# Service difficulty reports: N921WA, cancelled May 11, 2004

A list on [N921WA, cancelled May 11, 2004](https://openairdocs.org/deregistered/N921WA-2004-05-11.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 · 79 reports

- [SDR F3LA200300114](https://openairdocs.org/sdr/F3LA200300114.md): Fitting · corroded · Mar 10, 2003 · N921WA · Boeing 7372Y5 · Horizontal Stabilizer, Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED RT. HORIZONTAL STAB CENTER SECTION, AFT UPPER ATTACH CLEVIS, AFT LUG, CORRODED. REPAIRED PER EA 55-737-077.
- [SDR F3LA200300113](https://openairdocs.org/sdr/F3LA200300113.md): Door Frame · corroded · Mar 10, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR FRAME ON FUSELAGE CORRODED ON AFT SEALING SURFACE BETWEEN BOTTOM TO SECOND FROM BOTTOM STOP PAD FITTINGS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PER SRM 53-30-03, FIG. 46 AND EA 53-737-199
- [SDR F3LA200300094](https://openairdocs.org/sdr/F3LA200300094.md): Panel · corroded · Mar 2, 2003 · N921WA · Boeing 7372Y5 · Service Doors
  > DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SERVICE PANEL CORRODED AT FWD HINGE. FOUND TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED REPLACEMENT PANEL AND DOUBLER PER EA 52F-737-091. ALODINED PER SRM 51-21-41, PRIMED AND PAINTED PER SOPM 20-41-02.
- [SDR F3LA200300092](https://openairdocs.org/sdr/F3LA200300092.md): Web · corroded · Feb 26, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED LOWER WEB FROM LAVATORY FLOOR TO FUSELAGE ON LT. SIDE OF FUSELAGE CORRODED AROUND CUTOUTS, STA. 277 TO STA. 294.5. FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-10-01, 51-40-02 AND SOPM 20-41-02.
- [SDR F3LA200300091](https://openairdocs.org/sdr/F3LA200300091.md): Floorbeam · corroded · Feb 25, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM AT STA. 772, LBL 12, AT FLOOR PANEL SPLICE STRIP, BOTTOM SIDE OF UPPER FLANGE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-5 AND SOPM 20-41-02.
- [SDR F3LA200300090](https://openairdocs.org/sdr/F3LA200300090.md): Mount Bracket · cracked · Feb 25, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED FWD FUSELAGE VHF 2 ANTENNA MOUNT BRACKET CRACKED AT STA. 500, RBL 2. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2.
- [SDR F3LA200300089](https://openairdocs.org/sdr/F3LA200300089.md): Sill · corroded · Feb 25, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED R-2 DOOR RT. MOP SILL CORRODED AT VARIOUS POINTS ALONG ENTIRE LENGTH OF MOP SILL. REPLACED DAMAGED MOP SILL PER SRM 51-30-2 AND BOEING DRAWING 65-45855.
- [SDR F3LA200300088](https://openairdocs.org/sdr/F3LA200300088.md): Intercostal · corroded · Feb 25, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT/INTERCOSTAL (WEB STRAP)FROM STA. 1006 BACK, LBL 2, CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP AND GALLEY BRACKET FROM STA. 1006 TO STA. 1031, LBL 2, PER SRM 51-30-02 AND BOEING DRAWING 6
- [SDR F3LA200300087](https://openairdocs.org/sdr/F3LA200300087.md): Sill · corroded · Feb 20, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FIG. 1, SHEET 4, DETAIL I. REPLACED SILL PER SRM 51-10-2 AND SRM 51-30-02.
- [SDR F3LA200300086](https://openairdocs.org/sdr/F3LA200300086.md): Intercostal · corroded · Feb 20, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL BETWEEN STA. 927 AND STA. 947.5 ON RT. SIDE OF AIRCRAFT CENTERLINE CORRODED. REMOVED CORROSION AND INTERCOSTAL PER SRM 51-30-02. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-10-06. FABRICATED AND INSTALLED
- [SDR F3LA200300085](https://openairdocs.org/sdr/F3LA200300085.md): Floor Support · corroded · Feb 20, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO FLOOR SUPPORT CORRODED ON LOWER FLANGE AT STA. 859, RBL 8. INSTALLED REPAIR PER SRM 53-10-5 AND MM 51-21-99.
- [SDR F3LA200300084](https://openairdocs.org/sdr/F3LA200300084.md): Web · corroded · Feb 20, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED WEB BETWEEN STA. 332 AND STA. 344, AFT OF R-1 DOOR, CORRODED ON BOTTOM SIDE. REMOVED DAMAGE ON WEB, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, PAGES 1-3 AND SOPM 20-41-02.
- [SDR F3LA200300083](https://openairdocs.org/sdr/F3LA200300083.md): Channel · corroded · Feb 20, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN SCREW HOLES OF FWD LAVATORY AFT BULKHEAD ATTACH ANGLE, HAT SECTION, STA. 312, LBL 12 TO LBL 42. REMOVED HAT SECTION PER SRM 51-30-2. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-10-1, SRM 51-30-2 AND
- [SDR F3LA200300082](https://openairdocs.org/sdr/F3LA200300082.md): Intercostal · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED SHORT INTERCOSTAL AT CENTERLINE BETWEEN STA. 1006 AND STA. 1016 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02.
- [SDR F3LA200300081](https://openairdocs.org/sdr/F3LA200300081.md): Intercostal · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED LT. INTERCOSTAL BETWEEN STA. 967 AND STA. 986.5 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SOPM 20-41-02
- [SDR F3LA200300080](https://openairdocs.org/sdr/F3LA200300080.md): Seat Track · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND SCREW HOLES AT SEAT TRACK BETWEEN STA. 328 AND STA. 344, RBL 54. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-3.
- [SDR F3LA200300078](https://openairdocs.org/sdr/F3LA200300078.md): Intercostal · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT GALLEY FLOOR INTERCOSTAL AT STA. 957, LBL 18.75 THRU LBL 40.5. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SRM 51-
- [SDR F3LA200300077](https://openairdocs.org/sdr/F3LA200300077.md): Seat Track · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT NUTCLIP HOLES, RT. SIDE BETWEEN FLOORBEAM AT STA. 986.5 TO STA. 1016. REPLACED SEAT TRACK PER SRM 53-10-01, FIG. 3, SRM 51-30-02, MM 51-21-41 AND SOPM 20-41-02.
- [SDR F3LA200300075](https://openairdocs.org/sdr/F3LA200300075.md): Floorbeam · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA. 312, LBL 13 TO RBL 10. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED NEW CAP PER SRM 53-10-1.
- [SDR F3LA200300076](https://openairdocs.org/sdr/F3LA200300076.md): Floorbeam · corroded · Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT SCREW HOLE, STA. 328, LBL 29. REMOVED TOP CAP REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE TO TOP CAP PER SRM 51-40-02.
- [SDR F3LA200300074](https://openairdocs.org/sdr/F3LA200300074.md): Stringer · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON STRINGER 18-R AT STA. 727B + 16. REPAIRED DAMAGED SECTION OF STRINGER PER SRM 53-10-1, PAGE 6, DETAIL VI, SRM 53-10-3, PAGE 10, DETAIL VII AND SOPM 20-41-02.
- [SDR F3LA200300073](https://openairdocs.org/sdr/F3LA200300073.md): Angle · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON BULKHEAD ANGLE AT STA. 947.5 LOWER ANGLE. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-1, 53-20-01, FIG. 5, DETAIL II, 51-30-02 AND SOPM 20-41-02.
- [SDR F3LA200300072](https://openairdocs.org/sdr/F3LA200300072.md): Panel · punctured · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED SMALL PUNCTURE IN TRANSITION PANEL BETWEEN STA. 767 AND 794. REPAIRED PANEL PER SRM 53-10-13 AND SOPM 20-4-02.
- [SDR F3LA200300071](https://openairdocs.org/sdr/F3LA200300071.md): Seat Track · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT STA 290, RBL 16. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2 AND 53-10-2.
- [SDR F3LA200300070](https://openairdocs.org/sdr/F3LA200300070.md): Clip · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED TIE CLIP AND ATTACHING HARDWARE CORRODED AT AFT END OF RT MOP SILL BEHIND R-2 DOOR. REPLACED CLIP HARDWARE PER SRM 51-30-2. NO CORROSION WAS FOUND ON CLIP. CLEANED AREA PER SOPM 20-41-02.
- [SDR F3LA200300069](https://openairdocs.org/sdr/F3LA200300069.md): Floorbeam · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, LBL 3, AT NUT PLATE ON UNDERSIDE OF FLANGE. FABRICATED AND INSTALLED FLOOR SUPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02.
- [SDR F3LA200300068](https://openairdocs.org/sdr/F3LA200300068.md): Floorbeam · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, RBL 3, AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE. FABRICATED AND INSTALLED FLOOR SUPPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02.
- [SDR F3LA200300067](https://openairdocs.org/sdr/F3LA200300067.md): Support Angle · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED FLOOR/LAVATORY SUPPORT BEAM BETWEEN STA 986.5 AND STA 1006 CORRODED. REMOVED SUPPORT ANGLE AND HAT CHANNEL PER SRM 51-30-02. FOUND CORROSION ON BOTH HAT CHANNEL AND SUPPORT ANGLE OUT OF LIMITS PER SRM 51-30-02. FABRICAT
- [SDR F3LA200300066](https://openairdocs.org/sdr/F3LA200300066.md): Stringer · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > DURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION AT STR 27-L BETWEEN STA 945 AND STA 953.5. REPLACED STRINGER FROM STA 945 TO STA 967.5, LBL 3, STR 27-L, PER SRM 53-10-3, 51-20-2 AND 51-30-5.
- [SDR F3LA200300065](https://openairdocs.org/sdr/F3LA200300065.md): Floorbeam · corroded · Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA 344, LBL 60 - RBL 14. REMOVED DAMAGE ON WEB BETWEEN STA 332 AND STA 344 AFT OF R-1 DOOR PER SRM 51-40-2, PAGES 1-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-02, PAGES 1-3, AND SOPM
- [SDR F3LA200300064](https://openairdocs.org/sdr/F3LA200300064.md): Attach Angle · corroded · Feb 17, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED RT RAM AIR DUCT ANGLE ATTACH POINT FOR CROSS BRACE UNDER WING BLEED AIR DUCT CORRODED AT STA 540, STR 22R. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, FIG 1, SHEET 2, 51-40-3.
- [SDR F3LA200300063](https://openairdocs.org/sdr/F3LA200300063.md): Floorbeam · corroded · Feb 17, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP CORRODED AT STA 290, RBL 15. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP PER SRM 53-10-2 AND 53-10-9.
- [SDR F3LA200300062](https://openairdocs.org/sdr/F3LA200300062.md): Floorbeam · corroded · Feb 14, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP AT STA 1006 CORRODED IN VARIOUS AREAS FROM CENTERLINE EXTENDING TO LEFT SIDE. REPAIRED PER SRM 53-10-9, FIG 7.
- [SDR F3LA200300061](https://openairdocs.org/sdr/F3LA200300061.md): Floorbeam · corroded · Feb 13, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE, STA 794, LBL 8. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-05, SRM 53-10-05, FIG 11, SHEET
- [SDR F3LA200200397](https://openairdocs.org/sdr/F3LA200200397.md): Trunnion · corroded · Dec 23, 2002 · N921WA · Boeing 7372Y5 · Nose/Tail Landing Gear Attach Section
  > DURING NOSE GEAR CHANGE, INSPECTED REPORTED LT NOSE GEAR TRUNNION BOSS CORRODED. REPLACED NOSE GEAR TRUNNION BOSS.
- [SDR F3LA200100113](https://openairdocs.org/sdr/F3LA200100113.md): Duct · broken · Oct 21, 2001 · N921WA · Boeing 7372Y5 · Air Distribution System
  > ENROUTE FROM SAN TO DEN, FLIGHT CREW REPORTED CABIN SIDEWALL AT ROW 7 EXTREMELY HOT TO THE TOUCH AND AN OVERHEAT ODOR. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO YUMA, AZ WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. MAINTENANCE REPLACED
- [SDR F3LA200100111](https://openairdocs.org/sdr/F3LA200100111.md): Door Frame · cracked · Sep 26, 2001 · N921WA · Boeing 7372Y5 · Cargo/Baggage Doors
  > DURING C-3 CHECK, INSPECTION REPORTED CRACK IN LOWER AFT CORNER OF C1 DOOR. DOOR WAS REPAIRED AT VENDOR AND RETURNED IN SERVICEABLE CONDITION.
- [SDR F3LA200100110](https://openairdocs.org/sdr/F3LA200100110.md): Door Frame · corroded · Sep 24, 2001 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LT SIDE OF E&E DOOR CUTOUT BETWEEN CHORD AND SKIN. REMOVED DOOR FITTINGS, CORRODED WEBS, SKIN AND CHORDS. INSTALLED NEW CHORDS, WEBS AND STIFFENERS, NEW SKIN, FASTENERS, DOOR FITTINGS AND ALL RELATED HARDWAR
- [SDR F3LA200100109](https://openairdocs.org/sdr/F3LA200100109.md): Door Frame · cracked · Sep 24, 2001 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR FRAME CRACKED AT LOWER SET OF BACK FASTENERS. REPAIRED PER SRM 51-40-04.
- [SDR F3LA200100106](https://openairdocs.org/sdr/F3LA200100106.md): Skin · cracked · Sep 15, 2001 · N921WA · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > DURING C-3 CHECK, INSPECTION REPORTED CRACK IN L-2 DOOR CUTOUT, LOWER FWD CORNER, BS 947.5, S-18L, APPROXIMATELY 3.5 INCHES LONG. REPAIRED CRACK PER SRM 53-30-3, FIGURE 24.
- [SDR F3LA200100064](https://openairdocs.org/sdr/F3LA200100064.md): Oil Filter · dirty · May 13, 2001 · N921WA · Boeing 7372Y5 · Turbine Engine Oil System
  > FLIGHT CREW REPORTED NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE. NR 1 ENGINE WAS SHUT DOWN IN FLIGHT AND AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO MCI FROM ITS PLANNED DESTINATION OF MDW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED
- [SDR F3LA200100050](https://openairdocs.org/sdr/F3LA200100050.md): Attach Fitting · broken · Mar 27, 2001 · N921WA · Boeing 7372Y5 · Trailing Edge Flaps
  > DURING A-CHECK, MAINTENANCE REPORTED LT WING OTBD FOREFLAP OTBD ATTACH LINK BROKEN. REPLACED LT WING OTBD FOREFLAP.
- [SDR F3LA200100009](https://openairdocs.org/sdr/F3LA200100009.md): Charger · inoperative · Jan 19, 2001 · N921WA · Boeing 7372Y5 · Emergency Lighting
  > L-1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED L-1 DOOR SLIDE LIGHT ASSY, BATTERY AND CHARGER PER MM 33-51-71.
- [SDR F3LA200000248](https://openairdocs.org/sdr/F3LA200000248.md): Stringer · corroded · Oct 3, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON STR 21-R, STA 847 TO 867, AND CORROSION ON INTERCOSTAL BETWEEN STR 21-R AND 22-R, STA 847 TO 867. MAINTENANCE REMOVED DAMAGED STRINGER AND INTERCOSTAL, FABRICATED REPLACEMENT PARTS AND INSTALLED PER SRM 53-10
- [SDR F3LA200000247](https://openairdocs.org/sdr/F3LA200000247.md): Door Frame · cracked · Sep 29, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CRACK IN R-1 DOOR CUTOUT UNDER SCUFF PLATE AT LOWER AFT CORNER. MAINTENANCE VERIFIED CRACK BY ACCOMPLISHING AN NDT INSPECTION PER SRM 53-30-3 AND FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-30-3, FIG 26.
- [SDR F3LA200000246](https://openairdocs.org/sdr/F3LA200000246.md): Stringer · corroded · Sep 25, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON INSIDE SURFACE OF STRINGER 25L, STA 1006, AROUND FASTENER. MAINTENANCE BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-00-4 AND 51-10-6. REMOVED DAMAGED STR 25L BETWEEN STA 1058 TO STA 1088 PER SR
- [SDR F3LA00240](https://openairdocs.org/sdr/F3LA00240.md): Skin · chafed · Sep 13, 2000 · N921WA · Boeing 7372Y5 · Wing, Plate/Skin
  > DEN - DURING C-2 CHECK INSPECTION, REPORTED CHAFING ON LEFT LEADING EDGE ABOVE NR 1 ENGINE PYLON. MAINTENANCE REPLACED WING LEADING EDGE SECTION ABOVE NR 1 ENGINE PYLON. REPLACED SKIN SECTION ON LEADING EDGE CAP OUTBOARD OF NR 1 PYLON AND REPAIRED SKIN INBOA
- [SDR F3LA00241](https://openairdocs.org/sdr/F3LA00241.md): Stringer · corroded · Sep 12, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > DEN - DURING C-2 CHECK INSPECTION, REPORT CORROSION ON STRINGER 23R FROM STATION 259 TO STATION 312. MAINTENANCE FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-10-03, FIGURE 1. (M)
- [SDR F3LA00235](https://openairdocs.org/sdr/F3LA00235.md): Structure · cracked · Sep 7, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CRACK IN FORWARD PRESSURE BULKHEAD FLOOR STRUCTURE NEXT TO INTERCOSTAL WL 207, RBL 27. MAINTENANCE INSTALLED NEW WEB PER SRM 51-30-2. (M)
- [SDR F3LA00234](https://openairdocs.org/sdr/F3LA00234.md): Structure · cracked · Sep 7, 2000 · N921WA · Boeing 7372Y5 · Fuselage Main, Structure
  > DEN - DURING C-2 CHECK, INSPECTION REPORTED CRACK IN FORWARD PRESSURE BULKHEAD FLOOR STRUCTURE NEXT TO INTERCOSTAL, WL 207, LBL 27. MAINTENANCE INSTALLED NEW WEB PER SRM 51-30-2. (M)

Next page: https://openairdocs.org/deregistered/N921WA-2004-05-11/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 = 'N921WA' AND deregistration_id = 'N921WA-2004-05-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N921WA-2004-05-11/reports

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