# Service difficulty reports: N920HA, cancelled Jul 24, 2003 A list on [N920HA, cancelled Jul 24, 2003](https://openairdocs.org/deregistered/N920HA-2003-07-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HNAA0000063](https://openairdocs.org/sdr/HNAA0000063.md): Battery Pack · discharged · Aug 17, 2000 · N920HA · Dhav DHC8102 · Emergency Lighting > FOUND MULTIPLE EMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHTS BATTERY PACKS 3351-PS1, 3351-PS2 AND 3351-PS4 DISCHARGED. REPLACED BATTERY PACKS. - [SDR HNAA0000048](https://openairdocs.org/sdr/HNAA0000048.md): Strut · broken · Jun 11, 2000 · N920HA · Dhav DHC8102 · Passenger/Crew Doors > PASSENGER DOOR WOULD NOT OPEN. FOUND THE FWD UPPER DOOR SUPPORT STRUT BROKEN. REPLACED FWD UPPER SUPPORT STRUT. - [SDR HNAA0000036](https://openairdocs.org/sdr/HNAA0000036.md): Sensor · out of adj · Apr 30, 2000 · N920HA · Dhav DHC8102 · Door Warning System > THE PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. FOUND THE DOOR PROXIMITY SENSOR GAP WAS TOO WIDE WITH THE AIRCRAFT PRESSURIZED. ADJUSTED DOOR PROXIMITY SENSOR GAP. - [SDR HNAA9900031](https://openairdocs.org/sdr/HNAA9900031.md): Seat Track · corroded · Feb 19, 1999 · N920HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings > LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REPLACED SEAT TRACK. - [SDR HNAA9900022](https://openairdocs.org/sdr/HNAA9900022.md): Structure · corroded · Jan 30, 1999 · N920HA · Dhav DHC8102 · Fuselage Main, Structure > CORROSION RIGHT FUSELAGE ON STRINGER SPLICE AT STR 32S FRAME 488, SPLICE ON STR 29 AND AT FRAME 488, FRAME 433 LEG AT ST 31S, STR 29.021 DEEP AT FRAME 529, SURFACE.006 DEEP ON SPLICE STR 28 AT FRAME 488, 7 AREAS RADIUS OF STR 31 MAX.013 DEEP BETWEEN FRAMES - [SDR HNAA9900017](https://openairdocs.org/sdr/HNAA9900017.md): Tab · broken · Jan 23, 1999 · N920HA · Dhav DHC8102 · Passenger/Crew Doors > LOWER AFT CORNER OF PASSENGER DOOR ENTRANCE COMBING HAS TAB BROKEN OFF. REPAIRED AS NECESSARY. - [SDR HNAA9900015](https://openairdocs.org/sdr/HNAA9900015.md): Skin · chafed · Jan 15, 1999 · N920HA · Dhav DHC8102 · Trailing Edge Flaps > RIGHT HAND WING OUTBOARD FLAP INBOARD UPPER SKIN HAS CHAFE, DEPTH IS.009 LENGTH AND WIDTH.3 BY.3 LOCATED 2.5 INCHES FROM INBOARD EDGE. REPAIRED AS NECESSARY. - [SDR HNAA9900014](https://openairdocs.org/sdr/HNAA9900014.md): Bracket · cracked · Jan 15, 1999 · N920HA · Dhav DHC8102 · Aileron Tabs > RIGHT HAND AILERON TRIM TAB ATTACH BRACKET CRACKED APPROXIMATELY 1 INCH RADIUS ON AFT SIDE FORWARD. REPLACED BRACKET. - [SDR HNAA9900013](https://openairdocs.org/sdr/HNAA9900013.md): Conduit · damaged · Jan 15, 1999 · N920HA · Dhav DHC8102 · Electrical Power System > RIGHT WING WIRE CONDUIT RIPPED OPEN AND BRACKET DAMAGED AT NR 4 FLAP JACKSCREW LOCATION. REPAIRED AS NECESSARY. - [SDR HNAA9900005](https://openairdocs.org/sdr/HNAA9900005.md): Boots · malfunctioned · Jan 8, 1999 · N920HA · Dhav DHC8102 · Airfoil Anti/De-ice System > EN ROUTE MULTIPLE DEICE BOOTS DID NOT INFLATE IN FREEZING CONDITIONS. CHECKED ALL BOOTS WITH SHOP AIR IN MANUAL AND AUTO MODE. REMOVED AND REINSTALLED DRAIN PLUGS WITH NO WATER FOUND OR ANY OTHER DISCREPANCIES. - [SDR HNAA9892064](https://openairdocs.org/sdr/HNAA9892064.md): Cover · corroded · Oct 10, 1998 · N920HA · Dhav DHC8102 · Wing, Plate/Skin > SBY - DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING MIDDLE FUEL TANK LID THAT WAS MAINTENANCE MANUAL LIMITS. REPAIRED IAW PIEDMONT AIRLINES E08-57-98-1033. (M) - [SDR HNAA9892063](https://openairdocs.org/sdr/HNAA9892063.md): Cover · corroded · Oct 10, 1998 · N920HA · Dhav DHC8102 · Wing, Plate/Skin > SBY - DURING C-CHECK INSPECTION, THE RIGHT WING MIDDLE FUEL CELL COVER PLATE WAS FOUND TO BE CORRODED BEYOND MAINTENANCE MANUAL LIMITS. REPAIRED THE COVER IAW PIEDMONT AIRLINES E08-57-98-1033. (M) - [SDR HNAA9892061](https://openairdocs.org/sdr/HNAA9892061.md): Plate · corroded · Oct 10, 1998 · N920HA · Dhav DHC8102 · Wing, Plate/Skin > SBY - DURING C-CHECK INSPECTION, FOUND CORROSION PITS WERE FOUND IN THE FUEL CELL LID AND LADDER PLATE ON THE OUTBOARD END. REPAIRED IAW PIEDMONT AIRLINES E08-57-98-1033. (M) - [SDR HNAA9892057](https://openairdocs.org/sdr/HNAA9892057.md): Valve · failed · Sep 16, 1998 · N920HA · Dhav DHC8102 · Landing Gear Retraction/Extension System > CLT/HHH - FLT 3160 - LOST HYDRAULIC QUANTITY AND PRESSURE AFTER LANDING GEAR EXTENSION. DIVERTED TO SAV. REMOVED AND REPLACED SOLENOID SEQUENCE VALVE FOR NOSE GEAR. SERVICED AND BLED NR 2 HYDRAULIC SYSTEM. OPS AND LEAK CHECK GOOD. (X) - [SDR HNAA9892044](https://openairdocs.org/sdr/HNAA9892044.md): Valve · failed · Sep 2, 1998 · N920HA · Dhav DHC8102 · Landing Gear Retraction/Extension System > FLT 3470 - CLT-CHA - UPON GEAR UP SELECTION AFTER TAKEOFF, 3 RED UNSAFE LIGHTS ILLUMINATED AND GEAR DID NOT MOVE. SELECTED GEAR DOWN AND 3 GEAR DOWN/LOCKED LIGHTS ON. RETURNED TO CLT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE, OPS CHECK GOOD. (M) - [SDR HNAA9792025](https://openairdocs.org/sdr/HNAA9792025.md): Wire · failed · Feb 23, 1997 · N920HA · Dhav DHC8102 · Ice/Rain Protection System Wiring > FLT 3030 - PHL-DCA - AFTER TAKEOFF, SMELLED SMOKE AND NOTICED SMOKE COMING FROM CAPTAINS WINDSHIELD HEAT TERMINALS. TURNED WINDSHIELD HEAT OFF AND RETURNED TO PHL WITHOUT INCIDENT. CHECKED RESISTANCE OF WINDSHIELD, CLEANED LEAD AND REMOVED AND REPLACED WIRE - [SDR HNAA9692011](https://openairdocs.org/sdr/HNAA9692011.md): Battery Pack · discharged · Feb 13, 1996 · N920HA · Dhav DHC8102 · Emergency Lighting > PHF/DCA - FLT 3091 - DURING PREFLIGHT WALK-AROUND, FOUND LEFT AND RIGHT UNDERWING INTERIOR AND EXTERIOR EEL LIGHTS INOPERATIVE. REMOVED AND REPLACED PS3 AND PS6 BATTERY PACKS. (X) - [SDR 95ZZZW675](https://openairdocs.org/sdr/95ZZZW675.md): Fuel Filter · failed · Apr 20, 1995 · N920HA · Dhav DHC8102 · Engine Fuel Distribution > FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 HIGT PRESSURE FUEL FILTER BYPASS PRESSURE SWITCH AND HIGHT AND LOW PRESSURE FU - [SDR 95ZZZW674](https://openairdocs.org/sdr/95ZZZW674.md): Switch · failed · Apr 20, 1995 · N920HA · Dhav DHC8102 · Engine Fuel Distribution > FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 HIGT PRESSURE FUEL FILTER BYPASS PRESSURE SWITCH AND HIGH AND LOW PRESSURE FUE - [SDR 95ZZZW555](https://openairdocs.org/sdr/95ZZZW555.md): Actuator · failed · Apr 1, 1995 · N920HA · Dhav DHC8102 · Landing Gear Door Actuator > FLT 3465 - MIA-MCO - AFTER TAKEOFF AND AFTER GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR FAILED TO CLOSE. AIRCRAFT TURNED BACK AND LANDED IN MIA WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT FORWARD GEAR DOOR ACTUATOR. (W) - [SDR 95ZZZW554](https://openairdocs.org/sdr/95ZZZW554.md): Retract Mech · malfunctioned · Mar 30, 1995 · N920HA · Dhav DHC8102 · Landing Gear Door Retract Section > FLT NR 3442 - TPA-JAX - AFTER TAKEOFF AND DURING GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR AMBER ADVISORY LIGHT ILLUMINATED. VISUAL INSPECTION CONFIRMED THE RIGHT MAIN GEAR FORWARD DOOR WAS OPEN. AIRCRAFT LANDED IN JAX WITHOUT INCIDENT. REGAPPED FORWARD DOOR ## 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 = 'N920HA' AND deregistration_id = 'N920HA-2003-07-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N920HA-2003-07-24/reports --- 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.