N46625
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
37 reports on file, 2000-12-27 – 2012-12-06.
Part: SKIN — DENTED (FWD FUSELAGE) · airframe 47,553 hrs · 25,268 cycles
DURING WALKAROUND, FOUND A DENT JUST AFT OF THE 178 BULKHEAD AT THE 7 O`CLOCK POSITION LOOKING FOWARD.
Part: SKIN — DENTED (BS 827) · airframe 47,553 hrs · 25,268 cycles
FUSELAGE SKIN DENTED AT STA 827, BL 0 (BELOW AFT CARGO DOOR CUTOUT) CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER REF ECRA 5331- 01668.
Part: SEAT TRACK — FAILED (COCKPIT) · airframe 47,288 hrs · 25,115 cycles
AT GATE , RELEASED PARK BRAKE, CAPTAIN`S SEAT BROKE. FOUND BOTH FWD CAPTAIN`S SEAT TRACKS CRACKED AND BROKEN OFF. REPLACED BOTH FWD SEAT TRACKS IAW AMM 25-11-11-406-005-001, PN S232T303 -1005, INSTALLED CAPTAIN`S SEAT IAW AMM 25-11-11- 422-132.
Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 47,057 hrs · 24,998 cycles
ON APPRAOCH, GEAR HANDLE DOWN, INDICATIONS SHOWED ONLY "RED" NOSE GEAR LIGHT. PERFORMED MANUAL GEAR EXTENSION, NO CHANGE, NOTICED LANDING GEAR AIR/GROUND RELAY CIRCUIT BREAKER TRIPPED & RESET, GEAR INDICATIONS NORMAL. REF L/PS 4584879 & 4584880, ACCOMPLISHED ALL REQ INSPECTIONS & OPS CHECKS FOR TRIPPED CIRCUIT BREAKER, IAW SWP 20-00-10 & AMM 20-60-01-201. VISUAL CHECK OF ELECTRICAL SYS & COMPONENTS ACCOMPLISHED WITH NO DEFECTS FOUND, SYS OPS CHECKED NORM WITH NO DEFECTS FOUND. CIRCUIT BREAKER REMAINS SET WITH NO DISCREPANCY NOTED, OK TO CONTINUE.
Part: CONTROL VALVE — INOPERATIVE (CABIN AIR) · airframe 46,833 hrs · 24,865 cycles
AT AT FL250, RT EQUIPMENT COOLING EXHAUST LIGHT CAME ON, PERFORMED QRH PROCEDURES. REPLACED THE AIR FLOW CONTROL VALVE IAW AMM 21-58-31-401. OPS CHECKED NORMAL.
Part: UPLOCK SENSOR — FAILED (LT MLG) · airframe 45,418 hrs · 24,164 cycles
LEFT GEAR UNSAFE LIGHT AFTER TAKEOFF. GEAR CAME DOWN NORMALLY FOR LANDING. T/S PER M/M 32-61-00-101. UPLOCK SENSOR S72 BAD. REPLACED S72 SW IAW M/M 36-61-21. SWUNG GEAR. OPS CHECK NORMAL.
Earlier reports · 2000–2010 · 31 reports
2010
Part: TEE FITTING — CORRODED (E&E BAY) · airframe 42,271 hrs · 22,469 cycles
SUPPORT TASK - INTERGRANULAR CORROSION IN E/E BILGE LBL 12 JUST FWD OF DOOR CUTOUT INTERIM REPAIRED ELECTRONIC ACCESS DOOR LBL 6.74 BEAM LOWER TEE CORD PER ECRA 5311-01503 AND INITIATED A DIP TO READ AS FOLLOWS: ON OR BEFORE SEPTEMBER /3/2012 PERFORM INSPECTION PER PART 2 FO ECRA 531-01503 ATTACH FORM 44.0008 PAGE 1-3 ITEM 1-14. //QC// ON OR BEFORE SEPTEMBER 3, 2012. PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-01503. DIP CTL#06821 LIMIT: 1) T/A: DUE 03 SEP 2012.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,271 hrs · 22,469 cycles
B737-53-3-0306 CORROSION ON SHEAR TIE FWD AND AFT SIDE OF STA 767 BL 0 BETWEEN STR 27 L AND 27 RT FABRICATED AND INSTALLED SHEAR TIE REPAIR REF SRM 53-00-07.
Part: CLEVIS — CORRODED (HORIZ STAB) · airframe 42,271 hrs · 22,469 cycles
SUPPORT TASK RT HORZ STAB AFT LOWER CLEVIS HAS CORROSION REMOVED LIGHT CORROSION AND TREATED AS REQUIRED PER SOPM 20-10-03 AND SRM 55-10-10.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,271 hrs · 22,469 cycles
SUPPORT TASK STA 303.9 FRAME WEB CRACKED AT S16L REF EA 5310-04 659 OP2 STEPS 8 & 9 CABIN INSTALLED REPAIR AT FRAME STA 303.9 REF EA 5310-04659 OP2.
Part: SKIN — CRACKED (FUSELAGE) · airframe 42,164 hrs · 22,407 cycles
SUPPORT TASK REF EA 5330-03736 REV B STEP 14 TWO FASTENER HOLES SHOW CRACK INDICATIONS. BOTH FASTENERS ARE IN A ROW AT STA 304 ONE AT WL 260 AND ONE AT WL 258.30 FWD ENTRY DOOR UPPER HINGE. CRACKS INDICATE ON AFT EDGE OF HOLES. FASTENER HOLES HAVE BEEN REPAIRED ALONG WITH THE INSTALLATION OF DOUBLER / TRIPLERS TO ENCOMPASS THE REPAIR AREA FWD FUSELAGE SKIN FWD OF L-1 DOOR STA 294-303.9 STR 9 L TO STR 15 L IAW 5331-01524 REF LG PGS 6925005 AND 6925006 FOR REQ DIPS.
2008
Part: STRAP — CRACKED (FUSELAGE) · airframe 38,130 hrs · 20,346 cycles
BOTTOM OF FLOORBEAM STABILIZER STRAP CRACKED AT BODY STATION 312 RBL-36. REPAIRED DAMAGED STABILIZER STRAP ON BOTTOM OF FLOORBEAM AT BODY STATION 312 RBL-36 PER B737-500 SRM 53-10-51, REPAIR 4.
Part: CABLE — BROKEN (EVAC SLIDE) · airframe 37,876 hrs · 20,206 cycles
L-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS, REFERENCE WORK CARD 24-0550-1-0004 STEP 16. REMOVED AND REPLACED L-2 DOOR ESCAPE SLIDE LATCH CABLE ASSY REF M/M 25-61-35.
Part: CABLE — BROKEN (EVAC SLIDE) · airframe 37,876 hrs · 20,206 cycles
R-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS, REFERENCE WORK CARD 24-0550-1-0004 STEP 16. REMOVED AND REPLACED R-2 DOOR ESCAPE SLIDE LATCH CABLE ASSY REF M/M 25-61-35.
Part: FAN — FAILED (RT A/C PACK) · airframe 37,218 hrs · 19,855 cycles
PASSING THROUGH 11000 ON DESCENT ELECTRICAL AND/OR RUBBER BURNING ODOR, WAS NOTED, NO SMOKE OBSERVED. A/C SMOKE FUME CHECKLIST PERFORMED AND ODOR LESSENED WHEN RT PACK ISOLATED. ODOR STARTED QUICKLY IN FIRST CLASS THRU MID CABIN AND DISSIPATED SOMEWHAT ONCE THE RIGHT PACK TURNED OFF AND ISOLATION CLOSED. AFTER LANDING AN ODOR WAS STILL APPARENT TO FIRE PERSONNEL. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-95-201, UNABLE TO DUBLICATE ON GROUND. TROUBLESHOT FOR RECIRCULATION FAN FAILURE. AIRCRAFT OK TO CONTINUE SERVICE.
Part: PAN — CRACKED (L1 DOOR) · airframe 36,498 hrs · 19,489 cycles
L1 DOOR PAN CRACKED AT AFT EDGE AROUND STOP PIN BRACKET 4TH FROM BOTTOM. INSTALLED REPAIR ANGLE REF ECRA 5210-02014.
Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 36,498 hrs · 19,489 cycles
L1 DOOR WEB CRACKED I/B OF TORQUE UPPER END (ONE BAY ABOVE TORQUE BOX). REMOVED AND INSTALLED NEW INTERCOSTAL AND CLOSED INNER SKIN REF SRM 51-40-02.
Part: PAN — CRACKED (L1 DOOR) · airframe 36,498 hrs · 19,489 cycles
L1 DOOR PAN CRACKED AT AFT EDGE AROUND NR 5 STOP PIN BRACKET FROM BOTTOM. INSTALLED REPAIR ANGLE REF ECRA 5210-02014.
Part: DOOR FRAME — CRACKED · airframe 36,498 hrs · 19,489 cycles
FWD CARGO DOOR CUTOUT AFT FRAME HAS 1 INCH CRACK, AT BOTTOM DOOR STOP PAD FOOT PRINT. REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FRAME REF SRM 51-40-02.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,498 hrs · 19,489 cycles
FWD CARGO DOOR CUTOUT AFT FRAME HAS 1 INCH CRACK, AT BOTTOM DOOR STOP PAD FOOT PRINT. REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FRAME REF SRM 51-40-02.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 36,498 hrs · 19,489 cycles
S16L CRACKED STA 482B-4". REPAIRED S16L STA 482B-4" REF SRM 53-00-03 REPAIR 1 FIG 201 PG 201.
Part: WEB — CRACKED (FUSELAGE) · airframe 36,498 hrs · 19,489 cycles
WEB CRACKED STA 277 AT S14R. INSTALLED WEB ASSY IAW SRM 51-40-02.
Part: WEB — CORRODED (FUSELAGE) · airframe 36,498 hrs · 19,489 cycles
AFT CARGO DOOR CUTOUT LOWER WEB CORROSION MARKED. REMOVED AND REPLACED WEB REF SRM 51-40-02.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 36,498 hrs · 19,489 cycles
AFT CARGO BETWEEN STA 747 AND 767, ANTENNA BRACKET CORROSION MARKED. REPLACED AFT CARGO ANTENNA BRACKET AT STA 747-767 PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (BS 277-290) · airframe 36,498 hrs · 19,489 cycles
RT SIDE OF FUSELAGE STA 277 TO 290 NR 9 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL AS REQUIRED IN SRM 51-10-2.
Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 36,498 hrs · 19,489 cycles
NR 3 MID FLAP I/B AND O/B TORQUE TUBES CORRODED AND PITTED. REMOVED AND REPLACED WITH SERVICEABLE TORQUE TUBES I/B AND O/B REF CMM 57-53-17.
Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 36,498 hrs · 19,489 cycles
NR 3 MID FLAP CARRIAGE, BOTH ARMS PITTED WITH CORROSION. REMOVED AND REPLACED WITH SERVICEABLE I/B AND O/B CARRIAGE HALVES ON O/B SIDE OF NR 3 MID FLAP.
2005
Part: FLOORBEAM — CORRODED (STA 986.5) · airframe 29,533 hrs · 15,799 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 9 TO RBL 45. REPAIRED IAW ECRA 5321-01273.
Part: ANGLE — CORRODED (STA 975-990) · airframe 29,533 hrs · 15,799 cycles
INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 975-990, RBL 50 TO RBL 51. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.
Part: CHANNEL — CORRODED (STA 277-360) · airframe 29,533 hrs · 15,799 cycles
INSPECTION FOUND L-1 DOOR ENTRY Z-CNANNEL CORRODED AT STA 277-360, LBL 39. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02.
2003
Part: STRIP — CRACKED (RT MLG WW) · airframe 24,325 hrs · 13,078 cycles
INSPECTION FOUND A .25 INCH CRACK AT O/B CORNER OF RT WHEEL WELL FORWARD FAIRING AFT ATTACH STRIP. AN ANGLE WAS INSTALLED IAW SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 24,325 hrs · 13,078 cycles
INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-30-51.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 24,325 hrs · 13,078 cycles
INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 380-400, BL 0. THE INTERCOSTAL WAS REMOVED NAD REPLACED IAW SRM 53-30-51.
Part: SKIN — CRACKED (STA 807) · airframe 23,794 hrs · 12,801 cycles
INSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BELOW AFT CARGO PIT THRESHOLD AT STA 807, S26R-S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-03214.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,794 hrs · 12,801 cycles
MAINTENANCE DISCOVERED A CREASE TO THE FUSELAGE SKIN AT BS 807 BETWEEN S26R AND S27R DURING GROUND OPERATIONS IN CLE. WHEN THE CREASED AREA WAS CUT OUT THE UNDERLYING SHEAR TIE WAS FOUND DAMAGED AND WAS REPLACED. A PERMANENT FUSELAGE SKIN REPAIR WAS PERFORMED IAW ECRA 5330-03214.
2000
Part: SKIN — DENTED (CARGO DOOR) · airframe 18,397 hrs · 9,910 cycles
INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED AND SCRATCHED. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: STRAP — CORRODED (DOOR FRAME) · airframe 18,397 hrs · 9,910 cycles
INSPECTION FOUND STRAP AT LOWER JAMB OF AFT CARGO DOOR CORRODED AT STA 807-847 ABOVE L27R. A NEW STRAP WAS INSTALLED IAW SRM 51-10-2.