# Service difficulty reports: N73751, cancelled Aug 9, 2006

A list on [N73751, cancelled Aug 9, 2006](https://openairdocs.org/deregistered/N73751-2006-08-09.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 · 122 reports

- [SDR XN0A1311](https://openairdocs.org/sdr/XN0A1311.md): Strut · low · Mar 17, 2006 · N73751 · Boeing 727227 · Nose/Tail Landing Gear Strut/Axle
  > ON TAXI OUT, KNOCKING SOUND FROM NOSE GEAR. SERVICED NOSE STRUT WITH NITROGEN IAW B727 MM CHAPTER 12-20-00.
- [SDR XN0A1286](https://openairdocs.org/sdr/XN0A1286.md): Relief Valve · out of adjust · Dec 21, 2005 · N73751 · Boeing 727227 · Turbine Engine Oil System
  > NR 1 ENGINE OIL PRESSURE WENT TO REDLINE ON THROTTLE. TO TAKEOFF POWER. ADJUSTED OIL PRESSURE RELIEF VALVE TO 43 PSI AT IDLE IAW MM 72-00. OPS AND LEAK CHECKS GOOD AT IDLE. (ORIG/CLOSED)
- [SDR XN0A1283](https://openairdocs.org/sdr/XN0A1283.md): Strut · low · Dec 13, 2005 · N73751 · Boeing 727227 · Nose/Tail Landing Gear
  > ON TAXI OUT THE NOSE GEAR SEEMED TO BOTTOM OUT. INSPECTED NOSE STRUT ASSY AND FOUND STRUT LOW ON NITROGEN, SERVICED NLG STRUT WITH NITROGEN IAW B727 MM CHAPTER 32-10-00.
- [SDR XN0A1278](https://openairdocs.org/sdr/XN0A1278.md): Wire · loose · Nov 23, 2005 · N73751 · Boeing 727227 · Flight Control System Wiring
  > SPEED BRAKE/ FLAP WARNING WILL NOT TEST IN TAXI OUT AND T/O WARNING HORN. SECURED LOOSE WIRE ON AURAL WARN CB. CHECKS GOOD ON GROUND.
- [SDR XN0A1270](https://openairdocs.org/sdr/XN0A1270.md): Transmitter · malfunctioned · Oct 1, 2005 · N73751 · Boeing 727227 · Crew Oxygen System
  > CREW O2 TO 0 PSI IN TAXI OUT SWF, BACK TO THE RAMP. RESET PRESS TRANSMITTER ON CREW BOTTLE, CHECK GOOD IAW 35-11-00.
- [SDR XNOA1187](https://openairdocs.org/sdr/XNOA1187.md): Warning System · activated · May 25, 2004 · N73751 · Boeing 727227 · Smoke Detection
  > MAIN CARGO AND LOWER CARGO WARNING IN FLIGHT WITH LIGHT AND BELL.
- [SDR CALA9801959](https://openairdocs.org/sdr/CALA9801959.md): Wire · broken · Oct 15, 1998 · N73751 · Boeing 727227 · Light System Wiring
  > EMERGENCY AISLE PATH LIGHTING INOP AT ROW 10 ABC. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01.
- [SDR CALA9800576](https://openairdocs.org/sdr/CALA9800576.md): Skin · debonding · Mar 20, 1998 · N73751 · Boeing 727227 · Leading Edge Devices
  > INSPECTION FOUND RT WING NR 6 KRUEGER FLAP DEBONDING. A REPAIR WAS ACCOMPLISHED IAW ECRA 5720-01064.
- [SDR CALA9800575](https://openairdocs.org/sdr/CALA9800575.md): Floorbeam · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP FLANGE OF FLOORBEAM CORRODED AT FS 1110, RBL 10 TO RBL 63. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9800574](https://openairdocs.org/sdr/CALA9800574.md): Seat Track · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND TOP AND BOTTOM OF RT OUTBOARD SEAT TRACK CORRODED AT FS 400 TO 440. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.
- [SDR CALA9800572](https://openairdocs.org/sdr/CALA9800572.md): Skin · gouged · Mar 20, 1998 · N73751 · Boeing 727227 · Trailing Edge Flaps
  > INSPECTION FOUND A 1 INCH GOUGE IN RT INBOARD FOREFLAP OUTBORD LEADING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED.
- [SDR CALA9800570](https://openairdocs.org/sdr/CALA9800570.md): Flap Track · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Trailing Edge Flaps
  > INSPECTION FOUND NR 7 FLAP TRACK AFT MOUNT CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.
- [SDR CALA9800569](https://openairdocs.org/sdr/CALA9800569.md): Floorbeam · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP FLANGE UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT FS 360, RBL 10 TO LBL 18. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.
- [SDR CALA9800568](https://openairdocs.org/sdr/CALA9800568.md): Chord · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TOP AND BOTTOM OF CHORD CORRODED AT FS 310 TO 362, LBL 56. ALSO, DOUBLER AT FS 360 HAD A.5 INCH CRACK. THE CHORD WAS REMOVED, CORROSION WAS REMOVED FROM AREA IAW SRM 51-10-6. A NEW DOUBLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5
- [SDR CALA9800567](https://openairdocs.org/sdr/CALA9800567.md): Circumferential · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3.
- [SDR CALA9800566](https://openairdocs.org/sdr/CALA9800566.md): Stringer · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING STA 656.50 STRINGER ON TOP OF CHORD RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW EA 5762-01050.
- [SDR CALA9800565](https://openairdocs.org/sdr/CALA9800565.md): Skin · eroded · Mar 20, 1998 · N73751 · Boeing 727227 · Rudder, Plate/Skin
  > INSPECTION FOUND RT SIDE OF LOWER RUDDER SKIN EDGE ERODED JUST ABOVE PANEL NR 9901. THE AREA WAS SANDED AND A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-40-8.
- [SDR CALA9800564](https://openairdocs.org/sdr/CALA9800564.md): Skin · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND A.1875 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075.
- [SDR CALA9800563](https://openairdocs.org/sdr/CALA9800563.md): Skin · deteriorated · Mar 20, 1998 · N73751 · Boeing 727227 · Rudder, Tab Structure
  > INSPECTION FOUND LT LOWER SIDE OF UPPER RUDDER TAB FIBERGLASS REPAIR DETERIORATED. THE FIBERGLASS REPAIR WAS SANDED, REWORKED, AND PRIMED IAW SRM 51-40-9 AND 51-10-6.
- [SDR CALA9800562](https://openairdocs.org/sdr/CALA9800562.md): Skin · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Service Doors
  > INSPECTION FOUND A.625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1.
- [SDR CALA9800561](https://openairdocs.org/sdr/CALA9800561.md): Angle · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.
- [SDR CALA9800560](https://openairdocs.org/sdr/CALA9800560.md): Angle · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN J-ANGLE SUPPORT ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. A REPAIR CHANNEL WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914.
- [SDR CALA9800559](https://openairdocs.org/sdr/CALA9800559.md): Flap Track · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Trailing Edge Flaps
  > INSPECTION FOUND UPPER MOUNT FLANGE OF NR 6 FLAP TRACK CORRODED AT FORWARD ATTACH CLEVIS. THE FLAP TRACK WAS REMOVED AND REPLACED.
- [SDR CALA9800558](https://openairdocs.org/sdr/CALA9800558.md): Attach Fitting · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Wing, Control Surface Attach Fittings
  > INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING AT BOTTOM OF WING CORRODED AT INBOARD FACE. THE FITTING WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 20-50-01.
- [SDR CALA9800557](https://openairdocs.org/sdr/CALA9800557.md): Angle · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing Miscellaneous Structure
  > INSPECTION FOUND TWO 1 INCH CRACKS AT BOLT HOLES OF LT WING LOWER LEADING EDGE SUPPORT ANGLE AT FS 120. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.
- [SDR CALA9800556](https://openairdocs.org/sdr/CALA9800556.md): Stiffener · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.625 INCH CRACK IN STIFFENER AT BOTTOM OF LT WING LEADING EDGE RIB, WBL 92.0. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.
- [SDR CALA9800555](https://openairdocs.org/sdr/CALA9800555.md): Rib · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.
- [SDR CALA9800554](https://openairdocs.org/sdr/CALA9800554.md): Skin · dented · Mar 20, 1998 · N73751 · Boeing 727227 · Aileron Tabs
  > INSPECTION FOUND RT OUTBOARD AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED.
- [SDR CALA9800553](https://openairdocs.org/sdr/CALA9800553.md): Angle · cracked · Mar 20, 1998 · N73751 · Boeing 727227 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL SUPPORT T-ANGLE. THE CRACK WAS LOCATED AT INBOARD AFT END, OUTBOARD OF NR 1 FLAP JACKSCREW. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-
- [SDR CALA9800552](https://openairdocs.org/sdr/CALA9800552.md): Floorbeam · corroded · Mar 20, 1998 · N73751 · Boeing 727227 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM TOP FLANGE UPPER AND LOWER SURFACE CORRODED AT FS 360, RBL 10 TO LBL 10. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.
- [SDR CALA9800551](https://openairdocs.org/sdr/CALA9800551.md): Skin · punctured · Mar 20, 1998 · N73751 · Boeing 727227 · Trailing Edge Flaps
  > INSPECTION FOUND A HOLE IN RT OUTBOARD FOREFLAP UPPER INBOARD SURFACE. THE DAMAGED AREA WAS CUTOUT AND A HOT BONDED REPAIR WAS APPLIED IAW SRM 51-40-6 AND 51-10-6.
- [SDR CALA9800550](https://openairdocs.org/sdr/CALA9800550.md): Flap Track · corroded · Mar 19, 1998 · N73751 · Boeing 727227 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 7 FLAP TRACK FORWARD LUGS CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.
- [SDR CALA9800549](https://openairdocs.org/sdr/CALA9800549.md): Rib · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Vertical Stabilizer, Spar/Rib
  > INSPECTION FOUND A.25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.
- [SDR CALA9800548](https://openairdocs.org/sdr/CALA9800548.md): Rib · worn · Mar 19, 1998 · N73751 · Boeing 727227 · Vertical Stabilizer, Spar/Rib
  > INSPECTION FOUND VERTICAL STABILIZER NR 7 RIB WORN AT STRINGER 2R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.
- [SDR CALA9800547](https://openairdocs.org/sdr/CALA9800547.md): Skin · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN LT VERTICAL STABILIZER AT STA 1253, JUST ABOVE AND AFT OF PANEL NR 9523. THREE 1 INCH CRACKS WERE FOUND IN THE LT VERTICAL STABILIZER AT STA 1264. THE CRACKED AREAS WERE CUTOUT IAW SRM 54-10-1. FILLER AND DOUBLER REPAIRS W
- [SDR CALA9800546](https://openairdocs.org/sdr/CALA9800546.md): Bulkhead Panel · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Fuselage Main, Bulkhead
  > INSPECTION FOUND THE NLG WHEEL WELL FORWARD BULKHEAD TOP RIGHT PANEL, TOP LEFT PANEL, AND TOP CENTER PANELS CRACKED AT FASTENER HOLES. THE CRACKS WERE.5 TO 1 IN LENGTH. THE CRACKED AREAS WERE CUTOUT IAW SRM 51-40-2. REPAIR DOUBLERS AND FILLERS WERE FABRICA
- [SDR CALA9800545](https://openairdocs.org/sdr/CALA9800545.md): Skin · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK WITH DENT IN AFT BAGGAGE COMPARTMENT DOOR SKIN 23 DOWN FROM TOP AND 16 AFT. THE DENTED AND CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3.
- [SDR CALA9800544](https://openairdocs.org/sdr/CALA9800544.md): Skin · dented · Mar 19, 1998 · N73751 · Boeing 727227 · Cargo/Baggage Doors
  > INSPECTION FOUND C-2 CARGO DOOR AFT LOWER EDGE BENT AND CORRODED. THE AFT LOWER FRAME SECTION WAS REMOVED IAW SRM 51-30-2 AND THE SKIN WAS STRAIGHTENED IAW SRM 51-40-1. THE NEW LOWER AFT FRAME SECTION WAS SEALED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.
- [SDR CALA9800543](https://openairdocs.org/sdr/CALA9800543.md): Frame · corroded · Mar 19, 1998 · N73751 · Boeing 727227 · Fuselage Main, Frame
  > INSPECTION FOUND FLOOR MOUNT FRAME CORRODED AT AFT BIN STA 1148 TO 1166 BETWEEN STRINGER 26 TO 27R. A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-40-5 AND SRM 51-30-2.
- [SDR CALA9800542](https://openairdocs.org/sdr/CALA9800542.md): Spar Web · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Wing Spar
  > INSPECTION FOUND A 4 INCH CRACK IN CENTER WING SECTION AT REAR SPAR WEB UPPER RADIUS ABOVE PRODUCTION PANEL FROM RBL 0 TO RBL 4. THE AREA WAS REPAIRED IAW EA SA004-5710-01843, DRAWING 65C37620, AND SERVICE BULLETIN 727-57A0182.
- [SDR CALA9800541](https://openairdocs.org/sdr/CALA9800541.md): Radome · eroded · Mar 19, 1998 · N73751 · Boeing 727227 · Aerodynamic Fairings
  > INSPECTION FOUND THE RADOME EXTERIOR SKIN HAD SOME SPOTS OF EROSION AND A SMALL HOLE. THE RADOME WAS REMOVED AND REPLACED IAW MM 53-15-0.
- [SDR CALA9800540](https://openairdocs.org/sdr/CALA9800540.md): Rib · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.25 INCH CRACK FROM END OF STRINGER ON TOP OF RIB, SECOND UPPER STRINGER FROM AFT SPAR, WS 656.50, ACCESS 7217. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-01050.
- [SDR CALA9800539](https://openairdocs.org/sdr/CALA9800539.md): Rib · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL SUPPORT RIB JUST INBOARD OF NR 3 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB SUPPORT WAS REMOVED, NEW PARTS WERE INSTALLED IAW SRM 51-10-6 AND 51-10-1.
- [SDR CALA9800535](https://openairdocs.org/sdr/CALA9800535.md): Rib · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.25 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL OUTBOARD SUPPORT RIB JUST INBOARD NR 4 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB AND ROD WERE REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9800534](https://openairdocs.org/sdr/CALA9800534.md): Skin · corroded · Mar 19, 1998 · N73751 · Boeing 727227 · Spoilers
  > INSPECTION FOUND BOTTOM OF LT WING NR 7 SPOILER CORRODED. THE SPOILER WAS REPAIRED BY AVIATION COMPOSITES AND IAW WORK CARD 07-5750-1-2717..
- [SDR CALA9800533](https://openairdocs.org/sdr/CALA9800533.md): Skin · separated · Mar 19, 1998 · N73751 · Boeing 727227 · Elevator, Tab Structure
  > INSPECTION FOUND THE LT ELEVATOR CONTROL TAB INBOARD CORNER SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.
- [SDR CALA9800532](https://openairdocs.org/sdr/CALA9800532.md): Skin · separated · Mar 19, 1998 · N73751 · Boeing 727227 · Elevator, Tab Structure
  > INSPECTION FOUND THE RT ELEVATOR CONTROL TAB TRAILING EDGE SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.
- [SDR CALA9800531](https://openairdocs.org/sdr/CALA9800531.md): Support · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 846, RBL 1. THE FLOOR SUPPORT WAS REMOVED. A DOUBLER AND FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-1.
- [SDR CALA9800530](https://openairdocs.org/sdr/CALA9800530.md): Stringer · cracked · Mar 19, 1998 · N73751 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, AND 53-10-3, PAGE 43, DETAIL 11.
- [SDR CALA9800529](https://openairdocs.org/sdr/CALA9800529.md): Subfloor · corroded · Mar 19, 1998 · N73751 · Boeing 727227 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD LAV OUTBOARD SUBFLOOR CORRODED AT FS 294-344, RBL 43-63. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-1.

Next page: https://openairdocs.org/deregistered/N73751-2006-08-09/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 = 'N73751' AND deregistration_id = 'N73751-2006-08-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N73751-2006-08-09/reports

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