# N44214: Boeing 737-130, registration cancelled 1998-02-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 18, 1998 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-130](https://openairdocs.org/model/boeing-737-130) (registry code 1384435) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19031 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 8, 1989 - Last registry action: November 20, 1996 - Mode S code: A554A3 - Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7533° N, 95.4129° W: Placed by OpenAirDocs at the center of ZIP code 77019, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N44214 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=44214 - Page: https://openairdocs.org/deregistered/N44214-1998-02-18 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-130: https://openairdocs.org/model/boeing-737-130.md ## Service difficulty reports (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9701680](https://openairdocs.org/sdr/CALA9701680), Nov 26, 1997: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. - [SDR CALA9701355](https://openairdocs.org/sdr/CALA9701355), Sep 12, 1997: HYD LINE. RUPTURED. THE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ILLUMINATION OF A PUMP LOW PRESSURE LIGHTS. THE A-SYSTEM HYDRAULIC FAILURE CHECKLIST WAS COMPL - [SDR CALA9701250](https://openairdocs.org/sdr/CALA9701250), Aug 28, 1997: STUD. FAILED. THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE ENROUTE FROM CAE TO EWR. THE ENG WAS SHUTDOWN AND T - [SDR CALA9701223](https://openairdocs.org/sdr/CALA9701223), Aug 15, 1997: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHT WHILE AT CRUISE. THE AIRCRAFT WAS RETURNED TO EWR WHERE - [SDR CALA9700843](https://openairdocs.org/sdr/CALA9700843), Jun 6, 1997: HYDRAULIC LINE. CHAFED. THE A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO NEAR ZERO WHILE EN ROUTE. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT AT - [SDR CALA9700071](https://openairdocs.org/sdr/CALA9700071), Jan 20, 1997: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS FLICKERED AND THE A-SYSTEM HYRDAULIC QUANTITY GAUGE READ ZERO ON APPROACH PRIOR TO GEAR AND FLAP EXTENSION. THE HYDRA - [SDR CALA9601911](https://openairdocs.org/sdr/CALA9601911), Dec 30, 1996: HYDRAULIC LINE. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SU - [SDR CALA9601876](https://openairdocs.org/sdr/CALA9601876), Dec 24, 1996: HYD LINE. LEAKING. THE A HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT INTO EWR. THE A SYSTEM PUMPS WERE TURNED OFF AND THE HYDRAULIC LOSS CHECKLIST WAS ACCOMP - [SDR CALA9601603](https://openairdocs.org/sdr/CALA9601603), Nov 4, 1996: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF C-2 DOOR AFT CUTOUT. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLERS WERE INSTALLED IAW ECRA 5330-02 - [SDR CALA9601561](https://openairdocs.org/sdr/CALA9601561), Nov 1, 1996: BULKHEAD SKIN. CRACKED. INSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM - [SDR CALA9601560](https://openairdocs.org/sdr/CALA9601560), Nov 1, 1996: SHEAR WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INBOARD RADIUS OF SHEAR WEB AT S18A, LT B.S. 664. NEW REPAIR ANGLES WERE INSTALLED IAW BOEING DRAWING NR 65C29228 AND SRM 51- - [SDR CALA9601555](https://openairdocs.org/sdr/CALA9601555), Oct 31, 1996: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INBOARD SKIN AT LOWER AFT CORNER OF C-2 DOOR CUTOUT. THE CRACKED SECTION OF SKIN WAS REMOVED. A DOUBLER AND TRIPLER REPAIR WA - [SDR CALA9601554](https://openairdocs.org/sdr/CALA9601554), Oct 31, 1996: BULKHEAD SKIN. CRACKED. INSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DO - [SDR CALA9601553](https://openairdocs.org/sdr/CALA9601553), Oct 31, 1996: BULKHEAD SKIN. CRACKED. INSPECTION FOUND A .50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFENER AT WL 218, RT SIDE. THE CRACKED AREA - [SDR CALA9601556](https://openairdocs.org/sdr/CALA9601556), Oct 30, 1996: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE AT LOWER AFT CORNER OF LT STA 520 WING TO BODY ATTACH FRAME. THE FASTENERS AND EXISTING ANGLE WERE REMOVED - [SDR CAL960560](https://openairdocs.org/sdr/CAL960560), May 6, 1996: HYDRAULIC LINE. CHAFED. EWR - FLT 0674 - THE B-HYDRAULIC SYSTEM LOW QUANTITY ILLUMINATED ON APPROACH TO DWR. THE 'A' AND 'B' SYSTEMS REMAINED AT 3,000 PSI WITH 2 GALLONS QUANTITY. THE - [SDR CAL960386](https://openairdocs.org/sdr/CAL960386), Mar 24, 1996: HYD LINE. LEAKING. BUF - FLT 1420 - AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM EWR TO BUF. THE AIRCRAFT LANDED IN BUF WITHOUT INCIDENT. MAINTENANCE FOUND THE HY - [SDR CAL960185](https://openairdocs.org/sdr/CAL960185), Feb 22, 1996: HYD LINE. CHAFED. FLT NR 1036 - GSO - THE 'A' HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM BNA TO EWR. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRA - [SDR CAL960067](https://openairdocs.org/sdr/CAL960067), Jan 30, 1996: HYD LINE. LEAKING. FLT NR 1069 - TPA - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE IN FLIGHT WITH THE QUANTITY GAUGE INDICATING ZERO. THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAIN - [SDR CAL960062](https://openairdocs.org/sdr/CAL960062), Jan 24, 1996: HYD LINE. CHAFED. FLT NR 1069 - TPA - AIRCRAFT LOST THE 'A' SYSTEM HYDRAULICS WHILE EN ROUTE FROM GSO TO TPA. QRH CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED A - [SDR CAL951157](https://openairdocs.org/sdr/CAL951157), Dec 15, 1995: TEE CHORD. CRACKED. GSO - INSPECTION FOUND A 2 INCH CRACK IN TEE CHORD AT STA 685, BL ZERO. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5710-01 - [SDR CAL950440](https://openairdocs.org/sdr/CAL950440), May 11, 1995: LAP SEAM. CORRODED. 31J - INSPECTION FOUND CORROSION IN THE LAP SEAM AT BS 420, STR 27R. THE CORRODED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IA - [SDR CAL950437](https://openairdocs.org/sdr/CAL950437), May 9, 1995: FITTING. CRACKED. 31J - INSPECTION FOUND A .3750 INCH CRACK IN THE RT BS 695 FRAME AFT LOWER FITTING AT THE OUTBOARD FASTENERS IN THE AFT HORIZONTAL FLANGE. THE CRACK WAS STOP DR - [SDR CAL950439](https://openairdocs.org/sdr/CAL950439), May 8, 1995: SHEAR BEAM. CRACKED. 3LJ - A .3750 INCH CRACK WAS FOUND IN THE RADIUS OF THE INBOARD FLANGE AT THE FORWARD END OF THE LT S18A SHEAR BEAM, AFT SIDE OF BS 664 BULKHEAD. THE CRACK WAS - [SDR CAL950438](https://openairdocs.org/sdr/CAL950438), May 8, 1995: FRAME. CRACKED. 31J - A 1 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF THE L-2 DOOR FRAME. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5210-01224. (X) - [SDR CAL950101](https://openairdocs.org/sdr/CAL950101), Feb 8, 1995: BATTERY CHARGER. INOPERATIVE. TPA - FLT 1790 - THE FLIGHT ATTENDANT REPORTED A SMOKY ODOR IN CABIN DURING CLIMB-OUT. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE ODOR SUBSIDED. THE - [SDR CAL950001](https://openairdocs.org/sdr/CAL950001), Jan 1, 1995: HYD LINE. CHAFED. FLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19960323007599I](https://openairdocs.org/incident/19960323007599I), Mar 23, 1996: Boeing 737100 (N44214), Buffalo, NY. Narrative: flight 1420 departed ewr at 20:35 enroute to buf while cruising at 23,000 MSL the "a" hydraulic system lost all hydraulic fluid quantity. Aircrft… ## Other aircraft with N44214 - [Registered now](https://openairdocs.org/aircraft/N44214): Infinity 2004, S/N IPP4247, built 2004 - [Cancelled 1965-09-13](https://openairdocs.org/deregistered/N44214-1965-09-13): Taylorcraft BC12-D1, S/N 10014. Owner: [Johnston Kruger E](https://openairdocs.org/faa-owner/JOHNSTON%20KRUGER%20E), [Savannah, GA](https://openairdocs.org/faa-place/GA/Savannah) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N44214-undated): Creamer Hector CGS HAWK B, S/N 1 --- 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.