# Service difficulty reports: Boeing 737-2X6C

A list on [Boeing 737-2X6C](https://openairdocs.org/model/boeing-737-2x6c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,351 reports

- [SDR TSAA20150307002](https://openairdocs.org/sdr/TSAA20150307002.md): Skin · cracked · Mar 7, 2015 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > CRACKS FOUND & CONFIRMED BY HFEC DURING ACCOMPLISHMENT OF ECO 3475R8 PART III & PART V. FUSELAGE SKIN CHEM MILLED LINES DETAILED & NDT INSPECTION, APPROX 2.0 INCHES LONG SKIN CRACK AT BS 540 MINUS 2 BETWEEN STRINGERS 2 & 3 L.
- [SDR TSAA20150307003](https://openairdocs.org/sdr/TSAA20150307003.md): Skin · cracked · Mar 7, 2015 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > CRACK FOUND & CONFIRMED BY HFEC DURING ACCOMPLISHMENT OF ECO 3475R8 PART III & PART V. FUSELAGE SKIN CHEM MILLED LINES DETAILED & NDT INSPECTION. APPROX 2.0 INCH LONG SKIN CRACK AT BS 787ABOVE STRINGER 19 L.
- [SDR TSAA201410200235](https://openairdocs.org/sdr/TSAA201410200235.md): Skin · cracked · Oct 20, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX FOUND A 2 INCH FUSELAGE SKIN CRACK ON THE LT SIDE BS 787 STRINGER 19L.
- [SDR TSAA20140806007](https://openairdocs.org/sdr/TSAA20140806007.md): Skin · cracked · Aug 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX FOUND A 4 INCH FUSELAGE SKIN CRACK ON THE RT SIDE BS 344 STRINGER 15R.
- [SDR TSAA20140806006](https://openairdocs.org/sdr/TSAA20140806006.md): Skin · cracked · Aug 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX FOUND A 3 INCH FUSELAGE SKIN CRACK ON THE LT SIDE BS 727B STRINGER 18L.
- [SDR 7AHR2014030782487](https://openairdocs.org/sdr/7AHR2014030782487.md): Floorbeam · corroded · Mar 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANGE CABIN FLOORBEAM, BS 807 BETWEEN LBL 45 AND RBL 45. INSTALLED REPAIR IAW DWG 53-14034-1 WITH 8110-3 APPROVAL.
- [SDR 7AHR2014030782403](https://openairdocs.org/sdr/7AHR2014030782403.md): Door Frame · gouged · Mar 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Structure
  > GOUGE IN LOWER BS 348 DOOR FRAME STRINGER 16L. INSTALLED NEW FRAME IAW SRM 53-10-2, FIG 1 AND DRG 65-54961-1, SH 1.
- [SDR 7AHR2017030782302](https://openairdocs.org/sdr/7AHR2017030782302.md): Spar · corroded · Mar 7, 2014 · N840AL · Boeing 7372X6C · Wing Spar
  > LT WING L/E SPAR AT STA 278 HAS CORROSION AROUND FASTENER HOLES. INSTALLED REPAIR IAW DWG 57-14014-1 AND FAA 8110-3, APPROVAL.
- [SDR 7AHR2014030782587](https://openairdocs.org/sdr/7AHR2014030782587.md): Skin · dented · Mar 6, 2014 · N840AL · Boeing 7372X6C · Trailing Edge Flaps
  > INBD LT FLAP WB 96 HAS DENT IN L/E UPPER SURFACE. INSTALLED REPAIR IAW SRM 57-50-4 & 51-30-2.
- [SDR 7AHR2014030782557](https://openairdocs.org/sdr/7AHR2014030782557.md): Skin · damaged · Mar 6, 2014 · N840AL · Boeing 7372X6C · Trailing Edge Flaps
  > RIGHT INBD MIDFLAP HAS AREAS OF CORROSION UPPER SURFACE AND PUNCTURE IN SKIN. REMOVED CORROSION IAW SRM 51-10-06. FABRICATED AND INSTALLED REPAIR TO SKIN IAW SRM 51-30-2.
- [SDR 7AHR2014030782538](https://openairdocs.org/sdr/7AHR2014030782538.md): Skin · dented · Mar 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > SEVERAL DENTS JUST FWD AT TAIL JACK POINT. FABRICATED REPAIR PARTS IAW SRM 53-30-3, PG 357-359 AND INSTALLED IAW SRM 51-30-2.
- [SDR 7AHR2014030782480](https://openairdocs.org/sdr/7AHR2014030782480.md): Seat Track · corroded · Mar 6, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON BOTH FLANGES OF CABIN SEAT TRACK BS 540 - 580. INSTALLED A REPAIR IAW DWG 57-14029 WITH 8110-3 APPROVAL.
- [SDR 7AHR2014037002801](https://openairdocs.org/sdr/7AHR2014037002801.md): Nut Plate · damaged · Mar 6, 2014 · N840AL · Boeing 7372X6C · Horizontal Stabilizer Structure
  > LT & RT HORIZONTAL STAB HINGE FITTINGS HAVE QUESTIONAL CLEARANCE. R & R NUTPLATES IAW DWG 55-14054-1 WITH 8110-3, APPROVAL.
- [SDR 7AHR2014030782476](https://openairdocs.org/sdr/7AHR2014030782476.md): Floorbeam · corroded · Mar 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANGE OF CABIN FLOORBEAM AT STA 727B BETWEEN LBL 24-RBL 45. INSTALLED A REPAIR IAW DWG 53-14028-1 WITH 8110-3, APPROVAL.
- [SDR 7AHR2014030722091](https://openairdocs.org/sdr/7AHR2014030722091.md): Spar · corroded · Mar 6, 2014 · N840AL · Boeing 7372X6C · Wing Spar
  > LT WING L/E CAVITY LOWER SPAR HAS CORROSION AROUND FASTENER HOLES. INSTALLED REPAIR IAW DWG 57-14015-1 WITH 8110-3 APPROVAL.
- [SDR 7AHR201403070001](https://openairdocs.org/sdr/7AHR201403070001.md): Bulkhead · damaged · Mar 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AFT SIDE PAN & COVER AREA CHAFED. REMOVED DAMAGE GORE WEB AND PREVIOUS REPAIR IAW SRM 51-30-2, PG 32 AND SR1-2020138697 INSTRUCTIONS. HFEC EDDY CURRENT HOLES AND SURROUNDING AREA.INSTALLED REPAIR IAW SRM 53-10-11, PG 119-127, DWG 53-1402
- [SDR 7AHR201403052210](https://openairdocs.org/sdr/7AHR201403052210.md): Spar · corroded · Mar 5, 2014 · N840AL · Boeing 7372X6C · Wing Spar
  > LT WING L/E CAVITY LOWER SPAR AT LWS 567 HAS CORROSION. CORRISON WAS OUT OF LIMITS. INSTALLED REPAIR IAW DWG 57-14014-1.
- [SDR 7AHR201403052209](https://openairdocs.org/sdr/7AHR201403052209.md): Spar · corroded · Mar 5, 2014 · N840AL · Boeing 7372X6C · Wing Spar
  > LEFT WING L/E CAVITY FWD LOWER SPAR AT LWS 476 HAS CORROSION. AREA OF CORROSION WAS OUT OF LIMITS. INSTALLED REPAIR IAW DWG 57-14015-1 WITH APPROVAL IAW 8110-3.
- [SDR 7AHR2014021282436](https://openairdocs.org/sdr/7AHR2014021282436.md): Floor Support · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CHANNEL CORRODED. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-20-1 FIG 7 & 51-30-2.
- [SDR 7AHR2014021282434](https://openairdocs.org/sdr/7AHR2014021282434.md): Floor Support · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CHANNEL CORRODED. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-20-1, FIG 7 AND 51-30-2.
- [SDR 7AHR2014021282258](https://openairdocs.org/sdr/7AHR2014021282258.md): Intercostal · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED IN FWD CARGO BAY BETWEEN BS 500B AND 520. FABRICATED INTERCOSTAL AND INSTALLED IAW SRM 51-20-1, FIG 3/6 AND 51-30-2, PARA 4.
- [SDR 7AHR2014021282365](https://openairdocs.org/sdr/7AHR2014021282365.md): Stiffener · cracked · Feb 12, 2014 · N840AL · Boeing 7372X6C · Vertical Stabilizer
  > VERTICAL STABILIZER FRONT SPAR AFT SURFACE AT VSS 200 RT HAS A CRACKED STIFFNER. FABRICATED AND INSTALLED STIFFNER IAW SRM 51-30-5 & 51-30-2.
- [SDR 7AHR2014021282386](https://openairdocs.org/sdr/7AHR2014021282386.md): Seat Track · broken · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CROWN IS BROKEN, BOTH SIDES AT BS 360+14 LBL 23. INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-5.
- [SDR 7AHR2014021282445](https://openairdocs.org/sdr/7AHR2014021282445.md): Support Fitting · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Attach Fittings
  > FITTING CORRODED LT SIDE APU BAY, BS 1144. AFT LATCH SUPPORT, FABRICATED AND INSTALLED LATCH SUPPORT FITTING IAW SRM 51-30-2.
- [SDR 7AHR2012021282584](https://openairdocs.org/sdr/7AHR2012021282584.md): Skin · dented · Feb 12, 2014 · N840AL · Boeing 7372X6C · Trailing Edge Flaps
  > INBD LT FLAP WB 117.10 L/E DENTED IN UPPER SURFACE. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW SRM 57-50-4, FIG 4.
- [SDR 7AHR2014021282716](https://openairdocs.org/sdr/7AHR2014021282716.md): Frame · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Frame
  > FWD CARGO BAY BS 500B, S26R HAS CORROSION UNDER FRAME LIP. INSTALLED FRAME REPAIR IAW SRM 53-10-4.
- [SDR 7AHR2014021282742](https://openairdocs.org/sdr/7AHR2014021282742.md): Skin · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Trailing Edge Flaps
  > RIGHT OTBD AFT FLAP HAS CORROSION ON UPPER L/E STARTING APPROX 144 INCHES FROM INBD EDGE OF PART. REMOVED DAMAGED AREA OF SKIN AND INSTALLED A REPAIR IAW SRM 57-50-4, FIG 5, NOTE 1.
- [SDR 7AHR2012021282745](https://openairdocs.org/sdr/7AHR2012021282745.md): Intercostal · cracked · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FWD PIT INTERCOSTAL CRACKED, BS 460-480, S25-26L. CUTOUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 737-51-40-3, PG 1.
- [SDR 7AHR2014021282746](https://openairdocs.org/sdr/7AHR2014021282746.md): Intercostal · cracked · Feb 12, 2014 · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FWD CARGO BAY INTERCOSTAL CRACKED AT BS 440-460, S25-26L. CUTOUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 51-40-3.
- [SDR 7AHR2014021282757](https://openairdocs.org/sdr/7AHR2014021282757.md): Shear Tie · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED IN AFT CARGO BAY BILGE BS 767, LBL 10-12. REPLACED SHEAR TIE IAW SRM 51-30-2..
- [SDR 7AHR2014021282257](https://openairdocs.org/sdr/7AHR2014021282257.md): Stringer · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > STRINGER 27L HAS AREAS OF CORROSION IN FWD CARGO BAY BETWEEN BS 440 - 500A. INSTALLED STRINGER REPAIR IAW SRM 53-10-3, FIG 1, SHT 7, DETAIL VI.
- [SDR 7AHR2014021282148](https://openairdocs.org/sdr/7AHR2014021282148.md): Support Channel · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > CORROSION UNDER AND AROUND NUTPLATES ON BOTTOM OF LT SIDEWALL SUPPORT CHANNEL FWD CARGO BAY AT BS 380 AND 520, LBL 23. INSTALLED SUPPORT CHANNEL AND SPLICE IAW SRM 53-10-13.
- [SDR 7AHR2014021282525](https://openairdocs.org/sdr/7AHR2014021282525.md): Floorbeam · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER SURFACE HAS CORROSION AT BS 887, BL 0 TO RBL 45. FLOORBEAM REPAIRED IAW SRM 53-10-9, FIG 7.
- [SDR 7AHR2014021282518](https://openairdocs.org/sdr/7AHR2014021282518.md): Seat Track · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK FLANGE HAS CORROSION AT BS 986+2 RBL 17. INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-5.
- [SDR 7AHR2014021282422](https://openairdocs.org/sdr/7AHR2014021282422.md): Seat Track · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CROWN HAS CORROSION AT BS 480+10, RBL 25. SEAT TRACK REPAIRED IAW SRM 53-10-5, FIG 8.
- [SDR 7AHR2014021282390](https://openairdocs.org/sdr/7AHR2014021282390.md): Seat Track · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FLANGE HAS CORROSION AT BS 476-480. INSTALLED THE SEAT TRACK REPAIR IAW SRM 51-30-05, FIG 7.
- [SDR 7AHR2014021282262](https://openairdocs.org/sdr/7AHR2014021282262.md): Support Channel · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > LT CARGO BAY SIDEWALL SUPPORT CHANNEL HAS NUMEROUS AREAS OF CORROSION LBL 22 BETWEEN BS 727 - 887. REPAIRED IAW SRM 53-10-13, FIG 1.
- [SDR 7AHR2014021282215](https://openairdocs.org/sdr/7AHR2014021282215.md): Support Channel · corroded · Feb 12, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF RT SIDEWALL SUPPORT CHANNEL IN FWD CARGO BAY BS 493 TO 520C, RBL 23. FABRICATED AND INSTALLED REPAIR SUPPORT CHANNEL IAW SRM 51-30-01, FIG 7 & 51-30-2.
- [SDR 7AHR2014020782305](https://openairdocs.org/sdr/7AHR2014020782305.md): Rib · cracked · Feb 7, 2014 · N840AL · Boeing 7372X6C · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB RIB LOWER ANGLE CRACKED STA 111, 15" FROM FRONT SPAR. REMOVED RIB WEB AND SECTION LOWER CHORD, FABRICATED REPAIR AND INSTALLED IAW SRM 55-10-3, FIG 8 AND 51-30-2.
- [SDR 7AHR2014020782474](https://openairdocs.org/sdr/7AHR2014020782474.md): Seat Track · corroded · Feb 7, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK, RBL 25 FROM BS 741-751. REMOVED DAMAGED AREAS OF SEAT TRACK IAW SRM 53-10-5, FIG 8. INSTALLED SECTION OF SEAT TRACK IAW SRM 51-30-2.
- [SDR 7AHR2014020782521](https://openairdocs.org/sdr/7AHR2014020782521.md): Sill · corroded · Feb 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > CABIN BELOW FLOOR SUPPORTS HAS CORROSION ON UPPER SURFACE BS 907+6, RBL 60. REMOVED CORRODED AREAS AND REPAIRED MOPSILL IAW SRM 51-30-2 AND 51-40-3.
- [SDR 7AHR2014020782717](https://openairdocs.org/sdr/7AHR2014020782717.md): Channel · corroded · Feb 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FWD CARGOBAY UNDER FLOOR SUPPORT RT DOOR THRESHOLD AT AFT DOOR FRAME HAS CORROSION. CLEANED AREA AND FOUND NUTPLATE CHANNEL CORRODED. R & R CHANNEL IAW SRM 51-40-4 PG 18 & 19 AND 51-30-2.
- [SDR 7AHR2014020782260](https://openairdocs.org/sdr/7AHR2014020782260.md): Stringer · corroded · Feb 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > STRINGER 27L CORRODED IN FWD CARGO BAY BS 380. REMOVED SECTION OF CORRODED STRINGER. FABRICATED, LOCATED AND DRILLED NEW SECTION IAW SRM 53-10-3, FIG 1. INSTALLED REPAIR PARTS IAW SRM 53-10-3.
- [SDR 7AHR2014020782330](https://openairdocs.org/sdr/7AHR2014020782330.md): Fairing · dented · Feb 7, 2014 · N840AL · Boeing 7372X6C · Engine Thrust Reverser
  > NR 1 ENGINE INBD THRUST REVERSER ACTUATOR FAIRING HAS A DENT. REMOVED DAMAGED AREA, AND INSTALLED A REPAIR IAW SRM 51-40-2, FIG 1, 51-40-2.
- [SDR 7AHR2014020782622](https://openairdocs.org/sdr/7AHR2014020782622.md): Channel · cracked · Feb 7, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FWD CARGO BAY HAT CHANNEL DOUBLER FOR VHF ANTENNA IS CRACKED. REMOVED HAT CHANNEL, FABRICATED NEW CHANNEL AND REINSTALLED NEW SECTION IAW SRM 51-30-2.
- [SDR 7AHR2014020682420](https://openairdocs.org/sdr/7AHR2014020682420.md): Seat Track · damaged · Feb 6, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CROWN DAMAGED AT BS 480+12 LBL 6L. CUT AND REMOVED DAMAGED AREA IAW SRM 53-10-05, FIG 9 AND INSTALLED REPAIR IAW SRM 51-30-02.
- [SDR 7AHR2014020642415](https://openairdocs.org/sdr/7AHR2014020642415.md): Seat Track · corroded · Feb 6, 2014 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FLANGE HAS CORROSION AROUND FASTENER HOLES UPPER & LOWER SURFACES BS 400 TO 460, RBL 62. INSTALLED REPAIR IAW SRM 53-10-5.
- [SDR 7AHR2014020582500](https://openairdocs.org/sdr/7AHR2014020582500.md): Floorbeam · corroded · Feb 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > FLOORBEAM UPPER SURFACE HAS CORROSION AT BS 616 BL 0-LBL 26. REPAIRED IAW SRM 51-30-2.
- [SDR 7AHR2014020548259](https://openairdocs.org/sdr/7AHR2014020548259.md): Intercostal · corroded · Feb 6, 2014 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED, FWD CARGO BAY LBL 24.5 BETWEEN BS 500B AND 500A. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2.
- [SDR TSAA20140113001](https://openairdocs.org/sdr/TSAA20140113001.md): Structure · corroded · Jan 9, 2014 · N841AL · Boeing 7372X6C · Horizontal Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED A CHECK INSPECTION, AN AREA CORROSION DAMAGE 1.25 INCHES WIDE & 0.875 INCHES LONG & 0.060 INCHES DEEP WAS FOUND ON THE LT STABILIZER AT ELEVATOR STATION 102.5. REMOVED CORROSION, SANDED, POLISHED, BLENDED, REWORKED AREA & APPLIED A DOUBLER

Next page: https://openairdocs.org/model/boeing-737-2x6c/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 = '7372X6C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2x6c/reports

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