# Boeing 737-36N - Type: Aircraft model (FAA registry) - Registry code: 1384408 - Manufacturer (registry): BOEING - Model: 737-36N - 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-737-36n 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 (53, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026F00172](https://openairdocs.org/sdr/2026F00172), Jul 31, 2026: WINDSHIELD. CRACKED. FLIGHT 650 CBB-VVI CRACKED WINDOW #R1 DURING DESCENT. CORRECTIVE ACTION: REMOVED AND REPLACED WINDOW #1 AND CHANGED CONTROL CABIN WINDOW HEAT. IN TEST NORMAL - [SDR 2025F00017](https://openairdocs.org/sdr/2025F00017), Jan 4, 2025: BATTERY. DISCHARGED. BOTH DC FAIL. LIGHTS ILLUMINATED. LOW BATTERY VOLTAGE. CANCELLED AIRCRAFT IN SLVR. CORRECTIVE ACTION: REMOVED AN REPLACED MAIN BATTERY - [SDR 2024F00268](https://openairdocs.org/sdr/2024F00268), Oct 31, 2024: CONTROL SYSTEM. FAILED. CANCELED FLIGHT 646 CBB/VVI DUE TO ENGINE #2 SLOW ACCELERATION IN DIFFERENTE PHASES OF FLIGHT AND HOT STARTS. CORRECTIVE ACTION: REMOVED AN INSTALLED MAIN ENGIN - [SDR 2024F00183](https://openairdocs.org/sdr/2024F00183), Jul 30, 2024: TIRE. FAILED. TIRE#2 TREAD LOSS. CANCELLED AIRCRAFT LEG CBB/TDD FLIGHT 466. CONDITIONAL INSPECTION PERFOMED. FOUND DAMAGE IN FLAP I NLEFT INBOARD FORE FLAP WITHIN LIMITS. LEF - [SDR 2024F00029](https://openairdocs.org/sdr/2024F00029), Feb 5, 2024: A/C PACK. TRIPPED. QRF TO VVI DUE TO PACK TRIP OFF#2 LIGHT ILLUMINATE AFTER TAKE OFF. CORRECTIVE ACTION: PERFORMED ADJUSTMENT/TEST IAW AMM 21-51-00/501 SYST WORK PROPERLY ON GROUN - [SDR 2023F00010](https://openairdocs.org/sdr/2023F00010), Dec 3, 2022: FITTING. CORRODED. MLG LH AND RH LUG FITTINGS WITH CORROSION DAMAGE LEFT SIDE: 0.070" AND 11HRS; 0.044" AT 10HRS; 0.049" AT 12HRS. RIGHT SIDE: 0.069" AT 12HRS,0.057" AT 11HRS. - [SDR 2022F00227](https://openairdocs.org/sdr/2022F00227), May 16, 2022: MOTOR. FAILED. TRAILING EDGE FLAP ASSYMETRY DURING TKEOFF, FLAPS ON THE RIGHT WING STUCK ON 1 AND FLAPS ON THE LEFT WING WENT UP. CORRECTIVE ACTION: HAS BEEN CHANGED FLAP HYDR - [SDR 2022F00232](https://openairdocs.org/sdr/2022F00232), May 8, 2022: NONE. NONE. STRONG NOISE AND VIBRATION DOOR 1L. CORRECTIVE ACTION:HAS BEEN CHANGED DOOR 1L IAW AMM 52-11-00/401 AND ADJUSTED TEST NORMAL IAW AMM 52-11-00/501 - [SDR 2022F00127](https://openairdocs.org/sdr/2022F00127), Mar 14, 2022: NONE. NONE. CRACKING ON STA 291.5 FRAME WEB - INTERCOSTAL STRAT CUTOUT AT STRINGER 14R. CRACKING ON STA 277 INTERCOSTAL - STRINGER 16R RADIUS TRIMOUT. THESE CRACKINGS WERE - [SDR 2022F00009](https://openairdocs.org/sdr/2022F00009), Nov 7, 2021: RELAY. BLOCKED. LANDING GEAR LEVE WILL NOT MOVE UP AFTER TAKEOFF. LANDING GEAR DOWN, THERE IS NO ANY GREEN LIGHT INDICATORS - [SDR UIEA2021072201607](https://openairdocs.org/sdr/UIEA2021072201607), Jun 28, 2021: FLAP. DAMAGED. MULTIPLE AREAS OF DAMAGE ON LH IB FLAP ASSY, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02. CUSTOMER REQUEST FLAP REPLACEMENT. REMOVED AND REPLACED LH IB FLAP ASSY - [SDR CA1912050006](https://openairdocs.org/sdr/CA1912050006), Jan 24, 2016: ADAPTER. FAILED. (CAN) FINAL APPROACH CONDUCTING LPV APPROACH AIRCRAFT WAS FULLY CONFIGURED AND STABLE ON APPROACH WITH LOCALIZER AND GLIDE SLOPE CAPTURED. EXACTLY WHILE CROSSIN - [SDR CA140627001](https://openairdocs.org/sdr/CA140627001), Jun 26, 2014: MECHANISM. STIFF. (CAN) PILOT REPORTED: F/O YOKE FEELS STIFF DURING CONTROL CHECK. ONLY STIFF WITH LT AILERON, F/O SIDE. FOUND STIFFNESS AND NOISE EMANATING FROM AILERON TRANSFER - [SDR 7AHR201404152372](https://openairdocs.org/sdr/7AHR201404152372), Apr 11, 2014: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR STRUCTURE AT LBL 14.00 AT STA 727A, 727D, 747, 787 AND 847 CARGO TIE DOWN FITTINGS CORRODED. REMOVED CORROSION ON FITTINGS AND FABRICATED NEW SE - [SDR 7AHR201404152449](https://openairdocs.org/sdr/7AHR201404152449), Apr 10, 2014: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 994, LBL 33-44 CORRODED. REMOVED CORROSION IN AREA AND REPAIRED IAW SRM 51-40-02. - [SDR 7AHR201404152522](https://openairdocs.org/sdr/7AHR201404152522), Apr 10, 2014: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT CHANNEL HAS CORROSION AT BS 956, RBL 50. REMOVED CORROSION, FABRICATED FLOOR SUPPORTS AND INSTALLED IAW SRM 51-10-07 AND 53-40-02. - [SDR 7AHR201404152462](https://openairdocs.org/sdr/7AHR201404152462), Apr 10, 2014: FLOORBEAM. CORRODED. AFT CARGO FLOORBEAM HAS CORROSION AT BS 867, BL 0. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-00-07, FIG 202, PGS 208-214. - [SDR 7AHR201404152451](https://openairdocs.org/sdr/7AHR201404152451), Apr 10, 2014: FRAME. CORRODED. RIGHT FUSELAGE FRAME AT BS 994, RBL 48 HAS CORROSION ON FWD & INBD SIDE OF FRAME. REMOVED CORROSION AND INSTALLED REPAIR TO FRAME IAW SRM 56-60-15 & 51-40-05. - [SDR 7AHR201404152335](https://openairdocs.org/sdr/7AHR201404152335), Apr 9, 2014: FRAME. CORRODED. AFT CARGO BAY, FRAME BS 747 BETWEEN S28L & 27R CORRODED. REMOVED CORROSION FROM AREAS, REPAIRED IAW SRM 53-00-07, FIG 201. - [SDR 7AHR201404152532](https://openairdocs.org/sdr/7AHR201404152532), Apr 9, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT BS 390, RBL 45. R & R SECTION OF SEAT TRACK IAW SRM 53-00-52. - [SDR 7AHR201404152106](https://openairdocs.org/sdr/7AHR201404152106), Apr 8, 2014: INTERCOSTAL. CRACKED. LEFT INBD MIDFLAP INTERCOSTAL INBD END OF OTBD TORQUE TUBE IS CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02. INTERCOSTAL FABRICATED IAW DWG 57-14105-01, REV NEW - [SDR 7AHR201404082448](https://openairdocs.org/sdr/7AHR201404082448), Apr 8, 2014: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUTPLATE HOLES FROM RBL 4-44 UPPER CAP. INSTALLED REPAIR IAW SRM 53-60-51. - [SDR 7AHR201404082445](https://openairdocs.org/sdr/7AHR201404082445), Apr 8, 2014: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT AT BS 967 LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 53-60-51. - [SDR 7AHR548B2444](https://openairdocs.org/sdr/7AHR548B2444), Apr 8, 2014: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT AT BS 952, LBL 16 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-2. - [SDR 7AHR201404082442](https://openairdocs.org/sdr/7AHR201404082442), Apr 8, 2014: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM HAS CORROSION BS 948, RBL 4. REMOVED CORROSION AND INSTALLED REPAIR TO IAW SRM 53-30-51, REPAIR 2. - [SDR 7AHR201404082374](https://openairdocs.org/sdr/7AHR201404082374), Apr 8, 2014: STRIKER. CORRODED. FWD CARGO DOOR SURROUND STRUCTURE AFT EDGE BS 490 LOWER AFT DOOR STOP HAS BROKEN STRIKER PLATE AND FITTING IS CORRODER. R & R STRIKER PLATE AND FITTING IAW SRM - [SDR 7AHR201404082339](https://openairdocs.org/sdr/7AHR201404082339), Apr 8, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME AT BS 807 HAS CORROSION FROM STRINGER 27L - 28RT. REMOVED CORROSION IAW SRM 53-00-07, FIG 207, REPAIR 17. - [SDR 7AHR201404082334](https://openairdocs.org/sdr/7AHR201404082334), Apr 8, 2014: SHEAR TIE. CORRODED. AFT CARGO BAY, BS 727E SHEAR TIE HAS CORROSION BETWEEN STRINGERS 27-28RT. REMOVED CORROSION AND FABRICATED NEW SHEAR TIE IAW SRM 53-00-07, FIG 202, REPAIR 17. - [SDR 7AHR201404082288](https://openairdocs.org/sdr/7AHR201404082288), Apr 8, 2014: INTERCOSTAL. CORRODED. FWD CARGO BAY INTERCOSTAL BS 420-440 RT HAS DOUBLE DRILLED HOLES AND CORROSION. R & R IAW SRM 53-30-04, FIG 1 AND 51-40-02. - [SDR F3LA200500011](https://openairdocs.org/sdr/F3LA200500011), Mar 8, 2005: ROLLER. WORN. MAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE P - [SDR F3LA200300191](https://openairdocs.org/sdr/F3LA200300191), Dec 31, 2003: ACTUATOR. INOPERATIVE. DURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOC - [SDR F3LA200300190](https://openairdocs.org/sdr/F3LA200300190), Dec 31, 2003: SKIN. DENTED. DURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202. - [SDR F3LA200300188](https://openairdocs.org/sdr/F3LA200300188), Dec 19, 2003: FLAP TRACK. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRA - [SDR F3LA200300187](https://openairdocs.org/sdr/F3LA200300187), Dec 19, 2003: BATTERY PACK. FAILED. DURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE. - [SDR F3LA200300186](https://openairdocs.org/sdr/F3LA200300186), Dec 19, 2003: INTERCOSTAL. CRACKED. DURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOST - [SDR F3LA200300185](https://openairdocs.org/sdr/F3LA200300185), Dec 19, 2003: OXYGEN BOTTLE. DISCHARGED. DURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-2 - [SDR F3LA200300184](https://openairdocs.org/sdr/F3LA200300184), Dec 19, 2003: MODULE. FAULTY. DURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G - [SDR F3LA200300183](https://openairdocs.org/sdr/F3LA200300183), Dec 19, 2003: FRAME. CRACKED. DURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1- - [SDR F3LA200300182](https://openairdocs.org/sdr/F3LA200300182), Dec 19, 2003: SHEAR TIE. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07. - [SDR F3LA200300181](https://openairdocs.org/sdr/F3LA200300181), Dec 19, 2003: SHEAR TIE. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07. - [SDR F3LA200200394](https://openairdocs.org/sdr/F3LA200200394), Dec 5, 2002: STRAP. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FILLER/STRAP PER SRM 51-40-02 AND 51-10-02. - [SDR F3LA200200393](https://openairdocs.org/sdr/F3LA200200393), Dec 5, 2002: STRAP. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED SILL STRAP PER SRM 51-40-07 AND 51-10-02. - [SDR F3LA200200392](https://openairdocs.org/sdr/F3LA200200392), Dec 5, 2002: WEB. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40 - [SDR F3LA200200391](https://openairdocs.org/sdr/F3LA200200391), Dec 3, 2002: ANGLE. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIRED ANGLE PER SRM 51-40-02, 51-40-05 AND 5 - [SDR F3LA200200396](https://openairdocs.org/sdr/F3LA200200396), Dec 3, 2002: SUPPORT ANGLE. GOUGED. DURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 5 - [SDR F3LA200200395](https://openairdocs.org/sdr/F3LA200200395), Dec 3, 2002: COWL DOOR. CHAFED. DURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITIONAL DAMAGE FOUND AT EDGE OF PREVIOUS REPAI - [SDR F3LA200200250](https://openairdocs.org/sdr/F3LA200200250), Aug 21, 2002: SHUTOFF VALVE. FAILED. AIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, - [SDR F3LA200100123](https://openairdocs.org/sdr/F3LA200100123), Nov 25, 2001: WIRE. BROKEN. PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER STANDARD PRACTICES 20-30-12, PERFORMED OPER - [SDR F3LA200000277](https://openairdocs.org/sdr/F3LA200000277), Dec 28, 2000: FITTING. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND RT. AFT LAVATORY OTBD AFT FLOOR MOUNT. MAINTENANCE FABRICATED AND REPLACED NEW FITTING PER EA 25-737-108. - [SDR F3LA99050](https://openairdocs.org/sdr/F3LA99050), May 19, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X) All 53: https://openairdocs.org/model/boeing-737-36n/reports.md --- 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.