# Service difficulty reports: N926UP, cancelled Sep 19, 2007

A list on [N926UP, cancelled Sep 19, 2007](https://openairdocs.org/deregistered/N926UP-2007-09-19.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 6 · 254 reports

- [SDR UPS06248770](https://openairdocs.org/sdr/UPS06248770.md): Light · inoperative · Dec 15, 2006 · N926UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES AND OPS CK IAW MM 33-50-01-5.
- [SDR UPS06248392](https://openairdocs.org/sdr/UPS06248392.md): Light · inoperative · Nov 1, 2006 · N926UP · Boeing 72731C · Emergency Lighting
  > FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AND OPERATIONAL CHECK PER MM 33-50-01-5 CKS NORMAL.
- [SDR UPS06247166](https://openairdocs.org/sdr/UPS06247166.md): Battery Pack · discharged · Jun 21, 2006 · N926UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT CABIN DOOR. REPLACED BATTERY PACK PER MM 33-50-90-2.
- [SDR UPS06247165](https://openairdocs.org/sdr/UPS06247165.md): Light · inoperative · Jun 21, 2006 · N926UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK NORMAL.
- [SDR UPS05245892](https://openairdocs.org/sdr/UPS05245892.md): Hydraulic System · leaking · Dec 23, 2005 · N926UP · Boeing 72731C · Hydraulic System, Main
  > INSPECTION TYPE:N/A ATB - HYD QTY AFTER TAKEOFF WENT TO 2.0 GALS AFTER FLAP RETRACTION QTY HELD STEADY AT 2.3 GALS. FOUND ASYS QTY LOW, SERVICED TO PROPER LEVEL PER M/M 12-12-00-2. CHECKED L/E SLAT ACTUATOR AND FLAP POW'S FOR LEAKS, NONE FOUND. NO OTHER LEA
- [SDR UPS05245846](https://openairdocs.org/sdr/UPS05245846.md): Light · inoperative · Nov 26, 2005 · N926UP · Boeing 72731C · Emergency Lighting
  > ONE LAMP INOP IN EMERGENCY EXIT LIGHT AT L1 DOOR. RELAMPED OK FOR SERVICE.
- [SDR UPS05245464](https://openairdocs.org/sdr/UPS05245464.md): Slide · inoperative · Sep 18, 2005 · N926UP · Boeing 72731C · Escape Slide
  > INSPECTION TYPE:N/A L-1 DOOR SLIDE INOP. REMOVED AND REPLACED SLIDE ASSY PER 25-60-14, THIS CLEARS M310071.
- [SDR UPS05244731](https://openairdocs.org/sdr/UPS05244731.md): Skin · corroded · Jun 15, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > C NDI HAS MATERIAL LOSS INDICATION AT S19 RT BS 441, SKIN CUT OUT AND REPAIR IN CONJUNCTION WITH NRC 792106 LAP REPAIR.
- [SDR UPS05244729](https://openairdocs.org/sdr/UPS05244729.md): Bushing · damaged · Jun 14, 2005 · N926UP · Boeing 72731C · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A.
- [SDR UPS05244728](https://openairdocs.org/sdr/UPS05244728.md): Structure · corroded · Jun 14, 2005 · N926UP · Boeing 72731C · Nacelle/Pylon Miscellaneous Structure
  > ENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A.
- [SDR UPS05244725](https://openairdocs.org/sdr/UPS05244725.md): Skin · cracked · Jun 13, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN BS 355 BETWEEN S26L AND 27L. REPAIR CARRIED OUT IAW SRM 53-30-3 AND 51-10-2.
- [SDR UPS05244732](https://openairdocs.org/sdr/UPS05244732.md): Fitting · cracked · Jun 12, 2005 · N926UP · Boeing 72731C · Fuselage, Stabilizer Attach Fittings
  > CLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CLEAT IAW SRM 51-30-2.
- [SDR UPS05244727](https://openairdocs.org/sdr/UPS05244727.md): Support Bracket · cracked · Jun 11, 2005 · N926UP · Boeing 72731C · Engine Thrust Reverser
  > ENG NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.
- [SDR UPS05244726](https://openairdocs.org/sdr/UPS05244726.md): Support Bracket · cracked · Jun 11, 2005 · N926UP · Boeing 72731C · Engine Thrust Reverser
  > ENG NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2.
- [SDR UPS05244733](https://openairdocs.org/sdr/UPS05244733.md): Skin · cracked · Jun 10, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > CRACK ON SKIN AT FWD ENTRY DOOR UPPER FWD AREA (BETWEEN S6 AND S 7L) OF CUT OUT. REPAIR CARRIED OUT IAW EO B727-5330-1460 OPTION 1.
- [SDR UPS05244730](https://openairdocs.org/sdr/UPS05244730.md): Support Bracket · cracked · Jun 10, 2005 · N926UP · Boeing 72731C · Trailing Edge Flap Actuator
  > NR 2 LE FLAP ACTUATOR O/B SUPPORT BRACKET CRACKED AT UPPER FWD CORNER. BRACKET FABRICATED AND REPLACED IAW SRM 51-20-1, 51-30-02 AND DRAWING 65 -16269.
- [SDR UPS05244738](https://openairdocs.org/sdr/UPS05244738.md): Hinge · cracked · Jun 7, 2005 · N926UP · Boeing 72731C · Ailerons
  > INSPECTION TYPE:C SUSPECT CRACK ON LEFT O/B AILERON I/B TAB HINGE ASSY LWR HALF. HFEC CARRIED OUT ON SUSPECT AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED. FWD HINGE HALF REPLACED IAW SRM 51-30-02. APPLIED CIC TO EXPOSED AREA IAW SRM 51-10-02.
- [SDR UPS05244737](https://openairdocs.org/sdr/UPS05244737.md): Skin · debonded · Jun 7, 2005 · N926UP · Boeing 72731C · Elevator, Tab Structure
  > INSPECTION TYPE:C RT ELEVATOR TAB DISBONDED AT LOWER SURFACE 24 INCHES O/B OF INNER EDGE, AT LOWER SURFACE 3 INCHES FROM O/B EDGE 2 SUSPECT AREA RT UPPER OUTER CORNER AND RT UPPER INNER CORNER. REMOVED ELEVATOR TAB IAW MM 27-30-11. REPAIRED TAB IAW SRM 51-40
- [SDR UPS05244736](https://openairdocs.org/sdr/UPS05244736.md): Skin · corroded · Jun 7, 2005 · N926UP · Boeing 72731C · Elevator, Tab Structure
  > INSPECTION TYPE:C LT ELEVATOR TAB UPPER SKIN CORRODED 5 INCHES FROM O/B END. REMOVED CORROSION IAW SRM 51-10-01, BLENDOUT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01. REMOVED TAB IAW MM 27-30-11. TAB UPPER SKIN REPAIRED IAW SRM 51-40-20. TAB REPAINTED IAW M
- [SDR UPS05244735](https://openairdocs.org/sdr/UPS05244735.md): Lap Joint · corroded · Jun 7, 2005 · N926UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT S19R BETWEEN BS 390 AND 441 AREA BETWEEN BS 390 AND 441 PAINT STRIPPED IAW MM 51-20-01. AREA REINSPECTED, COROSION FOUND EVIDENT CONTINUE OPEN UP AND REPAIR IAW APPX C OF EO B727-5330-0509. REMOVED CORROSION I
- [SDR UPS04243150](https://openairdocs.org/sdr/UPS04243150.md): Actuator · broken · Sep 22, 2004 · N926UP · Boeing 72731C · Landing Gear Actuator
  > INSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACED RIGHT MLG LOCK ACTUATOR, PERFORMED MAIN GEAR EXTENSION AND RETRACTION ADJ/TEST W/R/T MM 32-32-00
- [SDR UPS04243022](https://openairdocs.org/sdr/UPS04243022.md): Light · malfunctioned · Aug 25, 2004 · N926UP · Boeing 72731C · Emergency Lighting
  > FLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD.
- [SDR UPS04242900](https://openairdocs.org/sdr/UPS04242900.md): Switch · inoperative · Aug 13, 2004 · N926UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD.
- [SDR UPS04242550](https://openairdocs.org/sdr/UPS04242550.md): Light · inoperative · Jun 9, 2004 · N926UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL.
- [SDR UPS04242205](https://openairdocs.org/sdr/UPS04242205.md): Flap Track · cracked · Apr 7, 2004 · N926UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02.
- [SDR UPS04242181](https://openairdocs.org/sdr/UPS04242181.md): Casting · cracked · Apr 7, 2004 · N926UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. REPAIR SECTION FABRICATED IAW SRM 51-40-3 & INSTALLED IAW SRM 51-40-3.
- [SDR UPS04242260](https://openairdocs.org/sdr/UPS04242260.md): Angle · corroded · Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 REPAIR CARRIED OUT IAW SRM 51-20-1 AND SMRO EO 2004-027-002. UPS ENGINEERING FILE NR B727-5310-203
- [SDR UPS04242241](https://openairdocs.org/sdr/UPS04242241.md): Door Frame · cracked · Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE NR B727-5310-20302-A
- [SDR UPS04242206](https://openairdocs.org/sdr/UPS04242206.md): Frame · corroded · Apr 6, 2004 · N926UP · Boeing 72731C · Aerodynamic Fairings
  > INSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02.
- [SDR UPS04242204](https://openairdocs.org/sdr/UPS04242204.md): Beam · corroded · Apr 6, 2004 · N926UP · Boeing 72731C · Horizontal Stabilizer Structure
  > INSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987.
- [SDR UPS04242180](https://openairdocs.org/sdr/UPS04242180.md): Floorbeam · cracked · Apr 6, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8.
- [SDR UPS04242219](https://openairdocs.org/sdr/UPS04242219.md): Drum · corroded · Apr 5, 2004 · N926UP · Boeing 72731C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01.
- [SDR UPS04242179](https://openairdocs.org/sdr/UPS04242179.md): Floorbeam · cracked · Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7.
- [SDR UPS04242178](https://openairdocs.org/sdr/UPS04242178.md): Floorbeam · cracked · Apr 5, 2004 · N926UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8.
- [SDR UPS04242223](https://openairdocs.org/sdr/UPS04242223.md): Rib · cracked · Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.
- [SDR UPS04242220](https://openairdocs.org/sdr/UPS04242220.md): Rib · cracked · Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.
- [SDR UPS04242177](https://openairdocs.org/sdr/UPS04242177.md): Skin · cracked · Apr 3, 2004 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3.
- [SDR UPS02239194](https://openairdocs.org/sdr/UPS02239194.md): Stiffener · corroded · Aug 17, 2002 · N926UP · Boeing 72731C · Wing Main, Frame Structure
  > INSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060.
- [SDR UPS02239191](https://openairdocs.org/sdr/UPS02239191.md): Web · cracked · Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSPECTION CONFIRMED CRACK REMOV AL. REPAIR PARTS FABRICATED AND REPAIR INSTALLED IAW SRM 51-40-2, FI G. 1.
- [SDR UPS02239120](https://openairdocs.org/sdr/UPS02239120.md): Pressure Panel · cracked · Aug 15, 2002 · N926UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED DOUBLER & FILLER IAW
- [SDR UPS02239168](https://openairdocs.org/sdr/UPS02239168.md): Skin · cracked · Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02.
- [SDR UPS02239166](https://openairdocs.org/sdr/UPS02239166.md): Skin · cracked · Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082
- [SDR UPS02239165](https://openairdocs.org/sdr/UPS02239165.md): Skin · cracked · Aug 14, 2002 · N926UP · Boeing 72731C · Leading Edge Devices
  > INSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082
- [SDR UPS02239199](https://openairdocs.org/sdr/UPS02239199.md): Spar · corroded · Aug 14, 2002 · N926UP · Boeing 72731C · Wing Spar
  > INSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LOCATION BETWEEN WS 17
- [SDR UPS02239119](https://openairdocs.org/sdr/UPS02239119.md): Web · cracked · Aug 14, 2002 · N926UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SRM 51-10-4
- [SDR UPS02239167](https://openairdocs.org/sdr/UPS02239167.md): Doubler · cracked · Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DOUBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OUT CRACK CONFIRM ED & END OF CRACK MARKED. DOUBLER AND FILLERS FABRICATED AND INSTALL ED IAW SRM
- [SDR UPS02239197](https://openairdocs.org/sdr/UPS02239197.md): Web · cracked · Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB AREA. NEW WEB AND DOUBLERS FABRICATED AND INSTALLED IAW DRAWING 65-18414
- [SDR UPS02239190](https://openairdocs.org/sdr/UPS02239190.md): Skin · corroded · Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS INDICATION FROM BS 440 TO BS 411 APPR OX. 20% - 30%. CORRODED INTERNAL DOUBLER ALSO FOUND TO BE DISBONDED. DOUBLER REMOVED IAW SRM 51-30-2.
- [SDR UPS02239187](https://openairdocs.org/sdr/UPS02239187.md): Stiffener · cracked · Aug 13, 2002 · N926UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW EO B727-5311-0631 STEP 3. HEFC INSPECTION CONFIRMED CRACK CONTAINED. AREA REPAIRED IAW B727-5311-
- [SDR UPS02239115](https://openairdocs.org/sdr/UPS02239115.md): Stiffener · cracked · Aug 13, 2002 · N926UP · Boeing 72731C · Aerodynamic Fairings
  > INSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7.

Next page: https://openairdocs.org/deregistered/N926UP-2007-09-19/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 = 'N926UP' AND deregistration_id = 'N926UP-2007-09-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N926UP-2007-09-19/reports

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