N16649
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.
34 reports on file, 2003-07-04 – 2010-06-28.
Part: FRAME — CORRODED (BS 767 S26-27R) · airframe 33,022 hrs · 17,451 cycles
FRAME STA 767 AT S27R TO S26R HAS CORROSION. INSTALLED REPAIR PARTS ON FRAME, REPAIR 4 REF-SRM 53-00-07.
Part: FRAME — CORRODED (STA 767) · airframe 33,022 hrs · 17,451 cycles
FRAME STA 767 AT STR 27L TO STR 28L HAS CORROSION. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.
Part: HINGE FITTING — CRACKED (DOOR) · airframe 33,022 hrs · 17,451 cycles
SUPPORT TASK CRACK INDICATION W/HFEC HOLE PROBE REF STEP 20.0 OF 5330-03736. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-40-01 AND 51-10-02 PARAGRAPH 8.
Part: SKIN — CRACKED (L1 DOOR) · airframe 33,022 hrs · 17,451 cycles
SUPPORT TASK-L-1 DOOR OPENING SURROUND STRUCTURE-UPPER HINGE CUTOUT INTERNAL CASTING (FITTING) IS CRACKED APPROX .6250 INCH IN LENGTH (MARKED). REMOVED AND REPLACED L-1 DOOR UPPER HINGE CASTING REF SRM 51-40 -02.
Part: SKIN — CRACKED (L1 DOOR) · airframe 33,022 hrs · 17,451 cycles
L-1 DOOR INNER SKIN FASTENERS CRACKED (MARKED) TASK {B737-52-4-0048}. REMOVED AND REPLACED 91 MARKED INNER SKIN FASTENERS ON L-1 DOOR REF: SRM 51-40-02.
Part: WEB — CRACKED (FUSELAGE) · airframe 33,022 hrs · 17,451 cycles
WEB LOCATED AT BL 0 FROM STA 380-STA 400 IS CRACKED AT TOP, FWD FASTENER HOLE. INSTALLED NEW WEB AT BL 0 STA 380-400 REF SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,022 hrs · 17,451 cycles
MULT-06-3-0037 CABIN FLOOR INTERCOSTAL BETWEEN STA 380 AND STA 400 AT BL 0 IS CRACKED FASTENER HOLE. INSTALLED NEW CABIN FLOOR INTERCOSTAL BETWEEN STA 380-400 AT BL 0 REF SRM 51-40-02.
Earlier reports · 2003–2009 · 27 reports
2009
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 30,879 hrs · 16,317 cycles
AFT FLT ATTENDANT EMERGENCY MEGAPHONE SIREN WILL NOT TEST. REMOVED AND REPLACED THE AFT FLT ATTENDANT EMERGENCY MEGAPHONE. OPS CHECKS GOOD.
2008
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 360 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET INBOARD RIVET BETWEEN STRINGERS 8 AND 9. REPAIRED 360 FRAME AT STR 8-9 LEFT PER ECRA 5310-04845.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 400 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 400 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 787 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 827 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA5310-044498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 747 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 867 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 827 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 867 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR ANGLES PER EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 747 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 787 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498.
Part: WEB — DAMAGED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLOSE-OUT SECTION IAW B737 SRM 51-40-02.
Part: SKIN — DELAMINATED (L/E SLAT) · airframe 28,878 hrs · 15,283 cycles
RIGHT WING NUMBER 5 SLAT TRAILING EDGE OUTBOARD END DELAMINATED. REPAIRED DELAMINATION ON OUTBOARD END OF NUMBER 5 SLAT PER B737-500 SRM 51-70-10.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLOSE-OUT SECTION IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FUSELAGE STATION 400 LEFT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER'S 8L AND 9L. REPAIRED FRAME 400 LT PER EA 5310-04498 BETWEEN STR 8L AND 9L.
Part: ANGLE — CRACKED (CARGO BAY) · airframe 28,878 hrs · 15,283 cycles
AFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL TRANSITION ANGLE IS CRACKED AT STATION 747 AND STATION 727C. REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE FROM STATION 747 TO STATION 727C, FABRICATED REPAIR FROM BAC1496-377 EXTRUSION PO PAC45511Q, IAW B737 SRM 53-60-53. ALODINED AND PRIMED IAW B737 SRM 51-20-01. INSTALLED IAW B737 SRM 53-60-53.
Part: TORQUE BOX — CORRODED (L2 DOOR) · airframe 28,878 hrs · 15,283 cycles
L-2 DOOR TWO MOUNT HOLES ON TORQUE BOX CORRODED. REMOVED AND REPLACED L2 DOOR TORQUE BOX AS CORROSION WAS FOUND TO BE OUT OF LIMITS PER B737 CMM 52-6-03.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R. REPAIRED FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R PER B737-500 SRM 51-70-11.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FWD WET AREA CROSS BRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STA 340-360 LBL 46. REMOVED AND REPLACED INTERCOSTAL AT LBL 46 BS 328 TO BS 344 REF 737-500 SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,878 hrs · 15,283 cycles
FORWARD WET AREA CROSSBRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STATION 360-380 LBL 12. ORIGINAL DAMAGE WAS TO INTERCOSTAL LOCATED AT LBL 12 BETWEEN BODY STATIONS 344-360, REMOVED DAMAGE TO UPPER FLANGE OF INTERCOSTAL AT LBL 12 BETWEEN BS 344 TO BS 360. FABRICATED AND INSTALLED REPAIR PER 737-500 SRM 51-70-11 FIG 1.
2003
Part: SKIN — GOUGED (APU DOOR) · airframe 16,703 hrs · 8,961 cycles
APU ACCESS DOOR INNER SKIN GOUGED LT SIDE FORWARD OF AFT LATCH. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 5200-01.
Part: BUSHING — CORRODED (HORIZ STAB) · airframe 16,703 hrs · 8,961 cycles
FORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.
Part: BUSHING — CORRODED (HORIZ STAB) · airframe 16,703 hrs · 8,961 cycles
CORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.
Part: BUSHING — CORRODED (HORIZ STAB) · airframe 16,703 hrs · 8,961 cycles
FORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.
Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 16,703 hrs · 8,961 cycles
CORROSION ON FORWARD LOWER HORIZONTAL STAB CENTER SECTION LUG ON AFT CLEVIS ON AFT FACE AT BUSHING. REMOVED AND REPLACED BUSHING PER SOPM 20-50-03.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,703 hrs · 8,961 cycles
INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-990. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,844 hrs · 8,516 cycles
THE FUSELAGE SKIN WAS FOUND DAMAGED AFT OF BS 1088 BETWEEN STRINGER 18L AND 20L. THE TRIM OUT TO REMOVE DAMAGE MEASURED 1.3 X 1.15 INCH. THE AREA WAS REPAIRED IAW ECRA 5330-03264.