# Service difficulty reports: N924UP, cancelled Aug 24, 2007

A list on [N924UP, cancelled Aug 24, 2007](https://openairdocs.org/deregistered/N924UP-2007-08-24.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 · 108 reports

- [SDR UPS02237711](https://openairdocs.org/sdr/UPS02237711.md): Casting · corroded · Feb 6, 2002 · N924UP · Boeing 72731C · Wing Structure
  > INSPECTION TYPE:C #5 FLAP TRACK ATTACH POINT ON LWR SURFACE OF WING, CORROSION EXIDENT IN AFT PAD, O/B HOLE. CORROSION SEEMS TO BE CONFINED TO BARREL NUT CASTING. REMOVED CASTING ON O/B OF #5 FLAP TRACK IAW SRM 51-30-02, CASTING RE PLACED IAW BOEING DWGS
- [SDR UPS02237694](https://openairdocs.org/sdr/UPS02237694.md): Frame · cracked · Feb 6, 2002 · N924UP · Boeing 72731C · Passenger/Crew Doors
  > INSPECTION TYPE:C RH AFT FRAME ON E & E DOOR CRACKED FRAME REPLACED IAW DRAWING # 65-02163
- [SDR UPS02237712](https://openairdocs.org/sdr/UPS02237712.md): Support · cracked · Feb 4, 2002 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, AFT AIRSTAIRS ACTUATOR FITTING SUPPORT ANGLE CRACKED IN AFT RT TORQUE BOX AT STA 1273. REPAIRED IAW EO B727-5310-1239.
- [SDR UPS01237262](https://openairdocs.org/sdr/UPS01237262.md): Rod · broken · Nov 6, 2001 · N924UP · Boeing 72731C · Spoilers
  > INSPECTION TYPE:PRD INBOARD SPOILER CASTING SUPPORT ROD BROKEN LT WING. INBOARD SPOILER LT WING CASTING SUPPORT ROD REPLACED.
- [SDR UPS00233591](https://openairdocs.org/sdr/UPS00233591.md): Light · inoperative · Aug 18, 2000 · N924UP · Boeing 72731C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT CAME ON IN FLIGHT INTERMITTENTLY. EMERGENCY LIGHT REPLACED PER MM 33-50, CHECKED OK.
- [SDR UPS00233505](https://openairdocs.org/sdr/UPS00233505.md): Stringer · corroded · Jul 25, 2000 · N924UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C&SI, FOLLOWING REWORK AT BS 1183 STR 15R TO 5R HOLES AT 10R HAVE EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIR CARRIED OUT IAW SMRO EO 2000-026-006 & 2000-026-011 UPS ENGINEERING FILE NR 727-53-2269 & 727-53-2274.
- [SDR UPS00233498](https://openairdocs.org/sdr/UPS00233498.md): Structure · cracked · Jul 25, 2000 · N924UP · Boeing 72731C · Cargo/Baggage Doors
  > INSPECTION TYPE:C&SI, SEVERAL CRACKS IN FWD CARGO DOOR. FWD CARGO DOOR REPLACED IAW MM 2-31-01.
- [SDR UPS00233455](https://openairdocs.org/sdr/UPS00233455.md): Fitting · corroded · Jul 24, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C+SI, AFTER REWORK OF BS 360 ON SMRO EO2000-026-001, TWO HOLES AT STR END FITTING 3L ARE REAMED UP TO MAX LIMITS AND STILL SHOW EVIDENCE OF CORROSION INSIDE SURFACE OF HOLES. HOLES REWORKED IAW SHANNON MROEO2000-026-010.UPS FILE NR 727-53-2273
- [SDR UPS00233486](https://openairdocs.org/sdr/UPS00233486.md): Angle · cracked · Jul 20, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, G-NET ATTACH POINT AT BS 365 BETWEEN STR 15L AND 16L HAS CRACKED ANGLE. INSTALLED NEW ANGLE AND CLIPS IAW SRM 51-30-02.
- [SDR UPS00233485](https://openairdocs.org/sdr/UPS00233485.md): Frame · cracked · Jul 20, 2000 · N924UP · Boeing 72731C · Cargo/Baggage Doors
  > INSPECTION TYPE:C&SI, AFT CARGO DOOR HAS SUSPECT CRACKED FRAME AT STA 1072 BETWEEN NR 5 ST OPS. REMOVED AND REPLACED FRAME IAW SRM 53-30-2.
- [SDR UPS00233417](https://openairdocs.org/sdr/UPS00233417.md): Angle · cracked · Jul 20, 2000 · N924UP · Boeing 72731C · Cargo/Baggage Doors
  > INSPECTION TYPE:C&SI, FWD CARGO DOOR BS 577 AFT ANGLE CRACKED AT HINGE ATTACHMENT FWD CARGO DOOR REPLACED REF NRC 175922 FOR REPLACEMENT.
- [SDR UPS00233482](https://openairdocs.org/sdr/UPS00233482.md): Bracket · cracked · Jul 19, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, FIRE WIRE BRACKET CRACKED AT BS 1010 LBL 45.5 LWR SURFACE OF FLOOR I T CARGO BAY. REPAIRED IAW SRM 51-40-3 FIG 1.
- [SDR UPS00233481](https://openairdocs.org/sdr/UPS00233481.md): Bracket · cracked · Jul 19, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, SUSPECT CRACK TO HORIZ STIFFENER SUPPORT BRACKET AT BS 1183 RT AFT ENTRY UPPER DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-2.
- [SDR UPS00233416](https://openairdocs.org/sdr/UPS00233416.md): Bolt · cracked · Jul 19, 2000 · N924UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C&SI, ENGINE NR 2 CROSS STRUT AFT ATTACH BOLT FOUND CRACKED DURING NDI CHECK. BOLT REPLACED IAW MM 71-21-12.
- [SDR UPS00233470](https://openairdocs.org/sdr/UPS00233470.md): Angle · corroded · Jul 18, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C+SI, CORROSION ON LATERIAL SUPPORT ANGLE BS 850 LBL 6 AT DELTA BEAM. CORROSION ON SUPPORT ANGLE OUT OF LIMITS. NEW ANGLE FABRICATED IAW SRM 51-20-1. FASTENERS REMOVED IAW SRM 51-30-2. CORROSION REMOVED IAW SRM 51-10-6. REINSPECTED FOUND W
- [SDR UPS00233502](https://openairdocs.org/sdr/UPS00233502.md): Stringer · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C&SI, STR 10R AT BS 1105 HAS CRACK DUE TO CORROSION. REPAIR CARRIED OUT IAW SRM 51-40-4 FIG 1.
- [SDR UPS00233487](https://openairdocs.org/sdr/UPS00233487.md): Hinge · corroded · Jul 17, 2000 · N924UP · Boeing 72731C · Elevator Structure
  > INSPECTION TYPE:C&SI, NR 5 BALANCE BAY HINGE HALF RT SIDE CORRODED BEYOND LIMITS (AFT HINGE HALF). REPLACED HINGE HALF AND HARDWARE IAW MM 27-30-21.
- [SDR UPS00233483](https://openairdocs.org/sdr/UPS00233483.md): Frame · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Fuselage Main, Frame
  > INSPECTION TYPE:C&SI, 2 SUSPECT CRACKS ON FRAME BS 277 ON RT SIDE OF CONTROL CABIN AT STR 15 AND 16. FRAME REPAIRED IAW SRM 51-40-2 FIG 1.
- [SDR UPS00233477](https://openairdocs.org/sdr/UPS00233477.md): Beam · corroded · Jul 17, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, FWD CARGO BAY CORROSION ON I BEAM LWR CHORD LWR SURFACE AT BS 500 BL 0. REPAIR CARRIED OUT IAW SMRO EO 2000-026-008 UPS ENGINEERING FILE 727-53-2271.
- [SDR UPS00233454](https://openairdocs.org/sdr/UPS00233454.md): Link Rod · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:C+SI, CRACKED LINK AT LT MLG LINKAGE TO AIR GROUND SENSE. AIR GROUND SENSER LINK REPLACED IAW MM 20-80-01. FUNCTION CHECKED IAW MM 32-31-11 PG 501, FOUND SATISFACTORY.
- [SDR UPS00233427](https://openairdocs.org/sdr/UPS00233427.md): Skin · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Engine Thrust Reverser
  > INSPECTION TYPE:C&S,I ENGINE NR 1 THRUST REVERSER UPPER DOOR INNER RAMP SKIN CRACKED. NOTE: CRACK COMING OUT FROM UNDER PREVIOUS PATCH REPAIR. REPAIR CARRIED OUT IAW SRM 78-30-01 FIG 205.
- [SDR UPS00233412](https://openairdocs.org/sdr/UPS00233412.md): Stiffener · corroded · Jul 17, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, CONTROL CABIN, HORIZ STIFFENER ON BS 251.6 IS CORRODED ON LT SIDE AT WL 220 APPROX. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.
- [SDR UPS00233406](https://openairdocs.org/sdr/UPS00233406.md): Bracket · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Engine Thrust Reverser
  > INSPECTION TYPE:C&SI, ENGINE NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.
- [SDR UPS00233405](https://openairdocs.org/sdr/UPS00233405.md): Bracket · cracked · Jul 17, 2000 · N924UP · Boeing 72731C · Engine Thrust Reverser
  > INSPECTION TYPE:C&SI, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.
- [SDR UPS00233459](https://openairdocs.org/sdr/UPS00233459.md): Mount · corroded · Jul 16, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C+SI, CORROSION ON LWR ANTENNA SUPPORT BS 820 AT CENTER LINE. CORROSION REMOVED IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. CORRODED ANGLE SUPPORT REMOVED IAW SRM 51-30-2. NEW ANGLE SUPPORT FABRICATED IAW SRM 51-20-1. ANGLE SUPPORT RE-INST
- [SDR UPS00233468](https://openairdocs.org/sdr/UPS00233468.md): Floorbeam · corroded · Jul 15, 2000 · N924UP · Boeing 72731C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C+SI, BS 328 FLOORBEAM HAS SURFACE CORROSION AROUND FASTENERS ON TOP CAP, LBL30. CORROSION REMOVED IAW MM SRM 51-10-06. AREA FOUND TO BE OUT OF LIMITS IAW MM SRM 53-10-1 FIG 5 MAX 0.020 INCH. REPAIR CARRIED OUT IAW MM 53-10-8 FIG 7.
- [SDR UPS00233414](https://openairdocs.org/sdr/UPS00233414.md): Stringer · corroded · Jul 15, 2000 · N924UP · Boeing 72731C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C&SI, CORROSION ON STR 24R AT BS 460. REPAIR CARRIED OUT IAW SRM 53-10-1 AND SRM 53-10-3.
- [SDR UPS00233504](https://openairdocs.org/sdr/UPS00233504.md): Flange · corroded · Jul 14, 2000 · N924UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, NR 3 FLAP TRACK FWD ATTACH FLANGE UPPER SURFACE CENTRE HOLE AND O/B HOLE CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-026-004 UPS ENGINEERING FILE NR 727-57-2172.
- [SDR UPS00233503](https://openairdocs.org/sdr/UPS00233503.md): Flange · corroded · Jul 14, 2000 · N924UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, NR 3 FLAP TRACK AFT ATTACH FLANGE AND HOLES CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-02-004 UPS ENGINEERING FILE NR 727-57-2172.
- [SDR UPS00233479](https://openairdocs.org/sdr/UPS00233479.md): Carriage · corroded · Jul 14, 2000 · N924UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, NR 2 FLAP CARRIAGE SPINDLE THREADS CORRODED I/B DEADWEIGHT ROLLER HOLE CORRODED. REPLACED IAW OHM 57-58-01.
- [SDR UPS00233478](https://openairdocs.org/sdr/UPS00233478.md): Beam · cracked · Jul 14, 2000 · N924UP · Boeing 72731C · Spoilers
  > INSPECTION TYPE:C&SI, CRACK FOUND AT NR 8 SPOILER SUPPORT BEAM I/B OF I/B HINGE. REPAIR CARRIED OUT IAW SMRO EO 2000-026-002 UPS ENGINEERING FILE NR 727-57-2169.
- [SDR UPS00233457](https://openairdocs.org/sdr/UPS00233457.md): Bolt · corroded · Jul 14, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C+SI, BS1183 TENSION BOLTS CORRODED ABOVE STR 8R. REMOVED SUFFICIENT BOLTS TO VERIFY CONDITION OF SPLICE. BOLTS REMOVED FROM STR 5R - 15R BOLTS FOUND CORRODED, OK ABOVE 5R AND OK BELOW 15R. HOLES REWORKED PER SMROEO2000-026-006 AND BOLTS REP
- [SDR UPS00233426](https://openairdocs.org/sdr/UPS00233426.md): Pressure Panel · cracked · Jul 14, 2000 · N924UP · Boeing 72731C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C&SI, SUSPECT CRACK AT NOSE WHEEL WELL SIDEWALL AT RBL 23 AND STA 267 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.
- [SDR UPS00233424](https://openairdocs.org/sdr/UPS00233424.md): Mount · corroded · Jul 14, 2000 · N924UP · Boeing 72731C · Engine Mount Section
  > INSPECTION TYPE:C&SI, ENGINE NR 1 FWD MOUNT HOLES CORROSION IN BOTH I/B HOLES AND AFT O/B HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.
- [SDR UPS00233501](https://openairdocs.org/sdr/UPS00233501.md): Bracket · cracked · Jul 13, 2000 · N924UP · Boeing 72731C · Spoilers
  > INSPECTION TYPE:C&SI, LT WING T/E SUPPORT BRACKET CRACKED DIRECTLY AFT OF NR 4 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-30-02.
- [SDR UPS00233456](https://openairdocs.org/sdr/UPS00233456.md): Frame · cracked · Jul 13, 2000 · N924UP · Boeing 72731C · Fuselage Main, Frame
  > INSPECTION TYPE:C+SI, SUSPECT CRACK ON VERTICAL CHORD AT BS 178 BULKHEAD TO SKIN ATTACH POINT, WL 200 APPROX, LT SIDE. NDT REQUIRED TO CONFIRM. CRACK CONFIRMED. POST CUT OUT IAW B727-NDTM PT6 51-00-00 FIG 4. CRACK FOUND TO BE REMOVED. T-SUPPORT AT STR 17
- [SDR UPS00233404](https://openairdocs.org/sdr/UPS00233404.md): Bracket · cracked · Jul 13, 2000 · N924UP · Boeing 72731C · Spoilers
  > INSPECTION TYPE:C&SI, LT WING, T/E SUPPORT BRACKET CRACKED 6 INCHES O/B OF NR 5 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.
- [SDR UPS00233484](https://openairdocs.org/sdr/UPS00233484.md): Skin · corroded · Jul 12, 2000 · N924UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, SUSPECT COROSSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 ABOVE STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3.
- [SDR UPS00233480](https://openairdocs.org/sdr/UPS00233480.md): Splice Plate · cracked · Jul 12, 2000 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C&SI, ON REMOVAL OF BS 930 SPLICE PLATE AT STR 14 CRACK FOUND IN LWR END OF FUSELAGE UPPER FRAME. REPAIR CARRIED OUT ON FRAME IAW SRM 53-10-4 FIG 1.
- [SDR UPS00233453](https://openairdocs.org/sdr/UPS00233453.md): Skin · corroded · Jul 12, 2000 · N924UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON SKIN BS 1140 BETWEEN S3R & 4R. REPAIRED AREA IAW SRM 53-30-3 & UPS EO B727-5330-0509 APPEX 8.3 WEIGHT OF REPAIR 5.2 LBS. NOTE THIS IS A CAT B REPAIR AND REPAIR CRITICAL ROW ZERO TIMED.
- [SDR UPS00233408](https://openairdocs.org/sdr/UPS00233408.md): Carriage · corroded · Jul 12, 2000 · N924UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, NR 8 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE IAW MM 27-51-13.
- [SDR UPS00233407](https://openairdocs.org/sdr/UPS00233407.md): Carriage · corroded · Jul 12, 2000 · N924UP · Boeing 72731C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI, NR 1 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE IAW MM 27-51-13.
- [SDR UPS00233423](https://openairdocs.org/sdr/UPS00233423.md): Butt Joint · corroded · Jul 11, 2000 · N924UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION BS 1080 BUTT JOINT AFT EDGE BETWEEN S4L AND 2L. REPAIR CARRIED OUT IAW EO B727-5330-1177.
- [SDR UPS00233422](https://openairdocs.org/sdr/UPS00233422.md): Butt Joint · corroded · Jul 11, 2000 · N924UP · Boeing 72731C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION AT BS 1080 BUTT JOINT AFT EDGE (VIEWED INTERNALLY) BETWEEN S5R AND 2R. REPAIR CARRIED OUT IAW EO B727-5330-1177.
- [SDR UPS00231624](https://openairdocs.org/sdr/UPS00231624.md): Battery Pack · discharged · Feb 15, 2000 · N924UP · Boeing 72731C · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER COCKPIT DOOR AND ENTRANCE DOOR, GOT NO LIGHT WHEN TESTED BY CREW PRIOR TO DEPARTURE. REMOVED AND REPLACED BATTERY PACK. BATTERY REQUIRED CHARGING PRIOR TO INSTALLATION.
- [SDR UPS99230750](https://openairdocs.org/sdr/UPS99230750.md): Frame · cracked · Sep 23, 1999 · N924UP · Boeing 72731C · Fuselage Main, Frame
  > INSPECTION TYPE:C, BS 930 FRAME CRACK ON HORIZONTAL LEG OF FRAME AT FLOOR LEVEL. REPAIR TO FRAME CARRIED OUT IAW SMRO EO 99-30-003 UPS ENGINEERING FILE NR 727-53-2174.
- [SDR UPS99230723](https://openairdocs.org/sdr/UPS99230723.md): Bracket · cracked · Sep 20, 1999 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, FLOOR SUPPORT BRACKET CRACKED AT BS 440 RT IN E & E BAY. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10 -2.
- [SDR UPS99230722](https://openairdocs.org/sdr/UPS99230722.md): Beam · cracked · Sep 20, 1999 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, DURING REMOVAL TO FACILITATE REPLACEMENT OF BS 940 FITTING, FLAP ROLLER TRACK SUPPORT FOUND CRACKED IN THREE PLACES. BEAM ASSY REPLACED IAW SRM 51-30-2 AND OHM 20-50-01.
- [SDR UPS99230724](https://openairdocs.org/sdr/UPS99230724.md): Angle · cracked · Sep 18, 1999 · N924UP · Boeing 72731C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, ANGLE CRACKED ON AFT SIDE OF FRAME BS 560 STR 17 L. ANGLE REPLACED IAW SRM 51-40-03 FIG 1 & SRM 53-10-02.
- [SDR UPS99230749](https://openairdocs.org/sdr/UPS99230749.md): T-Edge · lightning strike · Sep 17, 1999 · N924UP · Boeing 72731C · Elevator Structure
  > INSPECTION TYPE:C, LIGHTNING DISCHARGE DAMAGE RT ELEVATOR TIP T-EDGE AT BASE LWR SURFACE & STRUCTURE AT PREVIOUS REPAIR. REPAIR CARRIED OUT IAW SRM 55-20-3 FIG 3.

Next page: https://openairdocs.org/deregistered/N924UP-2007-08-24/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 = 'N924UP' AND deregistration_id = 'N924UP-2007-08-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N924UP-2007-08-24/reports

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