOP FITTING BROKEN. REF SRT N/R 62. REPLACED FRAME PER SRM 52-12-01 REV 40/6/6/07 DWG ADA3752-7.
- [SDR WRLA2009005](https://openairdocs.org/sdr/WRLA2009005), Jan 11, 2009: STRINGER. CORRODED. BELOW CABIN DOOR, 3 RT, STRINGER CORRODED IN (2) POSITIONS, A08-CHECK/X-RAY, NDT. REMOVED CORROSION PER SRM 53-00-01 VOL 1 FIG 4 REV 40.
- [SDR WRLA2009003](https://openairdocs.org/sdr/WRLA2009003), Jan 11, 2009: DOOR FRAME. CORRODED. DOOR JAMB LT 3 AFT LWR CORNER, CORROSION FOUND (A08-CHECK/X-RAY, NDT. REWORKED CORROSION PER SRM 53-50-00 FIG 18 REV 40. INSTALLED PARTS PER SRM 53-50-269-87.
- [SDR WRLA2008050](https://openairdocs.org/sdr/WRLA2008050), May 24, 2008: DOUBLER. CORRODED. FOUND FUSELAGE WASTE SERVICE PANEL EXTERNAL DOUBLER CORRODED STA Y392.00 TO STA Y421.507 CENTER LINE. DOUBLER REPLACED PER SRM 51-30-00 VOL 2 REV 40.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.