# Service difficulty reports: N367PA, cancelled Mar 27, 2006

A list on [N367PA, cancelled Mar 27, 2006](https://openairdocs.org/deregistered/N367PA-2006-03-27.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 · 51 reports

- [SDR RIVA0000027](https://openairdocs.org/sdr/RIVA0000027.md): Nose Cowl · cracked · Aug 25, 2000 · N367PA · Boeing 727221 · Engine Cowling System
  > PSM, CRACK AT NR 3 NOSE COWL AT 12 O''CLOCK POS AT NAC STA 77.5, 6 AFT OF COWL L/E. DAMAGE AREA WAS CUT OUT OF NOSE COWL AT NAC STA 77.5. THE REP PLATE WAS FAB FROM.050 2024T-3. DRILLED EXISTING (AND REPAIRED) HOLES ONTO REP PLATE. DEBURRED ALL EDGES ON N
- [SDR RIVA0000028](https://openairdocs.org/sdr/RIVA0000028.md): Connector · damaged · Aug 24, 2000 · N367PA · Boeing 727221 · Smoke Detection
  > ADW, AT T/O, A FIRE BELL, FIRE WARN LIGHT, ENG FAIL LIGHT AND GROUND FAULT LIGHT ILLUM. THE CHECKLIST WAS COMPLETED AND THE TAKEOFF WAS ABORTED. THE A/C RETURNED BACK TO THE GATE W/O INCIDENT. THE NR3 ENG. AND PYLON FIRE DETECT. SYS WERE INSP. THE NR 3 ENG
- [SDR RIVA0000024](https://openairdocs.org/sdr/RIVA0000024.md): Clamp · displaced · Aug 18, 2000 · N367PA · Boeing 727221 · Crew Oxygen System
  > BGR, ON CLIMBOUT, THE NR 3 ENGINE INDICATED A FIRE WARNING AT 6500 FEET. THE ENGINE WAS SECURED BY THE APPROPRIATE CHECK LIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO BGR. AFTER LANDING, FIRE RESCUE CONFIRMED THAT THERE WAS NO FIRE. THE
- [SDR RIVA0000023](https://openairdocs.org/sdr/RIVA0000023.md): Duct · leaking · Aug 17, 2000 · N367PA · Boeing 727221 · Crew Oxygen System
  > BGR, ON CLIMBOUT AT 6000 FEET, THE NR 3 ENGINE INDICATED A FIRE WARNING. THE ENGINE WAS SECURED BY THE APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BGR.UPON INSPECTION, A PNEUMATIC DUCT LEAK WAS FOUND BLOWING BLEED AIR ON THE
- [SDR RIVA0000021](https://openairdocs.org/sdr/RIVA0000021.md): Connector · shorted · Jul 27, 2000 · N367PA · Boeing 727221 · Fire Detection
  > UPON APPROACH TO PIT, THE NR 3 ENGINE FIRE BELL SOUNDED WITH NO ASSOCIATED ENGINE FIRE LIGHT. THE SYSTEM TESTED NORMAL. THE NR 3 ENGINE DETECTOR GROUND LIGHT MOMENTARILY FLICKERED. AFTER LANDING, THE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED STEADILY. THE
- [SDR RIVA0000020](https://openairdocs.org/sdr/RIVA0000020.md): Fire Loop · malfunctioned · Jul 24, 2000 · N367PA · Boeing 727221 · Smoke Detection
  > YYZ - ON CLIMB-OUT AFTER TAKEOFF, THE ENGINE FIRE BELL AND LIGHT OPERATED INDICATING AN ENGINE FIRE. THE NR 3 ENGINE FIRE HANDLE WAS LIGHTED. THE EMERGENCY CHECK LIST WAS COMPLETED. THE AIRCRAFT RETURNED TO YYZ WITHOUT INCIDENT. NO FIRE WAS VISIBLE BY THE
- [SDR RIVA0000019](https://openairdocs.org/sdr/RIVA0000019.md): Duct · loose · Jul 23, 2000 · N367PA · Boeing 727221 · Engine Start Valves/Controls
  > AT 110 KNOTS ON TAKEOFF, THE NR 3 FIRE LIGHT WARN BELL AND GROUND FAULT LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE AT PSM WITHOUT INCIDENT. AN AIR DUCT ON THE START VALVE WAS FOUND TO BE LOOSE. THE DUCT WAS SECURED AND
- [SDR RIVA0000018](https://openairdocs.org/sdr/RIVA0000018.md): Fire Warning · false activation · Jul 22, 2000 · N367PA · Boeing 727221 · Fire Detection
  > PIT - AT 70 KNOTS ON TAKEOFF ROLL, THE NR 3 FIRE LIGHT, WARNING BELL AND GROUND FAULT LIGHT ILLUMINATED. THE BELL WENT OUT, AND WITH RETARDED THROTTLE, THE FIRE LIGHT EXTINGUISHED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE AT PIT WITHOUT INCI
- [SDR RIVA0000017](https://openairdocs.org/sdr/RIVA0000017.md): Csd · malfunctioned · Jul 20, 2000 · N367PA · Boeing 727221 · Alternator-Generator Drive
  > PSM - ON CLIMB-OUT, THE NR 3 CSD GENERATOR DRIVE OIL TEMPERATURE STEADILY ROSE TO APPROXIMATELY 155 DEGREES CELCIUS. AT THAT POINT, THE NR 3 GENERATOR CIRCUIT BREAKER TRIPPED. VOLTS AND FREQUENCY WERE NORMAL. THE AIRCRAFT RETURNED TO PSM WITHOUT INCIDENT.
- [SDR RIVA0000015](https://openairdocs.org/sdr/RIVA0000015.md): Skin · worn · Jul 12, 2000 · N367PA · Boeing 727221 · Leading Edge Devices
  > DURING C CHECK INSPECTION, IT WAS NOTED THAT THE RIGHT WING OUTBOARD FOREFLAP HAS A WEAR MARK IN SKIN AT LEADING EDGE, INBOARD OF INBOARD SEQUENCE CARRIAGE ATTACH BEARING. INSTALLED PATCH ON RIGHT WING OUTBOARD FOREFLAP LEADING EDGE (INBOARD OF INBOARD SEQUEN
- [SDR RIVA0000014](https://openairdocs.org/sdr/RIVA0000014.md): Structure · cracked · Jul 12, 2000 · N367PA · Boeing 727221 · Leading Edge Devices
  > DURING C CHECK INSPECTION, IT WAS NOTED THAT THE NR 2 SLAT HAS TWO CRACKS AT EDGE OF LIGHTENING HOLES. REMOVED FASTENERS IN THE NR 2 SLAT COVE PANEL IAW B727 SRM 51-30-2. BLENDED OUT ONE CRACK IAW SRM 57-50-1, REMOVED DAMAGED AREA OF OTHER CRACK IAW SRM 51-4
- [SDR RIVA0000016](https://openairdocs.org/sdr/RIVA0000016.md): Floorbeam · corroded · Jul 12, 2000 · N367PA · Boeing 727221 · Fuselage Main, Floor Beam
  > DURING C CHECK INSPECTION, IT WAS NOTED THAT ON THE LOWER SURFACE ON FLOORBEAM FLANGES AT STATION 344 HAVE CORROSION THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-8 FIG 1. REPAIRED CORRODED UPPER CHORD OF FUSELAGE FLOORBEAM AT STATION 344 FROM LBL 60 TO RB
- [SDR EISA98001](https://openairdocs.org/sdr/EISA98001.md): Engine · failed · Jan 14, 1998 · N367PA · Boeing 727221 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED ON GO AROUND. REMOVED AND REPLACED NR 2 ENGINE. (M)
- [SDR EISA97286](https://openairdocs.org/sdr/EISA97286.md): Wire · broken · Jan 4, 1998 · N367PA · Boeing 727221 · Engine Oil System Wiring
  > NR 2 OIL TEMP ABOVE RED LINE ON TAKEOFF ENGINE SHUTDOWN. REPAIRED BROKEN WIRE AT TEMP BULB ON NR 2 ENGINE, OPS CHECK NORMAL. (M)
- [SDR EISA97099](https://openairdocs.org/sdr/EISA97099.md): Receiver · inop · May 20, 1997 · N367PA · Boeing 727221 · Visual Omnirange (VOR) System
  > ON DEPART NR 1 VHF NAV INOP, RETURNED TO DFW. REPLACED NR 1 NAV RECEIVER. (M)
- [SDR EISA97032](https://openairdocs.org/sdr/EISA97032.md): Battery Pack · discharged · Feb 3, 1997 · N367PA · Boeing 727221 · Emergency Lighting
  > AFT SLIDE EMEGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. (M)
- [SDR EISA97004](https://openairdocs.org/sdr/EISA97004.md): Oil Press Switch · inoperative · Jan 14, 1997 · N367PA · Boeing 727221 · Engine Oil Pressure
  > NR 2 ENGINE OIL FILTER BYPASS/LOW PRESS LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED NR 2 LOW PRESS SWITCH. (M)
- [SDR EISA96285](https://openairdocs.org/sdr/EISA96285.md): Adi · inop · Dec 27, 1996 · N367PA · Boeing 727221 · Integrated Flight System
  > F/O'S ADI GYRO FLAG IN VIEW IN BOTH NORMAL AND ALTERNATE. REMOVED AND REPLACED F/O'S ADI. OPS CHECK GOOD IAW MM 34-23-11. (M)
- [SDR EISA95052](https://openairdocs.org/sdr/EISA95052.md): Floor Beam · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1130, LBL 10 INCHES, WL 208.1. REPAIRED PER DRAWING HSE-53-151. (Z)
- [SDR EISA95051](https://openairdocs.org/sdr/EISA95051.md): Beam · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON BS 1183 VERTICAL BEAM AT BL '0', WL 148. REPAIRED PER DRAWING HSE2-53-154 AND HSE2-53-150. (Z)
- [SDR EISA95050](https://openairdocs.org/sdr/EISA95050.md): Stringer · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AND 30, BETWEEN BS 990 AND 1010. REPAIRED PER DRAWING HSE2-53-147 AND BOEING FAX C00-SJ0-95-0037RR. (Z)
- [SDR EISA95049](https://openairdocs.org/sdr/EISA95049.md): Skin · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION BULGES AT AFT LAVATORY SERVICE PANEL. REPAIRED PER SRM 51-10-1 PAGE 4. (Z)
- [SDR EISA95048](https://openairdocs.org/sdr/EISA95048.md): Spar · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, STATION 223.05. REPAIRED PER DRAWING HSE2-55-146. (Z)
- [SDR EISA95047](https://openairdocs.org/sdr/EISA95047.md): Angle · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 970 TO BS 990, BL '0'. REPLACED PER SRM 51-10-1, PARA 4A, PAGE 4. (Z)
- [SDR EISA95046](https://openairdocs.org/sdr/EISA95046.md): Floor Beam · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1030, WL 208.1, LBL 1 INCH. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z)
- [SDR EISA95045](https://openairdocs.org/sdr/EISA95045.md): Intercostal · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL, BS 1110 TO BS 1130, BL '0'. REPAIRED PER SRM 51-10-1. (Z)
- [SDR EISA95044](https://openairdocs.org/sdr/EISA95044.md): Support · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BSL 1110 TO BS 1030, LBL 12 INCH. REPLACED PER SRM 51-10-1 PARAGRAPH 4A, FIGURE 4. (Z)
- [SDR EISA95043](https://openairdocs.org/sdr/EISA95043.md): Support · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT BS 1050 TO 1070, LBL 22. REPLACED PER SRM 51-30-2. (Z)
- [SDR EISA95042](https://openairdocs.org/sdr/EISA95042.md): Seat Track · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1070 TO BS 1140, WL 208.1, LBL 55 INCHES. REPAIRED PER SRM 51-10-1 PAGE 4. (Z)
- [SDR EISA95041](https://openairdocs.org/sdr/EISA95041.md): Seat Track · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1090 TO BS 1140, WL 208.1, LBL 24.75. REPLACED PER SRM 51-10-1. (Z)
- [SDR EISA95040](https://openairdocs.org/sdr/EISA95040.md): Track · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BSL 1090 TO BS 1140, WL 208.1, LBL 45.5. REPLACED PER SRM 53-10-5, FIGURE 7. (Z)
- [SDR EISA95039](https://openairdocs.org/sdr/EISA95039.md): Angle · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 1138 TO BS 1158, WL 208.1. REPAIRED PER SRM 51-10-1. (Z)
- [SDR EISA95038](https://openairdocs.org/sdr/EISA95038.md): Support · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BS 1110 TO 1130, LBL 12, WL 208.1. REPAIRED PER SRM 51-10-1. (Z)
- [SDR EISA95037](https://openairdocs.org/sdr/EISA95037.md): Floor Beam · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Floor Beam
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1110, WL 208.1. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z)
- [SDR EISA95036](https://openairdocs.org/sdr/EISA95036.md): Support · cracked · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND A CRACK IN THE FLOOR ANGLE SUPPORT, BS 760.95, WL 208.1, LBL 5. REPAIRED PER SRM 51-40-3, FIGURE 1, SHEET 4. (Z)
- [SDR EISA95035](https://openairdocs.org/sdr/EISA95035.md): Chord · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON CHORD AT BS 1176.9, WL 208.1 LBL 58 INCHES. REPAIRED PER BOEING SB 727-53-0184 AND DRAWING HSE2-53-149. (Z)
- [SDR EISA95034](https://openairdocs.org/sdr/EISA95034.md): Angle · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BETWEEN BS 312 AND BS 344, WL 208.1, LBL 62 INCHES. REPAIRED PER SRM 51-40-3. (Z)
- [SDR EISA95033](https://openairdocs.org/sdr/EISA95033.md): Skin · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE SKIN, BS 484 BETWEEN STRINGER 28L AND 28R. REPAIRED PER DRAWING HSE 2-53-153. (Z)
- [SDR EISA95032](https://openairdocs.org/sdr/EISA95032.md): End Fitting · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER END FITTING, STRINGER 28R, BS 1183. REPLACED PER SRM 51-10-1 PAGE 4. (Z)
- [SDR EISA95031](https://openairdocs.org/sdr/EISA95031.md): Intercostal · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL BETWEEN BS 1050 AND 1090, LBL 24 INCHES, WL 20 INCHES. REPLACED PER SRM 51-10-1, PAGE 4. (Z)
- [SDR EISA95030](https://openairdocs.org/sdr/EISA95030.md): Frame · damaged · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Frame
  > DURING A SCHEDULED C-CHECK, FOUND A HOLE IN THE AFT CARGO COMPARTMENT DOOR FRAME, BS 990, STRINGER 24R. REPAIRED PER SRM 51-40-7 FIGURE 3. (Z)
- [SDR EISA95029](https://openairdocs.org/sdr/EISA95029.md): Longeron · cracked · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK, FOUND A CRACK IN LONGERON, BS 970 TO BS 990, STRINGER 29R. REPAIRED PER SRM 53-10-8. (Z)
- [SDR EISA95028](https://openairdocs.org/sdr/EISA95028.md): Channel · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION BULGE FROM BS 990 TO BS 1010, STRINGER 27R. REPAIRED PER SRM 51-10-1. (Z)
- [SDR EISA95027](https://openairdocs.org/sdr/EISA95027.md): Stringer · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AT BS 950D TO 950E. REPAIRED PER BOEING FAX, C00 SJO-95-0037RR. (Z)
- [SDR EISA95026](https://openairdocs.org/sdr/EISA95026.md): Longeron · bent · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT LONGERONS BENT BETWEEN BS 950F TO BS 970, STRINGER 29L TO 30. REPAIRED PER SRM 53-10-5 FIGURE 6, PAGE 17 (Z)
- [SDR EISA95025](https://openairdocs.org/sdr/EISA95025.md): Angle · cracked · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT RIB REINFORCEMENT SECTION CRACKED BETWEEN BS 950 F TO 970, STRINGER 30. REPAIRED PER SRM 51-10-1, PARAGRAPH AA, PAGE 4. (Z)
- [SDR EISA95024](https://openairdocs.org/sdr/EISA95024.md): Angles · dented · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLES DENTED FROM BS 560 TO 580, STRINGER 29L TO 29R. REPAIRED PER SRM 51-40-1, FIGURE 1. (Z)
- [SDR EISA95023](https://openairdocs.org/sdr/EISA95023.md): Angle · cracked · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK, FOUND FLOOR SUPPORT ANGLE CRACKED, BS 410 WL 166.1, RBL 38 INCHES. REPAIRED PER SRM 51-40-4. (Z)
- [SDR EISA95022](https://openairdocs.org/sdr/EISA95022.md): Skin · damaged · Mar 6, 1995 · N367PA · Boeing 727221 · Cargo/Baggage Doors
  > DURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT DOOR FRAME AND SKIN DAMAGED, LOWER AFT CORNER. REPAIRED PER SRM 52-00-3 FIGURE 1. (Z)
- [SDR EISA95021](https://openairdocs.org/sdr/EISA95021.md): Beltframe · corroded · Mar 6, 1995 · N367PA · Boeing 727221 · Fuselage Main, Frame
  > DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE FRAME, BS 344 AT STRINGER 23R. REPAIRED PER SRM 53-10-4, FIGURE 1. (Z)

Next page: https://openairdocs.org/deregistered/N367PA-2006-03-27/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 = 'N367PA' AND deregistration_id = 'N367PA-2006-03-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N367PA-2006-03-27/reports

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