# Service difficulty reports: N604BX, cancelled May 1, 2014

A list on [N604BX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N604BX-2014-05-01.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 3 · 102 reports

- [SDR IXXA20121215035O](https://openairdocs.org/sdr/IXXA20121215035O.md): Warning Light · false activation · Dec 15, 2012 · N604BX · Doug DC873F · Door Warning System
  > DURING TAKEOFF, BELLY DOOR OPEN LIGHT ILUMINATED. TAKEOFF WAS ABORTED. RESET ALL CARGO DOORS IAW MM 52-70-0 ALL WARNING LIGHTS OUT.
- [SDR IXXA20120223004S0](https://openairdocs.org/sdr/IXXA20120223004S0.md): Door · out of rig · Feb 23, 2012 · N604BX · Doug DC873F · Passenger/Crew Doors
  > L1 DOOR OUT OF RIG. R & R L1 DOOR AND ADJUSTED TO OPENING IAW MM 52-11-1, OPS CHECKED GOOD.
- [SDR IXXA110072O](https://openairdocs.org/sdr/IXXA110072O.md): Engine · failed · Oct 27, 2011 · N604BX · Doug DC873F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. FOUND N1 SEIZED. REPLACED NR 2 ENGINE IAW J/C 7004, 7005, 7104, AND 7104. RAN ENGINE IAW ERH 70.01. OPS CHECKED GOOD. REJECTED TAKEO
- [SDR IXXA110046O](https://openairdocs.org/sdr/IXXA110046O.md): Link · failed · Jun 5, 2011 · N604BX · Doug DC873F · Landing Gear Door Retract Section
  > AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RT NOSE GEAR DOOR OPENED, NO FURTHER DEFECTS NOTED. THEY REPLACED RT FWD NOSE GEAR LINK. OPS CHECK GOOD IAW MM 32-22-1. ACFT WAS RE
- [SDR IXXA110040O](https://openairdocs.org/sdr/IXXA110040O.md): Fuel Control · out of adjust · May 12, 2011 · N604BX · Doug DC873F · Fuel Control/Turbine Engines
  > DURING CRUISE, NR 4 ENGINE FLAMEDOUT. THE CREW ATTEMPTED RESTART, ENGINE WOULD NOT START. THEY LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAULT TREE 51, CHANGED NR 4 FUEL FILTER, RAN ENGINE AND FOUND FLIGHT IDLE LOW, ADJUSTED FLIGHT IDLE. OPS CHECK GOO
- [SDR 2010FA0000680](https://openairdocs.org/sdr/2010FA0000680.md): Skin · dented · Jun 1, 2010 · N604BX · Doug DC873F · Trailing Edge Flaps
  > (SPUY) RT OTBD FLAP T/E PANEL UPPER SKIN WITH (02 EA) DENTS AT STA XF 310.000 AND 320.000.
- [SDR 2010FA0000679](https://openairdocs.org/sdr/2010FA0000679.md): Longeron · corroded · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage Main, Longeron/Stringer
  > (SPUY) AFT ACCY COMPT L-34L CORRODED AT STA 1700.000 (CORRECTING SOURCE DOCUMENT: CPCP 5600-0551).
- [SDR 2010FA0000678](https://openairdocs.org/sdr/2010FA0000678.md): Cargo Track · broken · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > (SPUY) MAIN CARGO COMPT - NR 4 SEAT TRACK LUG PLUG BROKEN (STA 140.000- 160.000).
- [SDR 2010FA0000677](https://openairdocs.org/sdr/2010FA0000677.md): Access Door · cracked · Jun 1, 2010 · N604BX · Doug DC873F · Wing, Plate/Skin
  > (SPUY) CTR WING AUX TANK RT SIDE - NR 516 ACCESS DOOR FLANGE WITH (02 EA) CRACKS AROUND STA XCW 23000, S57 AND S58.
- [SDR 2010FA0000676](https://openairdocs.org/sdr/2010FA0000676.md): Cargo Track · corroded · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > (SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK LUGS WORN AND CORRODED (STA 857.000- 880.000).
- [SDR 2010FA0000675](https://openairdocs.org/sdr/2010FA0000675.md): Vane · damaged · Jun 1, 2010 · N604BX · Doug DC873F · Trailing Edge Flaps
  > (SPUY) LT WING - INBD VANE SLOT WITH ELONGATED HOLES AT STA XS 247.000.
- [SDR 2010FA0000674](https://openairdocs.org/sdr/2010FA0000674.md): Skin · corroded · Jun 1, 2010 · N604BX · Doug DC873F · Rudder, Plate/Skin
  > (SPUY) RUDDER LT SIDE PLATING CORRODED AT STA ZR 140.000.
- [SDR 2010FA0000673](https://openairdocs.org/sdr/2010FA0000673.md): Cargo Track · worn · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > (SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK (03 EA) LUGS WORN AT STA 280.000.
- [SDR 2010FA0000672](https://openairdocs.org/sdr/2010FA0000672.md): Skin · dented · Jun 1, 2010 · N604BX · Doug DC873F · Elevator, Plate/Skin
  > (SPUY) LT HORIZ STAB - ELEVATOR UPPER PLATING DENTED 6" AT STA XE 90.000.
- [SDR 2010FA0000671](https://openairdocs.org/sdr/2010FA0000671.md): Access Door · cracked · Jun 1, 2010 · N604BX · Doug DC873F · Wing, Plate/Skin
  > (SPUY) LT WING - NR505F ACCESS DOOR PLATING SURFACE UPPER PART CRACKED 1".
- [SDR 2010FA0000670](https://openairdocs.org/sdr/2010FA0000670.md): Skin · cracked · Jun 1, 2010 · N604BX · Doug DC873F · Landing Gear Doors
  > NLG - LT AFT DOOR EXTERNAL SKIN CRACKED 1" AND WITH INTERIM REPAIR.
- [SDR 2010FA0000669](https://openairdocs.org/sdr/2010FA0000669.md): Fitting · cracked · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage Main, Attach Fittings
  > (SPUY) LT MLG WW, LT 24L, JOINT FITTNG LWR PART CRACKED.5" AT STA 879.000.
- [SDR 2010FA0000668](https://openairdocs.org/sdr/2010FA0000668.md): Fitting · corroded · Jun 1, 2010 · N604BX · Doug DC873F · Fuselage Main, Attach Fittings
  > (SPUY) LT MLG WW - L-24L, JOINT FITTING LWR PART CORRODED AT STA 940.000.
- [SDR IXXA10SMN055S](https://openairdocs.org/sdr/IXXA10SMN055S.md): Longeron · corroded · Apr 21, 2010 · N604BX · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT LONGERON 34 LT CORRODED AT STATION 1700.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON SEGMENT. FABRICATED STRAPS. CLEANED, TREATED, PRIMED AREA, STRAPS, AND NEW EXTRUSION. IN
- [SDR IXXA10SMN057S](https://openairdocs.org/sdr/IXXA10SMN057S.md): Seat Track · corroded · Apr 17, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS WORN AND CORRODED AT STA 857.000 - 880.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALL
- [SDR IXXA10SMN054S](https://openairdocs.org/sdr/IXXA10SMN054S.md): Flange · cracked · Apr 17, 2010 · N604BX · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP FOUND CTR WING AUX TANK RT SIDE NR 516 ACCESS DOOR FLANGE WITH CRACKED AROUND STATION XCW 23000, STRINGER 57 AND STRINGER 58. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING ANGLES AND WEB TO GAIN ACCESS. REMOVED DA
- [SDR IXXA10SMN058S](https://openairdocs.org/sdr/IXXA10SMN058S.md): Seat Track · broken · Apr 16, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 4 SEAT TRACK LUG PLUG BROKEN AT STA 140.000 -160.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SEAT TRACK. REMOVED DAMAGED AREA. FABRICATED NEW SEAT TRACK SEGEMENT, SPLICES. C
- [SDR IXXA10SMN053S](https://openairdocs.org/sdr/IXXA10SMN053S.md): Slot · damaged · Apr 16, 2010 · N604BX · Doug DC873F · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD VANE SLOT WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED VANE SLOT. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY NOTED. FABRIC
- [SDR IXXA10SMN052S](https://openairdocs.org/sdr/IXXA10SMN052S.md): Skin · corroded · Apr 15, 2010 · N604BX · Doug DC873F · Rudder, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND RUDDER LEFT SIDE SKIN CORRODED AT STATION ZR 140.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIME
- [SDR IXXA10SMN056S](https://openairdocs.org/sdr/IXXA10SMN056S.md): Seat Track · worn · Apr 13, 2010 · N604BX · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS ARE WORN AT STA 280.000. REMOVED DAMAGED FASTENERS AS NEEDED TO PERFORM RPAIR. REMOVED DAMAGED AREA. FABRICATED SEAT TRACK, SPLICES, SPLICES. CLEANED, TREATED, PRIMED AREA, AND REP
- [SDR IXXA10SMN051S](https://openairdocs.org/sdr/IXXA10SMN051S.md): Skin · dented · Apr 13, 2010 · N604BX · Doug DC873F · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER SKIN DENTED AT STATION XE 90.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL.
- [SDR IXXA10SMN050S](https://openairdocs.org/sdr/IXXA10SMN050S.md): Doubler · cracked · Apr 13, 2010 · N604BX · Doug DC873F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSP, FOUND LT WING NR 505F ACCESS DOOR MATING SURFACE UPPER PART CRACKED. REMOVED CHANNEL AND FASTENERS. REMOVE DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, INTERNAL REPAIR DOUBLER, AND
- [SDR IXXA10SMN049S](https://openairdocs.org/sdr/IXXA10SMN049S.md): Skin · cracked · Apr 9, 2010 · N604BX · Doug DC873F · Landing Gear Doors
  > DURING ROUTINE C-CHECK INSP, FOUND LT NLG AFT DOOR EXTERNAL SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PART IAW SRM C
- [SDR IXXA10SMN47S](https://openairdocs.org/sdr/IXXA10SMN47S.md): Fitting · corroded · Apr 7, 2010 · N604BX · Doug DC873F · Fuselage, Landing Gear Attach Fittings
  > DURING C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CORRODED AT STA 940.000 LONGERON 24 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS.
- [SDR IXXA10SMN048S](https://openairdocs.org/sdr/IXXA10SMN048S.md): Fitting · cracked · Apr 7, 2010 · N604BX · Doug DC873F · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CRACKED AT STA 879.000 LONGERON 24 LT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER, SHIMS. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING
- [SDR IXXA100022O](https://openairdocs.org/sdr/IXXA100022O.md): Warning Light · illuminated · Mar 12, 2010 · N604BX · Doug DC873F · Landing Gear Position and Warning
  > DURING CRUISE,THE CREW GOT UNSATISFACTORY UPLATCH CHECK, DOOR NOT LATCH LIGHT ILLUMINATED. THEY CYCLED GEAR, THE DOOR NOT LATCH LIGHT ILLUMINATED THEN GOES OUT INTERMITTENTLY DURING FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. THE CREW DEFERRED DOOR LIGHT IAW
- [SDR IXXA100010O](https://openairdocs.org/sdr/IXXA100010O.md): Wire Harness · broken · Jan 27, 2010 · N604BX · Doug DC873F · Fire Protection System Wiring
  > DURING CLIMBOUT, NR 1 ENG SHORT CIRCUIT LIGHT CAME ON. NR ONE ENG FIRE WARNING WOULD NOT TEST. CREW SHUTDOWN NR 1 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT LWR NINTH STAGE BLEED AIR DUCT BROKEN AT ENG CASE FLANGE AND CORE WIRING HARNE
- [SDR IXXA090059O](https://openairdocs.org/sdr/IXXA090059O.md): Oxygen System · low · Oct 20, 2009 · N604BX · Doug DC873F · Crew Oxygen System
  > DURING CLIMB OUT, CREW NOTICED OXYGEN REGULATOR AT JUMP SEAT HAD FLOW LEVER IN EMERGENCY POSITION, OXYGEN SYS DEPLETED DOWN TO 75 PSI. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX SERVICED OXYGEN SYS, OPS CHECK GOOD IAW MM 35-10-0. ACFT WAS RETURNE
- [SDR IXXA090034O](https://openairdocs.org/sdr/IXXA090034O.md): Plug · missing · Jun 21, 2009 · N604BX · Doug DC873F · Turbine Engine Oil System
  > DURING CLIMB-OUT FROM KLAX,THE CREW SHUTDOWN NR 4 ENGINE DUE TO LOST OF OIL QUANTITY. THE CREW LANDED IN KPDX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NUMBER FOUR ENGINE AND FOUND THE STARTER SERVICE PLUG OFF. MAINTENANCE INSTALLED SERVICE PLUG AND
- [SDR IXX2008F00011](https://openairdocs.org/sdr/IXX2008F00011.md): Landing Gear · malfunctioned · Jul 11, 2008 · N604BX · Doug DC873F · Main Landing Gear
  > DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PROCEDURES IN COCKPIT OPERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDING. AC LANDED UNEVE
- [SDR IXX2008F00004](https://openairdocs.org/sdr/IXX2008F00004.md): Strut · contaminated · Jul 11, 2008 · N604BX · Doug DC873F · Nose/Tail Landing Gear Strut/Axle
  > DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PORCEDURE IN COCKPIT OPERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDING. AC LANDED UNEVEN
- [SDR IXXA080021O](https://openairdocs.org/sdr/IXXA080021O.md): Landing Gear · malfunctioned · May 13, 2008 · N604BX · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING TAKEOFF FROM GOOY, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE CREW WAS ABLE TO RETRACT NOSE GEAR WITH HANDLE LATCH FLIGHT RELEASE. WHEN NOSE GEAR RETRACTED THE TAKEOFF WARNING HORN SOUNDED, THE CREW PULLED GROUND SHIFT BREAKERS, WHEN THE LEFT BREAKE
- [SDR IXXA080019O](https://openairdocs.org/sdr/IXXA080019O.md): Landing Gear · malfunctioned · May 7, 2008 · N604BX · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING CLIMB-OUT FROM KTOL LANDING GEAR WOULD NOT RETRACT. THE CREW GOT A INFLIGHT INDICATION OF MECHANICAL AND ELECTRICAL GROUND SHIFT FAILURE. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAISED THE AIRCRAFT OFF THE GROUND AND PERFOR
- [SDR IXXA080018O](https://openairdocs.org/sdr/IXXA080018O.md): Mechanism · out of adjust · May 6, 2008 · N604BX · Doug DC873F · Landing Gear Door Retract Section
  > DURING CLIMB-OUT FROM KTOL, THE CREW WAS UNABLE TO RAISE NOSE LANDING GEAR NORMALLY AFTER TAKEOFF. THE CREW ACCOMPLISHED COM PROCEDURE'S, USING THE HANDLE LATCH FLIGHT RELEASE THE NOSE GEAR CAME UP AND LOCKED. WHEN THE GEAR WAS BEING RAISED THE CREW HEARD A
- [SDR IXXA08SMN069S](https://openairdocs.org/sdr/IXXA08SMN069S.md): Link · cracked · Feb 8, 2008 · N604BX · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMOVED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. GOOD IAW DC8 MA
- [SDR IXXA08SMN068S](https://openairdocs.org/sdr/IXXA08SMN068S.md): Drive Link · bent · Feb 8, 2008 · N604BX · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LINK AT FLAP DRIVE LINK BENT AT STATION 3.000. REMOVED AND REPLACED LEFT WING FLAP DRIVE LINK IAW DC8 MAINTENANCE MANUAL 20-16-0 PAGE 202. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. OPERATIONAL CHECK GOOD
- [SDR IXXA07SMN275S](https://openairdocs.org/sdr/IXXA07SMN275S.md): Skin · misrepaired · Nov 26, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE BELOW AND AFT OF ACM, SPACING TOO LARGE AT STATION FS 8.000 LONGERON-30 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPEC
- [SDR IXXA07SMN274S](https://openairdocs.org/sdr/IXXA07SMN274S.md): Skin · misrepaired · Nov 26, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FORWARD FUSELAGE ACM AFT LOWER CORNER, SPACING TOO LARGE, AT STATION FS 8.000 LONGERON-30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPEC
- [SDR IXXA07SMN276S](https://openairdocs.org/sdr/IXXA07SMN276S.md): Skin · misrepaired · Nov 26, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE FORWARD GALLEY VENT ABOVE R-1 DOOR, RIVET SPACING TOO SMALL AT STATION FS 183.000, LONGERON-10.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED A
- [SDR IXXA070065S](https://openairdocs.org/sdr/IXXA070065S.md): Bulkhead · misrepaired · Nov 26, 2007 · N604BX · Doug DC873F · Fuselage Main, Bulkhead
  > DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FRAME SEGMENT, AND INT
- [SDR IXXA07SMN273S](https://openairdocs.org/sdr/IXXA07SMN273S.md): Bulkhead · misrepaired · Nov 26, 2007 · N604BX · Doug DC873F · Fuselage Main, Bulkhead
  > DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FRAME SEGMENT, AND INTERNAL
- [SDR IXXA07SMN272S](https://openairdocs.org/sdr/IXXA07SMN272S.md): Support · cracked · Nov 16, 2007 · N604BX · Doug DC873F · Wing, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL PART SUPPORT HAS A CRACK AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW SUPPORT I
- [SDR IXXA07SMN271S](https://openairdocs.org/sdr/IXXA07SMN271S.md): Attach Angle · corroded · Nov 16, 2007 · N604BX · Doug DC873F · Empennage Flight Control Surfaces, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED AND
- [SDR IXXA07SMN270S](https://openairdocs.org/sdr/IXXA07SMN270S.md): Skin · misrepaired · Nov 16, 2007 · N604BX · Doug DC873F · Rudder, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 253.000 TO STATION ZR 271.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER, BONDED PA
- [SDR IXXA07SMN269S](https://openairdocs.org/sdr/IXXA07SMN269S.md): Structure · cracked · Nov 16, 2007 · N604BX · Doug DC873F · Wing Main, Frame Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING. NUMBER 4 STUB WING LEADING EDGE LOWER PART DOUBLER HAS A CRACK AT STATION XFS 529.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL, INTERNAL REPAIR DOUBLER.

Next page: https://openairdocs.org/deregistered/N604BX-2014-05-01/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 = 'N604BX' AND deregistration_id = 'N604BX-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N604BX-2014-05-01/reports

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