N236WA
Registered owner: K&B LYONS LLC, IN (owner ≠ operator)
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.
20 reports on file, 1995-01-15 – 2004-01-16.
Part: FLOORBEAM — CRACKED (BL 0.07, BS667) · airframe 45,905 hrs · 36,838 cycles
DURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 665, BS 669 AND BS 673. DAMAGE WAS REPAIRED AS PER ERA 385959-14AD.
Part: FRAME — DAMAGED (BS440, S26R) · airframe 45,905 hrs · 36,838 cycles
A DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REPAIRED PER ERA 386004-14.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,905 hrs · 36,838 cycles
DENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14.
Part: SKIN — CRACKED (FUSELAGE) · airframe 45,905 hrs · 36,838 cycles
DURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 559 & 579. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3, FIG 42 AND ER/A 087880-14AD.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,905 hrs · 36,838 cycles
DURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH. UPPER CHORD WAS CUT OFF AND A NEW SECTION SPLICED IN PER ERA 385945-14.
Part: SKIN — DENTED (FUSELAGE) · airframe 45,905 hrs · 36,838 cycles
THE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14.
Part: FRAME — CRACKED (FUSELAGE) · airframe 45,905 hrs · 36,838 cycles
CRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRACKS INDICATIONS WERE REMOVED AND REPAIR INSTALLED PER ERA 385971-14.
Earlier reports · 1995–2000 · 13 reports
2000
Part: SUPPORT FITTING — CORRODED (LT & RT MLG) · airframe 42,599 hrs · 35,420 cycles
THE LOWER MAIN LUGS ON THE LT AND RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTINGS AT FS 685 WERE FOUND CORRODED. THE EXISTING BUSHINGS WERE REMOVED AND LUG BORES OVERSIZED TO REMOVE THE CORROSION. LARGER DIAMETER REPAIR BUSHINGS WERE INSTALLED TO REPAIR THE CONDITION PER ER/A 378835-14.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,952 hrs · 35,130 cycles
WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, A TYPICAL CRACK WAS FOUND IN THE BULKHEAD WEB AT WL 234 AND RBL 7. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER BAC S/B 737-53A1173 AND DOCUMENTED PER ER/A 377922-14AD.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,952 hrs · 35,130 cycles
WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD PER AD 2000-05-29, TYPICAL CRACKS WERE FOUND IN THE ADJACENT FLOOR WEBS AT WL 207 AND RBL & LBL 25. THE CRACKED WEBS WERE REMOVED AND NEW WEBS INSTALLED PER BAC S/B 737-53A1173 AND ER/A 377928-14AD.
Part: BULLET — DENTED (NR 1 ENGINE) · airframe 41,078 hrs · 34,747 cycles
EN ROUTE FROM BDL TO FLL, NR 1 ENGINE HAD COMPRESSOR STALLS. CREW PULLED THROTTLE TO IDLE. DIVERTED TO BOS. BOS MTC FOUND NR 1 ENGINE NOSE BULLET DETACHED AND FAN DAMAGE.
1999
Part: DUCT — FAILED (APU BLEED)
AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O CONFIGURED FOR RIGHT BLEED AND RIGHT PACK OPERATION. AUTO/STBY/AND MANUAL MODES ATTEMPED. OUTFLOW VALVE FULL CLOSED FWD OUTFLOW VALVE CLOSED. FOUND APU BLEED AIR DUCT RUPTURED. REPLACED SAME.
1998
Part: FAN — FAILED (A/C BAY)
GASPER FAN C/B FOUND OPEN, WHEN CLOSED IT RETRIPPED ACCOMPANIED BY A LOUD POP HEARD UNDER FLOOR IN MID CABIN AND STRONG ELECTRICAL SMELL. INSP GASPER FAN NO PROBLEMS. REPLACED FAN.
Part: LINE — CHAFFED (NR 2 ENGINE)
A/C RETURN ATL, DUE TO RT HYD PUMP LOW PRESS LIGHT AND HYD QTY ZERO ON CLIMB-OUT. FOUND HYD RTN LINE CHAFFED. REPLACED LINE AND FILTER AND EDP PER M/M. LEAK CK GOOD AND SYS OPS NML PER M/M.
Part: DUCT — CRACKED (APU AREA)
WITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMELL IN MID CABIN AREA. FOUND APU BLEED LINE CRACKED JUST AFT OF APU BLEED VALVE. REPLACED BLEED DUCT.
Part: SKIN — CRACKED (BS 951)
THE R2 DOOR OPENING SURROUND SKIN WAS FOUND WITH A .75 INCH LONG CRACK AT THE CUTOUT FOR THE LOWER HINGE. THE SKIN AND BONDED DOUBLERS WERE CUTOUT TO REMOVE THE CRACK. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 364647-14, REV A.
1997
Part: SKIN — CORROSION (BS 920)
A BULGE WAS FOUND IN THE FUSELAGE SKIN AT STA 927 BETWEEN STR 14R AND 15R. MX REMOVED THE AFFECTED AREA OF THE CHEM-MILLED LOWER SKIN (65-45778-82), JUST BELOW THE STR 14R LAP JOINT. THE CUTOUT MEASURED 2.5 BY 8. A TIME LIMITED REPAIR USING BLIND FASTENERS WAS INSTALLED.
1996
Part: BULKHEAD WEB — CRACKED (BS 178)
THREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 198. THE SECOND IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT WL 200. THE THIRD IS LOCATED NEAR LBL 5.7 AT APPROX WL 198. THE DAMAGE WAS REPAIRED WITH A DOUBLER APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-867, DTD 7-9-96.
1995
Part: FAIRING — CAME LOOSE (LT TE MIDFLAP)
LEFT INBD FLAP FAIRING CANOE BROKE LOOSE IN FLT AND WAS FOUND PARTLY DETACHED FROM WING DURING POST FLT. REMOVED LEFT WING MIDFLAP CANOE, REPLACED BELL CRANK ASSY, INBD AND OTBD STRUTS AND REINSTALLED FAIRING PER MM 27-51-21.
Part: BULB — FAILED (LT LOWER BODY)
AFT LOWER BODY EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD.