# Boeing 737-35B

- Type: Aircraft model (FAA registry)
- Registry code: 13844BM
- Manufacturer (registry): BOEING
- Model: 737-35B
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 149
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 1
- Page: https://openairdocs.org/model/boeing-737-35b

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)

- [N789LS](https://openairdocs.org/aircraft/N789LS): [Gryphon Trading 18 LLC](https://openairdocs.org/faa-owner/GRYPHON%20TRADING%2018%20LLC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1988, S/N 24269

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (55, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA070807001](https://openairdocs.org/sdr/CA070807001), Jul 27, 2007: LOCK ACTUATOR. FAILED. (CAN) DURING APPROACH, THE NOSE LANDING GEAR DID NOT RECEIVE A DOWNLOCK INDICATION IN THE COCKPIT. IT WAS BELIEVED BY THE CREW THAT THE GEAR FAILED TO EXTEND. A
- [SDR CA070312003](https://openairdocs.org/sdr/CA070312003), Mar 12, 2007: STARTER. FAILED. (CAN) APU SHUTDOWN ON ITS OWN AND WOULD NOT RE-START. NEW STARTER INSTALLED. NEW STARTER BLEW APART ON FIRST START ATTEMPT. SECOND STARTER INSTALLED AND OPERATE
- [SDR PIDR2006001](https://openairdocs.org/sdr/PIDR2006001), Jun 8, 2006: ATTACH FITTING. DAMAGED. DURING AN A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, MAINTENANCE DISCOVERED A TIME LIMITED BLENDOUT REPAIR TO THE AFT FACE OF THE LEFT HORIZONTA
- [SDR PIDR2006002](https://openairdocs.org/sdr/PIDR2006002), Jun 8, 2006: SKIN. CHAFED. INSPECTION NOTED A CHAFED AREA ON AN EXISTING SRM ALUMINUM REPAIR DOUBLER ON THE RIGHT WING OUTBOARD FLAP MID-FLAP LEADING EDGE 20 INCHES FROM THE INBOARD END. 
- [SDR PIDR2006004](https://openairdocs.org/sdr/PIDR2006004), Jun 8, 2006: SKIN. CRACKED. INSPECTION NOTED A GOUGE ON THE NR 5 SLAT UPPER LEADING EDGE SURFACE 28 INCHES FROM THE INBOARD END (SS169.0). REPAIRED DAMAGED AREA IN ACCORDANCE WITH PACE AIR
- [SDR PIDR2006005](https://openairdocs.org/sdr/PIDR2006005), Jun 8, 2006: SKIN. CRACKED. INSPECTION NOTED CRACKS AT SEVERAL FASTENER LOCATIONS IN THE NR 5 SLAT LOWER TRAILING EDGE SKIN PANEL UNDER THE SLAT ACTUATOR. REPAIRED DAMAGED AREA IN ACCORDAN
- [SDR PIDR2006006](https://openairdocs.org/sdr/PIDR2006006), Jun 8, 2006: SKIN. CRACKED. INSPECTION NOTED SEVERAL CRACKS IN THE NR 3 SLAT LOWER TRAILING EDGE SKIN BELOW THE SLAT ACTUATOR. REPAIRED DAMAGED AREA PER SRM 57-43-01.
- [SDR PIDR2006003](https://openairdocs.org/sdr/PIDR2006003), Jun 8, 2006: SKIN. DAMAGED. AN EXISTING REPAIR TO THE FUSELAGE SKIN BETWEEN THE L1 DOOR HINGES JUST FORWARD OF THE DOOR REQUIRES REWORK TO REMOVE THE DAMAGE. REWORKED DAMAGED AREA IAW EA N
- [SDR DL73G050629](https://openairdocs.org/sdr/DL73G050629), Oct 18, 2005: FAN. SEIZED. AFTER T/O THROUGH 5000 AND 7000 FEET, AN UNUSUAL SMELL THROUGH CABIN. REPLACED CABIN RECIRC FAN.
- [SDR DL73G050236](https://openairdocs.org/sdr/DL73G050236), Apr 18, 2005: SKIN. GOUGED. AT MID VISIT FOUND FUSELAGE SKIN GOUGED AT STA 1129-1138 WL 265. REPAIRED PER ERA 098117-14. TIME LIMITED REPAIR. ADDITIONAL ER/A IS REQUIRED FOR CONTINUED SERV
- [SDR DL73G040979](https://openairdocs.org/sdr/DL73G040979), Oct 13, 2004: CHARGER. UNSERVICEABLE. CREW REPORTED SMELL IN COCKPIT. BATTERY OVERHEATED AND VOLTAGE APPROXIMATELY 18 VOLTS. SMOKE COMING FROM TOP OF BATTERY. REPLACED BATTERIES AND CHARGER.
- [SDR DL73G040963](https://openairdocs.org/sdr/DL73G040963), Oct 13, 2004: BATTERY. OVERHEATED. CREW REPORTED SMELL IN COCKPIT. FOUND BATTERY OVERHEATED. REPLACED BATTERY AND CHARGER PER AMM. OPS CHECKS NORMAL. AIRED OUT COCKPIT. AIRCRAFT OK FOR SERVICE.
- [SDR DL73G040733](https://openairdocs.org/sdr/DL73G040733), Aug 7, 2004: BATTERY. ODOR. AIR TURNBACK, ODOR OF ELECTRICAL IN CABIN. REPLACED BATTERIES AND CHARGER.
- [SDR DL73G040739](https://openairdocs.org/sdr/DL73G040739), Aug 6, 2004: CONNECTOR. DISCONNECTED. ON PRE-DEPARTURE FOUND ROWS 1 AND 2 DEF EMERGENCY LIGHTS INOP ON SEATS. PINS WERE FOUND OUT OF THE CONNECTOR AND RE-INSERTED INCORRECTLY RESULTING IN THE FUSABL
- [SDR DL73G040403](https://openairdocs.org/sdr/DL73G040403), May 6, 2004: BULB. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SAME PER A.M.M. - OPS CKS GOOD
- [SDR DL73G040332](https://openairdocs.org/sdr/DL73G040332), Apr 12, 2004: SKIN. DENTED. TWO DENTS WERE NOTED IN THE FUSELAGE SKIN JUST ABOVE S16L, NEAR BS 384 AND 400. DAMAGE WAS REWORKED PER ERA 089089-14.
- [SDR DL73G040331](https://openairdocs.org/sdr/DL73G040331), Apr 12, 2004: FLOORBEAM. CORRODED. CORROSION WAS NOTED ON THE UPPER CAP OF THE BS 986.5 FLOORBEAM. UPPER CAP REMOVED AND NEW SECTION SPLICED IN PER ERA 089197-14.
- [SDR DL73G040330](https://openairdocs.org/sdr/DL73G040330), Apr 12, 2004: SKIN. DENTED. A DENT AND GOUGE WERE NOTED IN THE UPPER SKIN AT BS 807 NEAR S25R. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 089247-14.
- [SDR DL73G040310](https://openairdocs.org/sdr/DL73G040310), Apr 5, 2004: SKIN. DAMAGED. DAMAGE WAS NOTED TO THE FUSELAGE SKIN AT THE FWD EDGE OF THE C1 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089422-14.
- [SDR DL73G040309](https://openairdocs.org/sdr/DL73G040309), Apr 5, 2004: SPAR. FATIGUED. THE LEFT WING REAR SPAR CHORD WAS FOUND TO BE CRACKED AT APPROX RSS 223. THE SUBJECT HOLE IS COMMON TO THE MLG BEAM ATTACH FITTING. DAMAGE WAS REMOVED AND REWOR
- [SDR DL73G040219](https://openairdocs.org/sdr/DL73G040219), Mar 7, 2004: WIRE. DAMAGED. SEVERAL EMERGENCY LIGHTS INOP. REPAIRED WIRING, CHECKS NORMAL.
- [SDR DL73G030981](https://openairdocs.org/sdr/DL73G030981), Nov 5, 2003: IRU. FAILED. DIV DUE TO LOSS OF ALL HEADING INFORMATION. REPLACED NR 1 IRU.
- [SDR DL73G030817](https://openairdocs.org/sdr/DL73G030817), Sep 6, 2003: WIRE HARNESS. DAMAGED. EMERGENCY LIGHTING AT ROW 5DEF INOP. REPLACED E-PATH SEAT CABLE ASSY PER AMM. E-PATH LIGHTING CHECKS GOOD.
- [SDR DL73G030745](https://openairdocs.org/sdr/DL73G030745), Aug 12, 2003: FLANGE. CORRODED. DURING OVERHAUL OF THE MLG PISTON IAW CMM 32-11-11, THE BRAKE FLANGE FACE WAS LOCALLY BLENDED. SUBJECT CMM, FIGURE 403 NOTES NO BLENDING IS ALLOWED, AND TO CONT
- [SDR DL73G030705](https://openairdocs.org/sdr/DL73G030705), Jul 28, 2003: WIRE. SHORTED. UPON LANDING A ACRID ELECTRICAL ODOR NOTICED IN COCKPIT AND CABIN. REPAIRED SHORTED WIRE IN FWD CARGO COMPARTMENT AND REPLACED CABIN PRESSURE CONTROLLER
- [SDR DL73G030584](https://openairdocs.org/sdr/DL73G030584), Jun 24, 2003: COFFEEMAKER. SPARKS. COFFEEMAKER HAS ELECTRICAL SPARKS. REPLACED DISPENSER.
- [SDR DL73G030415](https://openairdocs.org/sdr/DL73G030415), May 2, 2003: CONTROLLER. FAILED. WHILE PREFORMING FCF FLIGHT - R-1 WINDSHIELD TERMINAL BLOCK AREA, UPPER RT CORNER, BEGAN TO SMOKE AND SPARK FOLLOWED BY FLAME APPEARING FOR SEVERAL SECONDS. REP
- [SDR DL73G030394](https://openairdocs.org/sdr/DL73G030394), Apr 25, 2003: BULKHEAD. CRACKED. THE FS 178 BULKHEAD WEB WAS FOUND WITH 3 TYPICAL CRACKS, 1 AT LBL 5.7 & WL 200, 1 AT RBL 5.7 & WL 200, AND 1 AT RBL 5.7 & WL 211. THE CRACKS ARE TYPICAL OF AD 2
- [SDR DL73G030392](https://openairdocs.org/sdr/DL73G030392), Apr 25, 2003: SKIN. CRACKED. A CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER AT THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN THE CORNER. THE CU
- [SDR DL73G030364](https://openairdocs.org/sdr/DL73G030364), Apr 15, 2003: BULKHEAD. CRACKED. INSPECTION OF THE FS 178 BULKHEAD WEB PER AD 2000-05-29 REVEALED SEVERAL CRACKS IN THE CENTER WEB BETWEEN WL 219 & 226 AND BETWEEN LBL 12 & RBL 5.7. THE CENTER 
- [SDR DL73G040937](https://openairdocs.org/sdr/DL73G040937), Sep 30, 2002: WINDSHIELD. CRACKED. L1 WINDOW SHATTERED IN FLIGHT. REPLACED WINDSHIELD.
- [SDR DL733020205](https://openairdocs.org/sdr/DL733020205), Feb 16, 2002: BATTERY. DISCHARGED. EMERGENCY EVACUATION LIGHTING DIM IN CABIN AISLE BETWEEN ROWS 11 AND 24. REPLACED BATTERY FOR CABIN LIGHTING SYSTEM.
- [SDR DL733020187](https://openairdocs.org/sdr/DL733020187), Feb 14, 2002: WARNING LIGHT. FALSE INDICATION. ON APPROACH TO LANDING HAD UNSAFE GEAR INDICATION. NO GREEN LIGHTS AND ONLY NOSE GEAR RED UNSAFE. JACKED AIRCRAFT AND CYCLED GEAR. UNABLE TO DUPLICATE.
- [SDR DL733011559](https://openairdocs.org/sdr/DL733011559), Sep 18, 2001: BATTERY. DISCHARGED. LT AFT DOOR EXT EMER LIGHT INOP REPLCED BATT. OP CKS GOOD
- [SDR DL733011558](https://openairdocs.org/sdr/DL733011558), Sep 18, 2001: BATTERY. DISCHARGED. AFT RT OVER DOOR EMER LIGHT REPLCD PWR SUPPLY AND BATT. OPS CKS GOOD
- [SDR DL733011557](https://openairdocs.org/sdr/DL733011557), Sep 18, 2001: POWER SUPPLY. DEFECTIVE. AFT CABIN EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED PWR SUPPLY AND BATTERY, OP CKS GOOD.
- [SDR DL733011477](https://openairdocs.org/sdr/DL733011477), Sep 4, 2001: MEGAPHONE. INOPERATIVE. AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE.
- [SDR DL733011308](https://openairdocs.org/sdr/DL733011308), Aug 9, 2001: LIGHT. DAMAGED. LAV AFT RT EMERGENCY TRACK LIGHT DAMAGED , LIGHT ASSY REPLACED, CHK OK.
- [SDR DL733010985](https://openairdocs.org/sdr/DL733010985), Jun 16, 2001: A/C PACK. FAILED. AFTER T/O, A/C WILL NOT PRESSURIZE WITH LEFT PACK IN AUTO AND RT PACK ON DEFERRAL. REPAIRED RT PACK. PRESSURIZED AIRCRAFT, OK FOR SERVICE.
- [SDR DL733010932](https://openairdocs.org/sdr/DL733010932), Jun 8, 2001: SKIN. CRACKED. DOOR SKIN CRACKED N/R 123 C-1 CK OPN 8727 IN DFW. ITEM:R-1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT AT AFT UPPER AND LOWER CORNERS. STOP DRILLED AND REMOVED CRAC
- [SDR DL733010933](https://openairdocs.org/sdr/DL733010933), Jun 7, 2001: SKIN. CRACKED. DOOR SKIN CRACKED N/R 122 C-1 CK OPN 8727 IN DFW. ITEM: R-1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT AT LOWER AFT CORNER.
- [SDR DL733010698](https://openairdocs.org/sdr/DL733010698), May 2, 2001: FRAME. CRACKED. A CRACK WAS FOUND IN THE LT SIDE CHORD OF THE FS 178 BLKHD. THE DAMAGE WAS REPAIRED PER S/B 737-53-1173 SECTION IX. THE CRACK WAS FOUND DURING THE AD INSPECTION
- [SDR DL733010421](https://openairdocs.org/sdr/DL733010421), Mar 14, 2001: SKIN. PUNCTURED. THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BETWEEN FS 312 & 331 AND BETWEEN STRINGERS 21R & 22R. THE DAMAGE WAS REMOVED WITH A 17 INCH X 6 INCH CUTOUT. T
- [SDR DL733001971](https://openairdocs.org/sdr/DL733001971), Oct 10, 2000: MEGAPHONE. INOPERATIVE. FIRST CLASS MEGAPHONE INOP ON LAYOVER CHECK IN STL. REPLACED SAME.
- [SDR DL733001080](https://openairdocs.org/sdr/DL733001080), Jun 2, 2000: SENSOR. FAILED. B-SYSTEM A/P APPROACHING FL 350, RAPID ROLL LEFT, DISCONNECTED AT FL 350, RE-ENGAGED B A/P, SLOWLY ROLLED RT DISCONNECTED, ENGAGED A A/P. ALSO, UNCOMMANDED SLOW
- [SDR DL733000882](https://openairdocs.org/sdr/DL733000882), May 3, 2000: BULKHEAD. CRACKED. THE STATION 178 BULKHEAD WEB WAS FOUND TO BE CRACKED AT WL 213 NEAR LBL 5.7. THE RESULTING CUTOUT MEASURED APPROX 1 INCH UP/DOWN BY 1 INCH I/B - O/B. CORRECTIVE
- [SDR DL733000811](https://openairdocs.org/sdr/DL733000811), Apr 25, 2000: BULKHEAD. CRACKED. STA 178 BULKHEAD WEB FOUND CRACKED AT WL 213 NEAR LBL 5.7. RESULTING CUTOUT MEASURED APPROXIMATELY 1 UP/DOWN BY 1 INBOARD/OUTBOARD. ER/A 334374-14AD.
- [SDR DL733000505](https://openairdocs.org/sdr/DL733000505), Mar 13, 2000: MASK. DEPLOYED. PASSENGER OXYGEN MASKS DROPPED, BY ACCIDENT, BY FLT CREW WHILE AT GATE. INSPECTED AND STOWED ALL MASKS PER MM. PAX SEATS 23 ABE AND 27 DEF MASKS DID NOT DEPLOY 
- [SDR DL733000336](https://openairdocs.org/sdr/DL733000336), Feb 18, 2000: RELAY. MALFUNCTIONED. TAKEOFF CONFIGURATION WARNING CAME ON DURING TAKEOFF ROLL WITH AIRCRAFT CONFIGURED CORRECTLY. REPLACED R2-238 AND R2-239 RELAYS. INSPECTED SWITCHES S-130, S-132
- [SDR DL733992790](https://openairdocs.org/sdr/DL733992790), Dec 18, 1999: TRANSMITTER. MALFUNCTIONED. SPLIT FLAP INDICATION AT 1 DEGREE FLAPS DURING DESCENT. MADE 1 DEGREE FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED CHECK OUT PER M/M CHAP 27

All 55: https://openairdocs.org/model/boeing-737-35b/reports.md

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