# Service difficulty reports: N948UP, cancelled Dec 18, 2006

A list on [N948UP, cancelled Dec 18, 2006](https://openairdocs.org/deregistered/N948UP-2006-12-18.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 · 143 reports

- [SDR UPS05244037](https://openairdocs.org/sdr/UPS05244037.md): Forging · cracked · Jan 5, 2005 · N948UP · Boeing 72725C · Vertical Stabilizer
  > INSPECTION TYPE: SV, RIGHT VERTICAL FIN FRONT SPAR LWR FORGING. A 2 INCH VISIBLE CRACK IN FORGING STA 1229-1231. CRACK IN RADIUS AREA OF STRAP 1.75 X.25 INCH. REPAIRED LEFT AND RIGHT VERTICAL STAB FRONT SPAR FORGING FOR FERRY FLIGHT STA 1229 - 1231 IAW UPS
- [SDR UPS04243324](https://openairdocs.org/sdr/UPS04243324.md): Battery · inoperative · Oct 7, 2004 · N948UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, NO HELP. REMOVED AND REPLACED EMERGENCY EXIT ASSY & NEW BATTERIES INSTALLED. OPS CHECK OK.
- [SDR UPS04243082](https://openairdocs.org/sdr/UPS04243082.md): Light · inoperative · Sep 3, 2004 · N948UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHTING INOP AT L1 EXIT DOOR. REPLACED EMERGENCY EXIT LIGHT ASSY AT L1 DOOR PER MM 33-50-01, OPS CHECK GOOD.
- [SDR UPS04242664](https://openairdocs.org/sdr/UPS04242664.md): Intercostal · corroded · Jun 24, 2004 · N948UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SUPPORT INTERCOSTAL FOR LWR CENTER LINE FAIRING CORRODED AT BS 740 BETWEEN S28L AND S28R. INTERCOSTAL REPLACED WITH FABRICATED INTERCOSTAL IAW SRM 51-30-02 AND 51-20-2.
- [SDR UPS04242678](https://openairdocs.org/sdr/UPS04242678.md): Floor Support · corroded · Jun 23, 2004 · N948UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, AFT CARGO FLOOR SUPPORT RAIL AT BS 1035 RBL 4 APPROX, CORRODED. SECTION OF FLOOR SUPPORT RAIL REPLACED IAW SRM 53-10-5 & DRAWING 65-19 388.
- [SDR UPS04242669](https://openairdocs.org/sdr/UPS04242669.md): Angle · cracked · Jun 23, 2004 · N948UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51-20-01 FIG 7 AND BOEING DRG 65-26786.
- [SDR UPS04242668](https://openairdocs.org/sdr/UPS04242668.md): Clip · cracked · Jun 23, 2004 · N948UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SUPPORT CLIP FOUND CRACKED AT BS 580 BETWEEN S2L AND S3L. SUPPORT CLIP FABRICATED AND INSTALLED IAW 51-20-01 AND 51-30-2.
- [SDR UPS04242617](https://openairdocs.org/sdr/UPS04242617.md): Web · punctured · Jun 23, 2004 · N948UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, VENTRAL STAIRS TORQUE BOX HORIZONTAL WEB PUNCTURED AFT OF BS 1243 RIGHT O/B END. REPAIRED AREA IAW SRM 51-40-02.
- [SDR UPS04242704](https://openairdocs.org/sdr/UPS04242704.md): Flap Track · corroded · Jun 22, 2004 · N948UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-061-003.
- [SDR UPS04242702](https://openairdocs.org/sdr/UPS04242702.md): Skin Panel · corroded · Jun 22, 2004 · N948UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, ON REMOVAL OF SKIN PANEL CORROSION FOUND ON LWR SKIN PANEL LAP JOINT S4R BETWEEN BS 615 & BS 540. REPAIR CARRIED OUT IAW AAAE 2004-061-006.
- [SDR UPS04242675](https://openairdocs.org/sdr/UPS04242675.md): Skin · cracked · Jun 22, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57-30-4 FIG 4.
- [SDR UPS04242682](https://openairdocs.org/sdr/UPS04242682.md): Stringer · worn · Jun 21, 2004 · N948UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, STR WORN ON BS 1183 AFT SIDE AT WL 208 I/B OF SYS-A PRESSURE MODULE. REPAIR CARRIED OUT IAW AAAE EO 2004-061-004, UPS ENGINEERING FILE NR 727-53-20150 & SRM 51-30-02.
- [SDR UPS04242677](https://openairdocs.org/sdr/UPS04242677.md): Bracket · cracked · Jun 21, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OHM 57-51-61.
- [SDR UPS04242676](https://openairdocs.org/sdr/UPS04242676.md): Bracket · cracked · Jun 21, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-81-11.
- [SDR UPS04242616](https://openairdocs.org/sdr/UPS04242616.md): Web · cracked · Jun 21, 2004 · N948UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SUPPORT WEB BENEATH STAND-BY PUMP CRACKED AT ACCESS HOLE FOR DRAIN PLUG. STOP DRILLED CRACK AND SUPPORT WEB REPAIRED IAW SRM 51-40-2.
- [SDR UPS04242717](https://openairdocs.org/sdr/UPS04242717.md): Skin · corroded · Jun 18, 2004 · N948UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SUSPECT CORROSION AT BS 640-680 S1L TO S4L. ON INVESTIGATION CORROSION FOUND INTERNALLY ON SKIN PANEL AT BS 680 - 660 S4R, BS 620 S2L - 1L, BS 540 - 530 S2L REPAIR CARRIED OUT IAW SRM 51-30-2, 33-30-01 DRAWING 65-42370, AAAE EO 2004-61-006
- [SDR UPS04242705](https://openairdocs.org/sdr/UPS04242705.md): Skin · cracked · Jun 18, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. REPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2.
- [SDR UPS04242703](https://openairdocs.org/sdr/UPS04242703.md): Flap Track · corroded · Jun 18, 2004 · N948UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE: C, NR 4 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD-B. REPAIR CARRIED OUT IAW AAAE 2004-061-003.
- [SDR UPS04242683](https://openairdocs.org/sdr/UPS04242683.md): Structure · cracked · Jun 18, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE EO 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113.
- [SDR UPS04242672](https://openairdocs.org/sdr/UPS04242672.md): Attach Fitting · cracked · Jun 18, 2004 · N948UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:C SUSPECT CRACK ON OFFSET GEARBOX AT ATTACHMENT LUG ON RIGHT I/B FLAPS. HFEC CONFIRMED CRACK ON LUG. OFFSET GEARBOX REPLACED IAW MM 27-51-60 PARA 1-3.
- [SDR UPS04242715](https://openairdocs.org/sdr/UPS04242715.md): Skin · delaminated · Jun 17, 2004 · N948UP · Boeing 72725C · Spoilers
  > INSPECTION TYPE: C, NR 2 SPOILER HAS DELAMINATION ON UPPER & LWR SURFACES. REPAIRED IAW SRM 51-40-5.
- [SDR UPS04242706](https://openairdocs.org/sdr/UPS04242706.md): Skin · worn · Jun 17, 2004 · N948UP · Boeing 72725C · Rudder, Plate/Skin
  > INSPECTION TYPE:C, SKIN ON LWR RUDDER L/E WORN IN SEVERAL PLACES ON LT & RT SIDES. LWR RUDDER REPLACED IAW MM 27-20-01, 27-20-11 & SRM 51-30-02.
- [SDR UPS04242681](https://openairdocs.org/sdr/UPS04242681.md): Skin · cracked · Jun 17, 2004 · N948UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, CRACK IN SKIN FOUND AT WING SCANNING LIGHT CUTOUT LT BS 675. REPAIR CARRIED OUT IAW AAAE EO 2004-061-001, UPS ENGINEERING FILE NR 727-53-20149 & SRM 53-30-3 & MM 33-41-02.
- [SDR UPS04242674](https://openairdocs.org/sdr/UPS04242674.md): Skin · cracked · Jun 17, 2004 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 NDTM PT6 51-00-00 FIG
- [SDR UPS04242714](https://openairdocs.org/sdr/UPS04242714.md): Yoke · cracked · Jun 16, 2004 · N948UP · Boeing 72725C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE:C TAIL SKID UNIT FOUND CRACKED. TAIL SKID YOKE ASSY REPLACED IAW MM 32-71-41 & 31-71-22 FUNCTION CHECK.
- [SDR UPS04242680](https://openairdocs.org/sdr/UPS04242680.md): Skin · damaged · Jun 16, 2004 · N948UP · Boeing 72725C · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51.
- [SDR UPS04242036](https://openairdocs.org/sdr/UPS04242036.md): Light · inoperative · Mar 16, 2004 · N948UP · Boeing 72725C · Emergency Lighting
  > FWD ENTRY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS.
- [SDR UPS02239932](https://openairdocs.org/sdr/UPS02239932.md): Floorbeam · corroded · Nov 12, 2002 · N948UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C MAIN ENTRY DOOR FLOORBEAM T ANGLE SUPPORT SHOWS EVIDENCE OF CORROSION BETWEEN FS 312 AND FS 344. REMOVED AND REPLACED T ANGLE SUPPORT.
- [SDR UPS02239931](https://openairdocs.org/sdr/UPS02239931.md): Floor Panel · corroded · Nov 12, 2002 · N948UP · Boeing 72725C · Fuselage Floor Panel
  > INSPECTION TYPE:C MAIN ENTRY DOOR FLOOR PANEL CORRODED BETWEEN FS 312 AND 344. REMOVED AND REPLACED FLOOR PANEL.
- [SDR UPS02238494](https://openairdocs.org/sdr/UPS02238494.md): Light · inoperative · May 29, 2002 · N948UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:PFLT COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY AND CLEANED CONNECTOR TO LIGHT ASSY MOUNTING PLATE, OPS CHECK GOOD PER MM 33-50-67.
- [SDR UPS02237609](https://openairdocs.org/sdr/UPS02237609.md): Control Panel · malfunctioned · Feb 12, 2002 · N948UP · Boeing 72725C · AC Power Distribution System
  > INSPECTION TYPE:N/A AIR TURNBACK DUE TO SMOKE IN COCKPIT SMELLED SMOKE CLIMBING THROUGH 4000 FT THEN WENT AWAY UNTIL CREW SAW SMOKE AND SMELLED HEAVY ELECTRICAL SMELL AFTER BLOCK IN WITH EXTERNAL POWER CONNECTED. INSPECTED BEHIND PANELS OF F/E PANEL. REMOVED
- [SDR UPS01235981](https://openairdocs.org/sdr/UPS01235981.md): Beam · cracked · Apr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:N/A VERTICAL BEAM AT BS 1183 CRACKED LBL 26.83 WL 260 APPROX 2 INCH LONG FROM LIGHTENING HOLE. REPAIRED CRACK BY STOP DRILLING. HFEC AREA INSTALLED REPAIR PER B727.
- [SDR UPS01235838](https://openairdocs.org/sdr/UPS01235838.md): Pressure Panel · cracked · Apr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT 243.7 TO LOWER CHORD. REMOVED LT SIDE WALL AND FASTENERS AT BS 243.7 IAW SRM 51-30-2. CUT OUT CRACK SECTION PER SRM 51-40-2 FIG 1. APPROX SIZE 7 X 1 INCH, INSTALLED DOUBLER
- [SDR UPS01235837](https://openairdocs.org/sdr/UPS01235837.md): Pressure Panel · cracked · Apr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT BS 277.5 TO LOWER CHORD. REMOVED NOSE WHEEL WELL ACCESS PANEL LT AFT TO GAIN ACCESS AND REMOVED FASTENERS LT SIDE AT 277.5 S PER B727 SRM 51-30-2. CUT OUT CRACK SECTION AS P
- [SDR UPS01235982](https://openairdocs.org/sdr/UPS01235982.md): Drag Brace · cracked · Apr 28, 2001 · N948UP · Boeing 72725C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A DRAG BRACE SUPPORT BEAM IS CRACKED AT LT AFT CORNER CONFIRMED BY HFEC. STOP DRILLED CRACK PER SRM HFEC INSPECTED AREA FOUND NO CRACKS BEYOND AREA. FOUND CRACK TO BE BEYOND REPAIRABLE LIMITS PER UPS EO B727 -5310-0943. REMOVED AND REPLACE
- [SDR UPS01235980](https://openairdocs.org/sdr/UPS01235980.md): Bulkhead · cracked · Apr 28, 2001 · N948UP · Boeing 72725C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C PRESSURE BULKHEAD CRACKED RBL 18 AT HAND PUMP LOWER OUTBOARD MOUNT BRACKET. CUT OUT CRACKED AREA AT BS 1183 RBL 18 AS PER SRM 51-10-1. NDI NO CRACK FOUND, INSTALLED DOUBLER PER B727 SRM 53-10-9.
- [SDR UPS01234788](https://openairdocs.org/sdr/UPS01234788.md): Switch · malfunctioned · Jan 27, 2001 · N948UP · Boeing 72725C · Landing Gear Position and Warning
  > INSPECTION TYPE:IN, RIGHT LDG GEAR LIGHT NOT ILLUMINATED WHILE TAXIING IN RIGHT LDG GEAR LIGHT EXTINGUISHED STOPPED AIRCRAFT WHILE MAINTENANCE PINNED GEAR. LIGHT ILLUMINATED AGAIN BRIEFLY THEN WENT OUT AGAIN. REMOVED AND REPLACED RIGHT LANDING GEAR DOWN AND
- [SDR UPS00233626](https://openairdocs.org/sdr/UPS00233626.md): Slide · deployed · Aug 24, 2000 · N948UP · Boeing 72725C · Escape Slide
  > INSPECTION TYPE:N/A, ESCAPE SLIDE DEPLOYED. *S/D* DEFERRED ESCAPE SLIDE PER MEL 52-15 CONTROL NR M197975 PLACARD INSTALLED.
- [SDR UPS00233043](https://openairdocs.org/sdr/UPS00233043.md): Jackscrew · slipped · Jun 21, 2000 · N948UP · Boeing 72725C · Stabilizer Control System
  > STAB TRIM COASTS THREE REVOLUTIONS IN FLIGHT. REMOVED AND REINSTALL JACK SCREW ASSY PER MM 27-40-41 OP CHECKS GOOD.
- [SDR UPS00231900](https://openairdocs.org/sdr/UPS00231900.md): Seat Track · broken · Feb 25, 2000 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, CABIN SEAT TRACK LBL 60.0 BS 610 ONE SIDE EAR HALF BROKEN OFF. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-5.
- [SDR UPS00231893](https://openairdocs.org/sdr/UPS00231893.md): Seat Track · broken · Feb 25, 2000 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, CABIN SEAT TRACK BS 755 AT BL 0 HAS BROKEN TANG. REPLACED SECTION OF CABIN SEAT TRACK AT BBL 0 FROM BS 750 TO BS 850 IAW WITH SRM 53-10-5.
- [SDR UPS00231870](https://openairdocs.org/sdr/UPS00231870.md): Seat Track · broken · Feb 25, 2000 · N948UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK LBL 60.0 BS610, ONE EACH SIDE EARS HALF BROKEN OFF. REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5. MATERIAL USED PART NUMBER BAC1520-1433.
- [SDR UPS00231902](https://openairdocs.org/sdr/UPS00231902.md): Floorbeam · corroded · Feb 12, 2000 · N948UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C, APPROXIMATE FS 600 FLOORBEAM LBL 10 FORWARD LOWER CHORD SECTION HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR IN ACCORDANCE WITH AVITAS ENGINEERING REPAIR ORDER AVHM-101RO-1A AND UPS ENGINEERING FILE NR 727-53 -2229.
- [SDR UPS00231901](https://openairdocs.org/sdr/UPS00231901.md): Floorbeam · corroded · Feb 12, 2000 · N948UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C APPROXIMATE FS 600 FLOORBEAM RBL 18 FORWARD LOWER CHORD SECTION HAS CORROSION. REMOVED CORROSION, REPAIRED ANGLES IAW AVITAS ENGINEERING REPAIR ORDER NR AVHM-101RO-1A AND UPS ENGINEERING FILE NR 727-53-2229.
- [SDR UPS00231891](https://openairdocs.org/sdr/UPS00231891.md): Floorbeam · cracked · Feb 10, 2000 · N948UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C, CABIN FS 870 UPPER FLANGE CRACKED IN UPPER RADIUS WHERE IT CONNECTS TO VERTICAL WEB RBL 43-RBL 47 FLOORBEAM UPPER CHORD. REPAIRED IAW WITH AVITAS ENGINEERING REPAIR ORDER NR AVHM-100RO-1 AND UPS EO FILE NR 727-53-2224. REMOVED ASSOCIATED PA
- [SDR UPS00231890](https://openairdocs.org/sdr/UPS00231890.md): Stringer · corroded · Feb 9, 2000 · N948UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, STRINGER 25 LEFT SPLICE CORRODED AT BS440. REPLACED DAMAGED SECTION OF STRINGER 25 LEFT, BS440 IAW B727 SRM 53 -10-2.
- [SDR UPS00231760](https://openairdocs.org/sdr/UPS00231760.md): Stringer · corroded · Feb 9, 2000 · N948UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, STRINGER 25 LT SPLICE CORRODED AT BS 440 BURNISHED AREA OUT OF LIMITS. REPLACED DAMAGED SECTION AS PER B727 SRM 51-30-2 AND 53-10-2.
- [SDR UPS00231898](https://openairdocs.org/sdr/UPS00231898.md): Rib · cracked · Feb 6, 2000 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 3 LEADING EDGE SLAT ACTUATOR ROD END ATTACH BOLT OUTBOARD SUPPORT RIB CRACKED AT AFT LOWER CORNER. INSTALLED REPAIR AT OUTBOARD SUPPORT RIB FOR NR 3 LEADING EDGE SLAT ACTUATOR ROD END, MATERIAL USED 321.032. 5 BY 3 IAW B727 SRM 57-50-3.
- [SDR UPS00231897](https://openairdocs.org/sdr/UPS00231897.md): Angle · cracked · Feb 6, 2000 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED ANGLES AT NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEB INBOARD AND OUTBOARD MATERIAL
- [SDR UPS00231895](https://openairdocs.org/sdr/UPS00231895.md): Angle · cracked · Feb 6, 2000 · N948UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SU

Next page: https://openairdocs.org/deregistered/N948UP-2006-12-18/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 = 'N948UP' AND deregistration_id = 'N948UP-2006-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N948UP-2006-12-18/reports

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