# Service difficulty reports: N12327, cancelled Feb 7, 2012

A list on [N12327, cancelled Feb 7, 2012](https://openairdocs.org/deregistered/N12327-2012-02-07.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 · 72 reports

- [SDR CALA0700611](https://openairdocs.org/sdr/CALA0700611.md): Skin · cracked · Oct 25, 2007 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727E + 3, S23L. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, PROCEDURE 5.
- [SDR CALA0700610](https://openairdocs.org/sdr/CALA0700610.md): Skin · cracked · Oct 25, 2007 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF OF STA 727E AND JUST BELOW STRINGER 23R. REPAIRED IAW ECRA 5331-01359.
- [SDR CALA0700609](https://openairdocs.org/sdr/CALA0700609.md): Skin · cracked · Oct 25, 2007 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D, S23R BELOW EMERGENCY LIGHT. REPAIRED IAW ECRA 5331-01359.
- [SDR CALA0700007](https://openairdocs.org/sdr/CALA0700007.md): Stringer · corroded · Jan 4, 2007 · N12327 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD BAGGAGE BIN AT STA 500A+10 TO 500C. THE CORRODED STRINGER SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0700006](https://openairdocs.org/sdr/CALA0700006.md): Keelbeam · corroded · Jan 4, 2007 · N12327 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND FUSELAGE SKIN BULGING AT S28L BETWEEN STA 500C AND 500D, 6 INCHES LEFT OF AIRCRAFT CENTERLINE. REPLACED FORWARD SECTION OF LT KEEL BEAM IAW SRM 53-60-12.
- [SDR CALA0700002](https://openairdocs.org/sdr/CALA0700002.md): Angle · cracked · Jan 3, 2007 · N12327 · Boeing 7373T0 · Service Doors
  > INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT R-1 DOOR TORQUE BOX UPPER FORWARD ATTACH HOLES, NEAREST TORQUE TUBE. THE ANGLE WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0600548](https://openairdocs.org/sdr/CALA0600548.md): Door Frame · cracked · Dec 31, 2006 · N12327 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A 1.5 INCH CRACK AT LOWER STOP PAD BRACKET OF FORWARD CARGO DOOR CUTOUT AFT FRAME, STA 493. THE FRAME WAS REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723.
- [SDR CALA0500082](https://openairdocs.org/sdr/CALA0500082.md): Actuator · inoperative · Mar 17, 2005 · N12327 · Boeing 7373T0 · Landing Gear Actuator
  > CREW REPORTED THAT THE NOSE LANDING GEAR REQUIRED A MANUAL EXTENSION ON APPROACH TO DTW. EXTENSIVE TROUBLESHOOTING WAS PERFORMED. MAINTENANCE FOUND THAT THE NLG LOCK ACTUATOR WAS AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-00. A F
- [SDR CALA0500058](https://openairdocs.org/sdr/CALA0500058.md): Actuator · malfunctioned · Feb 23, 2005 · N12327 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THE GEAR WAS CYCLED DURING A GO-AROUND AND THREE GREEN SAFE GEAR LIGHTS ILLUMINATED. A VISUAL INSPECTION OF THE GEAR ALSO REVEALED GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDE
- [SDR CALA0400739](https://openairdocs.org/sdr/CALA0400739.md): Actuator · inoperative · Dec 7, 2004 · N12327 · Boeing 7373T0 · Landing Gear Actuator
  > THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS LOWERED ON APPROACH TO IAH. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH NORMAL INDICATIONS. MAINTENANCE FOUND THE NLG LOCK ACTUA
- [SDR CALA0400688](https://openairdocs.org/sdr/CALA0400688.md): Skin · cracked · Oct 28, 2004 · N12327 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A.25 INCH CRACK IN NR 3 SLAT SKIN BELOW ACTUATOR. A DOUBLER WAS INSTALLED ON LOWER SKIN IAW SRM 57-43-01.
- [SDR CALA0400687](https://openairdocs.org/sdr/CALA0400687.md): Floorbeam · corroded · Oct 24, 2004 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, LBL 6 TO RBL 6. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA0400686](https://openairdocs.org/sdr/CALA0400686.md): Floorbeam · corroded · Oct 23, 2004 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 344, RBL 45 TO LBL 12. THE CORRODED AREA OF FLOORBEAM UPPER CHORD WAS REMOVED AND A NEW UPPER CHORD AND SPLICES WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA0400684](https://openairdocs.org/sdr/CALA0400684.md): Floorbeam · corroded · Oct 22, 2004 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND THE UPPER FLANGE OF FLOORBEAM CORRODED AT NUT PLATE HOLE, STA 312, RBL 8. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0400680](https://openairdocs.org/sdr/CALA0400680.md): Floorboard · corroded · Oct 19, 2004 · N12327 · Boeing 7373T0 · Fuselage Floor Panel
  > INSPECTION FOUND UPPER AFT FLANGE OF CABIN FLOORBOARD CORRODED AT NUT PLATE HOLE, STA 360, RBL 2. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51.
- [SDR CALA0400580](https://openairdocs.org/sdr/CALA0400580.md): Valve · inoperative · Jul 19, 2004 · N12327 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. A MANUAL EXTENSION WAS PERFORMED AND THE NOSE GEAR SHOWED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. L
- [SDR CALA0400569](https://openairdocs.org/sdr/CALA0400569.md): Actuator · inoperative · Jul 8, 2004 · N12327 · Boeing 7373T0 · Landing Gear Actuator
  > THE NOSE LANDING GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. THE RED UNSAFE LIGHT WAS ILLUMINATED. THE GEAR WAS CYCLED AND THE NLG EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT.
- [SDR CALA0400555](https://openairdocs.org/sdr/CALA0400555.md): Actuator · inoperative · Jun 28, 2004 · N12327 · Boeing 7373T0 · Landing Gear Actuator
  > THE NOSE GEAR DID NOT EXTEND INITIALLY WHEN THE GEAR WAS SELECTED DOWN ON APPROACH INTO IAH. THE GEAR WAS CYCLED RESULTING IN NORMAL EXTENSION AND INDICATIONS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. T
- [SDR CALA0400220](https://openairdocs.org/sdr/CALA0400220.md): Engine · malfunctioned · Mar 6, 2004 · N12327 · Boeing 7373T0 · Engine (Turbine/Turboprop)
  > THE NR 1 ENGINE EXPERIENCED A POWER LOSS AT CRUISE WHILE EN ROUTE FROM MCO TO CLE. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED IAW MM 71-00-00. SHOP TEARDOWN REVEALED A FAILED NR 4 BEARING.
- [SDR CALA0300120](https://openairdocs.org/sdr/CALA0300120.md): Skin · cracked · Mar 19, 2003 · N12327 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 5" CRACK IN SKIN AT AFT CARGO DOOR INSIDE INSPECTION HOLE ABOVE HANDLE BOX. A DOUBLER WAS INSTALLED IAW ECRA 5232-01024.
- [SDR CALA0200588](https://openairdocs.org/sdr/CALA0200588.md): Skin · cracked · Dec 16, 2002 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2.25" CRACK IN L/H FUSELAGE SKIN ABOUT TWO FEET AFT OF EMERGENCY LIGHT, AFT OF LEFT WHEEL WELL, STA 727E, S24L. REPAIRED IAW ECRA 5330-03188.
- [SDR CALA0200506](https://openairdocs.org/sdr/CALA0200506.md): Ballast · Oct 25, 2002 · N12327 · Boeing 7373T0 · Water and Waste System
  > SMOKE IN AFT LAVATORY. LEFT AFT LAVATORY MIRROR CIRCUIT BREAKER OUT. FOUND BREAKER FOR LIGHTS POPPED. BALLAST BURNT. REMOVED AND REPLACED BALLAST.
- [SDR CALA0001968](https://openairdocs.org/sdr/CALA0001968.md): Skin · cracked · Dec 20, 2000 · N12327 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND C-1 DOOR INNER SKIN CRACKED AROUND LIGHTENING HOLES. THE CRACKS WERE 1/2 TO 1 INCH LONG. THE SKIN WAS REPAIRED BY INSTALLING DOUBLERS IAW ECRA 5231-01029.
- [SDR CALA0001967](https://openairdocs.org/sdr/CALA0001967.md): Skin · dented · Dec 20, 2000 · N12327 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND C-1 DOOR SKIN DENTED. THE DOOR SKIN WAS REMOVED AND REPLACED IAW OHM 52-36-02 AND DRAWING 65-46921.
- [SDR CALA0001966](https://openairdocs.org/sdr/CALA0001966.md): Pan · cracked · Dec 20, 2000 · N12327 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN C-1 DOOR LOWER FORWARD DOOR PAN. THE LOWER FORWARD DOOR PAN WAS REMOVED AND REPLACED IAW OHM 52-36 AND DRAWING 65-46821.
- [SDR CALA0001938](https://openairdocs.org/sdr/CALA0001938.md): Skin · cracked · Dec 17, 2000 · N12327 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1/4 INCH CRACK IN NR 2 OB PYLON SKIN AFT OF UPPER T/R ABOVE PANEL 5824R. A DOUBLER AND FREEZE PLUGS WERE INSTALLED IAW SRM 5450-01330 AND ECRA 5430-01204.
- [SDR CALA0001911](https://openairdocs.org/sdr/CALA0001911.md): Cargo Track · corroded · Dec 13, 2000 · N12327 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND TIE DOWN RAIL CORRODED AT STA 500D-520 BETWEEN STRINGER 26L AND 27L. THE CORRODED SECTION OF TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53.
- [SDR CALA0001910](https://openairdocs.org/sdr/CALA0001910.md): Panel · corroded · Dec 13, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TRANSITION PANELS CORRODED AT STA 420, S26R, STA 492-520, S26L, STA 380-492, S26L, AND STA 500C +18R. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-10-2 AND 53-30-53.
- [SDR CALA0001906](https://openairdocs.org/sdr/CALA0001906.md): Web · cracked · Dec 13, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5" CRACK IN WEB AT STA 500C, LONGERON 26L IN FORWARD CARGO AREA. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0001905](https://openairdocs.org/sdr/CALA0001905.md): Web · cracked · Dec 13, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 12 INCH CRACK IN WEB AT LT SIDE OF FORWARD CARO AREA BETWEEN STA 500A AND 500B, STRINGER 25L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0001899](https://openairdocs.org/sdr/CALA0001899.md): Panel · corroded · Dec 12, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L/H TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES AT STA 877-947. A NEW TRANSITION PANEL WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0001879](https://openairdocs.org/sdr/CALA0001879.md): Skin · cracked · Dec 11, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN KEEL BEAM LOWER SKIN AT STA 706, LBL 6, WL 148.5. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-12, FIGURE 202, SHEET 3.
- [SDR CALA0001875](https://openairdocs.org/sdr/CALA0001875.md): Skin · dented · Dec 9, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 338-353 BETWEEN STRINGERS 19R AND 20R. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210.
- [SDR CALA0001874](https://openairdocs.org/sdr/CALA0001874.md): Stringer · cracked · Dec 8, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN STRINGER 14L AT BS 360. THE STRINGER WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0001865](https://openairdocs.org/sdr/CALA0001865.md): Support · corroded · Dec 5, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT DIAGONAL SUPPORT CORRODED AT STA 986-1016. A NEW DIAGONAL SUPPORT WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0001861](https://openairdocs.org/sdr/CALA0001861.md): Intercostal · cracked · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AFT OF BS 302 AT STRINGER 4L. A NEW STRAP AND INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA0001860](https://openairdocs.org/sdr/CALA0001860.md): Floor Support · corroded · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-1006, RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0001859](https://openairdocs.org/sdr/CALA0001859.md): Skin · dented · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 388, S16L. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201 AND 51-40-03, PARAGRAPH 4D.
- [SDR CALA0001858](https://openairdocs.org/sdr/CALA0001858.md): Angle · corroded · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT Z-ANGLE CORRODED BETWEEN STA 947 AND 998. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0001857](https://openairdocs.org/sdr/CALA0001857.md): Floorbeam · corroded · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AROUND FASTENERS AT STA 1016, RBL 5 TO RBL 6. A FLOORBEAM UPPER CHORD REPLACEMENT SECTION WAS INSTALLED IAW ECRA 5310-03851.
- [SDR CALA0001856](https://openairdocs.org/sdr/CALA0001856.md): Web · corroded · Dec 4, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED BETWEEN STA 1006 AND 1016, RBL 32. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0001854](https://openairdocs.org/sdr/CALA0001854.md): Spindle · corroded · Dec 3, 2000 · N12327 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING O/B MID NR 7 AND NR 8 FLAP MAIN CARRIAGE SPINDLES CORRODED. THE NR 7 AND NR 8 FLAP MAIN CARRIAGES WERE REMOVED AND REPLACED IAW MM 27-51-44.
- [SDR CALA0001853](https://openairdocs.org/sdr/CALA0001853.md): Floorbeam · corroded · Dec 2, 2000 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 6 TO LBL 27. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.
- [SDR CALA0001849](https://openairdocs.org/sdr/CALA0001849.md): Splice · cracked · Dec 1, 2000 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 1.25" CRACK IN STRINGER SPLICE AT BS 907, S4R. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0001843](https://openairdocs.org/sdr/CALA0001843.md): Seat Track · corroded · Dec 1, 2000 · N12327 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 924-933, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204, SHEETS 1-4.
- [SDR CALA9601902](https://openairdocs.org/sdr/CALA9601902.md): Skin · cracked · Dec 23, 1996 · N12327 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A.5 INCH CRACK AT RIVET IN LOWER SKIN OF NR 6 SLAT AT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159.
- [SDR CALA9601918](https://openairdocs.org/sdr/CALA9601918.md): Floorbeam · corroded · Dec 19, 1996 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, R-2 DOOR TO L-2 DOOR. A FLOORBEAM UPPER CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03385.
- [SDR CALA9601903](https://openairdocs.org/sdr/CALA9601903.md): Floorbeam · corroded · Dec 12, 1996 · N12327 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 5 AND LBL 5. A REPAIR WAS INSTALLED IAW SRM 53-50-01.
- [SDR CALA9601921](https://openairdocs.org/sdr/CALA9601921.md): Support · corroded · Dec 11, 1996 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 951, 12 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT CORRODED AT STA 951, 20 INCHES FROM RIGHT SIDEWALL. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03381.
- [SDR CALA9601920](https://openairdocs.org/sdr/CALA9601920.md): Support · corroded · Dec 11, 1996 · N12327 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED FROM STA 947.5 TO 967, 18 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT CORRODED FROM 967 TO 986.5, 18 INCHES LEFT OF CENTER. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03381.

Next page: https://openairdocs.org/deregistered/N12327-2012-02-07/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 = 'N12327' AND deregistration_id = 'N12327-2012-02-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12327-2012-02-07/reports

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