# Service difficulty reports: N605AL, cancelled May 1, 2014

A list on [N605AL, cancelled May 1, 2014](https://openairdocs.org/deregistered/N605AL-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 11 · 522 reports

- [SDR IXXA110060O](https://openairdocs.org/sdr/IXXA110060O.md): Engine · slow · Sep 11, 2011 · N605AL · Doug DC873F · Engine (Turbine/Turboprop)
  > REJECTED TAKEOFF DUE TO ASSYMETRICAL THRUST ON TAKEOFF ROLL. THE NR 4 ENGINE SLOW TO ACCELERATE, DID NOT REACH MAX POWER. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PREFORMED ACCELERATION CHECK, OPS CHECKED GOOD IAW ERH 72.01.1. PREFORMED REJE
- [SDR IXXA110049O](https://openairdocs.org/sdr/IXXA110049O.md): Damper · defective · Jun 27, 2011 · N605AL · Doug DC873F · Elevator Control System
  > DURING CLIMB OUT, THE CREW NOTICED AT 250 KNOTS A PULSING IN BOTH CONTROL COLUMNS. THE PULSE INCREASED THROUGH ANY PITCH CHANGE WHETHER USING THE AUTOPILOT OR MANUALLY FLYING THE ACFT (MORE NOTICEABLE PULSE). THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDEN
- [SDR IXXA110043O](https://openairdocs.org/sdr/IXXA110043O.md): Lock Sensor · defective · May 30, 2011 · N605AL · Doug DC873F · Engine Thrust Reverser
  > AFTER TAKEOFF, NR 2 THRUST REVERSER LIGHT WAS BLINKING. THE CREW ACTUATED THE EMERGENCY STOW PUMP BUT NO HELP. THEY RETURNED TO DEPARTURE AND UPON LANDING THE LIGHT WENT OUT. MX TROUBLESHOT THE THRUST REVERSER SYS AND FOUND RT UPPER AND LOWER THRUST REVERSE
- [SDR IXXA110020O](https://openairdocs.org/sdr/IXXA110020O.md): Proximity Switch · defective · Feb 11, 2011 · N605AL · Doug DC873F · Landing Gear Position and Warning
  > AFTER TAKEOFF, WHEN MLG RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED MLG AND LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MLG PROXIMITY SWITCH. OPERATIONAL CHECK GOOD IAW MM 32-60-0. AI
- [SDR IXXA110018O](https://openairdocs.org/sdr/IXXA110018O.md): Target · loose · Feb 9, 2011 · N605AL · Doug DC873F · Landing Gear Position and Warning
  > DURING CLIMBOUT, AFTER GEARS WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEARS, DOOR NOT LATCH LIGHT STILL REMAINED ON, AFTER ACCOMPLISHING UPLATCH CHECK LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH LT A
- [SDR IXXA110012O](https://openairdocs.org/sdr/IXXA110012O.md): Switch · contaminated · Feb 3, 2011 · N605AL · Doug DC873F · Landing Gear Position and Warning
  > AFTER TAKEOFF, WHEN GEAR WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEAR THE DOOR NOT LATCH LIGHT STILL REMAINED ON THE ALT GEAR DOOR LIGHT REMAINED OUT. ON DECENT THE LT ALT GEAR DOOR LIGHT MOMENTARILY FLASHED ON THEN OFF. THEY
- [SDR IXXA100057S](https://openairdocs.org/sdr/IXXA100057S.md): Skin · punctured · Dec 7, 2010 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > PUNCTURE IN LT FWD SIDE OF FUSELAGE AFT AND ABOVE OF LT ACM HEAT EXCHANGE LOUVER DOORS. REPAIRED IAW 53-10653-1. ACFT RETURNED TO SERVICE.
- [SDR IXXA100045O](https://openairdocs.org/sdr/IXXA100045O.md): Transceiver · defective · Sep 15, 2010 · N605AL · Doug DC873F · Ground Proximity System
  > AFTER TAKEOFF, "TOO LOW" AUDIBLE WARNING WENT OFF WITH BOTH RADIO ALTIMETER FLAGS IN VIEW AND GPWS LIGHT ON. DUE TO FUEL AND RVSM ISSUES THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED RADIO ALTIMETER TRANSCEIVER. OPS CHECK GOOD IAW MM 3
- [SDR IXXA100031O](https://openairdocs.org/sdr/IXXA100031O.md): Connector · dirty · May 4, 2010 · N605AL · Doug DC873F · Pneumatic System Wiring
  > DURING CLIMB OUT NR 4 BLEED AIR SHUTOFF VALVE CLOSED CONFIRMING NO BLEED FROM ENGINE. THE CREW CYCLED SWITCH SEVERAL TIMES AND MOVED THROTTLE WITH NO HELP. ON DESCENT NR 4 BLEED AIR SHUTOFF VALVE OPENED. THEY LANDED AT DEPARTURE WITHOUT FURTHER INCIDENT. MX IN
- [SDR IXXA100020O](https://openairdocs.org/sdr/IXXA100020O.md): Guide · misinstalled · Mar 3, 2010 · N605AL · Doug DC873F · Elevator Control System
  > DURING TAKEOFF THE CREW USED EXCESSIVE DOWNWARD FORCE ON ELEVATOR. THEY REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED ELEVATORS AND FOUND CABLE GUIDE UNDER F/O`S FLOOR (FWD) NOT PROPERLY INSTALLED, BOLT ON CABLE SECTOR DRIVE RU
- [SDR IXXA090056O](https://openairdocs.org/sdr/IXXA090056O.md): Steering Sys · lack of lube · Oct 7, 2009 · N605AL · Doug DC873F · Landing Gear Steering System
  > DURING TAKEOFF FROM KLRD THE NOSE WHEEL CONTROL DID NOT RESPOND TO CONTROL WHEEL OR RUDDER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MAINTENANCE LUBRICATED NOSE GEAR SREERING SYSTEM. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENA
- [SDR IXXA090033O](https://openairdocs.org/sdr/IXXA090033O.md): Seal · leaking · Jun 18, 2009 · N605AL · Doug DC873F · Engine Fuel and Control
  > DURING CLIMB-OUT FROM KBFI NUMBER THREE ENGINE FLAMED OUT. THE CREW ACCOMPLISHED QRH CHECKLIST, AND RESTART ATTEMPT, ENGINE WOULD NOT START. THE CREW LANDED IN KPDX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NUMBER THREE ENGINE AND FOUND FUEL LEAK ON F
- [SDR IXXA09SMN066S](https://openairdocs.org/sdr/IXXA09SMN066S.md): Skin · misrepaired · Apr 11, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 220.000-240.000 LONGERON 28-31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED
- [SDR IXXA09SMN065S](https://openairdocs.org/sdr/IXXA09SMN065S.md): Skin · misrepaired · Apr 11, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 480.000 LONGERON 23-24 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AREA, A
- [SDR IXXA09SMN059S](https://openairdocs.org/sdr/IXXA09SMN059S.md): Longeron Splice · cracked · Apr 9, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1770.000 LONGERON 17 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.
- [SDR IXXA09SMN64S](https://openairdocs.org/sdr/IXXA09SMN64S.md): Fitting · cracked · Apr 7, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SEMAN FORM-07
- [SDR IXXA09SMN058S](https://openairdocs.org/sdr/IXXA09SMN058S.md): Fitting · cracked · Apr 7, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BUTTOCKS LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-0
- [SDR IXXA09SMN055S](https://openairdocs.org/sdr/IXXA09SMN055S.md): Fitting · cracked · Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-4, AND DC8 SRM 51-1-8B.
- [SDR IXXA09SMN054S](https://openairdocs.org/sdr/IXXA09SMN054S.md): Fitting · cracked · Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-4, AND SRM 51-1-8B.
- [SDR IXXA09SMN057S](https://openairdocs.org/sdr/IXXA09SMN057S.md): Fitting · cracked · Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 65.000 LONGERON 21 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-07 IPI
- [SDR IXXA09SMN056S](https://openairdocs.org/sdr/IXXA09SMN056S.md): Fitting · cracked · Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 70.000 LONGERON 21 RIGHT- RIGHT BOTTOM LONE 50. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5
- [SDR IXXA09SMN062S](https://openairdocs.org/sdr/IXXA09SMN062S.md): Structure · cracked · Apr 1, 2009 · N605AL · Doug DC873F · Horizontal Stabilizer Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER CAP CRACKED STATION XE 29.812. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FORM-07 IPI NUMBER 2009420.
- [SDR IXXA09SMN53S](https://openairdocs.org/sdr/IXXA09SMN53S.md): Fitting · cracked · Apr 1, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 717.000 LEFT BOTTOM LINE 1. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1.
- [SDR IXXA09SMN052S](https://openairdocs.org/sdr/IXXA09SMN052S.md): Skin · cracked · Apr 1, 2009 · N605AL · Doug DC873F · Rudder, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT RUDDER SKIN CRACKED AT STATION ZR 71.437. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED RUDDER WEIGHT AND BA
- [SDR IXXA09SMN063S](https://openairdocs.org/sdr/IXXA09SMN063S.md): Cargo Track · worn · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK LUGS WORN AT STATION 1670.000-1752.000. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES. FABRICATED TRACK SEGMENT. CLEANED, TREATED, PRIMED AREA AND SEGMENT TRACK AND EXISTING SP
- [SDR IXXA09SMN050S](https://openairdocs.org/sdr/IXXA09SMN050S.md): Longeron · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35 RIGHT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALL
- [SDR IXXA09SMN049S](https://openairdocs.org/sdr/IXXA09SMN049S.md): Longeron · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35LEFT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED
- [SDR IXXA09SMN051S](https://openairdocs.org/sdr/IXXA09SMN051S.md): Longeron · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED AT STATION 1260.000 - 1280.000 LONGERON 36. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT EXTRUSION, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND
- [SDR IXXA09SMN048S](https://openairdocs.org/sdr/IXXA09SMN048S.md): Longeron · corroded · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CORRODED AT STATION 1490.000 - 1500.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON. FABRICATED LONGERON SEGMENT, AND SPLICES. PERFORMED
- [SDR IXXA09SMN047S](https://openairdocs.org/sdr/IXXA09SMN047S.md): Fitting · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT LONGERON BATHTUB FITTING CRACKED AT STATION 902.125 LONGERON 5 LEFT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1
- [SDR IXXA90SMN046S](https://openairdocs.org/sdr/IXXA90SMN046S.md): Fitting · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1230.000 LONGERON 32-33 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, AND SRM 51-3-1.
- [SDR IXXA09SMN045S](https://openairdocs.org/sdr/IXXA09SMN045S.md): Longeron · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 LEFT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW SRM 53-5-3 FIGURE 5 SHEET 1 I
- [SDR IXXA09SMN044S](https://openairdocs.org/sdr/IXXA09SMN044S.md): Longeron · cracked · Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW DC8 SRM 53-5-3 FIGURE 5 SHEE
- [SDR IXXA09SMN042S](https://openairdocs.org/sdr/IXXA09SMN042S.md): Stiffener · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Engine Thrust Reverser
  > DURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 3 ENGINE THRUST REVERSER RIGHT COWLING RAIL FITTING CRACKED AT 6 O'CLOCK POSITION. REMOVED RAIL FITTING FASTENERS. FABRICATED NEW STIFFENER. PROTECTED STIFFENER WITH CHROMIC ANODIZED. INSTALLED NEW FASTENERS,
- [SDR IXXA09SMN041S](https://openairdocs.org/sdr/IXXA09SMN041S.md): Skin · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.000 STRINGER 12. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORR
- [SDR IXXA09SMN061S](https://openairdocs.org/sdr/IXXA09SMN061S.md): Structure · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FO
- [SDR IXXA09SMN060S](https://openairdocs.org/sdr/IXXA09SMN060S.md): Structure · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 LEFT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, REPAIR SPECIFICATION NR 2003-05, AND SMN-FORM-07 IP
- [SDR IXXA09SMN039S](https://openairdocs.org/sdr/IXXA09SMN039S.md): Fitting · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR FITTING CRACKED AT STATION XF 337.000. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, ATI REPAIR S
- [SDR IXXA09SMN043S](https://openairdocs.org/sdr/IXXA09SMN043S.md): Fitting · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER FITTING CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.
- [SDR IXXA09SMN040S](https://openairdocs.org/sdr/IXXA09SMN040S.md): Fitting · cracked · Mar 30, 2009 · N605AL · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR HAS FITTING CRACKED AT STATION XF 411.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1, SRM 51-1-21.
- [SDR IXXA09SMN036S](https://openairdocs.org/sdr/IXXA09SMN036S.md): Skin · cracked · Mar 28, 2009 · N605AL · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN CRACKED AT STATION 104.000 - 122.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW SRM 57-7-1 FIGURE 1 ITEM "D",
- [SDR IXXA09SMN034S](https://openairdocs.org/sdr/IXXA09SMN034S.md): Structure · cracked · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO C
- [SDR IXXA09SMN033S](https://openairdocs.org/sdr/IXXA09SMN033S.md): Structure · cracked · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CR
- [SDR IXXA09SMN038S](https://openairdocs.org/sdr/IXXA09SMN038S.md): Fitting · cracked · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT PASSENGER DOOR FITTING CRACKED AT STATION 1621.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1.
- [SDR IXXA09SMN037S](https://openairdocs.org/sdr/IXXA09SMN037S.md): Fitting · cracked · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 781.500 LONGERON 13 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-1-8B, AND SRM 51-3-1.
- [SDR IXXA09SMN035S](https://openairdocs.org/sdr/IXXA09SMN035S.md): Fitting · cracked · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 11 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-23, SRM 51-1-20D, DC8 SRM 51-1-8B, AND SRM 51-3-
- [SDR IXXA09SMN032S](https://openairdocs.org/sdr/IXXA09SMN032S.md): Skin · corroded · Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR LOWER SKIN CORRODED AT STATION 660.000 LONGERON 31 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED A
- [SDR IXXA09SMN030S](https://openairdocs.org/sdr/IXXA09SMN030S.md): Structure · misrepaired · Mar 26, 2009 · N605AL · Doug DC873F · Cargo/Baggage Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON MAIN CARGO DOOR FORWARD LOWER JAMB CORNER AT STATION 120.000 - 210.000 LONGERON 19-23 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND.
- [SDR IXXA09SMN027S](https://openairdocs.org/sdr/IXXA09SMN027S.md): Skin · misrepaired · Mar 21, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD HAS IMPROPER REPAIR AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNA
- [SDR IXXA080033O](https://openairdocs.org/sdr/IXXA080033O.md): Gyro · failed · Nov 20, 2008 · N605AL · Doug DC873F · Directional Gyro and Indicating System
  > DURING CRUISE FROM KTOL TO KBFI, THE CAPTAINS ADI AND HSI FAILED. THE CREW DIVERTED TO KRFD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FIBER OPTIC VG/DG GYRO. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N605AL-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 = 'N605AL' AND deregistration_id = 'N605AL-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N605AL-2014-05-01/reports

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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.