# N77204: Boeing 737-130, registration cancelled 1999-03-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 17, 1999
- 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: 19021
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 8, 1989
- Last registry action: October 19, 1999
- Mode S code: AA72EA
- 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/N77204
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=77204
- Page: https://openairdocs.org/deregistered/N77204-1999-03-17

From the FAA registry file of November 5, 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 (26)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA9801859](https://openairdocs.org/sdr/CALA9801859), Sep 25, 1998: ACTUATOR. INOPERATIVE. THE GEAR HANDLE WAS PLACED IN THE OFF POSITION AFTER TAKEOFF AND THE NOSE GEAR CAME DOWN. THE GEAR HANDLE WAS PLACED UP AND THE NOSE GEAR RAISED. THE GEAR HANDL
- [SDR CALA9801589](https://openairdocs.org/sdr/CALA9801589), Aug 31, 1998: BULB. FAILED. NO NOSE GEAR INDICATION WAS RECEIVED WHEN GEAR WAS EXTENDED ON APPROACH. A GO-AROUND WAS INITIATED AND THE NOSE GEAR LIGHTS DID NOT TEST. THE NOSE GEAR INDICATO
- [SDR CALA9801498](https://openairdocs.org/sdr/CALA9801498), Aug 23, 1998: HYD PUMP. LEAKING. THE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST F
- [SDR CALA9801052](https://openairdocs.org/sdr/CALA9801052), Jun 12, 1998: SOCKET. CORRODED. INSPECTION FOUND AFT EXTERIOR EXIT SLIDES INOPERATIVE BOTH SIDES. THE RIGHT EXTERIOR SLIDE LIGHT SOCKET WAS CORRODED. THE SOCKET WAS REPLACED. IN ADDITION, BATT
- [SDR CALA9701234](https://openairdocs.org/sdr/CALA9701234), Aug 23, 1997: DNLOCK ACTUATOR. INOPERATIVE. THE LANDING GEAR WAS EXTREMELY STIFF DURING RETRACTION FROM UP TO OFF WITH NO NOTICEABLE DETENT AT OFF. THE NOSE GEAR EXTENDED APPROXIMATELY 12 TO 15 SECONDS AF
- [SDR CALA9700608](https://openairdocs.org/sdr/CALA9700608), Apr 23, 1997: LINE. CHAFED. LOST A-SYSTEM HYDRAULICS IN FLIGHT. REPLACED NUMBER 2 ENGINE HYDRAULIC SUPPLY LINE AT RIGHT WING ROOT.
- [SDR CALA9700299](https://openairdocs.org/sdr/CALA9700299), Mar 2, 1997: THERMO VALVE. INOPERATIVE. THE RT PACKED TRIPPED AT 6,000 FEET LEAVING EWR AND SMOKE BEGAN TO ENTER THE CABIN. SHORTLY AFTERWARDS THE BLEED TRIPPED. THE AIRCRAFT WAS RETURNED TO EWR WHERE
- [SDR CALA9700046](https://openairdocs.org/sdr/CALA9700046), Dec 31, 1996: STIFFENER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT WING VERTICAL STIFFENER AT STRINGER 13R. THE STIFFENER WAS REPAIRED IAW ECRA 5710-01773 AND IN REFERENCE TO BOEING DRAWING
- [SDR CALA9700049](https://openairdocs.org/sdr/CALA9700049), Dec 17, 1996: SPAR. TORN. INSPECTION FOUND A 3 BY .375 INCH TEAR IN LOWER FLANGE OF LT HORIZONTAL STABILIZER FORWARD LEADING EDGE SPAR. THE TEAR WAS LOCATED THREE FEET FROM OUTBOARD EDGE
- [SDR CALA9700047](https://openairdocs.org/sdr/CALA9700047), Dec 17, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BL 0 TO RBL 55. A FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-10-3.
- [SDR CALA9700050](https://openairdocs.org/sdr/CALA9700050), Dec 10, 1996: SUPPORT. CORRODED. INSPECTION FOUND CENTER FLOORBEAM SUPPORT CORRODED UNDER PANEL NR 8 BETWEEN STA 312 AND 328. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2.
- [SDR CALA9700048](https://openairdocs.org/sdr/CALA9700048), Dec 10, 1996: SKIN. CRACKED. INSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SR
- [SDR CALA9700051](https://openairdocs.org/sdr/CALA9700051), Dec 7, 1996: SKIN. CORRODED. INSPECTION FOUND LT WING ROOT LOWER SKIN PANEL CORRODED. THE SKIN WAS REPAIRED IAW ECRA 5730-01471.
- [SDR CALA9601601](https://openairdocs.org/sdr/CALA9601601), Nov 9, 1996: HYD LINE. BROKEN. THE A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHEN GEAR WAS LOWERED ON FINAL APPROACH TO CLE. THE FLAPS WERE LOWERED TO 15 DEGREES ELECTRICALLY A
- [SDR CALA9601136](https://openairdocs.org/sdr/CALA9601136), Aug 7, 1996: FIRELOOP. MALFUNCTIONED. THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB OUT OF EWR. BOTH FIRE BOTTLES WERE DISCHARGED, THE NR 1 ENGINE WAS SHUTDOWN, AND AIRCRAFT WAS
- [SDR CALA9600827](https://openairdocs.org/sdr/CALA9600827), Jun 16, 1996: HYD LINE. CHAFED. THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LAN
- [SDR CAL950980](https://openairdocs.org/sdr/CAL950980), Oct 27, 1995: ACTUATOR. INOPERATIVE. FLT NR 1598 - GSO - THE NR 4 SLAT WOULD NOT RETRACT DURING CLIMB-OUT OF GSO, THE AIRCRAFT WAS RETURNED TO GSO. MAINTENANCE FOUND THE NR 4 LEADING EDGE SLAT ACTU
- [SDR CAL950873](https://openairdocs.org/sdr/CAL950873), Sep 18, 1995: TRACK. CRACKED. EWR - INSPECTION FOUND A .25 INCH CRACK IN LT OUTBOARD TRAILING EDGE FLAP TRACK. THE CRACKED AREA WAS REPAIRED IAW ECRA 5750-02364. (X)
- [SDR CAL950261](https://openairdocs.org/sdr/CAL950261), Apr 1, 1995: INTERCOSTAL. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLE
- [SDR CAL950260](https://openairdocs.org/sdr/CAL950260), Apr 1, 1995: ANGLE. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN FRAME TO STRINGER ATTACH ANGLE AT STR 26R, STA 333. THE CRACKED ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND 
- [SDR CAL950259](https://openairdocs.org/sdr/CAL950259), Apr 1, 1995: STRINGER. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN STR 28R, LOCATED IN THE FORWARD PIT AT STA 420 - STA 440. THE DAMAGED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WER
- [SDR CAL950258](https://openairdocs.org/sdr/CAL950258), Apr 1, 1995: STRINGER. CORRODED. GSO - INSPECTION FOUND CORROSION ON STR 27R AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)
- [SDR CAL950257](https://openairdocs.org/sdr/CAL950257), Apr 1, 1995: ANGLE. CORRODED. GSO - INSPECTION FOUND CORROSION INSIDE WEB OF DOOR SILL ANGLE AND NUT PLATES AT STA 440, STR 25R. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND SRM 51-1-21A. (
- [SDR CAL950256](https://openairdocs.org/sdr/CAL950256), Apr 1, 1995: WEB. CORRODED. GSO - NOSE WHEELWELL, LEFT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION ON UPPER SURFACE AND INSIDE FASTENER HOLES. AN INTECOSTAL W
- [SDR CAL950255](https://openairdocs.org/sdr/CAL950255), Apr 1, 1995: WEB. CORRODED. GSO - THE NOSE WHEELWELL, RT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION INSIDE FASTENER HOLE. AN INTERCOSTAL WAS FABRICATED AND I
- [SDR CAL950254](https://openairdocs.org/sdr/CAL950254), Apr 1, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND CRACK INDICATIONS IN SKIN AT LEFT FS BS 188-253, WL 208.1 TO WL 234.35. THE CRACKS WERE APPROXIMATELY .50 INCH LONG. THE CRACKED AREAS OF

## FAA accident and incident reports (4)

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 19971001045039I](https://openairdocs.org/incident/19971001045039I), Oct 1, 1997: Boeing 737130 (N77204), Newark, NJ. Moving 737 from hangar to gate crossed a hold line sans a clearance. An airecraft had to go around mechanic pilot.
- [Incident 19961109040409I](https://openairdocs.org/incident/19961109040409I), Nov 9, 1996: Boeing 737130 (N77204), Cleveland, OH. Narrative: hyd system "a" failure on approach when gear lowered. #4 slat actuator hyd line found broken. Replaced line acft rtn to suc. Removed & replaced #1 &…
- [Incident 19921012045129I](https://openairdocs.org/incident/19921012045129I), Oct 12, 1992: Boeing 737130 (N77204), St Louis, MO, Minor damage. While taxiing into gate pilot struck baggage carts with left engine.
- [Incident 19910611035039I](https://openairdocs.org/incident/19910611035039I), Jun 11, 1991: Boeing 737130 (N77204), Rochester, NY. Landing gear down indicator light problem on approach. Landed safely. Left main gear light module had become loose.

## Other aircraft with N77204

- [Cancelled 1959-11-18](https://openairdocs.org/deregistered/N77204-1959-11-18): Cessna 120, S/N 11666, built 1946. Owner: [Oberlin Motor Co](https://openairdocs.org/faa-owner/OBERLIN%20MOTOR%20CO), [Oberlin, KS](https://openairdocs.org/faa-place/KS/Oberlin)

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