# Boeing 737-36Q - Type: Aircraft model (FAA registry) - Registry code: 1384409 - Manufacturer (registry): BOEING - Model: 737-36Q - 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-737-36q 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 (22) As reported by operators and repair stations, by the model named in the report. - [SDR CA191205007](https://openairdocs.org/sdr/CA191205007), Jan 26, 2017: ADAPTER. FAILED. (CAN) LPV APPROACH ANOMALY: GLIDE SLOPE DEVIATION POINTER MOMENTARILY SCALLOPED UP FOR A SPLIT SECOND AT FINAL APPROACH FIX ON RNAV LPV APPROACH TO RUNWAY. THIS - [SDR CA140811011](https://openairdocs.org/sdr/CA140811011), Aug 8, 2014: CLUTCH. UNDERTORQUED. (CAN) ON FLAP EXTENSION TO 15 UNITS AND BEYOND, THE AIRCRAFT EXPERIENCES A ROLL THAT REQUIRES A TRIM INPUT. WHEN THE FLAPS ARE AT 15, 1.5 UNITS LT ROLL TRIM REQ - [SDR CA140707008](https://openairdocs.org/sdr/CA140707008), Jun 27, 2014: JACKSCREW. FAILED. (CAN) ON THE 27TH OF JUNE 2014 THE ACFT WOULD NOT DEPLOY THE FLAPS BEYOND 27 DEGREES IN FLIGHT. ON THE GROUND THE FLAP SYS OPERATED CORRECTLY. THE AMM TROUBLESH - [SDR CA140311005](https://openairdocs.org/sdr/CA140311005), Feb 27, 2014: TIE BOLT. FAILED. (CAN) REJECTED TAKEOFF WHERE TWO MAIN WHEELS ON THE LT MLG BLEW OUT AT APPROXIMATELY 100 KNOTS. THE CREW NOTICED THE VIBRATION, REJECTED THE TAKEOFF, AND HAD TH - [SDR CA130830014](https://openairdocs.org/sdr/CA130830014), Aug 29, 2013: CABLE. FRAYED. (CAN) ON APPROACH CREW INDICATED THAT THEY HAD TO ADD MORE AILERON TRIM FOR EACH SELECTION OF FLAPS. WHEN FLAPS 40 WERE SELECTED THE CREW HAD TO HAVE LT AILERON - [SDR CA110627018](https://openairdocs.org/sdr/CA110627018), Jun 25, 2011: BEARING. STIFF. PILOT COMPLAINT OF ELEVATOR BEING STIFF, FOUND BEARING VERY HARD TO TURN, BEARING REPLACED ACFT RETURNED TO SERVICE. - [SDR F3LA200500004](https://openairdocs.org/sdr/F3LA200500004), Jan 27, 2005: FLOORBEAM. BROKEN. DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AND WEB BROKEN AT STA 685 FROM LT FRAME TO SEAT TRACK BEAM. REPLACED L STUB FRAME PER SRM 51-40-02 AND 51-10-02. - [SDR F3LA200400118](https://openairdocs.org/sdr/F3LA200400118), Dec 10, 2004: CONTROL CABLE. OUT OF ADJUST. FLIGHT CREW REPORTED ON SHORT FINAL APPROACH, FULLY CONFIGURED AILERON ROLL FELT TO BIND. ALL OTHER PHASES OF FLIGHT NORMAL. ADJUSTED LT AND RT AILERON BOS CABL - [SDR F3LA200400111](https://openairdocs.org/sdr/F3LA200400111), Oct 5, 2004: WARNING LIGHT. FALSE INDICATION. REJECTED TAKEOFF. FLIGHT CREW REPORTED FWD ENTRY DOOR LIGHT ILLUMINATED. CHECKED DOOR PROXIMITY SENSOR PER MM 52-71-11 AND CHECKED NORMAL. - [SDR F3LA200300124](https://openairdocs.org/sdr/F3LA200300124), Sep 4, 2003: PANEL. MISINSTALLED. ABORTED TAKEOFF. DURING TAKEOFF ROLL, FLIGHT CREW REPORTED AIRCRAFT WOULD NOT STEER TO LT. TAKEOFF REJECTED AT APPROXIMATELY 60 KNOTS. FOUND LOWER SIDEWALL PANE - [SDR F3LA200200390](https://openairdocs.org/sdr/F3LA200200390), Dec 3, 2002: INTERCOSTAL. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED INTERCOSTAL AT STR. 26-R BETWEEN STA.747-767 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DRAWING 69-165 - [SDR F3LA200200257](https://openairdocs.org/sdr/F3LA200200257), Sep 5, 2002: SKIN. DAMAGED. DURING C-5 CHECK, INSPECTION REPORTED 3 CREASES ON TOP SURFACE OF RIGHT INBOARD FOREFLAP. REMOVED, REPAIRED AND REINSTALLED RT INBOARD FOREFLAP PER MM 27-51-07, - [SDR F3LA200200252](https://openairdocs.org/sdr/F3LA200200252), Aug 28, 2002: SKIN. GOUGED. DURING C-5 CHECK, INSPECTION REPORTED SMALL GOUGE IN OUTER FUSELAGE SKIN AT BS 203, STR 18R. REPAIRED DAMAGE PER SRM 53-00-01 FIG 202. - [SDR F3LA200100091](https://openairdocs.org/sdr/F3LA200100091), Jun 15, 2001: ACTUATOR. LEAKING. AIR TURN BACK. FLIGHT CREW REPORTED "B" SYSTEM ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND LOSS OF "B" SYSTEM HYDRAULIC FLUID. MAINTENANCE R - [SDR F3LA200100006](https://openairdocs.org/sdr/F3LA200100006), Jan 14, 2001: CONTROL UNIT. MALFUNCTIONED. UPON ARRIVAL, MAINTENANCE REPORTED CARGO COMPARTMENT FIRE DETECTION/SUPPRESSION SYSTEM OK LIGHT WOULD NOT ILLUMINATE. REPLACED CENTRAL CONTROL UNIT AND SYSTEM C - [SDR F3LA00152](https://openairdocs.org/sdr/F3LA00152), Jul 16, 2000: SKIN. DAMAGED. LGA - FLT 417 - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED BELT LOADER STRUCK AIRCRAFT AFT OF FORWARD CARGO DOOR, SECTION 43, FS 500, BETWEEN STRINGER 23R AND 25R - [SDR F3LA00119](https://openairdocs.org/sdr/F3LA00119), Jun 4, 2000: LIGHT. INOPERATIVE. SFO - PRIOR TO DEPARTURE, MAINTENANCE REPORTED EMERGENCY FLOOR PROXIMITY PATH LIGHTING INOPERATIVE AT ROWS 6 THROUGH 11. MAINTENANCE REPAIRED FAULTY GROUND WIRE - [SDR F3LA00003](https://openairdocs.org/sdr/F3LA00003), Jan 11, 2000: BATTERY. DISCHARGED. DEN - DURING C-3 CHECK INSPECTION, REPORTED AFT ENTRY DOOR ESCAPE SLIDE BATTERY FAILED BATTERY CHECK. MAINTENANCE REPLACED AFT ENTRY DOOR ESCAPE SLIDE. (M) - [SDR F3LA99047](https://openairdocs.org/sdr/F3LA99047), May 15, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOTLAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X) - [SDR F3LA99046](https://openairdocs.org/sdr/F3LA99046), May 13, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK, INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X) - [SDR F3LA98173](https://openairdocs.org/sdr/F3LA98173), Oct 12, 1998: BOLT. MISSING. UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 LEADING EDGE FLAP INDICATOR SHOWED FLAP IN EXTENDED MODE AT ALL SETTINGS. MAINTENANCE INSTALLED MISSING BOLT AND NUT ASS - [SDR F3LA98003](https://openairdocs.org/sdr/F3LA98003), Feb 15, 1998: BOLT. MISSING. SEA - FLT 640 - AIR TURN BACK. FLIGHT CREW REPORTED LEADING EDGE FLAPS/SLATS WOULD NOT FULLY RETRACT WHEN TRAILING EDGE FLAPS SELECTED TO '0' DEGREES. MAINTENAN --- 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.