# Service difficulty reports: Boeing 737-3S1

A list on [Boeing 737-3S1](https://openairdocs.org/model/boeing-737-3s1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 65 reports

- [SDR DU4R0507157](https://openairdocs.org/sdr/DU4R0507157.md): Skin · dented · Jul 7, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT AT RT EXTERNAL FUSELAGE AT BS 871 BETWEEN S-22R AND S-23R.
- [SDR DU4R0507156](https://openairdocs.org/sdr/DU4R0507156.md): Skin · cracked · Jul 7, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN CRACKED AT S-24R BETWEEN BS 727D - 727E.
- [SDR DU4R0507155](https://openairdocs.org/sdr/DU4R0507155.md): Stringer · cracked · Jul 7, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Longeron/Stringer
  > STRINGER 27R CRACKED.
- [SDR DU4R0507153](https://openairdocs.org/sdr/DU4R0507153.md): Skin · dented · Jul 7, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS DENT AT BS 480 S-26R - S-28R.
- [SDR DU4R0507150](https://openairdocs.org/sdr/DU4R0507150.md): Skin · dented · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT AT RT EXTERNAL FUSELAGE SKIN AT BS 876 S-21R AND S-22R.
- [SDR DU4R0507149](https://openairdocs.org/sdr/DU4R0507149.md): Skin · dented · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT AT LT EXTERNAL FUSELAGE SKIN AT BS 997.5 BETWEEN S-13L AND S-14L.
- [SDR DU4R0507148](https://openairdocs.org/sdr/DU4R0507148.md): Skin · dented · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT AT RT EXTERNAL FUSELAGE SKIN AT BS 391.5 BETWEEN S-22R AND S-23R.
- [SDR DU4R0507147](https://openairdocs.org/sdr/DU4R0507147.md): Skin · dented · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT 3 IN DIAMETER, DEPTH.015 INCHES FUSELAGE S 1070 S-14L FRONTIER DENT TALLY ITEM NR 3.
- [SDR DU4R0507146](https://openairdocs.org/sdr/DU4R0507146.md): Bulkhead · cracked · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Bulkhead
  > CRACK APPROX 8 IN BELOW WL 207 INBD SIDE RBL 5.7 APPROX 1.5" IN LENGTH AT BS 178 BULKHEAD.
- [SDR DU4R0507145](https://openairdocs.org/sdr/DU4R0507145.md): Bulkhead · cracked · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Bulkhead
  > CRACK APPROX. 5.5 INCHES BELOW WL 207 IB SIDE LBL 5.7 APPROX. 1.2 INCH IN LENGTH AT BS 178 BULKHEAD.
- [SDR DU4R0507144](https://openairdocs.org/sdr/DU4R0507144.md): Frame · cracked · Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Frame
  > BS 178 BULKHEAD RT SIDE AFT SIDE FRAME HAS EVIDENCE OF CRACK ABOVE AND BELOW WL 207.
- [SDR DU4R0507135](https://openairdocs.org/sdr/DU4R0507135.md): Skin · dented · Jun 30, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > CREASE IN DENT AT BS 971 BETWEEN S-24L-25L 2 INCHES X.86 A/Y = 23.3. S/O NR 109002, OPS NR 25863.
- [SDR DU4R0507134](https://openairdocs.org/sdr/DU4R0507134.md): Skin · dented · Jun 30, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > CREASES IN DENTS AND ON TOP OF STRINGER 27R AT BS 951 - 952 A/Y = 24.7 A/Y 1.875 X.076.
- [SDR DU4R0507133](https://openairdocs.org/sdr/DU4R0507133.md): Skin · dented · Jun 30, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DENT IN LEFT FUSELAGE EXTERIOR SKIN BS 935 S-26L.
- [SDR F3LA200500015](https://openairdocs.org/sdr/F3LA200500015.md): Hinge Fitting · cracked · Mar 27, 2005 · N311FL · Boeing 7373S1 · Fuselage, Door Hinge
  > INSPECTION REPORTED R1 DOOR UPPER HINGE ARM FITTING CRACKED. DOOR FRAME CRACKED AT HINE ARM CUTOUT. REPLACED R1 DOOR UPPER HINGE CASTING PER SRM 51-40-02 AND 51-10-02
- [SDR F3LA200400047](https://openairdocs.org/sdr/F3LA200400047.md): Frame · cracked · Mar 8, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Frame
  > DURING C-7 CHECK, INSPECTION REPORTED BODY FRAME CRACKED AND BENT IN FWD CARGO COMPARTMENT AT STA 460, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-07, FIG. 203.
- [SDR F3LA200400046](https://openairdocs.org/sdr/F3LA200400046.md): Support · corroded · Mar 8, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02.
- [SDR F3LA200400032](https://openairdocs.org/sdr/F3LA200400032.md): Screw · loose · Mar 8, 2004 · N311FL · Boeing 7373S1 · Fasteners
  > DURING C-7 CHECK, INSPECTION REPORTED SCREWS F2 AND F4 WERE FOUND LOOSE PER RUDDER INSPECTION PERFORMED PER EO B3-55-00AD-0001-DY, PART 2, STEPS 2 AND 4. REPLACED BOLTS PER EO B3-55-00AD-004-DY.
- [SDR F3LA200400031](https://openairdocs.org/sdr/F3LA200400031.md): Floorbeam · corroded · Mar 8, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED AFT CABIN FLOORBEAM AT STA 986 CORRODED. CORROSION ON FLOORBEAM TOP FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-31. REMOVED FLOORBEAM UPPER FLANGE, FABRICATED REPAIR T-CAP, ALODINED, PRIMED, PAINTED AND INSTALLED REPA
- [SDR F3LA200400025](https://openairdocs.org/sdr/F3LA200400025.md): Channel · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > ZEE CHANNEL AT STA 993, LBL 30 TO LBL 40 CORRODED. FABRICATED AND INSTALLED REPLACEMENT Z-CHANNEL PER SRM 51-10-02, PAGE 37, SRM 51-30-01 AND SOPM 20-41-02.
- [SDR F3LA200400024](https://openairdocs.org/sdr/F3LA200400024.md): Floorbeam · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 950, RBL 26 TO RBL 49, WL 208 CORRODED AT FLOORBOARD HOLES. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM PER SRM 53-60-51 AND 51-10-02.
- [SDR F3LA200400023](https://openairdocs.org/sdr/F3LA200400023.md): Sill · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED SILL PLATE AT L2 DOOR FLOOR CORRODED. REPLACED MOP SILL PER SRM 51-10-02.
- [SDR F3LA200400022](https://openairdocs.org/sdr/F3LA200400022.md): Floorbeam · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM WEB CORRODED AT STA 986.5, LBL 42. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-60-51, 51-40-02, MM 51-21-41 AND BOLD DRAWING 65-46812.
- [SDR F3LA200400021](https://openairdocs.org/sdr/F3LA200400021.md): Floor Support · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED AT NUT PLATE HOLES, RBL 51, STA 947 TO STA 967, WL 208. REPLACED FLOOR SUPPORT PER SRM 51-40-2 AND 53-60-51.
- [SDR F3LA200400020](https://openairdocs.org/sdr/F3LA200400020.md): Floorbeam · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 947 CORRODED ALONG GOUGE 20 INCHES EITHER SIDE OF CENTER LINE. REPLACED T-CAP PER EA B3-53R-10330 AND SRM 51-40-02.
- [SDR F3LA200400019](https://openairdocs.org/sdr/F3LA200400019.md): Support · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED WALL SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02.
- [SDR F3LA200400018](https://openairdocs.org/sdr/F3LA200400018.md): Web · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Passenger/Crew Doors
  > DURING C-7 CHECK, INSPECTION REPORTED L-2 DOOR WEB CORRODED FROM STA 949 TO STA 991.5. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-40-02, 53-60-51, 53-60-15 AND DRAWING 65-45855.
- [SDR F3LA200400017](https://openairdocs.org/sdr/F3LA200400017.md): Floorbeam · corroded · Mar 3, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM CORRODED ON WEB AND UNDER GALLEY ATTACH POINT, RT SIDE, STA 986, RBL 42. BLENDED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REMOVED DAMAGED SHEAR WEB AND COMMON SUPPORT ANGLES P
- [SDR F3LA200400016](https://openairdocs.org/sdr/F3LA200400016.md): Web · corroded · Feb 20, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED LT TOILET SUPPORT WEB CORRODED. CORROSION FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-60-51. REMOVED DAMAGED LT AFT TOILET SUPPORT WEB. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C32707. ALODINED REPLACEMENT LT A
- [SDR F3LA200400015](https://openairdocs.org/sdr/F3LA200400015.md): Web · corroded · Feb 20, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED RT TOILET SUPPORT WEB CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-60-51. REMOVED RT AFT TOILET WEB SUPPORT. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C72707. ALODINED REPLACEMENT WEB
- [SDR F3LA200400014](https://openairdocs.org/sdr/F3LA200400014.md): Sill · corroded · Feb 19, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED L1 DOOR MOP SILL CORRODED THE WIDTH OF THE DOORWAY AND EXTENDING AFT TO THE END OF THE CORD. REPLACED MOP SILL IAW SRM 53-10-15.
- [SDR F3LA200400010](https://openairdocs.org/sdr/F3LA200400010.md): Skin · cracked · Feb 11, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DURING C-7 CHECK, INSPECTION REPORTED RT FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF R-1 DOOR CUTOUT. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-10-01 FIG 202.
- [SDR F3LA200400009](https://openairdocs.org/sdr/F3LA200400009.md): Mount · corroded · Feb 9, 2004 · N311FL · Boeing 7373S1 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-7 CHECK, INSPECTION REPORTED FWD LAVATORY MOUNT BLOCK AT STA 303, LBL 12, CORRODED. REPLACED LAVATORY MOUNT PER SRM 53-10-15, SRM 53-10-51 AND DRAWING 65C33970.
- [SDR F3LA200400008](https://openairdocs.org/sdr/F3LA200400008.md): Stringer · corroded · Feb 5, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Longeron/Stringer
  > DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AFT OF STA 727A, RT MID STRINGER. REPAIRED AFT CARGO COMPARTMENT FLOORBEAM PER SRM 53-00-53 FIG 201.
- [SDR F3LA200400007](https://openairdocs.org/sdr/F3LA200400007.md): Panel · cracked · Feb 5, 2004 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-7 CHECK, INSPECTION REPORTED TRANSITION PANEL IN FWD CARGO COMPARTMENT CRACKED AT NUT PLATE HOLE, STA 430 + 11, BL 24R. FABRICATED AND INSTALLED NEW TRANSITION STRIP PER SRM 51-40-02.
- [SDR F3LA200400006](https://openairdocs.org/sdr/F3LA200400006.md): Stringer · corroded · Feb 5, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Longeron/Stringer
  > DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AT STA 727B, STR 2L. REPLACED FLOOR BEAM STRINGER PER SRM 53-00-53 FIG 201.
- [SDR F3LA200400004](https://openairdocs.org/sdr/F3LA200400004.md): Skin · cracked · Jan 28, 2004 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DURING C-7 CHECK, INSPECTION REPORTED RT AFT FUSELAGE SKIN CRACKED JUST BELOW EMERGENCY LIGHT AT STA. 727, STR. 25R. CUT OUT DAMAGED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, PAGE 204-206.
- [SDR F3LA200300180](https://openairdocs.org/sdr/F3LA200300180.md): Spindle · worn · Dec 19, 2003 · N311FL · Boeing 7373S1 · Trailing Edge Flap Control System
  > INSPECTION REPORTED EXCESSIVE PLAY AND WEAR IN RT OB NR 8 FLAP CARRIAGE SPINDLE. REPLACED SPINDLE, SPINDLE BEARING AND BUSHINGS AND FLAP SADDLE.
- [SDR F3LA200300118](https://openairdocs.org/sdr/F3LA200300118.md): Floor Support · corroded · Apr 11, 2003 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA. 727D + 5. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53.
- [SDR F3LA200300117](https://openairdocs.org/sdr/F3LA200300117.md): Floor Support · corroded · Apr 11, 2003 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA. 772, BETWEEN RBBL 8.10 AND LBBL 12.5. FABRICATED AND INSTALLED REPAIRS PER SRM 53-00-53.
- [SDR F3LA200300116](https://openairdocs.org/sdr/F3LA200300116.md): Floor Support · corroded · Apr 11, 2003 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORTS BETWEEN STA. 847 AND 867. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53.
- [SDR F3LA200200108](https://openairdocs.org/sdr/F3LA200200108.md): Stringer · cracked · Mar 14, 2002 · N311FL · Boeing 7373S1 · Fuselage Main, Longeron/Stringer
  > DURING C-5 CHECK, INSPECTION REPORTED CRACK ON STRINGER 6L, STA 798.
- [SDR F3LA200200104](https://openairdocs.org/sdr/F3LA200200104.md): Floor Panel · cracked · Mar 6, 2002 · N311FL · Boeing 7373S1 · Fuselage Floor Panel
  > DURING C-5 CHECK, INSPECTION REPORTED CRACK IN FWD CARGO COMPARTMENT FLOOR PANEL AT STA 490, STR 26R.
- [SDR F3LA200100115](https://openairdocs.org/sdr/F3LA200100115.md): Proximity Switch · out of adj · Oct 22, 2001 · N311FL · Boeing 7373S1 · Door Warning System
  > REJECTED TAKEOFF. FLIGHT CREW REPORTED AFT CARGO COMPARTMENT DOOR LIGHT ILLUMINATED UPON REACHING TAKEOFF THRUST. ADJUSTED AFT CARGO COMPARTMENT DOOR PROXIMITY SWITCH.
- [SDR F3LA200100039](https://openairdocs.org/sdr/F3LA200100039.md): Skin · corroded · Feb 27, 2001 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/Skin
  > DURING C-4 CHECK, INSPECTION REPORTED INTERGRANULAR CORROSION ON INSIDE SKIN OF C2 DOOR CUTOUT, AFT LOWER CORNER. REMOVED CORROSION ON BEAR STRAP PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3, FIG
- [SDR F3LA200100038](https://openairdocs.org/sdr/F3LA200100038.md): Door Frame · corroded · Feb 27, 2001 · N311FL · Boeing 7373S1 · Fuselage Main, Structure
  > DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR FRAME CORRODED AT STA 867. MAINTENANCE REMOVED SUPPORT ANGLE, INTERCOSTAL AND TRANSITION WEB AT STR 25R, STA 847 TO 867, AND CUT OUT DAMAGED PORTION OF FRAME. FABRICATED AND INSTALLED FRAME DOU
- [SDR F3LA200100032](https://openairdocs.org/sdr/F3LA200100032.md): Floorbeam · corroded · Feb 22, 2001 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE FLOORBEAM AT STA 986.5 CORRODED ACROSS TOP. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT FLOOR BEAM PER SRM 53-00-51.
- [SDR F3LA200100031](https://openairdocs.org/sdr/F3LA200100031.md): Floorbeam · corroded · Feb 22, 2001 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM AT STA 867, RBL 15. MAINTENANCE REPLACED FLOOR SUPPORT BEAM PER SRM 51-30-02 AND 51-10-02.
- [SDR F3LA200100030](https://openairdocs.org/sdr/F3LA200100030.md): Floorbeam · corroded · Feb 22, 2001 · N311FL · Boeing 7373S1 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 847, STR 26R. MAINTENANCE REPLACED FLOORBEAM SUPPORT STRAP AND WEB PER SDR 51-10-02.
- [SDR F3LA200100029](https://openairdocs.org/sdr/F3LA200100029.md): Floor Support · corroded · Feb 21, 2001 · N311FL · Boeing 7373S1 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE FLOOR SUPPORT CORRODED AT LBL 16, STA 950. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-10-02.

Next page: https://openairdocs.org/model/boeing-737-3s1/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 aircraft_model_key = '7373S1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-3s1/reports

---
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