N802AL
Registered owner: ZIPLINE INTERNATIONAL INC, CA (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.
143 reports on file, 1995-07-10 – 2002-10-16.
Part: SPAR — CRACKED (RT WING)
REMOVED A CRACK AND CORROSION LOCKED AT RIGHT WING FRONT SPAR WEB AT FSS 124.79 AND FSS 134.80. HFEC INSPECTED TO ENSURE THE DAMAGE COMPLETELY REMOVED. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW ECO. AIRCRAFT RETURNED TO SERVICE.
Part: SPAR — CRACKED (RT WING)
RIGHT WING FRONT SPAR CRACK AND CORRODED AT FSS124.79 AND FSS134.80. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
FUSELAGE SKIN CRACKED AT BS 275 STRINGER 15L. TRIMMED OUT THE CRACK MAINTAINING A .5 INCH MINIMUM RADIUS. HFEC INSPECTED CUT OUT. FABRICATED REPAIR PLATE FROM 2024T3 CLAD. FINISHED ALL BARE ALUMINUM WITH ALODINE AND PRIMER. INSTALLED THE REPAIR PLATE WITH THE FASTENERS. MAKING THE FRAYING SURFACES SEAL. REPAIR COMPLETED. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
FOUND A 4 INCH CRACK AT BS 780 STRINGER 15R. TRIMMED OUT CRACK, MAINTAINING A .5 INCH MINIMUM RADIUS AND 2D EDGE MARGIN FROM FASTENERS. HFEC INSPECTED THE CUTOUT. FABRICATED REPAIR .040 INCH AND .050 INCH FILLER AND .050 INCH DOUBLER FROM 2024-T3 CLAD. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1 PRIMER. INSTALLED REPAIR PARTS WITH FASTENERS IDENTIFIED ON FIGURE 1. SHIMMED ALL GAPS GREATER THAN .01 INCHES UP TO A MAX OF .04 INCHES PRIOR TO FASTENERS INSTALLATION. INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3257R2. AIRCRAFT RETURNED TO SERVICE.
Part: PROXIMITY SWITCH — INOPERATIVE (PAX DOOR)
DURING CLIMB, OUT THE CABIN RATE OF CLIMB WAS 1750 FPM WITH BOTH OUTFLOW VALVES CLOSED AND ALL DOOR LIGHTS. UNABLE TO PRESSURIZE THE CABIN, THE AIRCRAFT RETURNED TO HNL FOR MAINTENANCE WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND THAT THE FORWARD ENTRY DOOR WAS NOT SECURED. THE DOOR PROXIMITY SWITCHES WERE CLEANED AND INSPECTED AND TOP AFT LATCH CAM FITTING WAS ADJUSTED IAW THE MM. OPERATIONAL CHECK OF THE DOOR AND PRESSURIZATION CHECK OF THE AIRCRAFT WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DOOR FRAME — CRACKED (FUSELAGE)
REPAIRED .25 INCH CRACK AT MAIN CARGO DOOR FRAME EXTENDING FROM THE RIVET AT BS 390. CUTOUT AND CONFIRMED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-40-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — DAMAGED (FUSELAGE)
CUT AND REMOVED THE DAMAGED PORTION OF THE TRACK AT BS 420 TO 480. FABRICATED NEW SEAT TRACK. INSTALLED THE REPAIR PARTS IAW SRM 53-10-5, FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
FOUND CRACK INDICATION FORWARD SIDE OF LEFT BULKHEAD 178 CENTER WEB LBL 10.0 WI234, ADJACENT TO RIVET HEAD. REMOVED CRACK AND MAINTAINED A MINIMUM OF .038 INCH AT EACH CORNER OF THE CUTOUT. VERIFIED CRACK REMOVED USING HFEC. MADE AN INSURANCE CUTOUT .004 INCHES LARGER WITH A MINIMUM RADIUS OF .038 INCH. FABRICATED AND INSTALLED .50 INCH 2024 T3 REPAIR DOUBLER IAW SRM 53-10-11. AIRCRAFT RETURNED TO SERVICE. (M)
Earlier reports · 1995–2001 · 135 reports
2001
Part: CIRCUIT BREAKER — FAULTY (COCKPIT)
FLT 950 - HNL-ITO - AFTER TAKEOFF DURING FLIGHT, THE NR 2 THRUST REVERSER AND NR 2 AFT FUEL PUMP CIRCUIT BREAKERS POPPED/TRIPPED. RESET NORMAL AND AFTER SEVERAL MINUTES THE SAME CIRCUIT BREAKERS POPPED/TRIPPED AGAIN. THE AIRCRAFT RETURNED TO HNL WITH NO FURTHER INCIDENT. REPLACED THE NR 2 GENERATOR CONTROL CIRCUIT BREAKER. OPS CHECK SYSTEM OK. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ACCESSORY UNIT — FAULTY (E/E BAY)
ON APPROACH, WITH GEAR DOWN THREE GREEN AND FLAPS AT 40 GREEN LIGHT, AURAL WARNING 'TOO LOW GEAR' SOUNDED AT APPROX 900 FT. THREE RED GEAR LIGHTS ILLUMINATED, THREE GREEN LIGHTS REMAINED ILLUMINATED. CREW EXECUTED GO AROUND APPROX 700 FT AND DELAYED GEAR RETRACTION TO HAVE TOWER CONFIRM GEAR CONFIGURATION. TOWER CONFIRMED GEAR WAS DOWN. GEAR WAS RETRACTED AND QRH PROCEDURES REVIEWED. DOWNWIND, THE LANDING GEAR EXTENDED AND FLAPS SELECTED TO 40, THE PROBLEM DID NOT RETURN. LANDING WAS ACCOMPLISHED WITH NO PROBLEMS. THE AIRCRAFT WAS INSPECTED AND FERRIED FOR MAINTENANCE. MAINTENANCE REPLACED THE LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY. (M)
Part: FRAME — CRACKED (FUSELAGE)
DISCOVERED CRACK PROPAGATING FROM THE AFT TO FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S18R DURING SCHEDULED INSPECTION VERIFIED BY METHOD OF HFEC AND ULTRASONIC INSPECTION. INSTALLED REPAIR AND AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (FUSELAGE)
DISCOVERED CRACK PROPAGATING FROM FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S-18L, DURING SCHEDULED INSPECTION VERIFIED BY METHOD OF HFEC AND ULTRASONIC INSPECTION. INSTALLED REPAIR AND AIRCRAFT RETURNED TO SERVICE. (M)
2000
Part: CONTROLLER — FAILED (E/E BAY)
FLT 942 - HNL-KOA - AFTER TAKEOFF, PRESSURIZATION IN AUTO FAILED. NOT CONTROLLABLE IN ANY MODE. RETURNED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,095 hrs · 71,681 cycles
REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED NR 4 PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED CENTER AISLE NR 6 LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (RT OVERWING)
REPLACED RIGHT OVERWING EXTERIOR EMERGENCY LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (FUSELAGE)
REPAIRED FUSELAGE SKIN AT BS 770, STRINGER 17L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (RT OVERWING)
REPLACED RIGHT OVERWING SLIDE LIGHTS BATTERY POWER SUPPLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED THE ENTRY DOOR EMERGENCY EXIT LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER SUPPLY DUE TO DIM LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SPLICE PLATE — CRACKED (FUSELAGE)
CENTER FUEL TANK SPLICE PLATE FOUND CRACKED. REPAIRED IAW ECO 1854. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ATTACH FITTING — CRACKED (TAIL SECTION)
LEFT AND RIGHT HORIZONTAL STABILIZER UPPER ATTACH FITTINGS FOUND CRACKED. BOEING AOG TEAM REPLACED THE HORIZONTAL STABILIZER UPPER ATTACH CHORD. AIRCRAFT RETURNED TO SERVICE. (M)
1999
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED NR 2 POSITION FLOOR LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR NR 4 AND NR 6 POSITION FLOOR LIGHT DUE TO LOW. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR NR 5 POSITION FLOOR LIGHT DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED CONTROL CABIN EXIT EMERGENCY LIGHT ASSY DUE TO NOT TURNING OFF. OPS CHECK OK. AIRCRAFT RETURNED TO SERICE. (M)
Part: CONDUIT — LEAKED (CENTER TANK)
IN THE PROCESS OF ACCOMPLISHING ECO 2956, CENTER TANK FLOAT SWITCH MOD, SB 737 28A1132, AD 99-05012, MECHANICS FOUND THAT FUEL HAD LEAKED INTO THE ELECTRICAL CONDUIT UPON REMOVAL. FURTHER INVESTIGATION (PRESSURE CHECKED) REVEALED THAT THE LEAK BETWEEN THE FLARELESS SLEEVE AND THE CONDUIT. NO OTHER DEFECTS SUCH AS WIRE CHAFFING OR ARCING WERE EVIDENT. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR NR 4 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR NR 1 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (BS 749)
FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 15L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (BS 536)
FUSELAGE SKIN CRACK AT BS 536 AT STRINGE R15R. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACK (BS 749)
FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 17L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 PAGE 25. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (SERVICE DOOR)
REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED NR 4 FLOOR PROXIMITY LIGHT ASSY DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 FLOOR LIGHT PROXIMITY BATTERY PACK DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)
REPLACED LEFT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED AFT EMERGENCY LIGHT TRANSMITTER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOP FOR POSITIONS 1, 2, 3 AND 4. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 SEAT EMERGENCY LIGHT ASSY BATTERY PACK DUE TO NO 'ALL WELL' LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOP (CABIN)
REPLACED FORWARD SERVICE DOOR OVERHEAD EMERGENCY LIGHT ASSY DUE TO BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD EMERGENCY CENTER OVERHEAD EXIT SIGN BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 2 SEAT EMERGENCY LIGHT BATTERY PACK NO LIGHT. REPLACED NR 2 BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD ENTRANCE EXIT IDENTIFIER BATTERY DUE TO LOW VOLTAGE. OPERATIONAL CHECK FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (NR 2 POS)
REPLACED NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO BEING INOP. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 1 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO BEING INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: LIGHT — INOPERATIVE (CABIN)
NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT DUE TO BEING INOPERATIVE. REPLACED LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: FRAME — CRACKED (FUSELAGE)
AFT CARGO DOORWAY AFT FRAME CRACKED AT RIVET HOLE AND SEPARATING FROM INTERNAL DOUBLER. REPLACED DOUBLER, INSTALLED WEB AND SCUFF PLATE IAW ECO 1474R6. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 3 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (BS 420)
FORWARD CARGO COMPARTMENT LOWER LOBE FRAME CRACKED AT BS 420 BETWEEN S21L AND S22L. INSTALLED REPAIR CHANNEL PER SRM 53-10-4 PAGE 2B. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 2 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
RT SIDE EMERGENCY EXIT IDENTIFIER BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 5 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: AILERON — CRUSHED (LT WING)
LEFT AILERON BOTTOM SIDE HAS DENT AND A LARGE SMASH NOTED. REPLACED LT AILERON IAW MM CHAPTER 27-11-0. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X)
Part: THRUST REVERSER — CRACKED (LT ENGINE)
FOUND 2.5 INCH CRACK IN THRUST REVERSER PIPE AT 9 O'CLOCK POSITION. CRACK WELDED IAW BOEING OVERHAUL MANUAL 78-38-43. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 4 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
RIGHT SIDE EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WEB — CRACKED (BS 664)
FOUND 2 INCH CRACK AT BS 664 AND 52 INCHES TO THE RIGHT OF BL. REPAIRED PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WEB — CRACKED (BS 664)
FOUND 1 INCH CRACK AT BS 664 AND 39.5 INCHES TO THE RIGHT OF BL. REPAIRED PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
CENTER AISLE OVERHEAD FOLDING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. TAT: 33,645.6 HOURS. TAC: 63,576. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 2 FLOOR PROX LIGHT ASSY SHOWS NO BATTERY LED'S ON TEST. REPLACED BATTERY, TESTED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO NO TESTING. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 3 EMERGENCY EXIT LIGHT DOES NOT PASS TEST. REPLACED NR 3 EMERGENCY EXIT LIGHT ASSY BATTERY PACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CIRCUIT BREAKER — TRIPPED (PRESSURE CONTROL)
AIRCRAFT DOES NOT PRESSURIZE AFTER TAKEOFF. FOUND PRESSURE CONTROL CIRCUIT BREAKERS TRIPPED. RESET CIRCUIT BREAKERS. PERFORMED BITE CHECK. NO OTHER DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 6 EMERGENCY LIGHT 'ALL IS WELL LIGHT' NOT COMING ON. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED RT AFT EMERGENCY EXIT LIGHT BATTERY DUE TO BEING LOW. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (RT WING)
RIGHT WING UPPER SURFACE ABOVE NR 5 L/E SLAT ANTI-ICING DUCT FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET. REPAIRED PER ECO 2159R5 BETWEEN SLAT STA SS163.4 AND SS 189.4. AIRCRAFT RETURNED TO SERVICE. (X)
Part: SKIN — CORRODED (RT WING)
RIGHT WING UPPER SURFACE ABOVE NR 5 L/E SLAT ANTI-ICING DUCT FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET. REPAIRED PER ECO 2159R5 BETWEEN SLAT STA SS 189.4 AND STA SS 215.4. AIRCRAFT RETURNED TO SERVICE. (X)
Part: FLOORBEAM — CORRODED (BS 790-827)
SURFACE CORROSION FOUND AROUND NUT PLATE HOLES RT CARGO FLOORBEAM BS 790-827 AFT PIT. REPLACED FLOORBEAM ON RT AFT PIT IAW 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (WS 163-189)
FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET AT RT SIDE WING UPPER SURFACE ABOVE NR 5 LE SLAT ANTI-ICING DUCT. REPAIRED AND TREATED AREAS BETWEEN SS 163.4 AND 189.4 CORROSION IAW ECO 2159R4. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (WS 311)
EXFOLIATION CORROSION ON RIGHT WING SURFACE AT DEFUELING PANEL AT FSS 311.0. REPAIRED AREA PER ECO 2135. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (BS 360)
GROUND AIR STARTER HOSE CAME LOOSE AND DENTED FUSELAGE AT BS 360 AND STRINGER 21R. CONFIRMED SKIN CRACK WITH HFEC. REPAIRED AIRCRAFT SKIN IAW BOEING SRM 53-30-3 FIGURE 28. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (BS 328)
GROUND AIR STARTER HOSE CAME LOOSE AND DENTED FUSELAGE AT BS 328 AND STRINGER 23R. CONFIRMED SKIN CRACK WITH HFEC. REPAIRED AIRCRAFT SKIN IAW BOEING SRM 53-30-3 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 4 EMEREGNCY FLOOR LIGHT WEAK. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERABLE. AIRCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,688:40 HOURS. TAC: 61,367. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,688:40 HOURS. TAC: 61,367. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 660,881. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X)
Part: SKIN — DAMAGED (BS 446/442)
DURING QC OPERATIONS, AIRCRAFT SUSTAINED DAMAGE ON OUTER SKIN (AT TWO LOCATIONS). LOCATION OF DAMAGED AREAS WERE BS 446 (2 INCHES BY .50 INCH) AND BS 442 (.75 INCH BY .50 INCH) ON MAIN CARGO DOOR CUT OUT (ABOVE S18L). DAMAGED AREAS REPAIRED PER EA 737-53-015 (ONE REPAIR FOR BOTH DAMAGED AREAS APPLIED). AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763.
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X)
1997
Part: COVER — LOOSE (CABIN)
PILOT REPORT NR 1- FLT 207 - AFT SERVICE DOOR EXIT LIGHT COVER FALLS OFF. REPLACED COVER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,249:18 HOURS. TAC: 60,357 HOURS. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,249:18 HOURS. TAC: 60,357.
Part: SKIN — DAMAGED (CARGO DOOR)
FLT 942 - LIH-HNL - AFTER ARRIVAL, GROUND CREW FOUND THE MAIN CARGO DOOR TO HAVE EXTERNAL SKIN DAMAGE ON THE MAIN CARGO DOOR AT BS 460, STRINGER 17, SKIN PULLED BACK .5 INCH BY 1 INCH. AIRCRAFT REPAIRED PER ECO 2788. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 2 FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,179:12 HOURS. TAC: 60,197. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 4 FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,179:12 HOURS. TAC: 60,197. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 4 AND 12 EMERGENCY FLOOR PROX LIGHT ASSEMBLY DUE TO INOP. OPERATIONAL CHECK OF AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — INOPERABLE (CABIN)
DURING OVERNIGHT CHECK, REPLACED ROW 8 EMERGENCY FLOOR LIGHT BATTERY DUE TO LED'S INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 31,339:46 HOURS. TAC: 58,265. (X)
Part: LIGHT — INOPERATIVE (CABIN)
DURING OVERNIGHT CHECK, REPLACED ROW 8 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO BEING INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 31,339:46 HOURS. TAC: 58,265. (X)
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED INSPECTION OF FUSELAGE SKIN, CRACKS IN LOWER SKINS AT LAP JOINTS (FAA AD94-25-05 AMPT 39-9089), DISCOVERED CRACK APPROXIMATELY .0625 INCH LONG FROM LOWER LAP FASTENER AT BS 727B PLUS 7 INCHES, STRINGER 20L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (BS 727)
DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK APPROXIMATELY 1.5 INCH LONG AT BS 727B PLUS 12, 1.5 INCH BELOW STRINGER 17R. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
1996
Part: SHEAR BEAM — CRACKED (BS 727)
DURING SCHEDULED INSPECTION AT STRINGER 18A SHEAR BEAM (REF AD 93-08-04 AMDT 39-8551), FOUND LEFT BS 727 STRINGER 18A SHEAR BEAM CRACKED APPROX 2 INCHES IN LENGTH. REPAIRED PER ECO 1732R4 PART III STEP E PER DRAWING 65C29228 WITH KIT 65C29228 3. AIRCRAFT RETURNED TO SERVICE. (M)
1995
Part: MODULAR UNIT — DEFECTIVE (MLG)
FLT 216, PIREP NR 1 - AFTER TAKEOFF WITH LANDING GEAR HANDLE PLACED 'UP' THEN 'OFF', NOSE GEAR INDICATED UP AND LEFT AND RIGHT MAIN GEAR INDICATED DOWN (GREEN LIGHT ILLUMINATED) WITH BOTH GEAR UNSAFE (RED LIGHT ILLUMINATED). GEAR HANDLE PLACED DOWN AND RED LIGHTS WENT OUT. OVERHEAD GEAR LIGHTS REMAINED ON (GREEN) BEFORE AND AFTER GEAR HANDLE PLACED DOWN. UNEVENTFUL LANDING-HNL. MX ACTION: RETRACTION CHK NORMAL. REPLACED 'A' SYS MODULAR PACKAGE, GEAR RETRACTION CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,302.37 HRS. TAC: 49,187. (X)
Part: APU INLET — CORRODED (BS 1088)
DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION AROUND APU INLET DUCT CUTOUT AT BS 1088. REPAIRED PER ECO 198OR6. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (BS 1064)
DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BULGE AT S20L LAP JOINT AND BS 1064. OPENED LAP JOINT, REMOVED CORROSION AND CLOSED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STIFFENER — EXFOLIATED (BS 1128)
DURING HEAVY MAINTENANCE VISIT, VERTICAL STIFFENER BS 1128 FWD SIDE EXFOLIATED. REPLACED STIFFENER PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SUPPORT — CORRODED (BS 847-947)
DURING HEAVY MAINTENANCE VISIT, SURFACE CORROSION ON FLOOR SUPPORT STRIP ABOVE 25R, BS 847 TO BS 947. REPAIRED PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STRINGER — CORRODED (BS 927)
DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON STRINGER 26L AT BS 927 PLUS 4 INCHES. REPAIRED PER ECO2599. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STIFFENER — CORRODED (BS 1128)
DURING HEAVY MAINTENANCE VISIT, VERTICAL STIFFENER APU TORQUE BOX AFT SIDE OF APU INLET BS 1128 HAS STRESS CORROSION. REPLACED STIFFENER PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
DURNG HEAVY MAINTENANCE VISIT, CORROSION FOUND ON SEAT TRACK LOCATED AT PANEL NR F-11 (O/B ONE) BETWEEN TRACK HOLD DOWN FASTENERS AS EVIDENT. CLEAN AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (BS 908)
DURING HEAVY MAINTENACNE VISIT, FOUND CORROSION BULGE AT BS 908 MINUS 1 INCH AND STRINGER 23L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (BS 787)
DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON THE FUSELAGE SKIN BETWEEN S-24L AND S-25L AT BS 787. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CHORD — CORRODED (BS 1109)
DURING HEAVY MAINTENANCE VISIT, LOWER RIGHT CHORD BS 1109 APU TORQUE BOX CORRODED. REPLACED CHORD PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (CABIN)
DURING HEAVY MAINTENANCE VISIT, FATIGUE/STRESS CRACKS FOUND ON SEAT TRACK (O/B ONE) ON FLOOR PANEL NR F-9 AS EVIDENT. REPAIRED PER SRM 53-10-5 FIG 7. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STRIGNER — CORRODED (BS 1124)
DURING HEAVY MAINTENANCE VISIT, FOUND STRINGER 17AR AT BS 1124 LOWR FLANGE CORRODED. REPAIRED PER SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: VERT SUPPORT — CORRODED (AC COMPT)
DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON LEFT VERTICAL SUPPORT WEB, INSIDE EXTERNAL AIR COND ACCESS COMPARTMENT. REPAIRED PER ECO2588. AIRCRAFT RETURNED TO SERVICE. (M)
Part: RIB — CORRODED (RT HORIZ STAB)
DURING HEAVY MAINTENANCE VISIT, RIGHT HORIZONTAL STABILIZER LOWER CHORD OF RIB AT BALANCE PANEL AREA STRINGER 221.5 HAS EXFOLIATION CORROSION. REPLACED PANEL PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WINDOW FRAME — CORRODED (CABIN)
DURING HEAVY MAINTENANCE VISIT, WINDOW FRAME AT 13R EXFOLIATION CORROSION NOTED ON THE FWD LOWER CORNER. REPAIRED PER SRM 56-20-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (APU DOOR CUTOUT)
DURING HEAVY MAINTENANCE VISIT, FOUND FUSELAGE SKIN BY THE APU DOR HINGE CUTOUT (FWD AND AFT) CRACKED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 201. REPAIRED PER ECO 2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 158. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (BS 344)
DURING HEAVY MAINTENANCE VISIT, CABIN SEAT TRACK AT STATION 344 RIGHT, 2ND TRACK FROM THE WALL, A LUG PORTION MISSING. REPAIRED PER ECO2605. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (BS 460)
DURING MAINTENANCE VISIT, CRACK APPROXIMATELY 3.5 INCHES LONG FOUND ON FUSELAGE LOWER LOBE LEFT SIDE FRAME STATION 460 AS EVIDENT BTW STRINGER 21L AND STRINGER 22L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M)
Part: RIB — CORRODED (RT HORIZ STAB)
DURING HEAVY MAINTENANCE VISIT, RIGHT HORIZONTAL STABILIZER LOWER CHORD OF RIB AT BALANCE PANEL AREA STRINGER 166.3 HAS EXFOLIATION CORROSION. CLEANED AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 132. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 81. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (CARGO DOOR)
DURING HEAVY MAINTENANCE VISIT, APPROXIMATE 1.5 INCHES LONG CRACK FOUND ON FWD CARGO DOOR AFT FRAME (INNER) AS EVIDENT. REPLACED FRAME PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FASTENERS — LOOSE (LT WING)
DURING HEAVY MAINTENANCE VISIT, FUEL LEAK AT LEFT WING INBOARD SKATE ANGLE FASTENERS. REPAIRED PER ECO1699 DEV A. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BEAM — CORRODED (RT HORIZ STAB TE)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER LOWER T/E BEAM AT STRINGER 125, ELS 76.45. REPAIRED PER ECO1584R3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURNG HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 195. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: REAR SPAR — CORRODED (VERT STAB)
DURING HEAVY MAINTENACNE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 86. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (BS 530)
DURING HEAVY MAINTENANCE VISIT, FOUND FRAME CRACKED AT BS 530, STRINGER R23R. REPAIRED PER SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (BS 480)
DURING HEAVY MAINTENANCE VISIT, CRACK APPROXIMATELY 3.5 INCHES LONG FOUND ON FUSELAGE LOWER LOBE, LEFT SIDE FRAME STATION 480 AS EVIDENT BETWEEN STRINGER 21L AND STRINGER 22L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M)