# Service difficulty reports: N326DL, cancelled Nov 18, 2008

A list on [N326DL, cancelled Nov 18, 2008](https://openairdocs.org/deregistered/N326DL-2008-11-18.md).

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

- [SDR KNN2008F00000](https://openairdocs.org/sdr/KNN2008F00000.md): Bolt · worn · Aug 22, 2008 · N326DL · Boeing 737232 · Elevator Tab Control System
  > IN FLIGHT AGGRESSIVE VIBRATION FELT AT VARIOUS AIRSPEEDS 190 KTS-290 KTS, ALTITUDE STARTING AT 10,300 FT NOT RELENTING UNTIL WELL BELOW 190 KTS. (K)
- [SDR KNNA20080003](https://openairdocs.org/sdr/KNNA20080003.md): Engine · failed · Mar 8, 2008 · N326DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > ACCORDING TO THE PILOT IN COMMAND’S REPORT, THEY HAD TO DEICE THE PLANE BEFORE TAKEOFF. THEN, ON TAKEOFF ROLL, DURING ROTATION, THERE WAS A LOUD BANG AND VIBRATION. THE CAPTAIN’S FIRST THOUGHT WAS THAT A TIRE HAD BLOWN. ONCE AIRBORNE, THE VIBRATION CONTINUE
- [SDR KNNA200700068](https://openairdocs.org/sdr/KNNA200700068.md): Skin · damaged · Dec 10, 2007 · N326DL · Boeing 737232 · Elevator, Plate/Skin
  > WHILE PERFORMING AN A-7 CHECK, A LIGHTNING STRIKE WAS FOUND ON THE LT ELEVATOR AT THE OUTBOARD TRAILING EDGE LOWER SIDE, UNDER I/B STATIC WICK, SPECIAL INSPECTION WAS PERFORMED IAW SKY KING GMM SECTION 4.03 AND AMM 05-51-151-201 WITH NO OTHER DAMAGE NOTED. EL
- [SDR KNNA200700043](https://openairdocs.org/sdr/KNNA200700043.md): Slat Track · jammed · Nov 13, 2007 · N326DL · Boeing 737232 · Leading Edge Devices
  > AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILI
- [SDR KNNA200700061](https://openairdocs.org/sdr/KNNA200700061.md): Slat Track · jammed · Nov 13, 2007 · N326DL · Boeing 737232 · Leading Edge Devices
  > AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILI
- [SDR KNNA200700030](https://openairdocs.org/sdr/KNNA200700030.md): Lever · binding · Apr 28, 2007 · N326DL · Boeing 737232 · Engine Thrust Reverser
  > IN FLIGHT DURING DESCENT INTERMITTENTLY AT FIRST THEN STEADY PROCEDURES WERE FOLLOWED WITH THRUST LEVERS BINDING (RESTRICTED) ENGINE 1 WAS SHUTDOWN IAW CHECK LIST. EMERGENCY DECLARED. THRUST REVERSER WAS TRANSFER TO DMI LOG TROUBLESHOOTING IS IN PROCESS.
- [SDR KNNA200700022](https://openairdocs.org/sdr/KNNA200700022.md): Floorbeam · corroded · Mar 14, 2007 · N326DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOOR PANEL ATTACH POINT STA 344, LBL 12 IS CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF STA 344, LBL 12 FLOOR PANEL ATTACH POINT. REMOVED AND REPLACED FLOORBEAM SRM 53-10-9 FIG 6.
- [SDR KNNA200700026](https://openairdocs.org/sdr/KNNA200700026.md): Frame · damaged · Mar 11, 2007 · N326DL · Boeing 737232 · Fuselage Main, Frame
  > AFT CARGO PIT, INTERIOR BILGE B-STA 867 BETWEEN STR 27 R AND STR 28 L FRAME BOTTOM SIDE, CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 867 BETWEEN STR 27R-27L BOEING SRM 53-10-4 FIGURE 7.
- [SDR KNNA200700025](https://openairdocs.org/sdr/KNNA200700025.md): Skin · corroded · Mar 11, 2007 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > AFT CARGO PIT INTERIOR BILGE, BS 927 BETWEEN STR-27L STR AND 27R, FRAME BOTTOM SIDE CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 927 BETWEEN STR 27L AND STR 28 R BOEING SRM 53-10-4 FIGURE 7.
- [SDR KNNA200700024](https://openairdocs.org/sdr/KNNA200700024.md): Skin · corroded · Mar 9, 2007 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CORRODED SKIN AT BS 500A+ 10' BETWEEN STR 27L/28L. PROVIDE INSTRUCTION ON REPAIR OF CORRODED EXTERIOR SKIN STA 500A + 10' STR 27L/28L.
- [SDR KNNA200700021](https://openairdocs.org/sdr/KNNA200700021.md): Floorbeam · cracked · Mar 9, 2007 · N326DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM CRACKED AT BS 460, RBBL 14.5 FWD CARGO COMPARTMENT. PROVIDE INSTRUCTIONS ON REPAIR OF CARGO FLOORBEAM BS 460 RBL 14.5. REMOVED AND REPLACED CARGO DOOR FLOORBEAM SRM 53-10-5 FIGURE 11.
- [SDR KNNA200700020](https://openairdocs.org/sdr/KNNA200700020.md): Skin · damaged · Mar 4, 2007 · N326DL · Boeing 737232 · Passenger/Crew Doors
  > MAIN ENTRY DOOR L-2 EXTERIOR SURFACE, UPPER AFT CORNER, SKIN BEND. PROVIDE INSTRUCTIONS ON REPAIR OF DOOR SKIN. CUT OUT BEND CORNER AND REPAIR PER SRM 52-00-3 FIGURE 5.
- [SDR KNNA200700023](https://openairdocs.org/sdr/KNNA200700023.md): Skin · corroded · Mar 1, 2007 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE, EXTERNAL SURFACE LOWER LOBE, B-STA 968, STR 27 L CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF FUSELAGE EXTERNAL SURFACE LOWER LOBE BS 968 STR 27 L. BOEING SRM 53-10-3 FIGURE 1 AND 53-30-3 FIGURE 48.
- [SDR DL73S060329](https://openairdocs.org/sdr/DL73S060329.md): Skin · cracked · Dec 20, 2005 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT THE AFT ENTRY DOOR UPPER HINGE CUTOUT HAS A.7500 IN. CRACK AT THE UPPER CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.
- [SDR DL73S050728](https://openairdocs.org/sdr/DL73S050728.md): Skin · deformed · Nov 18, 2005 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH AN OIL CAN CONDITION FROM BS 747-767 BELOW S-18R. INSTALLED DOUBLER PER ER/A 451596-14AD. REF AD 2005-13-30 & 2004-18-06.
- [SDR DL73S050718](https://openairdocs.org/sdr/DL73S050718.md): Skin · cracked · Nov 16, 2005 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND CRACKED AT BS 932, S-21R, CRACK IS 3 INCHES LONG. DOUBLER INSTALLED, REF AD 2004-18-06 & 2005-13-30.
- [SDR DL73S050712](https://openairdocs.org/sdr/DL73S050712.md): Floorbeam · cracked · Nov 14, 2005 · N326DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE OVERWING FLOORBEAM AT LBL 24.8 WAS FOUND CRACKED. INSPECTED PER ER/A 451613-14AD. REF AD 2001-17-18, SI 03-056673-12AD, ER/A 369397-14.
- [SDR DL73S050711](https://openairdocs.org/sdr/DL73S050711.md): Floorbeam · cracked · Nov 14, 2005 · N326DL · Boeing 737232 · Wing, Rib/Bulkhead
  > CRACKS WERE FOUND IN THE OVERWING FLOORBEAMS AT RBL 24.8. INSTALLED REPAIR DOUBLERS AND CHANNEL PER ER/A 451614-14AD. REF AD 2001-17-18, AD 93-17-08, AD 90-06-02, SI 03-056673-12AD.
- [SDR DL73S050710](https://openairdocs.org/sdr/DL73S050710.md): Skin · cracked · Nov 14, 2005 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 540 AND JUST BELOW LAP SPLICE AT S-14L. INSTALLED DOUBLER PER ER/A 451595-14AD AND SRM 53-30-3. REF AD 2004-18-06.
- [SDR DL73S041055](https://openairdocs.org/sdr/DL73S041055.md): Skin · cracked · Nov 20, 2004 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A 1.5 INCH CRACK WAS FOUND IN THE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18L AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 095229-14AD.
- [SDR DL73S040902](https://openairdocs.org/sdr/DL73S040902.md): Shutoff Valve · malfunctioned · Sep 19, 2004 · N326DL · Boeing 737232 · Fuel Selector/Shut-Off Valve
  > AFTER PUSHBACK ENGINE START, NR 2 ENGINE HAD A FLAME OUT OCCUR. DISCOVERED THAT THE NR 2 ENGINE FUEL SHUTOFF VALVE WAS AT FAULT. PART REPLACED BY TPA MTC AND ENGINE RUN NORMAL.
- [SDR DL73S031131](https://openairdocs.org/sdr/DL73S031131.md): Attach Fitting · corroded · Dec 24, 2003 · N326DL · Boeing 737232 · Horizontal Stabilizer Structure
  > CORROSION WAS NOTED DURING INSPECTION OF THE HORIZ STAB ATTACH LUGS PER 03-069697-03 AND 03-053025-03AD. THE RIGHT SIDE OUTBOARD HORIZ STAB REAR SPAR UPPER ATTACH LUG WAS BEYOND PUBLISHED ALLOWABLE LIMITS. CORROSION WAS REMOVED AND LUG REWORKED PER ERA 38598
- [SDR DL73S031129](https://openairdocs.org/sdr/DL73S031129.md): Skin · damaged · Dec 23, 2003 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > DAMAGED FASTENER HOLES WERE REPORTED DURING PERMANENT REPAIR ACCOMPLISHMENT TO THE R2 DOOR UPPER HINGE CUTOUT. AREA WAS REWORKED/REPAIRED PER ERA 360517-14, REV A.
- [SDR DL73S031128](https://openairdocs.org/sdr/DL73S031128.md): Skin · dented · Dec 23, 2003 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ABOVE S19L NEAR THE LWR AFT CORNER OF THE DOOR LOCATED NEAR BS 985. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385887-14.
- [SDR DL73S031127](https://openairdocs.org/sdr/DL73S031127.md): Frame · dented · Dec 23, 2003 · N326DL · Boeing 737232 · Fuselage Main, Frame
  > A DENT WAS FOUND IN THE INNER CHORD OF THE BS 767 FRAME JUST ABOVE S24L. DENT WAS REMOVED AND REPAIRED PER ERA 385960-14.
- [SDR DL73S031126](https://openairdocs.org/sdr/DL73S031126.md): Clevis · corroded · Dec 23, 2003 · N326DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CORROSION DAMAGE FOUND WHICH EXCEEDED LIMITS COVERED IN 03-085220-03. CORROSION WAS FOUND IN THE NR 6 AND NR 12 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND REWORKED PER ERA 386007-14.
- [SDR DL73S031123](https://openairdocs.org/sdr/DL73S031123.md): Skin · cracked · Dec 22, 2003 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK DAMAGE WAS NOTED ON THE KEEL BEAM LOWER SKIN PANEL. SKIN PANEL WAS REPLACED PER ERA 385927-14.
- [SDR DL73S031099](https://openairdocs.org/sdr/DL73S031099.md): Skin · corroded · Dec 16, 2003 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FWD INBD CORNER OF THE AFT LAV SERVICE DOOR CUTOUT NEAR FS 987 AND STRINGER 27R. THE DAMAGE WAS REMOVED WITH A 4 X 4 INCH CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED
- [SDR DL73S031089](https://openairdocs.org/sdr/DL73S031089.md): Bulkhead · corroded · Dec 15, 2003 · N326DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD AT BS 1016 AND BL 0, BETWEEN S26L AND 26R. CORROSION WAS REMOVED THEN REPAIRED PER ERA 385921-14AD.
- [SDR DL73S031078](https://openairdocs.org/sdr/DL73S031078.md): Skin · dented · Dec 12, 2003 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > DENTS WERE NOTED IN THE SKIN PANEL AT APPROXIMATELY BS 380 AND BETWEEN S15L AND S18L. DENTS WERE CUTOUT AND REPAIRED PER ERA 385947-14.
- [SDR DL73K010217](https://openairdocs.org/sdr/DL73K010217.md): Skin · cracked · Feb 6, 2001 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE SKIN AND UNDERLYING BEARSTRAP OF THE L2 DOOR CUTOUT WERE FOUND CRACK AT THE LOWER HINGE CUTOUT. CRACK REMOVAL RESULTED IN A 2 INCH X 2 INCH CUTOUT IN SKIN AND BONDED DOUBLER AND A.5 INCH CUTOUT IN THE BEARSTRAP. THE DAMAGE WAS REPAIRED WITH THREE EXTER
- [SDR DL73K010216](https://openairdocs.org/sdr/DL73K010216.md): Skin · cracked · Feb 6, 2001 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A 3 INCH LONG CRACK WAS FOUND IN THE SKIN JUST BELOW STRINGER 18R AT FS 749. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1 AND ER/A 379971-14, REV A.
- [SDR DL73K010200](https://openairdocs.org/sdr/DL73K010200.md): Skin · cracked · Feb 5, 2001 · N326DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FOUND ON T1 LETTER CK, COCKPIT WINDOW POST IS CRACKED AT THE UPPER OUTBD CORNER OF THE CAPTS WINDSHIELD. REPAIRED PER SRM 53-30-3.
- [SDR DL73K002013](https://openairdocs.org/sdr/DL73K002013.md): Engine · inoperative · Oct 13, 2000 · N326DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > OIL FILTER BYPASS LIGHT ON AFTER TAKEOFF. NR 1 ENG SHUT DOWN. RETURNED TO MCI. OIL PRESSURE WAS NORMAL WHILE ENGINE RUNNING. ENGINE WINDMILLED ABOUT 30 MIN. METAL FOUND IN MAIN FILTER AND GEARBOX CHIP DETECTOR. REPLACED NR 1 ENGINE PER CARD DECK 3T213.
- [SDR DL73K001848](https://openairdocs.org/sdr/DL73K001848.md): Window · shorted · Sep 23, 2000 · N326DL · Boeing 737232 · Flight Compartment Windows
  > AIRTURN BACK DUE TO UNIDENTIFIED ODOR IN COCKPIT. FOUND TERMINAL AND WIRE ON R2 SLIDING WINDOW OVERHEATED. REPLACED TERMINALS, WINDOW AND CONTROLLER. LEAKS CHECK AND OPERATIONAL CHECK GOOD. NO ODOR PRESENT.
- [SDR DL73K001847](https://openairdocs.org/sdr/DL73K001847.md): Valve · stuck · Sep 22, 2000 · N326DL · Boeing 737232 · Cabin Pressure Control System
  > ACRID ODOR IN COCKPIT DURING DESCENT, COULD NOT IDENTIFY SOURCE BUT VERIFIED BY ALL CREW MEMBERS DID NOT AFFECT CABIN AIR. ON GROUND AT GATE F/A REPORTS ODOR IN AFT GALLEY. FOUND 35 DEGREE VALVE ON LT PACK STICKING OPEN. REMOVED AND REPLACED 35 DEGREE VALV
- [SDR DL73K001489](https://openairdocs.org/sdr/DL73K001489.md): Light · damaged · Aug 6, 2000 · N326DL · Boeing 737232 · Emergency Lighting
  > SEAT 01D EMERGENCY LIGHT RIPPED OFF. REPLACED SAME, OPS NORMAL.
- [SDR DL73K992301](https://openairdocs.org/sdr/DL73K992301.md): Battery · discharged · Oct 19, 1999 · N326DL · Boeing 737232 · Emergency Lighting
  > ON L/O, FOUND AFT SECTION EMERGENCY LIGHTS INOP ROWS 17 TO 20 INCLUDING RT SIDE GALLEY. FOUND BATTERY AT MODULE M9222 INOP. REPLACED BATTERY, EMERGENCY LIGHTS OPN CKS NORMAL.
- [SDR DL73K991176](https://openairdocs.org/sdr/DL73K991176.md): Connector · chafed · May 25, 1999 · N326DL · Boeing 737232 · Overheat Detection
  > DURING CLIMBOUT HAD RAPID FLICKERING OF LT WING BODY OVERHEAT LIGHT. TURNED OFF LEFT BLEED, LIGHT STILL ON. PULLED BACK THROTTLE LIGHT EXTINGUISHED. RETURNED TO GATE. FOUND AND REPAIRED CONN (276) AT APU COMPT BULKHEAD.
- [SDR DL73K980450](https://openairdocs.org/sdr/DL73K980450.md): Intercostal · cracked · Feb 23, 1998 · N326DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION PER SI3-55852-12AD, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT TWO LOCATIONS, AT STG 8A AND 11. REPAIRED PER ERA 331396-14AD.
- [SDR DL73K971714](https://openairdocs.org/sdr/DL73K971714.md): Battery · discharged · Aug 31, 1997 · N326DL · Boeing 737232 · Emergency Lighting
  > ON INSPECTION, FOUND EMERGENCY TRACK LIGHTING INOP SEATS 5 TO 9. REPLACED BATTERY AND RACK ASSY, CKS NORMAL.
- [SDR DL73S961074](https://openairdocs.org/sdr/DL73S961074.md): Oven · failed · May 4, 1996 · N326DL · Boeing 737232 · Buffet/Galleys
  > AIRCRAFT RETURNED WITH LOG BOOK IRREG STRONG ODOR BEHIND PILOT SEATS BETWEEN C/B PANEL. THEN SMOKE FROM FORWARD GALLEY VENT AND OVENS. CORRECTIVE ACTION: FOUND FIRST CLASS OVEN FAN MOTOR BAD. REPLACED OVEN.
- [SDR DL73S960510](https://openairdocs.org/sdr/DL73S960510.md): Blkhd Web · cracked · Mar 3, 1996 · N326DL · Boeing 737232 · Fuselage Main, Bulkhead
  > DURING ACCOMPLISHMENT OF S.I. 3-69482-12, A 1 INCH CRACK WAS FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE LBL 5.7 VERTICAL STIFFENER AT BS 178. THE BULKHEAD WEB WAS ALSO FOUND CRACKED AT SEVERAL LOCATIONS BETWEEN WL 184.5 AND 207 AND LBL 5.7 TO RBL 5.7.
- [SDR DL73S954360](https://openairdocs.org/sdr/DL73S954360.md): Megaphone · failed · Nov 12, 1995 · N326DL · Boeing 737232 · Emergency Equipment
  > ON 7802L, FOUND F/C GALLEY MEGAPHONE WOULD NOT PROJECT VOICE WHEN THE BUTTON ON THE HANDLE WAS PUSHED. TRIED CHANGING THE BATTERIES, NO HELP. REPLACED MEGAPHONE.
- [SDR DL73S953678](https://openairdocs.org/sdr/DL73S953678.md): Actuator · cracked · Sep 6, 1995 · N326DL · Boeing 737232 · Drag Control Actuator
  > DURING APPROACH, LOST A-SYSTEM HYDRAULIC QTY AND PRESS. FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR, AS PRECAUTION REPLACED PUMP AND FILTER AND OPERATION NORMAL.
- [SDR DL73S952588](https://openairdocs.org/sdr/DL73S952588.md): Floorbeam · cracked · Jun 1, 1995 · N326DL · Boeing 737232 · Fuselage Main, Floor Beam
  > DURING LAY OVER, INSPECTION FOUND THE FLOORBEAM AT BL 0.07 OF THE WING CENTER SECTION CRACKED AT STA 661. IN ACCORDANCE WITH BAC S/B 737-57-1210, THE CRACKS ARE TYPICAL AND WILL BE REPAIRED BY THE S/B 737-57-1210.

## 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 = 'N326DL' AND deregistration_id = 'N326DL-2008-11-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N326DL-2008-11-18/reports

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