# Boeing 737-2P6

- Type: Aircraft model (FAA registry)
- Registry code: 1384609
- Manufacturer (registry): BOEING
- Model: 737-2P6
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 100
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-737-2p6

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 (200, newest 50)

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

- [SDR TSAA0777056](https://openairdocs.org/sdr/TSAA0777056), Oct 15, 2007: CONNECTOR. MISINSTALLED. NON-ETOPS FLIGHT 278 HNL-KOA, ON TAKEOFF AFTER THROTTLE ADVANCE, THE CREW NOTED THE NR 1 EPR AT 2.22 AND THE NR 2 EPR AT 1.74. THE CREW ABORTED THE TAKEOFF AT 1
- [SDR TSAA0773051](https://openairdocs.org/sdr/TSAA0773051), Sep 20, 2007: FUEL CONTROL. FAILED. NON-ETOPS FLIGHT 90 HNL-KOA, ON TAKEOFF ROLL, THE CREW NOTED THE NR 2 EGT CLIMBING FASTER THAN THE NR 1 EGT. ABORTED THE TAKEOFF AT 100 KTS INDICATED AIRSPEED D
- [SDR TSAA0629097](https://openairdocs.org/sdr/TSAA0629097), Nov 7, 2006: TRANSMITTER. FAILED. NON-ETOPS FLT 68 HNL-ITO: DURING CLIMB, THE CREW NOTED THAT THE HYDRAULIC A-SYSTEM PRESSURE GAUGE READ 800 PSI. THE CREW RETURNED TO FIELD AND LANDED IN WITHOUT
- [SDR TSAA0632091](https://openairdocs.org/sdr/TSAA0632091), Oct 24, 2006: LIGHT. INOPERATIVE. FLT 244 HNL-OGG - DURING APPROACH, CREW NOTED THE LEFT LANDING GEAR GREEN LIGHT WOULD NOT ILLUMINATE WITH THE LANDING GEAR LEVER SELECTED IN THE DOWN POSITION. 
- [SDR TSAA0632072](https://openairdocs.org/sdr/TSAA0632072), Aug 19, 2006: LIGHT. INOPERATIVE. NON-ETOPS FLT 226 LIH-HNL: DURING TAKEOFF, CREW NOTED RED NOSE GEAR WARNING LIGHT NOT ILLUMINATED. THE CREW RE-LAMPED THE NOSE GEAR WARNING LIGHT. AIRCRAFT LAND
- [SDR TSAA0632071](https://openairdocs.org/sdr/TSAA0632071), Aug 19, 2006: LIGHT. INOPERATIVE. ON APPROACH, CREW NOTED GREEN NOSE GEAR DOWN LIGHT NOT ILLUMINATED. THE CREW PERFORMED A GO-AROUND AND RE-LAMPED THE NOSE GEAR DOWN LIGHT. AIRCRAFT LANDED IN LI
- [SDR TSAA0621038](https://openairdocs.org/sdr/TSAA0621038), May 20, 2006: LINE. MISINSTALLED. PACK TRIP OFF AFTER T/O. BURNING RUBBER SMELL AND PRESSURE BUMP ON T/O AND LANDING. REMOVED & REPLACED RIGHT A/C BAY FLOW CONTROL VALVE, OPS AND LEAK CHECK OK. 
- [SDR TSAA0672037](https://openairdocs.org/sdr/TSAA0672037), May 12, 2006: ENGINE. MALFUNCTIONED. ON DESCENT THE CREW ADVANCED THE THROTTLES AND HEARD 3 LOAD BANG SOUNDS FROM THE NR 1 ENGINE. THERE WERE NO ABNORMAL ENGINE INDICATIONS. CREW RETARDED THROTTLES
- [SDR TSAA0632036](https://openairdocs.org/sdr/TSAA0632036), May 11, 2006: STRUT. LOW. DURING CRUISE THE CREW NOTED THAT THE RIGHT MAIN GEAR INDICATION LIGHTS ILLUMINATED BOTH GREEN AND RED (UNSAFE CONDITION). THE CREW MOVED THE LANDING GEAR SELEC
- [SDR F3LA200200384](https://openairdocs.org/sdr/F3LA200200384), Nov 1, 2002: STUD. LOOSE. DURING CLIMBOUT, THE FLIGHT CREW REPORTED THE NUMBER ONE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY WAS SHOWN AT ZERO. THE AIRCRAFT RETURNED TO 
- [SDR F3LA200200253](https://openairdocs.org/sdr/F3LA200200253), Aug 28, 2002: SKIN. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS, OUTBOARD OF MAIN TRACK. REMOVED DAMAGE, FABRICATED AND INSTALL
- [SDR F3LA200200195](https://openairdocs.org/sdr/F3LA200200195), Jul 5, 2002: STRUCTURE. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON RUDDER BULLNOSE BY NR 3 HINGE. REPLACED CORRODED AREA OF RUDDER BULLNOSE PER SRM 51-40-02 AND BOEING DRAWING 
- [SDR F3LA200200194](https://openairdocs.org/sdr/F3LA200200194), Jul 5, 2002: STRAP. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON STRAP AT BS 857, RBL 18. REPLACED STRAP PER SRM 51-30-5 AND 51-30-2.
- [SDR F3LA200200193](https://openairdocs.org/sdr/F3LA200200193), Jul 5, 2002: SILL. CRACKED. DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER 
- [SDR F3LA200200192](https://openairdocs.org/sdr/F3LA200200192), Jul 5, 2002: SILL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SEAL AND THRESHOLD SUPPORT. REMOVED CORROSION PER SRM 53-10-01 AND INSTALLED NEW MOP SEAL PER SRM
- [SDR F3LA200200191](https://openairdocs.org/sdr/F3LA200200191), Jul 5, 2002: ANGLE. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR ANGLE INBD OF R1 GUTTER AT BS 336, RBL 54. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLES PER BOEI
- [SDR F3LA200200188](https://openairdocs.org/sdr/F3LA200200188), Jul 4, 2002: SEAT TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TWO SEAT TRACKS BETWEEN BS 947 AND BS 967, RBL 11.50. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM
- [SDR F3LA200200187](https://openairdocs.org/sdr/F3LA200200187), Jul 3, 2002: SEAT TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF SEAT TRACK BETWEEN BS 947 AND BS 967, RBL 36.5. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SR
- [SDR F3LA200200185](https://openairdocs.org/sdr/F3LA200200185), Jul 2, 2002: SEAT TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR TRACK, STA 797 TO 809, RBL 14. REPLACED CARGO FLOOR TRACK PER SRM 51-30-02.
- [SDR F3LA200200182](https://openairdocs.org/sdr/F3LA200200182), Jul 2, 2002: FLOORBEAM. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 987.5, RBL 36 TO RBL 40. REPLACED FLOORBEAM PER SRM 53-10-9, FIG 3.
- [SDR F3LA200200181](https://openairdocs.org/sdr/F3LA200200181), Jul 2, 2002: FLOORBEAM. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA. 947.5, RBL 38 TO RBL 43.75. REPAIRED FLOOR BEAM PER SRM 53-10-9.
- [SDR F3LA200200189](https://openairdocs.org/sdr/F3LA200200189), Jul 1, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN BS 947 AND BS 967, FROM RBL 11.50 TO RBL 36.50. FABRICATED AND INSTALLED REPLAC
- [SDR F3LA200200186](https://openairdocs.org/sdr/F3LA200200186), Jul 1, 2002: FLOORBEAM. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOOR BEAM AT STA. 947.5, RBL 38. REPAIRED FLOOR BEAM PER SRM 53-10-9.
- [SDR F3LA200200184](https://openairdocs.org/sdr/F3LA200200184), Jul 1, 2002: SILL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR OPENING LOWER WEB SILL. REPLACED CARGO WEB SILL PER SRM 51-30-2.
- [SDR F3LA200200183](https://openairdocs.org/sdr/F3LA200200183), Jul 1, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED BETWEEN STA 967 TO 987.5, RBL 20. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-
- [SDR F3LA200200179](https://openairdocs.org/sdr/F3LA200200179), Jul 1, 2002: SILL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SILL AND THRESHOLD SUPPORT. REMOVED CORROSION ON MOP SILL AND FOUND TO BE OUT OF LIMITS PER SRM 5
- [SDR F3LA200200180](https://openairdocs.org/sdr/F3LA200200180), Jul 1, 2002: SILL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 51-40-
- [SDR F3LA200200178](https://openairdocs.org/sdr/F3LA200200178), Jul 1, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 967 AND 987.5, LBL 18. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT P
- [SDR F3LA200200177](https://openairdocs.org/sdr/F3LA200200177), Jul 1, 2002: FLOOR SUPPORT. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 987.5 AND 1006, BL 0. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PE
- [SDR F3LA200200176](https://openairdocs.org/sdr/F3LA200200176), Jun 29, 2002: GUSSET. GOUGED. DURING C-2 CHECK, INSPECTION REPORTED MULTIPLE GOUGES IN NR 1 ENGINE OTBD COWLING LOWER CHORD AND GUSSET AT SECOND LATCH FITTING FROM FWD SIDE OF COWL. REMOVED 
- [SDR F3LA200200175](https://openairdocs.org/sdr/F3LA200200175), Jun 25, 2002: SKIN. DENTED. DURING C-2 CHECK, INSPECTION REPORTED DENT IN AFT CARGO DOOR AT TOP OF DOOR. CUT OUT DAMAGE PER SRM 52-00-3. REMOVED STIFFENER PER SRM 51-30-02. FABRICATED DOUB
- [SDR F3LA200200174](https://openairdocs.org/sdr/F3LA200200174), Jun 25, 2002: INTERCOSTAL. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 500A TO 500B, RBL 25. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 
- [SDR F3LA200200173](https://openairdocs.org/sdr/F3LA200200173), Jun 25, 2002: CARGO TRACK. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO TRACK TIE DOWN SOCKET AT STA 947, LBL 17. REMOVED SECTION OF CARGO TRACK IN AFT BAY AT LBL 17 FROM STA 
- [SDR F3LA200200164](https://openairdocs.org/sdr/F3LA200200164), Jun 5, 2002: SKIN. DELAMINATED. ON WALKAROUND, FLIGHT CREW REPORTED LT ELEVATOR DELAMINATED ON TRAILING EDGE. REPAIRED PER SRM 51-40-9, PARAGRAPH 4 AND EA 55-737-063.
- [SDR F3LA200200118](https://openairdocs.org/sdr/F3LA200200118), Mar 23, 2002: LIGHT. INOPERATIVE. MAINTENANCE REPORTED EMERGENCY PATH LIGHTING AT ROW 1 INOPERATIVE AND EXPOSED WIRES NEAR ROW 16. REPLACED AISLE PATH LIGHT SOCKET AND LENS AT ROW 1 AND REPAIRIN
- [SDR F3LA200100112](https://openairdocs.org/sdr/F3LA200100112), Oct 4, 2001: ENGINE. OUT OF RIG. ABORTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE WOULD ONLY PRODUCE 2.0 EPR OF THE REQUIRED 2.05. PUSHED RT THROTTLE ALMOST TO FWD STOP WITH NO FURTHER THRUST.
- [SDR F3LA200100096](https://openairdocs.org/sdr/F3LA200100096), Jul 16, 2001: BATTERY PACK. DISCHARGED. PRIOR TO DEPARTURE, MAINTENANCE REPORTED BOTH EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING THE SYSTEM. AN ADDEND
- [SDR F3LA200100076](https://openairdocs.org/sdr/F3LA200100076), Jun 4, 2001: FITTING. LOOSE. REJECTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE EGT EXCEEDED RED RADIAL. AN ADDENDUM WILL BE ISSUED WHEN CAUSE OF FAILURE AND CORRECTIVE ACTION IS KNOWN. ADD
- [SDR F3LA200100054](https://openairdocs.org/sdr/F3LA200100054), Apr 23, 2001: POWER SUPPLY. DISCHARGED. PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. REPLACED FWD EMERGENCY AISLE PATH LIGHTING POWER SUPPLY.
- [SDR F3LA200100051](https://openairdocs.org/sdr/F3LA200100051), Mar 30, 2001: ANGLE. CRACKED. DURING C-1 CHECK, INSPECTION REPORTED CRACK IN ANGLE, VERTICAL STABILIZER AT APPROXIMATELY RUDDER STA 86.59. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES 
- [SDR F3LA200100047](https://openairdocs.org/sdr/F3LA200100047), Mar 20, 2001: SKIN. DENTED. DURING C1 CHECK, INSPECTION REPORTED 2 DENTS ON RIGHT FUSELAGE SKIN AT STA 1016, STR 20R. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED FILLER, REPAIRED DOUBLER,
- [SDR F3LA200100045](https://openairdocs.org/sdr/F3LA200100045), Mar 15, 2001: DOOR. CORRODED. DURING C-1 CHECK, INSPECTION REPORTED RT UPPER FWD CORNER OF E&E DOOR CORRODED. MAINTENANCE REMOVED CORROSION AND PERFORMED A WEB REPAIR PER SRM 51-40-02.
- [SDR F3LA200000275](https://openairdocs.org/sdr/F3LA200000275), Dec 26, 2000: ENGINE. STALLED. REJECTED TAKEOFF. FLIGHT CREW REPORTED HEARING TWO "BANGS" WHICH WAS THOUGHT TO BE A COMPRESSOR STALL AND ABORTED TAKEOFF AT 50 KNOTS WITHOUT INCIDENT. CREW COU
- [SDR F3LA200000273](https://openairdocs.org/sdr/F3LA200000273), Dec 17, 2000: STRUT. COLLAPSED. AIR TURNBACK. FLIGHT CREW REPORTED LT. MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH WITH GEAR HANDLE IN "UP" POSITION. RED UNSAFE AND GREEN GEAR LIGHT IL
- [SDR F3LA00239](https://openairdocs.org/sdr/F3LA00239), Sep 12, 2000: GIRT BAR. WRONG PART. FLT 430 - BLOCK TURN BACK, FLIGHT CREW REPORTED LEFT AFT EVACUATION SLIDE GIRT BAR WOULD NOT LOCK IN PLACE. MAINTENANCE INSTALLED CORRECT GIRT BAR PER MM 25-61-
- [SDR F3LA00114](https://openairdocs.org/sdr/F3LA00114), May 31, 2000: LIGHT. INOPERATIVE. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY FLOOR PROXIMITY LIGHT PATH STRIP INOPERATIVE AND TRACK DAMAGED AT ROW 1 THROUGH ROW 3. MAINTENANCE RE
- [SDR F3LA00093](https://openairdocs.org/sdr/F3LA00093), May 17, 2000: LINE. LEAKING. LAS - FLT 778 - AIR TURN BACK. FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE 
- [SDR F3LA99157](https://openairdocs.org/sdr/F3LA99157), Nov 22, 1999: SKIN. CORRODED. DEN - DURING C-7 CHECK INSPECTION, REPORTED FORWARD TIP OF RIGHT STABILIZER CORRODED. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER EA NR 55-737-010
- [SDR F3LA99164](https://openairdocs.org/sdr/F3LA99164), Nov 21, 1999: STRINGER. CORRODED. DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 987 TO BS 987.5. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-3
- [SDR F3LA99137](https://openairdocs.org/sdr/F3LA99137), Nov 12, 1999: ANGLE. CORRODED. DEN - DURING C-7 CHECK, INSPECTION REPORTED RIGHT FORWARD SERVICE DOOR INBOARD THRESHOLD SUPPORT ANGLE CORRODED. MAINTENANCE FABRICATED AND REPAIRED RIGHT FORWA

All 200: https://openairdocs.org/model/boeing-737-2p6/reports.md

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