N29UA
Registered owner: N29NY LLC, NJ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| N29NY LLC | Operator | on 2026-01-08 | Operator named in NTSB report |
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.
68 reports on file, 1995-04-05 – 2003-09-08.
Part: SPAR CAP — CRACKED (NR 4 PYLON) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON LT LOWER SPAR CAP WITH CRACK STA YOP 251 BY ACCESS DOOR NR 411.
Part: ANGLE — CRACKED (SPAR CAP) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON STUB WING BELOW LT SPAR CAP (Z) ANGLE WITH CRACK.
Part: SPAR CAP — CRACKED (NR 2 PYLON) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON LT CENTER SPAR CAP WITH CRACK STA YIP 235.
Part: ANGLE — CRACKED (NR 3 PYLON) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YIP NR 227 RT SIDE ANGLE WITH CRACK.
Part: FITTING — CRACKED (NR 3 PYLON) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON UPPER SECTION, FRONT SPAR AND FOOT STOOL SPLICE FITTING WITH 3 INCH CRACK.
Part: WEB — CRACKED (NR 1 PYLON) · airframe 53,883 hrs · 28,040 cycles
NR 188. DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 1 PYLON BETWEEN STATION YOP NR 226 AND STATION YOP NR 243 UPPER WEB DOUBLER WITH CRACKS. CORRECTIVE ACTION:
Part: SPAR CAP — DAMAGED (NR 4 PYLON) · airframe 53,883 hrs · 28,040 cycles
DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON INTERIOR STA YOP 225 LT LOWER SPAR CAP WITH STACK, BY ACCESS DOOR NR 426.
Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 53,824 hrs · 28,023 cycles
DURING FINAL APPROACH, AFTER GEAR EXTENSION, NOSE LANDING GEAR LIGHT DID NOT ILLUMINATED. RETARDING POWER LEVERS CAN'T GET THE AURAL WARNING TO COME ON. EXECUTED GO-AROUND, DURING GO AROUND NOSE LANDING GEAR LIGHT STARTED TO FLICKER. VISUAL INSPECTION OF THE NOSE GEAR DOWN AND LOCK MARKINGS DISPLAYED LOCKED POSITION. FLIGHT LANDED UNEVENTFUL. VISUAL CHECK NOSE GEAR, FOUND ALL OK. ADJUSTED NOSE GEAR DOWN AND LOCK PROX. SENSOR. TESTED SYSTEM AS IAW MM 32-60-0 PAR. 3B, NO GEAR SWING REQUIRED.
Part: WIRE — CHAFED (OIL PRESS IND)
AFTER TAKE-OFF NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED ACCOMPLISHED APPROPRIATE CHECKLISTS, AND RETURNED TO SJU. REMOVED AND CHECKED NR 1 ENGINE MAIN OIL FILTER, FOUND OK. RE-INSTALLED FILTER, FOUND TWO WIRES WERE CHAFING WITH COWLING SPLICE AND RE-ROUTED. ENGINE RUN PERFORMED, ALL CHECK NORMAL IAW MM 71-00 - 79-32-2 AND MM 20-50-1
Part: LINE — LEAKING (HYD SYSTEM) · airframe 53,632 hrs · 27,928 cycles
LOSS OF HYDRAULIC FLUID DOWN TO STAND-PIPE. LOSS OF HYDRAULIC CHECK LIST COMPLETED. INSPECTED NR 3 PYLON FOR EVIDENCE OF HYDRAULIC LEAK, FOUND RIGID LINE DAMAGED INSIDE PYLON AREA; REMOVED AND REPLACED RIGID LINE ASSEMBLY AS REQUIRED IAW MM 20-12-0; OPERATIONAL CHECK NORMAL IAW MM 29-00 AND MM 29-10-12; NO LEAKS FOUND. SERVICED RESERVOIR IAW 12-30-1.
Part: LINE — LEAKING (NR 2 ENGINE) · airframe 53,538 hrs · 27,884 cycles
DURING CRUISE, LOST HYDRAULIC QUANTITY FOLLOWED THE LOSS OF HYDRAULIC FLUID OR PRESSURE. ABNORMAL OR EMERGENCY CHECKLIST. REMOVED AND REPLACED FLEX HYDRAULIC LINE ON NR 2 ENGINE PER MM 29-10-12. RUN UP CHECK ACCOMPLISHED AS PER MM 71-00-0 NO LEAK FOUND IT AT NORMAL.
Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 53,325 hrs · 27,788 cycles
ON PRE-FLIGHT, LOWER CARGO SMOKE DETECTOR MAINTENANCE LIGHT ON. ENTERED ON DMI 17527 IAW MEL 26-10-1-1A. REMOVED AND REPLACED LOWER SMOKE DETECTOR UNIT (SDU) FA 16037. OPERATIONAL CHECK IAW STC ST00746LA-D FOUND NORMAL. CLEARED DMI # 17527 AND REMOVED PLACARD.
Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 53,303 hrs · 27,773 cycles
ON PRE-FLIGHT FOUND FORWARD "A" BELLY LOWER CARGO SMOKE DETECTOR INOPERATIVE. ENTERED ITEM ON DMI 17493 AS PER MEL 2G-10-1-0-1 CAT "B". REMOVED AND REPLACED SMOKE DETECTOR UNITS (SDUS) S/N 4566, 14470 & 13067 AS PER STC ST00746LA-D. OPERATIONAL CHECK GOOD. THIS CLEARS DMI 17493 (FORWARD A BELLY INOP LOWER CARGO SMOKE DETECTOR. SYSTEM CHECK NORMAL IAW STC # ST00746LA-D.
Earlier reports · 1995–2002 · 55 reports
2002
Part: HYDRAULIC LINE — LEAKING (NR 2 ENGINE) · airframe 52,675 hrs · 27,491 cycles
LOSS OF HYDRAULIC FLUID IN FLIGHT, PERFORMED EMERGENCY CHECKLIST AND LANDED IN MIA WITHOUT FURTHER INCIDENT. FOUND NR 2 ENGINE HYDRAULIC CASE DRAIN LINE LEAKING. REMOVED & REPLACED LINE IAW MM 20-12-0. SERVICED HYDRAULIC FLUID IAW MM 12-30-1, PREFORMED LEAK CHECK OF ENGINE IAW MM 71-00 & 29-00, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 52,266 hrs · 27,296 cycles
ON CLIMBOUT OF MIAMI AT 17,000 FEET F/O ARTIFICIAL HORIZON FAILED WITH ATTITUDE FLAG. RETURNED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING AT 273,000 LBS. WIRING CHECK ACCOMPLISHED IAW MM 34-2-2. REMOVED AND REPLACED 2 AMP C/B B10-58 AND NR 2 ADI AS PER MM 20-50-1 & 34-25-0, ALSO REMOVED AND REPLACED NR 2 INSTRUMENT AMPLIFIER. NR 2 HORIZON & COMPASS SYSTEM GROUND TEST NORMAL IAW MM 34-25-0 & 34-21-0. TEST FLIGHT FOUND NR 2 HORIZON SYSTEM OPERATING NORMAL. AIRCRAFT RETURNED TO SERVICE.
Part: GYRO — FAILED (NR 2)
AT START OF TAKEOFF ROLL F/O ARTIFICIAL HORIZON FAILED WITH FLAG, REJECTED TAKEOFF AT 40 KNOTS AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 VERTICAL GYRO IAW MM 34-25-0. GROUND TEST OK. AIRCRAFT RETURNED TO SERVICE.
Part: BLEED VALVE — SEIZED (NR 4 ENGINE) · airframe 52,226 hrs · 27,276 cycles
ENGINE NR 4 UNABLE TO SPOOL TO MAX POWER DURING TAKEOFF. REMOVED AND REPLACED ENGINE BLEED VALVE IAW MM 75-30-3; OPERATIONS CHECKED NORMAL IAW MM 71-00.
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 60,467 hrs · 51,012 cycles
AT BEGINNING OF TAKEOFF, ROLL SPOILER EXTENDED, LIGHT ILLUMINATED. ABORTED TAKEOFF. PERFORMED VISUAL INSPECTION OF SPOILERS DEPLOY SWITCHES AND MECHANISM; CLEANED CONNECTOR TO MICRO-SWITCH PERFORMED OPERATIONAL CHECK IAW MM 27-61-0 AND 27-63-0. OPERATIONAL CHECK ON THE GROUND NORMAL.
Part: HYDRAULIC LINE — LEAKING (NR 2 ENGINE) · airframe 52,092 hrs · 27,213 cycles
AT 2225Z IN CLIMBING, HYDRAULIC QUANTITY DROPPED TO STAND PIPE PRESSURE DROPPED TO ZERO RETURNED TO KMIA. PERFORMED LOSS HYDRAULIC PRESSURE EMERGENCY CHECKLIST ON HYDRAULIC FLUID; PERFORMED EMERGENCY CHECKLIST ON HYDRAULIC CHECK, NO FURTHER LOSS OF FLUID. USED ABNORMAL LANDING CHECKLIST. FOUND HYDRAULIC HOSE ASSY LEAKING AT NR 2 ENGINE; REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE HOSE ASSY AND REPLACED DRAIN CASE FILTER IAW MM 70-30-2 AND MM29-10-14; NO LEAKS NOTED ON RUN-UP IAW MM 71-0 AND MM 29-00. OPS FOUND NORMAL AND SERVICED HYDRAULIC SYSTEM IAW MM 12-30-1.
Part: PROXIMITY SWITCH · airframe 51,827 hrs · 27,083 cycles
LOG PAGE # 108372. DISCREPANCY: GEAR NOT LATCHED, DOOR NOT LATCHED, LIGHTS ILLUMINATED. ON LEFT MAIN LANDING GEAR NO DOWN LIGHTS. CORRECTIVE ACTION: REMOVED AND INSTALLED LEFT MAIN GEAR PROXIMITY SWITCH SENSOR. ACCOMPLISHED ADJ & TEST POSITION & WARNING SYSTEM IAW MM 32-60-0. ALL NORMAL.
Part: SPAR — CRACKED (LT WING) · airframe 51,814 hrs · 27,078 cycles
DURING C-CHECK, LEFT WING STA XW 60 AUXILIARY SPAR LUG WITH CRACK, ADJACENT TO MLG TRUNNION FITTING. REMOVED AND REPLACED AUXILIARY SPAR IAW DRAWING 5616128.
Part: GCU — FAILED (NR 4 ENGINE) · airframe 51,747 hrs · 27,047 cycles
DURING APPROACH NR 4 GENERATOR UNPARALLEL LIGHT AND BUS POWER FAIL LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. AIRCRAFT LANDED AT DESTINATION UNEVENTFUL. RESET NR 4 GENERATOR SYSTEM IN ACCORDANCE WITH MM 24-5-1 ENTERED ON DMI 16156 PER MEL 24-1 GEN NR 4 INOP. REMOVED AND REPLACED GENERATOR CONTROL UNIT IAW MM 24-20-1, OPS CHECK NORMAL. DMI CLEARED ON LOG PAGE 107253.
2001
Part: FILTER HOUSING — DEFECTIVE (NR 4 ENGINE) · airframe 51,730 hrs · 27,039 cycles
NR 4 ENGINE OIL PRESSURE ERRATIC FLUCTUATES BETWEEN 0 TO 20 PSI WITH OIL PRESSURE LIGHT ON. ENGINE SHUTDOWN AS PER ABNORMAL CHECKLIST AND PROCEDURES. AIRCRAFT LANDED UNEVENTFUL. REMOVED AND REPLACED GEARBOX IAW MM 72-00. ACCOMPLISHED RUN UP, NO LEAKS NOTED. OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED OIL FILTER HOUSING. ACCOMPLISHED RUN UP IAW MM 71-00. OIL PRESSURE NORMAL AND NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: TRANSMITTER — ERRATIC (NR 4 ENGINE) · airframe 51,728 hrs · 27,038 cycles
NR 4 OIL PRESSURE WENT TO 0 PSI AFTER TOP OF DESCENT, NR 4 OIL PRESS LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN. BLED NR 4 ENGINE OIL SYSTEM, REMOVED AND REPLACED MAIN OIL FILTER IAW P&W 72-0, FOUND OIL PRESS XMTR ERRATIC, R&R IAW MM 79-32-1, OPS CKD DURING ENGINE RUN UP OK IAW MM 71-00. AIRCRAFT RETURNED TO SERVICE.
Part: BRAKE — SEIZED (MLG) · airframe 51,605 hrs · 27,000 cycles
NR 2 MAIN LANDING GEAR BRAKE ASSEMBLY LOCKED-UP CAUSING NR 2 TIRE TO BLOW. BRAKE TEMPERATURE CHECK AND WITHIN LIMITS. REMOVED AND REPLACED NR 2 MAIN GEAR BRAKE ASSEMBLY IAW DC-8 MM 32-42-1. REMOVED AND REPLACED NR 2 MAIN GEAR WHEEL AND TIRE ASSEMBLY IAW MM 32-40-1. REMOVED AND REPLACED NR 1 MAIN GEAR WHEEL AND TIRE ASSEMBLY IAW MM 32-40-1.
Part: HYDRAULIC LINE — LEAKING (LT MLG)
AFTER T/O LOST HYDRAULIC FLUID TO STAND PIPE AND PRESS 0, PERFORMED LOSS OF HYDRAULIC FLUID AND PRESS CHECKLIST AND RETURNED TO MIAMI. LANDED IN MIAMI OVERWEIGHT AT 272,600 WITHOUT INCIDENT. FOUND LT MLG BUNGEE CYLINDER PRESSURE LINE LEAKING. REMOVED AND REPLACED LINE IAW MM 20-12-0, SERVICED HYDRAULIC SYSTEM IAW MM 12-30-1. PERFORMED LEAK CHECK IAW MM 29-00 FOUND NORMAL NO LEAK NOTED. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION A-INSPECTION IAW FA DC8 MM J/C 6100, NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
Part: STRINGER — CRACKED · airframe 51,084 hrs · 26,724 cycles
DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.CORRECTIVE ACTION:REPAIRED I.A.W. E.O. DRAWING # AS11300 DATED 08/09/01
Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,084 hrs · 26,724 cycles
DURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.REPAIRED IAW EO DRAWING NR AS11300 DATED 08/09/01
Part: CONTROL BOX — FAILED (MLG) · airframe 50,572 hrs · 26,460 cycles
ON GEAR DOWN HAD NO RIGHT MAIN GEAR GREEN LIGHT AND HAD GEAR NOT LATCHED AND DOOR NOT LATCHED RED LIGHTS ON. EMERGENCY CHECK LIST ACCOMPLISHED PLUS SEVERAL CYCLES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX. INDICATION SYSTEM WORK NORMAL IAW 32-60-0. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW 32-30-1, FOUND ALL INDICATION NORMAL.
2000
Part: DOOR LATCH — LACK OF LUBE (LANDING GEAR)
LANDING GEAR DOORS NOT LATCHED LIGHT ON AFTER GEAR RETRACTION - PERFORMED ABNORMAL CHECK-LIST CYCLED GEAR SEVERAL TIMES. PERFORMED OVERWEIGHT LANDING. CHECKED BOTH MLG DOOR UPLATCHES MECHANISM. BOTH FOUND NORMAL. CLEANED PROXIMITY SWITCHES AND LUBRICATED MECHANISM. OP'S CHECK NORMAL IAW MM 32-60-00 AND 32-31-4. ACCOMPLISHED OVERWEIGHT INSPECTION; NO DEFECTS NOTED IAW ARROW AIR DC8 MM J/C 6100.
Part: LIGHT — INOPERATIVE (COCKPIT)
WHILE ON THE GROUND AT SAN JUAN, CREW REPORTED EMERGENCY LIGHTS FAILED TO DISARM TEST. RESET EMERGENCY LIGHT C/B, OPERATIONAL CHECK NORMAL IAW MM 33-50-2. (M)
1999
Part: FIRE LOOP — LOOSE (NR 4)
NR 4 ENGINE FIRE WARNINGS CAME ON AFTER REACHING 3,000 FT FOLLOWED EMERGENCY CHECKLIST IAW FINE AIR POLICY. TROUBLESHOOT SYSTEM AND FOUD LOWER ENGINE FIRE LOOP LOOSE. RE-SECURED LOOP IAW MM 26-10-1. (M)
Part: FLOORBEAM — CORRODED (BS 1680)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA FS 1680. REPAIRED CORROSION DAMAGE IAW WITH FINE AIRLINES EA NR G5310-05:00, SEMAN EO 9908241.
Part: SPAR — CORRODED (RT AND LT WING)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON VERTICAL FIN ON LT AND RT REAR SPAR AT STA ZR 45. REPAIRED CORROSION DAMAGE IAW FINE LINES EA NR G5531-01:00, SEMAN EO NR 990092 AND BOEING MESSAGE M-7200-99-08438.
Part: PANEL — CORRODED (WS 408)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON RT WING AT INNER AFT PLATING PANEL AT STA XW 408 BETWEEN STRINGERS 5 AND 7. REPAIRED CORROSION DAMAGE IAW FINE AIR EA NR G5730-08:00, SEMAN EO 990103 AND BOEING MESSAGE M7200-99-08364.
Part: PANEL — CRACKED (LT WING)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CRACK AND CORROSION ON LT WING INNER AFT PLATING PANEL AT STA XRS 69 AFT OF REAR SPAR. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-07:00, SEMAN EO NR 990101 AND BOEING MESSAGE M-7200-99-08151.
Part: SKIN — CORRODED (BS 742)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA 742, LONGERON L1. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-11:00, SEMAN EO NR 990085 AND BOEING MESSAGE M-7200-99-08106.
Part: FITTING — CORRODED (BS 879.375)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, FITTING ON RIGHT LONGERON CORROSION DAMAGE AT STATION 879-375 IN RIGHT WHEEL WELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. (M)
Part: FITTING — CORRODED (BS 960)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 960 IN LT WHEELWELL. REPAIRED CORORSION DAMAGE IAW SRM 53-2-0.
Part: SKIN — CORRODED (BS 1260)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 1260, BETWEEN LONGERSONS L1 AND L2 RIGHT. REPAIRED CORROSION DAMAGE IAW FINE ARLINES EA NR G5313-06:00, SEMAN EO NR 990097 AND BOEING MESSAE M-7200-99-07702.
Part: FITTING — CORRODED (BS 879.3)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 879.375 IN LT WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0.
Part: LONGERON — CRACKED (BS 960-980)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT LONGERON 24 CRACKED BETWEEN STA 960 AND STA 980 IN LT WHEELWELL. REPAIRED CRACK IAW FINE LINES EA NR G5313-12:00, SEMAN EO NR 990089 AND BOEING MESSAGE M-7200-99-06994.
Part: PANEL — CORRODED (RT WING)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT WING CORRODED AT OUTER WING OUTBOARD OF EXTENDED LEADING EDGE AT STA XFS 710. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5754-01:00, SEMAN EO NR 990096 AND BOEING MESSAGE M-7200-99-08383 AND M-7200-99-08600.
Part: PANEL — CORRODED (WS 408)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION ON LEFT WING AT INNER AFT TOP PANEL PLATING AT STATION XW 408 STRINGER 5. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-06:00, SEMAN EO NR 990104 AND BOEING MESSAGE M-7200-99-07795. (M)
Part: FITTING — CORRODED (BS 940)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, FITTING ON RIGHT LONGERON 24 CORROSION DAMAGE AT STATION 940 IN RIGHT WHEEL WELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. (M)
Part: FITTING — CORRODED (BS 960)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON RT LONGERON 24 CORROSION DAMAGED AT STA 960 IN RT WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-20-0.
Part: FITTING — CORRODED (BS 940)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 940 IN LR WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0.
Part: PANEL — CRACKED (LT WING)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT WING INNER AFT TOP PANEL PLATING CRACKED AND CORRODED AT STA XW 408 BETWEEN STRINGERS 2 AND 3. REPAIRED CRACK IN WING IAW FINE AIRLINES EA NR G5730-04:00, SEMAN EO NR 990095 AND BOEING MESSAGE M-7200-99-07795.
Part: SPAR — CORRODED (WS 763)
DURNG C-CHECK INSPECTION, FOUND THE FOLLOWING, RIGHT WING HAS CORROSION DAMAGE ON REAR SPAR AT STATINO XRS 763. REPAIRED CORROSION DAMAGE AT RIGHT WING XRS 763 IAW FINE AIRLINES EA NR G5711-01:00. SEMAN EO NR 990083 AND BOEING MESSAGE SEU-LIM-99-00023H. (M)
Part: SKIN — CORRODED (BS 857)
DURING C-CHECK, INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 857 BETWEEN LONGERONS L1 AND L2 RIGHT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-08:00, SEMAN EO NR 990098 AND BOEING MESSAGE SEU-LIM-99-00016H.
Part: LONGERON — CRACKED (BS 960-980)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LEFT LONGERON 24 WITH TWO CRACKS BETWEEN STA 960 AND STA 980. REPAIRED CRACKS IAW FINE AIRLINES EA NR G5313-03:00, SEMAN EO NR 990088 AND BOEING MESSAGE M7200-99-06994.
Part: SKIN — CORRODED (BS 940)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION AT STA 940.000 AND BETWEEN LONGERONS L1 AND L2 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-09:00, SEMAN EO NR 990091 AND BOEING MESSAGE M-7200-99-07538.
Part: SKIN — CRACKED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT PASSENGER DOOR, LOWER AFT JAMB CORNER CRACKED. REPAIRED CRACK DOOR IAW FINE AIRLINES EA NR G5320-01:00; SEMAN EO NR 990082 AND BOEING MESSAGE M-7200-99-07463
Part: SKIN — CORRODED (BS 680-702)
DURING C-CHECK, INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA FS 680 TO STA FS 702 BETWEEN LONGERONS L4 LT TO L6 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-02:00, SEMAN EO NR 990080 AND BOEING MESSAGE M7200-99-07382.
Part: SKIN — CORRODED (BS 898-911)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 898 TO STA 911 BETWEEN LONGERONS L2 LT AND L4 RT. REPAIRED FUSELAGE CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-05:00, SEMAN EO 990099 AND BOEING MESSAGE SEU-LIM-99-00019H.
Part: FITTING — CRACKED (RT MLG)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RIGHT MAIN LANDING GEAR TRAPEZOIDAL SUPPORT FITTING WITH FOUR CRACKS AT STA 868 IN RT WHEELWELL. REPAIRED CRACKS IAW SEMAN EO NR 9900990 AND BOEING MESSAGE M-72-00-99-06884. FINE AIRLINES EA NR G3211-01:00.
Part: SKIN — CORRODED (BS 980)
DURING C-CHECK INSPECTION, FOUND FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 980, BETWEEN LONGERONS L2 LT AND L2 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-07: 00, SEMAN EO NR 990093 AND BOEING MESSAGE M-7200-99-07595.
Part: SKIN — CORRODED (BS 717)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA 717 BETWEEN LONGERONS L1 TO L2, LT. REPAIRED CORROSION DAMAGE IAW WITH FINE AIRLINES EA NR G5313-10:00, SEMAN EO NR 990084 AND BOEING MESSAGE M-7200-99-08106.
Part: SKIN — CRACKED (LT WING)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION AND CRACK ON LT WING INNER EXTENDED LEADING EDGE AT LOWER SKIN BETWEEN STA FS 304 TO XFS 341. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-03:00, SEMAN EO NR 990102 AND BOEING MESSAGE SEU-LIM-99-0025H.
Part: FLOORBEAM — CORRODED (BS 920)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA BS 920 APPROXIMATELY LBL 45. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5310-06:00, SEMAN EO NR 9908202.
Part: SKIN — CORRODED (BS 822-834)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING; CORROSION DAMAGE FUSELAGE TOP AT STATION 822-834, BETWEEN LONGERON L1 AND L2 RIGHT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-01;00, SEMAN EO NR 990094 AND BOEING MESSAGE M-7200-99-07589. (M)
Part: FLOORBEAM — CORRODED (BS 1640)
DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, MAIN CARGO COMPARTMENT RIGHT FLOORBEAM WEB CORRODED AT RBL 35 TO RBL 50, STATION 1640. REPAIRED CORROSION DAMAGE IAW FINE AIR EA NR G5310-04:00, SEMAN EO 9908201. (M)
Part: BOLT — BROKEN (NR 1 ENGINE)
DURING MAINTENANCE CHECK, FOUND OUTBOARD AFT ENGINE MOUNT ARM BOLT BROKEN IN THREADED AREA ON NR 1 ENGINE. REMOVED AND REPLACED AFT ENGINE MOUNT ASSEMBLY. RETURNED AIRCRAFT TO SERVICE. (M)
1997
Part: ACTUATOR — FAILED (LT TE MIDFLAP)
ON APPROACH GUA, FLAP INDICATOR HAD A 5 DEGREE DISAGREEMENT. LANDED WITHOUT INCIDENT. GROUND INSPECTION REVEALED LT FLAP ACTUATOR AT STA 219 LEAKING AND UPON REMOVAL, INBOARD LINK ASSY WAS FOUND BROKEN 4 INCHES AFT OF THE FORWARD END. REPLACED ACTUATOR ASSY AND RETURNED ACFT TO SERVICE. (X)
Part: PIN — SHEARED (LT MLG)
MAINTENANCE INSPECTION REVEALED THE LEFT MAIN LANDING GEAR RETRACT CYLINDER PIN WAS SHEARED AND EXHIBITED SIGNS OF CORROSION. REPLACED PIN ASSEMBLY AND SEALED PER S/B 32-102. AIRCRAFT RETURNED TO SERVICE. (M)
1996
Part: TERMINAL STRIP — BROKEN WIRE (LANDING GEAR)
ON ARRIVAL AT FL 574 - GUA-MIA - LANDING GEAR WAS EXTENDED. THE LEFT LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. WHEN FLAPS WERE SELECTED TO 35 DEGREES THE LANDING GEAR HORN WENT OFF. UPON ARRIVAL REPAIRED WIRE AT TERMINAL STRIP S-5 IAW MM 20-50-1 AND PERFORMED SWING IAW MM 32-60-0. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.
1995
Part: LINK — STICKING (NLG DOOR)
AFTER TAKEOFF SDQ, RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RELEASE PIN STICKING IN FORWARD RT DOOR LINK ASSY. REPLACED LINK EPR MM 32-22-2. RETURNED AIRCRAFT TO SERVICE.
Part: DOOR — OPEN (LT ENG CASCADE)
WINDSOR LOCKS, CN - DURING CLIMB, HEARD BANG AND AIRCRAFT YAWED LEFT. DUMPED FUEL TO LANDING WEIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. INSPECTION OF AIRCRAFT REVEALED NO DAMAGE. AFTER SHUT DOWN, NOTED LT CASCADE DOORS ON NR 1 ENGINE OPEN. RAN ENGINE AND OPS CHECKED OKAY. DEACTIVATED THRUST REVERSER AS PRECAUTION PER MEL 78-5. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES, 22,038.