# Service difficulty reports: N748UP, cancelled Oct 6, 2006

A list on [N748UP, cancelled Oct 6, 2006](https://openairdocs.org/deregistered/N748UP-2006-10-06.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 · 252 reports

- [SDR UPS06846125](https://openairdocs.org/sdr/UPS06846125.md): Smoke · detected · Feb 8, 2006 · N748UP · Doug DC871F · Air Distribution System
  > SMOKE IN COCKPIT, CARGO AREA. A/C INCURRED EXTENSIVE DAMAGE FROM CARGO COMPARTMENT FIRE. AIRCRAFT REMOVED FROM UPS OPERATION SPECIFICATION.
- [SDR UPS05843869](https://openairdocs.org/sdr/UPS05843869.md): Actuator · malfunctioned · Feb 9, 2005 · N748UP · Doug DC871F · Elevator Control System
  > CREW LOST NR 2 INS WITH A WARNING LIGHT. SMELLED ELECTRICAL FUMES FROM PEDESTAL AREA. TURNED NR 2 INS OFF. NOTICED PTC WAS NOT FULLY RETRACTED AND HAD 3/8 EXTENSION SHOWING. FOLLOWED PROCEDURES FOR PTC NOT FULLY RETRACTED. CREW DECLARED EMERGENCY W/TULSA.
- [SDR UPS04842340](https://openairdocs.org/sdr/UPS04842340.md): Seat Track · corroded · Apr 22, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, MAIN CABIN SEAT TRACK G & H AT FS 418 HAS EXFOLIATION. SEAT TRACK AREA DAMAGED RMVD LOCATED AND DRILLED NEW SEAT TRACK SPLICE FITTING AND SPLICE CHANNEL IAW EO DC8 5320-8309-D. INSTALLED IAW EO DC 8 5320-8309D.
- [SDR UPS04842330](https://openairdocs.org/sdr/UPS04842330.md): Fitting · cracked · Apr 22, 2004 · N748UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C-1 CORROSION AROUND FASTENER HOLE ON L35 RT STA 1040-1060 INTERNAL AFT PIT, REMOVED INTERCOSTAL & CLIP AT STA 1040 - 1060 RT L35 RT IAW DC8 SRM 51-1- 20D. FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-1 EVOL LONGERON SPLIC E 51-1-20D, FOUND TO
- [SDR UPS04842331](https://openairdocs.org/sdr/UPS04842331.md): Seat Track · gouged · Apr 20, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, SEAT TRACK C/H STA 1120-1140 GOUGED, REMOVED GOUGES IAW DC8 SRM 53-2-0 & FOUND TO BE OUT OF LIMITS REMOVED FLOOR PANEL F90 & F94 FOR ACCESS. LOCATE NEW SEAT TRACK DRILLED EXISTING FASTENER HOLES ALODINE & PRIME IAW 51-1-8. LOCATE SEAT T
- [SDR UPS04842312](https://openairdocs.org/sdr/UPS04842312.md): Seat Track · corroded · Apr 19, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, UPPER CARGO PIT BETWEEN STA 822 TO 837 FLOORBEAM AT STA 822 AT SEAT TRACK (E) IS CORRODED. CUT SEAT TRACK REPAIR FLOORBEAM INSTALLED NEW SEAT TRACK AND 4 EACH FITTING SPLICE.
- [SDR UPS04842329](https://openairdocs.org/sdr/UPS04842329.md): Skin · cracked · Apr 18, 2004 · N748UP · Doug DC871F · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HORIZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OUT DAMAGE & FAB REPAI
- [SDR UPS04842354](https://openairdocs.org/sdr/UPS04842354.md): Fitting · cracked · Apr 15, 2004 · N748UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, LONGERON FITTING IS CRACKED. REMOVED FITTING, RECEIVED, LOCATED, AND DRILLED FITTING, INSTALLED FIT TING; ALL IAW DC8 SRM 51-1-20D, 51-1-24.
- [SDR UPS04842345](https://openairdocs.org/sdr/UPS04842345.md): Longeron · gouged · Apr 7, 2004 · N748UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C1, LT MLG WW L34 BOTTOM SIDE GOUGED FWD STA 980. REMOVED ADF PANEL AND LONGERON IAW DC8 SRM 51-3-0 AND 51-1-20D. FABRIC ATED LONG -503 IAW DAC DWG 3750347. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -503 LONGERON IAW DC8 SRM 51-1-
- [SDR UPS04842347](https://openairdocs.org/sdr/UPS04842347.md): Doubler · corroded · Apr 6, 2004 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C1, FWD LWR CARGO STA 300 TO 308 L33R DOUBLER WITHIN TORQUE BOX CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED NEW DOUBLER FROM 7075-T6.063 IAW DC8 SRM 51-1-24 AND DAC DWG 3254065. ALODINED AND
- [SDR UPS04842332](https://openairdocs.org/sdr/UPS04842332.md): Fitting · cracked · Apr 6, 2004 · N748UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C-1, 680 LONGERON 11 LT LOWER AFT FITTING IS CRACKED, REMOVED CRACKED FITTING P/N 4751625-1 IAW DC8 SRM 51-3-0,51-1-20D & 51-1- 21 LOCATED AND DRILLED NEW FITTING IAW DAC DWG 4751625 AND DC8 SRM 51- 1-24 AND INSTALLED IAW DC8 SRM 51-1-20D, 51
- [SDR UPS04842324](https://openairdocs.org/sdr/UPS04842324.md): Doubler · corroded · Apr 6, 2004 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-1 FWD LWR CARGO STA 300 TC 308 L33R TO L34R DOUBLER HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8. ORIG THICKNESS WAS.063 IAW DAC DWG 3754065. MATERIAL RMVD WAS.020 AND IS OUT OF LIMITS IAW DC8 SRM 53-2-0 FAB NEW DOUBLER FROM 7075-T6.0
- [SDR UPS04842334](https://openairdocs.org/sdr/UPS04842334.md): Seat Track · worn · Apr 5, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, ENGINEERS SEAT TRACKS HAVE ELONGATED HOLES. REMOVED FWD F/E'S SEAT TRACK IAW DC8 SRM 51-3-0 LOCATED AND DRILLED SE AT TRACK IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-1
- [SDR UPS04842333](https://openairdocs.org/sdr/UPS04842333.md): Seat Track · worn · Apr 5, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, ENGINEER SEAT TRACKS HAVE ELONGATED HOLES. REMOVED F/E SEAT TRACKS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED FWD AND AFT TRACKS P/N 3657504-1 IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SR M 51-3-1
- [SDR UPS04842328](https://openairdocs.org/sdr/UPS04842328.md): Frame · gouged · Apr 5, 2004 · N748UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE: C-1, NLG RT CTR TUNNEL AREA (ACCESS THUR AFT PRESS PAL) FRAME & BRKT GOUGED JUST FWD OF PWR RECP BOX BLEND GOUGE IAW DC8 SRM 53-2-0, FIG 1F ORINGINAL THICKNESS.050 REMAIN ING MATERIAL OF.036 OUT OF LIMITS. ROUNDED GOUGE ON BRAKETT EDGE
- [SDR UPS04842336](https://openairdocs.org/sdr/UPS04842336.md): Seat Track · corroded · Apr 3, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, CORROSION AROUND NUTPLATES & FASTENER FROM STH 1480 TO 1540 AT CUSP LT SIDE OF AFT CARGO COMPT PUT A7763. REMOVED AIR GRILLS CUSP CLOSEOUT & FLOOR TO FOM REMOVED SEAT TRACK ORIG THICKNESS.090 IAW 51-2-0. REMOVED CORR IAW 51-1-8 AFTER BLE
- [SDR UPS04842335](https://openairdocs.org/sdr/UPS04842335.md): Intercostal · dented · Apr 3, 2004 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C-1, STA 1240-1260 L35L INTERCOSTAL DENTED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D MATERIAL ID & FAB OF NEW PART IAW DAC DWG 49758507, HEAT TREATED PART REF LOAD HT041904 -3. ALODINE & PRIMED INTERCOSTAL IAW DC8 SRM 51-1-8. INSTAL
- [SDR UPS04842322](https://openairdocs.org/sdr/UPS04842322.md): Channel · cracked · Apr 3, 2004 · N748UP · Doug DC871F · Trailing Edge Flaps
  > INSPECTION TYPE:C-1 RIGHT WING I/B FLAP O/B TRAILING EDGE IS CRACKED. REMOVED CRACKED CHANNEL. FAB NEW CHANNEL IAW DC8 SRM 57-7-1. ALODINED AND PRIMED CHANNEL IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-3-O,51-3-1,51-1-21 AND 51-1-21A
- [SDR UPS04842351](https://openairdocs.org/sdr/UPS04842351.md): Floorboard · corroded · Apr 2, 2004 · N748UP · Doug DC871F · Fuselage Floor Panel
  > INSPECTION TYPE: C1, MAIN DECK FLOOR PANEL CORRODED STA 50 LBL 14. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS. FABBED SPLICE PLATES IAW DC8 SRM 53-2-3; LOCATED, DRILLED, AND COUNTERSUNK NEW FLOOR PANEL SECTION IAW DC8 SRM 51-1-24. ALOD & PRIMED IA
- [SDR UPS04842338](https://openairdocs.org/sdr/UPS04842338.md): Longeron · corroded · Apr 2, 2004 · N748UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C-1 FWD PIT BETWEEN STA 200-300 LONGERON 34R CORRODED RMVD FASTENERS L34R FS 190-300 & FROM SHEARTIES & FRAMES AT FS 200& 220 AT L34R TO FOM. RMVD CORR FROM L34R AT FS 205-217. ORIG THICKNESS IS.092 MAT RMVD.030 MAT REMAINING.062 & IS OUT
- [SDR UPS04842337](https://openairdocs.org/sdr/UPS04842337.md): Fitting · corroded · Apr 2, 2004 · N748UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C-1C, FWD PIT- FWD SIDE OF TORQUE BOX (APPROX STA 275) BETWEEN LONGERONS 33R -34 RT ZEE ANGLE CORRODED. REMOVED OLD FITTING PN 3755824-1 IAW DC8 SRM 51-1-20D. RECIVED NEW FITT ING PN 3755824-1 TAG 00702413 DRILLED UP FITTING IAW DC8 SRM 51-1
- [SDR UPS04842352](https://openairdocs.org/sdr/UPS04842352.md): Angle · corroded · Apr 1, 2004 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C1, AFT PIT RT CUSP EXTRUSION CORRODED BETWEEN STA 1000 AND 1020 LONG 21 RT. REMOVED DAMAGED CUSP SECTION IAW TR53-179 STA 990-1030 L21 RT. IAW DC8 SRM 51-1-20D. REC'ED, LOCATED AND DRILLED -3 & -5 REPAIR ANGLES, -7 D OUBLER AND -9 CUSP SEC
- [SDR UPS04842350](https://openairdocs.org/sdr/UPS04842350.md): Angle · gouged · Apr 1, 2004 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C1, STA 1560-1580 L21L CUSP MEMBRANE GOUGED. REMOVED GOUGE ON CUSP TONGUE IAW DC8 SRM 53-2-0. OUT OF LIMITS. FABRICATED CUSP IAW DAD DWG 9750448. FABRICATED SPLICES IAW REO G09789. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP SECT
- [SDR UPS04842339](https://openairdocs.org/sdr/UPS04842339.md): Seat Track · broken · Apr 1, 2004 · N748UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C-1, SEAT TRACK STA 1700 LOBES BROKEN OFF. SEAT TRACK FOUND OUT OF LIMITS IAW DC8 SRM & UPS EO 5340-12053. REMOVED SEAT TRACK IAW 51-1-200 & 51-30 MAT ID SEAT TRACK P/N 3772660 IAW 53-7-1 LACATED & DRILLED HOLE IN SEAT TRACK F STA 1670-1710 I
- [SDR UPS04842349](https://openairdocs.org/sdr/UPS04842349.md): Fitting · cracked · Mar 31, 2004 · N748UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, MAIN CABIN, FRAME FITTING CRACKED ON BOTH SIDES FS 427 L11L (DOT 6603). REMOVED TEE FITTING TO GAIN ACCESS TO CRACKED FITTING, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING P/N 3755820- 1 IAW DC8 SRM 51-1-2
- [SDR UPS03841575](https://openairdocs.org/sdr/UPS03841575.md): Angle · corroded · Nov 25, 2003 · N748UP · Doug DC871F · Flight Compartment Windows
  > WINDOW FRAME ZEE CHANNEL LT LWR CORNER PITTED AND CORRODED. REMOVED AND INSTALLED NEW ZEE ANGLE IAW UPS EO DC8-5330-19614-A. FERRY TO GSO FOR REPAIR REFERENCE GSO NRC 632693
- [SDR UPS03841229](https://openairdocs.org/sdr/UPS03841229.md): Battery Pack · discharged · Sep 14, 2003 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH LEFT IN ARMED POS. BATTERY PACK DEAD. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. NOW OPS OK.
- [SDR UPS03840975](https://openairdocs.org/sdr/UPS03840975.md): Hinge Pin · out of adjust · Jul 11, 2003 · N748UP · Doug DC871F · Flight Compartment Windows
  > INSPECTION TYPE: PFLT, F/O'S COCKPIT WINDOW WILL NOT OPEN PROPERLY. *SUPPLEMENTAL MRR* T/S TO AFT WINDOW HINGE PIN OUT OF PLACE. REINSTALLED AFT HINGE PIN. PERFORMED ADJ, TEST ALL CKS GOOD.
- [SDR UPS03840275](https://openairdocs.org/sdr/UPS03840275.md): Switch · inoperative · Mar 11, 2003 · N748UP · Doug DC871F · Door Warning System
  > DOORS NOT LATCHED LIGHT ILLUMINATED REMAINED ON AFTER GEAR RETRACTION (LEFT GEAR DOOR). RECYCLED GEAR, BROUGHT FLAPS TO 10 DEG, LIGHT EXTINGUISHED. BROUGHT FLAPS UP, RESUMED NORMAL FLIGHT. CHECKS OK ON GROUND. REMOVED AND REPLACED LEFT ALT GEAR DOOR SWITCH
- [SDR UPS02839869](https://openairdocs.org/sdr/UPS02839869.md): Battery · discharged · Nov 5, 2002 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHEN SWITCH PLACED IN ARM POS AND BAT/EXT POWER SWITCH IN BAT FAILS TEST REF PS CHK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT, OPS CHK GOOD REF 33-50-02.
- [SDR UPS02839106](https://openairdocs.org/sdr/UPS02839106.md): Bulkhead · damaged · Aug 13, 2002 · N748UP · Doug DC871F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:LNSV NLG BULKHEAD DAMAGED. TRIMMED OUT DAMAGE ON BULKHEAD IAW REO G08732. DYE PENETRANT CHECKED FOR CRACKS, NONE NOTED. FABRICATED NEW STIFFENER, FILLERS, TRIPLER, AND FINGER DOUBLER PER DAC DWG 5615530 & REO G08732. INSTALLED IAW REO G0873
- [SDR UPS02839075](https://openairdocs.org/sdr/UPS02839075.md): Mount · broken · Aug 13, 2002 · N748UP · Doug DC871F · Landing Gear Actuator
  > INSPECTION TYPE:N/A ATB - NLG RETRACT CYLINDER AFT MOUNT ASSY BROKE CAUSING DAMAGE TO FUSELAGE SKIN. A/C FERRIED TO TCO FOR REPAIR 9150. TRIMMED DAMAGE ON BULKHEAD IAW REO G08732 STEP NR 1, DYE PENETRATE INSP IAW MIL-271F, NO CRACK NOTED IN CUTOUT. FABBED,
- [SDR UPS02837902](https://openairdocs.org/sdr/UPS02837902.md): Doubler · cracked · Mar 1, 2002 · N748UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C23 MOULD-LINE DOUBLER AT NR 1 PYLON HAS PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE I/B SIDE THATS CRACKED AT FASTENER HOLE. REMOVED DOUBLER, PERFORMED HFEC AND BOLT HAVE HFEC IAW NDT SPM 06-10.001 AND 06-10.003. CRACKS PRESENT IN 5 EA HOLES,
- [SDR UPS02837884](https://openairdocs.org/sdr/UPS02837884.md): Web · cracked · Mar 1, 2002 · N748UP · Doug DC871F · Trailing Edge Flaps
  > INSPECTION TYPE:C23 RG I/B FLAP CLOSEOUT WEB CRACKED AROUND BEADED AREA. REMOVED AND REPLACED IAW REO G08529.
- [SDR UPS02837824](https://openairdocs.org/sdr/UPS02837824.md): Web · cracked · Mar 1, 2002 · N748UP · Doug DC871F · Trailing Edge Flaps
  > INSPECTION TYPE:C23 LT WING I/B FLAP I/B END CLOSEOUT WEB IS CRACKED AND HAS LOOSE FASTENERS. REMOVED AND REPLACED WEB IAW REO G08529.
- [SDR UPS02837889](https://openairdocs.org/sdr/UPS02837889.md): Fitting · corroded · Feb 28, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C23 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CORRODED. REMOVED CORRODED ANGLE LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED ZEE FITTING REPAIR ANGLE IAW DC8 SRM 51-1-20D.
- [SDR UPS02837775](https://openairdocs.org/sdr/UPS02837775.md): Fitting · cracked · Feb 26, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED I/B OF L34R AT STA 1200. INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0.
- [SDR UPS02837888](https://openairdocs.org/sdr/UPS02837888.md): Skin Panel · cracked · Feb 21, 2002 · N748UP · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:C23 LT HORIZONTAL STAB UPPER O/B FWD SKIN PANEL CRACKED AT 2ND BOLT IN AFT DIRECTION. REMOVED AND REPLACED HORIZ STAB PLANK IAW DAC SB55-16 AND DAC DWG SRO 8 550001.
- [SDR UPS02837887](https://openairdocs.org/sdr/UPS02837887.md): Door Frame · cracked · Feb 21, 2002 · N748UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C23 L2 DOOR CORNER UPPER AFT SHOWS CRACK INDICATION IN REPAIR AREA GOING TO FASTENER HOLE. REMOVED EXISTING DOUBLERS, ROUTED OUT CRACK, FABBED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 18.
- [SDR UPS02837886](https://openairdocs.org/sdr/UPS02837886.md): Fitting · cracked · Feb 20, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L34R AT STA 1180. REMOVED CRACK Z-FITTING, LOCATED AND DRILLED NEW FITTING AND SPLICES IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0 AND 51-120D.
- [SDR UPS02837885](https://openairdocs.org/sdr/UPS02837885.md): Floorbeam · corroded · Feb 20, 2002 · N748UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C23 AFT PIT LT TUNNEL CORR ON BOTTOM OF CABIN FLOORBEAM UPPER FWD FLANGE AT STA 1240 LBL 62. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED IAW DC8 SRM.
- [SDR UPS02837774](https://openairdocs.org/sdr/UPS02837774.md): Fitting · cracked · Feb 20, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L35R STA 1180. REMOVED CRACKED FITTING, FABBED SPLICES FOR FITTING REPAIR AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 53-2-0 NOTE 17.
- [SDR UPS02837751](https://openairdocs.org/sdr/UPS02837751.md): Fitting · cracked · Feb 20, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B AT L28L STA 1180. REMOVED CRACKED Z-FITTING. INSTALLED FITTING AND SPLICES IAW DC8 SRM 53-2-0.
- [SDR UPS02837883](https://openairdocs.org/sdr/UPS02837883.md): Door Frame · cracked · Feb 18, 2002 · N748UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C23 L1 DOOR CORNER UPPER FWD DOUBLER CONDUCTIVITY TEST SHOWS NOT TO BE ALUMINUM. REMOVED EXISTING DOUBLER, ROUTED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-2-0 FIG 15.
- [SDR UPS01836409](https://openairdocs.org/sdr/UPS01836409.md): Cylinder · lack of lube · Jul 27, 2001 · N748UP · Doug DC871F · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A AIRCRAFT TURNS HARD LEFT DURING TAXI AND T/O. WHEN FLAPS ARE LOWERED ACFT BANKS LEFT 10 DEGREES. VISUALLY INSPECTED FLAP MECHANISM, NO DEFECTS NOTED T/S PER MM 27-50-00. FOUND OUTBOARD LOCK CYLINDER LOW, SERVICED AND BLED PER MM 27-51-10. F
- [SDR UPS01835562](https://openairdocs.org/sdr/UPS01835562.md): Aileron · lack of lube · Apr 11, 2001 · N748UP · Doug DC871F · Aileron Control System
  > AILERONS STIFF. INSPECTED AILERON CONTROL SYSTEM AND FOUND AILERONS IN NEED OF LUBE. LUBRICATED AILERONS IAW 27-10-06 AND PERFORMED AILERON SYS ADJ/TEST IA W MM 27-10-00. AILERONS CHECKED NORMAL OK FOR SERVICE
- [SDR UPS00833787](https://openairdocs.org/sdr/UPS00833787.md): Light · inoperative · Sep 22, 2000 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER MM 33-50-00, CKS NORMAL.
- [SDR UPS00833650](https://openairdocs.org/sdr/UPS00833650.md): Battery Pack · inoperative · Aug 25, 2000 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.
- [SDR UPS00833624](https://openairdocs.org/sdr/UPS00833624.md): Battery Pack · inoperative · Aug 24, 2000 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:P/F, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR UPS00833450](https://openairdocs.org/sdr/UPS00833450.md): Light · inoperative · Jul 30, 2000 · N748UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHTS DO NOT TEST. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-02.

Next page: https://openairdocs.org/deregistered/N748UP-2006-10-06/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 = 'N748UP' AND deregistration_id = 'N748UP-2006-10-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N748UP-2006-10-06/reports

---
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