# Service difficulty reports: N381WA, cancelled Apr 19, 2018

A list on [N381WA, cancelled Apr 19, 2018](https://openairdocs.org/deregistered/N381WA-2018-04-19.md).

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

- [SDR WRLA20131118603](https://openairdocs.org/sdr/WRLA20131118603.md): Spinner · failed · Nov 18, 2013 · N381WA · Doug MD11F · Turbine Engine Compressor Section
  > 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, SPINNER AND ALL 38 FAN BLADES, REF AMM 22-31-02. HIGH POWER ENGINE RUN C/W REF. AMM 71-00-00. ALL OPS
- [SDR WRLA20130225581](https://openairdocs.org/sdr/WRLA20130225581.md): Cargo Track · cracked · Feb 25, 2013 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Cargo Track · cracked · Feb 25, 2013 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Skin · corroded · Jul 17, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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 CHECK NORMAL.
- [SDR WRLA20120716550](https://openairdocs.org/sdr/WRLA20120716550.md): Skin · corroded · Jul 16, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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.md): Spar Cap · corroded · Jul 15, 2012 · N381WA · Doug MD11F · Wing Spar
  > 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.md): Skin · cracked · Jul 15, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20120715548](https://openairdocs.org/sdr/WRLA20120715548.md): Skin · cracked · Jul 15, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR WRLA20120714547](https://openairdocs.org/sdr/WRLA20120714547.md): Skin · corroded · Jul 14, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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 CHECK NORMAL.
- [SDR WRLA20120710552](https://openairdocs.org/sdr/WRLA20120710552.md): Skin · corroded · Jul 10, 2012 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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.md): Panel · cracked · Jan 31, 2011 · N381WA · Doug MD11F · Fuselage Main, Structure
  > 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.md): Skin · cracked · Jan 31, 2011 · N381WA · Doug MD11F · Trailing Edge Flaps
  > 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.md): Seat Track · worn · Jan 31, 2011 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Fitting · cracked · Jan 29, 2011 · N381WA · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > 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 00 REF U05002 FOR DETAIL.
- [SDR WRLA20110129467](https://openairdocs.org/sdr/WRLA20110129467.md): Trunnion · cracked · Jan 29, 2011 · N381WA · Doug MD11F · Fuselage, Landing Gear Attach Fittings
  > NOSE GEAR LT TRUNNION FITTING P/N ACA7017-501 CRACKED, NRC U05003 ISSUED.
- [SDR WRLA20110129465](https://openairdocs.org/sdr/WRLA20110129465.md): Fitting · cracked · Jan 29, 2011 · N381WA · Doug MD11F · Wing Miscellaneous Structure
  > FOUND THE FWD FITTING CRACKED AT LT WING LOWER WINGLET. NRC U01005 ISSUE.
- [SDR WRLA2009192](https://openairdocs.org/sdr/WRLA2009192.md): Access Panel · damaged · Jul 9, 2009 · N381WA · Doug MD11F · Wing, Plate/Skin
  > 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 W2009A57B-698.
- [SDR WRLA2009191](https://openairdocs.org/sdr/WRLA2009191.md): Seat Track · cracked · Jul 9, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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 ACCORDANCE WITH MD11F SRM 53-70-00, PAGE 2 REV 40.
- [SDR WRLA2009190A](https://openairdocs.org/sdr/WRLA2009190A.md): Vane · debonded · Jul 9, 2009 · N381WA · Doug MD11F · Trailing Edge Flaps
  > 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 39 X 12 INCHES BETWEEN XIFH 216.8 AND 255.8. REFERENCE EGAT NRC NR U07004. REPAIRED DISBONDED ARE
- [SDR WRLA2009190](https://openairdocs.org/sdr/WRLA2009190.md): Fuel Tank · corroded · Jul 9, 2009 · N381WA · Doug MD11F · Fuel Storage
  > 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 WITH EGAT EI NUMBER W2009A57B-704.
- [SDR WRLA2009188](https://openairdocs.org/sdr/WRLA2009188.md): Longeron Splice · corroded · Jun 23, 2009 · N381WA · Doug MD11F · Fuselage Main, Longeron/Stringer
  > 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.md): Doubler · cracked · Jun 22, 2009 · N381WA · Doug MD11F · Fuselage Miscellaneous Structure
  > 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.md): Doubler · cracked · Jun 22, 2009 · N381WA · Doug MD11F · Fuselage Miscellaneous Structure
  > 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.md): Skin · corroded · Jun 20, 2009 · N381WA · Doug MD11F · Fuel Storage
  > 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 REV00 REWORKED CORROSION ON UPPER SKIN SURFACE OF CENTER WING. CONDITION CHECK NORMAL.
- [SDR WRLA2009184](https://openairdocs.org/sdr/WRLA2009184.md): Longeron · corroded · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage Main, Longeron/Stringer
  > 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. CONDITION CHECK NORMAL.
- [SDR WRLA2009183](https://openairdocs.org/sdr/WRLA2009183.md): Doubler · cracked · Jun 20, 2009 · N381WA · Doug MD11F · Wing Miscellaneous Structure
  > 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 VOL II 51-35-01 REV 40 AT RT WING L/E XOS 546.2, FABRICATED NEW DOUBLER IAW EI W2009P57B-736 REV 0
- [SDR WRLA2009182](https://openairdocs.org/sdr/WRLA2009182.md): Seat Track · cracked · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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 IAW SRM VOL II 51-35-01 REV 40. REPAIRED AND INSTALLED SEAT TRACK IAW SRM VOL I 53-70-00 REV 40 CON
- [SDR WRLA2009181](https://openairdocs.org/sdr/WRLA2009181.md): Seat Track · worn · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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. REPAIRED SEAT TRACK IAW SRM VOL I 53-70-00 PAGE 2 REV40. INSTALLED REPAIRED PART AT M/D CGO STA 635,
- [SDR WRLA2009180](https://openairdocs.org/sdr/WRLA2009180.md): Seat Track · worn · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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; REPAIRED AND INSTALLED SEAT TRACK IAW SRM 53-70-00 REV 40. CONDITION CHECK NORMAL.
- [SDR WRLA2009179](https://openairdocs.org/sdr/WRLA2009179.md): Seat Track · cracked · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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 IAW SRM VOL II 51-35-01 REV 40. REPAIRED SEAT TRACK IAW SRM VOL I 53-70-00 PAGE 2 REV 40. INSTA
- [SDR WRLA2009178](https://openairdocs.org/sdr/WRLA2009178.md): Seat Track · cracked · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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; REPAIRED AND INSTALLED SEAT TRACK AT M/D STA 635, X=-27.5 IAW SRM 53-70-00 REV 40. CONDITION CHECK NORMAL
- [SDR WRLA2009177](https://openairdocs.org/sdr/WRLA2009177.md): Seat Track · cracked · Jun 20, 2009 · N381WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
  > 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=-47.5 IAW SRM VOL II 51-35-01 REV 40. REPAIRED SEAT TRACK IAW MD11 VOL I 53-70-00 PG 2 REV 40. INS
- [SDR WRLA2009165](https://openairdocs.org/sdr/WRLA2009165.md): Stiffener · cracked · Jun 15, 2009 · N381WA · Doug MD11F · Wing Miscellaneous Structure
  > 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 STIFFENER AT RT WING FIXED L/E UPPER PANEL 516ET IAW SRM 57-10-00 FIG 35 VOL I REV 40.2, CONDITION CHECK N
- [SDR WRLA2009164](https://openairdocs.org/sdr/WRLA2009164.md): Stiffener · cracked · Jun 15, 2009 · N381WA · Doug MD11F · Wing Miscellaneous Structure
  > 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 AT RT WING FIXED L/E UPPER PANEL 606FT IAW SRM 57-10-00 FIG 35 VOL I REV 40.2, CONDITION CHECK NORM
- [SDR WRLA2009163](https://openairdocs.org/sdr/WRLA2009163.md): Skin · debonded · Jun 14, 2009 · N381WA · Doug MD11F · Trailing Edge Flaps
  > 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. REMOVED FLAP VANE, REPAIRED THE DAMAGED AREA IAW EGAT EI W2009A57B-696 REV 00. REINSTALLED THE FLAP
- [SDR WRLA2009162](https://openairdocs.org/sdr/WRLA2009162.md): Tee Fitting · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Wing, Attach Fittings
  > 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 STRUCTURE XORS 412.329 TEE CHORD IAW SRM 51-33-01 VOL II REV 40 CONDITION CHECK NORMAL.
- [SDR WRLA2009161](https://openairdocs.org/sdr/WRLA2009161.md): Strap · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Wing, Rib/Bulkhead
  > 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/E NOSE CAVITY XOS906 WITH NEW PART IAW SRM 51-33-01 VOL II REV 40.2, CONDITION CHECK SATISFACTORY.
- [SDR WRLA2009160](https://openairdocs.org/sdr/WRLA2009160.md): Skin · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Air Conditioning Doors
  > 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; REPAIRED THE DAMAGED AREA IAW SRM VOL I 52-10-00 REV 40. CONDITION CHECK NORMAL.
- [SDR WRLA2009159](https://openairdocs.org/sdr/WRLA2009159.md): Rib · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Trailing Edge Flaps
  > 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.md): Rib · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Trailing Edge Flaps
  > 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.md): Strap · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Engine Thrust Reverser
  > 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 78-11-00-400-868 REV 64. REPLACED THE EXHAUST NOZZLE WITH NEW AND RESTORED ALL ASSEMBLY. ALL CONDITION CH
- [SDR WRLA2009156](https://openairdocs.org/sdr/WRLA2009156.md): Door · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Landing Gear Doors
  > 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 REPAIR IAW SRM VOL I 52-10-00 FIG 18. RE-INSTALLED LT MLG FLIPPER DOOR; PERFORMED SWING TEST FOR LT
- [SDR WRLA2009155](https://openairdocs.org/sdr/WRLA2009155.md): Bracket · cracked · Jun 14, 2009 · N381WA · Doug MD11F · Hydraulic System, Main
  > 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 LEFT MLG DOOR LATCH. REPLACED BRACKET IAW AMM 20-50-02-910-801 REV 64; CONDITION CHECK NORMAL.
- [SDR WRLA2009010](https://openairdocs.org/sdr/WRLA2009010.md): Stop Fitting · cracked · Jan 16, 2009 · N381WA · Doug MD11F · Service Doors
  > 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.md): Beam · broken · Jan 16, 2009 · N381WA · Doug MD11F · Service Doors
  > 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.md): Stringer · corroded · Jan 11, 2009 · N381WA · Doug MD11F · Fuselage Main, Longeron/Stringer
  > 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.md): Door Frame · corroded · Jan 11, 2009 · N381WA · Doug MD11F · Passenger/Crew Doors
  > 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.md): Doubler · corroded · May 24, 2008 · N381WA · Doug MD11F · Fuselage Main, Plate/Skin
  > 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.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N381WA' AND deregistration_id = 'N381WA-2018-04-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N381WA-2018-04-19/reports

---
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