# Service difficulty reports: N188AT, cancelled Apr 25, 2006

A list on [N188AT, cancelled Apr 25, 2006](https://openairdocs.org/deregistered/N188AT-2006-04-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR AMTA200400526](https://openairdocs.org/sdr/AMTA200400526.md): Engine · vibration · May 5, 2004 · N188AT · Lkheed 10113851 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM.8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z ENGIEN CONTINUED TO WINDMILL AT APPROX 14 PERCENT N1 PLUS MADE OIL PRESS B2 + C2 ATM'S RUN CONTINUOU
- [SDR AMTA200301515](https://openairdocs.org/sdr/AMTA200301515.md): Light · damaged · Dec 23, 2003 · N188AT · Lkheed 10113851 · Emergency Lighting
  > FOUND EGRESS TRACK DAMAGED AFT OF 39H. REPAIRED DAMAGED EGRESS TRACK AS REQUIRED. (M)
- [SDR AMTA200301175](https://openairdocs.org/sdr/AMTA200301175.md): Charger · inoperative · Sep 15, 2003 · N188AT · Lkheed 1011 · Emergency Lighting
  > L3 DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED L3 DOOR EGRESS LIGHTING POWER PA CHECK IAW MM 33-51-03, OPS. CHECK NORMAL.
- [SDR AMTA200301125](https://openairdocs.org/sdr/AMTA200301125.md): Skin · corroded · Sep 3, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN CORRODED. REPAIRED DAMAGED AREA PER ER/A L10-53R-5272. (M)
- [SDR AMTA200301276](https://openairdocs.org/sdr/AMTA200301276.md): Skin · dented · Aug 27, 2003 · N188AT · Lkheed 10113851 · Leading Edge Devices
  > FOUND 5R SLAT L/E SKIN DENTED AT MID SECTION. REPAIRED SLAT L/E SKIN IAW SRM 57-51-00, FIG 807. (M)
- [SDR AMTA200301274](https://openairdocs.org/sdr/AMTA200301274.md): Attach Fitting · broken · Aug 25, 2003 · N188AT · Lkheed 10113851 · Wing, Attach Fittings
  > LT OUTBOARD AILERON OUTBOARD ACTUATOR WING SIDE ATTACH POINT ANTI-ROTATION TAB BROKEN. REPLACED AILERON ACTUATOR ATTACH FITTING IAW SRM 51-10-01 AND SRM 51-40-01. (M)
- [SDR AMTA200301102](https://openairdocs.org/sdr/AMTA200301102.md): Shear Tie · cracked · Aug 25, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Structure
  > FRAME, SHEAR TIE CRACKED AND CORRODED OUT OF LIMITS AT FS 1800 FROM STRINGER 33 TO STRINGER 36. REMOVED CRACKED AND CORRODED SECTION OF SHEAR TIE AND REPLACED WITH NEW SECTION IAW SRM 51-40-01. (M)
- [SDR AMTA200301266](https://openairdocs.org/sdr/AMTA200301266.md): Stringer · gouged · Aug 16, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > FOUND C2 PIT STRINGER GOUGED AND HAS ENLARGED HOLE. REPAIRED STRINGER IAW SRM 51-50-02 AND 51-21-02. (M)
- [SDR AMTA200301277](https://openairdocs.org/sdr/AMTA200301277.md): Skin · dented · Aug 15, 2003 · N188AT · Lkheed 10113851 · Leading Edge Devices
  > FOUND 7R SLAT SKIN DENTED AT OUTBOARD LEADING EDGE. REPAIRED SLAT SKIN IAW SRM 57-51-00, FIG 807. (M)
- [SDR AMTA200301100](https://openairdocs.org/sdr/AMTA200301100.md): Longeron · corroded · Aug 13, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 30 CORRODED AT APPROX FS 1808 JUST FWD OF APB FRAME. REPAIRED STRINGER IAW SRM 53-13-00 SEE PARTAIL ACCOMPLISHED AND ATTACHED M12A. (M)
- [SDR AMTA200301267](https://openairdocs.org/sdr/AMTA200301267.md): Web · cracked · Aug 12, 2003 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > C3 PIT WEB ABOVE STRINGER 29 IS CRACKED. REPAIRED WEB IAW SRM 53-23-00 AND 51-50-01, FIG 2. (M)
- [SDR AMTA200301099](https://openairdocs.org/sdr/AMTA200301099.md): Frame · corroded · Aug 12, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Frame
  > FOUND BULKHEAD FRAME, CORRODED BETWEEN STRINGER 33 AND STRINGER 39 AT FS 1809 APB. FRAME WAS REPAIRED PER SRM 53-11-00 FIG 848 REF M-12 1342M-12A 10591 ITEMS 5 AND 6 AT FS 1809 FROM STRINGER 40 TO BETWEEN STRINGER 24 AND 25, REF M-12A FOR OTHER SIGN-OFFS. (M
- [SDR AMTA200301101](https://openairdocs.org/sdr/AMTA200301101.md): Stringer · corroded · Aug 11, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER CORRODED NEAR APB. REMOVED CORRODED STRINGER SECTION AND REPAIRED IAW SRM 53-13-00. (M)
- [SDR AMTA200301086](https://openairdocs.org/sdr/AMTA200301086.md): Stiffener · corroded · Aug 11, 2003 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AFT OF STRINGER 33, CORRODED AT FRAME ATTACH POINT. INSTALLED FASTENERS AND REPAIR PARTS PER SRM 53-11-00 FIG 8 59. EDGE SEALED PER SRM 51-25-00. (M)
- [SDR AMTA200301265](https://openairdocs.org/sdr/AMTA200301265.md): Skin · dented · Aug 8, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED FORWARD OF LAV SERVICE DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-31-00, FIG 802. (M)
- [SDR AMTA200301278](https://openairdocs.org/sdr/AMTA200301278.md): Support · damaged · Aug 7, 2003 · N188AT · Lkheed 10113851 · Wing, Landing Gear Attach Fittings
  > INTERIM REPAIR OF CORROSION TO RIGHT MLG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4741. (M)
- [SDR AMTA200301279](https://openairdocs.org/sdr/AMTA200301279.md): Support · damaged · Aug 6, 2003 · N188AT · Lkheed 10113851 · Wing, Landing Gear Attach Fittings
  > INTERIM REPAIR OF LEFT MUG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4752. (M)
- [SDR AMTA200301094](https://openairdocs.org/sdr/AMTA200301094.md): Stiffener · corroded · Aug 6, 2003 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > ON APB RIGHT RADIAL STIFFENER IN C3 CARGO COMP AT STRINGER 25 CORROSION AROUND DRAIN HOLE. REPAIRED APB RT RADIAL STIFFENER AT STRINGER 25 IAW SRM 53-11-00. SEE M12A'S AND 156 FORMS FOR OTHER WORK ACCOMPLISHED AND PARTS FABRICATION. (M)
- [SDR AMTA200301137](https://openairdocs.org/sdr/AMTA200301137.md): Threshold · cracked · Aug 6, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Structure
  > C-2 CARGO THRESHOLD AFT TOP BEAM/TRACK CRACKED AT FASTENER HOLE WERE FLOOR PANEL AND THRESHOLD MEET. REMOVED AND REPLACED C-2 CARGO THRESHOLD AFT TOP BEAM WITH SERVICEABLE UNIT AS PER SRM 51-40-01. (M)
- [SDR AMTA200301135](https://openairdocs.org/sdr/AMTA200301135.md): Keelbeam · corroded · Aug 2, 2003 · N188AT · Lkheed 10113851 · Fuselage Main, Keel
  > TOP PORTION OF LOWER FLANGES OF BOTH KEELBEAMS CORRODED. AREA WAS REPAIRED PER E/R L10-53R-5281. (M)
- [SDR 200201206](https://openairdocs.org/sdr/200201206.md): Engine · bird ingestion · Sep 18, 2002 · N188AT · Lkheed 10113851 · Powerplant System
  > NR 2 ENGINE SHUTDOWN FOR HIGH VIBS, 2.6 BOTH CHANNELS. OIL PRESSURE 19 PSI, ALL PARAMETERS NORMAL. INSPECTED INLET AND EXHAUST, REMOVED EVIDENCE OF BIRD STRIKE FROM ONE BLADE, INSPECTED CHIP DETECTORS (NO DEBRIS FOUND), RAN ENGINE ANE PERFORMED TEST NR 11.
- [SDR 2002F00812](https://openairdocs.org/sdr/2002F00812.md): Fuel Filter · dirty · Aug 15, 2002 · N188AT · Lkheed 10113851 · Engine Fuel Distribution
  > ON DESCENT NR 3 ENGINE FUEL PRESSURE LIGHT ON, THROTTLES AT IDLE, ENGINE FLAMED-OUT. PERFORMED EMERGENCY RESTART, OK. REMOVED AND REPLACED NR 3 ENGINE LP FUEL FILTER IAW M/M 73-11-02, PERFORMED LP FUEL PUMP DRIVE TEST 19 OF M/M 71-00-00, OK.
- [SDR 2002F00431](https://openairdocs.org/sdr/2002F00431.md): Bulkhead · corroded · Mar 30, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Bulkhead
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON BULKHEAD LOWER WEB AT FS 315, LBL 18 TO RBL 18. MAINTENANCE REPLACED THE LOWER WEB IN ACCORDANCE WITH LOCKHEED SRM 51-40-01.
- [SDR 2002F00433](https://openairdocs.org/sdr/2002F00433.md): Channel · corroded · Mar 24, 2002 · N188AT · Lkheed 10113851 · Wing Miscellaneous Structure
  > DURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR TORQUE BOX LOWER AFT BATHTUB FITTING CHANNEL WAS CORRODED (LEVEL 2). MAINTENANCE REMOVED AND REPLACED THE FITTING CHANNEL IN ACCORDANCE WITH LOCKHEED SRM 51-40-01, FS 1230, WS 319 LEFT.
- [SDR 2002F00432](https://openairdocs.org/sdr/2002F00432.md): Doubler · cracked · Mar 19, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSPECTION A 3 INCH CRACK WAS DISCOVERED AT FESC INTERNAL SKIN DOUBLER. MAINTENANCE REPAIRED THE DOUBLER IN ACCORDANCE WITH AMTA ER/A L10-53R-4728 FS 315 TO 335, LBL 10 TO LBL 21.
- [SDR 2002F00350](https://openairdocs.org/sdr/2002F00350.md): Support · corroded · Mar 15, 2002 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION CABIN FLOORBEAM SUPPORT AT FS 1523, WL 195, RBL 83 HAD LEVEL 2 CORROSION. MAINTEANCE COMPLIED WITH AMTA ERA L10-53R-4737 FS 1523 FLOORBEAM SUPPORT MODIFICAITON.
- [SDR 2002F00430](https://openairdocs.org/sdr/2002F00430.md): Floorbeam · corroded · Mar 12, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Floor Beam
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON CABIN FLOORBEAM UPPER CAP, FS 901, WL 200, LBL 115 TO RBL 14. MAINTENANCE REPAIRED THE FLOORBEAM IN ACCORDANCE WITH LOCKHEED SRM 53-21-00, FIGURE 815.
- [SDR 2002F00323](https://openairdocs.org/sdr/2002F00323.md): Stringer · corroded · Mar 5, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > FORWARD FUSELAGE SECTION, STRINGER 30, FS 235 TO 297, BL 24 HAS LEVEL 2 CORROSION. MAINTENANCE REMOVED AND REPLACED STRINGER 30 AT STATION 235 - 297 IN ACCORDANCE WITH SRM 51-40-01.
- [SDR 2002F00321](https://openairdocs.org/sdr/2002F00321.md): Stiffener · cracked · Mar 3, 2002 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > MAIN FRAME VERTICAL STIFFENER ON FORWARD BULKHEAD OF LEFT ACM BAY IS CRACKED (LOWER STIFFENER) CRACK LENGTH 3.760 INCHES FS 315, BL 36L, WL 125. MAINTENANCE REPAIRED VERTICAL STIFFENER ON FORWARD BULKHEAD OF LEFT ACM BAY PER LOCKHEED SRM 53-11-00.
- [SDR 2002F00346](https://openairdocs.org/sdr/2002F00346.md): Shear Tie · corroded · Feb 27, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Structure
  > DURING SCHEDULED INSPECTION, FORWARD FUSELAGE SECTION, SHEAR TIE AT FS 297, RBL 8 TO 32 RIGHT WAS CORRODED, LEVEL 2 CORROSION. MAINTENANCE REMOVED AND REPLACED SHEAR TIE IAW SRM 53-12-00 FIG 805.
- [SDR 2002F00371](https://openairdocs.org/sdr/2002F00371.md): Frame · cracked · Feb 25, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION MAIN FRAME CHORD FS 315 WAS FOUND CRACKED AT RBL 22. CRACK WAS 1 INCH IN LENGTH. MAINTENANCE COMPLIED WITH ER/A L10-53R-4740, ER/A L10-53R-4733, AND SRM 51-40-01 FOR REPAIR.
- [SDR 2002F00349](https://openairdocs.org/sdr/2002F00349.md): Frame · cracked · Feb 24, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION MAIN FRAME, SPLICE ANGLE AND STRAP FOR FS 328 FRAMES WHERE FOUND TO BE CRACKED. 3 CRACKS WERE DISCOVERED AND EACH CRACK WAS 2.00 INCHES IN LENGTH. MAINTENANCE FABRICATED SPLICE ANGLE AND STRAP FOR FS 328 AFT SIDE OF CHORD CTR. INSTA
- [SDR 2002F00385](https://openairdocs.org/sdr/2002F00385.md): Floorbeam · corroded · Feb 18, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Floor Beam
  > DURING SCHEDULED INSPECTION FOUND LEVEL 2 CORROSION AT CABIN FLOOR SUPPORT, FLOORBEAM AT FS 865, LBL 34, RBL 39 AS VIEWED FROM LOWER GALLEY. MAINTENANCE REPAIRED AREA PER ER/A L10-53R-4727.
- [SDR 2002F00384](https://openairdocs.org/sdr/2002F00384.md): Torque Box · cracked · Feb 18, 2002 · N188AT · Lkheed 10113851 · Wing Main, Frame Structure
  > DURING SCHEDULED INSPECTION A 2 INCH CRACK WAS FOUND AT THE LEFT MAIN LANDING GEAR TORQUE BOX AFT WEB WALL, LOWER INBOARD CORNER. MAINTENANCE INSTALLED ANGLE AND WEB PER SRM 51-40-01, FS 1284, WSL 319, LBL 222.
- [SDR 2002F00383](https://openairdocs.org/sdr/2002F00383.md): Floor Support · corroded · Feb 18, 2002 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION WAS FOUND AT CABIN FLOOR SUPPORT, LOWER GALLEY, LOWER T-CAP ABOVE LEFT ELEVATOR DOOR FS 901, WL 190, RBL 55 TO LBL 38. MAINTENANCE REPAIRED AREA IN ACCORDANCE WITH ER/A L10-53R-4724.
- [SDR 2002F00382](https://openairdocs.org/sdr/2002F00382.md): Skin · corroded · Feb 15, 2002 · N188AT · Lkheed 10113851 · Elevator, Plate/Skin
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON LEFT ELEVATOR LOWER SURFACE FROM ES 180 TO ES 451. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IN ACCORDANCE WITH MM 27-31-03.
- [SDR 2002F00395](https://openairdocs.org/sdr/2002F00395.md): Floor Support · corroded · Feb 14, 2002 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION THE CABIN FLOOR SUPPORT FS 1521, RBL 48.5-74.5 WAS FOUND TO HAVE LEVEL 2 CORROSION. MAINTENANCE REPAIRED THE FLOOR SUPPORT AT FS 1521, RBL 48.5-74.5 IAW THE L1011 STRUCTURAL REPAIR MANUAL, 53-21-00, FIG 815. (M)
- [SDR 2002F00381](https://openairdocs.org/sdr/2002F00381.md): Splice · corroded · Feb 14, 2002 · N188AT · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON MOUNT PAD FOR NOSE LANDING GEAR RIGHT FORWARD GEAR DOOR FORWARD HINGE ATTACH BRACKET TO AIRFRAME, AFT SIDE FS 318 TO 355, RBL 22. MAINTENANCE REPAIRED LONGERON SPLICE IN ACCORDANCE WITH ER/A L10-53R-4712.
- [SDR 2002F00375](https://openairdocs.org/sdr/2002F00375.md): Pressure Panel · corroded · Feb 14, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Bulkhead
  > DURING SCHEDULED INSPECTION LEVEL 2 CORROSION ON NOSE LANDING GEAR WHEEL WELL TOP PANEL AT FS 369, RBL 22, AFT RIGHT OUTBOARD CORNER OF FORWARD WHEEL WELL PANEL FOUND. MAINTENANCE REPAIRED THE CORRODED AREA IN ACCORDANCE WITH ER/A L10-53R-4717.
- [SDR 2002F00322](https://openairdocs.org/sdr/2002F00322.md): Stringer · corroded · Feb 14, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > MID FUSELAGE SECTION, MAIN EQUIPMENT SERVICE CENTER, STRINGER 30, FS 930 TO 983, BL 25 AFT SIDE OF BULKHEAD 943 LEVEL 2 CORROSION. MAINTENANCE REPAIRED IN ACCORDANCE WITH SRM 53-13-00.
- [SDR 2002FA0000382](https://openairdocs.org/sdr/2002FA0000382.md): Stinger · corroded · Feb 13, 2002 · N188AT · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > FORWARD FUSELAGE SECTION, FORWARD E/E, SURFACE CORROSION ON TOP OF STRINGER 38, FS 297 TO FS 312, BL 45. MAINTENANCE REPAIRED STRINGER AT FS 297 TO 312 IAW SB.
- [SDR 99ZZZM48](https://openairdocs.org/sdr/99ZZZM48.md): Sensor · failed · Dec 31, 1998 · N188AT · Lkheed 10113851 · Landing Gear Position and Warning
  > DTW - DURING CLIMB, THE LANDING GEAR TRUCK WARNING LIGHT CAME ON. AIRCRAFT WAS RETURNED TO BLOCK. LANDED SAFELY. THE LEFT MAIN LANDING GEAR TRUCK POSITIONER WAS REPLACED IAW 32-32-03, LEAK CHECKED OK. (M)
- [SDR 98ZZZM464](https://openairdocs.org/sdr/98ZZZM464.md): Light · malfunctioned · May 16, 1998 · N188AT · Lkheed 10113851 · Emergency Lighting
  > DURING CRUISE, THE EMERGENCY EVACUATION LIGHTS CAME ON, HAD TO TURNOFF AT OVERHEAD PANEL. THE EMERGENCY SENSE C/B 'J6' POPPED, WOULD NOT RESET. CONTINUED FLT. T/S EMERGENCY LIGHT SYSTEM PER FIM 33-59-10 UNABLE TO DUPLICATE PROBLEM. SYSTEM OPERATIONAL. (M)
- [SDR 98ZZZM408](https://openairdocs.org/sdr/98ZZZM408.md): Light Panel · failed · Jan 2, 1998 · N188AT · Lkheed 10113851 · Emergency Lighting
  > CLE - WHEN REMOVING POWER FROM AIRCRAFT ALL EMERGENCY LIGHTS (INSIDE AND OUT) CAME ON. WOULD NOT TURN OFF UNTIL POWER WAS REAPPLIED TO AIRCRAFT. INSTALLED NEW EXTERIOR LIGHTS PANEL PER MM 33-51-01. EMERGNCY LIGHTS CHECKED NORMAL. (M)
- [SDR 95ZZZX5190](https://openairdocs.org/sdr/95ZZZX5190.md): Shut-Off Valve · inoperative · Jul 8, 1995 · N188AT · Lkheed 10113851 · Aircraft Fuel Distribution System
  > DTW - DURING CLIMB THROUGH 26,000 FEET, NR 3 ENGINE TANK VALVE FLOW BAR LIGHT WENT OUT WHICH WAS ASSOCIATED WITH NR 3 ENGINE FLAMING OUT. ENGINE WINDMILL FOR 20 MINUTES OIL PRESS. REPLACED NR 3 ENGINE FUEL TANK SHUT-OFF VALVE IAW MM 28-24-15 AND VALVE SWITCH
- [SDR 95ZZZW680](https://openairdocs.org/sdr/95ZZZW680.md): Tripler · cracked · Mar 28, 1995 · N188AT · Lkheed 10113851 · Passenger/Crew Doors
  > IND - DURING A 'C4' CHECK, THE L1 DOOR WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER, APPROX 1.5 INCHES LONG. A VISUAL INSPECTION DETECTED THIS CRACK TO A TRIPLER CUTOUT. STACKED DOUBLER ARRANGEMENT INSTALLED IAW SRM 53-31-00, FIG 836.

## 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 = 'N188AT' AND deregistration_id = 'N188AT-2006-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N188AT-2006-04-25/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.