# Service difficulty reports: N364DH, cancelled May 16, 2017

A list on [N364DH, cancelled May 16, 2017](https://openairdocs.org/deregistered/N364DH-2017-05-16.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 · 133 reports

- [SDR DHLA200900036](https://openairdocs.org/sdr/DHLA200900036.md): Oil Filter · clogged · Jun 16, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil System
  > FILTER CLOG LIGHT ILLUMINATED ON MWP. FILTER NR 2 OIL CLOG LIGHT ILLUMINATED ON S/O PANEL AFTER TAKEOFF. REMOVED AND REPLACED MAIN ENGINE OIL FILTER P/N AC9380F4010 IAW MM 79-22-01. OPS AND LEAKS CK GOOD IAW JRH 18.1.
- [SDR DHLA200900032](https://openairdocs.org/sdr/DHLA200900032.md): Switch · failed · May 26, 2009 · N364DH · Airbus A300B42C · Engine Oil System (Airframe Furnished)
  > ENGINE NR 2 "OIL CLOG" LIGHT ILLUMINATED INFLIGHT ENGINE 2 WAS SHUTDOWN WITH INFLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURE ALL ENG IND NORMAL. REPLACED NR 2 ENG OIL FILTER CLOGGING SWITCH PER MM 79-35-11. RAN NR 2 ENG PER JRH 16.5. SYS OPS TEST NORMAL. FOLLO
- [SDR DHLA200900025](https://openairdocs.org/sdr/DHLA200900025.md): Coalescer Bag · dirty · Apr 14, 2009 · N364DH · Airbus A300B4203 · Humidity Control System
  > REPLACED NR 2 COALESCER P/N 20D10-3 IAW MM 21-51-16. THIS DOES NOT CLOSE DMI.
- [SDR DHLA200900023](https://openairdocs.org/sdr/DHLA200900023.md): Coalescer Bag · contaminated · Apr 8, 2009 · N364DH · Airbus A300B42C · Humidity Control System
  > NR 2 PACK STILL HAS AN OILY ODOR 25 MIN INTO FLT R FWD CABIN SMOKE LIGHT ILLUM COMPLIED WITH EMERGENCY CHECK LIST SMOKE LIGHT WENT OUT WHEN NR 2 PACK SELECTED OFF RESOLUTION: FOUND RESIDUAL OIL IN WATER SEPARATOR BAGS (RT). PURGED RT A/C SYSTEM IAW MM 21-51-0
- [SDR DHLA200900022](https://openairdocs.org/sdr/DHLA200900022.md): Engine · leaking · Apr 4, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil System
  > STRONG OIL ODOR FROM PACK NR 2 WHEN THROTTLE AT IDLE AND HP VALVE ON ENGINE NR 2 OPEN. ALL PRESS AND TEMPS NORMAL. PLACED NR 2 PACK ON DMI LIST PER MEL 21-51-01, CAT C, DDD 4-14-09. CONTROL NR 34715. PLACARD INSTALLED. BOROSCOPE ENGINE FOUND OIL WETTING,
- [SDR DHLA20090020](https://openairdocs.org/sdr/DHLA20090020.md): Coalescer Bag · contaminated · Apr 3, 2009 · N364DH · Airbus A300* · Humidity Control System
  > FLT 165 OIL ODOR WITH NR 2 PACK OPERATING. DEFFERED NR 2 PACK IAW MEL 21-51-01 CAT C ASSIGNED DMI 34713 PLACARDS INSTALLED. R/R NR 2 COALESCAR SOCK IAW MM 21-51-16 NO ODOR NOTED WHEN OPERATING NR 2 PACK, THIS CLEARS DMI 34713 PLACARD REMOVED P/N 20D10-3. AIRCR
- [SDR DHLA200900021](https://openairdocs.org/sdr/DHLA200900021.md): Unknown · odor · Apr 1, 2009 · N364DH · Airbus A300B4203 · Air Distribution System
  > ACFT HAS AN UNUSUAL ODOR COMING THRU THE A/C PACKS FLT DECK DUCT TEMP WAS AT 150 COMPT TEMP 68. RAN NR 1 AND NR 2 PACK SYS OPS CKED NORMAL ON GROUND IAW AMM 21-00-00 COULD NOT DUPLICATE NO UNUSUAL ODORS
- [SDR DHLA200800004](https://openairdocs.org/sdr/DHLA200800004.md): Uplock Switch · malfunctioned · Jan 10, 2008 · N364DH · Airbus A300B4203 · Landing Gear Door Retract Section
  > FLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESECURED RT MLG INBD DOOR UPLOCK SWITCHES, OPERATED GEAR DOORS. NO DEFECTS NOTED, REF M/M 32-30-00. OPS NORMAL AT THIS TIME. ACFT GROUNDED.
- [SDR DHLA200700079](https://openairdocs.org/sdr/DHLA200700079.md): Sequence Valve · malfunctioned · Dec 8, 2007 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > UPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LANDING GEAR UNSAFE INDICATION ABNORMAL PROCEDURE. LOWERED GEAR. GOT ALL 3 GREEN. CONTACTED MAINT AND FLIGHT CONTROL. RETURNED TO JFK.
- [SDR DHLA200700040](https://openairdocs.org/sdr/DHLA200700040.md): Pitot Tube · malfunctioned · Aug 8, 2007 · N364DH · Airbus A300B4203 · Pitot/Static System
  > NO AIRSPEED INDICATION ON STANDBY AIRSPEED INDICATION AT 80 KTS ON CAPT AND FO'S INDICATORS. REJECTED T/O TO WEIGHT 231.2 OAT 26 DEGS C PA 103FT BRAKE TEMP 200 DEGS C 1. REMOVED AND REPLACED STANDBY AIRSPEED PITOT PROBE AS PER A300 MM 34-11-15. PERFORMED LE
- [SDR DHLA200700039](https://openairdocs.org/sdr/DHLA200700039.md): Pitot Line · obstructed · Aug 8, 2007 · N364DH · Airbus A300B4203 · Pitot/Static System
  > NO AIRSPEED INDICATION ON STANDBY A/S IND AT 80KTS ONCA AND FO IND REJECTED T/O WEIGHT 273.6 26C OAT P.A 73FT BRAKE TEMP230 1. FLUSHED PITOT STATIC SYSTEM AS PER 34-11-10. OPS NORM AS PER MM 34-11-22 A/C RVSM COMPLIANT.
- [SDR DHL2007364001](https://openairdocs.org/sdr/DHL2007364001.md): Frame · bent · Jul 1, 2007 · N364DH · Airbus A300B4203 · Fuselage Main, Frame
  > DURING A "A"-8 CHECK AT AVBOURNE HVY MX IN MIAMI, THE FOLLOWING DISCREPANCIES WERE NOTED. EXISTING FRAME DOUBLER AT STA 1499 FRAME 21 BETWEEN STR 6 AND 7R WAS BENT. REMOVED EXISTING REPAIR IAW A300 SRM 53-10-10, FABRICATED REPAIR DOUBLER FROM 2024-O.071, H
- [SDR DHL2007364007](https://openairdocs.org/sdr/DHL2007364007.md): Mechanism · contaminated · Feb 15, 2007 · N364DH · Airbus A300B4203 · Escape Slide
  > LEFT MAIN DOOR SLIDE WARNING LIGHT FLASHING IN FLIGHT WITH SLIDE ARMED AND NO DOORS LIGHT ILLUMINATED. REMOVED ICE DEBRIS FROM LT DOOR SLIDE ARMING MECHANISIM. OPS CK GOOD IAW AMM 52-10-30.
- [SDR DHL2006364007](https://openairdocs.org/sdr/DHL2006364007.md): Smoke Detector · activated · Jun 27, 2006 · N364DH · Airbus A300B4203 · Smoke Detection
  > PRIOR TO T/O, DURING STATIC RUNUP, MWP SMOKE LIGHT ACCOMPANIED BY MAIN DECK SMOKE DETECTORS 7 & 8 ILLUMINATED ACCOMPANIED BY ACRID SMELL. REPLACED GRD AIR CART DUE TO SUSPECTED OIL CONTAMINATION. RAN ENGS PER ASTAR JRH 16.5. NO FURTHER DEFECTS NOTED.
- [SDR DHL2006364006](https://openairdocs.org/sdr/DHL2006364006.md): Smoke Warning · malfunctioned · Jun 27, 2006 · N364DH · Airbus A300B4203 · Smoke Detection
  > MWP SMOKE WARNING DURING T/O ACCOMPANIED BY ILLUMINATION OF CABIN DETECTORS NR 7 & NR 8 CAUSED REJECTED TAKEOFF, LIGHTS WENT OUT WHILE WAITING ON TAXIWAY. PERFORMED SYS TEST OF MAIN DECK FIRE DETECTION SYSTEMS. OP CK GOOD IAW AMM 26-14-00. ALSO PERFORMED OP
- [SDR DHL2006364504](https://openairdocs.org/sdr/DHL2006364504.md): Tee Fitting · cracked · May 11, 2006 · N364DH · Airbus A300B4203 · Nacelle/Pylon, Frame/Spar/Rib
  > PERFORM EDDY CURRENT INSPECTION OF NR 1 PYLON RIB NR 4 I/B SIDE TEE BRACKET TO VERIFY PREVIOSLY ID CRACK AS PER SB A300-54-068. REMOVED AND REPLACED "T" BRACKET AND RIB NR 4 AT NR 1 PYLON I/B AREA AS PER SRM 51-10-40.
- [SDR DHL2006364503](https://openairdocs.org/sdr/DHL2006364503.md): Seat Track · corroded · Apr 26, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK FLANGE AT FS 37 - FS 22 AT RBL 16 HAS CORROSION (MARKED 35/079) UNDER THE FLOOR PANEL. REMOVED CORROSION FROM FS 22 - FS 37 IAW A300 SRM 51-40-11, FOUND OUT OF LIMITS FROM FS 23 - FS 26 AND BET FS 32 AND FS 34, ORIG MAT.078 MAX MAT. R
- [SDR DHL2006364502](https://openairdocs.org/sdr/DHL2006364502.md): Seat Track · corroded · Apr 26, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK FLANGE AT FS 42 - FS 47 RBL16 HAS CORROSION. REMOVED CORROSION AT CABIN FLOOR SEAT TRACK FLANGE BETWEEN FS 42- FS 47 AT RBL 16 IAW A300 SRM 51-40-11, ORIG MAT.078 IAW A300 SRM 51-21-20 FIG 55 MAT. REMOVED.003 MAT REMAINING.075 FOUND WITHI
- [SDR DHL2006364501](https://openairdocs.org/sdr/DHL2006364501.md): Seat Track · corroded · Apr 26, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK FLANGE AT FS 37 - FS 22 AT RBL 58, SUPPORT FLANGES FOR FLOOR PANELS HAS CORROSION. REMOVED CORROSION AT CABIN SEAT TRACK FLANGES FS 22 - FS 37 RBL 58 IAW A300 SRM 51-40-11 ORIGINAL MAT.078 FOUND OUT OF LIMITS 4 SPOTS AT FS 24 O/B, FS 2
- [SDR DHL2006364505](https://openairdocs.org/sdr/DHL2006364505.md): Seat Track · corroded · Apr 26, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN FLOOR SEAT TRACK FLANGE AT FS 25 - FS 22 AT LBL78 HAS CORROSION AT FLOOR SUPPORT FLANGE (MARKED 35/088). REMOVED CORROSION AT SEAT TRACK FROM FS 22 - FS 25 LBL78 IAW SRM A300 51-40-11. FOUND OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612, ORIG MAT.
- [SDR DHL2006364509](https://openairdocs.org/sdr/DHL2006364509.md): Seat Track · corroded · Apr 26, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK FLANGE AT FS 70 AT RBL 78 HAS CORROSION. CUTOUT CORRODED SECTION. FABRICATED, AND INSTALLED REPAIR AT SEAT TRACK FLANGE AT FS 70 RBL78 IAW A300 SRM 53-10-10 FIG 721A.
- [SDR DHL2006364506](https://openairdocs.org/sdr/DHL2006364506.md): Seat Track · corroded · Apr 25, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN SEAT TRACK FLANGE AT FS 45 - FS 46 AT LBL 38 HAS CORROSION. REMOVED CORROSION AT FLANGE SEAT TRACK FS 45-46 LBL38 PER A300 SRM 51-40-11 ORIG MAT.078 MAT. REMOVED.016 MAT. REMAINING.052 FOUND OUT OF LIMITS PER A300 SRM 53-10-00 FIG 612. CUTOU
- [SDR DHL2006364507](https://openairdocs.org/sdr/DHL2006364507.md): Seat Track · corroded · Apr 25, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK FLANGE FS 47 - FS 54 AT RBL 38 HAS CORROSION. REMOVED CORROSION AT SEAT TRACK FROM FS 47 - FS 54 RBL38 IAW A300 SRM 51-40-11. FOUND OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612 ORIG MAT.078 MAT REMOVED.027 MIN REMAINING MAT..051. REMOVED
- [SDR DHL2006364508](https://openairdocs.org/sdr/DHL2006364508.md): Seat Track · corroded · Apr 25, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK FLANGE BETWEEN FS 41 - FS 47 HAS CORROSION LBL16. REMOVED CORROSION FROM FS 41 - FS 47 IAW A300 SRM 51-40-11. FOUND OUT OF LIMITS FROM FS 44 - FS 47 IAW A300 SRM 53-10-00 FIG 612, ORIG MAT.078 MAX MAT. REMOVED.027 MIN MAT REMAINING.051.
- [SDR DHL2006364500](https://openairdocs.org/sdr/DHL2006364500.md): Seat Track · corroded · Apr 25, 2006 · N364DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR PANEL SUPPORT AT FRAME 47 THRU FRAME 50 AT LBL 78 SEAT TRACK FLANGE BEAM HAS CORROSION. REMOVED CORROSION AT SEAT TRACK FROM FR 47 TO FR 50 LBL 78 IAW A33 SRM 51-40-11, FOUND OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612 ORIG MAT.078" MAT REMOVED.
- [SDR DHL2006364511](https://openairdocs.org/sdr/DHL2006364511.md): Structure · corroded · Apr 22, 2006 · N364DH · Airbus A300B4203 · Fuselage Main, Structure
  > UPPER FUSELAGE LT STA 4641 (FS 75) STR 6L HAS CORROSION. REMOVED CORROSION AT UPPER FS LT STA 4641 (FS 75) STR 6L MAT. REMOVED.020 MAT, REMAINING.063 BEYOND LIMITS IAW A300 SRM 53-10-00. CUT OUT AREA OF DAMAGE 4" BY 3 1/2" IAW A300 SRM 53-10-00 FIG 701. I
- [SDR DHL2006364510](https://openairdocs.org/sdr/DHL2006364510.md): Stringer · corroded · Apr 22, 2006 · N364DH · Airbus A300B4203 · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE RT, STA 4641 (FR75) STR 6R HAS CORROSION. REMOVED CORROSION AT UPPER FUSELAGE STA 4641 (FR75) STR 6R. MAT REMOVED.017 MAT REMAINING.O66 BEYOND LIMITS IAW A300 SRM 53-10-00. CUT OUT AREA DAMAGE 3 1/2" NR 3 1/4" PER A300 SRM 53-10-20 FIG 701.
- [SDR DHL2006364005](https://openairdocs.org/sdr/DHL2006364005.md): Downlock Switch · dirty · Mar 30, 2006 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > RIGHT MLG RED UNSAFE LIGHT ILLUMINATED ON S/O PANEL ON GEAR EXTENSION. GEAR WARNING SOUNDED. PERFORMED ABNORMAL FORWARD PANEL INDICATED 3 GREEN. UNABLE TO DUPLICATE CONDITION. CLEANED DOWNLOCK SWITCH CONNECTOR AT RIGHT MLG, OPS CHECKED GOOD PER MM 32-61-00
- [SDR DHL2006364004](https://openairdocs.org/sdr/DHL2006364004.md): Throttle Cable · stiff · Mar 24, 2006 · N364DH · Airbus A300B4203 · Power Lever
  > AT FL350-MINUS 48C NR 1 THROTTLE VERY DIFFICULT TO MOVE. THROTTLE DOES NOT MOVE AT ALL IN AUTO THROTTLE. PERFORMED IN FLT ENG SHUT DOWN DUE TO JAMMED NR 1 THROTTLE. REMOVED AND REPLACED NR 1 ENG THROTTLE CABLE ASSY FROM PYLON AT PANEL 423DL TO MEC, C/W S/B
- [SDR DHL2006364003](https://openairdocs.org/sdr/DHL2006364003.md): Brake · overheated · Mar 16, 2006 · N364DH · Airbus A300B4203 · Landing Gear Brake System
  > RTO - BRAKES HOT LIGHT NR 1 BRAKE LIGHT ON S/O PANEL BRAKE TEMP MAX 420 WITH FANS ON BRAKE COOLED WHILE STOPPED AND ROSE TO 320 DURING TAXI IN. RTO=105 KIAS, 5 C AMBIENT, MODERATE BRAKING USED, 60' PRESSURE ALTITUDE. PLACED NR 1 BRAKE ON DMI 24688 AS PER MEL
- [SDR DHL2006364002](https://openairdocs.org/sdr/DHL2006364002.md): Slide · unknown · Jan 28, 2006 · N364DH · Airbus A300B4203 · Escape Slide
  > L1 DOOR WILL NOT MOVE TO THE OPEN AND LOCKED POSITION. TRANSF'D TO DMI 24185 PER MEL 52-61-01-2 CAT -C-. DEF: BY 8597. REF DMI 24185 L1 DOOR WILL NOT MOVE TO THE OPEN AND LOCKED POSITION. REMOVED AND REPLACED L1 MED ESCAPE SLIDE PER MM 25-61-12, OPS NORMA
- [SDR DHL2006364001](https://openairdocs.org/sdr/DHL2006364001.md): Fitting · loose · Jan 12, 2006 · N364DH · Airbus A300B4203 · Landing Gear Door Retract Section
  > WHEN LANDING GEAR RETRACTED AFTER TAKEOFF, THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED ON BOTH INDICATORS WITH GEAR HANDLE OFF VIBRATION WAS FELT WITH HANDLE UP, NO VIBRATION. FOUND LT NOSE GEAR DOOR LOCK FITTING LOOSE. SECURED FITTING, OPS CHECKED GOOD PE
- [SDR DHL2005364003](https://openairdocs.org/sdr/DHL2005364003.md): Selector Valve · inoperative · Oct 2, 2005 · N364DH · Airbus A300B4203 · Landing Gear Door Retract Section
  > ON THE GROUND DURING TAXI WHEN MAKING LARGE TURN REQUIRING MORE THAN 10 DEG TILLER. TILLER IS VERY DIFFICULT TO TURN; REQUIRES TWO HANDS. ALSO DURING THIS TIME, WHEN PRESSING THE RUDDER PEDALS, CAN FEEL A HIGH FREQUENCY VIBRATION IN RUDDER PEDALS. DURING LAND
- [SDR DHAL200536400](https://openairdocs.org/sdr/DHAL200536400.md): Roller · loose · Jul 28, 2005 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > ON DEPARTURE FROM CVG. NOSE GEAR DOORS LIGHT REMAINED ON. PERFORMED ABNORMAL PROCEDURE AND CONTINUED TO DESTINATION RII REQUIRED. FOUND RT NOSE GEAR DOOR UPLATCH ROLLER LOOSE AND OUT OF RIG. TIGHTENED AND ADJUSTED PER MM 32-22-11. OPS CK GOOD RII JLUTZ 33
- [SDR DHL2005364001](https://openairdocs.org/sdr/DHL2005364001.md): Frame · damaged · Apr 25, 2005 · N364DH · Airbus A300B4203 · Fuselage Main, Frame
  > FRAME 47 REPAIR RSA FROM AIRBUS IS INTERIM FOR 6 MONTH REF RAS/AS/0114/2004 MSI 05574. REPAIR DESIGN APPROVAL SHEET REF RAS/AS/0114/2004 ISSUE B DATE 12/10/04 INTERIM LIMIT NONE THIS CLEARS MSI 05574.
- [SDR DHL2004364018](https://openairdocs.org/sdr/DHL2004364018.md): Stringer · cracked · Dec 18, 2004 · N364DH · Airbus A300B4203 · Fuselage Main, Longeron/Stringer
  > DURING A-CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 4418 CRACK AT FR 21 STR 9R INTERNAL. REMOVED FASTENERS OUT OF DAMAGE AREA AS PER A-300 SRM 51-30-30. REMOVED DAMAGE AT FRAME 21 STR 9R AS PER A-300 SRM 53-10-10 (2 INCH
- [SDR DHL2004364017](https://openairdocs.org/sdr/DHL2004364017.md): Brake Assy · binding · Nov 19, 2004 · N364DH · Airbus A300B4203 · Landing Gear Brake System
  > EXCESSIVE BREAKAWAY THRUST REQUIRED TO MOVE AIRCRAFT NR 3 BRAKE ASSY, REMOVED. FOUND NR 3 BRAKE BOUND. REMOVED NR 3 BRAKE ASSY PER MM 32-00-00 AND 32-42-27 XFER TO DMI 18528 PER MEL 32-42-09-1, CAT C. NR 3B RAKE ASSY REMOVED. INSTALL SERVICEABLE BRAKE ASSY
- [SDR DHL2004364015](https://openairdocs.org/sdr/DHL2004364015.md): Proximity Sensor · malfunctioned · Oct 29, 2004 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > FRONT PANEL LEFT MAIN LANDING GEAR RED UNSAFE MOMENTARILY ILLUMINATED ON APP TO CVG. 2ND OFFICER LEFT MAIN LANDING GEAR INDICATED GREEN AT ALL TIMES WITH LANDING GEAR EXTENDED. PERFORMED OPS CHECK OF PROXIMITY DETECTOR MODULE UNIT IAW M/M 32-61-12, OPS GOOD
- [SDR DHL2004364016](https://openairdocs.org/sdr/DHL2004364016.md): Frame · corroded · Aug 24, 2004 · N364DH · Airbus A300B4203 · Fuselage Main, Frame
  > IN CONJUCTION WITH DHL2004364015, REMOVE & REPLACE DOUBLER AT FRA, 26 & LONGERON 43 LEFT. REMOVED FLOOR PANEL, SIDE WALL PANEL TO GAIN ACCESS TO REPAIR AT STR 43L, FR 26. REMOVED REPAIR DOUBLER AT STR 43L, FR 26, CUT-OUT UPPER SKIN AND BONDED DOUBLER IN AREA
- [SDR DHL3642004015](https://openairdocs.org/sdr/DHL3642004015.md): Skin · corroded · Aug 21, 2004 · N364DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > FUSELAGE LAP SEAM 44L HAS A BULGE AND A RIVET POPPED JUST AFT OF FR 26. OPEN ACCESS PANELS FOR SHEETMETAL REPAIR AREA FRAME 26 STRINGER 43. CUT OUT LONGERON 43 TO FRAME 26. CUT OUT INNER SKIN DAMAGED AREA, PERFORMED HFEC AT CUTOUT AREA, NO CRACK INDICATED.
- [SDR DHL2004364014](https://openairdocs.org/sdr/DHL2004364014.md): Landing Gear · slow · Aug 20, 2004 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > LT MAIN GEAR TOOK 15 SECONDS LONGER THAN OTHER GEAR TO EXTEND,TO LOCK.
- [SDR DHL2004364013](https://openairdocs.org/sdr/DHL2004364013.md): Proximity Sensor · malfunctioned · Aug 6, 2004 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > COULD NOT RAISE LANDING GEAR HANDLE ON SYSTEM 2. COMPLIED WITH ABNORMAL PROC. DID RAISE GEAR ON SYSTEM 1. PROBES ON MWP WAS CAPT PITOT LIGHT ON S/O PANEL. COMPLIED WITH ABNORMAL PROC. PERFORMED FIM 22.23.00. REMOVED AND REPLACED PROX DETECTOR. SYS TESTS
- [SDR DHL2004364012](https://openairdocs.org/sdr/DHL2004364012.md): Bulb · inoperative · Jul 10, 2004 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > NOSE GEAR INDICATOR ON PILOT'S LANDING GEAR PANEL DID NOT ILLUMINATE GREEN WHEN GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED THREE GREEN ON S/O PANEL. RELAMPED LANDING GEAR INDICATOR (P/N 3115) IAW M/M 33-13-00, OPS CHECKED GOOD.
- [SDR DHL2004364011](https://openairdocs.org/sdr/DHL2004364011.md): Lever · malfunctioned · Jul 9, 2004 · N364DH · Airbus A300B4203 · Escape Slide
  > EXIT DOOR 1R ESCAPE SLIDE DISARM LEVER DOES NOT REACH FULL DISARM POSITION. DEFERRED IAW MEL 52-61-01-2 DMI NR 17140 CAT (C) PLACARD INSTALLED.
- [SDR DHL2004364010](https://openairdocs.org/sdr/DHL2004364010.md): Landing Gear · malfunctioned · Jun 29, 2004 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > UNABLE TO RAISE THE LANDING GEAR HANDLE AFTER TAKEOFF. SYSTEM 1 INOPERATIVE. COMPLIED WITH ABNORMAL PROCEDURES. DEFERRED NR 1 LEVER LOCK AND WARNING SYSTEM IAW MEL 32-31-02A, DMI NR 17050 PLACARD INSTALLED, SYS NR 2, OPS NORMAL.
- [SDR DHL2004364009](https://openairdocs.org/sdr/DHL2004364009.md): Girt Bar · dirty · Jun 11, 2004 · N364DH · Airbus A300B4203 · Escape Slide
  > UNABLE TO DISARM R-1 DOOR. REMOVED DIRT FROM GIRT BAR. OPS CHECK GOOD IAW 52-10-00. NO PARTS REPLACED.
- [SDR DHL2004364008](https://openairdocs.org/sdr/DHL2004364008.md): Proximity Sensor · failed · Jun 4, 2004 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. COMPLETED ABNORMAL PROCEDURE AND GEAR HANDLE OPERATED NORMALLY. SWITCHED TO SYSTEM 1. PERFORMED OPS CHECK OF GEAR PROXIMITY UNIT REVEALED FAULT AT B12; SLAVED IN NLG SENSOR, NO HELP. RESTORED ORIGINAL.
- [SDR DHL2004364007](https://openairdocs.org/sdr/DHL2004364007.md): Proximity Sensor · faulty · Jun 3, 2004 · N364DH · Airbus A300B4203 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION GEAR WOULDN'T RAISE. LANDING GEAR HANDLE CANNOT BE RAISED. COMPLETED ABNORMAL, GEAR RAISED NORMALLY. LANDING GEAR LEVER LOCK WAS IN POSITION NR 1 TO BEGIN. REPLACED PROXIMITY BOX IAW M/M 32-61-12. OPS CHECKED GOOD AT THIS TIME.
- [SDR DHL2004364006](https://openairdocs.org/sdr/DHL2004364006.md): Fire Loop · faulty · Jun 2, 2004 · N364DH · Airbus A300B4203 · Fire Detection
  > ON CLIMBOUT ENGINE NR 2 LOOP-A LIGHT ILLUMINATED WITH SINGLE STROKE CHIME (SSC) ON MASTER WARNING PANEL (MWP). RAN ABNORMAL PROCEDURE AND TEST WAS SUCCESSFUL. DEFERRED NR 2 ENGINE A-LOOP AS PER MEL 26-12-01-1 CAT-B. ASSIGNED DMI 16774 PLACARD PANEL. REMOVE
- [SDR DHL2004364005](https://openairdocs.org/sdr/DHL2004364005.md): Fire Loop · malfunctioned · May 30, 2004 · N364DH · Airbus A300B4203 · Fire Detection
  > LOOPS-A ON ENGINE NR 2 ILLUMINATED ON S/O'S PANEL WITH LOOPS LIGHT ON MASTER WARNING PANEL (MWP) ILLUMINATED WITH A CHIME. COMPLETED ABNORMAL PROCEDURES. LOOP-B TESTS OK. DEFERRED A-LOOP ON NR 2 ENGINE IAW MEL 26-12-01, CAT-B, DMI 16753. PLACARDS INSTALLED

Next page: https://openairdocs.org/deregistered/N364DH-2017-05-16/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 = 'N364DH' AND deregistration_id = 'N364DH-2017-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N364DH-2017-05-16/reports

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