N604AL

Service difficulty reports not matched to an aircraft · 332

They name N604AL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N604AL' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IXXA110045OLatch · failedAFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NOSE GEAR AND FOUND RT NOSE GEAR DOOR OPENED. THEY CLOSED AND SECURED DOOR LOCK MECHANISM DOOR. OPS CHECK GOOD IAW MM 32-22-1. Jun 5, 2011 · N604AL · Doug DC873F · Landing Gear DoorsSDR DHL2004809005Rib · crackedLEFT-HAND INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 INCH CRACK OUTBOARD RIB LOWER CORD 40 INCHES FROM TRAILING EDGE. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 16040E. Mar 15, 2004 · N604AL · Doug DC873F · Trailing Edge FlapsSDR DHL2004809004Spar · crackedLT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 1604Mar 15, 2004 · N604AL · Doug DC873F · Wing SparSDR DHL2004809003Fitting · crackedRIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTERED AS DMI 16041E. ONLY 2 REVENUE FLIGMar 15, 2004 · N604AL · Doug DC873F · Wing, Attach FittingsSDR DHL2004809002Windshield · crackedF/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S FORWARD SIDE WINDOW IAW DC8 M/M 56-10-2, NO LEAKS NOTED.Feb 27, 2004 · N604AL · Doug DC873F · Flight Compartment WindowsSDR DHL2004809001Fan · noisyON TAKEOFF AND AT CRUISE ALTITUDE, RECIRCULATION FAN IS LOUD & VIBRATION IS FELT UNDERFLOOR NEAR LAV NOISE DECREASES WITH FAN OFF. DEFERRED RECIRCULATION FAN, PLACARD INSTALLED. AT FL 330, 30 MINUTES INTO FLT, NOTED BURNING ODOR IN FLOOR AREA NEAR LAV MID CAFeb 17, 2004 · N604AL · Doug DC873F · Air Distribution FanSDR DHL2003809011Battery · inoperativeDURING BISE CHECK - EMERGENCY LIGHT SWITCH MUST BE RECYCLED ONCE BEFORE EMERGENCY LIGHTS FUNCTION NORMALLY. REMOVED AND REPLACED AIRCRAFT BATTERY, OPS CHECKED GOOD PER DC-8 M/M 24-30-1.Dec 31, 2003 · N604AL · Doug DC873F · Emergency LightingSDR DHL2003809010Bellcrank · crackedMAIN ENTRY DOOR IS DIFFICULT TO OPEN AND CLOSE. FOUND BAYONET BELLCRANK CRACKED, ALSO FOUND DAMAGED ROLLER ASSEMBLY ON DOOR SEAL ACTUATING CRANK. REMOVED BAD PARTS.Dec 28, 2003 · N604AL · Doug DC873F · Passenger/Crew DoorsSDR DHL2003809009Door · lack of lubeMAIN CABIN DOOR HARD TO CLOSE. LUBED MAIN CABIN DOOR MECHANISM. OPS CHECKED GOOD PER 52-11-1.Dec 27, 2003 · N604AL · Doug DC873F · Passenger/Crew DoorsSDR DHL2003809008Battery · dischargedEMERGENCY EXIT LIGHT OVER ENTRY DOOR INOPERATIVE. RECHARGED BATTERY AND OPS CHECKED GOOD PER M/M 33-50-0.Dec 2, 2003 · N604AL · Doug DC873F · Emergency LightingSDR DHL2003809007Door · out of adjustCOCKPIT DOOR BINDING OUTSIDE KNOB SO SMOOTH YOU CAN NOT PULL DOOR OPEN WHEN UNLOCKED. ADJUSTED DOOR IAW SMM 52-51-01 OPS CHECKED OK.Nov 29, 2003 · N604AL · Doug DC873F · Fixed Inner DoorsSDR DHL2003809006Latch · out of adjustFLIGHT DECK DOOR WILL NOT LATCH CLOSED PROPERLY AND JAMS IN CLOSED POSITION. ADJUSTED UPPER LATCH AND OPS CHECKED PER MSI M/M 52-10-0. ALL CHECKS GOOD.Nov 22, 2003 · N604AL · Doug DC873F · Passenger/Crew DoorsSDR DHL2003809005Handle · unsecureAT BEGINNING OF TAKEOFF ROLL BELLY DOOR LIGHT ILLUMINATED. DURING TAXI DOOR LIGHT ILLUMINATED INTERMITTENTLY. FOUND B PIT DOOR HANDLE NOT SECURED. RE-SECURED HANDLE. OPS CHECKED NORMAL IAW M/M 25-51-0. REJECTED T/O RWY 27 AT 271,000 LBS. AT 70 KTS. / ZONE 2Nov 12, 2003 · N604AL · Doug DC873F · Door Warning SystemSDR DHL2003809004Door · out of adjustCOCKPIT ENTRY DOOR JAMS AND IS VERY HARD TO OPEN FROM THE GALLEY SIDE. ADJUSTED DOOR PER SMM AND M/M 51-10-0.Nov 8, 2003 · N604AL · Doug DC873F · Fixed Inner DoorsSDR DHL2003809003Door · out of adjustCOCKPIT DOOR IS HARD TO OPEN FROM THE OUTSIDE. DOOR JAMMED CLOSED. ADJUSTED COCKPIT DOOR PER M/M 52-10-0. OPS CHECKED GOOD.Oct 31, 2003 · N604AL · Doug DC873F · Fixed Inner DoorsSDR DHL2003809002Mec · malfunctionedNR 3 ENG FAILED 3-5 MIN AFT SETTING CRUISE THRUST (0938Z) ENG LOST POWER SLOWLY. PERFORMED ENG FAILURE CHECKLIST ATTEMP RESTART, NO FUEL FLOW, OR EGT INDICATION, BOOST PUMP 21 PSI. ENG WINDMILL TIME 1 HR 22 MIN. OIL PRESS DROPPED TO 0 AFT APPROX 10-15 MIN AOct 8, 2003 · N604AL · Doug DC873F · Fuel Control/Turbine EnginesSDR DHL2003809001Battery · dischargedDURING PREFLIGHT EMERGENCY EXIT LIGHTS AND STANDBY ATTITUDE INDICATOR WERE FOUND INOPERATIVE. TROUBLESHOT SYSTEM, FOUND EMERGENCY LIGHTS NOT GETTING ENOUGH POWER FROM AC BATTERY. REPLACED AC BATTERY. SYSTEM OPS CHECKED GOOD IAW 33-50-0.Sep 12, 2003 · N604AL · Doug DC873F · Emergency LightingSDR DHL2003604790Warning System · faultyGPWS FAIL LIGHT ILLUMINATED. REPLACED GPWS MK II WITH GPWS/WS MKVII AND OPS CHECKED GOOD IAW J/C EA34450002-001-D.Aug 18, 2003 · N604AL · Doug DC873F · Ground Proximity SystemSDR DHL2003604756Door Frame · damagedTWO INTERIM REPAIRS ON LT AFT LWR CORNER OF MAIN CARGO DOOR STA 270.000 BETWEEN L-20L AND L-22L. REMOVED FASTENERS AND INTERIM REPAIR. TRIMMED OUT DAMAGED AREA IAW EODHL-030584 ED-3486. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. Jul 24, 2003 · N604AL · Doug DC873F · Fuselage Main, StructureSDR DHL2003604696Splice · crackedFWD CARGO COMPT SPLICE FITTING CRACKED 2.000 STA 440.000 - 460.000, L-31L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITJul 14, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604747Skin · corrodedFUSELAGE NOSE SECTION EXTERNAL SKIN CORRODED & DENTED BETWEEN STA 35.000 AND STA 70.000, L-31L TO L-31R. REMOVED FASTENERS & EXISTING EXTERNAL DOUBLER. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN PANEL SEGMENT. PERFORMED EDDY CURRENT IJul 14, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604757Stringer · crackedLT WING NR 1 ALT TANK, S-59 CRACKED 1.500 (LOWER), NEAR XRS 463.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG 3D, 3E, 3F. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED SPLICES (02 EA), CLIPS (02) AND SPACERS (04 EA) Jul 9, 2003 · N604AL · Doug DC873F · Wing, Longeron/StringerSDR DHL2003604675Frame · brokenAFT CARGO COMPT. DOOR NR 4 FRAME ANGLE BROKEN, STA.1440.000. REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG.1. FABRICATED NEW ANGLE (2024-T3 AL0.040) IAW SRM 53-2-0 PG.1-2. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-Jul 8, 2003 · N604AL · Doug DC873F · Fuselage Main, FrameSDR DHL2003604676Angle · brokenAFT CARGO COMPT DOOR NR 4 FRAME ANGLE BROKEN, STA 1440.000 CORR REMOVED BROKEN ANGLE IAW SRM 51-3-0 PG 1. FABRICATED NEW ANGLE IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED, AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0 PG 1.Jul 7, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604670Attach Fitting · crackedLT WING T/E INNER UPPER FITTING CRACKED 1.000 AT XRS.434.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON LT. WING T/E AT XRS. 434.000 IAW SRM 51-1-20DJul 4, 2003 · N604AL · Doug DC873F · Wing, Attach FittingsSDR DHL2003604758Skin · dentedRT ELEVATOR UPPER PLATING CTR. SECTION HAS DENTS FROM XE. 132.000 TO XE. 246.000 PERFORMED MAJOR REPAIR IAW EODHL-030525, ED-3276. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030525, ED-3276. CLEANED, TREATED AND PRIMED AREA IAJun 28, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604787Skin · dentedFUSELAGE EXTERIOR SKIN SHOWS DENTS (03 EA), FS 255.000, L-24L TO L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030516, ED-3357. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DENTS IAW EODHL-030516, ED-3357. PERFORMED EDDY CURRENT INSPECTION Jun 25, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604672Skin · damagedLT IB AILERON LWR SURFACE WITH INTERIM REPAIR BETWEEN STA.XA441.000 AND XA.502.000. PERFORMED MAJOR REPAIR IAW EODHL-030569, ED-3399. REMOVED FASTENERS AND DAMAGED SKIN SEGMENT INCLUDING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW SKIN SEGMENT (2024-TJun 25, 2003 · N604AL · Doug DC873F · AileronsSDR DHL2003604591Panel · crackedRT OUTBOARD SLOT UPPER CENTER DOOR WITH 0.500 CRACK IN IT. REMOVED AND REPLACED RT OUTBOARD SLOT UPPER CENTER DOOR IAW MM 27-80-2 PG 201-204. REFER TO NR 0531 FOR OPS CHECK.Jun 25, 2003 · N604AL · Doug DC873F · Leading Edge DevicesSDR DHL2003604793Cargo Track · wornMAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA -55.000 - STA 310.000. REMOVED NR 2 TRACK WITH WORN LUGS IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW NR 2 TRACK ON MAIN CARGO COMPT STA -55.000 - STA 310.000 IAW SRM 51-3-0 Jun 24, 2003 · N604AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003604667Skin · corrodedRT ELEVATOR UPPER SKIN INBD SECTION SHOW CORROSION, SEVERAL DENTS AND INTERIM REPAIR FROM STA XAR 0.000 TO XE 132.000. REMOVED FASTENERS AND THE DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKINJun 24, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604666Skin · corrodedRT ELEVATOR LOWER OUTER SKIN CORRODED ON SEVERAL SPOTS FROM STA XE 246.000 TO STA XH 285.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030574, ED 3411. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IJun 24, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604674Skin · corrodedRT ELEVATOR LOWER PART EXTERNAL SKIN SHOWS DEFLECTION AND CORROSION FROM STA. XAR.0.000 TO XE.132.000. PERFORMED MAJOR REPAIR IAW EODHL-030521, ED-3405. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1, SRM 51-1-21A PG.4. CLEANED, TREATED AND PRIJun 24, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604768Skin · corrodedRT ELEVATOR UPPER PLATING OTBD SECTION SHOWS INTERIM REPAIR AND CORROSION FROM STA XE 246.000 TO XH 285.000. REMOVED FASTENERS, REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL, CLEANED, TREATED AND PRIMED AREA. FABRICATED NEW SKIN PANEJun 24, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604777Fitting · crackedMAIN CARGO COMPT DOOR FRAME LOWER INTERNAL SKIN FITTING 2.00 CRACKED AT STA 255.000, L-21L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLEJun 24, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604748Skin · dentedRT ELEVATOR OUTER LOWER SKIN HAS DENTS ON SEVERAL SPOTS FROM STA. XE.132.000 TO XE.246.000. PERFORMED MAJOR REPAIR IAW EODHL-030522, ED-3406. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1, SRM 51-1-21A PG.4. CLEANED, TREATED AND PRIMED AREA IAWJun 24, 2003 · N604AL · Doug DC873F · Elevator, Plate/SkinSDR DHL2003604762Skin · corrodedFWD CTR SECTION SHOWS SEVERAL SPOTS OF CORROSION AND DOUBLER REPAIR (03 EA.) BETWEEN STA.660.000 AND STA.725.000, L-34L TO L-34R. PERFORMED MAJOR REPAIR IAW EODHL-030564, ED-3389. REMOVED FASTENERS AND DOUBLER REPAIRS, REMOVED CORROSION. FOUND OUT OF LIMITS.Jun 22, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604738Skin · corrodedLOWER FUSELAGE PLATING SHOWS 04 SPOTS OF CORROSION BETWEEN STA 743.000 AND STA 767.000, L-35L TO L-35R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT THE DAMAGED SKIN AREA IAWJun 22, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604603Fairing · delaminatedLT OTBD FAIRING ASSY WITH EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED OB FAIRING ASSY ON LT WING IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 0531.Jun 22, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003604664Plate · dentedRT WING INBD FLAP UPPER PLATING SHOWS DENTS AND WEAR OUT OR LIMITS BETWEEN STA XW 104.000 TO XW 115.000. REMOVED FASTENERS AND DAMAGED SKIN PANEL IAW SRM 51-1-21 PG.1. CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN PANEL ( 2024-T3AL 0.Jun 21, 2003 · N604AL · Doug DC873F · Trailing Edge FlapsSDR DHL2003604701Frame · crackedFWD ACCY COMPT FRAME CRACKED 2.000, STA 55.000, L-24L. TRIMMED OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW FRAME SEGMENT (7075-T6 AL0.071) AND SPLICE ANGLE (02 EA) (7Jun 21, 2003 · N604AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003604741Skin · corrodedLT WING INBD. L/E SLANT PANEL UPPER CAP SHOWS CORROSION FROM XFS.63.750 TO XFS.82.500 AND REPAIR DOUBLER FROM XFS.201.000 TO XFS.207.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 5Jun 20, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003604724Skin · corrodedRT INNER WING LE SLANT PANEL UPPER CAP SHOWS CORROSION BETWEEN XFS.93.000 AND XFS.107.500, REPAIR DOUBLERS. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-2-1 FIG.37, SRM 57-3-3 FIG.2. REMOVED CORROSION ON UPPER CAP IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LJun 20, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003604725Door Frame · crackedSECTION AROUND EMERGENCY EXIT DOOR AFT LOWER JAMB HAS TWO CRACKS OF 0.750 AND 0.500 AT STA. 415.250 BETWEEN L-19L AND L-22L PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM. PERFORMED STOP HOLE ON CRACKS END USING A 0.250 DIA. DRILL AND TRIMMED OUT THE CRACKJun 19, 2003 · N604AL · Doug DC873F · Fuselage Main, StructureSDR DHL2003604582Skin · delaminatedRT NR 2 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER ON RT WING IAW 27-81-1 PG 201-206. FOR OPS CHECK SEE N/R 0531.Jun 19, 2003 · N604AL · Doug DC873F · SpoilersSDR DHL2003604729Splice · crackedFWD CARGO COMPT. SPLICE FITTING CRACKED 1.000, STA.200.000 - 220.000, L-27R. (MAJOR REPAIR) CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM NR P0201388, DWG. 4653726. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG.21, SRM 51-1-21 PG.1. FABRICATED SPJun 17, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604709Skin · dented"A" CARGO DOOR EXTERNAL SKIN HAS (2) INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG.1, SRM 52-4-1 FIG.2 BOEING MESSAGE DHL-CVG 03-00079H. REMOVED DAMAGED SKIN IAW SRM 51-1-21 OG,1, SRM 51-1-20D PG.21. CLEANED, TREATED AND Jun 17, 2003 · N604AL · Doug DC873F · Cargo/Baggage DoorsSDR DHL2003604785Frame · corrodedFWD CARGO COMPT PRESSURE BULKHEAD FRAME CORRODED STA 70.000, L-28L - L-32L. REMOVED FASTENERS AND ATTACH FITTING (04 EA). REMOVED CORROSION ON FRAME STA.70.000, L-28L - L-32L, FOUND OUT OF LIMITS. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIJun 17, 2003 · N604AL · Doug DC873F · Fuselage Main, FrameSDR DHL2003604774Splice · crackedAFT ACCESSORY COMPT FRAME SPLICE FITTING HAS A 2.000 CRACK, STA 660.000 L-35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201385, DWG 3750498. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FJun 17, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604681Frame · corrodedLT MLG W/W SPOILER AND AILERON ACTUATING MECH SUPPORT Z-FORMER CORRODED AT STA 857.000, LBL-54. REMOVED CORROSION ON FORMER IAW SRM 51-1-8 PG 17, 18. FOUND OUT LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED Z-FORMER IAW SRM 51-1-21 PG 1. CLEANED, TREATED ANJun 16, 2003 · N604AL · Doug DC873F · Fuselage Main, Frame
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