# Service difficulty reports: N17407, cancelled Jan 18, 2002

A list on [N17407, cancelled Jan 18, 2002](https://openairdocs.org/deregistered/N17407-2002-01-18.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 · 68 reports

- [SDR CALA9900377](https://openairdocs.org/sdr/CALA9900377.md): Power Supply · inoperative · Apr 9, 1999 · N17407 · Boeing 727243 · Emergency Lighting
  > THE INTERIOR EMERGENCY EXIT LIGHTS FOR LEFT OVERWING DOOR WOULD NOT ILLUMINATE. THE POWER SUPPLY WAS REMOVED AND REPLACED.
- [SDR CALA9900143](https://openairdocs.org/sdr/CALA9900143.md): Battery · discharged · Feb 15, 1999 · N17407 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9900142](https://openairdocs.org/sdr/CALA9900142.md): Duct · failed · Feb 12, 1999 · N17407 · Boeing 727243 · Pneumatic Distribution System
  > NR 3 ENG FIRE WARNING ACTIVATED AFTER T/O FROM BWI. THE A/C WAS RETURNED TO BWI WHERE IT LANDED W/O INCIDENT. MX FOUND THE PNEUMATIC DUCT LEADING TO NR 3 NOSE COWL ANTI-ICE VALVE BLOWN. THE NOSE COWL FLANGE FITTING FOR COWL ANTI-ICE INLET WAS ALSO BLOWN. T
- [SDR CALA9900115](https://openairdocs.org/sdr/CALA9900115.md): Duct · broken · Feb 7, 1999 · N17407 · Boeing 727243 · Pneumatic Distribution System
  > A FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGI
- [SDR CALA9802196](https://openairdocs.org/sdr/CALA9802196.md): Anti Ice Duct · broken · Dec 24, 1998 · N17407 · Boeing 727243 · Air Intake Anti/De-Ice System
  > THE NR 3 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB-OUT OF IAH. THE ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. WHEN POWER WAS ADVANCED THE WARNING LIGHT CAME ON AGAIN. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT
- [SDR CALA9802172](https://openairdocs.org/sdr/CALA9802172.md): Chord · corroded · Dec 11, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT RT LAV FLOOR REINFORCEMENT CHORD CORRODED AT BS 1176, RBL 26. THE CORRODED AREA WAS BLENDED OUT. A FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5310-03799 AND BOEING SKETCH CAL-MIA-98-CC55TR.
- [SDR CALA9802171](https://openairdocs.org/sdr/CALA9802171.md): Track · corroded · Dec 10, 1998 · N17407 · Boeing 727243 · Trailing Edge Flaps
  > THE RT WING NR 5 FLAP TRACK WAS FOUND CORRODED. THE NR 5 FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-57-31.
- [SDR CALA9802170](https://openairdocs.org/sdr/CALA9802170.md): Fitting · cracked · Dec 10, 1998 · N17407 · Boeing 727243 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1.
- [SDR CALA9802168](https://openairdocs.org/sdr/CALA9802168.md): Cylinder · corroded · Dec 9, 1998 · N17407 · Boeing 727243 · Main Landing Gear Strut/Axle/Truck
  > INSPECTION FOUND THE RT MLG OUTER CYLINDER THREADS FOR GLAND NUT CORRODED. THE RT MLG WAS REMOVED AND REPLACED.
- [SDR CALA9802167](https://openairdocs.org/sdr/CALA9802167.md): Stiffener · cracked · Dec 9, 1998 · N17407 · Boeing 727243 · Elevator Structure
  > INSPECTION FOUND A.5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7.
- [SDR CALA9802166](https://openairdocs.org/sdr/CALA9802166.md): Fitting · corroded · Dec 9, 1998 · N17407 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-19297.
- [SDR CALA9802165](https://openairdocs.org/sdr/CALA9802165.md): Mount Pad · corroded · Dec 9, 1998 · N17407 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND NR 5 FLAP TRACK AFT MOUNTING FLANGE ON FALSE SPAR WORN AND CORRODED. THE MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 1.
- [SDR CALA9802164](https://openairdocs.org/sdr/CALA9802164.md): Skin · bent · Dec 9, 1998 · N17407 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD FOREFLAP INBOARD MOST UPPER SKIN LOOSE AND BENT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3.
- [SDR CALA9802158](https://openairdocs.org/sdr/CALA9802158.md): Power Supply · inoperative · Dec 9, 1998 · N17407 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND LT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW MM 33-50-0.
- [SDR CALA9802157](https://openairdocs.org/sdr/CALA9802157.md): Power Supply · inop · Dec 9, 1998 · N17407 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND RT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-0.
- [SDR CALA9802156](https://openairdocs.org/sdr/CALA9802156.md): Stiffener · corroded · Dec 9, 1998 · N17407 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.
- [SDR CALA9802155](https://openairdocs.org/sdr/CALA9802155.md): Skin · debonded · Dec 9, 1998 · N17407 · Boeing 727243 · Ailerons
  > INSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, PAGE 18 AND 51-8-4.
- [SDR CALA9802154](https://openairdocs.org/sdr/CALA9802154.md): Floorbeam · corroded · Dec 9, 1998 · N17407 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 34. A REPAIR WAS INSTALLED IAW ECRA 5310-03790.
- [SDR CALA9802153](https://openairdocs.org/sdr/CALA9802153.md): Angle · cracked · Dec 9, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN L ANGLE AT FORWARD I/B CORNER OF RT MLG WHEEL WELL, BEHIND APU, STA 870. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9802152](https://openairdocs.org/sdr/CALA9802152.md): Bracket · cracked · Dec 9, 1998 · N17407 · Boeing 727243 · Elevator Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN RT ELEVATOR NR 4 ATTACH HINGE BRACKET AT ELEVATOR STA 99.79. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2, PAGE 1, 51-10-1, AND 51-10-2.
- [SDR CALA9802151](https://openairdocs.org/sdr/CALA9802151.md): Stringer · cracked · Dec 8, 1998 · N17407 · Boeing 727243 · Wing, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED IAW EA 5762-01050.
- [SDR CALA9802150](https://openairdocs.org/sdr/CALA9802150.md): Stringer · cracked · Dec 8, 1998 · N17407 · Boeing 727243 · Vertical Stabilizer
  > INSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IAW SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-4 AND 51-10-2, PAGE 21.
- [SDR CALA9802149](https://openairdocs.org/sdr/CALA9802149.md): Skin · corroded · Dec 8, 1998 · N17407 · Boeing 727243 · Aileron Tabs
  > INSPECTION FOUND LT O/B AILERON TAB LOWER SURFACE CORRODED AT O/B END AND A SMALL DEBONDED AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PAGE 401-403.
- [SDR CALA9802148](https://openairdocs.org/sdr/CALA9802148.md): Chord · corroded · Dec 8, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHORD CORRODED IN COCKPIT FLOOR PANEL AT F/E SEAT AFT STOP. THE CHORD WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.
- [SDR CALA9802147](https://openairdocs.org/sdr/CALA9802147.md): Rib · cracked · Dec 8, 1998 · N17407 · Boeing 727243 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 3, 51-40-3, 51-10-6, PAGE 1, AND 51-10-1, PAGE 1.
- [SDR CALA9802146](https://openairdocs.org/sdr/CALA9802146.md): Skin · dented · Dec 8, 1998 · N17407 · Boeing 727243 · Aileron Tabs
  > INSPECTION FOUND RT O/B AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.
- [SDR CALA9802124](https://openairdocs.org/sdr/CALA9802124.md): Support · corroded · Nov 30, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT STA 420, RBL 62. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW 53-30-2 AND 51-30-2.
- [SDR CALA9802123](https://openairdocs.org/sdr/CALA9802123.md): Web · corroded · Nov 30, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED WHERE R-1 FORWARD DRAIN LINE FITTING ATTACHES, FS 378. THE CORRODED AREA OF WEB WAS REMOVED IAW SRM 51-40-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, PAGE 7 AND 51-10-2, PAGE 2.
- [SDR CALA9802122](https://openairdocs.org/sdr/CALA9802122.md): Bracket · cracked · Nov 30, 1998 · N17407 · Boeing 727243 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-7.
- [SDR CALA9802121](https://openairdocs.org/sdr/CALA9802121.md): Floorbeam · corroded · Nov 30, 1998 · N17407 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 1110, RBL 44. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8, PAGE 44.
- [SDR CALA9802111](https://openairdocs.org/sdr/CALA9802111.md): Bracket · cracked · Nov 25, 1998 · N17407 · Boeing 727243 · Leading Edge Slat Actuator
  > INSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2, FIGURE 1.
- [SDR CALA9802104](https://openairdocs.org/sdr/CALA9802104.md): Chord · cracked · Nov 24, 1998 · N17407 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.
- [SDR CALA9802102](https://openairdocs.org/sdr/CALA9802102.md): Skin · corroded · Nov 24, 1998 · N17407 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14.
- [SDR CALA9802097](https://openairdocs.org/sdr/CALA9802097.md): Floorbeam · corroded · Nov 23, 1998 · N17407 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO FLOORBEAM CORRODED AT STA 1070, RBL 12 TO 48. A REPAIR WAS INSTALLED IAW SRM 53-10-8.
- [SDR CALA9802094](https://openairdocs.org/sdr/CALA9802094.md): Angle · cracked · Nov 23, 1998 · N17407 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED IAW SRM 51-30-2, PAGE 3 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-2, PAGE 12 AND 51-30-2
- [SDR CALA9802093](https://openairdocs.org/sdr/CALA9802093.md): Stiffener · cracked · Nov 23, 1998 · N17407 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.
- [SDR CALA9800361](https://openairdocs.org/sdr/CALA9800361.md): Light · inoperative · Mar 2, 1998 · N17407 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT ROW 28 AND 29 INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED. ALSO, MAINTENANCE FOUND PIN AT SIGN CANNON PLUG BENT AND BROKEN WIRING. THE PIN AND WIRING WERE REPAIRED AND OPERATION OF THE LIGHT WAS NORMAL.
- [SDR CALA9800092](https://openairdocs.org/sdr/CALA9800092.md): Frame · cracked · Jan 20, 1998 · N17407 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3.5 CRACK IN UPPER AFT CORNER OF R-1 DOOR FRAME. A REPAIR WAS FABRICATED AND INSTALLED IAW DRAWING 69-69978, SRM 57-10-02, AND ECRA 5240-01223.
- [SDR CALA9800091](https://openairdocs.org/sdr/CALA9800091.md): Lugs · corroded · Jan 19, 1998 · N17407 · Boeing 727243 · Horizontal Stabilizer Structure
  > INSPECTION FOUND HORIZONTAL STABILIZER LEFT AND RIGHT BEARING SUPPORT VERTICAL LUGS CORRODED. THE LT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01033. THE RT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01141.
- [SDR CALA9800090](https://openairdocs.org/sdr/CALA9800090.md): Skin · corroded · Jan 19, 1998 · N17407 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING INBOARD MID-FLAP UPPER SKIN PILLOWED WITH DISHED FASTENERS IN AREA ABOVE REAR SPAR UPPER CHORD APPROXIMATELY 21 INCHES FROM INBOARD END AND EXTENDING OUTBOARD 6.5 INCHES. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SR
- [SDR CALA9800083](https://openairdocs.org/sdr/CALA9800083.md): Torus · cracked · Jan 19, 1998 · N17407 · Boeing 727243 · APU Core Engine
  > INSPECTION FOUND A 5 INCH CRACK IN INBOARD WELD SEAM OF APU TORUS ASSEMBLY. THE APU WAS REMOVED AND REPLACED IAW MM 49-10-01. LEAK AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA9800082](https://openairdocs.org/sdr/CALA9800082.md): Skin · corroded · Jan 17, 1998 · N17407 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1060, STRINGER 27L. THE CORROSION WAS REMOVED AND THE SKIN WAS REPAIRED IAW SRM 53-30-3.
- [SDR CALA9800081](https://openairdocs.org/sdr/CALA9800081.md): Floorbeam · corroded · Jan 17, 1998 · N17407 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUTS, STA 380, RBL 24 TO RBL 62. TWO L-ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-30-8 FIGURE 8.
- [SDR CALA9800080](https://openairdocs.org/sdr/CALA9800080.md): Floorbeam · corroded · Jan 17, 1998 · N17407 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUT ON UPPER FORWARD FLANGE LOWER SURFACE AT STA 328, LBL 48. THE FLOORBEAM WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-10-8 AND 53-20-11.
- [SDR CALA9701252](https://openairdocs.org/sdr/CALA9701252.md): Slide · low pressure · Aug 29, 1997 · N17407 · Boeing 727243 · Escape Slide
  > THE CREW FOUND L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE L-1 DOOR SLIDE WAS REMOVED AND REPLACED PER MM 25-60-15.
- [SDR CALA9601700](https://openairdocs.org/sdr/CALA9601700.md): Angle · cracked · Nov 13, 1996 · N17407 · Boeing 727243 · Spoilers
  > INSPECTION FOUND RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING INBOARD ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.
- [SDR CALA9601687](https://openairdocs.org/sdr/CALA9601687.md): Skin · corroded · Nov 6, 1996 · N17407 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN CORRODED UNDER WEB IN AFT CARGO COMPARTMENT AT STA 970, STRINGER 28L. THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9601689](https://openairdocs.org/sdr/CALA9601689.md): Stringer · corroded · Nov 5, 1996 · N17407 · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28L CORRODED AT STA 965 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A REPLACEMENT STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.
- [SDR CALA9601697](https://openairdocs.org/sdr/CALA9601697.md): Rib · cracked · Nov 3, 1996 · N17407 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-3.
- [SDR CALA9601696](https://openairdocs.org/sdr/CALA9601696.md): Rib · cracked · Nov 3, 1996 · N17407 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A.75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N17407-2002-01-18/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 = 'N17407' AND deregistration_id = 'N17407-2002-01-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17407-2002-01-18/reports

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