# Service difficulty reports: N671UP, cancelled Jan 14, 2004

A list on [N671UP, cancelled Jan 14, 2004](https://openairdocs.org/deregistered/N671UP-2004-01-14.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 3 · 114 reports

- [SDR UPS02439975](https://openairdocs.org/sdr/UPS02439975.md): Control Module · malfunctioned · Dec 10, 2002 · N671UP · Boeing 747123 · Central Warning
  > ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. TAKEOFF WARNING HORN SOUNDS WHEN THRUST LEVERS ARE ADVANCED WITH THE FOLLOWING CONDITIONS: FLAPS 20, TRIP 4.9 UNITS. REMOVED AND REPLACED AURAL WARNING CONTROL LOGIC MODULE PER MM -31-26-03
- [SDR UPS02439891](https://openairdocs.org/sdr/UPS02439891.md): Light · inoperative · Nov 7, 2002 · N671UP · Boeing 747123 · Emergency Lighting
  > INSPECTION TYPE: ASV AFT MOST CEILING EMERGENCY LIGHT INOP. REF LP915141. RELAMPED AFT MOST CEILING EMERGENCY LIGHT OPS CHECK GOOD THIS CLEARS M 248535.
- [SDR UPS02439806](https://openairdocs.org/sdr/UPS02439806.md): Light · inoperative · Oct 21, 2002 · N671UP · Boeing 747123F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS IN UPPER DECK DOOR FRAME INOPERATIVE. RELAMPED OPS CK NORMAL
- [SDR UPS02438072](https://openairdocs.org/sdr/UPS02438072.md): Seat Track · cracked · Apr 16, 2002 · N671UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE O/B LEFT SIDE HAS LARGE AMOUNT OF CORROSION ON SEAT TRACK. SEAT TRACK IS ALSO CRACKED. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-05 FIG 5. FABBED NEW SECTIO
- [SDR UPS02438071](https://openairdocs.org/sdr/UPS02438071.md): Attach Fitting · cracked · Apr 16, 2002 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE LOCATED FAR LEFT SIDE IS CRACKED ON I/B UPPER LEG OF FRAME BOTTOM SIDE. REMOVED CRACKED RESTRAINT FITTING IAW SRM 51-30-02. INSTALLED NEW RESTRAINT FITTING IAW SRM 51-
- [SDR UPS02438070](https://openairdocs.org/sdr/UPS02438070.md): Attach Fitting · cracked · Apr 16, 2002 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE IS CRACKED ON LOWER LEG OF FRAME. LOCATED ON 2ND FROM RIGHT ATTACH STRUCTURE. INSTALLED NEW VR ATTACH FITTING IAW 51-30-02.
- [SDR UPS02438069](https://openairdocs.org/sdr/UPS02438069.md): Attach Fitting · cracked · Apr 16, 2002 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:MX FWD LOWER CARGO COMPT POS 5 AFT RT O/B VERTICAL RESTRAINT ATTACH STRUCTURE APPEARS CRACKED AT FWD I/B BOLT HOLE. VERIFIED CRACK WITH HEFC. INSTALLED NEW SUPPORT FITTING IAW SRM 51-30-02.
- [SDR UPS02438032](https://openairdocs.org/sdr/UPS02438032.md): Light · inoperative · Apr 11, 2002 · N671UP · Boeing 747123 · Emergency Lighting
  > INSPECTION TYPE:PFLT MAIN DECK CARGO AFT EMERGENCY EXIT LIGHT IN CEILING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-51-07, OPS CHECK OK.
- [SDR UPS02437413](https://openairdocs.org/sdr/UPS02437413.md): Structure · corroded · Jan 16, 2002 · N671UP · Boeing 747123 · Wing, Center Box
  > INSPECTION TYPE:SP CENTER WING BOX UPPER SKIN HAS EXFOLIATION CORROSION APPROX 4 INCHES IN DIAMETER STA 1110, RBL 104. REPAIRED AREA IAW ENGINEERING FILE 747-57-20016.
- [SDR UPS02437412](https://openairdocs.org/sdr/UPS02437412.md): Angle · cracked · Jan 16, 2002 · N671UP · Boeing 747123F · Wing, Center Box
  > INSPECTION TYPE:SP STA 1140 ON RT SIDE UNDERNEATH SECOND FLOOR PNL, I/B AND BENEATH DUCTING A 2 INCH CRACK WAS FOUND AND CORROSION ON CTR WING BOX.
- [SDR UPS02437386](https://openairdocs.org/sdr/UPS02437386.md): Structure · corroded · Dec 30, 2001 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:IN AT STA 1140 RT UNDERNEATH SECOND FLOOR PANEL I/B BENEATH DUCTING FOUND CRACK AND CORROSION ON CONTROL WING BOX.
- [SDR UPS01435930](https://openairdocs.org/sdr/UPS01435930.md): Rib · cracked · May 11, 2001 · N671UP · Boeing 747123 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION TYPE:C-2, NR 1 PYLON - RESERVOIR LT STRUCTURE RIB CRACK FOUND AS MARKED. NR 1 PYLON HYD RESERVOIR LT RIB REPLACED PER SRM 51-10-01. LEAK CHECKED SATISFACTORY PER MM 29-11-00.
- [SDR UPS01435928](https://openairdocs.org/sdr/UPS01435928.md): Seat Track · corroded · May 11, 2001 · N671UP · Boeing 747123 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C-2 U/D - BS 480-520 RBL 65 SEAT TRACK FOUND HEAVY CORROSION DURING FLOOR COVERING REMOVED. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01.
- [SDR UPS01435906](https://openairdocs.org/sdr/UPS01435906.md): Door Frame · cracked · May 11, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > VINSPECTION TYPE:C-2 M/D - LT BS 1265 FRAME NR 2 DOOR STOP FTG AREA FOUND TWO FASTENER HOLES CRACKED. ONE CRACK AT FRAME INNER CHORD. ANOTHER CRACK AT FRAME WEB. CHORD AND WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E.
- [SDR UPS01435941](https://openairdocs.org/sdr/UPS01435941.md): Trunnion · cracked · May 10, 2001 · N671UP · Boeing 747123 · Nose/Tail Landing Gear Attach Section
  > INSPECTION TYPE:C-2 NLG W/W - LT BS 380 TRUNNION FITTING MOST FWD LOWER HOLE FOUND CRACKED AT 5 O''CLOCK AND 11 O''CLOCK POSITION (LOOKING O/B). THE DISCREPANT CRACK STOP DRILLED, OPEN HOLE HFEC INSP C/O & NLG W/W LT BS 380 TRUNNION FITTING AND FOUND CRACK FR
- [SDR UPS01435960](https://openairdocs.org/sdr/UPS01435960.md): Fitting · cracked · May 9, 2001 · N671UP · Boeing 747123 · Passenger/Crew Doors
  > INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FITTING FOUND CRACKED AT BS 1265 S-23L. STOP FITTING REPLACED AS PER SRM 51-10-01.
- [SDR UPS01435929](https://openairdocs.org/sdr/UPS01435929.md): Stop Fitting · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S3L. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF 069231.
- [SDR UPS01435919](https://openairdocs.org/sdr/UPS01435919.md): Pressure Panel · corroded · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16-28 CANTED PRESS DECK REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS01435918](https://openairdocs.org/sdr/UPS01435918.md): Pressure Panel · corroded · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16 TO 28 CANTED PRESS DECK REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS01435914](https://openairdocs.org/sdr/UPS01435914.md): Splice Plate · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2 NLG W/W STA 400 S-44L SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6, 51-00-00 FIG 1. NIL CRACK FOUND AT AFT HOLES OF PREVIOUS CRACKED HOLE. EXISTING REPAIR DOUBLER REINSTALLED AS PER SRM 51-30-02.
- [SDR UPS01435913](https://openairdocs.org/sdr/UPS01435913.md): Splice Plate · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2 NLG W/W STA 400 S-44R SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6 51-00-00 FIG 1. CRACK FOUND AT AFT HOLE AT SPLICE FITTING, BUT NIL CRACK AFTER AFT HOLE REF SCATCH ON CWS 330869. EXISTING REPAIR DOUBLER REI
- [SDR UPS01435905](https://openairdocs.org/sdr/UPS01435905.md): Frame · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Frame
  > INSPECTION TYPE:C-2 CABIN - RT NR 3 MED CUTOUT FWD FRAME BELOW LOWER STILL FOUND 1 FASTENER HOLE CRACK AT FRAME WEB. WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E.
- [SDR UPS01435904](https://openairdocs.org/sdr/UPS01435904.md): Stop · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S-23L. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF069231.
- [SDR UPS01435903](https://openairdocs.org/sdr/UPS01435903.md): Stop Fitting · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D - R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACK AT NR 5. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF 069341.
- [SDR UPS01435902](https://openairdocs.org/sdr/UPS01435902.md): Stop Fitting · cracked · May 9, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D- R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACKED NR 3. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF069228.
- [SDR UPS01435974](https://openairdocs.org/sdr/UPS01435974.md): Frame · cracked · May 8, 2001 · N671UP · Boeing 747123 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION TYPE:C-2, NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LOWER SPAR FITTING FOUND 1 HOLE CRACK AT 2 O''CLOCK POSITION (LOOKING FWD) APPROX 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LWR SPAR FITTING REPAIRED AS PER HX RS R54-53-3
- [SDR UPS01435940](https://openairdocs.org/sdr/UPS01435940.md): Pressure Panel · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C-2 NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND LOWER STANDOFF HOLE CRACKED APPROX.25 INCH &.375 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01.
- [SDR UPS01435937](https://openairdocs.org/sdr/UPS01435937.md): Pressure Panel · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP (COUNT FROM TOP) FOUND CRACK AT STAND OFF HOLE APPROX.125 INCH LONG. BS 320 LT WEB REPLACED PER SRM 51-10-01 & 51-30-02.
- [SDR UPS01435936](https://openairdocs.org/sdr/UPS01435936.md): Pressure Panel · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C-2 NOSE W/W TUNNEL - RT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP FOUND CRACK AT STANDOFF HOLW APPROX.125 &.0625 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01 & 51-30-02.
- [SDR UPS01435935](https://openairdocs.org/sdr/UPS01435935.md): Pressure Panel · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND CRACK AT LOWER STAND OFF HLE APPROX.375 &.25 INCH LONG. LT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & 51-30-02.
- [SDR UPS01435901](https://openairdocs.org/sdr/UPS01435901.md): Door Frame · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D L3 DR FWD CUTOUT LWR CORNER REVEAL FOUND CRACKED. LWR CORNER REVEAL FTG REPLACED IAW SRM 51-10-01 WITH HX S/TAG FF069254.
- [SDR UPS01435898](https://openairdocs.org/sdr/UPS01435898.md): Skin · cracked · May 8, 2001 · N671UP · Boeing 747123 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 EMP - RT UPPER FUSELAGE SKIN FOUND CRACKED AT STA 2654 TO STA 2658 WL 314 STR 9R (AS MARK). EMP - RT UPPER FUSELAGE SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.
- [SDR UPS01435963](https://openairdocs.org/sdr/UPS01435963.md): Doubler · cracked · May 7, 2001 · N671UP · Boeing 747123 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-2 M/D - L5 DOOR FWD CUTOUT UPPER REVEAL DOUBLER FOUND CRACKED AT BS 2230 STR 15-16. DOUBLER REPLACED AS PER SRM 51-10-01.
- [SDR UPS01435962](https://openairdocs.org/sdr/UPS01435962.md): Shear Tie · cracked · May 7, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 FWD CARGO COMPT AFT BHD BS 1000 RBL 34 UPPER EDGE SHEAR TIE CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01.
- [SDR UPS01435916](https://openairdocs.org/sdr/UPS01435916.md): Panel · cracked · May 7, 2001 · N671UP · Boeing 747123 · Passenger Compartment Equipment
  > INSPECTION TYPE:C-2 M/D - L3 DR FWD CUTOUT UPPER REVEAL CRACKED AT LWR EDGE AREA. REVEAL PANEL REPLACED AS PER SRM 51-10-01.
- [SDR UPS01435911](https://openairdocs.org/sdr/UPS01435911.md): Support · corroded · May 6, 2001 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 920 RBL 60 - LBL 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 920 LBL 60 TO RBL 60 PER SRM 53-50-04 FIG 2.
- [SDR UPS01435910](https://openairdocs.org/sdr/UPS01435910.md): Support · corroded · May 6, 2001 · N671UP · Boeing 747123 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 880 RBL 0 - 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 880 BL 0 TO RBL 40 PER SRM 53-50-04 FIG 2.
- [SDR UPS01435900](https://openairdocs.org/sdr/UPS01435900.md): Door Frame · cracked · May 4, 2001 · N671UP · Boeing 747123 · Fuselage Main, Structure
  > INSPECTION TYPE:C-2 M/D -L3 DOOR FWD CUTOUT REVEAL FOUND CRACKED AT NR 3 TO 4 STOP FITTING AREA AS MARK. REVEAL PANEL REPLACED IAW SRM 51-10-01 WITH HX S/TAG FF069197.
- [SDR UPS01435032](https://openairdocs.org/sdr/UPS01435032.md): Computer · malfunctioned · Feb 21, 2001 · N671UP · Boeing 747123 · Autopilot System
  > INSPECTION TYPE:N/A, WHILE CLIMBING THRU FL 345 TO FL 350 (500 FT TO GO), AT 500 FT PER MINUTE THE A-AUTOPILOT PITCHED UP TO CAPTURE THE ALTITUDE WITH A 1500 TO 2000 FPM CLIMB. CREW HAD TO INTERCEDE TO PREVENT OVERSHOOT IN RVSM AIRSPACE. RESEATED A A/P PITCH
- [SDR UPS01434754](https://openairdocs.org/sdr/UPS01434754.md): Thrust Reverser · failed · Jan 25, 2001 · N671UP · Boeing 747123 · Engine Thrust Reverser
  > INSPECTION TYPE:IN PIREP NR 4 THRUST REVERSER FAILED TO DEPLOY. REMOVED AND REPLACED NR 4 T/R PDU PER MM 78-31-01 AND INSTALLED NEW FLEX SHAFT PER MM 78-31-02, OPS TEST OK PER MM 78-31-00. S/N ON P-2527, SHAFT P/N ON 121652-1. CLEARED M208055, REMOVED PLACA
- [SDR UPS00434522](https://openairdocs.org/sdr/UPS00434522.md): Frame · cracked · Dec 2, 2000 · N671UP · Boeing 747123F · Fuselage Main, Frame
  > INSPECTION TYPE:N/A L/H BODY GEAR THE FLYING DOOR FRAME IS SEPARATING FROM AIRCRAFT FRAM E ***SUPPLEMENTAL MRR*** INSTALLED REPAIR DOUBLER ON AFT END OF FRAME PER SRM 51-40-03.
- [SDR UPS00434396](https://openairdocs.org/sdr/UPS00434396.md): Harness · damaged · Nov 2, 2000 · N671UP · Boeing 747123 · Air Data Computer
  > INSPECTION TYPE:N/A, INS PWR RELAY NR 3 POPPED C/B. INS ASHU NR 3 POPPED C/B. ALT INS NR 3 POPPED C/B. NR 3 INS WARN LIGHT CAME ON. NR 2 AFT AND NR 3 FWD BOOST PUMP C/B POPPED. INSTRUMENT SWITCHING PROBLEM. *S/D* REPAIRED WIRE BUNDLE W84 AND REPLACED
- [SDR UPS00433789](https://openairdocs.org/sdr/UPS00433789.md): Light · inoperative · Sep 23, 2000 · N671UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:N/A REF M199323, EMERGENCY LIGHT ON CEILING AFT OF P6 C/B PNL INOP IN TEST. TROUBLESHOOTING PER WDM 33-51-12 PG 1, FOUND OPEN CIRCUIT AT CONNECT OR DX328 PIN 4. REPAIRED AND OPERATION TEST PER MM 33-51-00, OK. CLEARED AND REMOVED PLACARD.
- [SDR UPS00433790](https://openairdocs.org/sdr/UPS00433790.md): Light · inoperative · Sep 22, 2000 · N671UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT OVER UPPER RIGHT ESCAPE DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-04, OPS CHECK GOOD.
- [SDR UPS00432626](https://openairdocs.org/sdr/UPS00432626.md): Battery Pack · inoperative · May 14, 2000 · N671UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:N/A, UPPER DECK CREW EVAC DOOR AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM 33-51-04, OPS CK OK.
- [SDR UPS00431882](https://openairdocs.org/sdr/UPS00431882.md): Torque Tube · disconnected · Mar 6, 2000 · N671UP · Boeing 747123F · Trailing Flap Position Indicating System
  > AIR TURN BACK TO OAK, DUE TO R/T INBD FLAP INOP AT 1 DEGREE POSITION. FOUND RIGHT INBD FLAP TORQUE TUBE COUPLING DISCONNECTED. SECURED COUPLING, SAFETIED AND RIGGED IAW MM 27-51-01. GROUND FLAP OPERATION AND COCKPIT INDICATION CHECKS NORMAL.
- [SDR UPS00431381](https://openairdocs.org/sdr/UPS00431381.md): Light · failed · Jan 22, 2000 · N671UP · Boeing 747123F · Emergency Lighting
  > INSPECTION TYPE:W/E AT L1 CREW ENTRY DOOR THE FWD CIRCULAR AND RECTANGULAR EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK FOR FWD L1 DOOR EMERGENCY LIGHTS, SYSTEM OPS CHECK OK.
- [SDR UPS99430614](https://openairdocs.org/sdr/UPS99430614.md): Panel · cracked · Sep 12, 1999 · N671UP · Boeing 747123 · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:N/A, APPROX 11 INCH CRACK ON NR 3 PYLON I/B SIDE FWD OF LOWER ACCESS PANEL. PERFORM CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING LETTER 99-00318H. *S/D* COMPLISHED CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING REQUEST LETTER 99-00
- [SDR UPS99430416](https://openairdocs.org/sdr/UPS99430416.md): Retract Mech · lack of lube · Aug 22, 1999 · N671UP · Boeing 747123 · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A, UPON THE SECOND DEPARTURE THE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION. COMPLETED CHECKLIST AND RETURNED TO KIX. BOTH PRIMARY AND ALT AGREE. ***REFERENCE UPS99430415 FOR REPEAT WRITE-UP*** JA
- [SDR UPS99430415](https://openairdocs.org/sdr/UPS99430415.md): Retract Mech · malfunctioned · Aug 22, 1999 · N671UP · Boeing 747123 · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A, UPON DEPARTURE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION. CREW COMPLETED CHECKLIST AND RETURNE D TO KIX. ***REFERENCE UPS99430416 FOR REPEAT WRITE-UP*** INSPECTED ALL LANDING GEAR, NO DEFECTS F

Next page: https://openairdocs.org/deregistered/N671UP-2004-01-14/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 = 'N671UP' AND deregistration_id = 'N671UP-2004-01-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N671UP-2004-01-14/reports

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