# Service difficulty reports: N851UP, cancelled Mar 8, 2011

A list on [N851UP, cancelled Mar 8, 2011](https://openairdocs.org/deregistered/N851UP-2011-03-08.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 5 · 231 reports

- [SDR UPS08852590](https://openairdocs.org/sdr/UPS08852590.md): Light · inoperative · Jun 26, 2008 · N851UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A ON EMERGENCY LIGHT TEST STANDBY ATTITUDE INDICATOR (SAI) AND STANDBY ALTIMETER INSTRUMENT LIGHTS INOP. EMERGENCY LIGHTING SYS CHECKS OK M/M 33-50-01-2-2.
- [SDR UPS08852167](https://openairdocs.org/sdr/UPS08852167.md): Slide · inoperative · May 2, 2008 · N851UP · Doug DC873F · Escape Slide
  > WITH MAIN DOOR SHUT AND SLIDE ARMED, DOOR WAS OPENED AND SAFETY WIRE REMOVED FROM SLIDE HOUSING. REMOVED AND REINSTALLED MAIN CABIN DOOR ESCAPE SLIDE IAW AMM 25-60-01-2. INSTALLATION CHECK WAS GOOD.
- [SDR UPS08851879](https://openairdocs.org/sdr/UPS08851879.md): Skin · punctured · Mar 14, 2008 · N851UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:N/A RIGHT WING O/B FLAP UPPER SKIN HAS PUNCTURE DAMAGE 2 INCHES I/B OF CUTOUT (ACTUATOR) AND 18 INCHES AFT OF LEADING EDGE. DAMAGE MEASURES.375" X.250". ACCOMPLISHED REPAIR PER DC8 SRM 57-02-01-0 FIG 002Q. CLASS B REPAIR. RAN FLAPS, NO INT
- [SDR UPS08851694](https://openairdocs.org/sdr/UPS08851694.md): Skin · dented · Feb 19, 2008 · N851UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A DENT APPROX 12 INCHES ABOVE MAIN STATIC PORT ON RT SIDE OF A/C. INSPECTED PER EO DC8-5330-28630-A. NO FURTHER DEFECTS NOTED. A 30 DAYS PERM REPAIR ACCOMPLISHED HFEC OF AREA PER DC8 SPM 06-10-01-001, NO CRACKS DETECTED. OK FOR SERVICE.
- [SDR UPS09854453](https://openairdocs.org/sdr/UPS09854453.md): Slide · out of position · Jan 28, 2008 · N851UP · Doug DC873F · Emergency Equipment
  > INSPECTION TYPE:N/A ESCAPE SLIDE FELL OUT OF HOLDER. DEFERRED SLIDE PER MEL M393690 ASSIGNED. INSTALLED EVACUATION SLIDE IAW M/M 25 60 01 2. THIS CLEARS M393690.
- [SDR UPS07851089](https://openairdocs.org/sdr/UPS07851089.md): Battery Pack · inoperative · Nov 2, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK IAW MM 33-50-01-2.
- [SDR UPS07850636](https://openairdocs.org/sdr/UPS07850636.md): Battery Pack · discharged · Sep 10, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01-2. OPS CHECKS NORMAL.
- [SDR UPS07850621](https://openairdocs.org/sdr/UPS07850621.md): Slide · out of position · Sep 5, 2007 · N851UP · Doug DC873F · Escape Slide
  > ESCAPE SLIDE ON CAPTAIN'S SIDE FELL OUT. 10-8-07 REINSTALLED CAPTAIN'S ESCAPE TAPE (ROPE) AND LINING IAW DC8 MM 25-61-13-04.
- [SDR UPS07850471](https://openairdocs.org/sdr/UPS07850471.md): Fitting · cracked · Aug 15, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 CRACKED END FITTING AT STA 1240 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1240 L35R IAW SRM 51-1-20D AND SRM 51-3-2.
- [SDR UPS07850472](https://openairdocs.org/sdr/UPS07850472.md): Web · cracked · Aug 1, 2007 · N851UP · Doug DC873F · Rudder Miscellaneous Structure
  > INSPECTION TYPE:C2 RUDDER HAS 1.5 INCH CRACK IN LWR STRUCTURE JUST AFT OF TORQUE TUBE MOUNTING. REMOVED CRACKED WEB ON RUDDER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR WEB ON RUDDER STA ZR 59.54 IAW SRM 51-03-00-0, AND DWG 5701251.
- [SDR UPS07850574](https://openairdocs.org/sdr/UPS07850574.md): Frame · corroded · Jul 31, 2007 · N851UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C2 HEAVY CORROSION ON LWR FLANGE OF FRAME AT STA 1240 L35R. CUT OUT CORRODED AREA OF LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995. REPAIRED LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995, UPS RAA DC8-53-20650
- [SDR UPS07850552](https://openairdocs.org/sdr/UPS07850552.md): Longeron · corroded · Jul 26, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 L-35R CORRODED FROM STA 1220-1260 ON INBD LONGERON. REMOVED AND REPLACED LONGERON AND BATHTUB FITTINGS FROM STA 1210 TO 12 0 IAW SRM 53-2-0 AND DWG 5750322.
- [SDR UPS07850444](https://openairdocs.org/sdr/UPS07850444.md): Fitting · cracked · Jul 25, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 L-31R END FITTING CRACKED AT STA 1690. REMOVED AND REPLACED LONGERON END FITTING AT STA 1690 L31R IAW SRM 51-1-21, AND SRM 51-3-0.
- [SDR UPS07850337](https://openairdocs.org/sdr/UPS07850337.md): Web · punctured · Jul 25, 2007 · N851UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C2 WEB PUNCTURED AT STA 70 L21L. CUT OUT DAMAGED AREA ON WEB AT STA 70 L21L IAW SRM 53-02-00-0 FIG1F FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 70 L21L IAW SRM 53-03 -03-0.
- [SDR UPS07850613](https://openairdocs.org/sdr/UPS07850613.md): Skin · corroded · Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 C-PIT STA 1240-1260 BETWEEN L36 AND L34R INTERNAL DOUBLER HAS CORROSION AND EXTENDS UNDER L35R. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 1242 L35R IAW SAA EA 008-5330-01-A0985, UPS RAA DC8-53-20644, AD FAA FORM 8100-9.
- [SDR UPS07850474](https://openairdocs.org/sdr/UPS07850474.md): Splice · cracked · Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 L36 SPLICE BETWEEN STA 1260 AND 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SAA EA 008-5310-01-A0987.
- [SDR UPS07850372](https://openairdocs.org/sdr/UPS07850372.md): Skin · canning · Jul 24, 2007 · N851UP · Doug DC873F · Elevator, Plate/Skin
  > INSPECTION TYPE:C2 LEFT ELEVATOR UPPER SKIN INBOARD OIL CANNED. REMOVED, FABRICATED, AND INSTALLED ELEVATOR SKIN IAW SRM 51-1-21, 55-0 2-01, 51-1-8 AND 51-1-21A.
- [SDR UPS07850371](https://openairdocs.org/sdr/UPS07850371.md): Floorbeam · corroded · Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 24 CRACKED AND CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 5 3-2-0, 51-02-00 FIG 1, 51-1-8, 51-1-20D, AND DWG 2759472.
- [SDR UPS07850394](https://openairdocs.org/sdr/UPS07850394.md): Floorbeam · gouged · Jul 23, 2007 · N851UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C2 A-PIT STA 120 LBL 26 FLOORBEAM GOUGED AND FASTENER SHEARED. CUT OUT DAMAGED AREA ON FLOORBEAM AT STA 120 LBL 26 IAW SRM 51-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AT STA 120 LBL 26 IAW SRM 51-02-00 FIG 1, AND SRM 53-02-00 FIG 1F.
- [SDR UPS07850338](https://openairdocs.org/sdr/UPS07850338.md): Angle · cracked · Jul 23, 2007 · N851UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C2 C-PIT FWD BULKHEAD STA 986 LBL 46, ANGLE CRACKED. STOP DRILLED CRACKED ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0 FIG 001B. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0, AND DWG 5704721
- [SDR UPS07850443](https://openairdocs.org/sdr/UPS07850443.md): Attach Angle · cracked · Jul 22, 2007 · N851UP · Doug DC873F · Vertical Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C2 LEFT SIDE OF VERT STAB LWR ATTACH ANGLE CRACKED AT STA 1766. REPAIRED LEFT SIDE OF VERT STAB LWR ATTACH ANGLE AT STA 1766 IAW SRM 53-02-05-0 FIG 016A.
- [SDR UPS07850407](https://openairdocs.org/sdr/UPS07850407.md): Angle · cracked · Jul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C2 LT HORIZ STAB UPPER MOVEABLE FAIRING MOST AFT H-ANGLE CRACKED. REMOVED AND REPLACED LT HORIZ STAB MOVEABLE FAIRING AFT H-ANGLE IAW SRM 51-03-00-0, DWG 3702464, AND SRM 51-03-02.
- [SDR UPS07850396](https://openairdocs.org/sdr/UPS07850396.md): Angle · cracked · Jul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C2 RT HORIZ STAB MOVEABLE FAIRING 2ND AFT H-ANGLE UPPER, CRACKED. REMOVED CRACKED H-ANGLE ON RT HORIZ STAB MOVEABLE FAIRING IAW SRM 51-03-00-0. FABRICATED AND INSTALLED RT HORIZ STAB FAIRING ATTACH H-ANGLE IAW SRM 51-03-02, DWG 3702464, AND S
- [SDR UPS07850393](https://openairdocs.org/sdr/UPS07850393.md): Angle · cracked · Jul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C2 RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE CRACKED. REMOVED AND REPLACED RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE IAW SRM 51-3-0, 51-1-20D, SRM 51-3-2, AND DC8 AMM 55-10-00-2.
- [SDR UPS07850388](https://openairdocs.org/sdr/UPS07850388.md): Frame · cracked · Jul 20, 2007 · N851UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C2 STA 70 FRAME CRACKED AND CORRODED BETWEEN L31R AND L32R IN A/C COMPT. REPAIRED CRACKED AND CORRODED FRAME AT STA 70 BETWEEN L31R AND L32R IN A/C BAY IAW SRM 53-02-05 FIG 08C2.
- [SDR UPS07850397](https://openairdocs.org/sdr/UPS07850397.md): Skin · cracked · Jul 18, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 FUSE SKIN CRACKED AND BULGING AT STA 1692 L28R. REPAIRED FUSELAGE EXTERIOR SKIN AT STA 1692 L28R IAW UPS EO DC8- 5330-20248-D APPX E AND SRM SRO8530032.
- [SDR UPS07850395](https://openairdocs.org/sdr/UPS07850395.md): Skin · damaged · Jul 18, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 CREASE ON UPPER FUSE SKIN AT STA 1800 L9L. CUT OUT DAMAGED AREA ON FUSE SKIN AT STA 1800 L9L IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER AT STA 1800 L9L IAW SRM 53-2-1 FIG 7, AND SRM 53-5-3 FIG 1 SHEET 1.
- [SDR UPS07850345](https://openairdocs.org/sdr/UPS07850345.md): Doubler · punctured · Jul 18, 2007 · N851UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:C2 LEFT WING INBOARD FLAP STA 110 UPPER SURFACE SKIN DENT AND EXISTING DOUBLER PUNCTURED. REMOVED DAMAGED DOUBLER ON LEFT WING INBOARD FLAP STA 110 UPPER SURFACE IAW SRM 51-01-21-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT WING UPPER S
- [SDR UPS07850339](https://openairdocs.org/sdr/UPS07850339.md): Skin · gouged · Jul 18, 2007 · N851UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C2 LH INBD UPPER SURFACE SKIN EXSISTING REPAIR DOUBLER HAS DEEP GOUGE AT STA 100 REMOVED DAMAGED DOUBLER AT L/WING STA 100 IAW SRM 51-01-21-0 FABRICATED AND INSTALLED REPAIR DOUBLER AT LH WING INBD UPPER SURFACE STA 100 IAW SRM 57-07-01-0 A
- [SDR UPS07849587](https://openairdocs.org/sdr/UPS07849587.md): Battery Pack · inoperative · Apr 1, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A FWD PASSAGEWAY AND EMERGENCY LIGHT NEXT TO EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED PASSAGEWAY AND EMERGENCY LIGHT. LIGHT OPS GOOD.
- [SDR UPS07849542](https://openairdocs.org/sdr/UPS07849542.md): Light · malfunctioned · Mar 22, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > AFTER TAKEOFF, EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH EXCEPT TO DISARM EMERGENCY LIGHTS. FOUND C/B PULLED. RESET C/B AND PERFORMED EMERGENCY LIGHTS. OPS CHECK PER MM 33-50-01-2. EMERGENCY LIGHTS, OPS CHECK GOOD.
- [SDR UPS07848982](https://openairdocs.org/sdr/UPS07848982.md): Battery Pack · discharged · Jan 24, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A DURING PDC, EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 AMM 33-50-01-2. CHECK SERVICEABLE.
- [SDR UPS07848831](https://openairdocs.org/sdr/UPS07848831.md): Battery Pack · inoperative · Jan 5, 2007 · N851UP · Doug DC873F · Emergency Lighting
  > COURIER EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD 33-31-01-2.
- [SDR UPS06848360](https://openairdocs.org/sdr/UPS06848360.md): Fan · odor · Oct 28, 2006 · N851UP · Doug DC873F · Air Distribution Fan
  > RECIRC FAN VERY LOUD (NOISY) WITH A SLIGHT ODOR. REMOVED AND REPLACED RECIRC FAN PER MM 21-21-01-2. OPS CKS NORMAL.
- [SDR UPS06848092](https://openairdocs.org/sdr/UPS06848092.md): Battery Pack · discharged · Sep 28, 2006 · N851UP · Doug DC871F · Emergency Lighting
  > FOUND EMERGENCY LIGHT BATTERY PACK DEAD ON PRE-FLIGHT. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND SYSTEM CHECK SERVICEABLE.
- [SDR UPS06847743](https://openairdocs.org/sdr/UPS06847743.md): Battery Pack · inoperative · Aug 21, 2006 · N851UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER AMM 33-50-01-2. OPS CHECK GOOD.
- [SDR UPS05845881](https://openairdocs.org/sdr/UPS05845881.md): Battery Pack · inoperative · Dec 12, 2005 · N851UP · Doug DC873F · Emergency Lighting
  > EMERGENCY BATTERY PACK NEEDS REPLACING. REPLACED BAT PACK EMERGENCY LIGHT. OPS NORMAL. OK TO CONTINUE.
- [SDR UPS05845849](https://openairdocs.org/sdr/UPS05845849.md): Wire · open · Nov 30, 2005 · N851UP · Doug DC873F · Landing Gear System Wiring
  > N/A RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE DURING LANDING. GEAR WAS DOWN. T/S. FOUND WIRE FROM RT GEAR SWITCH TO TERMINAL BLOCK OPEN. REMOVED AND REPLACED WIRE IAW SWP 20-00-00. OPS CK IAW AMM 32-60-00-2 (E) STEPS 1 TO 6. OPS CK OK ALL 3 GREEN OK.
- [SDR UPS05845615](https://openairdocs.org/sdr/UPS05845615.md): Windshield · cracked · Oct 14, 2005 · N851UP · Doug DC873F · Flight Compartment Windows
  > INSPECTION TYPE:N/A, F/O'S WINDSHIELD TOP EDGE GLOWING. WINDSHIELD CRACKED AT 17K FT. REMOVED AND REPLACED F/O WINDSHIELD W/REF TO MM 56-10-02-2.
- [SDR UPS05844985](https://openairdocs.org/sdr/UPS05844985.md): Floorbeam · corroded · Jul 10, 2005 · N851UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C1, CORROSION ON FLOORBEAM AT STA 60 RBL 45. REMOVED DAMAGE ON UPPER TEE CAP OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW SAA SK 851-857217.
- [SDR UPS05845052](https://openairdocs.org/sdr/UPS05845052.md): Intercostal · corroded · Jul 6, 2005 · N851UP · Doug DC873F · Fuselage Miscellaneous Structure
  > STA 70 RBL 48 UNDER THE SEAT TRACK INTERCOSTAL HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-20D, 51-3-2 AND DWG 5890314.
- [SDR UPS05844981](https://openairdocs.org/sdr/UPS05844981.md): Skin · cracked · Jul 2, 2005 · N851UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C1 RH WING UPPER AFT SKIN PANEL AT XCW 69.500 CRACKED 1 INCH LONG. CUT OUT DAMAGE,FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-02-01 FIG. 20.
- [SDR UPS05844984](https://openairdocs.org/sdr/UPS05844984.md): Finger Doubler · corroded · Jul 1, 2005 · N851UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C1, COCKPIT SUBFLOOR AT STA -32 TO -52 RBL 60 FINGER DOUBLER CORRODED. REMOVED FINGER DOUBLER, CORROSION FOUND OUT OF LIMITS, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5612298 AND DC-8 SRM 51- 1-20D AND 51-1-15.
- [SDR UPS05844983](https://openairdocs.org/sdr/UPS05844983.md): Finger Doubler · corroded · Jul 1, 2005 · N851UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C1, COCKPIT SUBFLOOR STA -32 TO -12 RBL 48 FINGER DOUBLER HAS SEVERAL SHEA R HEAD FASTENERS AND POSSIBLE CORROSION. REMOVED FINGER DOUBLER, CORROSION ON FINGER DOUBLER FOUND OUT OF LIMIT S, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUB
- [SDR UPS05845059](https://openairdocs.org/sdr/UPS05845059.md): Spar Cap · cracked · Jun 30, 2005 · N851UP · Doug DC873F · Wing Spar
  > LT AFT LWR WING SPAR CAP F/S 857 IS CRACKED IN THREE PLACES FROM LBL27-LBL45. REPAIRED LT LWR SPAR CAP IAW SRO DWG 8570009, SRM 51-1-20D, 51-1-24.
- [SDR UPS05844930](https://openairdocs.org/sdr/UPS05844930.md): Fitting · cracked · Jun 30, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, CRACKED FITTING APPROX 2 INCHES ON LONGERON 32R STA 1200 C-PIT ENTRY WAY. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844929](https://openairdocs.org/sdr/UPS05844929.md): Longeron · cracked · Jun 30, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C1, STA 1756 L4R CRACKED.250 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.
- [SDR UPS05844980](https://openairdocs.org/sdr/UPS05844980.md): Fitting · cracked · Jun 29, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, MAIN CARGO STA 860 LONGERON 19R FITTING CRACKED APPROX. 2 INCHES ON FWD SIDE OF FRAME. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844931](https://openairdocs.org/sdr/UPS05844931.md): Skin · cracked · Jun 29, 2005 · N851UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:C1 C-PIT DOOR LOWER AFT CORNER REPAIR DOUBLER IS NOT PER SRM 53-2-0 FIG 22 AND THERE IS A CRACK IN THE REPAIR FILLER. REMOVED EXISTING REPAIR, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 22.
- [SDR UPS05845056](https://openairdocs.org/sdr/UPS05845056.md): Spar · cracked · Jun 28, 2005 · N851UP · Doug DC873F · Wing Spar
  > FS 855 AFT SIDE OF REAR SPAR LOWER CHORD UPPER SURFACE FROM RBL36.5 -45.00 HAS 8.5" CRACK. REPAIRED REAR SPAR IAW SRO 8570009.

Next page: https://openairdocs.org/deregistered/N851UP-2011-03-08/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 = 'N851UP' AND deregistration_id = 'N851UP-2011-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N851UP-2011-03-08/reports

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