# N77215: Boeing 737-130, registration cancelled 1998-03-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 11, 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: 19032 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 8, 1989 - Last registry action: November 20, 1996 - Mode S code: AA730E - 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/N77215 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=77215 - Page: https://openairdocs.org/deregistered/N77215-1998-03-11 From the FAA registry file of October 31, 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 (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9701432](https://openairdocs.org/sdr/CALA9701432), Oct 11, 1997: SLIDE. LOW PRESSURE. L-1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH MM 25-61-311. - [SDR CALA9700860](https://openairdocs.org/sdr/CALA9700860), May 20, 1997: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 360, STRINGER 17L. THE DENTED SECTION OF SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 28 AND ECRA 5330-0 - [SDR CALA9601542](https://openairdocs.org/sdr/CALA9601542), Oct 31, 1996: HYD LINE. LEAKING. THE A-HYDRAULIC SYSTEM QUANTITY GRADUALLY DECREASED TO 1 GALLON WHILE EN ROUTE. THE A-SYSTEM HYDRAULIC PUMPS WERE TURNED OFF. WHEN THE PUMPS WERE TURNED ON TO L - [SDR CALA9601447](https://openairdocs.org/sdr/CALA9601447), Oct 12, 1996: LINE. LEAKING. LOSS OF A-SYSTEM HYDRAULICS. FOUND PRESSURE LINE FROM NR 2 ENGINE LEAKING. REPLACED LINE AND BOTH ENGINE DRIVEN AND ELECTRIC HYDRAULIC PUMPS AND REPLACED ALL FI - [SDR CALA9601325](https://openairdocs.org/sdr/CALA9601325), Sep 23, 1996: AIR DIST FAN. INOPERATIVE. A STRONG ELECTRICAL ODOR WAS SMELLED IN THE COCKPIT AFTER TAKEOFF. THE FLIGHT ATTENDANT'S REPORTED SMOKE IN THE AFT/MID CABIN. THE AIR DISTRIBUTION FAN WAS TURN - [SDR CALA960491](https://openairdocs.org/sdr/CALA960491), Apr 15, 1996: BATTERY. DISCHARGED. GSO - THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE RIGHT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHT - [SDR CAL960492](https://openairdocs.org/sdr/CAL960492), Apr 15, 1996: BATTERY. DISCHARGED. GSO - THE LEFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE LEFT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS - [SDR CAL960485](https://openairdocs.org/sdr/CAL960485), Mar 27, 1996: CHORD. CRACKED. GSO - INSPECTION FOUND LT OUTBOARD CHORD CRACKED PAST SECOND FASTENER HOLE AT STA 727. THE CHORD SEGMENT WAS REMOVED AND RPELACED IAW BOEING DRAWING 65C33722. ( - [SDR CAL960484](https://openairdocs.org/sdr/CAL960484), Mar 25, 1996: FLOOR BEAM. CRACKED. GSO - INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FLOOR BEAM LOWER T-CHORD AT BBL ZERO, STA 675. THE FLOOR BEAM CHORD WAS REPAIRED IAW ECRA 5710-01462 AND BOEI - [SDR CAL960483](https://openairdocs.org/sdr/CAL960483), Mar 25, 1996: SKIN. DELAMINATED. GSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR W - [SDR CAL960487](https://openairdocs.org/sdr/CAL960487), Mar 23, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 259 TO STA 306, STR 24L TO STR 27L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A NEW SECTION OF SKIN AND DOU - [SDR CAL960486](https://openairdocs.org/sdr/CAL960486), Mar 23, 1996: STRINGER. CORRODED. GSO - INSPECTION FOUND STR 21R AND SKIN PANEL CORRODED AT STA 294.5. THE STRINGER AND SKIN PANEL WERE REMOVED. A NEW STRINGER, SKIN SECTION, AND DOUBLERS WERE F - [SDR CAL960489](https://openairdocs.org/sdr/CAL960489), Mar 21, 1996: SKIN. DELAMINATED. GSO - INSPECTION FOUND UPPER AFT TRAILING EDGE SECTION OF RUDDER DELAMINATING. THE LENGTH OF DELAMINATION WAS APPROXIMATELY 12 INCHES. THE DELAMINATED SECTION O - [SDR CAL960488](https://openairdocs.org/sdr/CAL960488), Mar 21, 1996: CHORD. CORRODED. GSO - INSPECTION FOUND LOWER CHORD CORRODED AT LEFT AND RIGHT ENDS ON UPPER AND LOWER SURFACES OF HORIZONTAL FLANGE, STA 294.5. THE CORRODED CHORD SEGMENT WAS R - [SDR CAL960482](https://openairdocs.org/sdr/CAL960482), Mar 21, 1996: SKIN. CRACKED. GSO - INSPECTION FOUND A 0.3 INCH CRACK IN RT WING LEADING EDGE SKIN ON OUTBOARD EDGE OF OUTBOARD SLAT TRACK CUT-OUT, WBL 304. THE CRACK WAS ROUTED OUT IAW ECRA - [SDR CAL960481](https://openairdocs.org/sdr/CAL960481), Mar 21, 1996: ANGLE. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESSURE PANEL AT BS 663.75. BOTH ANGLES WERE - [SDR CAL960480](https://openairdocs.org/sdr/CAL960480), Mar 4, 1996: SKIN. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT NR 2 SLAT AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER RE - [SDR CAL960490](https://openairdocs.org/sdr/CAL960490), Mar 3, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME. THE CRACK LENGTH WAS NOT IDENTIFIED. TH - [SDR CAL960152](https://openairdocs.org/sdr/CAL960152), Feb 14, 1996: HYD LINE. LEAKING. FLT NR 1446 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN - [SDR CAL950519](https://openairdocs.org/sdr/CAL950519), Jun 5, 1995: T-ANGLE. CORRODED. 31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING - [SDR CAL950518](https://openairdocs.org/sdr/CAL950518), Jun 1, 1995: PRESSURE PANEL. CORRODED. 31J - THE NOSE WHEEL WELL PRESSURE BULKHEAD WAS FOUND WITH A CORROSION BULGE 1 INCH IN DIAMETER, AT THE AFT FORWARD OUTBOARD CORNER OF THE LEFT ACCESS PANEL BET - [SDR CAL950241](https://openairdocs.org/sdr/CAL950241), Mar 30, 1995: HYDRAULIC LINE. CHAFED. EWR - FLT 1204 - THE B-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE TO EWR. THE A-SYSTEM QUANTITY GAUGE DECREASED TO ONE GALLON. THE AIRCRAFT LANDED AT EWR ## 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 19920610026509I](https://openairdocs.org/incident/19920610026509I), Jun 10, 1992: Boeing 737130 (N77215), Covington - Cin, OH. Lost a system hydraulic quanity on climb. Returned. Landed safely. Replaced left MLG uplock hydraulic line. ## Other aircraft with N77215 - [Cancelled 2007-07-12](https://openairdocs.org/deregistered/N77215-2007-07-12): Cessna 525, S/N 525-0149, built 1996. Owner: [Moonchild Aviation LLC](https://openairdocs.org/faa-owner/MOONCHILD%20AVIATION%20LLC), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) - [Cancelled 1951-01-26](https://openairdocs.org/deregistered/N77215-1951-01-26): Cessna 140, S/N 11677, built 1946. Owner: [Miami Valley Flying Service](https://openairdocs.org/faa-owner/MIAMI%20VALLEY%20FLYING%20SERVICE), [Dayton 9, OH](https://openairdocs.org/faa-place/OH/Dayton%209) --- 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.