# Service difficulty reports: N750UP, cancelled Apr 19, 2010

A list on [N750UP, cancelled Apr 19, 2010](https://openairdocs.org/deregistered/N750UP-2010-04-19.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 6 · 261 reports

- [SDR UPS07850577](https://openairdocs.org/sdr/UPS07850577.md): Starter · leaking · Sep 1, 2007 · N750UP · Doug DC871F · Engine Cranking
  > INSPECTION TYPE:N/A IFSD - NR 1 ENG SHUTDOWN IN CLIMB PASSING 25000 DUE TO OIL QTY GOING TO ZERO. OIL PRESSURE WAS 12 PSI. SERVICED OIL, RAN ENGINE, FOUND OIL LEAKING FROM STARTER. REMOVED AND REPLACED NR 1 ENGINE STARTER IAW MM 80-10-01-2. OPS CHECK REQUI
- [SDR UPS07849884](https://openairdocs.org/sdr/UPS07849884.md): Skin · corroded · Jun 4, 2007 · N750UP · Doug DC871F · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN, FINGER DOUBLER AND LONGERON 31R, STARTING AT STA 70 AND EXTENDING APPROX 6 FEET REFERENCE D351779 AND FERRY PERMIT 9033. [06-29-07] REMOVED LWR FWD PANEL IN "A" PIT TO ACCESS AREA PER SRM 51-3-0 & OPENED UP EXTERNA
- [SDR UPS07849428](https://openairdocs.org/sdr/UPS07849428.md): Light · inoperative · Mar 14, 2007 · N750UP · Doug DC871F · Emergency Lighting
  > ON CREW PREFLIGHT, FOUND EMERGENCY LIGHTS INOP AWAITING CLOSING LP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-50-01-2. CHECKS GOOD.
- [SDR UPS07849093](https://openairdocs.org/sdr/UPS07849093.md): Relay · inoperative · Jan 31, 2007 · N750UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY/RELAY UNIT. NOW OPS OK. REF 33-50-01-2.
- [SDR UPS07849092](https://openairdocs.org/sdr/UPS07849092.md): Relay · inoperative · Jan 31, 2007 · N750UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTT BATTERY/RELAY UNIT. NOW OPS OK. REF 33-50-01-2.
- [SDR UPS07848864](https://openairdocs.org/sdr/UPS07848864.md): Battery Pack · inoperative · Jan 14, 2007 · N750UP · Doug DC871F · Emergency Lighting
  > EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK ASSY IAW MM 33-50-01-2.
- [SDR UPS06848786](https://openairdocs.org/sdr/UPS06848786.md): Battery Pack · inoperative · Dec 18, 2006 · N750UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A ON PRE-DEPARTURE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2.
- [SDR UPS06848341](https://openairdocs.org/sdr/UPS06848341.md): Battery Pack · inoperative · Oct 24, 2006 · N750UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD.
- [SDR UPS06848323](https://openairdocs.org/sdr/UPS06848323.md): Battery Pack · inoperative · Oct 24, 2006 · N750UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS. OPS CKS GOOD.
- [SDR UPS06847301](https://openairdocs.org/sdr/UPS06847301.md): Fuse · blown · Jul 7, 2006 · N750UP · Doug DC871F · Instrument Panel
  > INSPECTION TYPE:N/A SMOKE AND ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACKGROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE (5AMP) OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.
- [SDR UPS06847293](https://openairdocs.org/sdr/UPS06847293.md): Fuse · blown · Jul 7, 2006 · N750UP · Doug DC871F · Electrical Power System Wiring
  > SMOKE & ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACK GROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE-5 AMP. OP'S CHECK NORMAL ON BACKGROUND LIGHTS PER WDM 33.
- [SDR UPS05845559](https://openairdocs.org/sdr/UPS05845559.md): Ground Wire · shorted · Oct 7, 2005 · N750UP · Doug DC871F · Fire Protection System Wiring
  > CARGO SMOKE LIGHT ILLUMINATED - ALL POSITIONS. T/S SYS FOUND & REPAIRED BAD GROUND WIRE 8M OHMS ON SMOKE DETECTOR UNIT NR 1. FOUND & REPAIRED BAD GND WIRE ON SDU NR 3. FOUND AND REPAIRED BAD GNU D WIRE ON SDU NR 5. ALL OTHER SDU GND WIRES CKD GOOD PER WDM 26
- [SDR UPS05845283](https://openairdocs.org/sdr/UPS05845283.md): Doubler · cracked · Aug 19, 2005 · N750UP · Doug DC871F · Landing Gear Doors
  > NOSE SECTION FUSELAGE SKIN HAS 3/8" CRACK AT AFT HINGE ACCESS DOOR. REMOVED CRACKED DOUBLER AT NOSE EXTERIOR AFT SKIN IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG56126127 AND SRM 51-1-20E.
- [SDR UPS05845421](https://openairdocs.org/sdr/UPS05845421.md): Spar · cracked · Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE:C1 RIGHT KEEL BEAM AT FS 857 2.5 INCH CRACK ON LWR SPAR. STOP DRILLED CRACK AT XCW 4.0 IAW SRM 51-1-20D NDT HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED FILLERS VERTICAL FILLERS AND -136 ANGLE AND STIFFENERS AND I
- [SDR UPS05845275](https://openairdocs.org/sdr/UPS05845275.md): Finger Doubler · corroded · Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Plate/Skin
  > COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEAR HEAD RIVETS AND CORRODED AT STA -67 TO -80 RBL 60. REMOVED FINGER DOUBLER IAW SRM 51-1-21 AND 51-3-0. REMOVED CORROSION FROM WEB IAW SRM 51-1-8, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER AT STA -67
- [SDR UPS05845241](https://openairdocs.org/sdr/UPS05845241.md): Frame · cracked · Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Frame
  > FRAME ON 62 DOOR OPENING IS CRACKED INSIDE OPENING RT SIDE. FAB`D DOUBLER AND REPAIRED IAW SRM 53-05-01 AND 51-1-21A.
- [SDR UPS05845236](https://openairdocs.org/sdr/UPS05845236.md): Fitting · corroded · Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > HEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR UPS05845369](https://openairdocs.org/sdr/UPS05845369.md): Floorbeam · cracked · Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C1 FLOORBEAM CRACKED AT FS 55 LBL 12. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 TEMP REV 53-152, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 TEMP REV 53-152 AND 51-1-20D.
- [SDR UPS05845285](https://openairdocs.org/sdr/UPS05845285.md): Fitting · cracked · Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21.
- [SDR UPS05845282](https://openairdocs.org/sdr/UPS05845282.md): Fitting · cracked · Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > STA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D.
- [SDR UPS05845256](https://openairdocs.org/sdr/UPS05845256.md): Fitting · cracked · Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > END FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D.
- [SDR UPS05845383](https://openairdocs.org/sdr/UPS05845383.md): Splice · cracked · Aug 14, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 CRACKED SPLICE ANGLE INSIDE CHANNEL AT FS 450 L33R. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-21D, MACHINED AND INSTALLED LONGERON SPLICE AT STA 450 L33R IAW DWG 3750330.
- [SDR UPS05845368](https://openairdocs.org/sdr/UPS05845368.md): Splice · cracked · Aug 14, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 SPLICE FITTING AT FS 450 L31R IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31R IAW DWG 5754814 AND SRM 51-1-20D.
- [SDR UPS05845385](https://openairdocs.org/sdr/UPS05845385.md): Fitting · cracked · Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND INSTALLED FITTING AND INTERCOSTAL IAW DWG 4758514 AND DWG 9754949.
- [SDR UPS05845292](https://openairdocs.org/sdr/UPS05845292.md): Fitting · corroded · Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > LWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED.500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTING AT FS 1230 L32R IAW SRM 51-3-2 AND 51-1-20D.
- [SDR UPS05845255](https://openairdocs.org/sdr/UPS05845255.md): Skin · cracked · Aug 13, 2005 · N750UP · Doug DC871F · Aileron Tabs
  > LT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR DOUBLER IAW 57-02-00-0 AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 AND 57-08-00-0. REPA
- [SDR UPS05845242](https://openairdocs.org/sdr/UPS05845242.md): Rib · cracked · Aug 13, 2005 · N750UP · Doug DC871F · Wing, Rib/Bulkhead
  > LT LE UPPER RIB CRACKED AT XFS 766.250. FAB`D DOUBLER AND REPAIRED IAW DWG 5769470 AND SRM57-02-00 FIG 2.
- [SDR UPS05845240](https://openairdocs.org/sdr/UPS05845240.md): Rib · cracked · Aug 13, 2005 · N750UP · Doug DC871F · Wing, Rib/Bulkhead
  > LT WING LE UPPER RIB CRACKED AT XFS 707. FABED DOUBLER AND REPAIRED RIB IAW DWG 5769466, AND SRM 57-2-0 FIG 2.
- [SDR UPS05845239](https://openairdocs.org/sdr/UPS05845239.md): Finger Doubler · corroded · Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Plate/Skin
  > COCKPIT SUBFLOOR FINGER DOUBLER HAS SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER DOUBLER AT FS -67 TO -52 LBL24. REMOVED AND REPLACED FINGER DOUBLER IAW SRM DWG 5612298 AND SRM 51-1-21 AND 51-1-20D.
- [SDR UPS05845420](https://openairdocs.org/sdr/UPS05845420.md): Cusp Web · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 CUSP CRACKED FS 1100 L21R. REMOVED CUSP DOUBLER AT FS 1100 L21R AND REMOVED DAMAGED SECTION OF L21R IAW SRM 51-1-20A AND SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED SPLICE PLATE -3 AND -5, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53
- [SDR UPS05845384](https://openairdocs.org/sdr/UPS05845384.md): Pan · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Passenger/Crew Doors
  > INSPECTION TYPE:C1 L1 DOOR LWR AFT CORNER JAMB INSIDE WEB CRACKED 2 INCHES LONG. REMOVED DOOR JAMB AND WEB CUT OUT DAMAGED AREA IAW DWG 5597646, FABRICATED DOUBLER AND SPLICE AND INSTALLED REPAIR PARTS IAW DWG 5597646.
- [SDR UPS05845294](https://openairdocs.org/sdr/UPS05845294.md): Cusp Web · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > CUSP HAS SHEAR HEAD FASTENER AND CRACK 1 INCH LONG FS 1420 L21R. REMOVED DAMAGED CUSP FROM BS 1390-1430 L21R IAW SRM 51-1-20D AND 51-1-2. FABRICATED AND INSTALLED REPAIR PARTS AND CUSP ANGLE IAW SRM 53-2-5 FIG 15 AND DWG 9754069 AT BS 1390-1430 L21R.
- [SDR UPS05845257](https://openairdocs.org/sdr/UPS05845257.md): Longeron · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > LONGERON 7R CRACKED AT FS 1746. REMOVED DAMAGED AREA IAW SRM 53-02-02 FIG 11, FABRICATED AND INSTALLED REPAIR SPLICE FILLER AND REPAIR ANGLES IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.
- [SDR UPS05845254](https://openairdocs.org/sdr/UPS05845254.md): Longeron · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > LONG 15L CRACKED AT FS 1726. REMOVED DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED REPAIR SPLICE FILLER AND REPAIR ANGLES AND INSTALLED IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.
- [SDR UPS05845252](https://openairdocs.org/sdr/UPS05845252.md): Angle · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > C1 ANGLE CRACKED AT FS 1766 LONG 6L. REMOVED ANGLE IAW SRM 51-1-20D AT FS 1766 LONG 6L. FABRICATED AND INSTALLED ANGLE AT FS 1766 LONG 6L DWG 5773844 AND SRM 51-1-20D.
- [SDR UPS05845251](https://openairdocs.org/sdr/UPS05845251.md): Angle · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous Structure
  > C1 ANGLE CRACKED AT FS 1766 LONG 6R. REMOVED CRACKED ANGLE AT FS 1766 L6R IAW SRM 51-1-20D. FABRICATED AND INSTALLED ANGLE AT FS 1766 L6R IAW SRM DWG 5773844 AND SRM 51-1-20D.
- [SDR UPS05845229](https://openairdocs.org/sdr/UPS05845229.md): Fitting · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > MAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0.
- [SDR UPS05845228](https://openairdocs.org/sdr/UPS05845228.md): Longeron · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > LONGERON 14R CRACKED FS 1746. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 11.
- [SDR UPS05845227](https://openairdocs.org/sdr/UPS05845227.md): Bulkhead · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007.
- [SDR UPS05845219](https://openairdocs.org/sdr/UPS05845219.md): Fitting · cracked · Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05845371](https://openairdocs.org/sdr/UPS05845371.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG 3643110 AND 51-1-20D.
- [SDR UPS05845366](https://openairdocs.org/sdr/UPS05845366.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8
- [SDR UPS05845293](https://openairdocs.org/sdr/UPS05845293.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420.
- [SDR UPS05845281](https://openairdocs.org/sdr/UPS05845281.md): Fitting · corroded · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > MAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTING AT FS 980 LBL 40 IAW SRM 51-3-0, 51-1-21, AND 51-3-2.
- [SDR UPS05845280](https://openairdocs.org/sdr/UPS05845280.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > LONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0.
- [SDR UPS05845279](https://openairdocs.org/sdr/UPS05845279.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > LONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.
- [SDR UPS05845277](https://openairdocs.org/sdr/UPS05845277.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > CRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,51-1-20D AND 51-01-23 FIG 48.
- [SDR UPS05845276](https://openairdocs.org/sdr/UPS05845276.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > MAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SRM 51-1-8. REMOVED AND REPLACED "T" FITTING IAW SRM 51-3-2 AND DWG 3649114.
- [SDR UPS05845274](https://openairdocs.org/sdr/UPS05845274.md): Fitting · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2.
- [SDR UPS05845258](https://openairdocs.org/sdr/UPS05845258.md): Angle · cracked · Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
  > CENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D.

Next page: https://openairdocs.org/deregistered/N750UP-2010-04-19/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 = 'N750UP' AND deregistration_id = 'N750UP-2010-04-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N750UP-2010-04-19/reports

---
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