# Boeing 737-2M6C - Type: Aircraft model (FAA registry) - Registry code: 138449G - Manufacturer (registry): BOEING - Model: 737-2M6C - 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-737-2m6c 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 (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19910518021819I](https://openairdocs.org/incident/19910518021819I), May 18, 1991: Boeing 7372M6C (N805AL), Honolulu, HI, Minor damage. Left main outboard tire blew on takeoff. Continued to destination. Landed without incident. ## Service difficulty reports (144, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR TSAA0632027](https://openairdocs.org/sdr/TSAA0632027), Mar 29, 2006: CIRCUIT CARD. MALFUNCTIONED. FERRY FLIGHT 320 HNL-MHV - AFTER TAKEOFF AND GEAR UP, CREW HAD UNSAFE LANDING GEAR INDICATION. CREW LOWERED THE LANDING GEAR AND RETURNED TO HNL WITHOUT FURTHER - [SDR TSAA0532049](https://openairdocs.org/sdr/TSAA0532049), Oct 18, 2005: BRAKE. INOPERATIVE. PILOTS OBSERVED BOTH ANTI-SKID LIGHTS CAME ON IN FLIGHT ONLY WHEN THE LANDING GEAR IS IN THE (OFF) POSITION; LANDED WITH NO DIFFICULTIES. REMOVED AND REPLACED P - [SDR TSAA0426077](https://openairdocs.org/sdr/TSAA0426077), Nov 15, 2004: CONNECTOR. DAMAGED. FLT 942, HNL-KOA: (NON-ETOPS) AFTER ENGINES WERE STARTED, THE NR 2 ENGINE FIRE WARNING SWITCH AND BELL CAME ON. FOLLOWED THE QRH AND SHUT DOWN THE ENGINE. REPLA - [SDR TSAA0427072](https://openairdocs.org/sdr/TSAA0427072), Sep 20, 2004: WARNING LIGHT. ILLUMINATED. NON-ETOPS CARGO FLIGHT 909, HNL-LIH, ON CLIMB-OUT PASSING 2000-3000 FT, THE FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON. RETURNED TO HNL. BLEW OUT ELEVATOR PITOT T - [SDR TSAA0429071](https://openairdocs.org/sdr/TSAA0429071), Sep 20, 2004: HYDRAULIC SYSTEM. CONTAMINATED. NON-ETOPS CARGO FLIGHT 909, HNL-LIH: ON CLIMB-OUT PASSING 1500 FT THE FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. RETURNED TO HNL. REPLACED THE B HYDRAULIC SY - [SDR TSAA0427042](https://openairdocs.org/sdr/TSAA0427042), May 29, 2004: CONTROL CABLE. OUT OF ADJUST. AT 34,000 FT DURING CRUISE THE L/E FLAP TRANSIT LIGHT CAME ON, AUTO-PILOT KICKED OFF AND ON DESCENT THE CONFIGURATION HORN CAME ON. RETURNED TO HNL. ADJUST FLAP - [SDR TSAA0453023](https://openairdocs.org/sdr/TSAA0453023), Jan 20, 2004: DOOR FRAME. CRACKED. FOUND CRACK ON LOWER INBOARD CORNER OF FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. VERIFIED CRACK REMOVED USING HFEC INSPECTION. FABRICATED A REPAIR ANG - [SDR TSAA0330154](https://openairdocs.org/sdr/TSAA0330154), Jun 25, 2003: SHUTOFF VALVE. DEFECTIVE. FLT 952 - HNL-ITO, NR 2 ENGINE COWL ENGINE ICE LIGHT REMAINS ON IN TRANSITION (BRIGHT BLUE). RETURNED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR - [SDR TSAA0333113](https://openairdocs.org/sdr/TSAA0333113), May 3, 2003: BATTERY PACK. INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCAFT RETURNED TO SERVICE. (M) - [SDR TSAA0379039](https://openairdocs.org/sdr/TSAA0379039), Feb 23, 2003: SWITCH. INOPERATIVE. DURING CLIMB, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED I - [SDR TSAA0353016](https://openairdocs.org/sdr/TSAA0353016), Feb 4, 2003: SKIN. CORRODED. TRIMMED OUT DAMAGE SKIN AT BS 918 ABOVE STRINGER 25R. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY .04 INCH INSURANCE CUT. NDT INSPECTED THE OUTER ROW - [SDR TSAA0353007](https://openairdocs.org/sdr/TSAA0353007), Feb 4, 2003: SKIN. CORRODED. REMOVED DAMAGED SKIN AND STRINGERS 26L, 27L, AND 27R BETWEEN BS 908 AND BS 1016. REPLACED SKIN PANEL PER PRODUCTION DRAWINGS 65-45776-55 AND 65-45776-56. INSTAL - [SDR TSAA0353017](https://openairdocs.org/sdr/TSAA0353017), Feb 4, 2003: SKIN. CORRODED. TRIMMED OUT DAMAGE SKIN AT BS 947.5 ABOVE STRINGER 25L. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY .040 INCH INSURANCE CUT. NDT INSPECTED THE OUTE RO - [SDR TSAA0353011](https://openairdocs.org/sdr/TSAA0353011), Jan 30, 2003: STRINGER. CORRODED. TRIMMED OUT DAMAGE STRINGER SECTION. FABRICATED A .090 INCH THICK J AND U-CHANNEL FROM 7075-T6. ALODINED AND APPLIED TWO COATS PRIMER TO ALL BARE ALUMINUM. INST - [SDR TSAA0353004](https://openairdocs.org/sdr/TSAA0353004), Jan 30, 2003: STRINGER. CRACKED. EXTERIOR 1 INCH FUSELAGE CRACK AT BS 375 AT STRINGER 15L. TRIMMED OUT DAMAGE. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIMMED AREA BY .040 INCH INSURANCE - [SDR TSAA0353003](https://openairdocs.org/sdr/TSAA0353003), Jan 29, 2003: SKIN. CRACKED. EXTERIOR 1 INCH CRACK BETWEEN BS 440 AND BS 460 AT BL 0. TRIMMED OUT DAMAGED AREA ON LOWER LOBE ANTENNA CUT OUT. PERFORMED NDT INSPECTION OF CUTOUT, SKIN AND SA - [SDR TSAA0353005](https://openairdocs.org/sdr/TSAA0353005), Jan 20, 2003: STRINGER. CRACKED. TWO RIVETS SHOW CRACK INDICATIONS USING LFEC AT BS 227.8 STRINGER 27R. REMOVED ADJACENT FASTENERS AND STRINGER. USING HFEC CONFIRMED NO CRACK INDICATION USING R - [SDR TSAA0226197](https://openairdocs.org/sdr/TSAA0226197), Sep 22, 2002: PITOT TUBE. OBSTRUCTED. FLT 930 - HNL-OGG - DURING THE CLIMB-OUT OF HNL, THE FIRST OFFICERS AIR SPEED INDICATOR WAS INDICATING 40 KNOTS SLOWER THAN THE CAPTAIN'S INDICATOR. THE AIRCRAF - [SDR TSAA0251185](https://openairdocs.org/sdr/TSAA0251185), Aug 13, 2002: FRAME. CRACKED. CRACK LOCATED AT BS 807, S-14L. CUT AND REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL UTILIZING HFEC METHOD NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR ANG - [SDR TSAA0251190](https://openairdocs.org/sdr/TSAA0251190), Aug 13, 2002: FRAME. CRACKED. TEAR STRAP FASTENER HOLE CRACK AT BS 777, S-20L. REMOVED FASTENER AND VERIFIED CRACK UTILIZING HFEC ROTARY HOLE PROBE METHOD IAW WITH NDT, REMOVED DAMAGED AREA - [SDR TSAA0251189](https://openairdocs.org/sdr/TSAA0251189), Aug 13, 2002: STIFFENER. CRACKED. LT WING FRONT SPAR STIFFENER CRACK AT FSS 473.31 AND FSS 475.55. REMOVED, FABRICATED AND INSTALLED STIFFENERS. NEW STIFFENERS FABRICATED FROM 7178-T6511 EXTRUSI - [SDR TSAA0251188](https://openairdocs.org/sdr/TSAA0251188), Aug 13, 2002: WINDOW FRAME. CRACKED. RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 727B. VERIFIED CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTAR PROBE METHOD, REAMED WINDOW FRAME FASTEN - [SDR TSAA0251187](https://openairdocs.org/sdr/TSAA0251187), Aug 13, 2002: WINDOW FRAME. CRACKED. RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 380. CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTARY PROBE METHOD, REAMED WINDOW FRAME FASTENER HOLE U - [SDR TSAA0251186](https://openairdocs.org/sdr/TSAA0251186), Aug 13, 2002: SKIN. CRACKED. RT BS 1129 AND BS 1138 FUSELAGE SKIN CRACKS LOCATED AT S5R AND S12R. TRIMMED OUT CRACKS MAINTAINING A MINIMUM TRIM OUT CORNER RADIUS .050 INCHES AT A SURFACE FI - [SDR TSAA0253144](https://openairdocs.org/sdr/TSAA0253144), Jun 1, 2002: FRAME. CRACKED. REPAIRED RIGHT OUTBOARD CHORD AT BS727, S18A DUE TO FASTENER HOLE CRACK. UTILIZED HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC METHODS. REMOVED AND INSTALLED CHOR - [SDR TSAA0251145](https://openairdocs.org/sdr/TSAA0251145), May 20, 2002: SKIN. CRACKED. REPAIRED FUSELAGE SKIN CRACK AT BS 727B, S-17. CUT OUT DAMAGED AREA AND PERFORMED HFEC INSPECTION AROUND CUT OUT, PERFORMED INSURANCE CUT OF .040 INCH, FABRICAT - [SDR TSAA0251140](https://openairdocs.org/sdr/TSAA0251140), May 20, 2002: FRAME. CRACKED. FOUND CRACK ON THE FRAME AT BS 480 ABOVE STRINGER 17R. CUT OUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. VERIFIED CUTOUT WITH HFEC. DETERMINED FROM TABLES - [SDR TSAA0233117](https://openairdocs.org/sdr/TSAA0233117), Apr 24, 2002: BATTERY PACK. DISCHARGED. REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0253105](https://openairdocs.org/sdr/TSAA0253105), Apr 6, 2002: SKIN. CRACKED. FOUND 3 INCH CRACK ON THE FUSELAGE SKIN AT BS 887 ALONG STRINGER 24R. CUT OUT DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC. FABRICATED AND INSTALL - [SDR TSAA0253059](https://openairdocs.org/sdr/TSAA0253059), Mar 1, 2002: SKIN. CORRODED. FOUND SKIN BULGE ON RIGHT SIDE VERTICAL FIN RIGHT SPAR AT FWL 112.356. FABRICATED REPAIR ANGLE, EXTERNAL DOUBLER, TWO FS 173.10 IN SPAR RIB CLIPS, REPLACEMENT F - [SDR TSAA0253060](https://openairdocs.org/sdr/TSAA0253060), Mar 1, 2002: SPAR. CRACKED. FOUND CRACK IN THE VERTICAL STABILIZER IN SPAR WEB ON THE VERTICAL STABILIZER. TRIMMED OUT CRACK IAW FIGURE 2. FABRICATED A REPAIR DOUBLER AND A FILLER AS SHOWN - [SDR TSAA0255025](https://openairdocs.org/sdr/TSAA0255025), Jan 14, 2002: SPAR. NICKED. FOUND NICKS ON CENTER SECTION REAR SPAR UPPER FORWARD SIDE FITTING. REMOVED NICKS/DAMAGED MATERIAL TO A MAXIMUM OF .01 INCH AND TAPERED. APPLIED A CHEMICAL CONV - [SDR TSAA0255024](https://openairdocs.org/sdr/TSAA0255024), Jan 14, 2002: ATTACH FITTING. GOUGED. FOUND GOUGE MARKS ON LEFT HORIZONTAL STABILIZER CENTER SECTION LUG, UPPER FORWARD FITTING. REMOVED GOUGE / DAMAGED MATERIAL TO A MINIMUM WIDTH OF .10 INCH AND R - [SDR TSAA0133165](https://openairdocs.org/sdr/TSAA0133165), Dec 1, 2001: BATTERY PACK. INOPERATIVE. REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0126118](https://openairdocs.org/sdr/TSAA0126118), Sep 16, 2001: FIRE WARNING. FALSE ACTIVATION. FLT - 117 - HNL-LIH - ON SHORT FINAL LANDING IN LIHUE, HI, THE APU WAS STARTED AND FOLLOWED BY AN ILLUMINATION OF THE APU FIRE WARNING HANDLE, THE SOUNDING OF T - [SDR TSAA0153077](https://openairdocs.org/sdr/TSAA0153077), Jun 18, 2001: SPAR. CORRODED. FOUND CORROSION DURING HEAVY CHECK AT RIGHT WING FRONT SPAR LOWER CHORD FORWARD FLANGE LOWER SURFACE AT FSS 476.0 THROUGH FSS 481.7. (M) - [SDR TSAA0153075](https://openairdocs.org/sdr/TSAA0153075), Jun 15, 2001: BEAR STRAP. CORRODED. DISCOVERED CORROSION AT FORWARD CARGO DOOR BEAR STRAP (AFT UPPER CORNER). (M) - [SDR TSAA0153076](https://openairdocs.org/sdr/TSAA0153076), Jun 15, 2001: SKIN. CRACKED. FOUND .62 INCH CRACK DURING HEAVY CHECK AT RIGHT UPPER WING SKIN AFT EDGE BETWEEN WBL 157 AND WBL 183.4. (M) - [SDR TSAA0133022](https://openairdocs.org/sdr/TSAA0133022), Feb 22, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0133016](https://openairdocs.org/sdr/TSAA0133016), Feb 16, 2001: BATTERY PACK. DISCHARGED. REPLAED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0153012](https://openairdocs.org/sdr/TSAA0153012), Feb 9, 2001: FRAME. CRACKED. FOUND IDENTIFIED CRACK AT BS 727, STRINGER 18L UPPER CHORD BY UTILIZING HFEC METHOD. (M) - [SDR TSAA0033243](https://openairdocs.org/sdr/TSAA0033243), Dec 14, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033224](https://openairdocs.org/sdr/TSAA0033224), Oct 27, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0053219](https://openairdocs.org/sdr/TSAA0053219), Sep 12, 2000: FRAME. CRACKED. PREVENTIVE MODIFICATION INCORPORATED INCONJUNCTION WITH CRACK REPAIR AT BS 480 INNER FRAME FLANGE. REPAIR INCLUDED TRIM OUT OF CRACK, HFEC INSPECTION OF TRIM OU - [SDR 20001012AP002](https://openairdocs.org/sdr/20001012AP002), Jun 28, 2000: SEAL. WORN. FLT 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING BODY OVERHEAT LIGHT ON. LIGHT WENT OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOSED - [SDR TSAA0026160](https://openairdocs.org/sdr/TSAA0026160), Jun 28, 2000: CLAMP. WORN. FLT - 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING-BODY OVERHEAT LIGHT ON. LIGHT WETN OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOS - [SDR TSAA0033154](https://openairdocs.org/sdr/TSAA0033154), Jun 24, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY POWER PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033153](https://openairdocs.org/sdr/TSAA0033153), Jun 23, 2000: BATTERY PACK. INOPERATIVE. REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER POWER PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0053127](https://openairdocs.org/sdr/TSAA0053127), Apr 26, 2000: STRINGER. CRACKED. REPAIRED 1.75 INCH CRACK AT STRINGER 16L APPROX 4 INCHES AFT OF BS 727 AND 2 INCH CRACK AT STRINGER 17L APPROX 7 INCHES AFT OF BS 727 CONFIRMED BY USING HIGH FR - [SDR TSAA0033122](https://openairdocs.org/sdr/TSAA0033122), Apr 24, 2000: BATTERY PACK. INOPERATIVE. REPLACED FORWARD OVERHEAD EXIT IDENTIFIER BATTERY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) All 144: https://openairdocs.org/model/boeing-737-2m6c/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.