N17619
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.
46 reports on file, 1995-02-05 – 2012-06-27.
Part: POSITION SENSOR — INOPERATIVE (NLG WHEEL WELL) · airframe 47,991 hrs · 25,581 cycles
AFTER GEAR RETRACTION AND GEAR LEVER PLACED TO OFF POS HAD INTERMITTENT RED NOSE GEAR LIGHT & AMP; INTERMITTEN GREEN LIGHT CYCLE GEAR LEVER UP FROM OFF IAW QRH NO CHANGE ALL MLG RED/GREEN LOGIC GOOD TROUBLESHOT REF AMM 32-61-01 R & AMP; R S845 & AMP; S846 SENSORS REF WDM 32 -64-12 PERFORMED NLG RETRACTION & AMP; EXTENSION REF AMM 32-33-00 SYS, OPS CHECK GOOD AT THIS TIME ACFT OK TO CONTINUE.
Part: FLOORBEAM — CORRODED (BS 344) · airframe 47,796 hrs · 25,482 cycles
FLOORBEAM 344 HAS CORROSION BL-0 TO RBL-23. REPAIRED FLOORBEAM STA 344 IAW ECRA-5311-01555.
Part: FRAME — CORRODED (BS 227.5) · airframe 47,796 hrs · 25,482 cycles
CORROSION AT FRAME STA 227.5 FROM BL0 TO RBL 5.7 IAW EA5100-02244. REPAIRED BULKHEAD LOWER OTBD CHORD STA 227.8, REF-EC/RA 5310-01556.
Part: FLOORBEAM — CORRODED (BS 328) · airframe 47,796 hrs · 25,482 cycles
FLOORBEAM BS 328 HAS CORROSION BL 0 TO RBL 23. REPAIRED FLOORBEAM IAW ECRA 5311-01554
Part: FRAME — CRACKED (BS 360 S8-9L) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE LT FRAME CRACKED STA 360 BETWEEN S 8 & 9 REPAIRED FRAME IAW ECRA.5311-01551.
Part: FRAME — CRACKED (BS 827) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE FRAME RT CRACKED STA 827, BETWEEN STR 8 & AMP; 9. SEE WIPS, ATTACHED FORMS 44.0008 AND HEAT TREAT FORMS 43.0150. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS REF ECRA 5311-01550.
Part: ANGLE — CRACKED (R1 DOOR) · airframe 47,796 hrs · 25,482 cycles
ANGLE CRACKED LOWER AFT CORNER OF R1 DOOR INTERIOR-PN69-45871- 508. R & R ANGLE PN 65-45871-149, REF SRM 51-40-02.
Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 47,796 hrs · 25,482 cycles
R1 DOOR HAS A CRACK AT AFT LOWER CORNER OF DOOR FRAME AND STOP MOUNT BOLT AS VIEWED FROM INSIDE OF DOOR, MARKED. R & R DOUBLER, PN 69-69854-1, REF SRM 51-40-02.
Part: FRAME — CRACKED (R1 DOOR) · airframe 47,796 hrs · 25,482 cycles
R1 DOOR AFT FRAME CRACKED AT LOWER END. CUT-OUT SECTION OF DAMAGED, INSTALLED NEW FRAME SECTION PN 69-6 9854-11, FRAME WEB SPLICE -2, -3, -4 AND STRAP REF DWG 6 9-69854.
Part: BEAM — CRACKED (R1 DOOR) · airframe 47,796 hrs · 25,482 cycles
R1 DOOR HAS A CRACK AT AFT CORNER OF LOWER WEB AND STOP MOUNT AS VIEWED FROM INSIDE OF DOOR, R & R R1 DOOR LOWER BEAM PN 65-45071-39, REF SRM 51-40-02.
Part: FLOORBEAM — CORRODED (BS 986) · airframe 47,796 hrs · 25,482 cycles
CABIN FLOORBEAM, STA 986 HAS MILD CORROSION ON UPPER SURFACE LBL36 TO LBL46. R & R UPPER T CHORD AT STA 986 FROM LBL 10 TO LB L 48 IN REF WITH ECRA 5310-04494. REPAIR OPTION B.
Part: INTERCOSTAL — CORRODED (BS 986.5 S21L) · airframe 47,796 hrs · 25,482 cycles
INTERCOSTAL CORRODED, STR 21 LT AT STA986.5 TO 1006 REMOVED AND FABRICATED NEW INTERCOSTAL AND INSTALLED REF SRM 51-04-02.
Part: SHIM — CRACKED (FLOOR SUPPORT) · airframe 47,796 hrs · 25,482 cycles
FLOOR SUPPORT SHIM CRACKED, STA 540 BETWEEN LT OTBD AND LT INBD SEAT TRACK. R & R FLOOR SUPPORT. REF: SRM 51-40-02.
Part: FRAME — CRACKED (BS 482) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE RT FRAME CRACKED ST 482 BETWEEN STR 8 AND AMP; 9. REMOVED DAMAGE FROM FRAME, REPAIRED REF EA 5310-04498, REV B.
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 47,796 hrs · 25,482 cycles
FLOOR SUPPORT AT STA 540 BETWEEN BL-0 & AMP; LT INBD SEAT TRACK IS CRACKED. R & R CRACKED FLOOR SUPPORT. REF:SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 47,796 hrs · 25,482 cycles
FLOOR SUPPORT AT STA 540 BETWEEN RT OTB & AMP; RT INBD SEAT TRACK TOP STRIP IS CRACKED. R & R FLOOR SUPPORT. REF: SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 47,796 hrs · 25,482 cycles
FLOOR SUPPORT CRACKED, STA 540, BL0 TO RT INBD SEAT TRACK. R & R FLOOR SUPPORT. REF: SRM 51-40-02
Part: FRAME — CRACKED (BS 907 S8-9R) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE RT FRAME CRACKED, STA 907, BETWEEN STR 8 & AMP; 9. COMPLIED WITH FRAME REPAIR REF EA 5310-04498, REV B, OP 02.
Part: FRAME — CRACKED (BS 360 S8-9R) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE RT FRAME CRACKED STA 360 BETWEEN STR 8 & AMP; 9. COMPLIED WITH FRAME REPAIR REF EA 5310-04498, REV B, OP 02.
Part: FRAME — CRACKED (BS 727B S9L) · airframe 47,796 hrs · 25,482 cycles
FRAME CRACKED STA 727B AT S-9L. REPAIRED CRACKED FRAME AT FS 727B AT PSU RAIL ATTACH BRACKET REF EA 5310-04498, REV B, OP 2.
Part: FRAME — CRACKED (BS 440) · airframe 47,796 hrs · 25,482 cycles
FUSELAGE RT FRAME CRACKED BS 440 BETWEEN STR 8 & AMP; 9. REPAIRED RT FRAME STA 440 BETWEEN. STR 8 & AMP; 9. REF EA 5310-04498, REV B, OP 02.
Part: FLOOR SUPPORT — CRACKED (STA 344-360) · airframe 47,796 hrs · 25,482 cycles
FLOOR SUPPORT, STA 344 TO STA 360, CRACKED BL 0. R & R FLOOR SUPPORT, PN 65C33970-53 FROM STA 344 TO STA 360, BL 0, REF SRM 51-40-02.
Earlier reports · 1995–2009 · 24 reports
2009
Part: SKIN — DELAMINATED (RUDDER) · airframe 41,753 hrs · 22,337 cycles
LEFT SIDE OF RUDDER HAS PUNCTURE HOLE (DELAMINATION) APPROXIMATELY 31 INCHES FROM BOTTOM AND 6 INCHES FROM TRAILING EDGE. INITIAL REPAIR ON N00060 FAILED. ENSURED RUDDER WITHIN BALANCE LIMITS PER B737-500 SRM 51-60-07 IAW EC/RA 5540-01264 REV A PART D STEP 3. INSTALLED NEW DATA TAG "BAL BY CALC 12-31-09 SBHM +319.148", NO WEIGHTS ADDED 24 WEIGHTS SPACES FILLED WITH 12 SPACES REMAINING. INSTALLED REPAIR PER EC/RA 5540-01264 REV A.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,753 hrs · 22,337 cycles
CORROSION ON INTERCOSTAL AT STA 947 ABOVE S26R. FABRICATED AND INSTALLED INTERCOSTAL AT STA 947 ABOVE S26R REF BOEING DRAWING 65-49680 AND SRM 51-40-02.
Part: BULKHEAD — WORN (FUSELAGE) · airframe 41,753 hrs · 22,337 cycles
SUPPORT TASK FRAME AT STA 1064 BL 0 WORN WHERE APU PNEUMATIC DUCT RUNS THROUGH. CLEANED, MEASURED, ALODINED, AND PRIMED AREA PER ECRA 5311-01475.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,753 hrs · 22,337 cycles
CRACKS AT PNL FASTENERS IN UPPER CHORD OF STRESS WEB STA 927 TO STA 947 BL-0 OF MAIN DECK FLOOR STRUCTURE. REMOVED AND REPLACED SHEAR WEB ANGLE AT STA 927-947 BL-0 REF SRM 51-40-02.
Part: WIRE HARNESS — FAULTY (CABIN) · airframe 41,664 hrs · 22,293 cycles
ROW 17 ABC EMERGENCY LIGHT INOP. FOUND SEAT WIRE HARNESS AT FAULT. INSTALLED SERVICEABLE PART. OPS CHECKS NORMAL.
Part: BRACKET — BROKEN (NLG) · airframe 40,827 hrs · 21,831 cycles
NOSE GEAR DOOR - PLEASE CHECK - IN-FLIGHT SOUNDS AS SEAL MISSING. FOUND RIGHT NLG DOOR ACTUATOR BRACKET CRACKED. REMOVED AND REPLACED DOOR OPERATOR BRACKET PER THE 737 CMM 32-21-38. NLG DOOR ADJ CHECKS GOOD PER THE 737-300/500 AMM 32-33-61.
2007
Part: SKIN — CORRODED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
TOOLING MARKS AND SURFACE CORROSION AT UPPER ATC ANTENNA MOUNT SURFACE. SHEET METAL REPAIR COMPLETED AS PER ECRA 5331-01375 AND AMM 34-53-11.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED STA 727B BETWEEN STRINGERS 8R AND 9R. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGERS 8R AND 9R REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME CRACKED AT STA 787 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED STATION 827 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED STA 907 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
CABIN STA 400 BETWEEN RIGHT STRINGER 8 AND PUS RAIL ATTACH BRACKET TO FRAME CRACKED. REPIARED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED STATION 867 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED AT STA 787 BETWEEN STRINGER 8R AND 9R. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
FUSELAGE FRAME IS CRACKED AT STA 747 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684.
Part: FRAME — CRACKED (FUSELAGE) · airframe 36,796 hrs · 19,749 cycles
CABIN STATION 440 BETWEEN STRINGER 8 AND 9 PSU RAIL ATTACH BRACKET TO FRAME CRACKED LEFT SIDE. REPAIRED PER ECRA 5310-04684.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,795 hrs · 19,749 cycles
PAX CABIN STR 11 L HAS CRACKED ATTACHMENT CLIP AT STA 360. REMOVED AND REPLACED PER EA5311-01383.
2005
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,324 hrs · 16,376 cycles
INSP FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 986.5, LBL 14 TO LBL 43. FLOORBEAM UPPER CAP REPAIR WAS INSTALLED IAW ECRA 5310-04471.
2004
Part: LINKAGE — BROKEN (RT NLG DOOR) · airframe 28,031 hrs · 15,216 cycles
A LOUD NOISE WAS HEARD AND VIBRATION WAS FELT COMING FROM THE NOSE GEAR WHEEL WELL AREA AFTER GEAR RETRACTION LEAVING JAX. THE NOISE STOPPED WHEN THE GEAR WAS LOWERED FOR A RETURN TO JAX. MAINTENANCE FOUND RT NOSE GEAR DOOR LOWER LINKAGE BROKEN. THE LINKAGE WAS REMOVED AND REPLACED IAW MM 32-22-11. THE DOOR WAS ADJUSTED IAW MM 32-33-61 AND OPERATIONAL CHECKS WERE GOOD.
2003
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,165 hrs · 13,697 cycles
INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT AT STA 344, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-3.
2000
Part: APU — INOPERATIVE (TAIL) · airframe 19,270 hrs · 10,452 cycles
THE APU FIRE WARNING ACTIVATED DURING APU START WHILE ON FINAL APPROACH TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. THE APU WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 49-11-00, PAGE 201 AND PAGE 501. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW MM 26-22-11.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 18,986 hrs · 10,299 cycles
INSPECTION FOUND SEAT TRACK CORRODED AT STA 907 - 947, LT LAV. THE CORRODED SECTION OF TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52.
1995
Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)
ELP - FLT 1684 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO ELP. MAINTENANCE FOUND THE LANDING GEAR LEVER LATCH AND PRESSURE WARNING CIRCUIT BREAKER TRIPPED. THE CIRCUIT BREAKER AS RESET. OPERATION OF THE LANDING GEAR HANDLE CHECKED NORMAL IAW MM 32-31-00, PAGE 501. (X)