# Service difficulty reports: N961R, cancelled Jul 5, 2002

A list on [N961R, cancelled Jul 5, 2002](https://openairdocs.org/deregistered/N961R-2002-07-05.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 7 · 331 reports

- [SDR 2003F00055](https://openairdocs.org/sdr/2003F00055.md): Floorbeam · corroded · Jun 17, 2002 · N961R · Doug DC873F · Fuselage Main, Floor Beam
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, AT STATION 1600 LBL 42 INCH FLOORBEAM UPPER FLANGE LOWER SURFACE HAS 1 INCH BY 2 INCH CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER, FILLER IAW EO NR 02-039. TREATED, PRIMED
- [SDR 2002F01102](https://openairdocs.org/sdr/2002F01102.md): Web · cracked · Jun 11, 2002 · N961R · Doug DC873F · Trailing Edge Flaps
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT INBOARD FLAP INBOARD WEB HAS PREVIOUS REPAIR CRACK EXTENDS TO NEW STOP DRILL AT END OF CRACK BEYOND REPAIR DOUBLER. STOP DRILLED END OF CRACK IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-0, FIG 2.
- [SDR 2002F01101](https://openairdocs.org/sdr/2002F01101.md): Spar Cap · cracked · Jun 11, 2002 · N961R · Doug DC873F · Wing Spar
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT WING LOWER FRONT SPAR CAP FORWARD TANG APPROXIMATELY STATION 520 SPAR CAP HAS CRACK. REMOVED INTERNAL REPAIR ANGLE FOR EVALUATION IAW DC-8 SRM 51-1-20D. REPAIR IS ACCEPTABLE AS TEMP REPAIR PER BOEING LETTER TEK-
- [SDR 2002F01100](https://openairdocs.org/sdr/2002F01100.md): Longeron · cracked · Jun 11, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 55 LEFT LONGERON 31 HAS NO SUPPORTING DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. CRACK HAD EXTENDED.5 BEYOND STOP DRILL. STOP DRILLED CRACK IAW DC-8 SRM 53-2-0. FABRICATED REPAIR DOUBLER
- [SDR 2002FA0000724](https://openairdocs.org/sdr/2002FA0000724.md): Longeron · damaged · Jun 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (LONGERON 24/ FITTING) FOUND DURING (D) CHECK INSPECTION, STA 960 AND LONGERON 24L HOLES ELONGATED IN FITTING AND LONGERON 24 TWO FORWARD.
- [SDR 2002FA0000723](https://openairdocs.org/sdr/2002FA0000723.md): Panel · corroded · Jun 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > (BULKHEAD PANELS) FOUND DURING (D) CHECK INSPECTION. RIGHT W/W STA. 980 CNAT BULKHEAD PANELS HAVE CORROSION SPOTS FROM LONG 24R TO LONGERON 25R.
- [SDR 2002F01098](https://openairdocs.org/sdr/2002F01098.md): Fitting · corroded · Jun 7, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT LONGERON AND BATHTUB FITTING STATION 960 AFT SIDE HAS SPOT OF SURFACE CORROSION. REMOVED CORROSION FROM LONGERON 24R AND BATHTUB FITTING IAW DC-8 SRM 51-1-8. LONGERON 24 REPAIRED. REMOVED AND REPLACED BATHTUB F
- [SDR 2002F01104](https://openairdocs.org/sdr/2002F01104.md): Skin · damaged · Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/Skin
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 275 RIGHT 31 AND 32 HAS NO SUPPORTING DOCUMENTATION. REMOVED REPAIR IAW DC-8 SRM 51-1-20D. FABRICATED FILLER, DOUBLER. TREATED AND PRIMED AND INSTALLED REPAIR PER EO NR 02-039, WITH APPROVED 8110-3
- [SDR 2002F01103](https://openairdocs.org/sdr/2002F01103.md): Longeron · cracked · Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 300 RIGHT LONGERON 33 HAS NO SUPPORT DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. IT IS ACCEPTABLE TO USE EXISTING FILLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED ALL PARTS AND INSTALLED
- [SDR 2002F01105](https://openairdocs.org/sdr/2002F01105.md): Frame · corroded · Jun 4, 2002 · N961R · Doug DC873F · Fuselage Main, Frame
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, STATION 460 HAS CORROSION ON FRAME BETWEEN STRINGERS 2/3 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 53-2-0 AND 53-2-0, FIG 1F.
- [SDR 2002F01095](https://openairdocs.org/sdr/2002F01095.md): Fitting · corroded · Jun 3, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, LONGERON 24L SURFACE CORROSION ON BOTH SIDES OF BATHTUB FITTING STATION 940 AT LONGERON ATTACH. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING STATION 940 IAW DC-8 SRM 51-1-24, 51-3-0.
- [SDR 2002F01094](https://openairdocs.org/sdr/2002F01094.md): Skin · corroded · Jun 3, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/Skin
  > FOUND DURING DOUGLAS D-CHECK INSPECTION, LIGHT SURFACE CORROSION ON LOWER CENTER FUSELAGE AREA BETWEEN CENTER WING STRINGERS 67 AND 68 5 INCHES RIGHT OF ECWO. CORROSION OUT OF LIMITS STATION 759-768, 6 INCHES RIGHT OF CENTER LINE, ITEM 4 ON FORM 84. REMOVED
- [SDR 2002FA0000720](https://openairdocs.org/sdr/2002FA0000720.md): Longeron · corroded · Jun 2, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (LONGERON/BATHTUB FITTING) FOUND DURING (D) CHECK INSPECTION, LEFT LONGERON, LEFT LONGERON, 24 STA. 960.
- [SDR 2002FA0000725](https://openairdocs.org/sdr/2002FA0000725.md): Longeron · corroded · May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (LONGERON) FOUND DURING (D) CHECK INSPECTION, STA960 AND LONGERON 24L AFTER FITTING REMOVAL, FOUND CORROSION ON LONGERON 24 AT FASTENER HOLES.
- [SDR 2002FA0000722](https://openairdocs.org/sdr/2002FA0000722.md): Web · corroded · May 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > (WEB SKIN) FOUND DURING (D) CHECK INSPECTION, RIGHT W/W STA. 980 CNAT BULKHEAD WEB SKIN AND ANGLES HAS SURFACE CORROSION FROM LONGERON 24 TO LONGERON 27R.
- [SDR 2002FA0000721](https://openairdocs.org/sdr/2002FA0000721.md): Longeron · corroded · May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (LONGERON 24) FOUND DURING (D) CHECK INSPECTION, LEFT WHEEL WELL STA. 902 FITTING AND LONGERON 24 CORROSION EMINATING FROM BETWEEN FITTING AND LONGERON LOWER SURFACE.
- [SDR 2002FA0000726](https://openairdocs.org/sdr/2002FA0000726.md): Floorbeam · corroded · May 6, 2002 · N961R · Doug DC873F · Fuselage Main, Floor Beam
  > (FLOORBEAM) FOUND DURING (D) CHECK INSPECTION. CORROSION AT STA 920. 63 INCHES LEFT OF CENTER, FLOORBEAM.
- [SDR 2002FA0000719](https://openairdocs.org/sdr/2002FA0000719.md): Stringer · corroded · May 3, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (STRINGER) FOUND DURING (D) CHECK INSPECTION, STRINGER 31R HAS CORROSION AT STA 680.
- [SDR RRXA010060](https://openairdocs.org/sdr/RRXA010060.md): Gyro · failed · Aug 9, 2001 · N961R · Doug DC873F · Attitude Gyro and Indicating System
  > CAPT'S VG FAILURE AFTER TAKEOFF. R&R CAPT'S VG IAW DC8 MM 34-25-0. OPS CHECKS GOOD.REMOVED & REPLACED CAPTS. ADI SYSTEM CHECKS GOOD IAW DC-8 MM 34-25-0 NO DEFECTS NOTED
- [SDR RRXA010009](https://openairdocs.org/sdr/RRXA010009.md): Light · malfunctioned · Feb 11, 2001 · N961R · Doug DC873F · Engine Oil Pressure
  > NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 3900 FEET, M.8 249 KIAS OIL PRESS 42, PSI IDLE 32 PSI. LIGHT REMAINED ILLUMINATED AS POWER REDUCED FROM CRUISE TO IDLE POWER. INFLIGHT SHUTDOWN PERFORMED IAW QRH. AFTER SHUTDOWN OIL PRESSURE LIGHT REMAINE
- [SDR RRXA001077](https://openairdocs.org/sdr/RRXA001077.md): Flow Valve · failed · Oct 27, 2000 · N961R · Doug DC873F · Cabin Cooling System
  > ON CLIMBOUT WITH RT PACK AT MAX FLOW COULD NOT MAINTAIN CABIN ALTITUDE BELOW 10,000 FT. RETURNED TO AIRPORT. REMOVED AND REPLACED FLOW CONTROL VALVE. RAN ENGS AND PRESSURIZED IAW 21-31-0, OPS CHECK GOOD.
- [SDR RRXA003427](https://openairdocs.org/sdr/RRXA003427.md): Frame · corroded · Sep 2, 2000 · N961R · Doug DC873F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE 'B' PIT DOOR FRAME AT STA 520 AND L30R TO L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW E.O. L40-R01.
- [SDR RRXA001052](https://openairdocs.org/sdr/RRXA001052.md): Structure · corroded · Aug 31, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > HEAVY CORROSION AT FRAME STA 520 BETWEEN LONGERONS 30R & 29 R,CARGO LIGHT SWITCH AREA. REPAIRED STA 250, L30R AND L29R, FRAME REF: ENG DRAWING NR L40-R01. MAT USED 7075-0,.090. HEAT TREATED REF DC-8 SRM 51-1-1.
- [SDR RRXA003730](https://openairdocs.org/sdr/RRXA003730.md): Panel · corroded · Jul 3, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT AFT LOWER STAB WIPER PANEL AT STA 1723-1849, L15R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4,
- [SDR RRXA001002](https://openairdocs.org/sdr/RRXA001002.md): Structure · cracked · Jun 20, 2000 · N961R · Doug DC873F · Landing Gear Doors
  > LT GEAR DOOR CRACKED IN TWO PLACES (MAIN LANDING). PERFORMED PLATING REPAIR IAW DC-8 SRM CHAP 52-2-0 FIG 2.
- [SDR RRXA000296](https://openairdocs.org/sdr/RRXA000296.md): Harness · corroded · May 14, 2000 · N961R · Doug DC873F · Engine EGT/TIT Indicating System
  > NR 1 ENGINE INFLIGHT SHUT DOWN DUE TO ERRATIC -OFF SCALE EGT INDICATION FOR BOTH ANALOG AND DIGITAL EGT READOUT. TESTED NR 1 EGT SYSTEM IAW M/M 77-20-4, FOUND ALL TO BE WITHIN LIMITS. USED WHEATSTONE BRIDGE (TT1000A) TEST BOX TO VERIFY EGT GAUGE AND EGT HARN
- [SDR RRXA002020](https://openairdocs.org/sdr/RRXA002020.md): Retainer · inadequate · Apr 27, 2000 · N961R · Doug DC873F · Engine Mount Section
  > DURING A MAINTENANCE VISIT FOUND ALL 4 AFT MOUNT BOLT RETAINERS ARE TOO SHORT AND DO NOT FIT OVER BOLT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BOLTS IAW DC-8 SRM 51-3-0,
- [SDR RRXA001886](https://openairdocs.org/sdr/RRXA001886.md): Retainer · wrong part · Apr 27, 2000 · N961R · Doug DC873F · Engine Mount Section
  > DURING A MAINTENANCE VISIT FOUND THE AFT MOUNT BOLT RETAINERS ARE TOO SHORT (DO NOT FIT OVER BOLT), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MOUNT BOLT IAW DC-8 SRM 51-3-0, 72-22
- [SDR RRXA002026](https://openairdocs.org/sdr/RRXA002026.md): Doubler · cracked · Apr 25, 2000 · N961R · Doug DC873F · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE EXISTING DOUBLER AT BOTTOM OF A-PIT DOOR EXTERNAL SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-055 WITH APPROVED 8
- [SDR RRXA001892](https://openairdocs.org/sdr/RRXA001892.md): Doubler · cracked · Apr 25, 2000 · N961R · Doug DC873F · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE EXISTING DOUBLER ON THE BOTTOM OF A-PIT DOOR EXTERNAL SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED DOUBLER IAW EO NR 00-055
- [SDR RRXA001910](https://openairdocs.org/sdr/RRXA001910.md): Panel · cracked · Apr 20, 2000 · N961R · Doug DC873F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK ON THE RT WING I/B SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PANEL IAW DC-8 SRM 51-3-0 AND MM 27-80-1.
- [SDR RRXA001774](https://openairdocs.org/sdr/RRXA001774.md): Panel · cracked · Apr 20, 2000 · N961R · Doug DC873F · Nacelle/Pylon Structure
  > DURING A MAINTENANCE VISIT, FOUND A 2 1/2 INCH CRACK ON THE RT WING IB SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1.
- [SDR RRXA001948](https://openairdocs.org/sdr/RRXA001948.md): Boss · corroded · Apr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Attach Section
  > DURING A MAINTENANCE VISIT FOUND THE MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEEDED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-05
- [SDR RRXA001813](https://openairdocs.org/sdr/RRXA001813.md): Strut · corroded · Apr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Strut/Axle/Truck
  > DURING A MAINTENANCE VISIT MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED, REWORKED AND INSTALLED RETRACT PIN IAW EWA MA-AI
- [SDR RRXA001947](https://openairdocs.org/sdr/RRXA001947.md): Outflow Valve · corroded · Apr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow Valve
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RETANGULAR OUTFLOW VALVE (SUGAR SCOOP) IN THE AFT ACCESSORY COMPT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR I
- [SDR RRXA001946](https://openairdocs.org/sdr/RRXA001946.md): Web · corroded · Apr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN THE LWR PIT C ON WEB AT STA 1200 BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 53-
- [SDR RRXA001945](https://openairdocs.org/sdr/RRXA001945.md): Web · corroded · Apr 14, 2000 · N961R · Doug DC873F · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED
- [SDR RRXA001812](https://openairdocs.org/sdr/RRXA001812.md): Outflow Valve · corroded · Apr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow Valve
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT ACCESSORY COMPT RETANGULAR OUTFLOW VALVE BETWEEN STA 1670 TO 1690, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND BLENDED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVI
- [SDR RRXA001811](https://openairdocs.org/sdr/RRXA001811.md): Web · corroded · Apr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN LWR PIT C ON WEB AT STA 1200 AND BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RETURNED TO SERVICE IAW
- [SDR RRXA001810](https://openairdocs.org/sdr/RRXA001810.md): Web · corroded · Apr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RET
- [SDR RRXA002135](https://openairdocs.org/sdr/RRXA002135.md): Intercostal · misdrilled · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL IN THE UPPER CARGO COMPT. AT FS 798 TO 822 AND L5L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1
- [SDR RRXA002040](https://openairdocs.org/sdr/RRXA002040.md): Angle · corroded · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "L" ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D.
- [SDR RRXA002019](https://openairdocs.org/sdr/RRXA002019.md): Frame · cracked · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE C PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW
- [SDR RRXA001944](https://openairdocs.org/sdr/RRXA001944.md): Angle · corroded · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D AND 53-2-0. (
- [SDR RRXA001914](https://openairdocs.org/sdr/RRXA001914.md): Spar Cap · damaged · Apr 13, 2000 · N961R · Doug DC873F · Wing Spar
  > DURING A MAINTENANCE VISIT FOUND GOUGED HOLES AND ELONGATED UPPER SPAR CAP ON RT WING FRONT SPAR AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 EO NR 00-055 W
- [SDR RRXA001885](https://openairdocs.org/sdr/RRXA001885.md): Frame · cracked · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A CRACK AT THE C'' PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED AN
- [SDR RRXA001809](https://openairdocs.org/sdr/RRXA001809.md): Angle · corroded · Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-20D AND 53-2-0.
- [SDR RRXA001778](https://openairdocs.org/sdr/RRXA001778.md): Spar Cap · damaged · Apr 13, 2000 · N961R · Doug DC873F · Wing Spar
  > DURING A MAINTENANCE VISIT, FOUND GOUGED AND ELONGATED HOLES IN THE RT WING UPPER SPAR CAP AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES & RE-COUNTER SUNK AND INSTALL
- [SDR RRXA001921](https://openairdocs.org/sdr/RRXA001921.md): Skin · cracked · Apr 12, 2000 · N961R · Doug DC873F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DENTED AND CRACKED THE LEFT O/B STUB WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW EO NR 00-055 WITH APPROVED 8110-3 DATED 3-
- [SDR RRXA001902](https://openairdocs.org/sdr/RRXA001902.md): Panel · delaminated · Apr 12, 2000 · N961R · Doug DC873F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, RIVETS PULLING THROUGH AND RIVET HEADS SHEARING OFF ON THE RT FLAP SCISSORS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL

Next page: https://openairdocs.org/deregistered/N961R-2002-07-05/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 = 'N961R' AND deregistration_id = 'N961R-2002-07-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N961R-2002-07-05/reports

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