# Service difficulty reports: N919UP, cancelled Dec 4, 2007

A list on [N919UP, cancelled Dec 4, 2007](https://openairdocs.org/deregistered/N919UP-2007-12-04.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 2 · 92 reports

- [SDR UPS07248886](https://openairdocs.org/sdr/UPS07248886.md): Slide · dislodged · Jan 19, 2007 · N919UP · Boeing 72730C · Escape Slide
  > FWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GOOD.
- [SDR UPS06248684](https://openairdocs.org/sdr/UPS06248684.md): Skin · cracked · Nov 14, 2006 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > 3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCHES. C/W EO B727-5330-25585A TO FERRY A/C TO BFM 9014 D337794 ISSUED.
- [SDR UPS06248513](https://openairdocs.org/sdr/UPS06248513.md): Slide · dislodged · Nov 7, 2006 · N919UP · Boeing 72730C · Escape Slide
  > FOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2.
- [SDR UPS06248330](https://openairdocs.org/sdr/UPS06248330.md): Battery · inoperative · Oct 26, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER MM 33-50-90-2. REMOVED AND REPLACED BATTERIES ON COCKPIT ENTRY DOOR. OPS CHECK GOOD.
- [SDR UPS06247827](https://openairdocs.org/sdr/UPS06247827.md): Slide · dislodged · Aug 28, 2006 · N919UP · Boeing 72730C · Escape Slide
  > INSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2.
- [SDR UPS06247717](https://openairdocs.org/sdr/UPS06247717.md): Battery · inoperative · Aug 17, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL.
- [SDR UPS06247529](https://openairdocs.org/sdr/UPS06247529.md): Battery · discharged · Jul 31, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED.
- [SDR UPS06246808](https://openairdocs.org/sdr/UPS06246808.md): Fairing · delaminated · May 8, 2006 · N919UP · Boeing 72730C · Aerodynamic Fairings
  > DELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PAN
- [SDR UPS05245266](https://openairdocs.org/sdr/UPS05245266.md): Skin · corroded · Aug 6, 2005 · N919UP · Boeing 72730C · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND COR
- [SDR UPS05245265](https://openairdocs.org/sdr/UPS05245265.md): Stiffener · corroded · Aug 5, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > LT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1.
- [SDR UPS05245262](https://openairdocs.org/sdr/UPS05245262.md): Stiffener · corroded · Aug 4, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > RT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4.
- [SDR UPS05245263](https://openairdocs.org/sdr/UPS05245263.md): Floorbeam · corroded · Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Main, Floor Beam
  > FLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2.
- [SDR UPS05245207](https://openairdocs.org/sdr/UPS05245207.md): Intercostal · corroded · Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02.
- [SDR UPS05245205](https://openairdocs.org/sdr/UPS05245205.md): Support · corroded · Aug 2, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2.
- [SDR UPS05245261](https://openairdocs.org/sdr/UPS05245261.md): Skin · corroded · Aug 1, 2005 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > AREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A.
- [SDR UPS05245264](https://openairdocs.org/sdr/UPS05245264.md): Attach Angle · corroded · Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Main, Attach Fittings
  > RT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2.
- [SDR UPS05245206](https://openairdocs.org/sdr/UPS05245206.md): Web · corroded · Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2.
- [SDR UPS05243629](https://openairdocs.org/sdr/UPS05243629.md): Light · inoperative · Jan 6, 2005 · N919UP · Boeing 72730C · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD.
- [SDR UPS04242069](https://openairdocs.org/sdr/UPS04242069.md): Fitting · cracked · Mar 17, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.
- [SDR UPS04242070](https://openairdocs.org/sdr/UPS04242070.md): Fitting · cracked · Mar 12, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.
- [SDR UPS04242058](https://openairdocs.org/sdr/UPS04242058.md): Stringer · corroded · Mar 11, 2004 · N919UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3.
- [SDR UPS04242073](https://openairdocs.org/sdr/UPS04242073.md): Skin · corroded · Mar 10, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG.
- [SDR UPS04242072](https://openairdocs.org/sdr/UPS04242072.md): Door Frame · corroded · Mar 9, 2004 · N919UP · Boeing 72730C · Landing Gear Doors
  > INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61.
- [SDR UPS04242060](https://openairdocs.org/sdr/UPS04242060.md): Cargo Track · cracked · Mar 9, 2004 · N919UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8.
- [SDR UPS04242075](https://openairdocs.org/sdr/UPS04242075.md): Support · corroded · Mar 8, 2004 · N919UP · Boeing 72730C · Drag Control Actuator
  > INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01.
- [SDR UPS04242059](https://openairdocs.org/sdr/UPS04242059.md): Mount · corroded · Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.
- [SDR UPS04242057](https://openairdocs.org/sdr/UPS04242057.md): Mount · corroded · Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B.
- [SDR UPS04242056](https://openairdocs.org/sdr/UPS04242056.md): Skin · bulged · Mar 4, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOS
- [SDR UPS03240251](https://openairdocs.org/sdr/UPS03240251.md): Torque Tube · loose · Mar 4, 2003 · N919UP · Boeing 72730C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A ATB-AFTER T/O, LG RAISED AND RIGHT MAIN GEAR STAYED DOWN. RED GEAR LIGHT AND DOORS LIGHT REMAINED ON. GEAR CAME DOWN NORMALLY. REPLACED 6 EA SHEARED RIVETS ON UPLOCK TORQUE TUBE, OPS CHECKS GOOD PER MM 32-30-00.
- [SDR UPS02239549](https://openairdocs.org/sdr/UPS02239549.md): Battery · discharged · Sep 30, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, OPS CHECKS GOOD, BATTERIES IAW MM 33-50-01.
- [SDR UPS02239530](https://openairdocs.org/sdr/UPS02239530.md): Contactor · dirty · Sep 20, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED LIGHT ASSY OVER CREW CABIN DOOR, CLEANED CONTACTS, OPS CK OK IAW MM 33-50-01.
- [SDR UPS02238920](https://openairdocs.org/sdr/UPS02238920.md): Battery · discharged · Jul 29, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT L1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS02238919](https://openairdocs.org/sdr/UPS02238919.md): Battery · discharged · Jul 29, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT COCKPIT. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS02238737](https://openairdocs.org/sdr/UPS02238737.md): Light · not seated · Jul 2, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOP. SEATED EXIT LIGHT ASSY OPS CHECKS GOOD
- [SDR UPS02238641](https://openairdocs.org/sdr/UPS02238641.md): Battery · discharged · Jun 17, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:PFLT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM 33-50-01.
- [SDR UPS02237755](https://openairdocs.org/sdr/UPS02237755.md): Light · inoperative · Mar 3, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:IN FWD EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OP CHECK GOOD IAW MM 33-50-01.
- [SDR UPS02237516](https://openairdocs.org/sdr/UPS02237516.md): Cover · loose · Jan 24, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:PFLT CABIN EXIT LIGHT COVER OVER CABIN DOOR IS LOOSE. CHECK SECURITY OF EXIT LIGHT ASSY PER MAINT PRACTICES MM 33-50-01 AND INSTALLED LIGHT COVER, NO DEFECTS NOTED.
- [SDR UPS02237439](https://openairdocs.org/sdr/UPS02237439.md): Light · not seated · Jan 20, 2002 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS DIM, RESEATED LIGHT ASSY. OPS CHECKS GOOD PER MM 33-50-101.
- [SDR UPS01236604](https://openairdocs.org/sdr/UPS01236604.md): Fairing · cracked · Aug 5, 2001 · N919UP · Boeing 72730C · Trailing Edge Flaps
  > INSPECTION TYPE:PFLT LT INBD FLAP LT OUTBD CANOE FIXED FAIRING HAS A CRACK ON AFT UPPER CORNER OF PREVIOUS REPAIR. DEFFERRED PER MMOC
- [SDR UPS01236163](https://openairdocs.org/sdr/UPS01236163.md): Actuator · leaking · Jun 22, 2001 · N919UP · Boeing 72730C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A RIGHT MAIN GEAR DOOR OPENED ENROUTE GEAR HANDLE PLACED TO "UP" POSIT ION DOOR CLOSED GEAR HANDLE RETURNED TO "OFF" POSITION OPS NORMAL ****SUPPLEMENTAL MRR*** REMOVED AND REPLACED GEAR DOOR ACTUATOR R/H PER MM 32-32-81 ADJ TEST GROUND D
- [SDR UPS01235279](https://openairdocs.org/sdr/UPS01235279.md): Frame · cracked · Mar 5, 2001 · N919UP · Boeing 72730C · Fuselage Main, Frame
  > INSPECTION TYPE:C-CK, CRACK AT FUSELAGE FRAME BS 930 ABOVE STR 13L. CUT OUT DAMAGE SECTION OF FRAME BETWEEN STR 12L & 13L. INSTALLED FORMED ANGLE REPAIR, HEAT TREATED.
- [SDR UPS01235278](https://openairdocs.org/sdr/UPS01235278.md): Stringer · corroded · Feb 28, 2001 · N919UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C-CK, STRINGER 18 LEFT CORRODED BETWEEN BS 440 TO BS 460. REMOVED CORROSION ON STRINGER FLANGE. FOUND OUT OF UNIT. INSTALLED STRINGER REPAIR.
- [SDR UPS01235402](https://openairdocs.org/sdr/UPS01235402.md): Fitting · cracked · Feb 26, 2001 · N919UP · Boeing 72730C · Wing, Attach Fittings
  > INSPECTION TYPE:C CHECK LT WING FRONT SPAR INTERIOR & LBBL 70.5 TERMINAL FITTING ATTACH V SHAPE FITTING TO UPPER SHOW CRACK MIGRATING FROM OB BOLT. REMOVED FITTING LT WING FRONT SPAR INTERIOR LBL 70.5 V SHAPE. INSTALLED LT WING UPPER FRONT SPAR CONER NEW FIT
- [SDR UPS01235399](https://openairdocs.org/sdr/UPS01235399.md): Duct · cracked · Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake System
  > INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS. 1 EA 4 INCH CRACK 93 INCHES FROM AFT EDGE 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR.
- [SDR UPS01235398](https://openairdocs.org/sdr/UPS01235398.md): Duct · cracked · Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake System
  > INSPECTION TYPE:C CHECK NR 2 ENGINE INLET S DUCT INNER SKIN HAS CIRCUMFERENTIAL CRACKS 2 EA APPX 100-104 INCH FROM AFT EDGE. 1 EA 7 INCH Y SHAPED CRACK & 1 EA 1.5 INCH CRACK APPX 4 OCLOCK. CUT OUT DAMAGED AREA. INSTALLED REPAIR. HEAT TREATED.
- [SDR UPS01235284](https://openairdocs.org/sdr/UPS01235284.md): Intake Duct · cracked · Feb 19, 2001 · N919UP · Boeing 72730C · Engine Air Intake System
  > INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 6 INCH CIRCUMFERENTIAL CRACK AT 4 O''CLK APPROX 30 INCHES AFT OF WHERE S-DUCT ATTACHES TO INLET. CUT OUT DAMAGED AREA APPROX 7 X 1 INCHES. PERFORMED NDT AND NO CRACK INDICATIONS. INSTALLED SK
- [SDR UPS01235283](https://openairdocs.org/sdr/UPS01235283.md): Skin · cracked · Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-CK, FUSELAGE SKIN HAS CORROSION BULGE AND APPROX 3 INCH LATERAL CRACK. REMOVED FASTENERS, REMOVED CORROSION. NDT INSP C/W CUT DAMAGE AREA AND INSTALL DOUBLER REPAIR AT FUSE SKIN.
- [SDR UPS01235282](https://openairdocs.org/sdr/UPS01235282.md): Skin · corroded · Feb 19, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-CK, LOW FREQ EDDY CURRENT INSP OF SKIN AT BS 441 BETWEEN STRG 18R & 19R HAS INDICATION OF CORROSION LOSS GREATER THAN 10 PERCENT. REMOVED EQUIPMENT TO ACCESS REPAIR, CUT DAMAGED AREA AND INSTALLED REPAIR PER EO -1371.
- [SDR UPS01235221](https://openairdocs.org/sdr/UPS01235221.md): Duct · cracked · Feb 19, 2001 · N919UP · Boeing 72730C · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR.
- [SDR UPS01235401](https://openairdocs.org/sdr/UPS01235401.md): Lap Joint · bulged · Feb 18, 2001 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CK LAP JOINT 19RT HAS SKIN BULGE AT BS 620. CUT OUT DAMAGED SKIN LWR & UPPER AREA. INSTALLED REPAIR PART AT LAP JOINT STR 19 BS 620.

Next page: https://openairdocs.org/deregistered/N919UP-2007-12-04/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 = 'N919UP' AND deregistration_id = 'N919UP-2007-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N919UP-2007-12-04/reports

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