# Service difficulty reports: N273WA, cancelled Feb 16, 2017

A list on [N273WA, cancelled Feb 16, 2017](https://openairdocs.org/deregistered/N273WA-2017-02-16.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 4 · 195 reports

- [SDR WRLA20130224579](https://openairdocs.org/sdr/WRLA20130224579.md): Unknown · smoke · Feb 24, 2013 · N273WA · Doug MD11 · Air Distribution System
  > 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 RTS OF ALL SYSTEMS THRU CFDS, ALL TESTS PASSED. REPLACED 3 COALESCER BAGS.
- [SDR WRLA20121229577](https://openairdocs.org/sdr/WRLA20121229577.md): Battery Pack · failed · Dec 29, 2012 · N273WA · Doug MD11 · Emergency Lighting
  > 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 NR 2 BATTERY IAW MM 33-51-01. OPS CHECK OK.
- [SDR WRLA20120524545](https://openairdocs.org/sdr/WRLA20120524545.md): Structure · corroded · May 24, 2012 · N273WA · Doug MD11 · Wing, Center Box
  > 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.md): Fitting · cracked · May 21, 2012 · N273WA · Doug MD11 · Fuselage, Landing Gear Attach Fittings
  > 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 THE CRACK AREA IAW SRM 53-10-14 FIGURE 202 RE. 49 REPAIR 2 IAW AMM 32-21-01-400 REINSTALLED NOSE L
- [SDR WRLA20110806499](https://openairdocs.org/sdr/WRLA20110806499.md): Vent · corroded · Aug 6, 2011 · N273WA · Doug MD11 · Air Distribution System
  > 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.md): Stanchion · broken · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > BROKEN-- STA 6-70 X=42 STANCHION A6A7094-11 BROKEN. NRC U05087 ISSUED.
- [SDR WRLA20100907450](https://openairdocs.org/sdr/WRLA20100907450.md): Stanchion · deformed · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DEFORM--STA 6-70 X=29 STANCHION A6A7094-7 DEFORM. NRC U05086 ISSUED.
- [SDR WRLA20100907449](https://openairdocs.org/sdr/WRLA20100907449.md): Stanchion · deformed · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DEFORM-- STA6-70 X=-29 STANCHION A6A7094-15 DEFORM. NRC U05090 ISSUED.
- [SDR WRLA20100907448](https://openairdocs.org/sdr/WRLA20100907448.md): Stanchion · broken · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > BROKEN-- STA 6-70 X=-47 STANCHION A6A7094-11 BROKEN. NRC U05089 ISSUE.
- [SDR WRLA20100907447](https://openairdocs.org/sdr/WRLA20100907447.md): Stanchion · deformed · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DEFORM-- STA6-70 X=57 STANCHION A6A7094-13 DEFORM. NRC U05088 ISSUED.
- [SDR WRLA20100907446](https://openairdocs.org/sdr/WRLA20100907446.md): Stanchion · deformed · Sep 7, 2010 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > DEFORM- STA 6-70 X=57 STANCHION A6A7094-5 DEFORM. NRC U05085 ISSUED.
- [SDR WRLA20100907445](https://openairdocs.org/sdr/WRLA20100907445.md): Skin · cracked · Sep 7, 2010 · N273WA · Doug MD11 · Leading Edge Devices
  > CRACK AND CHAFING ON LT WING DROOP SLAT SKIN AT XDLE308.
- [SDR WRLA20100824443](https://openairdocs.org/sdr/WRLA20100824443.md): Battery Pack · discharged · Aug 24, 2010 · N273WA · Doug MD11 · Emergency Lighting
  > 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.md): Slide · damaged · Jan 20, 2010 · N273WA · Doug MD11 · Escape Slide
  > R4 EVAC SLIDE FELL FROM CONTAINER AND IS DAMAGED. REMOVED AND REPLACED R4 SLIDE.
- [SDR WRLA2009060](https://openairdocs.org/sdr/WRLA2009060.md): Angle · cracked · Feb 14, 2009 · N273WA · Doug MD11 · Engine Oil Cooler
  > 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 3 ENGINE PRECOOLER LT SIDE UPPER IAW MD11 SRM VOL II 51-35-01 REV 40.
- [SDR WRLA2009058](https://openairdocs.org/sdr/WRLA2009058.md): Stiffener · cracked · Feb 14, 2009 · N273WA · Doug MD11 · Landing Gear Doors
  > 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 REV 40.
- [SDR WRLA2009059](https://openairdocs.org/sdr/WRLA2009059.md): Stiffener · cracked · Feb 11, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 51-35-01 REV 40.
- [SDR WRLA2009055](https://openairdocs.org/sdr/WRLA2009055.md): Fitting · cracked · Feb 10, 2009 · N273WA · Doug MD11 · Wing Miscellaneous Structure
  > 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 AT O/B FLAP I/B SIDE. FABRICATED SUPPORT PER EGAT EI W2009P57B-078 AND SRM VOL 2 51-35-01 REV 40
- [SDR WRLA2009054](https://openairdocs.org/sdr/WRLA2009054.md): Support Angle · cracked · Feb 9, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 IAW SRM 51-35-01.
- [SDR WRLA2009051](https://openairdocs.org/sdr/WRLA2009051.md): Doubler · cracked · Feb 9, 2009 · N273WA · Doug MD11 · Wing Miscellaneous Structure
  > 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 FIXED L/E AT XOS605 IAW SRM VOL 2 51-33-01 REV 40 AND EGAT EI W2009P57B-076.
- [SDR WRLA2009041](https://openairdocs.org/sdr/WRLA2009041.md): Hinge Bracket · broken · Feb 9, 2009 · N273WA · Doug MD11 · Fuselage, Door Hinge
  > 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.md): Support Angle · cracked · Feb 8, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 AVIONICS COMP STA 463 X=10, NO CRACK FOUND. REF IAW SRM VOL II 51-50-00 REV 40. REF EGAT N/R U05132.
- [SDR WRLA2009039](https://openairdocs.org/sdr/WRLA2009039.md): Support Bracket · cracked · Feb 8, 2009 · N273WA · Doug MD11 · Aerodynamic Fairings
  > 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 NO W2009P53B-081 REV 0.
- [SDR WRLA2009037](https://openairdocs.org/sdr/WRLA2009037.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 - JOB CARD 004589. REINSTALLED NR 2 LT S
- [SDR WRLA2009036](https://openairdocs.org/sdr/WRLA2009036.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PANEL ON NR 2 RT PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. REINSTALLED NR 2 RT S
- [SDR WRLA2009035](https://openairdocs.org/sdr/WRLA2009035.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 - JOB CARD 004587. RE-INSTALLED NR 3 LT
- [SDR WRLA2009034](https://openairdocs.org/sdr/WRLA2009034.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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 PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED SPOILER PANEL PER AMM 27-60-30-400-801.
- [SDR WRLA2009033](https://openairdocs.org/sdr/WRLA2009033.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED PANEL PER AMM 27-60-30-400
- [SDR WRLA2009032](https://openairdocs.org/sdr/WRLA2009032.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED PANEL PER AMM 27-60-30-400-801.
- [SDR WRLA2009031](https://openairdocs.org/sdr/WRLA2009031.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94. RE-INSTALLED NR 5 LT SPOILER PANEL PER
- [SDR WRLA2009030](https://openairdocs.org/sdr/WRLA2009030.md): Skin · damaged · Feb 8, 2009 · N273WA · Doug MD11 · Spoilers
  > 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. REPLACED UPPER SKIN SURFACE SKIN PANEL PER SRM VOL 1 57-10-00 FIG 79 REV 94 ATTACHING JOB CARD 004581.
- [SDR WRLA2009044](https://openairdocs.org/sdr/WRLA2009044.md): Tee Fitting · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Wing, Attach Fittings
  > 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 II 51-33-01 REV 40.
- [SDR WRLA2009045](https://openairdocs.org/sdr/WRLA2009045.md): Tee Fitting · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Wing Miscellaneous Structure
  > 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). REPLACED THE TEE CHORD ON RT INBOARD AILERON FIXED T/E AT STA 412.329 IAW MD-11 SRM VOL II 51-33-01 REV 40
- [SDR WRLA2009046](https://openairdocs.org/sdr/WRLA2009046.md): Support Angle · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Wing Miscellaneous Structure
  > 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 LT WING TO BODY FAIRING STA Y=1431 L31L PER SRM 51-35-01 REV 40 MD-11 VOL II. REPEAT INSPECTION AND
- [SDR WRLA2009047](https://openairdocs.org/sdr/WRLA2009047.md): Support Angle · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Wing Miscellaneous Structure
  > 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 RT WING TO BODY FAIRING STA Y=1341 L31R IAW MD SRM 51-35-01 VOL II REV. 40. REPEAT INSPECTION AND A
- [SDR WRLA2009052](https://openairdocs.org/sdr/WRLA2009052.md): Rib · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Wing, Rib/Bulkhead
  > 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.md): Support · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 SUPPORT AT LEFT AND AFT AIR CONDITIONING BAY IAW SRM VOL I 53-00-01 FIG 3 REV 40.
- [SDR WRLA2009050](https://openairdocs.org/sdr/WRLA2009050.md): Support Angle · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 VOL1 53-00-01 FIG 10 REV 40.
- [SDR WRLA2009038](https://openairdocs.org/sdr/WRLA2009038.md): Channel · cracked · Feb 7, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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 STA YID=310.3 X=0.00 IAW SRM VOL1 53-00-01 FIG 3 REV 40.
- [SDR WRLA2009053](https://openairdocs.org/sdr/WRLA2009053.md): Hinge Bracket · broken · Feb 6, 2009 · N273WA · Doug MD11 · Trailing Edge Flaps
  > 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 FAIRING HINGE IAW SRM VOL 2 51-35-01 REV 40.
- [SDR WRLA2009043](https://openairdocs.org/sdr/WRLA2009043.md): Door · cracked · Feb 6, 2009 · N273WA · Doug MD11 · Landing Gear Doors
  > 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 REV 40.
- [SDR WRLA2009042](https://openairdocs.org/sdr/WRLA2009042.md): Door · cracked · Feb 6, 2009 · N273WA · Doug MD11 · Landing Gear Doors
  > 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.md): Intercostal · cracked · Feb 6, 2009 · N273WA · Doug MD11 · Air Conditioning Doors
  > 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). REPLACED WITH NEW INTERCOSTAL IAW SRM 51-35-01 VOL 2 REV 40.
- [SDR WRLA2009057](https://openairdocs.org/sdr/WRLA2009057.md): Support Fitting · corroded · Feb 5, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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. BOLT HOLES CORRODED 3EA. REMOVED LT MLG ACTUATOR ATTACH FITTING PER AMM 32-33-20-000-301 REV 63
- [SDR WRLA2009056](https://openairdocs.org/sdr/WRLA2009056.md): Support Fitting · corroded · Feb 5, 2009 · N273WA · Doug MD11 · Fuselage Miscellaneous Structure
  > 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. BOLT HOLES CORRODED. REMOVED RT MLG ACTUATOR ATTACH FITTING PER AMM 32-33-20-000-301 REV 63 DRAW
- [SDR WRLA2009029](https://openairdocs.org/sdr/WRLA2009029.md): Longeron Splice · cracked · Feb 3, 2009 · N273WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > 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 SPLICE IAW SRM 51-33-01 VOL 2.
- [SDR WRLA2009028](https://openairdocs.org/sdr/WRLA2009028.md): Longeron Splice · cracked · Feb 3, 2009 · N273WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > 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 SPLICES PER EI W2009P53B-086. INSTALLED NEW SPLICES PER SRM 51-83-01 REV 40.
- [SDR WRLA2009027](https://openairdocs.org/sdr/WRLA2009027.md): Longeron · cracked · Feb 1, 2009 · N273WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > 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 VOL II 51-33-01 REV 40 AND EGAT EI W209P53B-075. COND CHECK NORMAL AND JOB COMPLETED. REF EGAT N/
- [SDR WRLA2009026](https://openairdocs.org/sdr/WRLA2009026.md): Longeron · cracked · Feb 1, 2009 · N273WA · Doug MD11 · Fuselage Main, Longeron/Stringer
  > 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-079 AND SRM VOL 2 51-33-01 REV 40.
- [SDR WRLA2009025](https://openairdocs.org/sdr/WRLA2009025.md): Seat Track · corroded · Feb 1, 2009 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
  > 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 U05053.

Next page: https://openairdocs.org/deregistered/N273WA-2017-02-16/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 = 'N273WA' AND deregistration_id = 'N273WA-2017-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N273WA-2017-02-16/reports

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