# Service difficulty reports: N603AL, cancelled Sep 18, 2015

A list on [N603AL, cancelled Sep 18, 2015](https://openairdocs.org/deregistered/N603AL-2015-09-18.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 6 · 295 reports

- [SDR IXXA20120306006S](https://openairdocs.org/sdr/IXXA20120306006S.md): Radome · damaged · Mar 5, 2012 · N603AL · Doug DC873F · Aerodynamic Fairings
  > NOSE RADOME DAMAGED. R & R NOSE RADOME IAW MM 53-50-1.
- [SDR IXXA110004O](https://openairdocs.org/sdr/IXXA110004O.md): Pin · sheared · Jan 18, 2011 · N603AL · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING CLIMB OUT, AFTER GEAR RETRACTION, CREW NOTICED AN UNSAFE GEAR LIGHT INDICATION. ACCOMPLISHED UPLATCH CHECK, AND WHEN CYCLING THE GEARS FELT A VIOLENT SHUDDER AND THE LT MLG DOWN LIGHT ILLUMINATED INTERMITTENTLY. RETURNED TO DEPARTURE AND LANDED WITHO
- [SDR IXXA100060O](https://openairdocs.org/sdr/IXXA100060O.md): Connector · loose · Dec 19, 2010 · N603AL · Doug DC873F · Fire Protection System Wiring
  > DURING CRUISE NR 1 ENGINE FIRE WARNING AND BELL FLICKERED MOMENTARILY AT 410, SAT -50, TAT -21, MANIFOLD PRESSURE 32, MANIFOLD AIR TEP 150. THE CREW TESTED FIRE WARNING AND SHORT CIRCUIT WERE NORMAL CONDITION, REMAINED NORMAL REST OF FLIGHT. THEY LANDED IN KSJ
- [SDR IXXA100058S](https://openairdocs.org/sdr/IXXA100058S.md): Skin · cracked · Dec 15, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING WALK AROUND, FOUND A CRACK ON BELLY CTR LINE LONGERON 36 AT STA 1400. MX REPAIRED IAW SRM 53-2-1 CLASS 3. ACFT WAS RETURNED TO SERVICE.
- [SDR IXXA100038O](https://openairdocs.org/sdr/IXXA100038O.md): Compressor · bird ingestion · Aug 3, 2010 · N603AL · Doug DC873F · Turbine Engine Compressor Section
  > DURING TAKEOFF, CREW EXPERIENCE A COMPRESSOR STALL ON RT SIDE. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS. MX INSPECTED BOTH NR (3) AND NR (4) ENGINE AND FOUND EVIDENCE OF A BIRD STRIKE ON NR (4) ENGINE. THEY PERFORMED BORESCOPE INSP, COMPLIED WITH CFM 56, F
- [SDR IXXA100028O](https://openairdocs.org/sdr/IXXA100028O.md): Pin · broken · Apr 30, 2010 · N603AL · Doug DC873F · Landing Gear Doors
  > DURING CLIMBOUT, ON GEAR RETRACTION, THE CREW HEARD LOUD BANG, BOTH DOORS NOT LATCH LIGHT AND GEAR NOT LATCH LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND RT MLG RETRACT CYL ATTACH PIN BROKE. THEY REPLACED RETR
- [SDR IXXA100027O](https://openairdocs.org/sdr/IXXA100027O.md): Uplock · failed · Apr 6, 2010 · N603AL · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING UPLATCH CHECK, GEAR NOT LATCH LIGHT CAME ON, CREW CYCLED THE GEAR AND GEAR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. MX DEFERRED MAIN UPLATCH SYS, IAW MEL 32-16-01. MX FOUND THE LT AND RT MAIN GEAR ACTUAT
- [SDR IXXA100026O](https://openairdocs.org/sdr/IXXA100026O.md): Switch · defective · Apr 2, 2010 · N603AL · Doug DC873F · Landing Gear Position and Warning
  > DURING UPLATCH CHECK, GEAR NOT LATCH LIGHT CAME ON, THE CREW CYCLED GEARS AND THE GEAR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND NLG UPLATCH OVER CTR MECHANISM BINDING, NOT GOING OVER CTR
- [SDR IXXA100025O](https://openairdocs.org/sdr/IXXA100025O.md): Uplock · malfunctioned · Mar 31, 2010 · N603AL · Doug DC873 · Landing Gear Position and Warning
  > DURING CLIMB OUT, DOOR NOT LATCH LIGHT ILLUMINATED, THE CREW CYCLED THE GEAR AND DOOR NOT LATCH LIGHT CAME ON AGAIN. WHEN GEAR HANDLE IS PLACED IN UPLATCH CHECK POSITION, THE GEAR HANDLE IN UP POSITION THE LIGHT WENT OUT AND STAYED OUT REMAINDER OF FLIGHT. THE
- [SDR IXXA100023O](https://openairdocs.org/sdr/IXXA100023O.md): Uplock · no test · Mar 18, 2010 · N603AL · Doug DC873F · Landing Gear Position and Warning
  > DURING "C" CHECK INSP TEST FLIGHT, GEAR UPLATCH CHECK FAILED AFTER TAKEOFF, THE CREW CYCLED GEAR AND UPLATCH CHECK FAILED A SECOND TIME WITH GEAR RED LIGHT STAYED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED LANDING GEAR EXTENSION A
- [SDR IXXA10SMN028S](https://openairdocs.org/sdr/IXXA10SMN028S.md): Web · cracked · Jan 26, 2010 · N603AL · Doug DC873F · Wing Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP FOUND LT WING INBD LOWER SLOT DOOR WEB BROKEN. REMOVED DAMAGED WEB. FABRICATED NEW WEB. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 51-3-0, SRM 57-1-0 PAGE 1, SRM 57-3-3 FIGURE 22 ITEM "G", DPS 4.7
- [SDR IXXA10SMN24S](https://openairdocs.org/sdr/IXXA10SMN24S.md): Skin · damaged · Jan 25, 2010 · N603AL · Doug DC873F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING NR 3 INBD SLOT VANE HOLES ELONGATED AT STA XW 257.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS, INTERNAL DOUB
- [SDR IXXA10SMN027S](https://openairdocs.org/sdr/IXXA10SMN027S.md): Web · cracked · Jan 23, 2010 · N603AL · Doug DC873F · Rudder Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP FOUND RUDDER WEB INTERIOR CRACKED AT STA ZR 163.000. REMOVED CRACKED WEB. FABRICATED WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. PERFORMED RUDDER BALANCE. F
- [SDR IXXA10SMN26S](https://openairdocs.org/sdr/IXXA10SMN26S.md): Skin · corroded · Jan 23, 2010 · N603AL · Doug DC873F · Rudder, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RUDDER LT EXTERNAL SKIN CORRODED AT STA ZR 155.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED
- [SDR IXXA10SMN023S](https://openairdocs.org/sdr/IXXA10SMN023S.md): Doubler · cracked · Jan 23, 2010 · N603AL · Doug DC873F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 505F DOUBLER CRACKED AT STA XRS 22.270 STR 6. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL, INT
- [SDR IXXA10SMN022S](https://openairdocs.org/sdr/IXXA10SMN022S.md): Doubler · cracked · Jan 22, 2010 · N603AL · Doug DC873F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 506C DOUBLER CRACKED AT STA XRS 22.750 STR 13. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED INTERNAL AND EXTERNAL D
- [SDR IXXA10SMN021S](https://openairdocs.org/sdr/IXXA10SMN021S.md): Door Frame · cracked · Jan 21, 2010 · N603AL · Doug DC873F · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSP, FOUND FUSELAGE EXTERIOR "D" CARGO DOOR FWD UPPER JAMB CORNER CRACKED AT STA 1400.000 LONGERON 26 RT LONGERON 27 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABR
- [SDR IXXA10SMN025S](https://openairdocs.org/sdr/IXXA10SMN025S.md): Skin · cracked · Jan 20, 2010 · N603AL · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP T/E PANEL CRACKED AT STA XW 35.000 REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH ADHESIVE. CLEANED, TREATED, PRIMED
- [SDR IXXA10SMN017S](https://openairdocs.org/sdr/IXXA10SMN017S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STATION FS 668 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLERS AND FINGER DOUBLERS. PERFORMED NDT INSP. NO DISCREPANCY
- [SDR IXXA10SMN018S](https://openairdocs.org/sdr/IXXA10SMN018S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 1447 LONGERON 29 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED AREA
- [SDR IXXA10SMN016S](https://openairdocs.org/sdr/IXXA10SMN016S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 615 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED AREA AND R
- [SDR IXXA10SMN015S](https://openairdocs.org/sdr/IXXA10SMN015S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 36.5 LONGERON 30.5 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED ARE
- [SDR IXXA10SMN020S](https://openairdocs.org/sdr/IXXA10SMN020S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 1765 LONGERON 17.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED INTERNAL, EXTERNAL, DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INST
- [SDR IXXA10SMN019S](https://openairdocs.org/sdr/IXXA10SMN019S.md): Skin · misrepaired · Jan 11, 2010 · N603AL · Doug DC873 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 1480 LONGERON 33.5R RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED INTERNAL, EXTERNAL, DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS.
- [SDR IXXA090071O](https://openairdocs.org/sdr/IXXA090071O.md): Connector · dirty · Dec 11, 2009 · N603AL · Doug DC873F · Landing Gear System Wiring
  > ON FINAL APPROACH, WHEN MLG WAS EXTENDED THE LT MLG LIGHT STAYED OUT. THE CREW RECYCLED MAIN GEARS AND ALL WAS NORMAL. THEY LANDED WITHOUT FURTHER INCIDENT. MX REMOVED, CLEANED AND INSPECTED THE LT MAIN GEAR DOWN LOCK LIMIT SWITCH CONNECTOR. OPS CHECK GOOD I
- [SDR IXXA090066O](https://openairdocs.org/sdr/IXXA090066O.md): Switch · broken · Nov 6, 2009 · N603AL · Doug DC873F · Landing Gear Door Retract Section
  > DURING CLIMBOUT, MLG DOOR NOT LATCHED LIGHT CAME ON, THE CREW RECYCLED LANDING GEAR AND ACCOMPLISHED UPLATCH CHECK THE DOOR NOT LATCHED LIGHT STAYED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MLG AND FOUND RT GEAR DOOR SWITCH BROKEN. MX REPLACED
- [SDR IXXA090035O](https://openairdocs.org/sdr/IXXA090035O.md): Hsi · defective · Jul 29, 2009 · N603AL · Doug DC873F · Attitude and Direction Data System
  > DURING CLIMB OUT F/O ATTITUDE DIRECTOR INDICATOR AND HORIZONTAL SITUATION INDICATOR WENT BLANK. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED F/O HORIZONTAL SITUATION INDICATOR AND ATTITUDE DIRECTOR INDICATOR. OPS CHECK GOOD IAW MM 34-01-
- [SDR IXXA090015O](https://openairdocs.org/sdr/IXXA090015O.md): Fan · defective · Apr 9, 2009 · N603AL · Doug DC873F · Air Distribution Fan
  > DURING CRUISE FROM KPHL, THE CREW DETECTED SMOKE FROM THE RECIRCULATION FAN AND NOISY. THE CREW TURNED OFF RECIRCULATION FAN SMOKE ODOR DISSIPATED. THE CREW LANDED IN KEWR WITHOUT FURTHER INCIDENT. MAINTENANCE IN KEWR REPLACED THE RECIRCULATION FAN. OPERAT
- [SDR IXXA080030O](https://openairdocs.org/sdr/IXXA080030O.md): Uplock · defective · Oct 29, 2008 · N603AL · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING CLIMBOUT FROM BGTL DOOR NOT LATCH LIGHT ILLUMINATED AFTER RAISING MAIN LANDING GEAR. THE CREW ACCOMPLISHED COM PROCEDURE AND THE LIGHT STAYED ON. BOTH ALTERNATING MAIN LANDING GEAR LIGHTS WERE OUT AND TESTED GOOD. THE CREW LANDED IN KTOL WITHOUT FURT
- [SDR IXX2008F00028](https://openairdocs.org/sdr/IXX2008F00028.md): Element · malfunctioned · Jul 17, 2008 · N603AL · Doug DC873F · Fire Detection
  > FLIGHT NUMBER: 744/ETAR TO OJAM - DESCENDING INTO OJAM NUMBER THREE FIRE WARNING LIGHT AND RED LIGHT IN FIRE HANDLE CAME ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON, AND FIRE WARNING WAS INTERMITTENT. THE CREW LANDED IN OJA
- [SDR IXX2008F00026](https://openairdocs.org/sdr/IXX2008F00026.md): Fire Warning · activated · Jul 17, 2008 · N603AL · Doug DC873F · Fire Detection
  > FLT NR: 744/ETAR TO OJAM/. DESCENDING INTO OJAM NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND RED LIGHT IN FIRE HANDLE CAME ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON AND FIRE WARNING WAS INTERMITTENT. THE CREW LANDED IN OJ
- [SDR IXX2008F00023](https://openairdocs.org/sdr/IXX2008F00023.md): Fire Warning · activated · Jul 17, 2008 · N603AL · Doug DC873F · Fire Detection
  > FLT NR: 744/ETAR TO OJAM/. DESCENDING INTO OJAM NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND RED LIGHT IN FIRE HANDLE CAME ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON, AND FIRE WARNING WAS INTERMITTENT. THERE LANDED IN OJAM
- [SDR IXX2008F00012](https://openairdocs.org/sdr/IXX2008F00012.md): Engine · fire · Jul 11, 2008 · N603AL · Doug DC873F · Engine (Turbine/Turboprop)
  > DURING FLIGHT, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED MOMENTARILY. FLIGHT CREW RETARDED THE THROTTLES AND SHUTDOWN THE ENGINE. THE FIRE LIGHT AND WARNING WENT OUT. APPROX 30 MINUTES LATER FIRE WARNING CAME BACK ON. FLIGHT CREW FIRED (1) BOTTLE AND AGEN
- [SDR IXX2008F00005](https://openairdocs.org/sdr/IXX2008F00005.md): Fire Warning · malfunctioned · Jul 11, 2008 · N603AL · Doug DC873F · Fire Detection
  > DURING FLIGHT, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED MOMENTARILY. FLIGHT CREW RETARDED THE THROTTLES AND SHUTDOWN THE ENGINE. THE FIRE LIGHT AND WARNING WENT OUT. APPROX 30 MINUTES LATER FIRE WARNING CAME BACK ON. FLIGHT CREW FIRED ONE BOTTLE AND AGEN
- [SDR IXXA080003O](https://openairdocs.org/sdr/IXXA080003O.md): Connector · loose · Jan 23, 2008 · N603AL · Doug DC873F · Fire Protection System Wiring
  > DURING CRUISE FROM KTOL NUMBER THREE FIRE WARNING LIGHT STARTED TO FLICKER AND HORN SOUNDED. THE CREW TESTED NUMBER THREE ENGINE FIRE WARNING NO BELL OR LIGHT, PERFORMED FIRE DAMAGED CHECK LIST PULL FIRE HANDLE FORWARD TEST FIRE WARNING TESTED GOOD ALL ENGINE
- [SDR IXXA070054O](https://openairdocs.org/sdr/IXXA070054O.md): Warning System · malfunctioned · Oct 26, 2007 · N603AL · Doug DC873F · Landing Gear Position and Warning
  > DURING CLIMB-OUT FROM KDFW TO KIAH, AFTER GEAR RETRACTION THE CREW NOTICED DOOR NOT LATCH LIGHT STAYED ON UNTIL THE CREW RECYCLED THE GEARS AND LIGHT WENT OUT. CREW LANDED AT KIAH WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN LANDING GEAR DOOR TARGET AND STRI
- [SDR IXXA070038O](https://openairdocs.org/sdr/IXXA070038O.md): Actuator · out of adjust · Aug 10, 2007 · N603AL · Doug DC873F · Landing Gear Actuator
  > DURING CLIMB-OUT FROM KTOL, THE GEAR DOORS NOT LATCHED LIGHT ILLUMINATED. THE CREW PERFORMED AN UP-LATCH CHECK AND THE LEFT MAIN GEAR DOOR OPEN YELLOW LIGHT ILLUMINATED. THE CREW RECYCLED GEAR AND HAD A SUCCESSFUL UPLATCH CHECK BUT DOOR NOT LATCHED LIGHT REM
- [SDR IXXA07SMN193S](https://openairdocs.org/sdr/IXXA07SMN193S.md): Panel · deformed · Jul 4, 2007 · N603AL · Doug DC873F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION; FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER PANEL DEFORMED BETWEEN STATION XW 123.000 AND STATION XW 136.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS.
- [SDR IXXA07SMN187S](https://openairdocs.org/sdr/IXXA07SMN187S.md): Stringer · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Wing, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND NR 4 MAIN TANK CRACKED STRINGER AT STATION XRS 190.000 AND STRINGER 58. ACCESS THROUGH 505D DOOR. REMOVED FUEL PUMP MOUNT BRACKET. REMOVED DAMAGED AREA AT UPPER HORIZONTAL AND VERTICAL FLANGES. PERFORMED NDT INSPEC
- [SDR IXXA07SMN184S](https://openairdocs.org/sdr/IXXA07SMN184S.md): Fitting · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MID SHIP ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 660.000 LONGERON 35LEFT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING BETWEEN STATION 660.000 AND LONGERON 35LEFT IAW DC8 SRM 51-1-20D, 51-3-1.
- [SDR IXXA07SMN179S](https://openairdocs.org/sdr/IXXA07SMN179S.md): Skin · misrepaired · Jun 30, 2007 · N603AL · Doug DC873F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT ELEVATOR ON LOWER SKIN AT STATION XE 39.188. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL
- [SDR IXXA07SMN166S](https://openairdocs.org/sdr/IXXA07SMN166S.md): Skin · misrepaired · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 380 LONGERON 33RIGHT, RIGHT FORWARD FUSELAGE JUST AFT OF A-PIT DOOR OPENING. AVERAGE AND MAXIMUM RIVET SPACING EXCEEDED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. R
- [SDR IXXA07SMN163S](https://openairdocs.org/sdr/IXXA07SMN163S.md): Sill · misrepaired · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LONGERON 21 LEFT AT FS 235 MAIN CARGO DOOR LOWER AFT SILL TO AFT JAMB CORNER. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REP
- [SDR IXXA07SMN162S](https://openairdocs.org/sdr/IXXA07SMN162S.md): Sill · misrepaired · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT MAIN CARGO DOOR COVER SILL AT FS235 LONGERON 21 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREAT
- [SDR IXXA07SMN174S](https://openairdocs.org/sdr/IXXA07SMN174S.md): Longeron · broken · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT FLANGE ON LONGERON 19 RIGHT BROKEN AT STATION 200.000 TO 212.000. LONGERON FLANGE FROM AT STATION 200.000 TO 212.000, LONGERON19 RIGHT WAS TRIMMED OFF IN PRODUCTION. NO REPAIR IS REQUIRED. F
- [SDR IXXA07SMN191S](https://openairdocs.org/sdr/IXXA07SMN191S.md): Floorbeam · corroded · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Floor Beam
  > DURING ROUTINE C CHECK INSPECTION, FOUND IN AFT CARGO COMPARTMENT FLOORBEAM UPPER FLANGE SHOWS CORROSION AT STATION 1520.000 RIGHT BOTTOM LINE 44". REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALAN
- [SDR IXXA07SMN182S](https://openairdocs.org/sdr/IXXA07SMN182S.md): Bracket · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Wing, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 ALT FUEL TANK BOOSTER PUMP SUPPORTS CRACKED AT STRINGER 59 STATION XW 456.000. REMOVED CRACKED BRACKET. INSTALLED NEW BRACKET AT STATION XW 456.000, STRINGER 59 IAW DC8 SRM 51-1-20D AND 51-3-1.
- [SDR IXXA07SMN183S](https://openairdocs.org/sdr/IXXA07SMN183S.md): Fitting · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 1760.000 TO 1766.000 LONGERON 10 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1.
- [SDR IXXA07SMN185S](https://openairdocs.org/sdr/IXXA07SMN185S.md): Fitting · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND IN MIDSHIP ACCESSORY COMPARTMENT A FITTING CRACKED STATION 660.000 LONGERON 36. REMOVED CRACKED FITTING. INSTALLED NEW FITTING. IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.
- [SDR IXXA07SMN186S](https://openairdocs.org/sdr/IXXA07SMN186S.md): Fitting · cracked · Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT A CRACKED FITTING AT STATION 1180.000 LONGERON 34 RIGHT, AND LONGERON 35 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.

Next page: https://openairdocs.org/deregistered/N603AL-2015-09-18/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 = 'N603AL' AND deregistration_id = 'N603AL-2015-09-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N603AL-2015-09-18/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.
