# Service difficulty reports: N305DL, cancelled Jul 7, 2008

A list on [N305DL, cancelled Jul 7, 2008](https://openairdocs.org/deregistered/N305DL-2008-07-07.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 · 58 reports

- [SDR DL73S060620](https://openairdocs.org/sdr/DL73S060620.md): Connector · unsecure · Aug 3, 2006 · N305DL · Boeing 737232 · Light System Wiring
  > LEFT OVERWING EMERGENCY EXIT LIGHT INOP. RESECURED CONNECTOR ON LIGHT ASSY/ OPS NORMAL.
- [SDR DL73S060468](https://openairdocs.org/sdr/DL73S060468.md): Skin · cracked · May 30, 2006 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN HAS A 0.5 INCH CRACK AT THE LOWER HINGE CUTOUT FOR THE R1 DOOR. THE DAMAGED SKIN WAS CUTOUT AND A REPAIR DOUBLER WAS INSTALLED. ALSO MODIFIED PER S/B 737-53-1074.
- [SDR DL73S060195](https://openairdocs.org/sdr/DL73S060195.md): Skin · cracked · Mar 16, 2006 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK FOUND IN FASTENER HOLE AT FUSELAGE STATION 393 AND STRINGER 4R. DAMAGED SKIN WAS TRIMMED OUT AND REPAIR DOUBLER AND TRIPLER INSTALLED.
- [SDR DL73S060197](https://openairdocs.org/sdr/DL73S060197.md): Skin · cracked · Mar 16, 2006 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT CHEM MILL LINE STATION STATION 790 AND STRINGER 17L. REPAIR DOUBLER INSTALLED AND SURROUNDING AREA INSPECTED.
- [SDR DL73S060196](https://openairdocs.org/sdr/DL73S060196.md): Skin · cracked · Mar 16, 2006 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK FOUND IN FUSELAGE SKIN AT STATION 409 AND STR 4R. CRACK TRIMMED OUT AND REPAIR DOUBLER AND TRIPLER INSTALLED.
- [SDR DL73S060220](https://openairdocs.org/sdr/DL73S060220.md): Skin · cracked · Mar 14, 2006 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACK INDICATION IN FUSELAGE SKIN AT STA 481, S-4R LAP JOINT. INSPECTION CONFIRMED THAT NO CRACK EXISTS. NO REPAIR INSTALLED.
- [SDR DL73S050589](https://openairdocs.org/sdr/DL73S050589.md): Line · leaking · Oct 3, 2005 · N305DL · Boeing 737232 · Hydraulic System, Main
  > LOSS OF A SYSTEM HYD, ALT GEAR EXTENSION. REPLACED LEAKING PRESSURE LINE IN RIGHT PYLON.
- [SDR DL73S050111](https://openairdocs.org/sdr/DL73S050111.md): Skin · cracked · Feb 13, 2005 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 764 RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 19L. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUT OUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER
- [SDR DL73S050109](https://openairdocs.org/sdr/DL73S050109.md): Skin · cracked · Feb 13, 2005 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 18R RUNNING ALONG THE MILL LINE OF THE BONDED INTERNAL DOUBLER. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT TO THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR D
- [SDR DL73S040495](https://openairdocs.org/sdr/DL73S040495.md): Skin · cracked · Jun 1, 2004 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > APPROX 3 INCH LONGITUDINAL CRACK IN FUSELAGE SKIN STA 944 ABOVE STR 24R. REPAIRED PER SRM.
- [SDR DL73S040466](https://openairdocs.org/sdr/DL73S040466.md): Roller · out of position · May 25, 2004 · N305DL · Boeing 737232 · Trailing Edge Flaps
  > DURING ROTATION A STRONG RT WING UP FORCE WAS ENCOUNTERED AS THE AIRCRAFT BECAME AIRBORNE. SUBSTANTIAL RT AILERON WAS NECESSARY TO KEEPS WINGS LEVEL. FOUND LT OB FLAP IB TRACK WITH BELLCRANK ROLLER OUT OF CAMTRACK. REPLACED BELLCRANK.
- [SDR DL73S040430](https://openairdocs.org/sdr/DL73S040430.md): Skin · delaminated · May 12, 2004 · N305DL · Boeing 737232 · Trailing Edge Flaps
  > NR 2 AFT FLAP AFT SKIN SEPARATED/DELAMINATED AT IB END. REPAIRED IAW SRM 51-40-20 FIG 10.
- [SDR DL73S040418](https://openairdocs.org/sdr/DL73S040418.md): Skin · delaminated · May 10, 2004 · N305DL · Boeing 737232 · Elevator, Plate/Skin
  > WHILE WORKING N/R 13 FOUND LT ELEVATOR UPPER SURFACE DELAMINATED UNDER CONDUCTIVE FRAME REPAIRED PER SRM 55-20-03 FIG 1 TABLE 1.
- [SDR DL73S040426](https://openairdocs.org/sdr/DL73S040426.md): Skin · cracked · Apr 28, 2004 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > 3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER, FASTENER REPAIR PER SRM 53-30-3 FIG 6
- [SDR DL73S040395](https://openairdocs.org/sdr/DL73S040395.md): Skin · cracked · Apr 26, 2004 · N305DL · Boeing 737232 · Spoilers
  > DENT & CRACK ON LWR SIDE OF I/B GROUND SPOILER 1.5 INCH FWD OF T/E AFT OF INBOARD ACTUATOR.
- [SDR DL73S040105](https://openairdocs.org/sdr/DL73S040105.md): Skin · cracked · Jan 27, 2004 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 2.75 INCH CRACK RUNNING ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 19L BETWEEN FS 776 & 787. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC S/B 737-53-106
- [SDR DL73S030864](https://openairdocs.org/sdr/DL73S030864.md): Gasper Fan · failed · Sep 22, 2003 · N305DL · Boeing 737232 · Air Distribution Fan
  > ON CLIMBOUT FLIGHT ATTENDANTS REPORTED SMOKE ODOR IN CABIN, STRONGER IN AFT PART OF CABIN, NO SMOKE VISIBLE. GASPER FAN WAS TURNED OFF AND ODOR DISSIPATED. FOUND GASPER FAN AT FAULT. REPLACED SAME.
- [SDR DL73S030861](https://openairdocs.org/sdr/DL73S030861.md): Bear Strap · cracked · Sep 20, 2003 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING. THE UNDERLYING BEAR STRAP WAS UNCRACKED. THE CRACK WAS REMOVED WITH A 1.7 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER AND REPAIRED WITH AN E
- [SDR DL73S030476](https://openairdocs.org/sdr/DL73S030476.md): Bulkhead · cracked · May 19, 2003 · N305DL · Boeing 737232 · Fuselage Main, Bulkhead
  > WHILE ACCOMPLISHING INSPECTIONS OF THE AFT PRESSURE BULKHEAD IAW AD 99-08-23, 2 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN THE BULKHEAD AT THE ATTACH AREA. THE CRACKED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLER IAW SRM AND ER/A 38508
- [SDR DL73S030191](https://openairdocs.org/sdr/DL73S030191.md): Support Fitting · damaged · Feb 24, 2003 · N305DL · Boeing 737232 · Engine Mount Section
  > FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH O/S MOUNT HOLES. REPAIR PER ER/A 422119-14AD.
- [SDR DL73S030070](https://openairdocs.org/sdr/DL73S030070.md): Door Frame · cracked · Jan 15, 2003 · N305DL · Boeing 737232 · Cargo/Baggage Doors
  > DOOR / C-2 CARGO DOOR / FWD FRAME / LAP SPLICE: CRACK REPAIR THE C-2 CARGO DOOR WAS FOUND WITH A 1" CRACK IN THE UPPER AND LOWER FRAME WEB AT THE LAP JOINT FOR THE TWO FRAMES. THE CRACK WAS STOP D
- [SDR DL73K021467](https://openairdocs.org/sdr/DL73K021467.md): Smoke · detected · Dec 24, 2002 · N305DL · Boeing 737232 · Air Distribution System
  > SMOKE/ODOR OF UNKNOWN ORIGIN MID TO FWD CABIN TO COCKPIT, SIMILAR TO FIRECRACKER FUSE. AFTER DEPLANING, COULD NOT LOCATE A SOURCE FOR THE ODOR OR SMOKE, SUSPECT A PIECE OF GROUND EQUIPMENT WAS THE SOURCE. A/C OK FOR SVC.
- [SDR DL73K021384](https://openairdocs.org/sdr/DL73K021384.md): Tire · flat · Nov 27, 2002 · N305DL · Boeing 737232 · Tire
  > IR/ UPON EXTENSION OF GEAR AND 3 GREEN INDICATIONS. SEVERAL SECONDS LATER HEARD A THUMP NOISE. INSPECTED GEAR THROUGH NOSE GEAR PORT AND CONFIRMED GEAR DOWN. EMERGENCY DECLARED MCO. FOUND LEFT NOSE TIRE FLAT. REPLACED BOTH NOSE WHEEL ASSYS PER MM.
- [SDR DL73K021062](https://openairdocs.org/sdr/DL73K021062.md): Skin · cracked · Sep 8, 2002 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT FS 525 AND STRINGER 16R WAS FOUND TO BE CRACKED ALONG THE UPPER CHEM-MIL EDGE OF THE INTERNAL BONDED DOUBLER. THE CRACK FOUND WAS APPROXIMATELY 3 INCHES IN LENGTH. THE CRACK WAS NOT FOUND BY DOING INSPECTIONS PER BOEING SB 737-53A1210.
- [SDR DL73K020569](https://openairdocs.org/sdr/DL73K020569.md): Battery · discharged · May 19, 2002 · N305DL · Boeing 737232 · Emergency Lighting
  > RT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY, OPS NORMAL.
- [SDR DL73K020326](https://openairdocs.org/sdr/DL73K020326.md): Engine · failed · Mar 18, 2002 · N305DL · Boeing 737232 · Turbine Section
  > PASSING THROUGH 10,000 FT ON DEPARTURE, HAD LOUD BANG FROM NR 1 ENGINE. ENGINE RPM DECREASED RAPIDLY AND TEMPERATURE WENT TO MAX INDICATED ON GAUGE. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. REPLACED NR 1 ENGINE.
- [SDR DL73K020099](https://openairdocs.org/sdr/DL73K020099.md): Light · inoperative · Jan 26, 2002 · N305DL · Boeing 737232 · Emergency Lighting
  > OVERHEAD EMERGENCY FLOODLIGHT INOP AT SEAT 04C. RELAMPED.
- [SDR DL73K011806](https://openairdocs.org/sdr/DL73K011806.md): Coffeemaker · malfunctioned · Nov 14, 2001 · N305DL · Boeing 737232 · Buffet/Galleys
  > AFT COFFEEMAKER HAD SMALL AMOUNT OF SMOKE REPORTED BY FLT ATTENDANT. COFFEEMAKER TURNED OFF, SMOKE STOPPED. REQUESTED INSPECTION OF COFFEMAKER. INSPECTED WIRING AT COFFEEMAKERES 1 AND 2, ALL OK. COULD NOT DETERMINE 1 OF 2 INOP. PULLED AND COLLARED 1 AND
- [SDR DL73K002320](https://openairdocs.org/sdr/DL73K002320.md): Skin · cracked · Nov 28, 2000 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / AFT ENTRY DOOR OPENING / LWR HINGE CUTOUT:CRACK REPAIR THE LOWER HINGE CUTOUT OF THE AFT ENTRY DOOR OPENING SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER.
- [SDR DL73K001970](https://openairdocs.org/sdr/DL73K001970.md): Unknown · odor · Oct 10, 2000 · N305DL · Boeing 737232 · Air Distribution System
  > PILOTS DETECTED A MELTING PLASTIC SMELL AT CRUISE (FL 330.7M) SMELL WAS INTERMITTENT AND FLT CREW WAS UNABLE TO DETERMINE THE SOURCE. EXECUTED PRECAUTIONARY, DIVERT TO ATL. FUMES/SMELL DID NOT REOCCUR AFTER INITIAL DESCENT INTO ATL. INSP PACK INLETS, INSP B
- [SDR DL73K001288](https://openairdocs.org/sdr/DL73K001288.md): Skin · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED JUST ABOVE STR 19R AT FS 767. THE 2.5 INCH CRACK WAS CUTOUT AND A REPAIR WAS INSTALLED PER B737-200 SRM 53-30-3, FIGURE 6. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K001287](https://openairdocs.org/sdr/DL73K001287.md): Frame · damaged · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Frame
  > THE LOWER STUB FRAME FOR THE FORWARD SIDE OF THE AFT GALLEY DOOR CUTOUT WAS FOUND DAMAGE AND REPLACED ON ERA 334610-14 AT HMV.
- [SDR DL73K001286](https://openairdocs.org/sdr/DL73K001286.md): Skin · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED JUST BELOW STR 18L AT FS 727B. THE 3 INCH CRACK WAS CUTOUT AND AN EXTERNAL REPAIR WAS ACCOMPLISHED PER B737-200 SRM 53-30-3, FIGURE 6. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K001285](https://openairdocs.org/sdr/DL73K001285.md): Stringer · corroded · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > THE LT AFT KEEL CHORD (STR 27L) WAS FOUND CORRODED BETWEEN FS 907 AND FS 927. AS A RESULT STRINGER 27L WAS REMOVED FROM FS 907 TO FS 1016 AND A NEW SECTION SPLICED IN PER ERA 334591-14 AT HMV.
- [SDR DL73K001284](https://openairdocs.org/sdr/DL73K001284.md): Frame · misdrilled · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Frame
  > A DOUBLE DRILLED HOLE WAS FOUND ON THE ORIGINAL INSTALLATION OF THE FS 663 FRAME BETWEEN STRINGERS 9L AND 10L. THE HOLE WAS CLEANED UP AND REPAIRED PER ERA 334565-14 AT HMV.
- [SDR DL73K001282](https://openairdocs.org/sdr/DL73K001282.md): Floorbeam · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE BL.07 FLOORBEAM WAS FOUND CRACKED IN THE WEB BETWEEN FS 700 AND FS 717. ERA 334520-14 REPAIRED THE DAMAGE SIMILIARLY TO S/B 737-57-1210 AT HMV.
- [SDR DL73K001281](https://openairdocs.org/sdr/DL73K001281.md): Floorbeam · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE UPPER CAP AND WEB OF THE LBL 24 FLOOR BEAM WAS FOUND CRACKED BETWEEN STATIONS 670 AND 678. THE UPPER CAP WAS SPLICED AND THE WEB WAS REPAIRED PER ERA 334555-14 AT HMV.
- [SDR DL73K001280](https://openairdocs.org/sdr/DL73K001280.md): Floorbeam · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE FUSELAGE WING CENTER SECTION FLOOR BEAM AT RBL 12 WAS CRACKED IN THE WEB AND UPPER CAP. THE UPPER CAP WAS CUT AND SPLICED TO REMOVE THE DAMAGE AND THE WEB WAS REPAIRED PER ERA 334535-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K001279](https://openairdocs.org/sdr/DL73K001279.md): Attach Fitting · corroded · Jul 7, 2000 · N305DL · Boeing 737232 · Vertical Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE FUSELAGE SIDE OF THE VERTICAL FIN ATTACH LUGS. LUG BORES WERE OVERSIZED THE THE LUG FACES WERE SPOTFACED TO REMOVE THE CORROSION. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334526-14.
- [SDR DL73K001278](https://openairdocs.org/sdr/DL73K001278.md): Attach Fitting · corroded · Jul 7, 2000 · N305DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE LEFT AND RIGHT FORWARD AND AFT CLEVIS LUGS. THE DAMAGE WAS REMOVED BY INCREASING THE DIA OF THE BORES AND SPOTFACING SOME OF THE FACE OF THE NR 3 LUG. THE DAMAGE WAS FOUND AT HMV AND REPAIRED BY ERA 334525-14.
- [SDR DL73K001277](https://openairdocs.org/sdr/DL73K001277.md): Attach Fitting · corroded · Jul 7, 2000 · N305DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE RHS AFT SPAR LUGS OF THE HORIZ STABILIZER. CORROSION WAS REMOVED BY OVERSIZING THE BORES AND SPOTFACING THE FORWARD AND AFT FACES OF THE LUG. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334542-14.
- [SDR DL73K001276](https://openairdocs.org/sdr/DL73K001276.md): Frame · cracked · Jul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE LOWER FASTENER OF THE INBOARD CHORD OF THE FS 616 JUST BELOW THE CABIN FLOOR. THE CRACK IS SIMILIAR TO THAT OF S/B 737-53-1182. ADDITIONALLY, A PILOT HOLE FROM THE FACTORY WAS FOUND AT THE LOWER EDGE OF THE SIXTH FASTENER FROM TH
- [SDR DL73K001232](https://openairdocs.org/sdr/DL73K001232.md): Attach Fitting · corroded · Jun 29, 2000 · N305DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE HORIZONTAL STABILIZER FRONT AND REAR SPAR ATTACH FITTING LUGS. THE LUGS WERE SPOT FACED AND THE BORES OVERSIZED PER ERA 334517-14 AT HMV.
- [SDR DL73K001231](https://openairdocs.org/sdr/DL73K001231.md): Fitting · corroded · Jun 29, 2000 · N305DL · Boeing 737232 · Empennage Flight Control Surfaces, Attach Fittings
  > DURING HMV CORROSION WAS FOUND ON THE AFT FACES OF THE LEFT AND RIGHT VERTICAL STABILIZER PRIMARY REAR SPAR TERMINAL FITTING. THE AREA WAS BLENDED AND TREATED PER ERA 334527-14AT HMV.
- [SDR DL73K000978](https://openairdocs.org/sdr/DL73K000978.md): Transformer · failed · May 14, 2000 · N305DL · Boeing 737232 · Engine Oil Quantity
  > C/B POPPED, CREW REPORTED SMOKE AND BURNING SMELL BEFORE C/B POPPED. FOUND SHORTED TRANSFORMER IN OIL QTY INDICATOR. REPLACED SAME.
- [SDR DL73K000313](https://openairdocs.org/sdr/DL73K000313.md): Skin · cracked · Feb 15, 2000 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR (L2) CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.3 X 2.4 CUTOUT AND REPAIRED WITH 3 EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 24 AND ER/A 369
- [SDR DL73K991770](https://openairdocs.org/sdr/DL73K991770.md): Light · inop · Aug 8, 1999 · N305DL · Boeing 737232 · Emergency Lighting
  > DOOR 1R EMERGENCY LIGHT FLASHES.
- [SDR DL73K982533](https://openairdocs.org/sdr/DL73K982533.md): Skin · cracked · Dec 10, 1998 · N305DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN ASSY AND BEAR STRAP WERE FOUND WITH AN APPROX 1 INCH LONG CRACK AT THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND BEAR STRAP AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS. THE REPAIR WAS
- [SDR DL73K980650](https://openairdocs.org/sdr/DL73K980650.md): Sign · inoperative · Mar 24, 1998 · N305DL · Boeing 737232 · Emergency Lighting
  > 2L EMERGENCY DOOR LIGHT INOP. REPLACED ASSEMBLY.
- [SDR DL73K980385](https://openairdocs.org/sdr/DL73K980385.md): Press Pack · malfunctioned · Feb 14, 1998 · N305DL · Boeing 737232 · Hydraulic System, Main
  > LOST PRESSURE ON BOTH A-SYS HYD PUMPS, HYD QTY NML. MTC HAS FOUND NO FLUID LOSS. MOTORED ENG'S AT GATE HAD PRESSURE. CKD CASE DRAIN AND PRESS FILTERS, NO CONTAMINATION FOUND. REPLACED A-SYS HYD PRESS PACKAGE AND CASE DRAIN FILTERS, RAN BOTH ENG'S AND EXERCI

Next page: https://openairdocs.org/deregistered/N305DL-2008-07-07/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 = 'N305DL' AND deregistration_id = 'N305DL-2008-07-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N305DL-2008-07-07/reports

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