N214AU
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
57 reports on file, 1995-07-20 – 1999-10-13.
Part: HEAT DUCT — CRACKED (NR 2 ENGINE)
MLI - DURING CLIMB-OUT FROM MDW, FLIGHT CREW REPORTED THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT WAS DIVERTED TO MOLINE, IL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CRACKED FUEL HEAT DUCT AND CHECKED OK. (M)
Part: WIRE — BROKEN (CABIN)
DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN GROUND WIRE AFT OF BATTERY PACK CONNECTION. TC: 90,747. (X)
Part: WIRE — BROKEN (CABIN)
DEN - FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE AT D9022P AND CHECKED OKAY. TC: 90,745. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DEN - FLT 317 - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS FLICKERED IN-FLIGHT. MAINTENANCE RECHARGED BATTERY PACKS AND OPERATIONAL CHECKED OKAY. PART TC: 90,740. (X)
Part: BATTERY CHARGER — FAILED (CABIN)
DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING DID NOT EXTINGUISH WHEN TESTED. MAINTENANCE REPLACED AFT SEAT BATTERY CHARGING UNIT. TC: 9,073. (X)
Part: BEARING — OUT OF LIMITS (RT MLG)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN RIGHT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .057. MAINTENANCE REPLACED RIGHT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7007. (M)
Part: BEARING — OUT OF LIMITS (LT MLG)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN LEFT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .052. MAINTENANCE REPLACED LEFT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7006. (M)
Part: BATTERY PACK — DISCHARGED (L1 DOOR)
DEN - UPON WALK AROUND MAINTENANRE REPORTED EMERGENCY LIGHT ACTIVATION CABLE LOOSE AT SLIDE COVER ON L1 DOOR, EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK. SECURED CABLE ASSY AND CHECKED OK. (M)
Part: BRACKET — CRACKED (BLEED DUCT)
PHX - DURING C-CHECK INSPECTION, REPORTED FASTENER MISSING AND CRACKED MOUNT FLANGE ON 8TH STAGE BLEED DUCT. MAINTENANCE INSTALLED FASTENER AND REPAIRED BRACKET/FLANGE PER 727 OHM 36-10-3, PAGE 5. (M)
Part: WIRE — BROKEN (CABIN)
PHX - DURING C-CHECK INSPECTION, REPORTED CABIN EMERGENCY LIGHTING AND FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT OVERWING BATTERY PCK PER WDM 33-51-01. (M)
Part: FRAME — CRACKED (BS 380)
PHX - DURING C-CHECK INSPECTION, REPORTED A 4 INCH CRACK IN FRAME AT BS 380, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-4, FIG 1. (M)
Part: SKIN — CRACKED (RT WING)
PHX - DURING C-CHECK INSPECTION, REPORTED DENT AND CRACK ON RIGHT WING OUTBOARD SIDE OF PYLON, FLAP SIDE LOAD ROLLER AND CORROSION UNDER FLAP ROLLER WEAR STRIP. MAINTENANCE REMOVED DAMAGED SECTION. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-3 AND EA B737-5430-0021. (M)
Part: BULKHEAD FRAME — CRACKED (CARGO COMPT)
PHX - DURING C-CHECK INSPECTION, REPORTED FORWARD CARGO RIGHT FORWARD BULKHEAD FRAME CRACKED. MAINTENANCE REMOVED DAMAGED SECTION , FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-3, FIG 1. (M)
Part: WIRE — BROKEN (L1 DOOR)
PHX - DURING C-CHECK INSPECTION, REPORTED BROKEN WIRE IN L1 DOOR EXIT LIGHT. MAINTENANCE REPAIRED BROKEN WIRE PER SPWM 20-30-12. (M)
Part: STIFFENERS — CRACKED (NR 2 TR UNIT)
PHX - DURING C-CHECK INSPECTION, REPORTED WEB STIFFENERS ON FORWARD EDGE OF NR 2 ENGINE THRUST REVERSER COWL CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, FIG 1. (M)
Part: WEDGE — CRACKED (LT TE FLAP)
PHX - DURING C-CHECK INSPECTION, REPORTED 1 INCH BY 1.5 INCH CRACK IN LEFT WING TRAILING EDGE FLAP WEDGE. MAINTENANCE REPAIRED PER SRM 57-50-1, FIG 16, DETAIL 15. (M)
Part: SKIN — CRACKED (LT TE MIDFLAP)
PHX - DURING C-CHECK INSPECTION REPORTED A 1.25 INCH CRACK ON LEFT WING TRAILING EDGE INBOARD MIDFLAP INBOARD EDGE FLAP REAR SPAR T-CHORD. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-4, FIG 1 51-40-3 AND 51-30-02. (M)
Part: FITTING — BROKEN (LT AILERON)
PHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED ATTACH ANGLE AND REPAIRED PER SRM 51-30-2, 51-20-3, AND 51-20-1 AND 51-40-4. (M)
Part: RIB — CRACKED (BS 505)
PHX - DURING C-CHECK INSPECTION, RERPORTED CRACK ON FORWARD SIDE OF RIB AT BS 505. MAINTENANCE REPLACED RIB PER SRM 51-10-1, PAGE 5, AND 51-30-2. (M)
Part: FRAME — CRACKED (BS 360)
PHX - DURING C-CHECK INSPECTION, REPORTED A 4.5 INCH CRACK IN FRAME AT BS 360, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-40-3, AND 53-10-4. (M)
Part: HOUSING — CRACKED (NR 6 BEARING)
PHX - DURING C-CHECK INSPECTION, REPORTED 9 INCH CRACK ON NR 6 TURBINE BEARING EXHAUST CASE HOUSING BETWEEN 9-12 O'CLOCK POSITION ON NR 1 ENIGNE. MAINTENANCE REPAIRED PER JT8D MM 72-54, PARAGRAPH 4. (M)
Part: DOOR — BENT (LT MLG)
PHX - DURING C-CHECK INSPECTION, REPORTED LEFT MAIN GEAR AFT OUTER CORNER OF INBOARD DOOR BENT AND BULGING. MAINTENANCE REMOVED FASTENERS, CLEANED AREA, RESEALED AND INSTALLED NEW FASTENERS PER SRM 51-20-4 AND 51-30-2. (M)
Part: SKIN — CRACKED (RT WING)
PHX - DURING C-CHECK INSPECTION, REPORTED A .125 INCH CRACK ON RIGHT WING UPPER WING SKIN AT NR 5 SPOILER CENTER HINGE. MAINTENANCE REPAIRED PER SRM 57-30-1, FIG 4, DETAIL 7. (M)
Part: SKIN — CRACKED (LT WING)
PHX - DURING C-CHECK INSPECTION, REPORTED A .5 INCH CRACK IN LEFT WING UPPER SKIN AT WBL 157. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER/TRIPLER AND REPAIRED PER EO B737-5723-0001 AND DRAWING 65C30113. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PHX - DURING C-CHECK INSPECTION, REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RECHARGED BATTERY PACK PER MM 33-51-11. (M)
Earlier reports · 1995–1998 · 32 reports
1998
Part: BATTERY PACK — DISCHARGED (CABIN)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY. (X)
Part: WIRE — FAILED (CABIN)
ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT WAS 1 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
1997
Part: CONNECTOR — FAILED (CABIN)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED CANNON PLUG WIRE CONNECTING PIN AND CHECKED OK. (M)
Part: SKIN — CORRODED (BS 416)
PILLOWING SKIN BETWEEN RIVETS AT BS 416, STRINGER 221. REMOVED FASTENERS AND DISCOVERED CORROSION BETWEEN SKIN AND STRINGER, CORROSION ON SKIN OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGED SECTION OF SKIN AND ACCOMPLISHED EXTERNAL SKIN REPAIR IAW SRM 53-30-3. (M)
Part: SKIN — CORRODED (BS 270)
PAE - CORROSION ON INNER DOUBLER ON BACK SIDE OF FORWARD LAV SERVICING PAN AT STATION 270. CORROSION OUT OF LIMITS IAW SRM 51-10-6, 53-10-1. REMOVED AND REPLACED IAW PAN DOUBLER IAW SRM 51-30-2. (M)
Part: BULKHEAD — CRACKED (BS 727)
PAE - RIGHT BS 727 BULKHEAD LOWER CHORD DISCOVERED CRACKED DURING ACCOMPLISHMENT OF FRONTIER ENGINEERING ORDER NR 53-10-737-004. REMOVED AND REPLACED LOWER SECTION OF CHORD IAW EO NR 53-10-737-001. (M)
Part: SKIN — CRACKED (FUSELAGE)
PAE - CRACK IN UPPER AFT CORNER OF L-3 WINDOW CUTOUT. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-30-3. (M)
1996
Part: STRINGER — CORRODED (BS 947-967)
PAE - FOUND CORROSION AROUND FASTENERS IN STRINGER 27R, BS 947-967 WL 173. REMOVED DAMAGED SECTION OF STRINGER 27R, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-3. (M)
Part: BULKHEAD WEB — CRACKED (BS 178)
PAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS REPLACED IAW BOEING SRM AND BOEING DRAWING NR 65-16300. REPLACEMENT ACCOMPLISHED ON TRAMCO MWO FUSELAGE 212. (M)
Part: BULKHEAD WEB — CRACKED (BS 663.75)
PAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES BELOW PRESSURE DECK IAW EWO 96-0606. LEAK CHECKED ALL ITEMS. REMOVED FOR ACCESS, NO LEAKS FOUND. REF TRAMCO WORK ORDER FUSELGE 175. (M)
Part: FLOORBEAM — CRACKED (BS 520)
PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS BS 520 WL 207.75, RBL 25 AND RBL 46. REPAIRED FLOORBEAM CRACK AT BS 520, WL 207.75, RBL 25 AND RBL 46 IAW EWO 396-0643. (M)
Part: CHORD — CRACKED (BS 727)
PAE - FOUND CRACK INDICATIONS IN LT BS 727, STRINGER 18A OUTBOARD CHORD FORWARD AND AFT OF BOTH FASTENER HOLES. ACCESSED REPAIR AREA. FOUND CRACKS CONTAINED IN FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PARTS FOR INTERIM REPAIR PER SB 737-53A1166. RE-INSTALLED ALL ITEMS REMOVED FOR ACCESS. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 289. (M)
Part: FLOORBEAM — CRACKED (BS 520)
PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS AT BS 520, WL 207.75, LBL 25 - LBL 47. REPAIRED CRACKS IN FLOORBEAM AT BS 520, WL 207.75, LBL 25, LBL 45 AND LBL 47 PER EWO NR 96-0643. (M)
Part: CHORD — CRACKED (BS 178)
PAE - HFEC INSPECTION OF THE BS 178 LT SIDE CHORD AT WL 194-196 SHOWS A CRACK INDICATION. CUT OUT DAMAGED AREA OF CHORD. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER TRAMCO EWO NR 96-0619. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 276. (M)
Part: KEELBEAM — CRACKED (BS 814-818)
PAE - FOUND CRACK IN THE AFT END OF RT KEELBEAM BS 814-818, STRINGER 27 RT. REPAIRED CRACK IAW TRAMCO EWO 96-0613. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 255. (M)
Part: CHORD — CRACKED (BS 540)
HFEC INSPECTION EXHIBITS CRACK APPROX 1.5 INCH LONG IN RADIUS OF BS 540 CHORD BETWEEN STRINGER 21R AND STRINGER 22R, CRACK IS ON SPLICE PLATE. ACCESSED AREA, REMOVED DAMAGED SPLICE PLATE. FABRICATED NEW SPLICE PLATE PER TRAMCO EO NR 96-0629. INSTALLED NEW SPLICE PLATE AND ALL ITEMS REMOVED FOR ACCESS. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 284. (M)
Part: FRAME — CORRODED (BS 520)
PAE - FOUND CORROSION (C53-208-01) ON AFT SIDE OF FRAME BS 520 RBL 7, WL 150. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FRAME PER SRM 51-40-3. (M)
Part: DOOR FRAME — CRACKED (CARGO DOOR)
PAE - HFEC INSPECTION OF THE FORWARD CARGO DOOR FRAME, REVEALED A CRACK INDICATION AT STRINGER 23R ON THE FORWARD SIDE OF THE FRAME AT THE LOWEST OUTBOARD CORNER OF THE DOOR STOP FITTING. ACCESSED INDICATED AREA AND FOUND NUMEROUS GOUGES LOCATED BENEATH DOOR STOP FITTING. BLENDED GOUGES AND OVERSIZED FASTENER HOLES FOR STOP FITTING. RE-INSTALLED ALL ITEMS REMOVED FOR ACCESS REF TRAMCO EWO NR 96-0655. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 277. (M)
Part: STIFFENER — CRACKED (BS 203.5)
PAE - FOUND CRACK EMANATING FROM FASTENER HOLE AT BS 540, WL 203.5, LBL 26 ON VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER AND INSTALLED PER SRM 57-10-02, SRM 51-30-02. WORK DOCUMENTED ON TRAMCO MWO INTERIOR 174. (M)
Part: FRAME — CRACKED (BS 294.5)
PAE - FOUND CRACK IN FRAME WEB AT UPPER CORNER OF STRINGER CUTOUT BS 294.5, STRINGER 18R. FOUND CRACK CONTAINED IN FASTENER HOLE. REPAIRED PER SRM 51-40-02 AND TRAMCO ER100396MW3. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 233. (M)
Part: SHEAR TIE — CORRODED (BS 360)
PAE - FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-10-4, FIG 8. DURING REPAIR, FOUND DAMAGE TO BONDED DOUBLER BENEATH SHEAR TIE. CUT OUT DAMAGED DOUBLER AND REPAIRED PER SRM 53-30-3, FIG 17. REF WORK ORDER FUSELAGE 292. (M)
Part: FRAME — CORRODED (BS 807)
PAE - FOUND CORROSION ON FORWARD AND AFT SIDE OF FRAME AND CORRODED AND CRACKED SHEAR TIE BS 807, LBL 25 - RBL 25, WL 148-153. REMOVED CORROSION FROM FRAME AND FOUND WITHIN LIMITS OF SRM. CUTOUT DAMAGED SHEAR TIES BETWEEN STRINGER 26-27L AND STRINGER 27L-27R AND REPAIRED PER SRM 53-10-04, FIG 10. DURING REPAIR FOUND CORROSION ON SKIN INNER SURFACE BENEATH SHEAR TIE BETWEEN STRINGER 27L-27R WITH EVIDENCE OF PREVIOUS REWORK. AFTER CORROSION REMOVAL FOUND SKIN OUT OF LIMITS PER SRM. CUTOUT DAMAGED SKIN AND REPAIRED PER SRM 53-30-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC FUSELAGE 252. (M)
Part: STRINGER — CRACKED (BS 296)
PAE - FOUND CRACK IN STRINGER 10 LEFT, BS 296, WL 256. REMOVED DAMAGED SECTION OF STRINGER 10L BS 296, WL 256. REPAIRED STRINGER IAW SRM 53-10-3 FIGURE 3 RED WORK ORDER INTERIOR 154. (M)
Part: STRINGER — CRACKED (BS 277)
FOUND CRACK IN STRINGER 14R AT BS 277. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC INTERIOR 178. (M)
Part: INTERCOSTAL — CRACKED (CARGO DOOR)
PAE - FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS ARE CRACKED ON THE AFT OTBOARD FLANGE. REMOVED AND REPLACED FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS IAW SRM 51-10-1, 51-10-2, 51-30-2, REF WORK ORDER DOORS 93. (M)
Part: FLOORBEAM — CORRODED (BS 500)
PAE - FOUND CORROSION ON UNDERSIDE OF CARGO FLOORBEAM BS 500, RBL 18, WL 156. REMOVED CORROSION ON UNDERSIDE OF FLOORBEAM AND REPAIRED IAW SRM 53-10-1, 51-40-3 REF WORK ORDER FUSELAGE 262. (M)
Part: STRINGER — CRACKED (BS 380)
PAE - FOUND CRACK IN STRINGER 27 LEFT AT BS 380 PLUS 12. CUTOUT DAMAGED AREA OF STRINGER AND REPAIRED PER SRM 53-10-03. WORK DOCUMENTED ON NRC FUSELAGE 291. (M)
Part: LANDING GEAR — DAMAGED (RT MLG)
ABQ - BLOCK TURN-BACK. FLIGHT CREW REPORTED APPARENT RT MLG DAMAGE. MAINTENANCE FOUND NR 4 MAIN WHEEL, BRAKE, AND AXLE ASSYS DAMAGED. REPLACED THE LOWER STRUT ASSY, NR 4 BRAKE ASSY, NR 3 AND NR 4 TIRE ASSYS, WHEEL BEARING, WHEEL BEARING THRUST WASHER AND NUT, TRANSDUCER AND AXLE NUT, AND REPAIRED WIRING HARNESS AND CANNON PLUG. THE CAUSE OF DAMAGE IS UNDER INVESTIGATION. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED AS ADDITIONAL INFORMATION IS OBTAINED. C-CHECK: 1242.5 HRS. (X)
Part: BEARING — FAILED (RT MLG)
ABQ - FLT 322 - BLOCK TURN BACK. CREW REPORTED APPARENT RT MLG DAMAGE. MAINT FOUND THE NR 4 MAIN WHEEL, BRAKE AND AXLE ASSEMBLY DAMAGED. REPLACED THE LOWER STRUT ASSEMBLY, THE NR 4 BRAKE ASSEMBLY, THE NR 3 AND NR 4 TIRE ASSEMBLIES, WHEEL BEARING, WHEEL BEARING THRUST WASHER AND NUT, AND AXLE NUT, AND REPAIRED THE WIRING HARNESS AND CANNON PLUG. THE FAILURE OF THE OUTB WHEEL BEARING PRECIPITATED FRACTURE. FRICTIONAL HEATING CAUSED THE LOCKING TAB ON THE WHEEL LOCK WASHER TO SHEAR OFF. WITH THE LOCK TAB SHEARED OFF, THE WASHER WAS FREE TO ROTATE WITH THE WHEEL IN THE CLOCKWISE DIRECTION. THE TORQUE LOAD WAS THEN APPLIED TO THE AXLE NUT CAUSING IT TO TIGHTEN.
1995
Part: COALESOR — DIRTY (LEFT)
SLC - AIR TURN BACK. UPON TAKEOFF, FLIGHT CREW REPORTED AN ODOR IN THE COCKPIT AFTER TURNING ON LEFT PACK. THE SMOKE DETECTOR IN THE FORWARD LAVATORY ACTIVATED AND THE AIRCRAFT WAS RETURNED TO SLT. MAINTENANCE INSPECTED THE AIRCRAFT INTERIOR AND THE AIR CONDITIONING BAY AREA AND CHECKED OK. PLACARDED LEFT PACK INOPERATIVE PER MEL 21-1 AND 21-2. UPON ARRIVAL IN DEN, MAINTENANCE REPLACED THE LEFT WATER SEPARATOR BAG AND SYSTEM CHECKED OK. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND SYSTEM CHECKED OK. (M)
Part: OIL TEMP BULB — FAILED (RT ENGINE)
OMA - AIR TURNBACK, FLIGHT CREW REPORTED HIGH OIL TEMPERATURE INDICATED ON RIGHT ENGINE. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO OMAHA. UPON ARRIVAL IN OMAHA, MAINTENANCE REPLACED THE OIL TEMPERATURE SENSING BULB, CHECKED AND CLEANED ELECTRICAL CONNECTIONS. THE AIRCRAFT GROUND CHECKED OK AND WAS FERRIED TO DENVER. IN DENVER, MAINTENANCE DISASSEMBLED AND CHECKED CONNECTORS AND WIRING BETWEEN THE OIL TEMPERATURE SENSING BULB AND THE OIL TEMPERATURE INDICATOR, AND CHECKED OK. PERFORMED OPERATIONAL CHECK OF ENGINE AND CHECKED OK. (M)