N571SC
Registered owner: GOSPEL MINISTRIES INTERNATIONAL INC, TN (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.
81 reports on file, 1995-02-04 – 1999-10-07.
Part: ENGINE — FAILED (NR 1)
FLT 102 - LAX - NR 1 ENGINE EXHAUST GAS TEMPERATURE CAUTION LIGHT CAME ON EARLY ON CLIMB-OUT, NR 1 THRUST HAD TO BE REDUCED TO MAINTAIN EXHAUST GAS TEMPERATURE LIMITS. REPLACED NR 1 ENGINE DUE TO BOROSCOPE DAMAGE FOUND. (M)
Part: LIGHT — INOPERATIVE (CABIN)
FLT 9001 - SFO - FORWARD RIGHT PORTION OF ZONE 'A' EMERGENCY LIGHTS FLOOR AISLE INOPERATIVE. ISOLATED SHORT CIRCUIT EMERGENCY (FLOOR AISLE) LIGHTS OPERATION CHECKS NORMAL. (M)
Part: SLIDE — DEPLOYED (L1 DOOR)
FLT 9154 - SLC, LEFT NR 1 DOOR SLIDE DEPLOYED INADVERTENTLY. DEFERRED IN SLC CLEARED IN LAX. REPLACED ESCAPE SLIDE/RAFT PACK. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
FLT 007 - SFO - ON PREFLIGHT CHECK NUMEROUS EMERGENCY LIGHTS FAILED TO TEST IN FORWARD CABIN. RIGHT FLOOR LIGHTS AND SEVERAL DOOR AND FORWARD BULKHEAD LIGHTS. REPLACED FAULTY BATTERY POWER SUPPLY BOX. (M)
Part: LIGHT — LOOSE (ROW 23C)
FLT 008 IN SFO, EMERGENCY FLOOR LIGHT STRIP UNDER SEAT 23C IS LOOSE. REINSERT EMERGENCY FLOOR LIGHT STRIPS, OPERATIONAL CHECK NORMAL. (M)
Earlier reports · 1995–1998 · 76 reports
1998
Part: SLIDE — FAILED (R4 DOOR)
DURING DEPLOYMENT OF THE R4 DOOR SLIDE FOR TRAINING PURPOSES THE SLIDE FAILED TO INFLATE FULLY.
Part: WIRE — FAILED (CABIN)
A SMOKE SMELL AT ROW 22ABC. FOUND WIRES BURNT UNDER SEAT 22E TRACK. TAPED AND INSULATED INDIVIDUAL WIRES AND UNPLUGGED UNDERSEAT BURNT DECODER HARNESSES. PLACED SEATS ON MEL. REMOVED AND REPLACED MUX CABLE AT SEAT 22C. SEATS OPERATIONALLY CHECK GOOD REMOVED MEL.
Part: PACK — SMOKING (CABIN)
THE NUMBER THREE PACK APPEARS TO CAUSE LIGHT SMOKE WHEN ON IN THE AFT PORTION OF THE AIRCRAFT. RAN NUMBER THREE PACK OFF AND ON SETTING. INSPECTED DUCT, FOUND NO DEFECTS AND NO RETURNED SMOKE. PACK SYSTEM FUNCTIONALLY CHECKS GOOD.
1997
Part: EGT HARNESS — INOPERATIVE (NR 1 ENGINE)
AFTER DEPARTURE FROM HNL AT FLIGHT LEVEL 320, NUMBER 1 EGT BEGAN FLUCTUATING. RETURNED TO HNL. REMOVED AND REPLACED LOWER LT THERMOCOUPLE HARNESS. FUNCTIONALLY TESTED GOOD.
Part: LAMP HOLDERS — SHORTED (GALLEY)
AFTER TAKEOFF, A GLOWING EMBER WAS OBSERVED FALLING FROM THE AREA OF THE CEILING LIGHT IN THE FORWARD GALLEY. REPLACED BOTH LAMP HOLDERS ON FORWARD GALLEY LIGHT, OPS CHECK GOOD.
Part: WIRE — FAILED (CABIN)
EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOP AT LEFT AISLE FROM ROW 36 TO ROW 43. FOUND WIRE PULLED AT SPLICE AND REPAIRED SPLICE. FUNCTIONALLY TESTED NORMAL.
Part: FIRE CONTL BOX — FAILED (NR 3 ENGINE)
DURING DESCENT INTO DTW, THE NR 3 ENGINE FIRE WARNING SOUNDED, SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE BOTTLES. POST FLIGHT INSPECTION REVEALED NO SIGNS OF FIRE. TROUBLESHOOTING FOUND THE DUAL FIRE DETECTION CONTROL BOX AT FAULT, REPLACED CONTROL BOX AND BOTH FIRE BOTTLES PER DC-10 MM 26-11-01 AND 26-21-01.
Part: MEGAPHONE — INOPERATIVE (L2 DOOR)
MEGAPHONE AT L2 WOULD NOT SELF TEST. REMOVED AND REPLACED MEGAPHONE.
Part: DOOR SLIDE — INOPERATIVE (L3 DOOR)
DOOR SLIDE LIGHT AT L3 DOOR DOES NOT PUSH TO TEST. REMOVED AND REPLACED WIRE HARNESS AND LIGHT ASSEMBLY. DOOR SLIDE LIGHT CHECKS GOOD IN ACCORDANCE WITH MM 25-61-03.
1996
Part: POWER SUPPLY — INOPERATIVE (CABIN)
AFT EMERGENCY POWER SUPPLY FAILED SELF TEST. REMOVED AND REPLACED AFT EMERGENCY EXIT POWER SUPPLY AND OPS CHECKED GOOD.
Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY)
LAV 7 SMOKE DETECTOR LIGHT INOP. RESECURED WIRES TO LIGHT SOCKET AND OPS TESTED NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECKED NORMAL.
Part: PIGTAIL — SHORTED (CABIN)
THE LEFT FORWARD EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. FOUND THE EMERGENCY LIGHT PIGTAIL SHORTED AT THE SECOND MODULE FROM THE LEFT, AFT SIDE OF THE LEFT FORWARD EMERGENCY TRACK LIGHTING STRIP.
Part: SKIN — CORRODED (BS 1361)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON CENTER WING BOX UPPER SKIN FRM RBL 30 TO RBL 80 AT BS 1361, AT AFT SPAR. OPENED ACCESS TO CENTER WING BOX, REMOVED CORROSION, INSTALLED NEW FASTENERS, AND PERFORMED LEAK CHECKS IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS.
Part: SUPPORT — CORRODED (BS 1997)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON OVERHEAD GILL LINER SUPPORT AT BS 1997, RBL 18. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 53-00-01.
Part: STRINGER — CRACKED (BS 1099-1119)
DURING HEAVY MAINTENANCE, FOUND STRINGER 48L CRACKED BETWEEN BS 1099 AND BS 1119. STOP DRILLED 1 INCH CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH SRM 53-00-01.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND FLOOR SUPPORT DAMAGED AT BS 1964, RBL 48. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 53-00-01.
Part: BRACKET — CORRODED (BS 435)
DURING HEAVY MAINTENANCE, FOUND MOUNTING BRACKET CORRODED AT BS 435 CENTER TIE DOWN FITTING. REMOVED AND REPLACED MOUNTING BRACKET IN ACCORDANCE WITH SRM 51-30-01.
Part: SEAT TRACK — CORRODED (BS 791-840)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON TOP FLANGE OF THE LEFT HAND INBOARD SEAT TRACK AT BS 791 TO 840. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR DOUBLER PER ENGINEERING ORDER.
Part: SEAT TRACK — CORRODED (BS 1960)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 1960, LBL 78. REMOVED DAMGED SEAT TRACK SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-31-01.
Part: SUPPORT — CORRODED (BS 1835-1887)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1835 TO BS 1887, LBL 40. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01.
Part: SUPPORT — CORRODED (BS 1923)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1923, LBL 13 TO RBL 13. REMOVED CORRODED SECTION OF SUPPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-10-00 AND SRM 51-31-00.
Part: SUPPORT — CORRODED (BS 1921)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 13. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-31-00.
Part: SUPPORT — CORRODED (BS 1887)
DURING HEAVY MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, BL ZERO TO RBL 90. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01.
Part: SUPPORT — CORRODED (BS 1909)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1909, RBL 53 TO RBL 85. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01.
Part: SUPPORT — CORRODED (BS 1871)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1871 RBL 64 TO RBL 90. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01.
Part: SUPPORT — CORRODED (BS 1887-1920)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887 TO BS 1920, BL 0. REMOVED CORRODED SECTION OF SUPPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-31-00.
Part: BRACKET — CORRODED (G4 GALLEY)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON G4 GALLEY ATTACH BRACKET. FABRICATED AND INSTALLED A NEW ATTACH BRACKET IN ACCORDANCE WITH SRM 51-21-01.
Part: SUPPORT — CORRODED (BS 1921)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 20 TO RBL 49. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-21-00.
Part: SEAT TRACK — CORRODED (BS 1800)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1800, RBL 67 TO BS 1887, RBL 59. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-70-00.
Part: SUPPORT — CORRODED (BS 1900-1921)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1900 TO 1921, LBL 13. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-30-00.
Part: SEAT TRACK — CORRODED (BS 1887-1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK BETWEEN BS 1887 AND BS 1964, RBL 88 TO RBL 78. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK IN ACCORDANCE WITH 53-70-00.
Part: SEAT TRACK — CORRODED (BS 1835)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1835 LBL 65 TO BS 1887, LBL 60. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-70-00.
Part: SEAT TRACK — CORRODED (L1 DOOR)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK UNDER L1 DOOR THRESHOLD. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION IN ACCORDANCE WITH ENGINEERING AUTHORIZATION.
Part: SUPPORT — CORRODED (BS 1901)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1901, LBL 53 TO LBL 86. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01.
Part: SUPPORT — CORRODED (BS 1921-1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921 TO BS 1964, LBL 18. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-30-00.
Part: SEAT TRACK — CORRODED (BS 420)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 420, LBL 53. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS.
Part: SUPPORT — CORRODED (BS 1887)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1887 LBL 75. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: FLOOR SUPPORT — CORRODED (BS1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOOR SUPPORT AT BS 1964, RBL 39. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: SUPPORT — CORRODED (BS 1887)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, LBL 33. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: SUPPORT — CORRODED (BS 1887)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, LBL 45. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964, LBL 64. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-42-00.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, RBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964 RBL 64. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-21-03.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964 RBL 46. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-42-00.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964, LBL 46. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-40-00.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 39. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-16-01.
Part: SUPPORT — CORRODED (BS 1835-1837)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1835 - BS 1837, RBL 39. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: BRACE — CRACKED (WS 130)
DURING HEAVY MAINTENANCE FOUND SUPPORT BRACE CRACKED AT LEFT WING FRONT SPAR, STA XORS 130, INBOARD OF NR 1 SLAT, NR 3 TRACK. REMOVED SUPPORT BRACE, FABRICATED AND INSTALLED A NEW BRACE IN ACCORDANCE WITH SRM 53-00-01.
Part: SUPPORT — CORRODED (BS 1139)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT AFT END OF FORWARD CARGO COMPARTMENT, BS 1139, RBL 7 TO RBL 22. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-01.
Part: ACTUATOR ROD — CORRODED (LT ELEVATOR)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE LEFT HAND ELEVATOR ACTUATOR ROD. REMOVED AND REPLACED LEFT HAND ELEVATOR ROD IN ACCORDANCE WITH MM 27-33-01.
Part: FLOOR SUPPORT — CORRODED (BS 879)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON THE LEFT SIDE OF THE P-LIFT, APPROXIMATELY BS 879, OUTBOARD SIDE OF THE FLOOR BOARD. REMOVED CORRODED MATERIAL, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS.
Part: FLOOR SUPPORT — CORRODED (BS 839)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON THE LEFT SIDE OF THE P-LIFT, APPROXIMATELY BS 839, INBOARD SIDE OF THE FLOOR BOARD. REMOVED CORRODED MATERIAL, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS.
Part: SUPPORT — CORRODED (BS 1964)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT JUST FORWARD OF THE FLOOR BEAM AT BS 1964, RBL 22. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-30-00.
Part: SUPPORT — CORRODED (BS 1871)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BODY STATION 1871, LBL 63. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-30-01.
Part: ANGLE — CORRODED (CARGO DOOR)
DURING HEAVY MAINTENANCE, FOUND CORRODED ANGLE ON INSIDE CORNER OF AFT CARGO DOOR. REMOVED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IN ACCORDANCE WITH SRM 51-21-01 AND SRM 5121-02.
Part: SUPPORT — CORRODED (BS 1871)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1871, LBL 40. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-21-01 AND SRM 51-30-00.
Part: FLOORBEAM — CORRODED (BS 1921)
DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FOUR NUTPLATES ON STATION 1921 FLOOR BEAM, FROM LBL 20 TO LBL 38. REMOVED CORRODED SECTION OF FLOOR BEAM, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR BEAM IN ACCORDANCE WITH SRM 51-31-00.
Part: SUPPORT — CORRODED (BS 1600)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON LEFT HAND SIDE AT BS 1600. REMOVED, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.
Part: FRAME — CRACKED (BS 1119)
DURING HEAVY MAINTENANCE, FOUND A CRACK ON THE LOWER FLANGE OF A FRAME AT BS 1119, BETWEEN LONGERONS 49L AND 50R. REMOVED DAMAGED FLANGE CLIP AND INSTALLED A NEW FLANGE CLIP IN ACCORDANCE WITH SRM 53-30-00 FIGURE 5.
Part: SUPPORT — CORRODED (BS 836)
DURING HEAVY MAINTENANCE, FOUND CORROSION ON LEFT HAND CABIN FLOOR STRUCTURE, APPROXIMATELY STATION 836 AND 18 INCHES LEFT OF THE C-LIFT. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR PER ENGINEERING ORDER INSTRUCTIONS AND SRM CHAPTER 51.
Part: SUPPORT — CORRODED (BS 834)
DURING HEAVY MAINTENANCE FOUND CABIN FLOOR STRUCTURE CORRODED FROM C-LIFT TO FLOOR SUPPORT HAT CHANNEL ASSEMBLY, BS 834. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A SUPPORT ANGLE IN ACCORDANCE WITH SRM 51-31-01.
Part: LIGHT — INOPERATIVE (CABIN)
EMERGENCY TRACK LIGHTING IS INOPERATIVE AT ROW 6, BOTH SIDES. REPAIRED BROKEN WIRE IN TRACK ON BOTH SIDES. TRACK LIGHTING CHECKED GOOD PER 33-50-00.
Part: FIRE BOTTLE — DISCHARGED (NR 2 ENGINE)
NUMBER 2 ENGINE AGENT LOW LIGHT CAME ON IN FLIGHT. FOUND NUMBER 2 BOTTLE THERMAL DISCHARGED. REMOVED AND REPLACED BOTTLE PER MM 26-21-02, FOUND NO AIR LEAKS.
Part: SMOKE DETECTOR — FAILED (NR 1 LAV)
THE NUMBER 1 LAVATORY SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED THE NUMBER 1 LAVATORY SMOKE DETECTOR AND NEW DETECTOR OPS CHECKED GOOD.
Part: SMOKE DETECTOR — MALFUNCTIONED (NR 1 LAV)
THE NUMBER 1 LAV WAS FOUND TO BE INOPERATIVE. OPS CHECKED NUMBER 1 LAV SMOKE DETECTOR PER DC10 MM 26-00 AND NO DEFECTS WERE NOTED.
1995
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY FLOOR PATH LIGHTING WAS FOUND INOPERATIVE IN THE MID CABIN. REMOVED AND REPLACED MID CABIN BATTERY PACK IAW MM 33-51-01 AND LIGHTS OPS CHECKED NORMAL.
Part: EEL BATT CHARGER — FAILED (CABIN)
THE LEFT, AFT CABIN EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY PATH LIGHTING BATTERY CHARGER IAW MM 33-50-00 AND LIGHTS TESTED GOOD.
Part: EEL POWER SUPPLY — FAILED (CABIN)
AFT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR AFT EMERGENCY LIGHTS. ALL LIGHTS TEST GOOD.
Part: EEL POWER SUPPLY — FAILED (AFT EMER EXIT)
AFT EMERGENCY LIGHT POWER SUPPLY FAILS COCKPIT SELF-TEST. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPPLY (OVERHEAD) PER MM 33-51-01. OPS CHECKED GOOD.
Part: EEL MODULE — MALFUNCTIONED (CABIN)
CENTER CABIN, LEFT FLOOR EMERGENCY LIGHTING TRACK MODULE INOPERATIVE. REPAIRED DAMAGED WIRE AT MODULE. OPS CHECK GOOD.
Part: COALESCER BAG — FAULTY (NR 1 PACK)
ON THE GROUND IN DFW, WHEN NR 1 PACK WAS TURNED ON USING ONLY THE APU, A VISIBLE HAZE AND FUMES WERE NOTICED IN THE COCKPIT AND LOWER GALLEY. REMOVED AND REPLACED COALESCER BAG IAW MM 21-54. RAN PACKS FOR 30 MINUTES AT VARIOUS TEMP SETTINGS, NO ODOR OR FUMES NOTED.
Part: HYD LINE — CHAFED (NR 2 HYD)
NUMBER 2 HYDRAULIC SYSTEM WENT TO '0' QUANTITY DURING FLIGHT. FOUND PRESSURE BOOTSTRAP LINE CHAFED IN MAINTENANCE BAY FORWARD OF APU DOOR, PANEL NR 311AB. TEMPORARILY REPAIRED BY INSTALLING FLEX LINE IAW BMM 6-15-10 SECURED LINE, RAN A/C PUMPS AND PRESSURIZED NR 2 SYSTEM USING ENGINE PUMPS, NO LEAKS NOTED. SERVICED TO 8 GALLONS PRIOR TO RUN. CHECKED ALL FILTER DELTA PINS, NO DEFECTS NOTED.
Part: B-NUT — UNSECURE (NR 2 HYD SYS)
ONE HOUR INTO FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY WENT TO .5 GALLON WITH ALL OTHER INDICATIONS NORMAL. DURING FLAP EXTENSION FROM 15 TO 22 DEGREES, NR 2 HYDRAULIC QUANTITY DROPPED TO NEAR ZERO, AND BOTH LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 2 HYDRAULIC SUPPLY LINE LEAKING AT FIRE SHUTOFF VALVE. RESECURED B-NUT, RESERVICED SYSTEM, AND LEAK CHECKED GOOD.
Part: MAIN ENG CONTL — FAULTY (NR 1 ENGINE)
SJC - FLT 39 - DURING INITIAL POWER REDUCTION AT 33,000 FEET, THE NR 1 ENGINE COMPRESSOR STALLED. AT 20,000 FEET UPON INCREASE IN POWER, NR 1 ENGINE STALLED AGAIN. POWER WAS REDUCED TO IDLE, MAX TEMP DURING STALL WAS 800 DEGREES. PERFORMED BORESCOPE OF LPT, HPT. AND HIGH STAGE COMPRESSOR. FOUND TO BE OK. REPLACED CIT SENSOR. REMOVED AND REPLACED MEC AND RIGGED VARIABLE STATOR VANE SYSTEM IAW 73-20-01. OPERATED ENGINE IAW 71-00-TO 100 PERCENT POWER ASSURANCE AND ALL PARAMETERS WITHIN LIMITS. (W)