# Service difficulty reports: N931UP, cancelled Aug 23, 2006

A list on [N931UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N931UP-2006-08-23.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 · 131 reports

- [SDR UPS01237368](https://openairdocs.org/sdr/UPS01237368.md): Light · inoperative · Dec 7, 2001 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT IN COCKPIT INOP HGT SPARE PREFLIGHT. EMERGENCY EXIT LIGHT IN COCKPIT CHARGED AND OPERATIONAL PER 33-50, OPS CHECK GOOD OK FOR SERVICE.
- [SDR UPS01236098](https://openairdocs.org/sdr/UPS01236098.md): Fire Loop · contaminated · Jun 14, 2001 · N931UP · Boeing 72725C · Fire Detection
  > INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT AND BELL CAME ON ON APPROACH AT APPROX 3000 FT MSL WHEN GEAR EXTENDED, LIGHT EXTINGUISHED. NO APPARENT DAMAGE OR PROBLEMS ON LANDING. INSPECTED ALL WHEEL WELL FIRE LOOPS FOR GROUNDS. FOUND CONTAMINATION IN THE NOSE
- [SDR UPS01235893](https://openairdocs.org/sdr/UPS01235893.md): Door Seal · torn · May 15, 2001 · N931UP · Boeing 72725C · Passenger/Crew Doors
  > INSPECTION TYPE:N/A PILOT REPORT-AT 5000 FT LOST CABIN PRESSURIZATION REPAIRED MAIN ENTRY DOOR SEAL
- [SDR UPS01235292](https://openairdocs.org/sdr/UPS01235292.md): Contactor · corroded · Mar 16, 2001 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:PFLT PRE FLT - EMER EXIT LIGHT FWD ENTRY W/N STAY ILLUM. REMOVED LIGHT ASSY AFTER INSPECTION FOUND BATTERY CONTACTS TO HAVE LIGHT CORROSION. CLEANED CONTACTS, AND RE-LAMPED LIGHT ASSY, RE-INSTALLED OPS GOOD REF M/M 33-50-101.
- [SDR UPS01234577](https://openairdocs.org/sdr/UPS01234577.md): Bulb · malfunctioned · Jan 1, 2001 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A COCKPIT DOOR EMERGENCY EXIT LIGHT HAS ONE DIM BULB RELAMPED EMER. LIGHT OVER FLIGHT DECK ENTRY DOOR, OPS CHECK GOOD
- [SDR UPS00233533](https://openairdocs.org/sdr/UPS00233533.md): Stringer · corroded · Jul 26, 2000 · N931UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, STRINGER END 22L CORRODED BETWEEN BS 348.2 AND BS 360. INSTALLED NEW STRINGER SECTION, (P/N 65-18420-269) AND TIE FITTING (P/N 65-29876-7), IAW SRM 51-30-2.
- [SDR UPS00233531](https://openairdocs.org/sdr/UPS00233531.md): Seat Track · broken · Jul 25, 2000 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, AFT CARGO COMPARTMENT SEAT TRACK TONGUE BROKEN BETWEEN BS 1148 AND BS 1166 NEAR STRINGER 28 LEFT. REPLACED SECTION OF SEAT TRACK FROM STA 1063L TO STA 1166L. MATERIAL USED, P/N BAC 1520-843, SPLICE MAT 7075-T6, 0.250,.75 X 24 7 075-T6, 1.
- [SDR UPS00233529](https://openairdocs.org/sdr/UPS00233529.md): Seat Track · broken · Jul 19, 2000 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, FUSELAGE STATION 541, LBL 62.75, CARGO TRACK HAS 1 BROKEN TONGUE. REPLACED SECTION OF SEAT TRACK FROM BS 445 - 550, LBL 62.75 IAW SRM 53-10-5 FIG 7 MATERIAL USED P/N BAC 1520-1433.
- [SDR UPS00233528](https://openairdocs.org/sdr/UPS00233528.md): Seat Track · broken · Jul 19, 2000 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, FUSELAGE STATION 517, RBL 0.5 SEAT TRACK IS BROKEN (BROKEN TONGUE). REPLACED SECTION OF SEAT TRACK FROM STA 490 TO STA 550, RBL 0.5, MATERIAL USED, P/N BAC 1520-1331, 5 IAW SRM 53-10-5.
- [SDR UPS00233527](https://openairdocs.org/sdr/UPS00233527.md): Seat Track · deformed · Jul 19, 2000 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, FUSELAGE STATION 940, RBL 45.5, SEAT TRACK HAS 1 ELONGATED HOLE, DEFORMED TONGUE. REPLACED SECTION OF SEAT TRACK FROM BS 870 - BS 1000. MATERIAL USED, P/N BAC1520-1434, SIZE 12'' IAW B727 SRM 53-10-5 FIG 7.
- [SDR UPS00233366](https://openairdocs.org/sdr/UPS00233366.md): Drag Brace · inoperative · Jul 14, 2000 · N931UP · Boeing 72725C · Nose/Tail Landing Gear
  > INSPECTION TYPE:N/A, NOSE GEAR DID NOT EXTEND ON INITIAL TRY. FERRY PERMIT (9137) ISSUED AND SENT TO PRF, DURING INSP MX FOUND DURING GEAR EXTENSION, NOSE GEAR DELAYED SEVERAL SECONDS AND SOUNDED LIKE IT FREE FELL OR HUNG UP ON NOSE GEAR DOORS WITH A RESOUNDI
- [SDR UPS99228757](https://openairdocs.org/sdr/UPS99228757.md): Fitting · corroded · Feb 21, 1999 · N931UP · Boeing 72725C · Wing, Control Surface Attach Fittings
  > INSPECTION TYPE-C, NR 4 FLAP TRACK FORWARD MOUNT FITTING HAS CORROSION IN MOUNT HOLE BORES. NR 4 FLAP TRACK FITTING WAS REPLACED IAW OHM 20-50-01 PG 1 PARA 2 AND TABLE 1 AND M/M 27-51-31 PARA D8, ON NRC 879844.
- [SDR UPS99228743](https://openairdocs.org/sdr/UPS99228743.md): Stringer · cracked · Feb 16, 1999 · N931UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C WHILE WORKING (EO B727-5310-5474) DISCOVERED CRACK IN STRINGER 17 LT BS 850 BL 70.5 WL 208. INSTALLED RADIUS FILLERS BS 848-TO BS 856 AND FABRICATED AND INSTALLED INTERCOSTAL BS 848 TO 870 PER 727 SRM 51-30-2, 51-40-4 AND 51-20-4.
- [SDR UPS99228756](https://openairdocs.org/sdr/UPS99228756.md): Fitting · cracked · Feb 9, 1999 · N931UP · Boeing 72725C · Wing, Landing Gear Attach Fittings
  > INSPECTION TYPE-C, LT MLG FWD TRUNNION AFT SPAR SUPPORT CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING PER SRM 51-30-1, AND DWG 65-19297.
- [SDR UPS99228758](https://openairdocs.org/sdr/UPS99228758.md): Trunnion · cracked · Feb 8, 1999 · N931UP · Boeing 72725C · Main Landing Gear Attach Section
  > INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51.
- [SDR UPS99228755](https://openairdocs.org/sdr/UPS99228755.md): Trunnion · cracked · Feb 8, 1999 · N931UP · Boeing 72725C · Main Landing Gear Attach Section
  > INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51.
- [SDR UPS99228718](https://openairdocs.org/sdr/UPS99228718.md): Fitting · corroded · Feb 8, 1999 · N931UP · Boeing 72725C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C, TORQUE TUBE SUPPORT FITTING JUST O/B OF MAIN LANDING GEAR BEAM CORRODED AT INBD AND OTBD LOWER FASTENERS HOLES. REMOVED AND REPLACED L/WING O/B FLAP TORQUE TUBE SUPPORT FITTING IAW MM 27-51-131.
- [SDR UPS98227907](https://openairdocs.org/sdr/UPS98227907.md): Light · inoperative · Oct 15, 1998 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT INTERMITTENTLY FLASHES ON AND OFF WITH SWITCH IN ARM POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK NORMAL.
- [SDR UPS98227251](https://openairdocs.org/sdr/UPS98227251.md): Battery · discharged · Jul 28, 1998 · N931UP · Boeing 72725C · Emergency Lighting
  > ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OP'S CHK'S GOOD.
- [SDR UPS98226342](https://openairdocs.org/sdr/UPS98226342.md): Light · inoperative · Apr 9, 1998 · N931UP · Boeing 72725C · Emergency Lighting
  > FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPS IS INTERMINT AND BACK COVER IS MISSING. REMOVED AND REPLACED FWD ENTRY DOOR EMERG EXIT LIGHT ASSY PER M/M 33-50-01. OPS CHECK GOOD. OK FOR SERVICE. P/N: 10-0067-9,S/N OFF UNKNOWN S/N:ON 13697.
- [SDR UPS98226339](https://openairdocs.org/sdr/UPS98226339.md): Light · inoperative · Apr 8, 1998 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPERATION IS INTERMITTENT AND BACK COVER IS MISSING. REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY AS PER M/M 33-50-01, OP'S CHECKS GOOD.
- [SDR UPS98225395](https://openairdocs.org/sdr/UPS98225395.md): Light · malfunctioned · Jan 8, 1998 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, COCKPIT EXIT LIGHT CAME ON AFTER LANDING WITH SWITCH IN OFF. SECURED COCKPIT EMER EXIT LIGHT, OPERATION OK.
- [SDR UPS97224566](https://openairdocs.org/sdr/UPS97224566.md): Light · malfunctioned · Oct 1, 1997 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR ON WITH SWITCH IN ARMED POSITION. CYCLED SWITCH, OPS CKS GOOD.
- [SDR UPS97224538](https://openairdocs.org/sdr/UPS97224538.md): Light · inoperative · Sep 29, 1997 · N931UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A ON DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT, OPS GOOD.
- [SDR UPS97224520](https://openairdocs.org/sdr/UPS97224520.md): Light · inoperative · Sep 25, 1997 · N931UP · Boeing 72725C · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN TESTED. RESEATED EMERGENCY LIGHT ASSEMBLY OPS CK NML.
- [SDR UPS97224287](https://openairdocs.org/sdr/UPS97224287.md): Fitting · cracked · Aug 23, 1997 · N931UP · Boeing 72725C · Landing Gear Doors
  > INSPECTION TYPE:C RT MLG WING DOOR ATTACH FITTING CRACKED. FITTING REPLACED IAW EO B727-3210-2583F APP D.
- [SDR UPS97224284](https://openairdocs.org/sdr/UPS97224284.md): Pressure Web · cracked · Aug 19, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACKS CONFIRMED AT BS 242 WL 168 AND BS 282 WL 172 LT NOSE WHEEL WELL PRESSURE WEB. PRESSURE WEB REPLACED IAW DRG 65-18414.
- [SDR UPS97224283](https://openairdocs.org/sdr/UPS97224283.md): Pressure Web · cracked · Aug 19, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK CONFIRMED AT BS 282 WL 172 RT NOSE WHEEL WELL PRESSURE WEB PRESSURE WEB REPLACED IAW DRG 65-18414.
- [SDR UPS97224286](https://openairdocs.org/sdr/UPS97224286.md): Bracket · cracked · Aug 18, 1997 · N931UP · Boeing 72725C · Engine Cranking
  > INSPECTION TYPE:C PULLEY BRACKET FOR NR 2 ENG START CABLES BS 1260 CRACKED. PULLEY BRACKET REPLACED IAW MM 20-80-01.
- [SDR UPS97224282](https://openairdocs.org/sdr/UPS97224282.md): Chord · corroded · Aug 18, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LOWER AFT CARGO COMPARTMENT AT BS 1080 EYE BEAM HAS SOME SURFACE CORROSION. LOWER AFT CARGO COMPARTMENT CHORD REPLACED IAW SRM 53-10-2 FIG 7 AN D 51-10-5.
- [SDR UPS97224281](https://openairdocs.org/sdr/UPS97224281.md): Eye End · worn · Aug 18, 1997 · N931UP · Boeing 72725C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:C LT MLG MANUAL EXTENSION UPLOCK RELEASE SHAFT PUSHROD EYE ENDS WORN EYE ENDS REPLACED IAW MM 32-34-0.
- [SDR UPS97224280](https://openairdocs.org/sdr/UPS97224280.md): Chord · corroded · Aug 18, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SURFACE CORROSION ON LOWER CHORD OF LONGITUDINAL I MEMBEER FWD CARGO COMPT CEILING BS 594 BBL 0. REPAIR CARRIED OUT IAW SRS EO 97-20-003 UPS ENG FILE NUMBER 727-53-1 957.
- [SDR UPS97224295](https://openairdocs.org/sdr/UPS97224295.md): Hinge Bracket · cracked · Aug 17, 1997 · N931UP · Boeing 72725C · Landing Gear Doors
  > INSPECTION TYPE-C, LT I/B FLAP TRACK- AFT HINGE BRACKET ON FLAP TRACK FOR LT MLG WING DOOR IS CRACKED. REPLACED HINGE BRACKET IAW SRM 51-30-2.
- [SDR UPS97224285](https://openairdocs.org/sdr/UPS97224285.md): Skin · cracked · Aug 16, 1997 · N931UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE:C SKIN ON LOWER AFT CARGO DOOR AREA BLENDED OUT AT BS 1060 LOWER EDGE SIX INCHES IN FROM REAR EDGE HAS A CRACK. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
- [SDR UPS97224297](https://openairdocs.org/sdr/UPS97224297.md): Bracket · corroded · Aug 15, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION ON FLOOR BRACKET BETWEEN STN 294.5 AND STN 312 LBL 14.00. CORRODED BRACKET REMOVED AND FOUND TO BE OUTSIDE LIMITS OF SRM 51-10 -6. NEW BRACKET FABRICATED FROM 7075 T0 0.040 INCH AND HT TO T6 REF HT NR 97-20-03 AND SRM 51-20-1. B
- [SDR UPS97224274](https://openairdocs.org/sdr/UPS97224274.md): Channel · cracked · Aug 15, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CHANNEL SECTION BETWEEN BS 520 AND BS 540 RBL 17 IN FWD CARGO IS CRACKED. REPLACED CHANNEL SECTION IAW SRM 51-30-2 AND SRM 51-10-1.
- [SDR UPS97224273](https://openairdocs.org/sdr/UPS97224273.md): Door · dented · Aug 15, 1997 · N931UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE-C, DAMAGE TO FWD LOWER CARGO DOOR BOTTOM EDGE FIVE INCHES FWD FROM AFT EDGE STA 570 RT. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
- [SDR UPS97224269](https://openairdocs.org/sdr/UPS97224269.md): Pressure Panel · corroded · Aug 15, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, SURFACE CORROSION ON LT PRESSURE PANEL NLG WHEEL WELL CEILING. REPLACED DOME PANEL IAW SRM 51-10-1.
- [SDR UPS97224267](https://openairdocs.org/sdr/UPS97224267.md): Fitting · cracked · Aug 15, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE FRAME FITTING BS 740 LT BETWEEN S19L AND S2 0L. REPAIRED IAW UPS EO B727-5310-7497.
- [SDR UPS97224266](https://openairdocs.org/sdr/UPS97224266.md): Fitting · cracked · Aug 15, 1997 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CRACKS FOUND ON FUSELAGE FRAME FITTING BS 740 RT BETWEEN S18R AND 19R, S19R AND S20R, S23R AND S24R. FRAME REPAIRED IAW UPS EO B727-5310-7497.
- [SDR UPS97224279](https://openairdocs.org/sdr/UPS97224279.md): Skin · dented · Aug 14, 1997 · N931UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE:C LOWER AFT CARGO DOOR, AREA DRESSED OUT AT BS 1057 S24R OUTSIDE LIMITS AS PER SRM 52-00-2. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
- [SDR UPS97224278](https://openairdocs.org/sdr/UPS97224278.md): Skin · dented · Aug 14, 1997 · N931UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE:C LOWER AFT CARGO DOOR, AREA DRESSED OUT AT BS 1083 S19R OUTSIDE LIMITS AS PER SRM 52-00-2. CARRIED OUT REPAIR IAW SRM 52-00-3 FIG 4.
- [SDR UPS96221138](https://openairdocs.org/sdr/UPS96221138.md): Circuit Breaker · tripped · Sep 19, 1996 · N931UP · Boeing 72725C · Altimeter, Barometric/Encoder
  > INSPECTION TYPE-N/A, AFTER TAKEOFF ENTIRE CREW NOTED A STRONG ODOR IN COCKPIT RESEMBLING ELECTRICAL SMOKE. FOUND STBY ALT/AS CB POPPED, ODOR STOPPED. DID NOT ATTEMPT TO RESET CB. PERFORMED OPS CHK ON STBY ALT/AS IND PER MM 34-12-06 PG 501, SYS OPS CHK G
- [SDR UPS96220664](https://openairdocs.org/sdr/UPS96220664.md): Sense Wires · chafed · Jul 24, 1996 · N931UP · Boeing 72725C · Overheat Detection
  > NR 1 ENGINE STRUT OVERHEAT FLICKERED TWICE DURING CRUISE. FOUND STRUT DETECTOR WIRES WITH MINOR SIGNS OF CHAFING. CORRECTED ALL CHAFING AREAS. SYSTEM CHECKS NORMAL. OK FOR SERVICE.
- [SDR UPS96205661](https://openairdocs.org/sdr/UPS96205661.md): Light · inoperative · Mar 10, 1996 · N931UP · Boeing 72725C · Emergency Lighting
  > MAINTENANCE REPORTED EMERGENCY LIGHT IN COCKPIT FAILED. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.
- [SDR UPS205608](https://openairdocs.org/sdr/UPS205608.md): Stringer · corroded · Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRINGER 18A LT HAS NO EDGE DISTANCE AT STA 940, DUE TO CORROSION IN FASTENER HOLES. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EWO 96-2090.
- [SDR UPS205607](https://openairdocs.org/sdr/UPS205607.md): Forging · cracked · Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WHILE WORKING FUSELAGE CUST NR 433165, FOUND A CRACK ON THE BS 950 FORGING AT THE FWD SIDE OF PRESSURE WEB ATTACH FITTING. DRILLED CRACK AND VERIFIED CRACK CONTAINMENT, INSTALLED NEW FITTING AND REPAIRED IAW EO 96-20
- [SDR UPS205606](https://openairdocs.org/sdr/UPS205606.md): Floorbeam · corroded · Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor Beam
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER FLANGE BS 1110 RBL 50 TO 56 LBL 3 TO 20 AND 40 TO 44. REMOVED CORROSION, OUT OF LIMITS REPAIRED PER EWO 96-2087.
- [SDR UPS205605](https://openairdocs.org/sdr/UPS205605.md): Skin · corroded · Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN BS 640 TO 660 BETWEEN STR 2 TO 3 LT. REMOVED CORROSION, OUT OF LIMITS PER SRM 53-30-2 FABRICATED REPAIR PARTS AND INSTALLED IAW 96-2089.
- [SDR UPS205604](https://openairdocs.org/sdr/UPS205604.md): Forging · cracked · Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT AFT 870 TERMINAL FORGING IS CRACKED AT BS 870 WL 188 LBL 67. REMOVED CRACKED AREA AND NDT VERIFIED CRACK CONTAINMENT, REPAIRED IAW EO 96-2060.

Next page: https://openairdocs.org/deregistered/N931UP-2006-08-23/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 = 'N931UP' AND deregistration_id = 'N931UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N931UP-2006-08-23/reports

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