# Boeing 737-33R - Type: Aircraft model (FAA registry) - Registry code: 1384407 - Manufacturer (registry): BOEING - Model: 737-33R - 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: 0 - Page: https://openairdocs.org/model/boeing-737-33r 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 None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (23) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000166](https://openairdocs.org/sdr/2026FA0000166), Mar 7, 2026: WINDSHIELD. CRACKED. FLIGHT 942 CBB/VVI: WINDOW DAMAGE L1 FORWARD CRACKED. CORRECTIVE ACTION: HAS BEEN REPLACED WINDOW L1 IAW AMM 56-11-11/401 AND ADJUSTMENT TEST NORMAL OPERATION I - [SDR 2023F00353](https://openairdocs.org/sdr/2023F00353), Dec 22, 2023: MEC. FAILED. ENGINE#1 N2 REACH AMBER BAND DURING CRUISE THRUST WAS REDUCED AT APROX 80%, THERE WAS SURGE ON THE ENGINE AND VIBRATION OF 3.0, THRUST WAS FURTHER REDUCED AND S - [SDR 2023FA0000787](https://openairdocs.org/sdr/2023FA0000787), Nov 19, 2023: VALVE. INOPERATIVE. ENGINE NUMBER 2 COWL VALVE OPEN LIGHT, BRIGHT BLUE WITH ENGINE ANTI ICE SWITCH ON - [SDR 2022F00460](https://openairdocs.org/sdr/2022F00460), Nov 14, 2022: UNKNOWN. UNKNOWN. THE DOOR 1L BEGAN TO SLAM DURING THE ASCENT (LOUD SOUND). PERFORMED INSPECTION AT FORWARD ENTRY DOOR PRESSURE SEAL CHECK AND FLAPPER SEAL CHECK IAW AMM 52-11-00 - [SDR 2022F00451](https://openairdocs.org/sdr/2022F00451), Nov 5, 2022: LINKAGE. OUT OF ADJUST. NOSE LDG DID NOT RETRACT IN FLIGHT. CORRRECTIVE ACTION: NOSE LANDING GEAR WEL DOOR LINKAGE ADJUSTMENT IAW AMM 32-33-62-705-001 - [SDR 2022F00243](https://openairdocs.org/sdr/2022F00243), May 17, 2022: ACTUATOR. NONE. HIGH VIBRATION DURING TAKEOFF AND CLIMB AND GETTING WORSE WHILE INCREASING SPEED IN THE LOWER NOSE. CORRECTIVE ACTION:HAS BEEN CHANGED ROD ASSEMBLY IAW TASK 32- - [SDR 2022F00101](https://openairdocs.org/sdr/2022F00101), Feb 15, 2022: NONE. NONE. CRACKING ON VERTICAL STIFFENER RBL 6.15. BS 663.75 CENTER WING BOX AFT VERTICAL STIFFENER RBL 6.15. - [SDR 2022F00100](https://openairdocs.org/sdr/2022F00100), Feb 15, 2022: NONE. NONE. CRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02 - [SDR 2022F00099](https://openairdocs.org/sdr/2022F00099), Feb 15, 2022: NONE. NONE. CRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02 - [SDR 2022F00102](https://openairdocs.org/sdr/2022F00102), Feb 15, 2022: NONE. NONE. CRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02 - [SDR 2016F00233](https://openairdocs.org/sdr/2016F00233), Nov 27, 2016: VALVE. FAULTY. DURING CLIMB RT PACK DOES NOT CONTROL THE CABIN PRESSURIZATION - [SDR 2016F00187](https://openairdocs.org/sdr/2016F00187), Sep 17, 2016: SHIMMY DAMPENER. FAILED. RIGHT SHIMMY DAMPER FAILED ON LANDING ROLL. COLETERAL DAMAGE TO LANDING DEAR WHEELS, BRAKES, HIDRAULIC FLUID LINES, TORSION LINKS AND SECONDARY FLIGHT CONTROLS - [SDR W8PA980027](https://openairdocs.org/sdr/W8PA980027), Jan 22, 1998: BATTERY. DISCHARGED. DEN- FWD LEFT EMERGENCY FLASHLIGHT IS INOP. REPLACED BATTERY PER CHAPTER 25-60-00, OPS CHECK GOOD. - [SDR W8PA980018](https://openairdocs.org/sdr/W8PA980018), Jan 14, 1998: CONTROLS. MALFUNCTIONED. ELEVATOR JAMMED ON LANDING FLARE. REQUIRED APPROX 50 TO 60 LBS FORCE TO FREE THE ELEVATOR. INSPECTED ELEVATORS, ELEVATOR POWER CONTROL UNIT, ALL ACCESSIBLE ELEV - [SDR W8PA980002](https://openairdocs.org/sdr/W8PA980002), Jan 1, 1998: WIRE. BROKEN. DEN- EMERGENCY TRACK LIGHTING INOP AT ROW 7 AND 15. REPAIRED WIRE AT ROW 7 AND 15, OPS CHECK GOOD. - [SDR W8PA971521](https://openairdocs.org/sdr/W8PA971521), Dec 5, 1997: CABLE. MISROUTED. CHECK AFT LEFT DOOR EMERGENCY SLIDE RELEASE CABLE FOR PROPER ROUTING. CABLE IMPROPERLY ROUTED DURING AIRCRAFT MANUFACTURE. REROUTED CABLE PER MAINT MANUAL CHAPT - [SDR W8PA971520](https://openairdocs.org/sdr/W8PA971520), Dec 4, 1997: SOCKET. DIRTY. DEN- EMERGENCY LIGHT ON RIGHT SIDE OF FUSELAGE AFT OF WING IS INOP. CLEANED CONTACTS ON BULB AND SOCKET, OPS CHECK NORMAL. - [SDR W8PA971516](https://openairdocs.org/sdr/W8PA971516), Dec 1, 1997: LAMP. FAILED. DEN- L1 DOOR EMERGENCY LIGHT IS INOP. REPLACED LAMPS, OPS CHECK GOOD. - [SDR W8PA971495](https://openairdocs.org/sdr/W8PA971495), Oct 12, 1997: WIRE. BROKEN. DEN- EMERGENCY LIGHT INOP AT ROW 2. REPAIRED BROKEN WIRE, OPS CHECK GOOD. - [SDR W8PA971442](https://openairdocs.org/sdr/W8PA971442), Sep 23, 1997: LAMP. FAILED. ROW 6 EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECK GOOD. - [SDR W8PA971436](https://openairdocs.org/sdr/W8PA971436), Sep 11, 1997: LIGHT. FAILED. EMERGENCY LIGHT ON SEAT 4L IS INOP. RELAMPED, OPS CHECK GOOD. - [SDR W8PA971433](https://openairdocs.org/sdr/W8PA971433), Sep 11, 1997: WIRE. DISCONNECTED. EMERGENCY AISLE LIGHTING INOP AT ROW 2. RECONNECTED WIRES, OPS CHECK GOOD. - [SDR W8PA971397](https://openairdocs.org/sdr/W8PA971397), Aug 19, 1997: SWITCH. SEIZED. REJECTED TAKEOFF AT 15 KNOTS WHEN TAKEOFF WARNING HORN SOUNDED. FOUND PARKING BRAKE SWITCH STUCK. FREED SWITCH, PERFORMED TAKEOFF WARNING TEST PER MM. ALL CHECK --- 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.