# Boeing 737-36M - Type: Aircraft model (FAA registry) - Registry code: 138443B - Manufacturer (registry): BOEING - Model: 737-36M - 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-737-36m 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 (29) As reported by operators and repair stations, by the model named in the report. - [SDR PIDA200500011](https://openairdocs.org/sdr/PIDA200500011), Apr 19, 2005: ATTACH ANGLE. CRACKED. UPPER ATTACH ANGLE ON INTERCOSTAL AT BL 0 BETWEEN BS 380 AND BS 400 AT WL 208 IS CRACKED. REPLACED ANGLE PER SRM 51-10-02. - [SDR PIDA200500006](https://openairdocs.org/sdr/PIDA200500006), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS AT RIVET HOLE IN BS 867 FRAME AT STR 9 RT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500004](https://openairdocs.org/sdr/PIDA200500004), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS IN BS 787 FRAME AT RIVET HOLE AT STR 9RT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500013](https://openairdocs.org/sdr/PIDA200500013), Apr 19, 2005: INTERCOSTAL. CRACKED. INTERCOSTAL AT BS 540 CRACKED AT I/B AFT ATTACH FASTENER AT RBL 1. REPLACED INTERCOSTAL PER DWG 65-52894 AND SRM 51-10-2. - [SDR PIDA200500008](https://openairdocs.org/sdr/PIDA200500008), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS IN BS 827 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500007](https://openairdocs.org/sdr/PIDA200500007), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS IN BS 787 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500009](https://openairdocs.org/sdr/PIDA200500009), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS IN BS 867 FRAME AT STR 9LT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500012](https://openairdocs.org/sdr/PIDA200500012), Apr 19, 2005: CHANNEL. CRACKED. CRACK IN LOWER RADIUS AT AFT END OF THE LEFT MOUNT HAT CHANNEL FOR THE RADAR TR UNIT. REPAIRED HAT CHANNEL PER SRM 51-70-12. - [SDR PIDA200500010](https://openairdocs.org/sdr/PIDA200500010), Apr 19, 2005: WEB. CRACKED. FOUR CRACKS IN WEB PANEL AT LBL 4 BETWEEN BS 967 AND BS 986. REPAIRED PER DWG 65-46816 AND SRM 51-10-2. - [SDR PIDA200500015](https://openairdocs.org/sdr/PIDA200500015), Apr 19, 2005: SUPPORT ANGLE. CRACKED. NUMBER 5 SPOILER O/B HINGE I/B SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE PER SRM 51-10-2. - [SDR PIDA200500003](https://openairdocs.org/sdr/PIDA200500003), Apr 19, 2005: FLOORBEAM. CORRODED. CORROSION AT CLIP NUT HOLE AT LBL 27 ON FLOORBEAM AT BS 312. REPAIRED PER SRM 53-10-51. - [SDR PIDA200500014](https://openairdocs.org/sdr/PIDA200500014), Apr 19, 2005: SUPPORT ANGLE. CRACKED. NUMBER 5 SPOILER I/B ATTACH BRACKET SUPPORT ANGLES CRACKED. REPLACED ANGLES PER SRM 51-10-2. - [SDR PIDA200500005](https://openairdocs.org/sdr/PIDA200500005), Apr 19, 2005: FRAME. CRACKED. TWO CRACKS IN BS 827 FRAME AT STR 9RT. REPAIRED PER SRM 53-00-07. - [SDR PIDA200500002](https://openairdocs.org/sdr/PIDA200500002), Apr 19, 2005: SKIN PANEL. DAMAGED. IMPACT DAMAGE (DENT) AT BS 483 SKIN PANEL BETWEEN STR 21 LT AND STR 22 LT. REPAIRED PER SRM 53-00-01 FIG 229. - [SDR PIDA200500001](https://openairdocs.org/sdr/PIDA200500001), Apr 19, 2005: SKIN. DAMAGED. IMPACT DAMAGE TO THE FUSELAGE SKIN, FORWARD ENTRANCE DOORWAY BEARSTRAP AND BS 294.5 BULKHEAD SHEAR TIE AND WEB BETWEEN STR 19LT AND STR 20LT. REPAIRED PER EA 53 - [SDR 374PA0012](https://openairdocs.org/sdr/374PA0012), Sep 3, 2004: CIRCUIT BREAKER. FAILED. AUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN. REPLACED AURAL WARNING CIRCUIT BREAKER - [SDR 374PA0013](https://openairdocs.org/sdr/374PA0013), Sep 2, 2004: LINE. LOOSE. RIGHT ENGINE DOESN'T SPOOL UP. ADJUSTED GROUND IDLE PER MM. ADJUSTED SPECIFIC GRAVITY PER MM. TIGHTENED LINE AT BLEED REGULATOR. BOTH ENGINES OPERATE NORMAL PER - [SDR 374PA0011](https://openairdocs.org/sdr/374PA0011), May 17, 2004: SKIN. DENTED. DENT AT RIGHT SIDE OF AIRCRAFT AT BS 312 AND STR 20. REPAIRED PER SRM 53-00-01 AND EA 53-121. - [SDR 374PA0010](https://openairdocs.org/sdr/374PA0010), May 17, 2004: SKIN. DENTED. DENT IN FUSELAGE SKIN AFT OF L1 DOOR AT STA 400 BETWEEN STR 17 LT AND STR 18 LT. REPAIRED AREA PER SRM 53-00-01 AND EA 53-120. - [SDR 374PA0009](https://openairdocs.org/sdr/374PA0009), May 17, 2004: THRESHOLD. CRACKED. AFT CARGO DOOR CENTER SECTION OF THRESHOLD CRACKED. WELDED PER BAC 5975. - [SDR 374PA0008](https://openairdocs.org/sdr/374PA0008), May 17, 2004: ANGLE. CORRODED. CORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE IAW SRM 53-60-53. - [SDR 374PA0007](https://openairdocs.org/sdr/374PA0007), Mar 3, 2004: BOLT. LOOSE. FOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55A1087. REPLACED HARDWARE AT LOCATIONS F1 - [SDR 374PA0006](https://openairdocs.org/sdr/374PA0006), Jan 24, 2004: WARNING HORN. FALSE ACTIVATION. WARNING HORN ON TAKEOFF ROLL. NO LEADING EDGE FLAP/SLAT INDICATION. RESET LEADING EDGE POSITION INDICATOR CIRCUIT BREAKER. SYSTEM OPS CHECKS GOOD PER MM 27-88-0 - [SDR 374PA0005](https://openairdocs.org/sdr/374PA0005), Nov 21, 2003: SKIN. DAMAGED. FUSELAGE DAMAGED LEFT SIDE FROM BS 907 TO BS 927 AT STR 16 LT, AT BS 907 BETWEEN STR 21 LT AND 22 LT AND FRAME SHEAR TIE DAMAGED AT BS 908 BETWEEN STR 21 LT AND - [SDR 374PA0004](https://openairdocs.org/sdr/374PA0004), Nov 2, 2003: LAMP. INOPERATIVE. RT EMERGENCY OVERWING EXIT SIGN LOCATOR LIGHT INOPERATIVE. RE-LAMPED LOCATOR LIGHT IAW MM 33-51-11. OPS CHECKS NORMAL. - [SDR 374PA0003](https://openairdocs.org/sdr/374PA0003), Aug 9, 2003: COUPLER. FAILED. YAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD. - [SDR 374PA0002](https://openairdocs.org/sdr/374PA0002), Jan 12, 2003: BATTERY. DISCHARGED. FWD FLIGHT ATTENDANT JUMPSEAT OUTBOARD EMERGENCY FLASHLIGHT LED WILL NOT FLASH. ITEM DEFERRED PER MEL 25-12, CONTROL NR 0112001. 1/15/2003. R & R BATTERY POWER - [SDR 374PA0001A](https://openairdocs.org/sdr/374PA0001A), Oct 4, 2002: SENSOR. FAILED. TAKEOFF WARNING HORN ACTIVATED DURING T/O ROLL, OBSERVED LE FLAPS TRANSIT LIGHT ILLUMINATED, PERFORMED RTO. FOUND NR 1 KRUGER FLAP POSITION SENSOR BAD. R&R PROX - [SDR 374PA0001](https://openairdocs.org/sdr/374PA0001), Oct 4, 2002: SENSOR. Takeoff warning horn activated during T/O roll, observed LE flaps transit light illuminated, performed RTO. R&R #1&2 tires and brakes, R&R #3&4 brakes per 32-41 --- 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.