N342UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | 2015-04-12 – 2015-04-12 | Operator named in NTSB report |
| UNITED PARCEL SERVICE CO | Operator | 2015-04-12 – 2015-04-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WHEEL WELL FIRE DETECTION TEST DOESN'T WORK WHEN TEST BUTTON IN FLIGHTDECK PRESSED. T/S CARRIED OUT IAW FIM 26-17 FAULT TREE 803 REV. 148. FOUND WHEELWELL FIRE TEST BUTTON U/S. FIRE/OVERHEAT TEST PANEL REPLACED IAW AMM 26-11-01 PB. 401 REV. 148. POST INSTALLATION TEST SATIS.
BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLETED REPAIR TO LEADING EDGE PANEL PER SRM 51-70-05-0G-0 ALL STEPS OF REPAIR COMPLETE. REPAIR PLIES INSTALLED AND CURED. REAPPLIED PROTECTIVE COATINGS AND PERFORM POST REPAIR REQUIREMENTS. INSTALLED REPAIRED PANEL 666AT PER AMM 06-44-00-992-006 AND AMM 20-11-00-910-802
BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. REMOVED PANEL 666AT AND ROUTED TO SHEET METAL SHOP FOR REPAIR.
ATB FMC LOCKED UP WITH STBY ONE MSG PRESENT (FULL WRITEUP IN FAULT DESCRIPTION). + PERFORMED TROUBLE SHOOTING REF B767 FIM 34-61 FAULT TREE 854,NO FAULTS FOUND.REMOVED AND REPLACED L/H FMC REFB767AMM 34-61-01 9 (PRECAUTIONARY) OPS CHECK GOOD ATT.
ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIEWED.
DISBOND PNL, RT WING NR 8 L/E SLAT INBD, SIDE INNER UPPER WEDGE. INST THE EXT DBLR WITH FILM ADHESIVE & CURE IAW SRM 51-70-10-2R-0 PARA 18 & 20. PERFORMED NDT/UT FOR REWORKED AREA & 8" FROM WHERE EDGES OF HEAT BLANKET, IAW NDT MANUAL PT1 51-01-01 & 51-04-00 REV:139. NO DEFECT FOUND. CLEAN, SEAL & FINISH REP AREA IAW SRM 51-70-10-2R-0 PARA 22 REV.91. IAW AMM27-81-02-424-099 REV.144 STEP 3.A TO 3.H(16) INST RT WING NR 8 SLAT IAW AMM 27-81-02-424-099 REV.144 STEP 3.H(17) TO 3.I(13) ADJUST & TEST NR 8 SLAT RT WING RESULT CONDITION CK SATIS IAW AMM 30-11-06-404-009 REV 144 INST DUCT. CONDITION CK IAW AMM 30-11-00-790-801 REV 144, LEAK CK, TEST OF 8-9 ANTI-ICE DUCT, SATIS & NO LEAK FOUND.
FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 145T5876-68 PANEL NO: 241AFF STA 731~STA 834 LBL 11~RBL 11. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF STA 1440~STA 1540 LBL 77.5~LBL 54.75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015, AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED.
FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.252YFF AND CONDITION CHECK NORMAL. I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANEL AT STA 1578 RIGHT SIDE TOTAL:2EA AND CONDITION CHECK NORMAL.
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91 INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL NO.251CGF AND CONDITION CHECK NORMAL. I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANEL AT STA 1578 LEFT SIDE TOTAL:2EA. AND CONDITION CHECK NORMAL.
FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF STA 1197+22~STA 1197+110 LBL 55~LBL 77. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-9 PANEL NO: 241KFF STA 1197+22~STA 1197+110 LBL 77~LBL 88. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015 AND AMM 25-58-01-404-005 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
LUZ DE CAPT PITOT ENCENDIDA DESPUES DEL ARRANQUE DE MOTORES, PROBETA DE TUBO PITOT DEL CAPITAN DAÃADA CAPT PITOT LIGHT ON AFTER STARTING, PITOT TUBE DAMAGED.
INSPECTION TYPE:C6, DAMAGE ON M/D CARGO FLOORBEAM, BS 246, LBL 53. FABRICATED A REPLACEMENT IAW DWG 141T5146 SH 15 REV B, PL REV F AND PSDL REV-. REPLACED IAW SRM 51-40-02-0G-0 REV. 85.01.
INSPECTION TYPE:N/ACREW ENTRY DOOR SEAL MAKES VERY LOUD HISSING NOISE IN FLIGHT.PRESSURISATION OKAYFOUND CREW ENTRY DOOR BOTTOM SEAL DETACHED SECURED AND CLEANED DOOR SEAL PER AMM 52-09-01-424-019 FOUND SATIS
INSPECTION TYPE:N/ASUPPLEMENTAL SDR**DIVERSION**EMERG DECLARED**A/C LANDED W/OUT INCIDENT**APU FAULT AT FL 390 DIVERTED TO STL. DEFERRED PER MEL 49-11-1A ASSIGNED M766577REPLACED APU COOLING FAN AMM 49-51-03-401 AND APU OIL COOLER AMM 49-27-09-404-011. OPS & LEAK CKS GOOD. THIS CLEARS M766577, PLACARD REMOVED. EFF SOURCE REF: IPC 49-51-00-01-046K AND 49-27-00-01-265.
INSPECTION TYPE:N/A** EMERGENCY DECLARED ** THE FIRE TRUCKS FOLOWED THE A/C TO THE RAMP & THE FIRE CHIEF DETERMINED IT WAS SAFE TO TAXI TO THE GATE & FOLLOWED THE AIRCRAFT TO THE GATE ** # 7 MLG TIRE HEATSHIELD DAMAGED.R & R'D # 7 MAIN WHEEL ASSY IAW MM 32-45-01-401, SPACER & WASHER VERIFIED INSTALLED. IPC 32-45-01-01B ITM. 051T.
INSPECTION TYPE:N/AHYDRAULIC POWER CAME ON PRIOR TO ENGINE START ON PUSHBACK, BOTH YOKES WENT 3/4 FULL LEFT TURN FOR NO REASON. A/P OFF.R/R AILERON RUDDER TRIM AILERON CONTROL MODULE PER AMM 27-21-23-022-001 & 27-21-23-422-007 OPS TEST AILERON & AILERON TRIM CONTROL SYS PER AMM 27-11-00-715-417 & OPS TEST RUDDER TRIM CONTROL SYS PER AMM 27-21-00-715-001-002.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATT PACK PER AMM 33-51-07 OPS CHK GOOD. ESR: IPC 33-51-07-32.
EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-16-962-001 OPS CKS OK
INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834-STA 930, LBL 11 - RBL 11, PNL NR 241FFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
INSPECTION TYPE:C4 BROKEN ON LOWER SKIN PANEL OF RT WING INBD AFT FLAP NEAR IFS 119.75. REPAIR IAW SRM 57-53-01 REPAIR 1, SRM 51-70-10 REPAIR 2, SRM 51-70-10 GENERAL, SRM 51-70-03 GENERAL, REV.73.01
INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP W/ REF TO AMM. 33-51-16. LIGHT OPERATES NORMAL P/N ON/OFF 767.
MCD FLOOR PANEL PUNCTURED POSITION 2R, FABRICATED NEW PANEL IAW EO B767-5320-9693-I.
RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED THE RT FWD LOWER FIRE LOOP DETECTOR IAW AMM 26-11-02 AND TESTED NORMAL.
DURING MAJOR MAINTENANCE VISIT NR 6749, FOUND DENT ON SKIN, BULK CARGO DOOR OUTER SURFACE, STA 1447, BETWEEN S-23L AND S-24 L/E, EVALUATED DAMAGE IAW SRM 52-30-01-1A-1, FIG 101, REF: TAIL VI, REV 61.00 INFORMATION SUBMITTED FOR ADM, DENT WITHIN ALLOWABLE DAMAGE, REF LOG PAGE 694809.
EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.
CAPTAIN'S OVERHEAD ESCAPE ROPE DOOR LATCH INOPERATIVE. OVERHEAD PANEL ASSY R & R IAW AMM TASK 25-1 4-02. ROPE INSTALLED IAW AMM TASK 25-61-02-682-001, REV 110, 02.
FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.
INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 1.75"(LENGTH) X 1.5"(WIDTH) X 0.031"(DEPTH) AT OSS 807. REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.88" (LENGTH) X 0.62"(WIDTH) X 0.025" (DEPTH) AT OS S 804.5 REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.62" (LENGTH) X 0.55" (WIDTH) X 0.012"(DEPTH) AT OSS 805.5 REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 0.78" (LENGTH) X 0.55" (WIDTH) X 0.012" (DEPTH) AT OSS 801.5. REPAIR IAW 767-300F SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
INSPECTION TYPE:C01, LT WING NR 3 SLAT T/E WEDGE ASSY UPPER SKIN DENTED AT OSS 819. DAMAGE SIZE IS MEASURED AS 1.0" (LENGTH) X 0.66"(WIDTH) X 0.013"(DEPTH) AND THE CUT OUT IS MEASURED AS 1" DIAMETER. REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4 FIG 201, REV 55.
MAIN CARGO DECK FLOOR PANEL POS NR 12L OTBD HAS DENT CENTER OF PANEL. REPAIRED IAW SRM 53-00-50-2R.
MAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320--9693-H.
MAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693 H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320-9695-H. INSTALLED INSERTS.
MAIN CARGO COMPARTMENT FLOOR PANEL HAS A .5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693H, FABRICATED A REPL PANEL FROM A402H ACCOMPLISHED PARA B STEP 5&6 REF EO B767-5320-9695-H. INSTALLED INSERTS.