# Service difficulty reports: N272WA, cancelled May 30, 2018

A list on [N272WA, cancelled May 30, 2018](https://openairdocs.org/deregistered/N272WA-2018-05-30.md).

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

Page 1 of 2 · 71 reports

- [SDR WRLA20130922602](https://openairdocs.org/sdr/WRLA20130922602.md): Apu · shutdown · Sep 22, 2013 · N272WA · Doug MD11 · APU Core Engine
  > DURING DEPARTURE, APU SHUTDOWN AT NR2 ENGINE START. ENGINE AROUND 22 PERCENT N2 WHEN APU STARTED TO ROLL BACK AND COULD NOT SUSTAIN THE ENGINE START. SHUT IT DOWN AND REQUESTED AN AIR START. GROUND PERSONNEL REPORTED SMOKE COMING FROM THE NR 2 ENGINE. MX
- [SDR WRLA20130304586](https://openairdocs.org/sdr/WRLA20130304586.md): Door · nicked · Mar 4, 2013 · N272WA · Doug MD11 · Wing, Plate/Skin
  > CRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND TWO NICKS ON THE SKIN OF LEFT WING SLAT ACTUATOR DOOR PANEL 518FB.
- [SDR WRLA20130304585](https://openairdocs.org/sdr/WRLA20130304585.md): Skin · corroded · Mar 4, 2013 · N272WA · Doug MD11 · Fuselage Main, Plate/Skin
  > CRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON THE UPPER SURFACE OF FWD UNDERWING BARREL LOWER SKIN BETWEEN STA 1521 AND STA 5-00/1531, LONGERON 51R AND 50R.
- [SDR WRLA20130301584](https://openairdocs.org/sdr/WRLA20130301584.md): Longeron · cracked · Mar 1, 2013 · N272WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > CRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON THE LONGERON L-40R AT STA Y=1987.
- [SDR WRLA20130301583](https://openairdocs.org/sdr/WRLA20130301583.md): Seat Track · cracked · Mar 1, 2013 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON CABIN SEAT TRACK AT STA Y=522, X=-75.25.
- [SDR WRLA20130301582](https://openairdocs.org/sdr/WRLA20130301582.md): Skin · cracked · Mar 1, 2013 · N272WA · Doug MD11 · Fuselage Main, Plate/Skin
  > CRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON UPPER SKIN UPPER SURFACE OF CENTER WING AT STA Y=1240, X=107.25 AND STA Y=1250, X=107.25.
- [SDR WRLA20120602546](https://openairdocs.org/sdr/WRLA20120602546.md): Skin · gouged · Jun 2, 2012 · N272WA · Doug MD11 · Fuselage Main, Plate/Skin
  > GOUGE / DENT FOUND DURING PRIMARY INSPECTION AT FUSELAGE STA 755 L-24 & L25 MEASURED 3.00 X.133. ACCOMPLISHED HFEC INSPECTION ON DENT, NO CRACKS FOUND FOLLOWING BLEND-OUT OF THE EFFECTED AREA ACCOMPLISHED UT INSPECTION OF EFFECTED AREA AND FOUND SKIN THICKNE
- [SDR WRLA20111020524](https://openairdocs.org/sdr/WRLA20111020524.md): Light · no test · Oct 20, 2011 · N272WA · Doug MD11 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED.
- [SDR WRLA20111009523](https://openairdocs.org/sdr/WRLA20111009523.md): Strap · cracked · Oct 9, 2011 · N272WA · Doug MD11 · Wing Miscellaneous Structure
  > STRAP ON RT WING L/E CRACKED FROM BOLT HOLE ABOUT 1" XOS 608. REMOVED DAMAGED STRAP IAW SRM 51-35-01 REV.47. FABRICATED STRAP IAW EI W2011P57B-2164 REV 00 AND REV 01. REPLACED DAMAGED STRAP IAW SRM 51-35-01 REV 47.
- [SDR WRLA20111009522](https://openairdocs.org/sdr/WRLA20111009522.md): Skin · cracked · Oct 9, 2011 · N272WA · Doug MD11 · Wing, Plate/Skin
  > RT WING SKIN SURFACE L/E CRACKED. REPAIRED CRACK IAW EI W2011A57B-2156, REV 00 AND REV 01.
- [SDR WRLA20111007521](https://openairdocs.org/sdr/WRLA20111007521.md): Skin · cracked · Oct 7, 2011 · N272WA · Doug MD11 · Wing, Plate/Skin
  > DURING 3C+A12 CHECK, A 0.5 INCH CRACK WAS FOUND ON RT WING L/E SKIN AT LWS 889. REPAIRED CRACK IAW EI W2011A57B-2129 REV.00, REV.01 AND REV.02.
- [SDR WRLA20111005519](https://openairdocs.org/sdr/WRLA20111005519.md): Intercostal · cracked · Oct 5, 2011 · N272WA · Doug MD11 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED STA 2141, L9R. PERFORMED EI NO: W2011A53B-2141 REV.00 AND REV.01.
- [SDR WRLA20111005520](https://openairdocs.org/sdr/WRLA20111005520.md): Door · damaged · Oct 5, 2011 · N272WA · Doug MD11 · Air Conditioning Doors
  > REMOVE EXISTING DOUBLER FOR INSPECTION DUE NO REPAIR DOCUMENTATION. AIR CONDITIONING EQUIP SYS 3 ACCESS DOOR UPPER FWD DOOR CORNER SKIN REF: EGAT N/R U05004. RMV THE DOUBLER IAW SRM 51-35-01 REV. 47. REPAIR DAMAGED AREA IAW SRM 52-40-01. REPAIR 1 FIGURE 201
- [SDR WRLA20111004516](https://openairdocs.org/sdr/WRLA20111004516.md): Structure · damaged · Oct 4, 2011 · N272WA · Doug MD11 · Cargo/Baggage Doors
  > AFT CARGO DOOR LWR AFT CORNER DAMAGED. REPAIRED DAMAGE AREA IAW EI: W2011A52B-2148 REV. 00, REV.01 REV.02.
- [SDR WRLA20111003518](https://openairdocs.org/sdr/WRLA20111003518.md): Trunnion · cracked · Oct 3, 2011 · N272WA · Doug MD11 · Fuselage, Landing Gear Attach Fittings
  > FOUND NOSE LANDING GEAR TRUNNION FITTING ON LT SIDE HAS CRACK STA Y=595 L=0.6. REPAIRED IAW SRM 53-10-14, REPAIR 2, FIG 202, REV. 47 AND EI W2011A53B-2159. REV. 00
- [SDR WRLA20111003515](https://openairdocs.org/sdr/WRLA20111003515.md): Seat Track · corroded · Oct 3, 2011 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND LT MAIN DECK SEAT TRACK CORROSION STA Y535 X = 75.25. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 1 REV.47 AND EI W2011A53B-2224, REV.00.
- [SDR WRLA20111003514](https://openairdocs.org/sdr/WRLA20111003514.md): Seat Track · corroded · Oct 3, 2011 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RT MAIN DECK SEAT TRACK STA Y = 535 X = 75.25. REPLACED DAMAGED TRACK WITH NEW PART IAW SRM 53-33-01 AND 51-35-01 REV 47.
- [SDR WRLA20101011454](https://openairdocs.org/sdr/WRLA20101011454.md): Engine · overtemp · Oct 11, 2010 · N272WA · Doug MD11 · Engine (Turbine/Turboprop)
  > GOING THRU FLT LVL 220 HAD NR 1 ENG SURGE PULLED BACK THOTTLES RETURNED TO HIK.
- [SDR WRLA20100217344](https://openairdocs.org/sdr/WRLA20100217344.md): Fitting · corroded · Feb 17, 2010 · N272WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DURING PERFORM TASK CARD WA3209, FOUND STA 1986 S50L SHEAR CLIP CORROSION. RE-IDENTIFY THE DEFECT POSITION IS STA 1975 S-51L, REPLACED THE SHEAR CLIP P/N AGA8002-19 IAW SRM 15-33-01 REV 42M, CONDITION SATISFACTORY.
- [SDR WRLA20100211343](https://openairdocs.org/sdr/WRLA20100211343.md): Fitting · cracked · Feb 11, 2010 · N272WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING PERFORM TASK CARD WA5750, FOUND RT WING LOWER WINGLET FWD FITTING (ARB7772-70) CRACKED, ISSUED NRC U01048. REMOVED AND KEPT THE WINGLET AND THE ATTACHING PARTS, REPLACE THE WINGLET FWD FITTING ACCORDING EI W2010A57B-494 REV 00, INSTALL THE RIGHT WING L
- [SDR WRLA20100210342](https://openairdocs.org/sdr/WRLA20100210342.md): Seat Track · corroded · Feb 10, 2010 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORM TASK CARD WA3603, FOUND MAIN DECK SEAT TRACK P/N S4929147 CORROSION AT STA 1838, X=-27.5, Z=-10.5. NRC U05117 ISSUED. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52. REPAIR 1 FIGURE 201 REV 42, COND SATISFACTORY.
- [SDR WRLA20100210339](https://openairdocs.org/sdr/WRLA20100210339.md): Seat Track · corroded · Feb 10, 2010 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORM TASK CARD WA3603, FOUND MAIN DECK SEAT TRACK P/N S4929147 CORROSION AT STA 1836, X=27.5, Z=-10.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 FIGURE 201 REV 42. CONDITION SATISFACTORY.
- [SDR WRLA20100210338](https://openairdocs.org/sdr/WRLA20100210338.md): Seat Track · corroded · Feb 10, 2010 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORM TASK CARD WA 3603 FOUND MAIN DECK SEAT TRACK P/N S4929147 CORROSION AT ST 1838 X = -8.50 Z=10.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 FIGURE 201 REV 42. CONDITION SATISFACTORY.
- [SDR WRLA20100207341](https://openairdocs.org/sdr/WRLA20100207341.md): Spar Cap · corroded · Feb 7, 2010 · N272WA · Doug MD11 · Wing Spar
  > DURING PERFORM TASK CARD WA5729 FOUND LEFT WING REAR SPAR UPPER CAP P/N ARB7413-1 CORROSION AT XW840 NRC. BLENDOUT THE CORROSION AREA AND THE DAMAGE WITHIN ALLOWABLE LIMITS IAW SRM 57-00-10 FIG 101 REV 42, APPLY PROTECTIVE COATING, COND CHECK NORMAL.
- [SDR WRLA20100207340](https://openairdocs.org/sdr/WRLA20100207340.md): Spar Cap · corroded · Feb 7, 2010 · N272WA · Doug MD11 · Wing Spar
  > DURING PERFORM TASK CARD WA5729, FOUND LEFT WING REAR SPAR UPPER CAP P/N ARB7413-1 CORROSION ST XW899 NRC. RE-IDENTIFY THE CORROSION AREA IS AT XORS 1052 AND PFM EI: W2010A57B-383 REV00 REPAIR CORROSION ON LT WING REAR SPAR UPPER CAP UPPER SURFACE AT XORS 105
- [SDR WRLA20100204337](https://openairdocs.org/sdr/WRLA20100204337.md): Fitting · cracked · Feb 4, 2010 · N272WA · Doug MD11 · Wing Miscellaneous Structure
  > DURING PERFORM TASK CARD WA3007, FOUND RT WING TIP FITTING ARB7602-R CRACKED. PER AMM 20-50-02-900-801 REV 66 REPLACED THE FITTING, CONDITION SATISFACTORY.
- [SDR WRLA20100204336](https://openairdocs.org/sdr/WRLA20100204336.md): Seat Track · corroded · Feb 4, 2010 · N272WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERFORM TASK CARD WA3603, FOUND MAIN DECK SEAT TRACK AFA7789-541 CORROSION AT STA 1962 X=107.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 PAGE 203 REPAIR I REV 42. CONDITION CHECK SATISFACTORY.
- [SDR WRLA20100204335](https://openairdocs.org/sdr/WRLA20100204335.md): Rib · cracked · Feb 4, 2010 · N272WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING PERFORM TASK CARD WA5750, FOUND LEFT LOWER WINGLET RIB ARB7774-5 CRACKED. REPLACED THE DAMAGE RIB IAW MD-11 SRM 51-35-01 REV 42, CONDITION CHECK SATISFACTORY.
- [SDR WRLA20100204334](https://openairdocs.org/sdr/WRLA20100204334.md): Rib · cracked · Feb 4, 2010 · N272WA · Doug MD11 · Wing, Rib/Bulkhead
  > DURING PERFORM TASK CARD WA5750, FOUND LEFT LOWER WINGLET RIB ARB7774-51 CRACKED. REPAIRED THE CRACK AREA AT LT LWR WINGLET FWD FITTING ASSY RIB IAW SRM 57-00-00 FIG 205 REV 42, COND CHECK NORMAL.
- [SDR WRLA2009001](https://openairdocs.org/sdr/WRLA2009001.md): Engine · defective · Jan 1, 2009 · N272WA · Doug MD11 · Engine (Turbine/Turboprop)
  > IN CRUISE RECEIVED A LVL 2 ENG 2 OIL FILTER ALERT. NOTICED INCREASING EVM COMP INDICATION AND RECIEVED A LVL 1 ENG 2 VIB HI ALERT. LATER MODERATE A/C VIB NOTICED, EVM COMP OF 5.0, A LVL 2 SEL FADEC ALT ALERT AND A DROP IN N1 OF NR 2 ENG COMPLETED IFSD PROCEDUR
- [SDR WRLA2008105](https://openairdocs.org/sdr/WRLA2008105.md): Flap · debonded · Dec 8, 2008 · N272WA · Doug MD11 · Trailing Edge Flaps
  > DURING 1C+12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP VANE LOWER SKIN DISBOND AT XOFH=499 ~ XOFH=533 (34 X 9.5), REFER TO EGAT NRC U01027. OPEN
- [SDR WRLA2008104](https://openairdocs.org/sdr/WRLA2008104.md): Repair · debonded · Dec 8, 2008 · N272WA · Doug MD11 · Trailing Edge Flaps
  > DISBOND-DURING 1C+12A CHK, EGAT MECHANIC FOUND LEFT WING INBOARD FLAP VANE LWR SKIN EXISTING REPAIR DISBOND & EXTEND TO THE ORIGINAL SKIN AT XIFH=152~XIFH=213(61 X 19), THE EXISTING REPAIR:(70 X31) AND XIFH=243~XIFH=258 (15X23) REFER TO EGAT NRC U01026. OPEN
- [SDR WRLA2008073](https://openairdocs.org/sdr/WRLA2008073.md): Skin · corroded · Aug 26, 2008 · N272WA · Doug MD11 · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND FUSELAGE SKIN AND REINFORCING DOUBLER CORRODED AT AFT LAV EXHAUST PORT STA 1959 BETWEEN LONGERONS LS9R AND L40R. CORRECTIVE ACTION: REF. DELTA ERA 47026114 REMOVED DAMAGED AREA, PERFORMED HF EDDY CURRENT INSPECTION AS REQUIRED, FABRICA
- [SDR WRLA2008022](https://openairdocs.org/sdr/WRLA2008022.md): Sensor · malfunctioned · Feb 11, 2008 · N272WA · Doug MD11 · Leading Edge Slat Position Indicating System
  > DURING APPROACH RECEIVED SLAT DISAGREE ALERT, FOLLOWED BY STICK SHAKER. PERFORMED SLAT DISAGREE CHECKLIST, DIVERTED TO KPSM DUE TO RUNWAY CONDITIONS. EMERGENCY DECLARED. REPLACED SLAT POS. SENSORS D1-17 AND D1-18 PER MM 27-84-02. PERFORMED THE SLAT RANGE OF
- [SDR WRLA2008017](https://openairdocs.org/sdr/WRLA2008017.md): Skin · cracked · Feb 1, 2008 · N272WA · Doug MD11 · Trailing Edge Flaps
  > DURING A CHECK INSPECTION 9 INCH CRACK FOUND RIGHT WING INBOARD FLAP UPPER SKIN INBOARD AFT SKIN PANEL AT XIFH231.2. REPAIRED PER MD-11 SRM 57-20-00 VOL 1 REF ERA 466462-14.
- [SDR WLDA200428](https://openairdocs.org/sdr/WLDA200428.md): Valve · failed · Jun 14, 2004 · N272WA · Doug MD11 · Aircraft Fuel Distribution System
  > AIRCRAFT N272WA FLT. NR WOA584 ON TAKEOFF ROLL, (TANK WING OVERFILL)LEVEL TWO ALERT, CREW ABORTED TAKEOFF TAXIED BACK TO THE GATE. MECHANIC FOUND NR 1 FILL VALVE FAILD, REPLACED THE VALVE SYSTEM CHECK NORMAL.
- [SDR WRLA200418](https://openairdocs.org/sdr/WRLA200418.md): Pump · failed · Apr 23, 2004 · N272WA · Doug MD11 · Hydraulic Pump (Electric/Engine), Main
  > NR 1 HYDRAULIC SYSTEM FAIL INFLIGHT, THE CREWS CONTINUED TO DESTINATION AND FOLLOWED STANDARD EMERGENCY PROCEDURE. AT KBWI MAINTENANCES FOUND NR 1 ENGINE RT HYD. DRIVEN PUMP INOP. THEY REMOVED AND REPLACED NR 1 ENGINE BOTH RT & LT EDP. OP'S & LEAKS CHECK NORM
- [SDR WRLA200316](https://openairdocs.org/sdr/WRLA200316.md): Pump · cracked · Jul 16, 2003 · N272WA · Doug MD11 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC 1 SYSTEM FAILED IN FLIGHT. AIRCRAFT DESTINATION WAS CHANGED FROM BGR TO ATL FOR REPAIRS. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS RAN ENGINES FOUND NO LEAKS. REMOVED AND REPLACED FILTER PER MM. REPLACE ENGINE DRIVEN HYDRAULIC PUMPS. (
- [SDR WRLA200215](https://openairdocs.org/sdr/WRLA200215.md): Actuator · inoperative · Jul 2, 2002 · N272WA · Doug MD11 · Aileron Control System
  > AILERON DEFLECT DISAGREE LEVEL ALERT AFTER TAKE OFF AND AT SLAT RETRACT. SLATS AND FLAPS (15) RECYCLED WITH ALERT REMAINING. CONFIG. PAGE AND VISUAL SCAN CONFIRMED LEFT OUTBOARD AILERON WAS DEFLECTED. CHECK LIST PREFORMED AND RETURNED TO STATION. ENTERED I
- [SDR WRLA200208](https://openairdocs.org/sdr/WRLA200208.md): Fire Loop · malfunctioned · Mar 17, 2002 · N272WA · Doug MD11 · Fire Detection
  > ABORTED TAKEOFF DUE TO NR 1 ENGINE FIRE DETECTOR LIGHT, FDCU FAUTL 'PYLON FIRE DETECTOR ASSEMBLY B' LOOP B FAULT. (M)
- [SDR 20000412SH010](https://openairdocs.org/sdr/20000412SH010.md): Brake · damaged · Feb 17, 2000 · N272WA · Doug MD11 · Landing Gear Brake System
  > BRAKE ASSY WAS RECEIVED FROM AIR CARRIER FOR AN OVERHAUL SERVICE. UPON DISASSEMBLY, IT WAS IDENTIFIED THE AFFECTED BRAKE SUFFERED AN EXTREME CARBON OXIDATION BREAK-DOWN ON THE INNER DIAMETER OF THE HEAT SINK. SUBMITTER SUGGESTED AN ANALYSIS OR REVIEW OF THE
- [SDR WRLA99001](https://openairdocs.org/sdr/WRLA99001.md): Shutoff Valve · failed · Feb 14, 2000 · N272WA · Doug MD11 · Hydraulic System, Main
  > DURING CLIMB OUT FROM WIKB, ''HYDRAULIC 3 ELEVATOR OFF'' LEVEL 1 ALERT ILLUMINATED. HYDRAULIC QTY STABILIZED AT 4.8 GALLONS. THIRTY MINUTES LATER ''HYDRAULIC QTY 3 LOW'' ALERT LEVEL 2 ILLUMINATED FOLLOWED BY ''HYDRAULIC FAIL'' LEVEL 3 ALERT. EMERGENCY PROCED
- [SDR WRLA99022](https://openairdocs.org/sdr/WRLA99022.md): Blade · bent · Nov 9, 1999 · N272WA · Doug MD11 · Turbine Engine Compressor Section
  > DURING FLT, NR 3 ENGINE SHUTDOWN DUE TO VIBRATION, VIBRATION MONITOR AT 5 FOR COMPRESSOR DURING T/O. VIBRATION MONITOR REDUCED TO 2.5 AT LOWER RPM IAW FCOM VOL I PROCEDURES FUEL WAS DUMPED TO MAXIMUM LANDING WEIGHT (85,000 LBS) AND A/C RETURNED TO SSN WITHOUT
- [SDR WRLA990](https://openairdocs.org/sdr/WRLA990.md): Relay · failed · Apr 9, 1999 · N272WA · Doug MD11 · AC Power Distribution System
  > NR 2 BUS TIE RELAY FAILED CAUSING LOSS OF NR 2 GENERATOR BUS DURING FLIGHT RESULTING IN AN AIR TURNBACK TO WMKK. MAINTENANCE REMOVED AND REPLACED NR 2 BUS TIE RELAY AND THE ELECTRICAL POWER CONTROL UNIT. OPERATIONAL CHECKS OF THE SYSTEM CHECKED OK. (M)
- [SDR WRLA99017](https://openairdocs.org/sdr/WRLA99017.md): Idg · failed · Apr 8, 1999 · N272WA · Doug MD11 · AC Generator-Alternator
  > NR 2 IDG FAULTED ON ENGINE START, REPORTED BY FLIGHT CREW. DOWN POWERED AIRCRAFT AND THEN RESET FAULT THROUGH CFDS. SYSTEM THEN OPS CHECK OK. (M)
- [SDR WRLA99013](https://openairdocs.org/sdr/WRLA99013.md): Dme · overheated · Feb 25, 1999 · N272WA · Doug MD11 · DME/TACAN System
  > FLT 5129 - DURING CRUISE, FLIGHT CREW NOTED LIGHT SMOKE AND BURNING ELECTRICAL SMELL IN COCKPIT. ADDITIONALLY, NR 2 DME CIRCUIT BREAKER POPPED. SMOKE APPEARED IN VICINITY OF CAPTAIN'S OVERHEAD MAP LIGHT. NON-ESSENTIAL OVERHEAD LIGHTING WAS SWITCHED OFF. DM
- [SDR WRLA98090](https://openairdocs.org/sdr/WRLA98090.md): Connector · contaminated · Aug 7, 1998 · N272WA · Doug MD11 · AC Power Distribution System
  > DURING TAXI FOR TAKEOFF, FLIGHT CREW WAS UNABLE TO OBTAIN ELECTRICAL POWER FROM NR 2 ENGINE IDG. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND ELECTRICAL CANNON PLUG ON
- [SDR WRLA98083](https://openairdocs.org/sdr/WRLA98083.md): Duct · loose · May 2, 1998 · N272WA · Doug MD11 · Pneumatic Distribution System
  > DURING T/O ROLL, NR 2 ENG EXPERIENCED HIGH EGT. FLT CREW ELECTED TO ABORT T/O. A/C RETURNED TO GATE W/O INCIDENT. HOWEVER, WHILE A/C WAS STANDING ON GATE 4 MAIN WHEEL ASSY'S LOST AIR PRESS DUE TO THERMAL PLUG RELEASE. MX PERSONNEL COOLED A/C BRAKES, AND RE
- [SDR WRLA97146](https://openairdocs.org/sdr/WRLA97146.md): Light · shorted · Dec 3, 1997 · N272WA · Doug MD11 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, MAINTENANCE PERSONNEL NOTED EMERGENCY FLOOR TRACKING WOULD NOT ILLUMINATE. MAINTENANCE PERSONNEL REPLACED SHORTED EGRESS MODULES AT ROWS 17 AND 24 DE. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR WRLA97046](https://openairdocs.org/sdr/WRLA97046.md): Light · inoperative · Jul 5, 1997 · N272WA · Doug MD11 · Emergency Lighting
  > DURING MAINTENANCE PREFLIGHT, MAINTENANCE PERSONNEL IDENTIFIED EMERGENCY ESCAPE PATH LIGHTING STRIPS WERE INOPERATIVE IN 'C' ZONE. MAINTENANCE PERSONNEL IDENTIFIED A SHORTED WIRE IN LIGHT STRIP. REPAIRED SHORT IN WIRE. OPS CHECK PERFORMED WITHOUT FAULT. AI

Next page: https://openairdocs.org/deregistered/N272WA-2018-05-30/reports.md?page=2

## 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 = 'N272WA' AND deregistration_id = 'N272WA-2018-05-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N272WA-2018-05-30/reports

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