# Boeing 737-2T5 - Type: Aircraft model (FAA registry) - Registry code: 1384474 - Manufacturer (registry): BOEING - Model: 737-2T5 - 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-737-2t5 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 (39) As reported by operators and repair stations, by the model named in the report. - [SDR CA030417011](https://openairdocs.org/sdr/CA030417011), Apr 15, 2003: PCU. INOPERATIVE. (CAN) AFTER PUSHBACK AND START, FLAP 2 SELECTED AND HYDRAULIC SYSTEM A LOW PRESSURE ILLUMINATED AND HYD QTY GUAGE DECREASED TO ZERO. MAINTENANCE FOUND THE A SYS - [SDR CA030225003](https://openairdocs.org/sdr/CA030225003), Feb 23, 2003: OXYGEN MASK. MISINSTALLED. (CAN) A/C EXPERIENCED RAPID DEPRESSURIZATION. CLIMBED TO 15,000 FT IN APPROX 5-10 SECONDS. O2 SYS DEPLOYED AUTOMATIC. STANDBY MODE DID NOT OPERATE NORMALLY BUT - [SDR CA030121007](https://openairdocs.org/sdr/CA030121007), Jan 9, 2003: BEARING. (CAN) LOG SNAG - ON FLAP SELECTION TO ONE UNIT, LE FLAP TRANSIT LIGHT REMAINED ON. NO. 4 SLAT REMAINED AMBER. ALL OTHERS GREEN. ON SELECTION OF FLAP 10, NO. 4 W - [SDR CA030106004](https://openairdocs.org/sdr/CA030106004), Jan 3, 2003: CONNECTOR. BURNED. (CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR - [SDR CA030103020](https://openairdocs.org/sdr/CA030103020), Jan 2, 2003: CONNECTOR. BURNED. (CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER O - [SDR CA030121003](https://openairdocs.org/sdr/CA030121003), Jan 1, 2003: BEARING. LOOSE. (CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING S - [SDR P2EA2001M0004](https://openairdocs.org/sdr/P2EA2001M0004), Sep 23, 2001: COMPUTER. Auto Pilot twitches in pitch on VG1. Auto Pilot pulls back on controls continuiously when operated on system "A". Corrective action: Removed and replaced Pitch - [SDR P2EA2001M0006](https://openairdocs.org/sdr/P2EA2001M0006), Sep 22, 2001: CONTROL PANEL. Heading Hold will not hold heading with Auto Pilot in B channnel. Corrective action: Deffered Heading Hold per MEL 22-1, CI#M120076 per MX CNTL Mic. Replaced Mo - [SDR P2EA2001M0003](https://openairdocs.org/sdr/P2EA2001M0003), Sep 21, 2001: GYRO. FAULTY. AUTO PILOT ON HDG2 HOLD WILL NOT MAINTAIN BANK AND ROLL LEVEL AND OCCASIONALLY JERKS ABRUPTLY. REPLACED NR 1 VERTICAL GYRO PER MM 34-22-11, OPERATIONAL CHECK OK - [SDR P2EA01167](https://openairdocs.org/sdr/P2EA01167), Aug 20, 2001: SKIN. CRACKED. SJO - DURING Q-CHECK, RIGHT WING OUTBOARD MID FLAP WBL 304.5, SKIN WITH CRACK. RIGHT WING OUTBOARD MID FLAP L/E OF CENTER TRACK CAVITY SKIN SECTION REPAIRED IAW - [SDR P2EA01162](https://openairdocs.org/sdr/P2EA01162), Aug 18, 2001: SKIN. DENTED. SJO - DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 500A PLUS 12, BETWEEN STRINGER 1 AND STRINGER 2L. REPAIRED FUSELAGE SKIN SECTION FROM BS 500A - [SDR P2EA01163](https://openairdocs.org/sdr/P2EA01163), Aug 15, 2001: CARGO TRACK. CORRODED. DURING Q-CHECK, FOUND FORWARD CARGO COMPARTMENT FROM BS 380 TO BS 520 LBL 18.5, CARGO TRACK WITH CORROSION. (M) - [SDR P2EA01164](https://openairdocs.org/sdr/P2EA01164), Aug 15, 2001: FLOOR SUPPORT. CORRODED. DURING Q-CHECK, AFT CARGO COMPARTMENT BETWEEN BS 767 AND BS 847 AT STRINGER 25 RIGHT FLOOR SUPPORT WITH CORROSION. (M) - [SDR P2EA01156](https://openairdocs.org/sdr/P2EA01156), Aug 14, 2001: DOUBLER. CRACKED. SJO - DURING Q-CHECK, EXTERNAL FUSELAGE DOUBLER WITH CRACK AT BS 1138, WL 266 LEFT SIDE. (M) - [SDR P2EA01159](https://openairdocs.org/sdr/P2EA01159), Aug 13, 2001: SKIN. CANNING. DURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWE - [SDR P2EA01158](https://openairdocs.org/sdr/P2EA01158), Aug 12, 2001: STRINGER. DENTED. SJO - DURING Q-CHECK, LOWER FUSELAGE TAIL CONE STRINGER 27 LEFT WITH DENT AT BS 1035. REPAIRED STRINGER 27 LEFT FROM BS 1032 TO BS 1045 DUE TO DENT IAW SRM 53-1 - [SDR P2EA01157](https://openairdocs.org/sdr/P2EA01157), Aug 10, 2001: BULKHEAD. CRACKED. DURING Q-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD BS 178, WEB CRACKED AT RBL 11.5-WL 213, PRESSURE BULKHEAD BS 178 FLOOR WEB SECTION CRACKE - [SDR P2EA01151](https://openairdocs.org/sdr/P2EA01151), Aug 9, 2001: FRAME. CRACKED. DURING Q-CHECK, FUSELAGE AFT CARGO COMPARTMENT AT FRAME BS 807, BETWEEN STRINGER 27 LEFT AND 27 RIGHT, LOWER SECTION WITH CRACK. S/D - REPAIRED FRAME SECTION AT - [SDR P2EA01154](https://openairdocs.org/sdr/P2EA01154), Aug 8, 2001: SKIN. DENTED. DURING Q-CHECK, FOUND EXTERNAL SKIN WITH DENT AT BS 500A PLUS 12 INCHES, BETWEEN STRINGER 1 AND 2 LEFT. (M) - [SDR P2EA01153](https://openairdocs.org/sdr/P2EA01153), Aug 8, 2001: SKIN. DENTED. DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 590, STRINGER 1. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 590 TO BS 599 BETWEEN STRINGER 2 LEFT - [SDR P2EA01150](https://openairdocs.org/sdr/P2EA01150), Aug 6, 2001: SKIN. DENTED. DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1040, BETWEEN STRINGER 27 LEFT AND 27 RIGHT. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 1030 TO B - [SDR P2EA01145](https://openairdocs.org/sdr/P2EA01145), Aug 6, 2001: SKIN. DENTED. DURING Q-CHECK, FOUND TWO DENTS RIGHT SIDE OF AFT OUT FLOW VALVE. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 922 BETWEEN STRINGER 21 RIGHT AND 23 RIGHT DU - [SDR P2EA01146](https://openairdocs.org/sdr/P2EA01146), Aug 6, 2001: SKIN. DENTED. DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1051, BETWEEN STRINGER 16 LEFT AND 17 LEFT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1047.5 TO BS 1055.5 BE - [SDR P2EA01152](https://openairdocs.org/sdr/P2EA01152), Aug 5, 2001: FLOORBEAM. CORRODED. SJO - DURING Q-CHECK, FOUND PAX CABIN AT BS 294, BETWEEN BL 0 AND RBL 40 INCHES, WL 208, UPPER SECTION AND BS 294.5 BETWEEN BL 0 AND LBL 30, FLOORBEAM WITH CORR - [SDR P2EA01149](https://openairdocs.org/sdr/P2EA01149), Aug 4, 2001: STRINGER. CORRODED. DURING Q-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 968, STRINGER 27 RIGHT WITH CORROSION. S/D - REPAIRED STRINGER 27 RIGHT FROM BS 958.5 TO BS 976 - [SDR P2EA01148](https://openairdocs.org/sdr/P2EA01148), Aug 3, 2001: SKIN. DENTED. SJO - DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 807, BETWEEN STRINGER 26 LEFT AND 27 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 789.5 TO BS 815 - [SDR P2EA01122](https://openairdocs.org/sdr/P2EA01122), Jul 7, 2001: INDICATOR. INOPERATIVE. MCI - FLT 350 - DURING CRUISE AT 33,000 FEET CABIN RATE OF CHANGE WAS PLUS 250 FEET PER MINUTE AND CABIN PRESSURE WAS AT 9,500 FEET AND SHOULD BE AT 800 FEET FO - [SDR CA010522007](https://openairdocs.org/sdr/CA010522007), May 1, 2001: CSD. UNRELIABLE. (CAN) AT FL 230, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. FLIGHT ELECTED TO RETURN DUE APU ELECTRICS WERE UNRELIABLE. REPLACED NR 1 CSD AS - [SDR CA010404008](https://openairdocs.org/sdr/CA010404008), Mar 18, 2001: WINDSHIELD. LEAKING. (CAN) CLIMBING THROUGH 13,000 FEET, APPROXIMATELY 4 PSI CABIN PRESSURE, CAPTS WINDSHIELD POPPED WITH A NOTICEABLE PRESSURIZATION LEAK. RETURNED. WINDOW INSPECTE - [SDR P2EA00221](https://openairdocs.org/sdr/P2EA00221), Jul 12, 2000: GASPER FAN. MALFUNCTIONED. FLT 307 - MYR - SMOKE AND FUMES NOTED IN COCKPIT. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO MYR LANDING UNEVENTFUL. FOUND FAULTY GASPER FAN, DEFERRED PER MEL - [SDR P2EA00212](https://openairdocs.org/sdr/P2EA00212), Jul 11, 2000: CONTROL CABLE. LOOSE. MCI - FLT 589 - EMERGENCY DECLARED, NR 1 ENGINE SHUT DOWN 5 MINUTES BEFORE LANDING, AIRCRAFT RETURNED TO MCI, LANDING UNEVENTFUL. LOST THROTTLE CONTROL NR 1 ENG - [SDR P2EA00202](https://openairdocs.org/sdr/P2EA00202), Jun 2, 2000: SKIN. DELAMINATED. YYC - DURING C-CHECK, RIGHT OUTBOARD FOREFLAP, REPAIR DELAMINATED ON UPPER SURFACE 87 INCHES OUTBOARD OF INBOARD END. REPAIRED FOREFLAP IAW SRM 51-40-6, PAGE 8 - [SDR P2EA00203](https://openairdocs.org/sdr/P2EA00203), Jun 1, 2000: SKIN. DENTED. YYC - DURING C-CHECK, FOUND DENT WITH SHARP CREASE AT BS 860, BETWEEN STRINGERS 15L AND 16L. REPAIRED DENT AT BS 860 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-30 - [SDR CA000209003](https://openairdocs.org/sdr/CA000209003), Feb 1, 2000: BOLT. BROKEN. (CAN) NR 4 SLAT BOLT BROKEN THROUGH GREASE PASSAGE DUE TO LACK OF LUBRICATION, BOLT WORN. REPLACED. - [SDR P2EA99275](https://openairdocs.org/sdr/P2EA99275), Sep 13, 1999: ENGINE. BIRD STRIKE. MDW - FLT 815 - ABORTED TAKEOFF, NO EMERGENCY DECLARED, RETURNED TO BLOCKS. AT APPROXIMATELY 100 KNOTS DURING TAKEOFF ROLL, INGESTED BIRD IN NR 1 ENGINE. (X) - [SDR CA981125024](https://openairdocs.org/sdr/CA981125024), Nov 16, 1998: SENSOR. MALFUNCTIONED. (CAN) AT TOP OF DESCENT, RT RED GEAR WARNING LIGHT FLICKERED WITH GEAR SELECTED UP. REPLACED RT MLG UPLOCK SENSOR. - [SDR CA970904013](https://openairdocs.org/sdr/CA970904013), Aug 18, 1997: ROD END BEARING. BROKEN. (CAN) ROD END BEARING SHEARED AT NECK. DETACHED FROM MAIN LANDING GEAR PANEL. REPLACED. - [SDR CA970327007](https://openairdocs.org/sdr/CA970327007), Mar 13, 1997: LINE. FAILED. (CAN) ONE HOUR OUT 'B' SYSTEM QTY LOSS, AIRCRAFT RETURNED. FOUND 'B' PUMP PRESSURE LINE FAILED. REPLACED. - [SDR CA970318002](https://openairdocs.org/sdr/CA970318002), Feb 2, 1997: BEARING. FAILED. (CAN) ON LANDING CREW REPORTED NOSE WHEEL SHIMMY. INBOARD BEARING OF THE L/H WHEEL WAS FOUND TO HAVE FAILED. THE ROLLER AND CAGE ASSEMBLY DEPARTED THE AIRCRAFT --- 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.