# Service difficulty reports: N706UP, cancelled Mar 30, 2010

A list on [N706UP, cancelled Mar 30, 2010](https://openairdocs.org/deregistered/N706UP-2010-03-30.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 4 · 179 reports

- [SDR UPS06848022](https://openairdocs.org/sdr/UPS06848022.md): Slide · inoperative · Sep 21, 2006 · N706UP · Doug DC871F · Escape Slide
  > MAIN CABIN EXIT SLIDE/SLIDE INOP, LOW PRESSURE. REMOVED AND REPLACED SLIDE ASSY PER 25-60-01-2. CLEARED, PLACARD REMOVED AND BOTH COURIER SEATS REACTIVATED.
- [SDR UPS06846679](https://openairdocs.org/sdr/UPS06846679.md): Door Frame · cracked · Mar 29, 2006 · N706UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A CRACK APPROX.125" ON THE L-2 DOOR UPPER FWD DOOR JAMB CORNER EXTENDING FROM FASTENER. CUT OUT DAMAGE AT L-2 DOOR UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 18. FABRICATED AND INSTALLED FILLER, DOUBLER,
- [SDR UPS06846711](https://openairdocs.org/sdr/UPS06846711.md): Fairing · corroded · Mar 24, 2006 · N706UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 LT STA 98 CANOE CORRODED UNDER BOTH FLAP TRACKS. REMOVED LT STA 98 FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION BY MACHINING IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 LT IAW DC8- MM
- [SDR UPS06846718](https://openairdocs.org/sdr/UPS06846718.md): Stringer Clip · cracked · Mar 23, 2006 · N706UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 CRACKED STRINGER CLIP ON OTBD SKATE ANGLE C/S-STRINGER 62 NR 4 MAIN TANK. REMOVED CRACKED CLIP AT OTBD SKATE ANGLE C/S STRINGER 62 NR 4 MAIN TANK IAW SRM 51-01-20D. FABRICATED AND INSTALLED CLIP ON O/B SKATE ANGLE C/S STRINGER 62 34 MAIN T
- [SDR UPS06846598](https://openairdocs.org/sdr/UPS06846598.md): Longeron · cracked · Mar 23, 2006 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON SPLICE L36 STA 1260-1280 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1260-1280 L36 IAW SRM 51-1-20D, AND 51-1-8.
- [SDR UPS06846719](https://openairdocs.org/sdr/UPS06846719.md): Fitting · cracked · Mar 21, 2006 · N706UP · Doug DC871F · Wing, Attach Fittings
  > INSPECTION TYPE:C3 STA 98 FLAP ACTUATOR REAR SPAR FITTING O/B LUG FOR SUPPORT LINK ARM IS BROKEN. FABRICATED AND INSTALLED NEW FITTING FROM 7050-T7451 PER AMS 4050 PLATE IAW UPS ENG FILE # DC8-57-20160, SAA EA#008-2760-01- A0133 REV A, DOUGLAS PSAMSL DWG 7981
- [SDR UPS06846709](https://openairdocs.org/sdr/UPS06846709.md): Fairing · corroded · Mar 21, 2006 · N706UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 FLAP STA 98FH, CORROSION FOUND ON CANOE UNDER FLAP TRACKS. REMOVED STA 98 RH FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION FROM FLAP CANOE IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 RT
- [SDR UPS06846680](https://openairdocs.org/sdr/UPS06846680.md): Splice · corroded · Mar 21, 2006 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > A-PIT TORQUE BOX STA 280-270 LONGERON 34L-35L FITTING HAS CORROSION. REMOVED BATH TUB FITTING AT STA 280, AND REMOVED LONGERON SPLICE FITTING AT STA 270-280 L35L IAW SRM 51-1-20, AND SRM 53-2-2 FIG 10 LOCATED AND DRILLED AND INSTALLED NEW LONGERON SPLICE FITT
- [SDR UPS06846597](https://openairdocs.org/sdr/UPS06846597.md): Longeron · cracked · Mar 20, 2006 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 LONGERON 15R IS CRACKED WHERE VERTICAL STAB ATTACHES STA 1740. REMOVED CRACKED LONGERON SECTION AT STA 1730-1750 15R IAW SRM 51-01-21-0 AND SRM 53-02-02-0. FABRICATED AND INSTALLLED LONGERON SPLICE SECTION AT STA 1730-1750 L15R IAW SRM 53-
- [SDR UPS06846518](https://openairdocs.org/sdr/UPS06846518.md): Rib · cracked · Mar 18, 2006 · N706UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT CENTER LE XRS 323 RIB IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-0, 57-3-1 AND 51-01-20D.
- [SDR UPS06846059](https://openairdocs.org/sdr/UPS06846059.md): Windshield · cracked · Jan 27, 2006 · N706UP · Doug DC871F · Flight Compartment Windows
  > OUTER PANE WINDSHIELD ON F/O'S SIDE CRACKED. REMOVED AND REPLACED RT WINDSHIELD PER MM 56-10-02-2, OPS AND LK CKS OK.
- [SDR UPS05845646](https://openairdocs.org/sdr/UPS05845646.md): Engine · flamed out · Oct 26, 2005 · N706UP · Doug DC871F · Powerplant System
  > NR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL.
- [SDR UPS04843616](https://openairdocs.org/sdr/UPS04843616.md): A/C Pack · odor · Dec 20, 2004 · N706UP · Doug DC871F · Cabin Cooling System
  > ON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INSPECTED A/C FOR SPILLED FLUIDS IN CARGO AREA AND LOWER PITS. NONE FOUND. A/C OK FOR SERVICE.
- [SDR UPS04843555](https://openairdocs.org/sdr/UPS04843555.md): Battery Pack · discharged · Nov 29, 2004 · N706UP · Doug DC871F · Emergency Lighting
  > EMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD.
- [SDR UPS04843333](https://openairdocs.org/sdr/UPS04843333.md): Lamp · inoperative · Oct 9, 2004 · N706UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD.
- [SDR UPS04842661](https://openairdocs.org/sdr/UPS04842661.md): Link · broken · Jul 7, 2004 · N706UP · Doug DC871F · Brake
  > NR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002
- [SDR UPS04842061](https://openairdocs.org/sdr/UPS04842061.md): Fitting · cracked · Mar 6, 2004 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.
- [SDR UPS04842063](https://openairdocs.org/sdr/UPS04842063.md): Longeron · cracked · Mar 5, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-290, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10.
- [SDR UPS04842062](https://openairdocs.org/sdr/UPS04842062.md): Longeron · cracked · Mar 5, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10.
- [SDR UPS04842035](https://openairdocs.org/sdr/UPS04842035.md): Floor Support · corroded · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D, 51-1-21 AND 51-3-0.
- [SDR UPS04842034](https://openairdocs.org/sdr/UPS04842034.md): Skin · cracked · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPAIR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING DOUBLER, CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBL
- [SDR UPS04842031](https://openairdocs.org/sdr/UPS04842031.md): Support Fitting · cracked · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D, 51-3-0.
- [SDR UPS04842029](https://openairdocs.org/sdr/UPS04842029.md): Longeron · cracked · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION, INSTALLED STRAPS AND SPLICE FITTING IAW SRM 53-2-2 FIG 10.
- [SDR UPS04842014](https://openairdocs.org/sdr/UPS04842014.md): Doubler · corroded · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17D, 51-1-20D, 51-1-21.
- [SDR UPS04842013](https://openairdocs.org/sdr/UPS04842013.md): Longeron · cracked · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10.
- [SDR UPS04842010](https://openairdocs.org/sdr/UPS04842010.md): Shear Tie · cracked · Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2A.
- [SDR UPS04842033](https://openairdocs.org/sdr/UPS04842033.md): Frame · corroded · Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SECTION, FABRICATED, INSTALLED 2 SPLICES, ANGLES AND REPLACEMENT FRAME SECTION IAW SRM 53-2-0 FIG 2.
- [SDR UPS04842030](https://openairdocs.org/sdr/UPS04842030.md): Skin · cracked · Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.
- [SDR UPS04842017](https://openairdocs.org/sdr/UPS04842017.md): Skin · cracked · Mar 2, 2004 · N706UP · Doug DC871F · Rudder, Plate/Skin
  > INSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01.
- [SDR UPS04842011](https://openairdocs.org/sdr/UPS04842011.md): Skin · corroded · Mar 2, 2004 · N706UP · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4.
- [SDR UPS04842009](https://openairdocs.org/sdr/UPS04842009.md): Fitting · cracked · Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D, 53-1-0.
- [SDR UPS04842067](https://openairdocs.org/sdr/UPS04842067.md): Skin · corroded · Feb 28, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKIN FILLER IAW SAA SK 706-550 AND DC8-5330-20148-A.
- [SDR UPS04841751](https://openairdocs.org/sdr/UPS04841751.md): Relief Valve · stuck · Jan 16, 2004 · N706UP · Doug DC871F · Landing Gear Steering System
  > DURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND BOGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT MAIN FEAR STUCK OPEN. REPLACED RELIEF VALVE POF 32-53-02. NO LEAKS DETECTED. HYD WAS SERVICED.
- [SDR UPS03841456](https://openairdocs.org/sdr/UPS03841456.md): Skin · corroded · Oct 17, 2003 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > FOUND EXTENSIVE CORROSION AT STATION 1746 SEVERAL RIVETS PULLED THROUGH SKIN. SKIN IS CRACKED AT L36 AND STA 1746. REMOVED FASTENERS IN CORRODED AREA FOUND L36 AFT OF STA 1746. REMOVED 9 X 6 SECTION OF SKIN REF SRM 53-02-011 NR 39550, REF ECA 56908 LOG PAGE
- [SDR UPS03841223](https://openairdocs.org/sdr/UPS03841223.md): Fitting · cracked · Sep 15, 2003 · N706UP · Doug DC871F · Trailing Edge Flaps
  > LT INBOARD FLAP HINGE CRACKED (MARKED) LT WING STA 98. DEFERRED PER FERRY PERMIT 9020. REMOVED STA 98 BASED FTG & ATTACHING STRUCTURE. LOCATED & DRILLED NEW 5751182-505 BASE FTG IAW DAC DWG 5751172. INSTALLED BASE FTG IAW DAC DWG 5751172. INSTALLED CLOSUR
- [SDR UPS03840376](https://openairdocs.org/sdr/UPS03840376.md): Smoke Detector · inoperative · Mar 27, 2003 · N706UP · Doug DC871F · Smoke Detection
  > NR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD.
- [SDR UPS02837958](https://openairdocs.org/sdr/UPS02837958.md): Odor · detected · Mar 30, 2002 · N706UP · Doug DC871F · Air Distribution System
  > INSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUPLICATE ODOR. OK FOR CONTINUED SERVICE.
- [SDR UPS02837935](https://openairdocs.org/sdr/UPS02837935.md): Fitting · corroded · Mar 11, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D, 51-1-21.
- [SDR UPS02837932](https://openairdocs.org/sdr/UPS02837932.md): Doubler · corroded · Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACED DOUBLER IAW DWG 5649028, AND SRM 51-1-20D, 51- 1-21.
- [SDR UPS02837908](https://openairdocs.org/sdr/UPS02837908.md): Longeron · corroded · Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LONG 35L BETWEEN STA 1650-1680, FABRICATED AND REPLACED LONGERON SECTION AND END FITTINGS IAW DWG 3647110, AND SRM 51-1-20D, 51-3-0.
- [SDR UPS02837897](https://openairdocs.org/sdr/UPS02837897.md): Fitting · cracked · Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D, 51-1-20D.
- [SDR UPS02837896](https://openairdocs.org/sdr/UPS02837896.md): Fitting · cracked · Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D, 53-2-0 FIG 2D.
- [SDR UPS02837911](https://openairdocs.org/sdr/UPS02837911.md): Fitting · cracked · Mar 7, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5616306, AND SRM 51-1-20D.
- [SDR UPS02837914](https://openairdocs.org/sdr/UPS02837914.md): Skin · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15A.
- [SDR UPS02837904](https://openairdocs.org/sdr/UPS02837904.md): Skin · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.
- [SDR UPS02837900](https://openairdocs.org/sdr/UPS02837900.md): Skin · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND SKIN IS CRACKED AT STA 60 BETWEEN LONG 20L AND 21L. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER
- [SDR UPS02837899](https://openairdocs.org/sdr/UPS02837899.md): Skin · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CRACKED AT LONG 22R APPROX. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED DOUBLE
- [SDR UPS02837895](https://openairdocs.org/sdr/UPS02837895.md): Fitting · corroded · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITTING HAVE INTERGRANULAR CORROSION AT STA 280 LONG 21L. REMOVED AND REPLACED FITTINGS IAW DWG 4773295 AND SRM 51-3-0, 51-1-20D.
- [SDR UPS02837878](https://openairdocs.org/sdr/UPS02837878.md): Door Frame · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.
- [SDR UPS02837873](https://openairdocs.org/sdr/UPS02837873.md): Skin · cracked · Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKIN IS CRACKED BETWEEN LONG 31R AND 32R. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG 22.

Next page: https://openairdocs.org/deregistered/N706UP-2010-03-30/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 = 'N706UP' AND deregistration_id = 'N706UP-2010-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N706UP-2010-03-30/reports

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