# Service difficulty reports: N950UP, cancelled Aug 23, 2006

A list on [N950UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N950UP-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 5 · 220 reports

- [SDR UPS04243611](https://openairdocs.org/sdr/UPS04243611.md): Light · malfunctioned · Dec 16, 2004 · N950UP · Boeing 72725C · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT FLICKERS VERY DIM WHEN SWITCH PLACED TO ON. REMOVED AND REPLACED EMERGENCY LIGHT PER 33-50-1, TEST OK.
- [SDR UPS04242988](https://openairdocs.org/sdr/UPS04242988.md): Light · inoperative · Aug 19, 2004 · N950UP · Boeing 72725C · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERIES IN FWD & AFT EXIT LIGHTS, ALL CHECK GOOD IAW MM 33-50.
- [SDR UPS04242566](https://openairdocs.org/sdr/UPS04242566.md): Seat Track · corroded · Jun 2, 2004 · N950UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:N/A ON INSPECTION SEAT TRACK SECTION FOUND CORRODED AT BS 730 AT RBBL 625 APPROX. NEW SEAT TRACK SECTION FABRICATED IAW SRM 51-20-1 AND ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW EO B727-5310-7477 STEP 28.
- [SDR UPS04242582](https://openairdocs.org/sdr/UPS04242582.md): Bulkhead · cracked · Jun 1, 2004 · N950UP · Boeing 72725C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02.
- [SDR UPS04242575](https://openairdocs.org/sdr/UPS04242575.md): Fairing · cracked · Jun 1, 2004 · N950UP · Boeing 72725C · Engine Thrust Reverser
  > INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING IS CRACKED AT MID AFT END. REPLACED FAIRING IAW MM 78-30-43.
- [SDR UPS04242590](https://openairdocs.org/sdr/UPS04242590.md): Bulkhead · cracked · May 31, 2004 · N950UP · Boeing 72725C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51.
- [SDR UPS04242588](https://openairdocs.org/sdr/UPS04242588.md): Web · cracked · May 31, 2004 · N950UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, NOSE WHEEL WELL STRUCTURE HAS EVIDENCE OF CRACK AT BSTA 240 LBL. REPAIR CARRIED IAW SRM 51-40-02. LEAK CHECKED SATISFACTORY.
- [SDR UPS04242584](https://openairdocs.org/sdr/UPS04242584.md): Skin · cracked · May 31, 2004 · N950UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01.
- [SDR UPS04242576](https://openairdocs.org/sdr/UPS04242576.md): Panel · cracked · May 31, 2004 · N950UP · Boeing 72725C · Wing, Plate/Skin
  > INSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02.
- [SDR UPS04242574](https://openairdocs.org/sdr/UPS04242574.md): Attach Fitting · corroded · May 31, 2004 · N950UP · Boeing 72725C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, ATTACH FITTING AT THE BASE OF THE BS 950 STRUCTURAL FITTING HAS EVIDENCE OF INTERGRANULAR CORROSION. FITTING REPLACED IAW SRM 51-30-02 & DRAWING 65-16338.
- [SDR UPS04242558](https://openairdocs.org/sdr/UPS04242558.md): Fitting · cracked · May 31, 2004 · N950UP · Boeing 72725C · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE: C, AREA ABOVE NR 2 HORIZONTAL FIREWALL, UPPER LEFT FITTING AT STA 1470. 5 AND WL 300.15 IS CRACKED. FITTING REMOVED IAW SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02 AND BOEING DRAWING 65-17553.
- [SDR UPS04242557](https://openairdocs.org/sdr/UPS04242557.md): Web · cracked · May 31, 2004 · N950UP · Boeing 72725C · Ailerons
  > INSPECTION TYPE: C, LEFT I/B AILERON, O/B WEB CRACKED AT AFT UPPER FASTENER, AND FASTENER MISSING FROM WEB. REPAIR CARRIED OUT IAW 51-30-02.
- [SDR UPS04242577](https://openairdocs.org/sdr/UPS04242577.md): Skin · corroded · May 30, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, FASTENER HEAD POPPED & BULGE IN SKIN. SUSPECT CORROSION BETWEEN SKIN & STR AT BS 1065 S29L. SKIN CUTOUT BETWEEN BS 1061 AND BS 1072 AT S29L, CORROSION REMOVED IAW SRM 51-10-6. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR COMPLETED IAW AAA
- [SDR UPS04242569](https://openairdocs.org/sdr/UPS04242569.md): Skin · corroded · May 30, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, DUE TO BELOW MIN EDGE DISTANCE & CORROSION ON SKIN DURING RT 740 FITTING REPLACEMENT, SKIN REPAIR REQUIRED BETWEEN S17 & S18 RT TO BETWEEN S24 & 25 RT. REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING EO 2004-054-005 & SRM 51-30-2 7 51
- [SDR UPS04242581](https://openairdocs.org/sdr/UPS04242581.md): Skin · corroded · May 29, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, BULGING IN SKIN AT BS 1183 BETWEEN S6R AND S10R. CUT OUT INTERNAL BONDED DOUBLER BETWEEN S6R TO S10R BS 1183 TO BS 1177 REFERENCE SRM 53-30-3. HFEC CARRIED OUT, NO DEFECTS FOUND. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3. REP
- [SDR UPS04242580](https://openairdocs.org/sdr/UPS04242580.md): Angle · corroded · May 29, 2004 · N950UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, CORROSION AT BS 312L VIEW IN 3RD LIGHTENING HOLE FROM FRONT OM INBOARD ANGLE MIDWAY BETWEEN UPPER AND LOWER NWW CHORDS. CORRODED ANGLE FABRICATED AND INSTALLED IAW DWG 65-18415.
- [SDR UPS04242570](https://openairdocs.org/sdr/UPS04242570.md): Skin · cracked · May 29, 2004 · N950UP · Boeing 72725C · Wing, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00.
- [SDR UPS04242565](https://openairdocs.org/sdr/UPS04242565.md): Skin · cracked · May 28, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460 & SRM 51-30-02.
- [SDR UPS04242559](https://openairdocs.org/sdr/UPS04242559.md): Panel · corroded · May 28, 2004 · N950UP · Boeing 72725C · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE: C, NR 5 LEFT BALANCE BAY PANEL HAS VERY LITE SURFACE CORROSION. UPON INVESTIGATION, CORROSION FOUND TO BE BEYOND LIMITS. BALANCE PANEL PLATE REPLACED IAW MM 27-30-27.
- [SDR UPS04242571](https://openairdocs.org/sdr/UPS04242571.md): Skin · corroded · May 27, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SKIN CORRODED AT BS 1263 S9R. CORROSION REMOVED IAW SRM 53-30-3 FIG 4. HFEC CARRIED OUT AROUND CUTOUT, NO DEFECTS FOUND. COMPLETED REPAIR IAW AAAE EO 2004-054-003.
- [SDR UPS04242556](https://openairdocs.org/sdr/UPS04242556.md): Support · cracked · May 27, 2004 · N950UP · Boeing 72725C · Engine Mount Section
  > INSPECTION TYPE: C, CENTER ENGINE LEFT AND RIGHT SUPPORT WEBS AT BS 1387 ARE CRACKED. WEBS REMOVED IAW SRM 51-30-02. NEW WEBS FABRICATED IAW BOEING DRAWING 65-17553, NEW WEBS INSTALLED IAW SRM 51-30-02.
- [SDR UPS04242555](https://openairdocs.org/sdr/UPS04242555.md): Tee Fitting · cracked · May 27, 2004 · N950UP · Boeing 72725C · Wing, Attach Fittings
  > INSPECTION TYPE: C, TEE FITTING CRACKED ON UPPER I/B T-EDGE PANEL FOR APU EXHAUST 70.5 WBL. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-10-2.
- [SDR UPS04242564](https://openairdocs.org/sdr/UPS04242564.md): Skin · corroded · May 22, 2004 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, FASTENERS POPPED AT S25R BETWEEN BS 290 & BS 300 SUSPECT CORROSION BETWEEN SKIN & STRINGER. REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-02, 51-10-1, 53-30-01, 51-20-04 & 51-80-01.
- [SDR UPS04242573](https://openairdocs.org/sdr/UPS04242573.md): Fitting · cracked · May 20, 2004 · N950UP · Boeing 72725C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, RIGHT BS 740 FITTING CRACKED BEYOND LIMITS OUTBOARD FLANGE. FITTING REPLACEMENT & REPAIR CARRIED OUT IAW AAAE EO 2004-054-005 UPS ENG FILE 727-53-20144 & UPS EO B727-5310-7477, DRG 65C13724 & SRM 51-30-2.
- [SDR UPS03241052](https://openairdocs.org/sdr/UPS03241052.md): Light · inoperative · Aug 6, 2003 · N950UP · Boeing 72725C · Emergency Lighting
  > L-1 DOOR EMERGENCY LIGHT TEST INOPERABLE. REMOVED AND REPLACED AND CKD OK USED AMERICAN AIRLINES BORROWED PART MM 33-50-01 P/N ON OFF 10-0067-9, S/N OFF 7012 S/N ON 22921.
- [SDR UPS02239809](https://openairdocs.org/sdr/UPS02239809.md): Butt Joint · corroded · Oct 11, 2002 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > C CHECK FUSELAGE AT SKIN BUTT JOINT BS 260 AND BETWEEN STR 12 RT & 13 RT IS BULGING CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AS PER BOEING DRAW ING 69-62161 AND UPS E.O. B727-5310-1371-F APPENDIX E
- [SDR UPS01237133](https://openairdocs.org/sdr/UPS01237133.md): Window · cracked · Oct 20, 2001 · N950UP · Boeing 72725C · Flight Compartment Windows
  > INSPECTION TYPE:N/A, F/O SLIDING WINDOW CRACKED. REMOVED AND REPLACED NR 2 WINDOW ASSY PER MM 56-12-11. OPS CHECKS NORMAL P/N OFF/ON 5-71762-42 SN OFF 56WIN1244 ON UP01358.
- [SDR UPS01236105](https://openairdocs.org/sdr/UPS01236105.md): Stringer · corroded · May 31, 2001 · N950UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C STRINGER TERMINAL FITTING CORRODED AT BS 1183 STR 18L REMOVED CORRODED STRINGER BS 1183, STR18L. PER SRM 51-30-2, FABRICATED STRINGER TERMINAL FITTING PER BOEING DRAWING 65-242276 AND B727 SRM 51-10-2 TREATED AND PRIMED. INSTALLED STRINGE
- [SDR UPS01236102](https://openairdocs.org/sdr/UPS01236102.md): Skin · cracked · May 29, 2001 · N950UP · Boeing 72725C · Fuselage Structure (General)
  > INSPECTION TYPE:C NOSE WHEEL WELL R/H SIDE WALL SHOW CRACK AT BS 294 WL165 CRACK ABOUT 10" LONG LOOKING GROM INSIDE REMOVED VERTICAL ANGLE FOR ACCESS REPAIR PER B727 SRM 51-30-2 CUT OUT DAMAGE AREA PER B727 SRM 51-40-2 APP.4 SIDE CUT OUT 6"X1" PERFORMED
- [SDR UPS01236104](https://openairdocs.org/sdr/UPS01236104.md): Keelbeam · cracked · May 27, 2001 · N950UP · Boeing 72725C · Fuselage Main, Keel
  > INSPECTION TYPE:C KEEL BEAM BS 900 APPROX APU COMPARTMENT ACCESS PANEL SHOWS A HOLE AND CRACKED AREA. CUT DAMAGED AREA AT KEEL BEAM ACCESS PANEL BS 900 APU COMPARTMENT AS PER B727 SRM 51-10-1, INSTALLED DOUBLER ON KEEL BEAM ACCESS PANEL AS PER B727 SRM 51-40-
- [SDR UPS01236103](https://openairdocs.org/sdr/UPS01236103.md): Spar · cracked · May 27, 2001 · N950UP · Boeing 72725C · Wing Spar
  > INSPECTION TYPE:C, LEFT WING REAR SPAR UPPER CHORD AT WING STATION APPROX CRACK INDICATION IS ABOUT 2 INCHES LONG OUTBOARD OF NR 1 FUEL SOV. REMOVE CRACK AT REAR SPAR UPPER CHORD AT WS 190 AND INSTALL FILLER AND DOUBLER REPAIR AS PER BOEING DRAWING 65C196447,
- [SDR UPS01236100](https://openairdocs.org/sdr/UPS01236100.md): Bulkhead · cracked · May 27, 2001 · N950UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACKS AT BULKHEAD STA 294.5 RBL 12, NOSE LANDING GEAR WHEEL WELL, INSPECTED. INSPECTED NLG WHEEL WELL BULKHEAD AND VERIFY CRACK AS PER B727 NAT MANUAL PART 6 51-00-00 FIG 4. REMOVED VERTICAL ANGLE TO ACCESS REPAIR AND CUT OUT CRACK AREA
- [SDR UPS01236101](https://openairdocs.org/sdr/UPS01236101.md): Skin · corroded · May 26, 2001 · N950UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, INDICATION OF MATERIAL LOSS GREATER THAN 10 8/0 IN THE SKIN AT CIRCUMFERENTIAL JOINT BS 441 BETWEEN S 17R AND S 20R FORWARD PANEL. CUT DAMAGED AREA ON STA 441 BETWEEN STA 17R AND STA 20R PER DRAWING 69-62161. INSTALLED DOUBLER REPAIR IN C
- [SDR UPS01235110](https://openairdocs.org/sdr/UPS01235110.md): Battery · discharged · Feb 28, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN, EMERGENCY EXIT LIGHTS INOP ON LT OVERWING LIGHTS AND LT REAR EMERGENCY EXIT LIGHT NEXT TO LAV DOOR. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS01235079](https://openairdocs.org/sdr/UPS01235079.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN, FWD BULKHEAD EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235077](https://openairdocs.org/sdr/UPS01235077.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN, FWD PAY DOOR LOWER FLOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235075](https://openairdocs.org/sdr/UPS01235075.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, RIGHT FWD OVERWING FLOOR EMERGENCY LIGHT FAILED TO TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235072](https://openairdocs.org/sdr/UPS01235072.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, RT CEILING OVERWING EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235071](https://openairdocs.org/sdr/UPS01235071.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN RT FWD OVERWING EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235070](https://openairdocs.org/sdr/UPS01235070.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN, LEFT LOWER FLOOR EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235069](https://openairdocs.org/sdr/UPS01235069.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, AFT LEFT LAV LOWER EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235068](https://openairdocs.org/sdr/UPS01235068.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, REAR EXIT CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED REAR EXIT CEILING EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235067](https://openairdocs.org/sdr/UPS01235067.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, FORWARD ENTRY WAY CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED FWD ENTRY WAY CEILING EMERGENCY EXIT LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235066](https://openairdocs.org/sdr/UPS01235066.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, ROW 19 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 19 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235065](https://openairdocs.org/sdr/UPS01235065.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN ROW 9 LEFT SEAT EMERGENCY LIGHT TEST. REMOVED AND REPLACED ROW 9 SEAT EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235064](https://openairdocs.org/sdr/UPS01235064.md): Battery · discharged · Feb 23, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN ROW 4 SEAT 4 EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 4 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01234853](https://openairdocs.org/sdr/UPS01234853.md): Battery · discharged · Feb 2, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN REF M208478 RT OVERWING DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY, OPS GOOD.
- [SDR UPS01234832](https://openairdocs.org/sdr/UPS01234832.md): Light · inoperative · Jan 31, 2001 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY INTERIOR OVERWING LIGHT INOP ACFT IN CARGO MODE. *S.D* REMOVED AND REPLACED BATTERY, OPS GOOD. THIS CLEARS M208478.
- [SDR UPS01234575](https://openairdocs.org/sdr/UPS01234575.md): Indicator · failed · Dec 31, 2000 · N950UP · Boeing 72725C · Fuel Quantity Indicator
  > INSPECTION TYPE:N/A ATB - NB 2 FUEL QTY WENT TO ZERO. SUMPED NR 2 FUEL TANK. PERFORMED ADJ/TEST OF NR 2 FUEL QTY INDICATION SYSTEM PER REF 28-41-00. SYS OPS CKS NORMAL. THIS CLEARS M206491. PLACARD REMOVED.
- [SDR UPS01234580](https://openairdocs.org/sdr/UPS01234580.md): Battery Pack · failed · Dec 29, 2000 · N950UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY LIGHT INOP RNR'D BATTERY PACK, OPS GOOD.

Next page: https://openairdocs.org/deregistered/N950UP-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 = 'N950UP' AND deregistration_id = 'N950UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N950UP-2006-08-23/reports

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