# Service difficulty reports: N921R, cancelled Feb 16, 2011

A list on [N921R, cancelled Feb 16, 2011](https://openairdocs.org/deregistered/N921R-2011-02-16.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 2 · 80 reports

- [SDR N921RM81664](https://openairdocs.org/sdr/N921RM81664.md): Skin · cracked · Oct 26, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > "D" PIT DOOR DAMAGED FORWARD UPPER SKIN AT CORNER. APPROX.375 INCH CRACK RADIATED FROM EDGE OF FUSELAGE SKIN IN DOOR RADIUS AND TERMINATED AT FIRST FASTENER.
- [SDR N921R63501](https://openairdocs.org/sdr/N921R63501.md): Skin · dented · Jan 9, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE EXTERIOR STA 78 BTW L17L AND L18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000 0551.
- [SDR N921R63504](https://openairdocs.org/sdr/N921R63504.md): Skin · dented · Jan 9, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000-0551.
- [SDR N921R54017](https://openairdocs.org/sdr/N921R54017.md): Splice · corroded · Jan 8, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > LWR FUSELAGE EXTERIOR STA 1766 L-33L MANUFACTURING SPLICE WITH CORROSION. REMOVED SPLICE IAW DPS 3.67.27, FABRICATED NEW SPLICE IAW DC8 SRM 53-4-1 AND DPS 3.69.4. PRIMED NEW SPLICE IAW DC8 SRM 51-1-8 AND INSTALLED NEW SPLICE IAW DC8 SRM 51-1-21 CPCP 5000 055
- [SDR N921R54815](https://openairdocs.org/sdr/N921R54815.md): Skin · dented · Jan 8, 2007 · N921R · Doug DC863F · Trailing Edge Flaps
  > LT WING XW 68 INBOARD FLAP TRAILING EDGE LOWER SURFACE WITH DENT ( L=3 1/8, A=2 1/2, Y=.0935). CUTOUT DAMAGED AREA AND FABRICATED FILLER, SPLICE AND SKIN IAW DC8 SRM 57-2-5 AND DC8 SRM 57-7-1. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8. INS
- [SDR N921R53410](https://openairdocs.org/sdr/N921R53410.md): Door Frame · cracked · Jan 8, 2007 · N921R · Doug DC863F · Fuselage Main, Structure
  > FUSELAGE STA 8 NLG W/W DOOR JAMB RT CORNER SKIN WITH 1" CRACK. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 51-07030-1 REV NEW 01-25-07 PAGE 1 AND 2. ISSUED FAA FORM 8110-3 CPCP 4000 0551.
- [SDR N921R53309](https://openairdocs.org/sdr/N921R53309.md): None · none · Jan 8, 2007 · N921R · Doug DC863F · Standard Practices/Structures
  > FUSELAGE STA 8 NLG WW DOOR JAMB LT CORNER SKIN WITH TEMPORARY REPAIR. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 53-07030-1 REV NEW 01-25-09 PAGE 1/3. ISSUED FAA FORM 8110-3. CPCP 4000 0551
- [SDR N921R53506](https://openairdocs.org/sdr/N921R53506.md): Skin · damaged · Jan 8, 2007 · N921R · Doug DC863F · Landing Gear Doors
  > FUSELAGE STA 32 NLG DOOR SKIN HAS 2 NICKS. REPAIRED SKIN OF FUSELAGE STA 32 NLG RT DOOR IAW DC8 SRM 52-2-0 CPCP 4000 0551.
- [SDR N921R53905](https://openairdocs.org/sdr/N921R53905.md): Skin · corroded · Jan 8, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERIOR STA 720 L-17L SKIN WITH CORROSION. OPENED SKIN AREA IAW DPS 3-67-27, FOUND CORRODED INNER DOUBLER, REMOVED INNER DOUBLER IAW DPS 3-67-27. FABRICATED NEW INNER DOUBLER IAW DC8 SRM 53-5-3 & DPS 3-69-4. TREATED AND PRIMED AREA AND NEW D
- [SDR N921R50502](https://openairdocs.org/sdr/N921R50502.md): Skin · dented · Jan 6, 2007 · N921R · Doug DC863F · Rudder, Plate/Skin
  > RUDDER ZR 138 LEFT SKIN AFT SECTION WITH DENT. REMOVED LT SKIN SECTION IAW DPS 3.67-27. FABRICATED NEW SKIN IAW DPS 3.69-4. TREATED AND PRIMED AREA AND NEW SKIN IAW DC8 SRM 51-1-8. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21.
- [SDR N921R40407](https://openairdocs.org/sdr/N921R40407.md): Frame Splice · corroded · Jan 5, 2007 · N921R · Doug DC863F · Fuselage Main, Frame
  > MAIN CARGO COMPARTMENT STA 520, L-17R FRAME SPLICE WITH CORROSION. REMOVED FRAME SPLICE IAW DPS 3-67-29. FABRICATED NEW FRAME SPLICE IAW DPS 3-69-4, PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-27 CPCP 5730-0551.
- [SDR N921R28116](https://openairdocs.org/sdr/N921R28116.md): Stringer Splice · cracked · Jan 4, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT BTW STA 440 AND 460, L31L SPLICE FITTING WITH 3/4" CRACK. REMOVED AND REPLACED SPLICE FITTING OF FWD CARGO COMPARTMENT BTW STA 440 AND STA 460, L31L IAW DC8 SRM 51-1-20 AND SRM 53-4-1 CPCP 557L 0551.
- [SDR N921R28211](https://openairdocs.org/sdr/N921R28211.md): Finger Doubler · corroded · Jan 4, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT STA. 480, L31R FINGER DOUBLER WITH CORROSION. CLEANED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8 CPCP 557R 0551.
- [SDR N921R72213](https://openairdocs.org/sdr/N921R72213.md): Longeron · corroded · Jan 3, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > FOUND FUSELAGE STA 1540 L29L SKIN RIVETS SHEARED AND LONGERON 29L WITH CORROSION. REPAIRED LONGERON 29L AT FS 1540 IAW DC8 SRM 53-2-2 FIGURE 8.
- [SDR N921R19512](https://openairdocs.org/sdr/N921R19512.md): Stringer Splice · cracked · Jan 3, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > FOUND MAIN CARGO COMPARTMENT STA 680, L4R AFT SPLICE FITTING WITH CRACK. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20 AND 53-4-1 CPCP 5730-0553.
- [SDR U2RA3201](https://openairdocs.org/sdr/U2RA3201.md): Skin · corroded · May 24, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > TOP OF LT MAIN LANDING GEAR TOP SURFACE CORRODED APPROXIMATELY 1 X 4 INCHES AT STATION 860, LBL 40 TO LBL 44.
- [SDR U2RA3218](https://openairdocs.org/sdr/U2RA3218.md): Frame · damaged · May 23, 2005 · N921R · Doug DC863F · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED AT STATION 1560, L21L.
- [SDR U2RA3142](https://openairdocs.org/sdr/U2RA3142.md): Pressure Panel · corroded · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > FS 980 TO FS 970 TOP SURFACE OF THE RIGHT MAIN LANDING GEAR WELL HAS POPPED RIVETS/BULGING AT ATTACH ANGLE, IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR U2RA3147](https://openairdocs.org/sdr/U2RA3147.md): Frame · corroded · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Frame
  > SEVERAL SMALL AREAS OF CORROSION IN FWD ACCESSORY COMPARTMENT AT AFT BULKHEAD CIRCUMFERENTIAL FS 80 L32L TO L32R. IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR U2RA2962](https://openairdocs.org/sdr/U2RA2962.md): Finger Doubler · corroded · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > RIVET HEAD POPPED FS 200, RT SIDE OF THE AIRCRAFT BELOW THE AUX STATIC PORT IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR U2RA3216](https://openairdocs.org/sdr/U2RA3216.md): Fitting · cracked · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Attach Fittings
  > FITTING CRACKED AFT OF CARGO DOOR AT FS 300 AT CUSP LT SIDE.
- [SDR U2RA3399](https://openairdocs.org/sdr/U2RA3399.md): Stringer · cracked · May 10, 2005 · N921R · Doug DC863F · Wing, Longeron/Stringer
  > RIGHT WING LOWER INNER STRINGER CRACKED AT WING STATION X624.
- [SDR U2RA3140](https://openairdocs.org/sdr/U2RA3140.md): Fitting · cracked · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Attach Fittings
  > LONGERON 24 LT AFT BATHTUB FITTING CRACKED AT FS 1690.
- [SDR U2RA3396](https://openairdocs.org/sdr/U2RA3396.md): Skin · cracked · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > R2 DOOR HAS CRACK INDICATION AT UPPER AFT CORNER FS 1660, L11R.
- [SDR U2RA2982](https://openairdocs.org/sdr/U2RA2982.md): Skin · corroded · May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > FS 12 IN NOSE WHEEL WELL CEILING SKIN BULGING WITH 3 POPPED RIVETS, IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 2039](https://openairdocs.org/sdr/2039.md): Skin Panel · cracked · May 22, 2004 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED FUSELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH.
- [SDR 2025](https://openairdocs.org/sdr/2025.md): Oil Filter · leaking · May 13, 2004 · N921R · Doug DC863F · Engine Oil Quantity
  > SHUTDOWN NR 2 ENGINE CLIMBING OUT OF ILG AT FL240 AT 1220Z OIL QUANTITY DROPPED TO 1 GALLON, WINDMILLING OIL PRESSURE 20 PSI.
- [SDR 2006](https://openairdocs.org/sdr/2006.md): Track · damaged · Apr 23, 2004 · N921R · Doug DC863F · Engine Thrust Reverser
  > POST FLIGHT INSPECTION NR 2 THRUST REVERSER AND TRANSLATING RING DAMAGED.LOWER T/R TRACK STOP AND ATTACHING HARDWARE MISSING. DOUGLAS SERVICE BULLETIN 78-100 IDENTIFIES THIS PROBLEM.
- [SDR 1982](https://openairdocs.org/sdr/1982.md): Wire · shorted · Mar 18, 2004 · N921R · Doug DC863F · Engine Oil Pressure
  > NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENGINE AT 2245Z, OIL PRESSURE 45PSI,OIL TEMP 95 DEGREES C, WINDMILLING OIL PRESSURE 32 PSI.
- [SDR 1965](https://openairdocs.org/sdr/1965.md): Crank Assy · fractured · Feb 28, 2004 · N921R · Doug DC863F · Leading Edge Slat Control System
  > FLIGHT CREW REPORTED WING SLOT LIGHT ON WITH FLAPS EXTENDED. FOUND RIGHT AHND EXTENDED LEADING OOUTBOARD SLOT DOOR INOPERATIVE DUE TO FRACTURED AND BROKEN CRANK ASSEMBLY AT STA.XS476
- [SDR U2R2004F00001](https://openairdocs.org/sdr/U2R2004F00001.md): Fastener · mismanufactured · Oct 29, 2003 · N921R · Doug DC863F · Fasteners
  > REPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM.
- [SDR U2R2004F00000](https://openairdocs.org/sdr/U2R2004F00000.md): Spar Cap · cracked · Oct 29, 2003 · N921R · Doug DC863F · Wing Spar
  > DURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.
- [SDR U2RB102903](https://openairdocs.org/sdr/U2RB102903.md): Spar Cap · cracked · Oct 29, 2003 · N921R · Doug DC863F · Wing Spar
  > DURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITIO
- [SDR 20010124SG002](https://openairdocs.org/sdr/20010124SG002.md): Compressor · overserviced · Dec 13, 2000 · N921R · Doug DC863F · Cabin Compressor System
  > ON TEST FLIGHT, SMOKE IN COCKPIT. FOUND NR 2 AND NR 3 TURBO COMPRESSORS OVERSERVICED. SERVICED PROPERLY IAW MM 21-10-01. (M)
- [SDR RRXA99803](https://openairdocs.org/sdr/RRXA99803.md): Control Cable · unsecure · May 20, 1999 · N921R · Doug DC863F · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. NO ATTEMPT AT HANDLE LATCH FLIGHT RELEASE. FOUND LANDING GEAR ANTI RETRACTION CABLE NOT SECURE, SECURED SAME LDG GEAR HANDLE AND GEAR OPS NORMAL ON GRD CK.
- [SDR RRXA98270](https://openairdocs.org/sdr/RRXA98270.md): Wheel · broke off · Jul 20, 1998 · N921R · Doug DC863F · Wheel/Ski/Float
  > ON LANDING, THE NR 1 MLG WHEEL AND TIRE ASSEMBLY BROKE FROM AXLE. TIRE ASSEMBLY ROLLED INTO PARKED EQUIPMENT. AIRCRACFT WAS TOWED TO RAMP FOR INSPECTION. *S/D* REMOVED AND REPLACED NR 1 MAIN WHEEL AND TIRE ASSEMBLY, REPLACED NR 1 MAIN BRAKE ASSEMBLY, REPLA
- [SDR RRXA97321](https://openairdocs.org/sdr/RRXA97321.md): Floorbeam · corrosion · Dec 14, 1997 · N921R · Doug DC863F · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT, FOUND FLOORBEAM CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT STA 920.57 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED COTNEY ENGINEERING SKETCH D02-R04. TREATED AREA IAW DC-8 SRM 51-1-8.
- [SDR RRXA97265](https://openairdocs.org/sdr/RRXA97265.md): Pressure Web · corroded · Sep 12, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER FINGER DOUBLER ATTACH TO PRESSURE WEB AT, STA 974 AND BL 65 RIGHT SIDE. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R16 AN
- [SDR RRXA97262](https://openairdocs.org/sdr/RRXA97262.md): Longeron · corroded · Sep 12, 1997 · N921R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON LONGERON 31 LEFT AT, STA 163 TO STA 170. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R17 AND DC-8 SRM 51-1-8, 51-1-21 AND 53-2
- [SDR RRXA97263](https://openairdocs.org/sdr/RRXA97263.md): Beam · corroded · Sep 11, 1997 · N921R · Doug DC863F · Fuselage Main, Structure
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT PRESSURE BULKHEAD VERTICAL BEAM AT STA 1754 RIGHT SIDE, LOWER AFT FACE. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R18.
- [SDR RRXA97256](https://openairdocs.org/sdr/RRXA97256.md): Support · corroded · Sep 4, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE PAST LIMITATIONS ON FLOOR SUPPORT AT, STA 1660 AND BL 33 RIGHT. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED (2 EACH) FILLERS AND DOUBLERS IAW FAA DER APPROVED ENGINEERING SKETCH D02-R15 AND DC-8
- [SDR RRXA97264](https://openairdocs.org/sdr/RRXA97264.md): Longeron · cracked · Sep 3, 1997 · N921R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT, FOUND CRACK ON LONGERON 34 RIGHT AT, STA 1270. *S/D* REMOVED LONGERON 34R, FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D02-R09.
- [SDR RRXA97319](https://openairdocs.org/sdr/RRXA97319.md): Skin · damaged · Aug 27, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT, FOUND FUSELAGE OUTER SKIN BENT AND DAMAGED BELOW A PIT DOOR BETWEEN STA 296 TO STA 302. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R01.
- [SDR RRXA97252](https://openairdocs.org/sdr/RRXA97252.md): Skin · corroded · Aug 27, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND BULGE IN FUSELAGE SKIN LONGERON 28 LT FS 1655 TO 1660.
- [SDR RRXA97249](https://openairdocs.org/sdr/RRXA97249.md): Pressure Web · corroded · Aug 27, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND PRESSURE WEB UPPER SURFACE CORRODED FS 923 BL 0.
- [SDR RRXA97251](https://openairdocs.org/sdr/RRXA97251.md): Angle · corrosion · Aug 26, 1997 · N921R · Doug DC863F · Wing Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND LT WING INBD L/E UPPER SCREW ATTACH HOLES CORRODED AT ATA XFS 41 TO 55. *S/D* REMOVED CORROSION AND FOUND LEADING EDGE UPPER SPAR ATTACHMENT ANGLE DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED ATTACHMENT ANGLE, FABRICATED
- [SDR RRXA97250](https://openairdocs.org/sdr/RRXA97250.md): Angle · corrosion · Aug 26, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND LT WHEEL WELL UPPER PRESSURE WEB ATTACH ANGLE CORRODED FS 857 BL 41 TO 46 LT. *S/D* REMOVED ATTACHMENT ANGLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-5 FIGURE 16 SHEET 2. TREATED AREA IAW
- [SDR RRXA97248](https://openairdocs.org/sdr/RRXA97248.md): Skin · corroded · Aug 26, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK, INSPECTION FOUND RT FWD WASTE SERVICE DOOR HINGE ATTACH AREA IS CORRODED FS 83 TO 96, LONGERON 27 RT AND 28. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER COTNEY ENGINEERING SKETCH D02-R10. TRE
- [SDR RRXA97247](https://openairdocs.org/sdr/RRXA97247.md): Frame · corroded · Aug 25, 1997 · N921R · Doug DC863F · Fuselage Main, Frame
  > DURING C-CHECK INSPECTION, FOUND FS 1020 FRAME HAS CORROSION ON UPPER FWD FLANGE ABOVE LONGERON 33 AND 34 LT.
- [SDR RRXA97246](https://openairdocs.org/sdr/RRXA97246.md): Skin · cracked · Aug 25, 1997 · N921R · Doug DC863F · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND LT WING CENTER OF LEADING EDGE CRACKED AT SCREW HOLE (LOWER SURFACE) STA XFS 520. *S/D* REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, IAW FAA DER APPROVED ENGINEERING SKETCH D02-R12, AND TREATED AR

Next page: https://openairdocs.org/deregistered/N921R-2011-02-16/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 = 'N921R' AND deregistration_id = 'N921R-2011-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N921R-2011-02-16/reports

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