# Service difficulty reports: N708UP, cancelled Mar 30, 2010

A list on [N708UP, cancelled Mar 30, 2010](https://openairdocs.org/deregistered/N708UP-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 5 · 243 reports

- [SDR UPS08851691](https://openairdocs.org/sdr/UPS08851691.md): Slide · out of position · Feb 18, 2008 · N708UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REMOVED EVACUATION SLIDE AND CONTAINER PER MM 25-60-01-2. REPOSITIONED SLIDE IN CONTAINER AND INSTALLED PER MM 25-60-01-2.
- [SDR UPS08851661](https://openairdocs.org/sdr/UPS08851661.md): Slide · out of position · Feb 12, 2008 · N708UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A CREW REPORTED THAT THE MAIN ENTRY DOOR SLIDE GIRT BAR WILL NOT LOCK IN TO FLOOR WITH DOOR CLOSED. REPACKED MAIN ENTRY DOOR SLIDE IAW MM 25-60, OPS CHECK GOOD.
- [SDR UPS08851653](https://openairdocs.org/sdr/UPS08851653.md): Bracket · broken · Feb 11, 2008 · N708UP · Doug DC871F · Escape Slide
  > EVAC SLIDE PSI AND EXPIRATION ILLEGIBLE FROM INSPECTION WINDOW. EVAC SLIDE COVER LATCH BRACKET IS BROKEN. SLIDE COVER REMOVED AND ROUTED FOR REPAIR INSTALLED LATCH AS REQUIRED PER SRM 51-01-21A. REINSTALLED SLIDE INSIDE COVER AND ON TO AIRCRAFT, REF MM 25-6
- [SDR UPS08851654](https://openairdocs.org/sdr/UPS08851654.md): Skin · gouged · Feb 10, 2008 · N708UP · Doug DC871F · Trailing Edge Flaps
  > RIGHT INBOARD T/E FLAP LOWER SURFACE DENT AT INBOARD LOCATION. MEASURE DENT AT 1 1/4 BY 1 3/4.063 DEEP. FOUND.015 GOUGE IN DENT AND BLENDED TO.019 DEEP. REMOVED DAMAGE PER SRM 57-02-05. VERIFIED DAMAGED REMOVED. OK TO INSTALL DOUBLER. INSTALLED DOUBLE
- [SDR UPS07851305](https://openairdocs.org/sdr/UPS07851305.md): Lamp · inoperative · Dec 16, 2007 · N708UP · Doug DC871F · Emergency Lighting
  > ONE EMERGENCY EXIT LIGHT IN COCKPIT INOP. RELAMPED COCKPIT DOME LIGHT IAW DC8 MM 33-50-02-2. OPS CHECK GOOD.
- [SDR UPS07851311](https://openairdocs.org/sdr/UPS07851311.md): Slide · dislodged · Dec 10, 2007 · N708UP · Doug DC871F · Escape Slide
  > ENTRY DOOR OPENED FROM OUTSIDE A/C BY LOAD SUP. SLIDE FELL OUT OF PACK, DID NOT INFLATE. REINSTALLED SLIDE AS REQUIRED IAW MM 25-60-01-2
- [SDR UPS07851114](https://openairdocs.org/sdr/UPS07851114.md): Light · smoke · Nov 7, 2007 · N708UP · Doug DC871F · Flight Compartment Lighting
  > HAD LIGHT ODOR OF SMOKE IN COCKPIT. F/E PANEL LIGHTS WENT OUT. APPEARS TO BE A 5 AMP FUSE HAS BLOWN ON F/E PANEL DID NOT REPLACE IN FLIGHT. REMOVED AND REPLACED F/E PANEL LIGHT. FUSE 5 IAW MM 33-13-00-5. OPS CHKS GOOD.
- [SDR UPS07850941](https://openairdocs.org/sdr/UPS07850941.md): Slide · out of position · Oct 18, 2007 · N708UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A ESCAPE SLIDE NOT PROPERLY STOWED. REPACK ESCAPE SLIDE, OK FOR SERVICE.
- [SDR UPS07850413](https://openairdocs.org/sdr/UPS07850413.md): Battery Pack · discharged · Aug 8, 2007 · N708UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD.
- [SDR UPS07849990](https://openairdocs.org/sdr/UPS07849990.md): Unknown · unknown · Jun 18, 2007 · N708UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS WOULD NOT COME ON WHEN PERFORMING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT AND TESTED IAW 33-50-01-2. TESTS OK.
- [SDR UPS07849327](https://openairdocs.org/sdr/UPS07849327.md): Battery · inoperative · Mar 5, 2007 · N708UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW MM 33-50-01.
- [SDR UPS06848795](https://openairdocs.org/sdr/UPS06848795.md): Battery · discharged · Dec 21, 2006 · N708UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WON'T TEST. FOUND ON PRE-DEPARTURE CK. REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT WITH REF TO M/M 33- 50-01-2. GROUND CKS GOOD.
- [SDR UPS06848254](https://openairdocs.org/sdr/UPS06848254.md): Fitting · cracked · Sep 25, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 70 L32R FWD SIDE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20 D.
- [SDR UPS06848095](https://openairdocs.org/sdr/UPS06848095.md): Fitting · cracked · Sep 25, 2006 · N708UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C3 FITTING CRACKED AT RT STA 70 L30R. REMOVED AND REPLACED FITTING IAW SRM 51-3-0,51-1-20D AND 51-3-2.
- [SDR UPS06848199](https://openairdocs.org/sdr/UPS06848199.md): Fitting · cracked · Sep 24, 2006 · N708UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE:C3 C-PIT STA 1160 INSIDE OF DOOR, SPYDER FITTING IS CRACKED AT THE BOLT. REMOVED CRACKED SPYDER FITTING AT STA 1160 IAW SRM 51-1-21, FABRICATED AND INSTALLED SPYDER FITTING AT STA 1160 INSIDE OF DOOR IAW SRM 51-3-0, 51-1-21, AND DWG 3754025
- [SDR UPS06848193](https://openairdocs.org/sdr/UPS06848193.md): Finger Doubler · corroded · Sep 23, 2006 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 STA 440-460 L34L-L34R FUSELAGE DOUBLER AND FINGER DOUBLER HAVE CORROSION. REMOVED FUSELAGE SKIN DOUBLER AND FINGER DOUBLER AT STA 440-460 L34L-L34R IAW SRM 53-2-0. FABRICATED AND INSTALLED SKIN DOUBLER AND FINGER DOUBLER AT STA 440-46- L34
- [SDR UPS06848191](https://openairdocs.org/sdr/UPS06848191.md): Stringer Splice · cracked · Sep 23, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 STA 440 TO STA 460 L36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L36 IAW SRM 51-1-20D, AND SRM 51-03-02-0.
- [SDR UPS06848220](https://openairdocs.org/sdr/UPS06848220.md): Doubler · corroded · Sep 22, 2006 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 AFTER SKIN REMOVAL A/C BAY FOUND INTERNAL DOUBLER CORROSION OUT OF LIMITS STA 8-70 BETWEEN L30L-32L. REMOVED INTERNAL DOUBLER FROM STA 8-70 L30L-32L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA 8-70 L30L-32L IAW SRM 53
- [SDR UPS06848192](https://openairdocs.org/sdr/UPS06848192.md): Longeron Splice · corroded · Sep 22, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 L36 AFT FITTING AND LONGERON AT STA 1690 HAVE CORROSION. FOUND CORROSION OUT OF LIMITS AT STA 1690 L36 SPLICE FITTING IAW SRM 51-20-00. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1690 L36 IAW SRM 51-1-20D, AND SRM 53-02-02-00.
- [SDR UPS06848287](https://openairdocs.org/sdr/UPS06848287.md): Rib · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING OB LE UPPER RIB CRACKED AT XFS 824. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-21, 51-01-20D.
- [SDR UPS06848094](https://openairdocs.org/sdr/UPS06848094.md): Doubler · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 597. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21,51-1-20D AND DWG 5769600.
- [SDR UPS06848058](https://openairdocs.org/sdr/UPS06848058.md): Doubler · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing Main, Frame Structure
  > INSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS566. REMOVED, FABRICATED AND INSTALLED INNER DOUBLER AND FILLER IAW DWG 5769600, SRM 51-1-21 AND 51-1-20D.
- [SDR UPS06848047](https://openairdocs.org/sdr/UPS06848047.md): Rib · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS 653. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.
- [SDR UPS06848046](https://openairdocs.org/sdr/UPS06848046.md): Rib · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS659. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.
- [SDR UPS06848045](https://openairdocs.org/sdr/UPS06848045.md): Rib · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS772. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D.
- [SDR UPS06848044](https://openairdocs.org/sdr/UPS06848044.md): Rib · cracked · Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > RT WING OB LE LWR RIB CRACKED AT XFS 734. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 51-1-20D,51-1-21.
- [SDR UPS06848289](https://openairdocs.org/sdr/UPS06848289.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.
- [SDR UPS06848288](https://openairdocs.org/sdr/UPS06848288.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002, 51-01-21, AND 51-01-20D.
- [SDR UPS06848286](https://openairdocs.org/sdr/UPS06848286.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 379. CRACK TERMINATES AT FASTENER HOLE. FABRICATED REPAIR ANGLES AND INSTALLED IAW DC-8 SRM 57-02-00-0 AND 51-01-20D.
- [SDR UPS06848285](https://openairdocs.org/sdr/UPS06848285.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:3C RT WING CENTER LE UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.
- [SDR UPS06848284](https://openairdocs.org/sdr/UPS06848284.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.
- [SDR UPS06848242](https://openairdocs.org/sdr/UPS06848242.md): Skin · corroded · Sep 20, 2006 · N708UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE:C3 AFTER REMOVAL OF CORROSION AT LWR D-PIT DOOR, SKIN, FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED D-PIT SKIN FROM 1350-1490 L31L-L31R IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS06848033](https://openairdocs.org/sdr/UPS06848033.md): Rib · cracked · Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE-C3 RT CENTER L/E UPPER RIB CRACKED AT XFS 366. STOPDRILLED CRACK AT RT L/E CENTER UPPER RIB AT XFS 366 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT RT L/E CENTER UPPER RIB AT STA XFS 366 IAW SRM 57-02-00 FIG 002 AND SRM
- [SDR UPS06848290](https://openairdocs.org/sdr/UPS06848290.md): Fitting · cracked · Sep 19, 2006 · N708UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C3 AT STA 742.2 FRAME FITTING IS CRACKED ON AFT UPPER SIDE OF CUSP. REMOVED AND REPLACED FRAME FITTING IAW DC-8 SRM 51-01-20D AND 51-01-21.
- [SDR UPS06848218](https://openairdocs.org/sdr/UPS06848218.md): Cusp Web · corroded · Sep 19, 2006 · N708UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 UPPER CUSP FROM STA 1260 TO 1290 EXFOLIATED CORROSION ON UPPER CUSP AND CRACKED LT SIDE. REMOVED DAMAGED CUSP AT STA 1260-1290 IAW SRM 51-3-0 AND SRM 51-1-8. REPAIRED DAMAGED CUSP AT STA 1250-1290 IAW SAA EA NR 008-5300-01-A0455 REV B, UPS
- [SDR UPS06848059](https://openairdocs.org/sdr/UPS06848059.md): Skin · cracked · Sep 19, 2006 · N708UP · Doug DC871F · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C3 NR 1 PYLON INBD SIDE FOUND CRACK AT APPROX STA YN 321. STOP DRILLED CRACK. CRACK TERMINATES AT STOP DRILL EO DC8-5740-0716.
- [SDR UPS06847643](https://openairdocs.org/sdr/UPS06847643.md): Battery Pack · discharged · Aug 9, 2006 · N708UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE: N/A EMERG LIGHTING BATT PACK PWR LOW. EMERG LIGHTING BATT PACK REPLACED IAW MM 33-50-01-2.
- [SDR UPS06846411](https://openairdocs.org/sdr/UPS06846411.md): Trim Tab · cracked · Mar 7, 2006 · N708UP · Doug DC871F · Elevator, Tab Structure
  > INSPECTION TYPE:N/A RT ELEV TRIM TAB CRACKED/DAMAGED ABOUT 1' OB OF PREVIOUS REPAIR. REMOVED RT ELEV GEAR TAB REF MM 27-30-03-2. OK TO INSTALL. TRIMMED OTBD EDGE OF RT ELEVATOR GEARED TRIM TAB PER EO DC8-5520-23895A AND INSTALLED TRIM TAB IAW MM 27-30-03. OPS
- [SDR UPS05844682](https://openairdocs.org/sdr/UPS05844682.md): Doubler · delaminated · Jun 9, 2005 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
  > UNDER BELLY PANELS (4EA) DELAMINATED ON PREVIOUS REPAIR. LT WING TO BODY LOWER FILLET PANEL DELAMINATED. D303878 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED D303879 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED.
- [SDR UPS05844594](https://openairdocs.org/sdr/UPS05844594.md): Battery Pack · inoperative · Jun 2, 2005 · N708UP · Doug DC871F · Emergency Lighting
  > EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER 33-50-01.
- [SDR UPS05844417](https://openairdocs.org/sdr/UPS05844417.md): Skin · corroded · Apr 27, 2005 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SP COMPLY WITH D 301309 REGARDING FUSELAGE SKIN CORROSION AT E/E DOOR STA 35. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330- 22128-A AND SAA SK 708-911.
- [SDR UPS05844380](https://openairdocs.org/sdr/UPS05844380.md): Skin · corroded · Apr 26, 2005 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE RT JUST OUTBOARD OF FWD EQUIPMENT CENTER DOOR MARKED. REMOVED DAMAGED SKIN IN CORRODED AREA DIM APPX 2.9 X 2.5 INCHES. REMOVED ADDITIONAL DAMAGED SKIN APPROX 10 X 9 INCHES TOTAL UNABLE TO CLEAN UP ALL OF UNDERLYING CORROSION AT THIS TIME
- [SDR UPS05843662](https://openairdocs.org/sdr/UPS05843662.md): Engine · flamed out · Jan 18, 2005 · N708UP · Doug DC871F · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FLAMED OUT IN FLIGHT. A/C IS OOS. PERFORMED STEP 4 UP TO FUEL FILTER REPLACEMENT ON FIGURE 139 SHEET 1 OF MM 71 00 00. TS (558010) PERFORMED ENG MAINT RUN PER MM 71-00-00-1, NO DEFECTS NOTED. A/C OK FOR SERVICE.
- [SDR UPS04843609](https://openairdocs.org/sdr/UPS04843609.md): Battery Pack · inoperative · Dec 15, 2004 · N708UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FAIL PRELIGHT TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50, OPS CK GOOD.
- [SDR UPS04843100](https://openairdocs.org/sdr/UPS04843100.md): Attach Angle · cracked · Aug 23, 2004 · N708UP · Doug DC871F · Vertical Stabilizer
  > INSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25043-17-7PH.080. HE
- [SDR UPS04843128](https://openairdocs.org/sdr/UPS04843128.md): Bulkhead · cracked · Aug 19, 2004 · N708UP · Doug DC871F · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPAIRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DATED 09/08/04 & 8110-3
- [SDR UPS04843101](https://openairdocs.org/sdr/UPS04843101.md): Fitting · corroded · Aug 19, 2004 · N708UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2, BATHTUB FITTING CORRODED AT STA 340 BETWEEN L35R & L34R. REMOVED BATHTUB FITTING PER SRM 51-1-20D. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING & REPAIR ANGLES PER SRM 51-1-20D, 53-2-0 FIG 2D.
- [SDR UPS04843099](https://openairdocs.org/sdr/UPS04843099.md): Fitting · corroded · Aug 19, 2004 · N708UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 A-PIT FS 300 BATHTUB FITTING BETWEEN L34L & L33L HAS HEAVY CORROSION. REMOVED BATHTUB FITTING. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2B. INSTALLED NEW FITTING AND REPAIR ANGLES PER SRM 53-2-0 FIG 2B, 51-1-20D.
- [SDR UPS04843098](https://openairdocs.org/sdr/UPS04843098.md): Fitting · cracked · Aug 19, 2004 · N708UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C2, FS 450 L31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31L.
- [SDR UPS04843027](https://openairdocs.org/sdr/UPS04843027.md): Fitting · cracked · Aug 19, 2004 · N708UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, STATION 1776 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.

Next page: https://openairdocs.org/deregistered/N708UP-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 = 'N708UP' AND deregistration_id = 'N708UP-2010-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N708UP-2010-03-30/reports

---
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