# Service difficulty reports: N9056R

A list on [N9056R](https://openairdocs.org/aircraft/N9056R.md).

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

- [SDR FXGA202212232233](https://openairdocs.org/sdr/FXGA202212232233.md): None · none · Dec 23, 2022 · N9056R · Doug DC6A · Wing Structure
  > CRACKED TANG ON FRONT SPAR UPPER CAP. TO REPAIR A CRACKED TANG ON THE FORWARD EDGE OF THE FRONT SPAR UPPER CAP. USE THIS EO IN CONJUNCTION WITH STS EA 81-2022-151.
- [SDR FXGA202110072132](https://openairdocs.org/sdr/FXGA202110072132.md): Skin · cracked · Oct 7, 2021 · N9056R · Doug DC6A · Horizontal Stabilizer, Plate/Skin
  > CRACKED R/H HORIZONTAL STABILIZER LEADING EDGE AT STATION 109. TO REPAIR A CRACK LEADING EDGE SKIN ON THE R/H HORIZONTAL STABILIZER AT STATION 109. STOP DRILL CRACK AND REPAIR LEADING EDGE PER DC-6 A&B OVERHAUL MANUAL FIGURED 15-31 SHEET 2 OF 2.
- [SDR FXGA20200813001](https://openairdocs.org/sdr/FXGA20200813001.md): Line · leaking · Aug 12, 2020 · N9056R · Doug DC6A · Hydraulic System, Main
  > DURING APPROACH, HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. DIVERTED. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN HYD PUMP HYDRALIC PRESSURE LINE LEAKING FROM HOSE FAILURE UNDER PROTECTIVE HOSE COVERING. NO EXTERNAL DAMAGE EVIDENT ON LINE ASSEMBLY,
- [SDR FXGA201909261976](https://openairdocs.org/sdr/FXGA201909261976.md): Angle · bent · Sep 26, 2019 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > FORWARD PRESSURE BULKHEAD BEAM REPAIR. TO REPAIR A BENT ANGLE ON THE FORWARD PRESSURE BULKHEAD, ON THE WHEEL WELL SIDE. AT F/STA 0. REPAIR RT END OF LOWER HORIZONTAL BEAM OF FORWARD PRESSURE BULKHEAD PER A&B OVERHAUL MANUAL FIGURE 12-5.
- [SDR FXGA201908281969](https://openairdocs.org/sdr/FXGA201908281969.md): Fitting · corroded · Aug 28, 2019 · N9056R · Doug DC6A · Wing, Attach Fittings
  > REPLACEMENT OF CORRODED FITTING AT STRINGER 17 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 17L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.
- [SDR FXGA201908281970](https://openairdocs.org/sdr/FXGA201908281970.md): Tee Fitting · corroded · Aug 28, 2019 · N9056R · Doug DC6A · Wing, Attach Fittings
  > REPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.
- [SDR FXGA2019082820191](https://openairdocs.org/sdr/FXGA2019082820191.md): Tee Fitting · corroded · Aug 28, 2019 · N9056R · Doug DC6A · Wing, Attach Fittings
  > REPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.
- [SDR FXGA201908261967](https://openairdocs.org/sdr/FXGA201908261967.md): Skin · cracked · Aug 26, 2019 · N9056R · Doug DC6A · Wing, Plate/Skin
  > MULTIPLE WING SKIN CRACKS AT W/STA 168R BETWEEN STRINGERS 6 AND 11. MULTIPLE SMALL CRACKS WERE FOUND ON THE UPPER WING SKIN IN THE HELL HOLE AREA AROUND W/STA 168R BETWEEN STRINGERS 6 AND 11. GAIN ACCESS TO THE REPAIR AREA BY REMOVING A SECTION OF NACELLE, R
- [SDR FXGA201908161966](https://openairdocs.org/sdr/FXGA201908161966.md): Skin · corroded · Aug 16, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT LOWER EDGE OF MAIN CARGO DOOR. TO REPAIR CORRODED FUSELAGE SKIN AT LOWER EDGE OF MAIN CARGO DOOR BETWEEN F/STA 768 AND 790. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.
- [SDR FXGA2019081261963](https://openairdocs.org/sdr/FXGA2019081261963.md): Stringer · cracked · Aug 6, 2019 · N9056R · Doug DC6A · Nacelle/Pylon, Main Frame
  > NR 4 NACELLE STRINGER AND SKIN SPLICE. TO SPLICE NR 4 NACELLE STRINGERS NR 1 AT STATION 436 AND STRINGER 32 AT STATION 432.5. THE NACELLE SKIN WILL BE SPLICED AT STRINGER 2 BETWEEN STATION 400 AND 473. NUMEROUS REPAIRS WERE PREVIOUSLY INSTALLED ON THE UPPER
- [SDR FXGA201908061964](https://openairdocs.org/sdr/FXGA201908061964.md): Stringer Splice · corroded · Aug 6, 2019 · N9056R · Doug DC6A · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER SPLICES ON STRINGER 32L BETWEEN F/STA 625 AND 638, STRINGER REPAIRED IAW A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA201908051958](https://openairdocs.org/sdr/FXGA201908051958.md): Spar Web · corroded · Jul 25, 2019 · N9056R · Doug DC6A · Wing Spar
  > CORRODED REAR SPAR WEB AT W/STA 359L. TO REPAIR A CORRODED REAR SPAR WEB AT W/STA 359L. CUT OUT CORRODED AREA AND REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-5.
- [SDR FXGA2019080521957](https://openairdocs.org/sdr/FXGA2019080521957.md): Spar · cracked · Jul 25, 2019 · N9056R · Doug DC6A · Wing Spar
  > CRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. TO REPAIR A CRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. PERFORM OUTER WING CENTER SPAR WEB REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-7.
- [SDR FXGA2019080541956](https://openairdocs.org/sdr/FXGA2019080541956.md): Skin · corroded · Jul 24, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPLACEMENT AND STRINGER REPAIRS BEHIND CABIN HEATER EXHAUST. TO REPLACE A CORRODED FUSELAGE SKIN FROM F/STA 596 TO 662; REPAIR CORRODED STRINGER #31L BETWEEN F/STA 629 AND 658, AND STRINGER 32L BETWEEN F/STA 629 AND 651. REMOVE AND REPLACE COR
- [SDR FXGA2019080591954](https://openairdocs.org/sdr/FXGA2019080591954.md): Skin · corroded · Jul 19, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT F/STA 801 STRINGER 8L. TO REPAIR CORRODED FUSELAGE SKIN LAP AFT OF THE MAIN CARGO DOOR AT F/STA 801 STRINGER 8L. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.
- [SDR FXGA201907091953](https://openairdocs.org/sdr/FXGA201907091953.md): Skin · corroded · Jul 9, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED ABOVE FORWARD BAG PIT DOOR. TO REPAIR CORRODED FUSELAGE SKIN ABOVE FORWARD BAG PIT DOOR, AT F/STA 162 BETWEEN STRINGER 23R & 24R. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.
- [SDR FXGA201906281950](https://openairdocs.org/sdr/FXGA201906281950.md): Rib · cracked · Jun 28, 2019 · N9056R · Doug DC6A · Wing, Rib/Bulkhead
  > LEADING EDGE RIB CAP REPAIR AT W/STA 184R. TO REPAIR A CRACKED LEADING EDGE RIB TEE CAP AT W/STA 184R. CUT CRACKED TEE CAP ANGLE IN A SUITABLE LOCATION FORWARD OF THE SWING PANEL HINGE. MANUFACTURE NEW TEE ANGLE AND SPLICE ANGLES PER DRAWING # 1950-01.
- [SDR FXGA201909051942](https://openairdocs.org/sdr/FXGA201909051942.md): Skin · corroded · May 17, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > CORRODED FUSELAGE SKIN REPAIRS AROUND MULTIPLE CABIN WINDOWS. TO REPAIR CORRODED FUSELAGE SKIN AROUND CABIN WINDOWS AT THE FOLLOWING LOCATIONS: F/STA 285 LEFT SIDE, F/STA 770 LEFT SIDE, F/STA 790 RIGHT SIDE AND F/STA 930 RIGHT SIDE. THE FUSELAGE SKIN IS CORR
- [SDR FXGA201905171943](https://openairdocs.org/sdr/FXGA201905171943.md): Doubler · cracked · May 17, 2019 · N9056R · Doug DC6A · Wing, Plate/Skin
  > NR 2 ALT ACCESS DOOR DOUBLER REPLACEMENT. TO REPLACE A CRACKED ACCESS DOOR DOUBLER AT NR 2 ATLERNATE TANK. REMOVE AND REPLACE NR 2 ALTERNATE TANK ACCESS DOOR DOUBLER PER SERVICE BULLETIN #842.
- [SDR FXGA201905141940](https://openairdocs.org/sdr/FXGA201905141940.md): Skin · corroded · May 14, 2019 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > CORRODED FUSELAGE SKIN AT F/STA 150 STRINGER 33L. CORROSION WAS FOUND 2 INCHES FORWARD OF AN EXISTING REPAIR MADE PER OVERHAUL MANUAL FIGURE 12-22. REMOVE EXISTING REPAIR AND CUT-OUT CORRODED AREA. EXTEND REPAIR PER OVERHAUL MANUAL FIGURE 12-22 TO COVER NEW
- [SDR FXGA201908051955](https://openairdocs.org/sdr/FXGA201908051955.md): Fitting · corroded · May 8, 2019 · N9056R · Doug DC6A · Wing, Attach Fittings
  > REPLACEMENT OF CORRODED FITTING AT STRINGER 20 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 20L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.
- [SDR FXGA201905081937](https://openairdocs.org/sdr/FXGA201905081937.md): Fitting · corroded · May 8, 2019 · N9056R · Doug DC6A · Wing Miscellaneous Structure
  > REPLACEMENT OF CORRODED FITTING AT W/STA 60L STRINGER 21L. TO REPLACE CORRODED FITTINGS ON STRINGER 21L, INBOARD AND OUTBOARD OF W/STA 60L. ON WING STRINGER 21L, REMOVE INBOARD AND OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH NEW ONES.
- [SDR FXGA2019062681938](https://openairdocs.org/sdr/FXGA2019062681938.md): Fitting · corroded · May 8, 2019 · N9056R · Doug DC6A · Wing, Attach Fittings
  > REPLACEMENT OF CORRODED FITTING AT W/STA 60R STRINGER 21. TO REPLACE CORRODED FITTING INBOARD AND OUTBOARD OF W/STA 60R. REMOVE INBOARD AND OUTBOARD RIGHT HAND STATION 60 FITTINGS AND REPLACE WITH NEW ONES.
- [SDR FXGA201807311816](https://openairdocs.org/sdr/FXGA201807311816.md): Skin · chafed · Jul 31, 2018 · N9056R · Doug DC6A · Trailing Edge Flaps
  > CHAFED SKIN ON RT FLAP UPPER SKIN AT W/STA 370R. THE RIGHT HAND FLAP UPPER SKIN WAS FOUND CHAFED ON THE LEADING EDGE SECTION AT W/STA 370R. REMOVE DAMAGE IN A RACE TRACK SHAPE AND REPAIR PER A&B OHM FIGURE 13-47A. USE NAS1097AD RIVETS INSTEAD OF AN426AD RIV
- [SDR FXGA201708031715](https://openairdocs.org/sdr/FXGA201708031715.md): Skin · cracked · Aug 2, 2017 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > CRACKED SKIN AT STATION 239 AND STRINGER 33 1/2. REPAIR TO SKIN CRACK AT STATION 239. INSTALL REPAIR IN ACCORDANCE WITH DC6 OVERHAUL MANUAL FIGURE 12-21 AND 12-22.
- [SDR 2017F00172](https://openairdocs.org/sdr/2017F00172.md): Line · cracked · Jul 19, 2017 · N9056R · Doug DC6A · Hydraulic System, Main
  > COMPLETE HYDRAULIC SYSTEM FAILURE, EMERGENCY LANDING PROCEDURES FOLLOWED. REPLACED HYDRAULIC PRESSURE LINE NR 2. FOUND CRACK AT B-NUT. REPLACED THE LINE. PREFORMED LEAK CHECK & OPS CHECK OKAY. RELEASED AIRCRAFT FOR CONT SERVICE.
- [SDR FXGA2016080916162](https://openairdocs.org/sdr/FXGA2016080916162.md): Stringer · corroded · Aug 9, 2016 · N9056R · Doug DC6A · Fuselage Main, Longeron/Stringer
  > CORRODED STRINGER 12L AT BS 1049. REPAIRED THE STRINGER IAW A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA201607181618](https://openairdocs.org/sdr/FXGA201607181618.md): Skin · damaged · Jul 18, 2016 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND STRINGER REPAIR AT BS 341, STRINGER 27L. TO REPAIR THE CORRODED SKIN AND STRINGER 27L AT BS 341. CUT-OUT OF THE CORRODED SKIN AND REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-22. CUT STRINGER 27L BETWEEN BS 332 AND 350. REPAIR PER A&B OVERHAUL M
- [SDR FXGA201607191616](https://openairdocs.org/sdr/FXGA201607191616.md): Skin · damaged · Jul 11, 2016 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > SKIN CORROSION AND HOLE IN SKIN AFT OF LOWER CORNER OF AFT BELLY DOOR BETWEEN STRINGERS 30 AND 31R. REPAIRED THE SKIN. REMOVE DAMAGE & PREFORM REPAIR IAW OVERHAUL MANUAL FIGURE 12-22.
- [SDR FXGA201511111542](https://openairdocs.org/sdr/FXGA201511111542.md): Bulkhead · damaged · Nov 11, 2015 · N9056R · Doug DC6A · Fuselage Main, Bulkhead
  > HOLE IN BULKHEAD AT FS 341 ABOVE STRINGER 32R. REPAIRED DAMAGED BULKHEAD IAW DC-6A & B OVERHAUL MANUAL FIGURE 12 - 6.
- [SDR FXGA201510281541](https://openairdocs.org/sdr/FXGA201510281541.md): Floor Skin · corroded · Nov 10, 2015 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SKIN BETWEEN FS 520 & 540. REPAIRED CORRODED SKIN IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-15.
- [SDR FXGA201510291540](https://openairdocs.org/sdr/FXGA201510291540.md): Floor Skin · corroded · Oct 28, 2015 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SKIN, BETWEEN FS 866 & 902, AROUND RBL 10. REPAIR CORRODED SKIN IAW DC-6 A & B, OVERHAUL MANUAL FIG 12-16.
- [SDR FXGA201503151512](https://openairdocs.org/sdr/FXGA201503151512.md): Skin · chafed · Mar 23, 2015 · N9056R · Doug DC6A · Wing, Plate/Skin
  > CHAFED WING SKIN AT WS 297R, STRINGER 26R. TO REPAIR CHAFING, CAUSED BY A FAIRING, BEAVER TAIL, RUBBING AGAINST THE LOWER WING SKIN AT WS 297R, STRINGER 26R. CUT OUT DAMAGED AREA & INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM AN 01-40NL-3 FIGURE 2-62.
- [SDR FXGA20150323001](https://openairdocs.org/sdr/FXGA20150323001.md): Stringer · corroded · Mar 23, 2015 · N9056R · Doug DC6A · Fuselage Main, Longeron/Stringer
  > REPAIR OF CORRODED FUSELAGE STRINGER FS 541, STRINGER 33L. CUT DAMAGED STRINGER. REMOVE CORRODED SECTION & INSTALLED NEW STRINGER SECTION & SPLICES IAW DC6 A & B OVERHAUL MANUAL FIGURE 12 - 2 PAGE 3 & 4.
- [SDR FXGA20141104001](https://openairdocs.org/sdr/FXGA20141104001.md): Unknown · leaking · Oct 31, 2014 · N9056R · Doug DC6A · Hydraulic System, Main
  > HYDRAULIC FAILURE, LOSS OF PRESS & QTY EXPERIENCED WHILE TURNING ONTO RUNWAY 33.
- [SDR FXGA201408121428](https://openairdocs.org/sdr/FXGA201408121428.md): Frame · cracked · Aug 12, 2014 · N9056R · Doug DC6A · Fuselage Main, Frame
  > FRAME CRACK AT FS 29.5L. THE LT FRAME RAIL LOCATED AT FS 29.5L CRACKED JUST ABOVE THE FWD HINGE POINT OF LT NLG DOOR. A NEW SECTION OF FRAME WILL BE SPLICED IN FROM STRINGER 22 TO 31.
- [SDR FXGA2014010901](https://openairdocs.org/sdr/FXGA2014010901.md): Structure · corroded · Jan 9, 2014 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FRONT SPAR OF LT REAR HYD COMPARTMENT APPROXIMATELY STATION 412 FROM STRINGERS 26 -30. REPLACED STRINGER 25L FROM SPLICE AT STATION 341 TO ITS END AT STATION 41. INSTALLED DOUBLER OVER CUTOUT, REQUIRED BY STRINGER REMOVAL, AT STATION 341-3
- [SDR FXGA201305131344](https://openairdocs.org/sdr/FXGA201305131344.md): Skin · corroded · May 13, 2013 · N9056R · Doug DC6A · Wing, Plate/Skin
  > CORROSION ON WING SKIN BETWEEN LWS 167 & WS 216. REPAIRED IAW EO 1344.
- [SDR FXGA201212071292](https://openairdocs.org/sdr/FXGA201212071292.md): Floor Support · corroded · Dec 7, 2012 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT BETWEEN BS 630 & 791L. R & R FLOOR SUPPORT.
- [SDR FXGA201210051279](https://openairdocs.org/sdr/FXGA201210051279.md): Structure · cracked · Oct 5, 2012 · N9056R · Doug DC6A · Powerplant System
  > NR 4 ENGINE AIRFOIL ANTI-ICE HEATER EXHAUST OPENING CRACKING. REPAIR OF CRACKING AROUND AIRFOIL ANTI-ICE HEATER EXHAUST DUCT ON NR 4 ENG EO 1279.
- [SDR FXGA201208301267](https://openairdocs.org/sdr/FXGA201208301267.md): Structure · corroded · Aug 30, 2012 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > HEATER COMPARTMENT CORRODED BS 500 - 541. REPAIRED IAW EO 1267.
- [SDR FXGAN9056R2](https://openairdocs.org/sdr/FXGAN9056R2.md): Skin · corroded · Oct 6, 2011 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FOUND SKIN CORROSION FUS STA 157 AT STR 31L. REPAIRED IAW EAC EO 1133 AND 8110-3 DATED 1-19-05.
- [SDR FXGAN9056R8](https://openairdocs.org/sdr/FXGAN9056R8.md): Skin · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > SKIN CORROSION DISCOVERED AT FUS STA 780 CENTERED UNDER FUS STR 32L. REPAIRED IAW EAC EO 11321 AND 8110-3 DATED 9/29/2011.
- [SDR FXGAN9056R7](https://openairdocs.org/sdr/FXGAN9056R7.md): Structure · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > CORROSION DISCOVERED ON THE CABIN FLOOR FROM STA 625 TO FUS STA 661. REPAIRED IAW EAC EO 1129 AND 8110-3 DATED9/27/2011.
- [SDR FXGAN9056R6](https://openairdocs.org/sdr/FXGAN9056R6.md): Stringer · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON FUS STR 32L AT FUS 780. REPAIRED IAW WITH EAC EO 1131 AND 8110-3 DATED 9/29/2011.
- [SDR FXGA20111003005](https://openairdocs.org/sdr/FXGA20111003005.md): Skin · dented · Oct 3, 2011 · N9056R · Doug DC6A · Wing, Plate/Skin
  > RT WING HAD A LARGE DENT FROM STA 655 TP 675. REPAIRED IAW EO 1128 AND 8110-3 DATED 9-29-2011.
- [SDR FXGA20111003002](https://openairdocs.org/sdr/FXGA20111003002.md): Floor Skin · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Miscellaneous Structure
  > FOUND CORRODED FLOOR SKIN AT FUS STA 120. REPAIRED IAW EAC EO 1135 AND 8110-3 DATED 9-20-11.
- [SDR FXGA20111003001](https://openairdocs.org/sdr/FXGA20111003001.md): Skin · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FOUND SKIN CORROSION AT FUS STA 157 BETWEEN STR 33L AND 33R. REPAIRED IAW EAC EO 1134 AND 8110-3 DATED 9-20-2011.
- [SDR FXGAN9056R1](https://openairdocs.org/sdr/FXGAN9056R1.md): Skin · corroded · Oct 3, 2011 · N9056R · Doug DC6A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FOUND CORRODED FUS STA 89 TO STA 111 BETWEEN STR 10L AND 13L. REPAIRED IAW EAC EO 1130 AND AND 8110-3 DATED 9/15/2011.
- [SDR FXGA9056R](https://openairdocs.org/sdr/FXGA9056R.md): Structure · corroded · Aug 20, 2010 · N9056R · Doug DC6A · Wing Miscellaneous Structure
  > DEEP CORROSION FOUND AT MULTIPLE NUT PLATE HOLES ALONG THE NR 2 NACELLE FILLET FAIRING BETWEEN THE FRONT AND CENTER SPAR. REPAIRED PER EAC EO 1044 AND 8110-3 DATED 8/20/10.

## 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 = 'N9056R' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N9056R/reports

---
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