N11651
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
31 reports on file, 2003-06-23 – 2010-10-20.
Part: WIRE HARNESS — BROKEN (CABIN) · airframe 33,488 hrs · 17,682 cycles
EMERGENCY LIGHT OUT AT SEAT ROW 23ABC. REMOVED AND REPLACED SEAT WIRE HARNESS ASSY AT SEAT 23 ABC EMERGENCY LIGHTS CHECK GOOD IAW MM 33-51-02.
Part: SKIN — CRACKED (FUSELAGE) · airframe 32,481 hrs · 17,133 cycles
L-1 DOOR, LOWER HINGE CUTOUT, FASTENER HOLE SHOWS 2EA CRACK INDICATIONS AT APPROX 2 & 10 O'CLOCK POSITIONS IN FASTENER HOLE. FASTENER HOLE LOCATION. 3RD HOLE DOWN FROM WL 236.68 & JUST FWD OF STA 303.90. (MARKED) TRIMMED OUT DAMAGE, FABRICATED AND INSTALLED A REPAIR TRIPLER, DOUBLER COMBINATION IN REF TO ECRA 5330-04025. CREATED DIP WITH THIS NON-ROUTINE FOR REPEAT INSPECTIONS PER ECRA 5330-04025 PAGE 7. ITEM 53-DIP CNTL NR 05382 BEFORE THE ACCUMULATION OF 72,133 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSP PER PART 2 OF ECRA 5330-04025. PLANNING TO CONTACT ENGINEERING AFTER THE ACCUMULATION OF 66,000 TOTAL FLIGHT CYCLES BUT BEFORE 67,000 TOTAL FLIGHT CYCLES FOR INSP DETAILS. INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-04025, PART 1. BEFORE THE ACCUMULATION OF 72,133 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5330-04025. PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 66,000 TOTAL FLIGHT CYCLES BUT BEFORE 67,000 TOTAL FLIGHT CYCLES FOR INSP DETAILS.
Part: FRAME — DAMAGED (BS 847) · airframe 32,481 hrs · 17,133 cycles
AFT CARGO STA 847 O/B OF STR 25 RIGHT HAS TWO EACH NR 40 DRILL MARKS ON TOP OF FRAME. REPAIRED FRAME DAMAGE AT AFT CARGO STA 847 O/B OF STR 25 RIGHT.
Earlier reports · 2003–2008 · 28 reports
2008
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 907 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L & 9L. REPAIRED CRACKED FRAME AT STATION 907 PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 787 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES AT STA 787 BETWEEN STR 8R AND 9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 440 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER 8L AND 9L. REMOVED DAMAGE AND A BRACKET AT FS 440 LT SIDE FRAME AT 8L TO 9L AND REPAIRED IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 559 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED BRACKET IAW EA5310-04498, CUT OUT DAMAGE IAW EA5310-04498. INSPECTED IAW 737 NOTM PT65100-00 FIG 23, NO DEFECTS NOTED, FABRICATED PARTS ALODINED, PRIMED PARTS AND CUTOUT IAW EA5310-04498 INSTALLED REPAIR PARTS AND BRACKET IAW EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 727B FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED CRACKED FRAME AT STA 727B PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 400 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET LT SIDE BETWEEN STRINGER 8L AND 9L. REPAIRED IN ACCORDANCE WITH EA5310-04498 REMOVED A/C RAIL BRACKET, CUT OUT DAMAGED AREA, PERFORMED HFEC, FABRICATED AND INSTALLED REPAIR PARTS IAW EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 747 FRAME IS CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES AT STATION 747 BETWEEN STR 8R AND 9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 867 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES ON FRAME 867 BETWEEN STR 8R AND 9R PER EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 706 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED BRACKET PER EA 5310-04498, CUT OUT DAMAGE PER EA 5310-04498, HEEL CUT OUT PER NDTM PTG 51-00-00 FIG 23, NO DEFECTS NOTED. FABRICATED REPAIR ANGLE C, D. TREATED AND PRIMED PART C, D PER EA 5310-04498. INSTALLED REPAIR PART C, D EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 400 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGE IN FRAME. PERFORMED HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 787 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED CRACKED FRAME AT STATION 787 PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 867 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED A/C RAIL BRACKET IAW EA 5310-04498, CUT OUT 2 EA HOLES IN FRAME IAW EA 5310-04498. HFEC INSPECTED IAW 737 NDTM PT6 51-00-00, FIG 23. NO DEFECTS NOTED. FABRICATED REPAIR ANGLES, TREATED AND PRIMED IAW EA 5310-04498. INSTALLED REPAIR ANGLES AND A/C RAIL BRACKET IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 907 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED BRACKET IAW EA5310-04498 CUT OUT DAMAGE IAW EA5310-04498 INSPECTED CUTOUT IAW 737 NOTM P T65100-00 FIG 23, NO DEFECTS NOTED. FABRICATED PARTS, ALODINED AND PRIMED PARTS AND CUTOUT IAW EA5310-04498. INSTALLED REPAIR ANGLES AND BRACKET IAW EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 440 FRAMED CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REPAIRED CRACKED FRAME AT STA 440 BETWEEN STR 8R AND 9R PER EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 597 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED BRACKET IAW5310-04498, CUT OUT DAMAGE IAW EA5310-04498. INSPECTED CUTOUT IAW 737 NDTMPT65100-00 FIG 23, NO DEFECT NOTED. FABRICATED PARTS, ALODINED, PRIMER PARTS AND CUT OUT IAW EA5310-004498 INSTALLED REPAIR ANGLES AND AIR CONDITIONING (AC) BRACKET IAW EA5310-04498 E.
Part: INTERCOSTAL — CRACKED (BS 540) · airframe 28,485 hrs · 15,075 cycles
INTERCOSTAL AT STA 540 FROM BL 0 TO LBL 24.0 IS CRACKED (VIEWED FROM FWD SIDE). REMOVED DAMAGED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL AND RE-INSTALLED IAW B737 SRM 51-40-05, 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 380 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGE TO FRAME. PERFORMED HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 827 FRAME IS CRACKED AT AC SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAME PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,485 hrs · 15,075 cycles
FS 747 FRAME IS CRACKED AT AC SUPPORT BRACKET BETWEEN STRINGERS 8L & 9L. REPAIRED PER EA 5310-04498.
Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 28,485 hrs · 15,075 cycles
INTERCOSTAL FOUND CRACKED UNDER FLOORBOARD IN AFT CABIN BETWEEN BODY STATION 947.5 AND 927 AT RBL 25". REMOVED DAMAGE FROM INTERCOSTAL BETWEEN BODY STATION 947.5 AND 927 AT RBL 25" UNDER FLOORBOARD IN AFT CABIN PER B737 SRM 51-70-11. FABRICATED REPAIR FROM 7075-T6 .050 ALUM SHEET PO 56315A PER B737 SRM 51-70-11, INSTALLED PER B737 51-40-02.
Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 28,485 hrs · 15,075 cycles
INTERCOSTAL CRACKED FROM BODY STATION 328-344 AT LBL 44. REMOVED AND REPLACED INTERCOSTAL PER B737 SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 28,485 hrs · 15,075 cycles
INTERCOSTAL CRACKED FROM BS 312-328 AT LBL 44. REMOVED AND REPLACED INTERCOSTAL PER B737 SRM 51-40-02.
2006
Part: COOLING FAN — MALFUNCTIONED (E/E BAY) · airframe 22,095 hrs · 11,749 cycles
A STRONG SULPHUR BURNING SMELL WAS NOTICED IN THE CABIN AT FL 360 WHILE EN ROUTE TO IAH. THE RECIRCULATION FAN WAS SHUT OFF AND THE ODOR CEASED. WHEN THE FAN WAS TURNED ON DURING DESCENT THE ODOR RETURNED. THE FAN WAS SHUTDOWN AGAIN. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING FOUND THE AVIONICS AIR COOLING FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED IAW MM 21-58-12. LEAK AND OPERATIONAL CHECKS WERE GOOD.
2003
Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 16,218 hrs · 8,664 cycles
INSPECTION FOUND BELTFRAME CORRODED AT STA 992, S17-18R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11.
Part: ATTACH ANGLE — GOUGED (FUSELAGE) · airframe 16,218 hrs · 8,664 cycles
INSPECTION FOUND A GOUGE ON VERTICAL ATTACH ANGLE ON RT SIDE OF VERTICAL STRAP AT STA 1121. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.
Part: ATTACH ANGLE — GOUGED (FUSELAGE) · airframe 16,218 hrs · 8,664 cycles
INSPECTION FOUND ATTACH ANGLE ON LT SIDE OF VERTICAL STABILIZER ON FUSELAGE EXTERIOR AT STA 1121 GOUGED. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.
Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 16,218 hrs · 8,664 cycles
INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD LUG HAD CORROSION AFT BUSHING. REMOVED AND REPLACED BUSHINGS ON LT HORIZONTAL STABILIZER FWD UPPER IAW SRM 55-10-10.
Part: SKIN — CRACKED (FUSELAGE) · airframe 15,411 hrs · 8,225 cycles
INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN OUTBOARD OF EE ACCESS DOOR AT STA 338 BETWEEN STRINGER 24R AND 25R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5330-03260.