# Boeing 737-7CG - Type: Aircraft model (FAA registry) - Registry code: 13844FA - Manufacturer (registry): BOEING - Model: 737-7CG - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-737-7cg Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N950TR](https://openairdocs.org/aircraft/N950TR): [Ohio Resources LLC](https://openairdocs.org/faa-owner/OHIO%20RESOURCES%20LLC), [Camden, DE](https://openairdocs.org/faa-place/DE/Camden), built 1999, S/N 30751 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (14) As reported by operators and repair stations, by the model named in the report. - [SDR CA061114008](https://openairdocs.org/sdr/CA061114008), Nov 1, 2006: WINDOW. FAILED. (CAN) ON NOV. 1, 2006 A/C 216 EXPERIENCED A CRACKED NR 4 RT EYEBROW WINDOW. THE A/C CONTINUED TO ITS DESTINATION WITHOUT ANY FURTHER EVENTS. THE NR 4 WINDOW WAS - [SDR CA061114010](https://openairdocs.org/sdr/CA061114010), Oct 31, 2006: WINDOW. FAILED. (CAN) ON OCT. 31, 2006 A/C 202 EXPERIENCED A CRACKED NR 4 LT EYEBROW WINDOW. THE A/C CONTINUED TO ITS DESTINATION WITHOUT ANY FURTHER EVENTS. THE NR 4 WINDOW WA - [SDR CA061114009](https://openairdocs.org/sdr/CA061114009), Oct 27, 2006: WINDOW. CRACKED. (CAN) ON OCT. 27, 2006 A/C 201 EXPERIENCED A CRACKED NR 4 LT EYEBROW WINDOW. THE A/C CONTINUED TO ITS DESTINATION WITHOUT ANY FURTHER EVENTS. THE NR 4 WINDOW WA - [SDR FAR145SDR061](https://openairdocs.org/sdr/FAR145SDR061), Sep 10, 2006: FRANGIBLE LINK. STUCK. DURING A MAINTENANCE TEST DEPLOYMENT OF THE AIRCRAFT EVACUATION SLIDES NG (REGISTRATION NR 02-0201), IAW TASK CARD 25-220-00-01, THE SLIDE AT THE AFT ENTRY DOOR - [SDR CA060620003](https://openairdocs.org/sdr/CA060620003), Jun 20, 2006: STATIC INVERTER. FAILED. (CAN) ON THE 20 JUNE 06 WHILE CONDUCTING A SCHEDULED PHASE 3 CHECK. MAINTENANCE FOUND ELEC LIGHT ILLUMINATED ON THE OVERHEAD PANEL. DURING THE TROUBLESHOOTING A - [SDR CA051020001](https://openairdocs.org/sdr/CA051020001), Oct 19, 2005: DISPLAY. FAILED. (CAN) SEAT VDU 22F WENT BLANK AND SEEMED HOTTER THAN OTHER SCREENS. A HINT OF BURNING WIRE SMELL WAS NOTICED. SMELL DISSIPATED. MAINTENANCE REPLACED THE VDU AND - [SDR CA051007006](https://openairdocs.org/sdr/CA051007006), Oct 6, 2005: DISPLAY. FAILED. (CAN) A/C WAS ON THE GROUND WHEN A BURNING ELECTRICAL SMELL WAS NOTICED AT ROW 13. SEAT 13B WAS DEACTIVATED. MAINTENANCE REPLACED THE VDU AND THE SYSTEM WAS TES - [SDR CA050825002](https://openairdocs.org/sdr/CA050825002), Aug 24, 2005: DISPLAY. FAILED. (CAN) ON AUGUST 24, 2005 A/C WAS IN CRUISE WHEN THE CREW WAS ADVISED THAT THE VDU AT SEAT 17C HAD QUIT WORKING AND THE PASSENGER SMELLED SMOKE. THE IFE SYSTEM W - [SDR CA050728007](https://openairdocs.org/sdr/CA050728007), Jul 25, 2005: DISPLAY. FAILED. A/C WAS IN CRUISE WHEN THE CREW WERE ADVISED THAT THE VDU AT SEAT 11A HAD QUIT WORKING AND THAT IT SMELLED LIKE BURNING WIRE. THERE WAS NO SMOKE OR ARCING OBSER - [SDR CA041216011](https://openairdocs.org/sdr/CA041216011), Dec 15, 2004: B-NUT. LOOSE. (CAN) APPROX 30 MINS AFTER TAKE OFF, CREW NOTED LOSS OF OIL QTY IN NR 2 ENG & DID AN AIR TURNBACK. SEVERAL MINS LATER CREW NOTED FLUCTUATING OIL PRESSURE IN NR - [SDR CA040531003](https://openairdocs.org/sdr/CA040531003), May 27, 2004: FAN BLADE. BIRD INGESTION. AIRCRAFT STRUCK ONE, POSSIBLY TWO SEAGULLS ON TAKEOFF, IMMEDIATE VIBRATION FELT. TAKEOFF ABANDONED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE CONDUCTED 'BIRD ST - [SDR JBXA000242](https://openairdocs.org/sdr/JBXA000242), Feb 11, 2001: CONNECTOR. DAMAGED. RIGHT MAIN LANDING GEAR DOWN INDICATION ON MAIN AND OVERHEAD PANEL WITH GEAR HANDLE IN THE UP POSITION. PSEU LIGHT ILLUMINATED UPON TOUCHDOWN. PERFORMED TASK 32 - [SDR JBXA000224](https://openairdocs.org/sdr/JBXA000224), Dec 4, 2000: ENGINE. MALFUNCTIONED. UPON TAKE OFF AFTER SPOOL UP OF ENGINES. RIGHT ENGINE WAS SLOW TO SPOOL ANY FATHER. IT DID NOT MATCH LEFT ENGINE WHICH APPEARED TO SPOOL NORMALLY. APORTED TAKE- - [SDR 20000707SH011](https://openairdocs.org/sdr/20000707SH011), Nov 16, 1999: LINE. CHAFED. INSPECTION REVEALED WIRE BUNDLE RUN W2705 (HGS) MAKES HARD CONTACT WITH TAT PROBE BLEED AIR LINE AT BS 312 LBL 47.0 WL 202.6. THIS HAS BEEN FOUND ON THE LAST 4 --- 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.