N922FD
Registered owner: FEDERAL EXPRESS CORP, 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.
195 reports on file, 2009-04-28 – 2024-07-21.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 74,218 hrs · 28,253 cycles
ON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AS PER 757 AMM 33-51-07-2-0. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. EMERGENCY LIGHT POWER SUPPLY- MANUFACTURER- RADIANT ILLUMINATION, P/N 2012-1, S/N 13973 EMERGENCY LIGHT BATTERY PACK. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AS PER 757 AMM 33-51-07-2-0. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
R / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN CORROSION R/H WING LOWER DRY BAY PANEL REPAIR AT ACCESS PANEL CUTOUT 644 AB, WS 775-806 WITH NO DEVIATION. MAJOR REPAIR.
Part: WEB — CORRODED (BS 600-620) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
FWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT OF LIMITS IAW B-757 SRM 53-30-13-1A FIG 101 DETAIL III ; REMOVED, FABRICATED AND INSTALLED SHEAR WEB IAW B-DWG # 143N5520 REV. B, SRM 51-40-02-0G AND E.A. # : F-5310 -T0378655 P1
Part: FAIRING — GOUGED (ZONE 300) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
SEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-03 AND AFTER EVALUATION TWO DIFERENT AREAS FOUND # 1 AREA AT STA 1862 TO STA 1865 FOUND WITHIN LIMITS AND AREA #2 AT STA 1853 TO STA 1862 FOUND OUT LIMITS IAW B-757 SRM 53-80-01-1A DETAIL VII FIG 101 SHT'S 5&6 ; REMOVED AND REPLACED PANEL FAIRING FOR AREA OUT OF LIMITS #2 PER E.A. # F-5350-T0378577 P1
Part: SEAT TRACK — CORRODED (BS 1180-1200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG. 101 DETAIL VIII REMOVED AND INSTALLED NEW SEAT TRACK SECTION TO STA. 1180-1280 RBL 45.50 IAW B DWN # 146N5120 REV. A, B DWN # PL 146N5130 REV. C AND B757 SRM 51-40-02-0G MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1100-1180 RBL-45.5 REMOVED CORROSION AT SEAT TRACK STA 1075-1180, RBL 455 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG 101, DETAIL VIII. REMOVED AND REPLACED NEW SEAT TRACK SECTION BETWEEN STA 1075-1180 RBL 45.5 IAW B DWG# PL 144N5021 REV C AND B 757 SRM 51-40-02-0G. MAJOR REPAIR
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
MAIN DECK, RIGHT CREASE BEAM HAS CORROSION BETWEEN STA.1260-1280. REMOVED CORROSION CREASE BEAM AT STA 1260 TO 1280 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FOUND TO BE OUT OF LIMTIS BETWEEN STA 1260-1280 IAW B757 SRM 53-60-13- 1A DETAIL VIII FIG 101, REPAIR CREASE BEAM AT STA 1240 TO 1300 RBL 64 IAW B 757 SRM 53-00-13- 2R ALTERNATIVE 1 FIG 201 MAJOR REPAIR
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
LH AFT MAIN CABIN CREASE BEAM HAS POSSIBLE CORROSION BETWEEN BS 1420 THRU BS 1640 REMOVED CORROSION AT CREASE BEAM BETWEEN STA. 1520 - 1605 IAW B757 SRM 51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-13-1A DETAIL VIII, REMOVED AND IINSTALLED NEW CREASE BEAM BETWEEN STA. 1360-1630 LBL 64.20 AND SPLICE REPAIR BETWEEN STA 1480 - 1500 IAW B757 SRM 53-00-13-2R REPAIR I TABLE 201 FIG. 201 DETAIL I MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
SEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1420 RBL44 IAW B757 SRM 51-10-02-0G, EVALUATED AREAS FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL VII, REMOVED AN REPLACED SEAT TRACK SECTION, STA 1320-1540 RBL 45.5 IAW B DWG# 146N5130 REV A, B DWG# PL 146N5130 REV C AND B757 SRM 51-40-02-0G. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL 24.75 REMOVED CORROSION AT SEAT TRAK BEWEEN STA 1180-1200 RBL 24.75 IAW B757 SRM 51-10-02- OG, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL VIII, REMOVED AND INSTALLED NEW SEAT TRACK SECTION AT STA 1180-1200 RBL 24.75 IAW B DWG # 146N5120 REV A, B DWG # PL 146N5130 REV C AND B757 SRM 51-40-02-0G. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1100-1180 RBL-24.5 REMOVED CORROSION AFT FLANGE SEAT TRACK A STA 1075-1180 RBL 24.5 IAW B57 SRM 51-10-02- 0G , FOUND TO BE OUT OF LIMTIS IAW B757 SRM 53-00-52-1A DETAIL VIII REMOVED AND INSTALLED NEW SEAT TRACK SECTION BETWEEEN STA 1075 TO 1180 RBL 24.5 IAW B DWG# 144N5021 REV A AND B 757 SRM 51-0-02-0G. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1320-1340, RBL-57 REMOVED CORROSION IAW B757 SRM 51-10-02-0G, NO LIMITS REPLACEMENT REQ. IAW B757 SRM 53-00-52-1A FIG 101 REMOVED AND INSTALLED NEW SEAT TRACK SECTION BETWEEN STA 1180 TO STA 1420 RBL58.22 IAW B757 DWG'S #657N3332 REV A, PL # 657N3332 REV C AND B 757 SRM 51-40- 02-0G. MAJOR REPAIR.
Part: ANGLE — CORRODED (BS 1440 S27R) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
AFT CARGO COMPARATMENT ON STA 1440 S-27 R\H CLIP ANGLE CORRODED. REMOVED, EVALUATED FOUND OUT OF LIMTIS, FABRICATE, TREATED, PRIMED, TOP COAT AND INSTALLED AFT CRG COMPARTMENT CLIP ANGLE P\N: 146N5422-4 AT STA 1440 S-27 R\H IAW B757 SRMS 51-40-02-0G, 51-20-01-0G AND 53-00-03-1A ACCOMPLISHED EA: F-5320-T0378503 P1 WITH NO DEVIATION. FABRICATED PART IAW BOEING DWG: 146N5422-4 REV: B. REPAIR MAJOR
Part: BRACKET — CORRODED (BS 1440) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
AFT CARGO COMPARTMENT F.STA 1440 S.27 R BRAKET SUPPOR CORRODED REMOVED, INSPECTED FOUND OUT OF LIMIT, FABRICATED, TREATED, PRIMED TOP COATED AND INSTALLED AFT CRG COMPARTMENT BRAKET P/N 146N8815-1 AT STA 1440 S.27 RH IAW EA F-5320- T0378505, B757 SRM 51-40-02-0G ,53-00-03-1A AND 51-40-05-0G, 51-20-01-0G. MAJOR REPAIR
Part: CREASE BEAM — CORRODED (BS 1580-1620) · airframe 74,064 hrs · 28,137 cycles
MAIN DECK RIGHT SIDE CREASE BEAM, HAS CORROSION BETWEEN STA 1580-1620. REMOVED CORROSION ON CREASE BEAM IAW B757 SRM 51-10-02-0G FOUND TO BE OUT OF LIMITS AT AREA BETWEEN STA 1583-1603 RBL 64.20, IAW B757 SRM 53-60-13-1A FIG 101 DETAIL VIII, REPAIR CREASE BEAM AT STA 1569-1629 BRL 64.20, IAW B757 SRM 53-00-13-2R ALTERNATIVE 1, DETAIL I FIG 201 MAJOR REPAIR
Part: SEAT TRACK — WORN (ZONE 200) · airframe 74,064 hrs · 28,137 cycles
MAIN CABIN, FOUND SEAT TRACK DAMAGED ON CROWN AREAS STA 1580 RBL 24.75. REWORKED DAMAGED AREAS AT SEAT TRACK CROWN AREA AT BETWEEN STA 1570-1590 RBL 24.5 IAW B757 SRM 51-10-02-0G, AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL 1, REMOVED AND INSTALLED NEW SEAT TRACK SECTION IAW B DWG #'S 146N5120 REV -, PL 146N5120 REV DB AND B757 SRM 51-40-02-0G AT STA 1540-1620, RBL 24.75 MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1320-1340, RBL-57.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
AFT CARGO COMPARTMENT BETWEEN F. STA 1280-1300 RBL 45.50 SEAT TRACK HAVE CORROSION REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA. 1280-1300 RBL 45.50 IAW B757 SRM 51-10-02-0G, BLENDED AREA FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A DETAIL VII, REMOVED AND INSTALLED NEW SEAT TRACK SECTION ON BS 1280-1320 RBL 45.50 IAW B DWG #'S 657N3318 REV. B, PL # 657N3318 REV. B AND B757 SRM 51-40-02-0G MAJOR REPAIR
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
REWORK REQUIRED ON NR# N00383 FOR NOT PERFORMING REQUIRED HARDNESS TEST FOR FLOOR SUPPORT LOCATED AT STA 339 LBL 60. PERFORMED REQUIRE HARDNESS TEST ON FABRICATED FLOOR SUPPORT P\N: 141N5170-39 LOCATED AT STA 339 LBL 60. MATERIAL 7075-T6 0.050" IAW B757 SRM 51-20-02-0G TABLE #1 AT FIGURE 2 SHEET 6. TOOLING USED: AVEX ID 01678 CAL DD: 01-09-25. SEE NO. 00383 FOR REMOVAL, FABRICATION AND INSTALLATION PROGESS. HRB: 87.8 PASS. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
SEAT TRACK HAS CORROSION, ON LOWER SURFACE OF CLIPS NUTS HOLES, BETWEEN STA/ 1300 - 1320 , RBL24.5 REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA/ 1300-1320 , RBL24.75 IAW B757 SRM 51-10-02-06 , BLENDED AREA FOUND OUT LIMITS IAW B757 SRM 53-00-52-1A DETAIL VII REMOVED AND INSTALLED NEW SEAT TRACK SECTION ON BS 1280-1320 RBL 24.75 IAW B DWG # 657N3318 REV B, B DWG PL # 657N3318 REV B AND B757 SRM 51-40-02-0G. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (BS 1537) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
MAIN DECK,SEAT TRACK HAS CORROSION AT FLANGE, STA 1537 RBL-57 REMOVED CORROSION AT SEAT TRACK I/B FLANGE IAW B757 SRM 51-10-02-0G, AREA NO LIMITS IAW B757 SRM 53-60-52-01 DETAIL II REMOVED AND INSTALLED NEW SEAT TRACK SECTION, BETWEEN STA 1420 TO STA 1620 RBL 58.22 IAW B DWG # ' S 657N3332 REV A, PL # 657N3332 REV C AND B757 SRM 51-40-02-0G MAJOR REPAIR
Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
R/H MAIN CABIN CREASE BEAM HAS CORROSION BETWEEN BS 840 THRU BS 880. MAIN CABIN CREASE BEAM BETWEEN BS 733-900 REMOVED CORROSION IAW B757 SRM 51-10-02- 0G, FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-30-13-1A DETIAL VIII, REMOVED AND REPLACED SECTION CREASE BEAM (INBD CHORD) IAW B DWG# PL 143N5520 REV. C, DWG 146N5590 REV F AND B757 SRM 51-40-02-0G. MAJOR REPAIR
Part: DECK PLATE — GOUGED (ZONE 200) · airframe 74,064 hrs · 28,137 cycles
MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1682 LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA. 1682 LBL 7 IAW B-757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I FIG. 201. MAJOR REPAIR.
Part: DECK PLATE — GOUGED (ZONE 200) · airframe 74,064 hrs · 28,137 cycles
MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1711, LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA 1711 LBL 7 IAW B-757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I FIG. 201. MAJOR REPAIR
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CORROSION ON SEAT TRACK FLANGE STA 1195 LBL-26. AFTER EVALUATED CORROSION AREA ON SEAT TRACK FLANGE AT STA. 1195, LBL 26 FOUND OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 SHEET 4 DETAIL VIII, REMOVED AND REPLACED SEAT TRACK SECTION AT STA. 1180 TO 1240 LBL 24.75 IAW B DWG. #146N5120 REV A, DWG. # PL 146N5130 REV C, AND B757 SRM 51-40-02-0G.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
SEAT TRACK HAS CORROSION, AT STA 1427 RBL-25. AFTER EVALUATED CORROSION AREA ON SEAT TRACK STA 1427 RBL25 FOUND OUT OF LIMTIS IAW B757 SRM 53-00-51-1A FIG 101 SHEET 4 DETAIL VIII & I, REMOVED AND REPLACED SEAT TRACK SECTION, STA 1320 TO 1540 RBL 24.75 IAW B DWG# 146N5120 REV A, B DWG# PL 146N5130 REV C AND B757 SRM 51-40-02-0G. MAJOR REPAIR
Part: CREASE BEAM — CORRODED (BS 1320-1350) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
CREASE BEAM HAS CORROSION, BETWEEN STA 1320-1350 NEXT TO R-3 DOOR. REMOVED CORROSION IAW B757 SRM 51-10-02-0G AT CHORD, OUT OF LIMTIS IAW B757 SRM 53-60- 13-1A DETAIL VIII, REMOVED AND REPLACED CHORD ON R\H STA 1300 TO 1400 RBL 64. IAW B757 SRM 51-40-02-0G AND B DWG# 146N8326 REV C. MAJOR REPAIR
Part: FLOOR SUPPORT — CORRODED (BS 339) · corrosion level 2 · airframe 74,064 hrs · 28,137 cycles
L-1 ENTRY DOOR UPPER SIDE OF THE FLOOR SUPPORT AT STA 339 LBL 60 FOUND CORROSION. REMOVED CORROSION AT L-1 ENTRY DOOR STA 339 LBL 60 ON FLOOR SUPPORT IAW B757 SRM 51-10-02-0G, OUT OF LIMITS IAW B757 SRM 53-10-15-1A DETAIL IV FIG 101, REMOVED AND INSTALLED FLOOR SUPPORT IAW B757 SRM'S 51-40-02-0G, 51-40-05-0G ABD B DWG# 141N5170 REV C & F ITEM -39 MAJOR REPAIR
Part: UNKNOWN — ODOR (CABIN) · airframe 74,043 hrs · 28,127 cycles
AT GATE, STATUS MESSAGES EQT CLG TEST AND WARN ELEX APPEARED, AT THE SAME TIME A STRONG FOUL RUBBER/ELECTRICAL ODOR PRESENTED ITSELF. EQUIPMENT COOLING SYSTEM TEST C/O NORMAL IAW FIM 21-58 FAULT TREE 912 133.3 NO FUMES OBSERVED/SMELLED
Earlier reports · 2009–2023 · 166 reports
2023
Part: CONTAINER — FAILED (PBE) · airframe 73,914 hrs · 28,019 cycles
POB AT COURIER AREA FOUND DAMAGE (PROTECTIVE BAG LOST VACUUM) PROTECTIVE BREATHING EQUIPMENT, NOT POB MEL 27OCT23 07:49 BCN U RELEASED FOR SERVICE PER MEL : 35-20-01 CATEGORY : D EXPIRATION : 24FEB24 "MEL 35-20-01: COURIER COMPARTMENT PBE UNIT - REMOVED FROM ACFT. AMM: 35-31-01-4-99 INSTALLED PBE PER MM 35-31-01-4-99.
Part: PANEL — DELAMINATED (ZONE 300) · airframe 73,637 hrs · 27,822 cycles
DURING OPEN UP FOR ELEVATOR LUBRICATION FOUND ACCESS PANEL 345BB EDGE DELEMINATED PERFORMED WET LAYUP REPAIR FOR MENTIONED PANEL PER SRM 51-70-17,PAR. 4.G. REF. SRM 55-10-01-2R, REP.5, FIG. 201,TABLE II. REP. DIM. : 4" X 2.5", REP. LOC. : 2" FROM I/B EDGE OF PANEL AT T/E. REPAIR MATERIAL P/N: EA9390, B/N: JH2BAE4907. REV. 138.1. MAJOR REPAIR.
2022
Part: EXHAUST VALVE — STUCK (N/A) · airframe 73,445 hrs · 27,678 cycles
PDIS 922 21-30 3695 07DEC22 CDG FACT U RECEIVED CABIN ALT WARNING IN FLIGHT AT FL400. CABIN ALT WAS JUST OVER 10,000 . DIFFERENTIAL PRESSURE WAS APPROXIMATELY 7PSI. WE DESCENDED TO 10,000 . EXECUTED THE QRC/QRH. WE KEPT THE CABIN ALTITUDE CONTROL IN AUTO. IT FUNCTIONED NORMALLY AFTER THAT. R/I 08DEC22 01:47 CDG U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 5669-18 POS: ONL SRL: 5487 ON MPN: 5669-18 CPN: 2112858 SRL: 5466 TAG NBR: I34563 AMM: 21-58-05-4 AMM: 05-51-24-2 CABIN PRESSURIZATION LEAKAGE TEST PERFORMED IAW AMM 05-51-24-2, FOUND EQUIPMENT COOLING OVERBOARD EXHAUST VALVE STUCK IN OPEN POSITION, UNABLE TO REACH THE FULLY CLOSED POSITION. REMOVED AND REPLACED VALVE IAW AMM 21-58-05-4, VALVE OPERATES PROPERLY AND PERFORMED PRESSURIZATION LEAKAGE TEST AGAIN, FOUND SATIS.
Part: CONTROL PANEL — FAILED (FIRE DETECTION) · airframe 73,403 hrs · 27,652 cycles
JUST PRIOR TO TOP OF DESCENT, RECEIVED A FIRE LOOK UP LIGHT WITH ALL MAIN CARGO FIRE INDICATORS ILLUMINATED. QRH COMPLETED & AN EMERGENCY DECLARED. THERMO IMAGED THE ENTIRE AIRCRAFT AND OBSERVED NO SIGNS OF FIRE . AMM 26-16-98-4-0 DURING INSPECTION, FOUND COCKPIT MAIN DECK SMOKE CONTROL PANEL FAULTY. REMOVED & REPLACED IAW AMM 26-16-98-4-0. ALL TESTS OK, NO FIRE INDICATIONS OR DEFECT FOUND. ACFT OK FOR SERVICE.
Part: OIL SYSTEM — LOW PRESSURE (APU) · airframe 73,371 hrs · 27,626 cycles
APU SHUTDOWN AT CRUISE RESULTING IN SINGLE GENERATOR REMAINING. EMERGENCY DECLARED AND RETURNED TO LFPG FOR NORMAL LANDING. EMERGENCY DECLARED, APU SHUT DOWN IS RELATED TO WRI 49-90/3559 WITH CORRECTIVE ACTION , APU OIL QTY IN STATUS , SUDDEN APU OIL CONSUMPTION . ORIG SUB DATE: 10/29/2022
Part: SENSOR — LOOSE (EMERGENCY EXIT) · airframe 73,184 hrs · 27,535 cycles
PDIS 922 52-20 3302 07AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE AFTER POWER TRANSFER T/S REF. B757 FIM 52-71 FT 802/805, NO FAULT CODES NOTED. TARGET TEST FAR WITH DOOR CLOSED, FOUND SENSOR LOOSE. SECURED SENSOR REF. B757 AMM 52-71-00-5-0, TEST OK.
Part: TARGET — FAULTED (EMERGENCY EXIT) · airframe 73,184 hrs · 27,535 cycles
PDIS 922 52-20 3299 06AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE DISPLAYED CLIMBING THROUGH 9,500 MSL. CAIN DIFFERENTIAL WAS 4.4 AND CABIN ALTITUDE WAS 800 FEET. REMAINED ILLUMINATED UNTIL 800 FEET AGL ON FINAL APPROACH THEN EICAS MESSAGE EXTINGUISHED. PER FIM 52-71 TREE 802 SENSOR ADJ NEEDS TO BE VERIFIED. SIDEWALL REMOVED. SENSOR GAP VERIFICATION NEEDS TO BE ACCOMPLISHED PER AMM 52-71-00-5. PERFORMED PSEU BITE REF B757 FIM 32-09 TREE 804. FOUND L EMER EXIT DOOR TARGET FAULTED. DOOR SENSOR GAP MEASURES .070IN. MINIMUM GAP IS .130IN. NEEDS SHIMS REMOVED. REF B757 AMM 52-71-00-5 AMM52-71-00-5 ADJUSTED THE L3 EMERGENCEY DOOR PROX.SWITCH AND CHECKED CLEARANCES REF AMM 52-71-00-5. PROX SWITCH READING .147 WITHIN LIMITS. NO LIGHT ON THE OVERHEAD P5 PANEL AND NO MESSAGES FOUND. ACFT OK FOR SERVICE.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE NOTED ON HOLE #3 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E P2) STEP #9, CAT B AND MAJOR REPAIR
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATINS NOTED IN HOLE #4 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, TITLE: WINGS-PLATES AND SKINS-LH WING-UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PT1, CAT B MAJOR REPAIR.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #15. #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV. E PART 1, CAT B AND MAJOR REPAIR
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #8. #1 PYLON FITTING PERFORMED REAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23. TITLE: WINGS-PLATES AND SKINS- LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PT1, CAT B AND MAJOR REPAIR
Part: DRAG FITTING — CRACKED (ZONE 500) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #4, #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 PT1 STEP 20 AND 23. TITLE: WINGS - PLATES AND SKINS - LH WING - UPPER SKIN AT DRAG FITTING CORROSION REPAIR - FED EX EO F-5730- E0340076 REV E PT 1. MAJOR REPAIR
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE NOTED ON HOLE #6 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING,CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E P2) STEP #9, CAT B AND MAJOR REPAIR.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE NOTED ON HOLE #4 #2 PYLON PERFORMED REPAIR ON EA F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING,UPPER SKIN AT DRAG FITTING, CORROSION REPAIR;FEDEX EO F-5730-E0340076 REV. E P2) STEP #4, CAT B AND MAJOR REPAIR.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #9 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10. TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-0340076 REV E PART 1, CAT B AND MAJOR REPAIR.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
#1 PYLON INBD. FITTING #12 HOLE DAMAGED IN SKIN ONLY PERFORMED REPAIR ON EA F-5730-T0361920 PT STEP 10, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX E.O. F-5730-E0340076 REV. E PART 1, CAT B AND MAJOR REPAIR.
Part: SKIN — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #3 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 21, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTING, CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PART 1, FITTING REPLACED ON N/R #00152, CAT B AND MAJOR REPAIR.
Part: DRAG FITTING — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #10 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10, WINGS-PLATES AND SKIN-LH WING, UPPER SKIN @ DRAG FITTING CORROSION REPAIR-FEDEX EO F-5730-E0340076 REV E PART 1 BY REPLACED OB DRAG FITTING, CAT 'B' REPAIR, MAJOR REPAIR.
Part: DRAG FITTING — CRACKED (ZONE 400) · airframe 73,174 hrs · 27,532 cycles
REJECTABLE DAMAGE NOTED ON HOLE #12 .593, #2 PYLON THRU SKIN AND FITTING TITLE-WINGS-PLATES AND SKINS-RH WING UPPER SKIN @ DRAG FITTING, CORROSION REPAIR- FEDEX E.O. F-5730-E0340076 REV. E PART 2, IS COMPLIED WITH STEP #9 ON FINAL EA # F-5730- T0369270 P1, MAJOR REPAIR, CAT 'B' REPAIR
2021
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,556 hrs · 27,121 cycles
MDIS 922 33-50 2242 13AUG21 CDG FACT U FOUND L1 EMER DOOR GROUND ILLUMINATION LIGHT INOP. SHGN 13AUG21 19:28 CDG U RELAMPED AS PER MM:33-51-06-2-1. LIGHT TEST OK. DURING L1 EMER LIGHT LENS REINSTALLATION, FOUND 4 SCREWS WORN AND UNABLE TO REINSTALL. NEED TO ORDER 4 SCREWS AND 4 SPACERS TO REINSTALL THE L1 EMER LIGHT LENS. SEE IPC:33-51-06-51 ITEM 25:PN:60-3500-9 ITEM 30: PN:31-5500-1 MPN: 31-5500-1 CPN: 3314378 QTY: 10 SPACER LIGHT-EVAC SLIDES RH MPN: 30-2041-2 CPN: 3311994 QTY: 1 INSTALLED L1 EMER LIGHT LENS WITH NEW SCREWS AS PER AMM 33-51-06-2-1.AC OK FOR SERVICE.
Part: DOOR — CRACKED (LT MLG) · airframe 72,519 hrs · 27,091 cycles
LMG BODY DOOR CRACKED AFT OF TANG REPAIRED LMG DOOR CRACKED AFT OF TANG IAW FEDEX B757 SRM: 52-80-02, 51-70-06-0G, DWG #149N6003 AND AMM 51-21-00. MINOR REPAIR
2020
Part: GIRT BAR — LACK OF LUBE (DOOR SLIDE) · airframe 71,779 hrs · 26,415 cycles
PDIS 922 52-10 0673 28JAN20 CDG OPEN U LOGPAGES:3026593 L SIDE DOOR FAILS TO DISARM APPROPRIATELY. LEVER DOES NOT FULLY DISENGAGE OR " LOCK OUT " IN ORDER TO DISARM DOOR. CLEANED AND ADJUSTED ALL L/H DOOR LOCKING SYST PER MM 52_11_01_6_0 AND 52_11_01_4_0. LUBRICATED GIRD BAR LOCKING MECANISM AND PER SEVERAL CHECK PER SAME MM. OPS CHECK OK. A/C OK TO CONTINUE.
Part: SPAR WEB — TORN (VERTICAL STAB) · airframe 71,768 hrs · 26,411 cycles
VERTICAL STABILIZER FORWARD SPAR WEB TORN/DAMAGED FSS 320 TO FSS 350 REPAIRED ON EA# F-5530-T0351942A TITLE STABILIZER-VERTICAL-FRONT SPAR-WEB AND CHORD SPLICE REPAIR-COVER E.A. MAJOR REPAIR
Part: SPAR — BENT (VERTICAL STAB) · airframe 71,768 hrs · 26,411 cycles
VERTICAL STABILIZER FORWARD SPAR LEFT CHORD BENT FSS 330 REPAIRED PER EA# F-5530-T0351942A THE STABILIZER-VERTICAL-FRONT SPAR-WEB AND CHORD SPLICE REPAIR-COVER E.A.
Part: WEB — DAMAGED (VERTICAL STAB) · airframe 71,768 hrs · 26,411 cycles
VERTICAL STABILIZER RIB FSS 371.308 WEB IS BUCKLED AT FORWARD SIDE REMOVED AND REPLACED WEB IAW SRM 51-40-02 MAJOR REPAIR
Part: SPAR — CRACKED (VERTICAL STAB) · airframe 71,768 hrs · 26,411 cycles
VERTICAL STABILIZER FORWARD SPAR RIGHT CHORD/TORN FSS 330 REPAIRED PER EA# F-5530-T0351942A TITLE STABILIZERS-VERTICAL-FRONTSPAR-WEB AND CHORD SPLICE REPAIR- COVER E.A.
Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 71,768 hrs · 26,411 cycles
AUXILIARY SPAR FSS 340 TO FSS 371 TORN/DAMAGED REMOVED AND REPLAICED AUX SPAR IAW SRM 51-40-02 MAJOR REPAIR
2019
Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 71,523 hrs · 26,167 cycles
DURING PREFLIGHT NOTED L/H SIDE EMERG. LIGHTS AND EXIT SIGN SHORTLY ILLUMINATING. REPLACED BATTERY PACK ON POS. 1 ACC AMM 33-51-07-902-001 REV. 123.16 TESTED PER AMM. ALL WORKING SATIS.
2018
Part: ROD — OUT OF ADJUST (NLG STEERING) · airframe 71,188 hrs · 25,861 cycles
A/C STILL YAWS LEFT ON LANDING. ALSO, IT SEEMED TO YAW TO THE LEFT ON T/O ALSO, AND TAXI. REPEAT WRITE UP. JACKED LT GEAR PER MM 07-11-03-2. FOUND NO GRABBING BRAKES, FOUND THE INPUT ROD FOR THE RUDDER PEDAL STEERING MISS ADJUSTED, ADJUSTED ROD PER MM 32-51-00-5-3. NEED TO PERFORM A/C TAXI. PERFOMED TAXI TEST PER JRH, AIRCRAFT GOING STRAIGHT, STEERING SYSTEM WORKING GOOD.
Part: WIRE — SHORTED (MAIN CARGO DOOR) · airframe 71,170 hrs · 25,844 cycles
DEPARTING LFPG PASSING FL/80 MAIN DECK DOOR LIGHT ILLUMINATED. RETURNED LFPG. NO DEPRESSURIZATION NOTED. FOUND CARGO DOOR LIGHT BREAKER POPPED. DURING T/S, FOLLOWING WDM 52-32-02 FOUND WIRE 1067-20 SHORTED WITH SHIELD GD827-ST BETWEEN PLUG D40072J PIN 54 AND LIGHT ASSY L651 PIN 5. REPAIRED WIRE W2406-1067-20 BETWEEN PLUG D40072J PIN 54 AND LIGHT ASSY L651 PIN 5 IAW WDM 52-32-02 AND SWPM 20-10-13. OPS CHECK OK. A/C OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,127 hrs · 25,802 cycles
AT SERVICE CHECK FOUND RT SIDE EMERGENCY LIGHTS NOT ILLUMINATING. TROUBLESHOOTING FOR RT EMERGENCY LIGHTS NOT ILLUMINATING ACCOMPLISHED PER FIM 33-51-00-815-803 R 122.0. REPLACED RT BATTERY PACK (BATTERY, HOLDER ASSY/BATTERY, PN 2013-1A, S/N OFF 90495) IAW AMM 33-51-07-902-001 R 122.0. OPS CHECK GOOD, A/C IS OK FOR SERVICE.
Part: INDICATOR — FAULTY (CARGO DOOR) · airframe 71,108 hrs · 25,784 cycles
LEVEL AT CRUISE AT FL 270, MAIN CARGO DOOR LIGHT ILLUMINATED WHEN INDICATOR LIGHT WERE ON DIM, LIGHT EXTINGUISHED. WHEN INDICATOR LIGHTS MOVED BACK TO BRIGHT, MAIN CARGO DOOR LIGHT ILLUMINATED. COMPLIED WITH QRH. R&R MCD OPEN INDICATOR L651 AS PER SMP. INDICATOR ILLUMINATED WELL WHEN MAIN DECK DOOR IS OPEN. OPS CHECK OF MAIN DECK CARGO DOOR PER MM 52-32-00-5-0. ALL LIGHTS INDICATORS WORKED NORMALLY.
Part: CIRCUIT BREAKER — WEAK (DOOR INDICATOR) · airframe 71,088 hrs · 25,764 cycles
DURING A TRANSIT CHECK, FOUND THE CARGO DOOR INDICATOR LIGHT CIRCUIT BREAKER A30 ON THE P11, OPEN AND IMPOSSIBLE TO CLOSE. DURING TROUBLESHOOTING, FOUND THE CARGO DOOR INDCATOR CIRCUIT BREAKER WEAK. R & R THE CIRCUIT BREAKER IAW SWPM 20-30-00. PERFORMED A MAIN CARGO DOOR ADJUSTMENT TEST IAW AMM 52-32-00-2. ALL TESTS PASSED. ACFT OK FOR SERVICE.
Part: METERING VALVE — FAULTY (NLG STEERING) · airframe 71,065 hrs · 25,740 cycles
AIRCRAFT PULLING TO LEFT ON TAKEOFF & LANDING. REQUIRED A LOT OF RIGHT RUDDER. CREW DEBRIEF SAID AIRCRAFT IS PULLING LEFT ONLY ON GROUND, AND THEY DID NOT NOTICE IT ON TAXI BECAUSE OF SINGLE ENGINE TAXI. REPLACED STEERING METERING VALVE REF MM 32-51-12-4 AND PERFORMED STEERING RIGGING AND ADJUSTEMENT REF 32-51-00-5-3.
Part: INDICATION SYS — MALFUNCTIONED (CARGO DOOR) · airframe 71,044 hrs · 25,724 cycles
WITH MAIN CARGO DOOR CLOSED AND OVERHEAD CARGO DOORS LIGHT NOT ILLUMINATED, DISCRETE RED MAIN CARGO DOOR LIGHT STAYS ILLUMINATED. ARM/DISARM SWITCH IS DISARMED. MAINT PROCEDURE PERFORMED A30 C/B OPENED AND COLLAR. EACH DEPARTURE INSPECTION REQUIRED MCD CLOSED, LATCHED, LOCKED. RE-ACTIVATED SYSTEM, REF WDM 52-32-02 SH1, CHECKED PLUG D40716P, FOUND OK. CHECKED VISUALLY ALL WIRES UNTIL PLUG D40072J, ALL OK PER SWPM. COMPLIED WITH OPS CHK PER MM 52-72-00-5, FOUND ALL GOOD SEVERAL TIMES.
Part: BEARING — MALFUNCTIONED (DOOR) · airframe 71,017 hrs · 25,701 cycles
FOUND DURING PRE-DEPARTURE CHECK, ON RT ARM SLIDE LIGHT PARTIALLY IS WORKING AND DOOR IS DIFFICULT TO ARM. FOUND DAMAGED BEARING IN EMER DOOR MECHANISM, REPLACED. ADJUSTED/TESTED GIRT BAR MECHANISM PER MM, OPS OK.
Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 71,012 hrs · 25,695 cycles
LT EMERGENCY DOOR EICAS DURING FLIGHT. FOLLOWED FIM 52-71, FAULT TREE 805, ADJUSTED THE L3 EMERGENCY EXIT DOOR SENSOR S10096 IAW MM 52-71-00-05, PARAGRAPH 3, PERFORMED A TEST IAW MM 52-71-00-05, TEST PASSED.
Part: CIRCUIT CARD — FAULTED (PSEU) · airframe 71,011 hrs · 25,694 cycles
EICAS L EMERG DOOR CAME ON PASSING 12K FT WENT OUT AFTER LANDING. COMPLETED FIM PROCEDURE 52-71-00-1 FIG 104A . ON PSEU FOUND CARD 003 FAULT AFTER RESET AND VERIFY NO FAULTS OBSERVED ANYMORE. ALSO VISUAL CHK ON LT EMERG DOOR ACTIONED ALL SATIS.
Part: PSEU — FAILED (DOOR WARNING) · airframe 71,010 hrs · 25,693 cycles
"L EMER DOOR" EICAS MESSAGE APPEARED AT 13000 FT, COMPLIED WITH QRH. CONTINUED FLIGHT TO CDG. PSEU CHANGED.
Part: FLAP TRACK — LOOSE (LT WING) · airframe 71,009 hrs · 25,692 cycles
LT WING, NR 1 AND NR 2 FLAP TRACKS LOOSE AT AFT ATTACH POINT TO REAR SPAR. REPLACED NR 1 AND NR 2 FLAP TRACK ATTACHING HARDWARE (WITH FLAP TRACKS REMOVED) IAW AMM 27-51-15 SEE SNRM N00557 FOR DETAILED WORK STEPS.
Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 71,009 hrs · 25,692 cycles
RT WING, NR 7 AND NR 8 FLAP TRACKS LOOSE AT AFT ATTACH POINT TO REAR SPAR. REPLACED NR 7 AND NR 8 FLAP TRACK ATTACHING HARDWARE (WITH FLAP TRACKS REMOVED) IAW AMM 27-51-15 SEE SNRM N00558 FOR DETAILED WORK STEPS.
Part: SKIN — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
CORROSION ON BUTT JOINT AT B STA 440, BETWEEN STR 24-25 RT PERFORMED SKIN REPAIR AT BUTT JOINT AT BSTA 440, STR 24-25R IAW EA F-5330-T0340309. TITLE: FUSELAGE - PLATES & SKINS - FUSE SKIN CORROSION AT BSTA 440 STR 24-25R.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
FLOORBEAM TOP CAP CORROSION BSTA 345, LBL9 - LBL 18. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-51-1A REV124. FLOORBEAM REPAIRED IAW SRM 53-00-51-2R REPAIR 10 REV 124.
Part: SKIN — DAMAGED (TE FLAP) · airframe 71,009 hrs · 25,692 cycles
RT IN/BD MAIN FLAP, PUNCTURE ON THE LOWER SURFACE OF TRAILING EDGE PANEL REPAIRED PUNCTURE ON THE LOWER SURFACE OF THE R/H IN/B MAIN FLAP 80" FROM IN/B EDGE AND 7" FROM AFT EDGE IAW EA F-5750-T0340210 P1.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
MAIN DECK FLOOR INTERCOSTAL AT BSTA 324 - 345, LBL 20 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-04-04-1A REV124. REPLACED INTERCOSTAL IAW SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
FLOORBEAM AT BL0 BSTA 345-365 FOUND TOP CAP CORROSION. CORROSION REMOVED & EVALUATED IAW SRM 53-00-51-1A, FIGURE 101, DETAIL III. FOUND OUT OF LIMITS. FLOORBEAM REPLACED IAW SRM51-40-01 REV124 AND DRAWING 141N5190.
Part: STRUCTURE — CORRODED (LE SLAT) · airframe 71,009 hrs · 25,692 cycles
LT WING, NR 1 L/E SLAT HAS CORROSION ALONG LOWER T/E CHORD. REPLACED CHORD IAW SRM 51-40-02 & DRAWING 114N4002-7.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,009 hrs · 25,692 cycles
MAIN DECK FITTING FOUND CORROSION AT BSTA 333, RBL 3. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-04-1A REV124. FABRICATED AND INSTALLED NEW FITTING IAW DRAWING 141N5161 AND SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,009 hrs · 25,692 cycles
MAIN DECK INTERCOSTAL CORROSION AT BSTA 331, RBL 31. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-04 REV124. INTERCOSTAL REPLACED IAW SRM 51-40-02 REV124.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
SEAT TRACK AT BSTA 345 - 377 LBL 7, FOUND CORRODED. SEAT TRACK REPLACED IAW SRM 51-40-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
SEAT TRACK AT BSTA 345 - 377 RBL 14 FOUND CORRODED. REPLACED IAW SRM 51-40-02.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 71,009 hrs · 25,692 cycles
MAIN DECK FLOORBEAM AT BSTA 297, RBL29 FOUND ELONGATED HOLES REPAIR CARRIED OUT IAW EAF-5310-T0340325 TITLE : FUSELAGE - MAINFRAME - FLOOR BEAM BSTA297 ELONGATED HOLES.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 71,009 hrs · 25,692 cycles
RIGHT OUTBOARD MAIN FLAP HAD DELAMINATION ON THE UPPER T/E PANEL AREA. REPAIRED IAW SRM 57-53-02, DETAIL VII, SRM 57-53-01-2R, DETAIL III, TABLE III, AND SRM 51-70-07-0G, FIGURE 2, REV 124. ACCOMPLISHED EA F-5750-T0340213.
Part: SKIN — CORRODED (LE SLAT) · airframe 71,009 hrs · 25,692 cycles
NR 1 LEADING EDGE SLAT HAD CORROSION ON THE INBOARD LOWER L/E SKIN. REPAIRED IAW SRM 57-43-01-2R, REPAIR 13, & EA F-5750-T0340268.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 71,009 hrs · 25,692 cycles
FWD WET AREA FLOOR PANEL 222BF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REV 124.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,009 hrs · 25,692 cycles
FWD WET AREA BOARD 222 MEF IS DAMAGED AND REQUIRES REPAIR. REPAIRED DAMAGED FLOOR PANEL 222MEF IAW SRM 53-00-50-2R FIG 201 REV 124.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,009 hrs · 25,692 cycles
FWD WET AREA BOARD 221 MAF IS DAMAGED AND REQUIRES REPAIR. REPAIRED FLOOR PANEL 221MAF IAW SRM 53-00-50 -2R FIG 201 REV 124.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,009 hrs · 25,692 cycles
FWD WET AREA BOARD 222 MDF IS DAMAGED AND REQUIRES REPAIR. REPAIRED FLOOR PANEL 22MDF IAW SRM 53-00-50-2R FIG 201 REV 124.
Part: SKIN — CORRODED (LE SLAT) · airframe 71,009 hrs · 25,692 cycles
NUMBER 7 LEADING EDGE SLAT HAS CORROSION ON THE LEADING EDGE SKIN, INBOARD UPPER SURFACE. NUMBER 7 LEADING EDGE SLAT REPAIRED IAW SRM 57-43-01-2R REPAIR 8 REV 124 AND EA F-5750-T0340218 P1.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 71,009 hrs · 25,692 cycles
MAIN CARGO FLOOR PANEL 251MXF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REV 124.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 71,009 hrs · 25,692 cycles
MAIN CARGO FLOOR PANEL 252MWF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 71,009 hrs · 25,692 cycles
MAIN CARGO FLOOR PANEL 252MUF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REV 124.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 71,009 hrs · 25,692 cycles
MAIN CARGO FLOOR PANEL 251MUF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R, FIG 201, REV 124.
Part: NUT PLATE — CORRODED (BS 1682) · airframe 71,009 hrs · 25,692 cycles
CORROSION FOUND ON THE NUTPLATE STRIP ON THE MAIN CARGO DECK FLOORBEAM AT BS 1682. REPAIRED IAW SRM 53-60-51-2R.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,009 hrs · 25,692 cycles
FWD WET AREA BOARDS 222AF DAMAGED AND REQUIRES REPAIR FOR DELAMINATION AND INSERTS. REPAIRED FLOOR PANEL 222AF IAW SRM 53-00-50-2R FIG 201 REV 124.
2017
Part: RESERVOIR — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 70,665 hrs · 25,415 cycles
L1 DOOR SLIDE DEPLOYED OPENING DOOR FROM INSIDE. DOOR ARMED LIGHT WAS OUT WITH KNOCKER DOWN R & R THE L1 SLIDE SLIDE IAW MM 25-66-01-4. CHECKED OK. R & R L1 DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4, ALL CHECKED OK. .ACFT OK FOR SERVICE.
Part: BOTTLE — FAILED (CREW OXYGEN) · airframe 70,643 hrs · 25,391 cycles
DURING REMOVAL PROCEDURE FOR FWD CREW OXYGEN BOTTLE, THE AFT CREW OXYGEN BOTTLE SHUT OFF VALVE WAS FOUND TO BE FAULTY AND WOULD NOT SHUT OFF CREW OXYGEN FLOW TO THE COCKPIT. BLED OFF ALL OF THE AFT OXYGEN CYLINDER CONTENTS. REMOVED AND REPLACED AFT OXYGEN BOTTLE IAW AMM 35-11-32
Part: COVER — OUT OF POSITION (L1 DOOR SLIDE) · airframe 70,560 hrs · 25,338 cycles
ON ARRIVAL, THE L1 DOOR DID NOT FULLY OPENED FROM INSIDE AND WAS STUCK IN MID TRAVEL. THE L1 DOOR SLIDE COVER WAS FOUND OUT OF PLACE . THE COVER WAS INSTALLED PROPERLY IAW MM 25-66-4.OPS CHECKED IAW MM 52-11-00-2, AND FOUND OK.
Part: LIFE RAFT — OUT OF POSITION (L1 DOOR) · airframe 70,349 hrs · 25,179 cycles
L1 DOOR WILL NOT OPEN PAST INITIAL UNLATCH. FOUND THE LIFE RAFT NOT IN THE PROPER POSITION, ADJUSTED THE RAFT IAW MM 25-66-01/401. ACFT OK FOR SERVICE .
Part: PROXIMITY SENSOR — DIRTY (GIRT BAR) · airframe 70,175 hrs · 25,056 cycles
SLIDE ARMED LIGHT ON R1 DOOR WOULD NOT ILLUMINATE. REPLACED THE BULB, WORKED INTERMITTENT IAW AMM 33-20-00. CONTACTS CLEANED AND DEBRIS REMOVED FROM GIRT BAR PROXIMITY SWITCHES ON FLOOR. ALL OPS NOW GOOD.
2016
Part: CONTROL PANEL — FAILED (CABIN) · airframe 69,860 hrs · 24,870 cycles
DURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHT SWITCH INOP. REPEAT WRITE UP. SWAPPED EMERGENCY LIGHT/PASENGER OXY CONTROL PANEL PER MM 33-51-08-4. PERFORMED TEST PER MM 33-51-00-05.
Part: LIGHT — NOT SEATED (CABIN) · airframe 69,859 hrs · 24,869 cycles
EMERGENCY EXIT 'UNARMED' LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS POSITIONED TO OFF. LIGHT CHECKS OK WHEN LIGHTS ARE TESTED, ITS NOT A BURNT OUT BULB. EMERGENCY 'UNARMED' CAUTION LIGHT FILAMENTS RESEATED. EMERGENCY LIGHTS TESTED FROM PILOTS SWITCH SATIS. 'UNARMED' LIGHT NOW ILLUMINATES IN THE OFF POSITION IAW AMM 33-51-00-5.
Part: MODULE — DEFECTIVE (COCKPIT) · airframe 69,859 hrs · 24,869 cycles
REPEAT WRITE UP-UNARMED LIGHT DOES NOT ILLUMINATE WHEN COCKPIT OVERHEAD EMERGENCY LIGHTS SWITCH PLACED TO OFF POSITION. R&R BOTH OF FUSE DIODE MODULE AND LENS CAP ASSEMBLY PER STANDARD WIRING PRACTICES MANUAL 20-84-18. OPS CHECK GOOD. A/C OK FOR SERVICE.
Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 69,814 hrs · 24,828 cycles
R1 DOOR - UNABLE TO DISARM THE SLIDE. FOUND DIRT AND TRASH AT THE GIRT BAR SLIDE MECHANISM. REMOVED,CLEANED AND LUBRICATED THE GIRT BAR MECHANISM IAW AMM 12-21-18-3. OPS CHECKED GOOD IAW AMM 25-66-00.
Part: SKATE ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
MAIN CABIN STATION 1018 LT SIDE, SKATE ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A. CUT OUT DAMAGED SECTION FROM STA 990 TO 1040 LT SKATE ANGLE. FABRCATED AND INSTALLED CREASE BEAM INBRD SPLICE REPAIR STA 990-1040 IAW B757 SRM 53-00-13-2R REPAIR 1.
Part: FRAME — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
RIGHT ELEVATOR TE 2ND STATIC WICK FROM OTBD END, HAS SIGNS OF CORROSION AROUND BASE. REMOVED 2ND STATIC WICK FROM O/B END, EVAL AREA FOUND CONDUCTIVE FRAME OUT OF LIMITS. REMOVED CONDUCTIVE FRAME , FABRICATED, LOCATED AND INSTALLED CONDUCTIVE FRAME ON RT ELEVATOR UPPER SURFACE IAW BOEING DWG 183N2007 REV B. INSTALLED SECOND STATIC WICK FROM O/B END IAW AMM 23-61-01-2, RESISTANCE CHECK IS GOOD IAW AMM 23-61-01-2.
Part: SKATE ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
MAIN CABIN, BETWEEN STATION 1180 - 1020, LT SIDE SKATE ANGLE CORRODED. REMOVED CORROSION FROM MAIN CABIN SKATE ANGLE IAW SRM 51-10-02. MATERIAL LOSS .035, ORIGINAL THICKNESS .071, REMAINING MATERIAL .036, OUT OF LIMITS IAW SRM 53-40-13-1A. CUT OUT DAMAGED SECTION & INSTALLED REPAIRS IAW SRM 53-00-13-2R REPAIR 2.
Part: SKATE ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
MAIN CABIN STATION 939 RT SKATE ANGLE CORRODED. REMOVED CORROSION IAW 51-10-02, MATERIAL LOSS OF .011, ORIGINAL THICKNESS.071, REMAINING MATERIAL .060, OUT OF LIMITS IAW SRM 53-60-13-1A. CUT OUT DAMAGED SECTION OF MAIN CABIN SKATE ANGLE, STATION 900 - 957. FABRICATED REPAIR PARTS & INSTALLED REPAIRS IAW SRM 53-00-13-2R REPAIR 2.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
MAIN CABIN, BETWEEN STATION 1420 - 1440 RT SIDE CUSP WEB CORRODED. R & R CUSP WEB MAIN CABIN IAW SRM 51-40-02 & DWG 1465590 REV E.
Part: FITTING — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 69,395 hrs · 24,548 cycles
NUMBER 2 ENG STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL OTBD AFT, INBD MOST FASTENER HOLE HAS CORROSION. WORK PERFORMED ON EA F-5450-T0325148 AT NR 2 ENG STRUT TO DIAGONAL BRACE FITTING, HORIZONTAL FLANGE OTBD AFT FASTENER HOLE. NACELLE & PYLON- PYLON STRUCTURES DEVIATION TO EO F-5450-7-5006 DUE TO CORROSION IN BULKHEAD AT BRACE FITTING MOUNT HOLE ON NR 2 RT PYLON.
Part: SKIN — GOUGED (LT HORIZ STAB) · airframe 69,395 hrs · 24,548 cycles
LEFT HORIZONTAL STAB LOWER SKIN HAS A DENT WITH GOUGE AT STAB STATION 104. EVALUATED GOUGED DENT ON LT HORIZONTAL STAB LOWER SKIN & FOUND TO BE OUT OF LIMITS DUE TO GOUGE IAW SRM 55-10-01-1A FIG 101 TABLE I DETAIL IV. BLENDED GOUGE & APPLIED PERMANENT REPAIR IAW SRM 51-70-10-2R REPAIR 2 PGH 4E & F.
Part: SKIN — CRACKED (L1 DOOR) · airframe 69,395 hrs · 24,548 cycles
L1 DOOR OUTER SKIN, UPPER FWD CORNER BENT WITH POSSIBLE CRACK. COMPLIED WITH REPAIR ON L1 DOOR OUTER SKIN UPPER FWD CORNER IAW SRM 52-10-01-2R REPAIR 7.
Part: SKIN — DENTED (FUSELAGE) · airframe 69,395 hrs · 24,548 cycles
DENT & GOUGED IN FUSELAGE SKIN, STATION 1580 - 1600, STRINGER 15R - 16R. CUT OUT DAMAGED AREA OF SKIN , DIM 2.3" X 1.8" & INSTALLED REPAIR IAW SRM 53-00-01-2R REPAIR 16.
Part: PANEL — CORRODED (TE FLAP) · airframe 69,395 hrs · 24,548 cycles
LEFT WING TE INBD MAIN FLAP, UPPER SURFACE TE WEDGE PANEL HAS SPOTS OF CORROSION AT MID OTBD SECTION. REPAIRED LT WING INBD MAIN FLAP UPPER SURFACE BY HOT BONDING FILLER & DOUBLER IAW SRM 57-53-01-2R FIG 201 & SRM 51-70-10-2R PARA 20.
Part: AUTOTHROTTLE SYS — MALFUNCTIONED (N/A) · airframe 69,320 hrs · 24,477 cycles
AT 40 KTS, MASTER CAUTION, AUTOTHROTTLE DISC, ALERT APPEARED ON EICAS. REJECTED TAKEOFF. CLEARED MESSAGE WITH AUTOTHROTTLE DISCONNECTS ON THROTTLE QUADRANT. PERFORMED TROUBLESHOOTING & TEST ITEM 02, 05, 10 IAW FIM 22-03 FAULT TREE 828 FIM 22-03 FAULT TREE 835, NO FAULT FOUND. ALL TEST PASSED. PERFORMED TEST MCDP ITEM 30 & 40 FOR LLM IAW AMM 22-00-02-2, TEST PASSED. OPERATIONS CHECKED OK. ACFT STILL CAT 3.
Part: WARNING LIGHT — FALSE ACTIVATION (AUTOTHROTTLE) · airframe 69,320 hrs · 24,477 cycles
AT 40 KTS, MASTER CAUTION, AUTO THROTTLE DISC, ALERT APPEARED ON EICAS. REJECTED TAKEOFF. CLEARED MSG WITH AUTOTHROTTLE DISCONNECTS ON THROTTLE QUADRANT. THRUST MANAGEMENT SYS & AUTO THROTTLE SYS INOPERATIVE. THRUST MANAGEMENT SYS & THROTTLE SYS INOPERATIVE. PERFORMED T/S AND TEST ITEM 02,05,10 PER FIM 22-03 FAULT TREE 828, FIM 22-03 FAULT TREE 830 AND FIM 22-03 FAULT TREE 835,NO FAULT FOUND,ALL TEST PASSED. PERFORMED TEST MCDP ITEM 30 AND 40 FOR LLM IAW AMM 22-00-02-2.TEST PASSED.OPS CHECK OK. ACFT STILL CAT 3.
2015
Part: PROXIMITY SWITCH — OUT OF ADJUST (GIRT BAR) · airframe 691 hrs · 24,331 cycles
DURING PRE-FLIGHT CHECK, FOUND ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT R1 DOOR WORKING INTERMITTENTLY. PROXIMITY SWITCH ADJUSTED IAW AMM 25-66-11-2.
Part: SLIDE — PARTIAL DEPLOY (RIGHT) · airframe 691 hrs · 24,328 cycles
DURING WALK AROUND FOUND RT FWD ESCAPE SLIDE PARTIALLY DEPLOY.
Part: TUBE — CRACKED (RT ENGINE) · airframe 690 hrs · 24,173 cycles
ON CLIMB OUT THE RT ENG SHOWED LOW FUEL FLOW 3.7 WITH A HIGH EPR 1.71. THE TMC EPR WAS 1.60. PUSHING THE THROTTLE UP TO MATCH FUEL FLOW WITH RT ENG RESULTED IN FUEL FLOW ONLY CHANGING 300 - 400 LBS AN HR TO APP 4.1, WHILE EPR INCREASED TO 1.8 - 1.9 WITH NO INCREASE IN POWER OUTPUT, NOTICEABLE YAW. AIRPLANE COULD NOT CLIMB ABOVE FL220. R & R RT ENG P1 TUBE ASSEMBLY IAW AMM 73-21-04-4.
2014
Part: SEAT TRACK — CORRODED (BS 680) · corrosion level 2 · airframe 68,062 hrs · 23,436 cycles
SEAT TRACK AT BS 680 RBL 45 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION BS 640-780 IAW SRM 51-40-02, SRM 51-20-01 AND DRAWING 143N5080.
Part: WIRE — BROKEN (PROXIMITY SENSOR) · airframe 68,062 hrs · 23,436 cycles
R1 DOOR SLIDE WILL NOT ARM DOOR CLOSED CORRECTLY. R & R R1 DOOR GIRT BAR & ADJUSTED FWD & AFT FLOOR FITTING IAW MM 25-66-10-2. VERIFIED PROXIMITY SWITCH ADJUSTMENT IAW MM 25-66-11-2. PERFORMED ADJUSTMENT TEST OF R1 DOOR & GIRT BAR IAW 52-11-25-5. FOUND WIRE BROKEN AT FWD SENSOR S10214, WIRE IS TOO SHORT FOR ENVIRONMENTAL SPLICE. REQUIRES NEW SENSOR. CAPPED WIRE AT SWITCH IAW WDM 25-66-11. REPLACED GIRT BAR, PERFORMED ADJUSTMENT TEST AMM 52-11-25-5.
2013
Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 67,545 hrs · 23,106 cycles
L1 DOOR IS DIFFICULT TO CLOSE. ARM DOES NOT SEEM TO BE ASSISTING-DOOR IS VERY HEAVY. PERFORMED LUBRIFICATION ARM HINGE IAW MM 12-21-18-3 AND TESTED L1 DOOR IAW MM 52-11-00-6 PARA 3. FOUND OK. FINAL CLOSED.
Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 67,159 hrs · 22,820 cycles
DURING TAKEOFF ROLL APPROX 80 KIRS GET SEVERAL EICAS ALERTS INCLUDING AUTOTHROTTLE DISC. PROBE HEAT FMC MESSAGE ALL SPEED BUGS ON AIRSPEED TAPE DISCONECTED THRUST REF ON UPPER EICAS WAS G/A AFTER LEVELING AT 6000 MSL AND RETRAITING FLAPS AUTO THROTTLE REENGAGED AND ALL MESSAGES WANT AWAY REMAINDER OF FLIGHT WAS NORMAL. PERFORMED PSEU BITE TEST AND FOUND SYS OK. FIM 32-61, TREE 803, ALSO VISUALLY CHECK PROXIMITY SENSORS. FOUND OK.
Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 67,037 hrs · 22,732 cycles
DURING TRANSIT CHECK, FOUND EMERGENCY POWER BOTTLE FOR DOOR 1R UNDER 1000 PSI. MUST BE REPLACED. R & R EMERGENCY POWER BOTTLE FOR DOOR 1R IAW MM: 52-11-33-4 . ACFT READY FOR SERVICE.
2012
Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 66,882 hrs · 22,586 cycles
LEFT EMERGENCY DOOR EICAS DURING CRUISE AT FL370. MESSAGE WENT OUT AT APPROX FL200. CLEANED SENSOR FOR LT EMERGENCY EXIT DOOR. PERFORMED PROXIMITY SWITCH TARGET TEST (096) AND DISPLAYED TARGET NEAR WITH LT EMERGENCY EXIT DOOR NR 3 IN CLOSED POSITION.
Part: SENSOR — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 66,843 hrs · 22,551 cycles
LEFT EMERGENCY DOOR EICAS MESSAGE AT FL 370 AT FL210. C/OUT PSEU BITE TEST IAW AMM 52-71-00-5. SENSOR 96 SHOWN. PSEU RESET AND TEST C/OUT AGAIN, OK. TARGET TEST SENSOR 96 NEAR-OK. DOOR PHYSICALLY CHECKED, CLOSED IAW MOC NO HISTORY ON FAULT.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,824 hrs · 22,535 cycles
LEFT WING, OTBD T/E AFT FLAP LOWER SKIN HAS A SHALLOW DENT 10 INCHES FROM T/E, APPROX 6 FEET OTBD OF INBD FLAP TRACK 2. LT WING OTBD T/E AFT FLAP LWR SKIN APPROX 6 FOOT OTBD OF INBD FLAP TRACK 2. REPAIRED IAW SRM 57-53-01, PARA 4C.
Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 66,824 hrs · 22,535 cycles
EVIDENCE OF CORROSION ON SHEAR PLATE BETWEEN STA 1701-1715.5 AT RBL 51.00. CORROSION REMOVED FROM SHEAR PLATE, ASSESSED AND FOUND TO REQUIRE A REPAIR IAW ASSESSMENT REF SRM 53-60-51, REPAIR CARRIED OUT IAW SRM 53-60-51. CAT A REPAIR. REPAIR CLASSED AS MAJOR.
Part: ANGLE — CRACKED (ZONE 100) · airframe 66,824 hrs · 22,535 cycles
RT FUSE WING TO BODY FAIRING SUPPORT STRUCTURE UPPER ATTACHMENT ANGLE FWD OF PANEL 196ER EVIDENCE OF A CRACK. REPLACED IAW SRM 51-40-02.
Part: SKIN — GOUGED (ZONE 200) · airframe 66,824 hrs · 22,535 cycles
GOUGE AROUND FASTENER AFT OF L3 DOOR, 3" ABOVE STRINGER 11 AT STATION 1352. GOUGE BLENDED OUT AND ASSESSED IAW SRM 53-00-01, FIG 101, DETAIL 2 AND FOUND TO BE WITHIN LIMITS. CLASSED AS MAJOR.
Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,824 hrs · 22,535 cycles
CORROSION FWD CARGO SILL CORROSION FOUND UNDER FWD CARGO BAY FITTING AT BS 600. CARRY OUT FABRICATION AND REPLACEMENT OF TEE FITTING IAW SRM 51-70-12 AND DWG 143N8522. REPAIR CARRIED OUT IAW EA F-5330162995
Part: PANEL — CRACKED (NR 10 SLAT) · airframe 66,824 hrs · 22,535 cycles
RIGHT WING NR 10 SLAT INNER COVE SKIN HAS EVIDENCE OF A SUSPECTED CRACK STARTING FROM A FASTENER.
Part: SKIN — CORRODED (ZONE 500) · airframe 66,824 hrs · 22,535 cycles
CORROSION FOUND ON LEFT WING UPPER SKIN PANEL BETWEEN WBL 80 AND 100. FOUND TO BE OUT OF SRM LIMITS REF 57-21-01, FIG 101, SHEET 4. ACCOMPLISHED IAW EA F-5721-162988
Part: SKIN — CRACKED (ZONE 600) · airframe 66,824 hrs · 22,535 cycles
RIGHT WING NR 9 SLAT INNER COVE SKIN INBD TRACK HAS EVIDENCE OF A SUSPECTED CRACK STARTING FROM A FASTNER 4TH FROM TOP APPROX .3" LONG. REPAIR ACCOMLISHED IAW EA 5740-162991.
Part: SKIN — CRACKED (ZONE 600) · airframe 66,824 hrs · 22,535 cycles
RIGHT WING NR 9 SLAT INNER COVE SKIN OTBD TRACK LOCATION HAS EVIDENCE OF A SUSPECTED CRACK FROM A FASTENER THIRD DOWN FROM SEAL LOCATION. REPAIR ACCOMPLISHED IAW EA F-5740-162991.
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 66,824 hrs · 22,535 cycles
DRY BAY PANEL 632BZ (RT WING) PANEL HAS DAMAGE TO 1 EA .2500 DIA BONDING HOLE. REPAIRED IAW SRM 57-20-09, 51-70-06 PARA 5 B REV 106
Part: SKIN — CORRODED (ZONE 600) · airframe 66,824 hrs · 22,535 cycles
RIGHT WING TOP SKIN UPPER SURFACE HAS CORROSION DAMAGE AROUND FASTENER AT APPROX WBL84, REAR SPAR ATTACHMENT AREA. AREA FOUND OUT OF LIMITS DUE TO FLAG NOTE (A) IN SRM 57-20-01, SHEET 4. ACCOMPLISHED IAW EA F-5720-162982
Part: PANEL — DENTED (LT WING LE SLAT) · airframe 66,824 hrs · 22,535 cycles
LEFT WING NR 5 SLAT HAS EVIDENCE OF A LARGE LIFTING PAINT CHIP ON THE INNER SKIN JUST OTBD OF THE CNT TRACK FITTING. FOUND TO BE FILLER REPAIR COVERING A LARGE DENT OUT OF SRM 57-43-01 LIMITS.
Part: SKIN — CHAFED (ZONE 600) · airframe 66,824 hrs · 22,535 cycles
RIGHT WING UPPER SKIN HAS ABRASION DAMAGE WHERE PANEL 192DR CONTACTS, ESPECIALLY AT STA 1040 AREA. SRM 57-20-01, FIG 101. REPAIRED IAW EA F-5720-162987
Part: SKIN — CHAFED (ZONE 500) · airframe 66,824 hrs · 22,535 cycles
LEFT WING UPPER SKIN HAS ABRASION DAMAGE WHERE PANEL 191DL CONTACTS, ESPECIALLY AT STA 1030-1040. SRM 57-20-01, FIG 101, TABLE 1. ACCOMPLISHED IAW EA F-5720-162986
Part: SKIN — CORRODED (ZONE 500) · airframe 66,824 hrs · 22,535 cycles
LEFT WING TOP SKIN HAS AREA OF CORROSION AROUND FASTENER AT APPROX WS772, 4" AFT OF THE FRONT SPAR SKIN EDGE. AREA FOUND TO BE OUT OF LIMIT DUE TO FLAG NOTE (A) REF SRM 57-20-01, SHEET 4. ACCOMPLISHED IAW F-5720-162983
Part: SKIN — DAMAGED (ZONE 500) · airframe 66,824 hrs · 22,535 cycles
LEFT WING UPPER AFT INBD PANEL HAS NUMEROUSE PULLED FASTENER HEADS ALONG THE FWD ROW LOCATED APROX WS177. REPAIRED IAW EA F-5751-162992
Part: FLOORBEAM — DAMAGED (BS 1681-1701) · airframe 66,824 hrs · 22,535 cycles
STRUCTURE FOUND MISSING FROM FLOOR SUPPORT BS 1681- 1701, LBL5.9. REPAIRED IAW EA F-5330-162996 AND SRM 51-40-02.
Part: SLIDE — FAILED (PAX DOOR) · airframe 66,811 hrs · 22,524 cycles
RIGHT ENTRY DOOR DID NOT PROPERLY DISARM. SLIDE DID NOT INFLATE. R & R RT EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4 AND CK IAW MM 52-11-30-6, ALL CK OK. PLACARD REMOVED, ACFT OK TO CONTINUE.
Part: HANDLE — UNKNOWN (PAX DOOR) · airframe 66,793 hrs · 22,503 cycles
L1 DOOR HANDLE RIDES UP IN FLIGHT (ACFT PRESSURIZED) 3 OR 4". ADJUSTMENT TEST ACCOMPLISHED IAW AMM 52-11-13-2 AND AMM 52-11-04-2. NO DISCREPANCIES FOUND. DOOR OPS CHECKED IAW AMM 52-11-00 ACFT REQUIRES CABIN PRESSURE CHECK. CABIN PRESSURIZED IAW AMM 05-51-24-2 DOOR LEVER RAISED 1.5" DURING PRESSURIZATION. PRESSURIZED CABIN PER MM 05-51-24-2 AND OBSERVED DOOR HANDLE. NO MOVEMENT NOTED. DOOR WARNING SYST TEST PER MM 52-71-00/501 SATISFACTORY. ALL DOOR OPS AND INDICATES NORMAL NOW. ACFT OK FOR SERVICE.
Part: TARGET — OUT OF ADJUST (DOOR WARNING) · airframe 66,738 hrs · 22,471 cycles
INTERMITTENT " LT FWD ENTRY DOOR " EICAS AFTER LANDING. ALL FLIGHT INFORMATION ON FMS WAS LOST AFTER EICAS MESSAGE, DOOR APPEARED CLOSED. ADJUSTED PROXIMITY TARGET IAW SMP OPS CHECKED GOOD.
Part: HOSE — LEAKING (HYD SYSTEM) · airframe 66,469 hrs · 22,273 cycles
ON SHORT FINAL EICAS "LT HYD QTY " ALL OTHER ASSOCATED EICAS MESSAGES CAME ON. 1-RUDDER RATIO 2-L YAW DAMPER 3- L HYD SYS PRESSURE. R & R FLEX HOSE FOR TEMPORARY REPAIR REF TO ER 12-02644. RETURN FILTER POPOUT IND CHECKED. FOUND NOT POPPED OUT. FOUND SATIS IAW AMM 29-11-00. OPS CHECK C/O. NO LEAK.
Part: STATIC LINE — OUT OF POSITION (R1 DOOR SLIDE) · airframe 66,152 hrs · 22,036 cycles
THE ARM LIGHT ON THE RT ENTRY DOOR IS NOT ILLUMINATED WHEN IN THE ARM POSITION. REPOSITIONED AND SECURED SLIDE PACK STATIC LINE REF AMM 25-66-01-4 & 25-66-10-2. SLIDE ARMED LIGHT CHECKED NORMAL.
2011
Part: RESERVOIR — LEAKING (L1 DOOR) · airframe 65,939 hrs · 21,906 cycles
DOOR ASSIST BOTTLE HAS 0 PRESSURE. R & R L1 DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.
Part: SKIN — DENTED (BS 1690 S14-15R) · airframe 65,335 hrs · 21,529 cycles
DENT STA 1690 STRINGERS 14R - 15R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER 2024T3, .080, STRUCTURAL FILLER 2024T3, .063. TAPERED FILLER 2024T3, .020 AND FILLER 2024T3, .071. INSTALLED REPAIR PARTS IAW EA NR F-5330-123584. CLOSED AND DEACTIVATED R4 DOOR IAW AMM P-F 52-11-13.
Part: SKIN — DENTED (BS 684 S26R) · airframe 65,335 hrs · 21,529 cycles
DENT ON FUSELAGE IN LAP SEAM, STA 684, STR 26R. FOUND DENT OUT OF LIMITS DUE TO LOCATION ON A LAP SEAM IAW SRM 53-00-01 FIGURE 101. TRIMMED OUT DAMAGE, FABRICATED REPAIR FILLER, STRUCTURAL FILLER, DOUBLER, AND TRIPLER IAW EA F-5330-123582. INSTALLED REPAIR PARTS AT STATION 684, STRINGER 26 RT IAW EA F-5330-123582.
Part: SPAR — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 65,335 hrs · 21,529 cycles
NR 5 SLAT FRONT SPAR HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-43-02. CUT OUT DAMAGED AREAS IAW SRM 51-70-11. FABRICATED REPAIR PARTS IAW SRM 51-70-11. INSTALLED REPAIR PARTS IAW SRM 51-70-11.
Part: SKIN — CORRODED (BS 480 S28L) · corrosion level 2 · airframe 65,335 hrs · 21,529 cycles
UPON REMOVAL OF DAMAGED STRINGER, FOUND PITTING CORROSION ON SKIN, BENEATH S28L AT STA 480, IMMEDIATELY AFT OF FRAME.
Part: CHANNEL — CORRODED (BS 480 S28L) · corrosion level 2 · airframe 65,335 hrs · 21,529 cycles
CORROSION INSIDE CHANNEL - STR 28L, STA 480, IMMEDIATELY AFT OF FRAME. REMOVED DAMAGED PORTION OF STRINGER DIM 9 1/4 LONG IAW B757 SRM 53-00-03. FIG 201. FABRICATED PORTION OF STRINGER IAW SRM 53-30-03 FIG 201. INSTALLED NEW PORTION OF STRINGER AND SPLICE IAW SRM 51-40-02 AND EA F-5330-123581.
2010
Part: GROUND WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 64,874 hrs · 21,257 cycles
EMERGENCY LIGHT IN COCKPIT ABOVE OBSERVER SEAT INOP. INSTALLED NEW EMERGENCY POWER SUPPLY, NO HELP, FOUND SHORT TO GROUND WIRE FROM FLIGHT DECK EMERGENCY LIGHT D5264, TO PIN 12 ON POWER SUPPLY CONNECTOR D68. SHORT IS BLOWING FUSE INSIDE POWER SUPPLY. REF WDM 33-51-12. REPLACED POWER SUPPLY IAW MM 33-51-07-2-0. NO HELP.
2009
Part: FITTING — DAMAGED (ZONE 700) · airframe 63,958 hrs · 20,678 cycles
RT TRUNNION,O/B SUPPORT BRACKET AND O/B HOLES IN TRUNNION AND ATTACH FITTING ASSY, HAS ELONGATED HOLES. FREEZE PLUGS FOR YOKE FABRICATED FREEZE PLUG FOR TRUNNION COMPLIED WITH E.A. F-5750-131116 AND FAA FORM 8100-9, DATED 09/01/2009. (INTERIM REPAIR DTA PENDING). (MAJOR REPAIR) FREEZE PLUG INSTALLED, IN THE RIGHT TRUNNION FITTING.
Part: FRAME — DAMAGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
FRAME 1280 INBD FLANGE IS DAMAGED AT STRINGER 16RT. FABRICATED DOUBLER AND FILLER FROM 7075T6 .080 ON MAE TRAVELER T9/790596 IAW SRM 51-70-11 AND INSTALLED IAW SRM 51-70-11.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
MAIN CABIN SEAT TRACK RBL 45 IS CORRODED AT BS 466 AND GOUGED AT BS 472. FABRICATED AND INSTALLED NEW SEAT TRACK FROM 602-6549/24 BATCH 0001541987 IAW SRM 53-30-52 AND SRM 51-40-02.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
SEAT TRACK HAS GOUGE ON CROWN AREA AT STA 1064, LBL 24. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK ON MAE TRAV T9/799981, INSTALLED SEAT TRACK AND PLATES IAW SRM 53-00-52. REPAIR 4, CATEGORY "A", MAJOR REPAIR.
Part: FRAME — MISALIGNED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
EXISTING HOLES IN FRAME AT STA 395, BETWEEN S3L-S3R, INTERFERES WITH INSTALLATION OF CABLE SHROUD MOD-. AT STA 395, S3L-S3R, FRAME REPAIR WAS ACCOMPLISHED , DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C 118450505AZD, AND MAE EA 757-2550-16-F2044, DATED MAY 18, 2009. THIS N/R IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION. (QUESTIONABLE SDR....P.L.T.)
Part: FRAME — MISALIGNED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
EXISTING HOLES IN FRAME AT STA 418, BETWEEN S2L-S2R, INTERFERES WITH INSTALLATION, OF CABLE SHROUD MOD- AT STA 418, BETWEEN S2L-S2R, FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C 118450505AZD, AND MAE EA NR 757-2550-16-F2044, DATED MAY 18, 2009. THIS N/R IS FOR TRACKING PURPOSES ONLY. (QUESTIONABLE SDR...P.L.T.)
Part: FLOORBEAM — NONE (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
MCD FLOORBEAM T-CHORD EXISTING REPAIR AT STA 324 FROM RBL 42, RBL 58, COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001, P1. COMPLIED WITH ATTACHMENT "B" OF EO NR F-5100-7-5001, PT1. PREVIOUSLY INSTALLED REPAIR ON MCD FLOORBEAM T-CHORD AT STA 324, RBL42-RBL58, WAS REWORKED/REPLACED IAW EA NR F-5310-131514, REMOVED STIFFNERS AND SUPPORT ANGLES AS REQUIRED TO FOM IAW SRM 51-40-02, REINSTALLED STIFFNERS AND SUPPORT ANGLES IAW SRM 51-40-02. MAJOR REPAIR.
Part: FLOORBEAM — MISALIGNED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
DUE TO EXISTING FLOORBEAM REPAIR AT STA 1320, LBL 4-38, CAN NOT INSTALL MOD FITTING NR 657N3320-1 AT STA 1640, WL 208.10, LBL 24.75, A PREVIOUS REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. A NEW REPAIR WAS ACCOMPLISHED ON MAE W/C 118350521EZ2, AND EA NR 757-5365-16-F2136, REV-A, JUNE 29, 2009. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION. (QUESTIONABLE SDR....P.L.T.)
Part: INTERCOSTAL — MISALIGNED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
EXISTING INTERCOSTAL 146N5190-5, WAS PREVIOUSLY REPAIRED AND DOES NOT MATCH UP TO THE NEW FLOORBEAM AT STA 1661, RBL 10. REMOVED INTERCOSTAL, RECIEVED NEW ON MAE TRAV T9/796860, INSTALLED INTERCOSTAL AND SHEAR WEB, STA 1661, RBL 10, IAW SRM 51-40-05, 51-40-02. CATEGORY "A", MAJOR REPAIR.
Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
WHILE WORKING FLOORBEAM REPLACEMENT AT STA 1661, THE CHANNEL PN 146N5323-5, BL 0, STA 1661- 1681, WAS FOUND CORRODED. REMOVED CHANNEL, RECEIVED NEW CHANNEL PN 146N5323Y5, INSTALLED CHANNEL BL 0, STA 1661- 1681, IAW SRM 51-40-02. CATEGORY "A". MAJOR REPAIR.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
WHILE WORKING N/R N00657, 1660 FLOORBEAM REPLACEMENT. THE LOWER CHORD ON INTERCOSTAL AT STA 1640- 1660, RBL- 12, WAS FOUND TO BE CRACKED. REMOVED CRACKED LOWER CHORD, RECEIVED ON MAE TRAV NR T9/793657, INSTALLED NEW LOWER CHORD IAW SRM 51-40-05, 51-40-02, RBL- 12, STA 1660- 1681, CATEGORY "A" MAJOR REPAIR.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
SEAT TRACK FLANGE CRACKED AT LBL-45, STA 1230. REMOVED, FABRICATED NEW TRACK WITH PN 60-6549/24, AND INSTALLED SEAT TRACK LBL-45, STA 1180- 1240, IAW SRM 51-40-02, CATEGORY "A" MAJOR REPAIR.
Part: STRINGER SPLICE — DAMAGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
FITTING PN 657N3250-18, STR 7L, STA 660, IF DRILLED WILL HAVE APPROX .300 ED ON MOST AFT FASTENER COMMON TO INBD EXISTING CHORD, ZWLG CALLOUT AT THIS LOCATION STA 660, S7L, STRINGER SPLICE REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118250277DSSR06, AND MAE EA NR 757-5331-16-F2109 DATE 01 JUNE 2008, THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY.
Part: SKIN — UNKNOWN (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
APPROX STA 660, STR 6L TO 14L, EXCESSIVE CONTOUR MISMATCH. AT BS 660, S6L- S14L, NEW DSS SKIN WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118250277DSSR06, AMD MAE EA 757-5331-16-F2064, REV A, MAY 27, 2009. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.
Part: SKIN — DENTED (ZONE 100) · airframe 63,958 hrs · 20,678 cycles
DENT AT BS 1640/ 1661, S23/ 28R COMPLIED WITH EA NR F-5330-124088- CATE "B", REPAIR WITH FOLLOW UP INP AT 37, 500, F/C, THEN REPEAT EVERY 3,000 F/C, METHOD- LFEC IAW NDT MANNUAL 53-00-06, PT 6. FUSE SKIN LWR LOBE DENT REPAIR STA 1640, STR 24R. MAJOR REPAIR.
Part: SPLICE — UNKNOWN (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
DUE TO EXISTING FASTENER PITCH ON WEB AT STA 1620-1640, LBL 60. SPLICE CHANNEL (657N4308-1) CAN NOT BE LOCATED. REPLACED SPLICE CHANNEL (657N4308-1) BET STA 1620- 1640, LBL 60. ACCOMPLISHED DUE TO DISCREPANCY AFFECTING THE PTF CONVERSION ON MAE MOD W/C 118350448Z2R04, AND MAE EA 757-5361-16-F2094, REV NEW, DATED 05/27/09, THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 63,958 hrs · 20,678 cycles
STA 520 LWR FRAME INTG, SPLICE CHORD PN 657N3222-1, 4EA EXISTING FASTENER HOLES WHEN DRILLED THROUGH CHORD ARE TOO CLOSE TO RADIUS TO ALLOW PROPER INSTALLATION OF FASTENERS AT STA 520, LWR FRAME INTG, AREA STR 26L, DUE TO DISCREPANCY AFFECTING THE PTF CONVERSION, A REPAIR WAS ACCOMPLISHED ON MAE MOD W/C NR 118250068DSSR05, AND MAE EA NR 757- 5332-16-2088, REV, DATED 05/26/2009. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.
Part: FRAME — ACTIVATED (FUSELAGE) · airframe 63,958 hrs · 20,678 cycles
UPON REMOVAL OF FASTENERS FROM FRAME SPLICE 640, AT STR'S 8- 9L TO FOM. UNABLE TO INSTALL DUE TO FASTENERS, HOLES DO NOT ALIGN. AT STA 640, STR'S 8- 9L, A MAJOR ALTERATION WAS ACCOMPLISHED DUE TO THE DISCREPANCY AFFECTING THE P TO F CONVERSION, ON MAE MOD CARD 118250277DSSR06, AND MAE EA NR 757- 5332-16- F2098, REV -, DATED 06/10/2009, THIS N/R IS FOR TRACKING PURPOSES ONLY.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MCD FLOORBEAM AT STA 310, BETWEEN RBL 25 TO RBL 60, HAS CORROSION AROUND FASTENER HOLES. COMPLIED WITH EA F-5310-123995. FUSE, MAIN FRAME BS 310, RBL25 TO RBL 60, FLOORBEAM MINOR CORROSION BLEND REPAIR. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MAIN CABIN FLOORBEAM STA 720, LBL- 62, HAS AREA OF CORRODED FUSE, MAIN FRAME BS- 720 FLOORBEAM MINOR CORROSION BLEND REPAIR, COMPLIED WITH EA F-5310-123996, LBL- 62. CATEGORY "A", MAJOR REPAIR.
Part: FRAME — MISALIGNED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
STA 1640 RT, THERE ARE 5EA EXISTING FASTENERS HOLES THAT WILL INTERFERE WITH INSTALLATION OF MOD AT STA 1640, FRMAE RT SIDE , WL 200-208, REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C NR 118350400EZ2R02, AND MAE EA NR 757-5362-F2089, REV NEW, DATED 05/22/2009. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. STA 1640, S18L. CATEGORY "A" MAJOR ALTERATION.
Part: CHANNEL — DAMAGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
DUE TO EXISTING FASTENER PITCH ON WEB AT STA 1620-1640, RBL- 0, TO LBL- 60, SPLICE CHANNEL CAN NOT LOCATE AND DRILL. FABRICATED AND INSTALLED 2EA REPAIR SPLICE CHANNELS AT STA 1620- 1640, RBL-0 TO LBL, 60. IAW WORK CARD 118350448EZ2R04, AND EA NR 757-5361-16-F2094, REV, NEW. THIS NON ROUTINE IS FOR TACKING PURPOSES ONLY. CATEGORY "A", MAJOR ALTERATION.
Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
AT STA 1370 LT CREASE BEAM CORRODED REMOVED CORROSION IAW SRM 51-10-06, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL 3, REMOVED INBD LT CREASE BEAM FROM STA 1370-1390 IAW SRM 51-40-02. FABRICATED REPAIR ANGLE AND BEAM IAW SRM 51-70-11 FIG. 1 AND DWG NR 146N5590. LOCATED AND DRILLED REPAIR ANGLE AND CHORD IAW SRM 51-10-02, INSTALLED REPAIR ANGLE AND BEAM IAW SRM 51-40-02 AND 51-70-11 FIG. 1
Part: WEB — CRACKED (ZONE 100) · airframe 63,958 hrs · 20,678 cycles
AFT CARGO FLOOR SUPPORT WEB AT BS 1520 TO 1540 LBL 28-29 CRACKED AT FASTENER HOLE. REMOVED WEB, RECEIVED NEW WEB. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED WEB IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.
Part: STRAP — CORRODED (APU INTAKE) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
APU INTAKE FWD EDGE OF SURROUND, HAS HIDDEN CORROSION/APU COMPOSITE INTAKE PANEL, BULGING SKIN. CLEANED AREA FWD, AFT, UPPER AND LWR EDGE OF SURROUND APU INLET IAW SOPM 20-30-03. CORROSION FOUND ON FWD AND AFT STRAP, UPPER AND LOWER ANGLES. REMOVED CORROSION ON AFT STRAP IAW SRM 53-80-05, FIG 101, DETAIL 5; , WITHIN LIMITS IAW SRM 53-80-05, FIG 101, DETAIL 5. REMOVED CORROSION ON FWD STRAP, UPPER AND LOWER ANGLES IAW SRM 53-80-05, FIG 101, DETAIL 5; OUT OF LIMITS IAW SRM 53-80-05, FIG 101, DETAIL 5. FABRICATED ALL REPAIR PARTS, LOCATED AND DRILLED ALL REPAIR PARTS PER SRM 51-40-05. ANODIZED REPAIR PARTS IAW BAC 5019. TREATED AND PRIMED ALL REPAIR PARTS IAW SRM 51-20-01 AND AMM51-21-10-07. INSTALLED NUTPLATES, REMOVED AND REPLACED FWD STRAP AND UPPER AND LWR ANGLES AT APU INTAKE FWD EDGE IAW SRM 51-40-02.
Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
MAIN DECK CARGO TRACK IS DAMAGED & GOUGED AT BS 465 AND 475 LBL 45. BLENDED CARGO TRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-52. REMOVED CARGO TRACK IAW SRM 51-40-02. FABRICATED NEW CARGO TRACK IAW SRM 53-30-52. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED CARGO TRACK IAW SRM 51-40- 02. CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.
Part: FRAME — OUT OF ALIGNMENT (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
EXISTING FASTENER HOLES AT STA 980, BETWEEN STR 4L AND 4R WILL INTERFERE WITH THE CABLE SHROUD MOD. REPAIRED FRAME IAW SRM 53-00-07, FIG 201. FABRICATED REPAIR PARTS ON MAE TRAV NR T9/793030, T9/793031, T9/793063, AT STA 980, BETWEEN STR 4L- 4R. CATEGORY "A", MAJOR REPAIR.
Part: INTERCOSTAL — CRACKED (BS 1360-1380) · airframe 63,958 hrs · 20,678 cycles
MAIN CARGO DECK INTERCOSTAL IS CRACKED AT BS 1361, S10L. REMOVED INTERCOSTAL, IAW SRM 51-40-02. UPON FURTHER INSPECTION, VERIFIED INTERCOSTAL WAS CRACKED. FABRICATED INTERCOSTAL, LOCATED AND DRILLED IAW SRM 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MAIN DECK BS 1640 FLOORBEAM AT LBL 12, HAS AREA OF CORROSION. REMOVED CORROSION IAW SRM 53-00-51 AND FOUND OUT OF LIMITS IAW SRM 53-00-51. REMOVED FLOORBEAM AT BS 1640, LBL 65-RBL 65, IAW SRM 51-40-02. RECEIVED NEW FLOORBEAM, LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED IAW SEM 53-60-15, FIG 101, SHEET 5 AND 6 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MAIN DECK FLOORBEAM AT BS 1660, RBL 9, HAS TOOLING MARKS. REMOVED TOOLING MARKS IAW SRM 53-00-51 AND FOUND OUT OF LIMITS PER SRM 53-00-51. REMOVED FLOORBEAM IAW SRM 51-40-02. RECEIVED NEW FLOORBEAM, LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED NEW FLOORBEAM IAW SRM 53-60-51, FIG.101, SHEETS 5 & 6 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.
Part: SKIN — DAMAGED (BS 650) · airframe 63,958 hrs · 20,678 cycles
APPROX BS 650, LAP 26, BOTTOM ROW OF FASTENERS, 1 FASTENER HOLE HAS AN ELONGATED HOLE .270 INCH DIAMETER AT BS 650, LAP 26, (BS 646 / S26L), SKIN REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C NR 118250287DSSR08, AND MAE EA 757-5331-16-F2059, REV NEW, DATED 05/11/2009. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 1290-1370) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
NR 3 LT EMERGENCY EXIT DOOR LOWER SILL BS 1343, HAS 1 RUSTY NUTPLATE. REMOVED NUTPLATE, CORROSION NOTED AT LOWER SILL TEE BRACKET & CREASE BEAM AT BS 1343. REMOVED CORROSION ON CREASE BEAM, FOUND OUT OF LIMITS IAW SRM 53-60-15. REMOVED CREASE BEAM AT BS 1290-1370, LBL 59, AND RECEIVED NEW CREASE BEAM. INSTALLED NEW CREASE BEAM AT BS 1290-1370, LBL 59, IAW SRM 51-40-02. REMOVED L3 DOOR HINGE FOR ACCESS IAW SRM 51-40-02. REMOVED CORROSION ON T-BRACKET, OUT OF LIMITS IAW SRM 53-60-15. FABRICATED REPAIR DOUBLERS IAW SRM 51-70-12. INSTALLED REPAIR DOUBLERS AT BS 1343, LBL 59, IAW SRM 51-40-02 AND REINSTALLED L3 DOOR HINGE IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT 'A" MAJOR REPAIR.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
MAIN CARGO DECK SEAT TRACK HAS GOUGES FROM STA 480-510, LBL-45. REMOVED SEAT TRACK IAW SRM 51-40-02. FABED NEW SEAT TRACK MAT P/N 60-6549-24, IAW SRM 53-30-52. INSTALLED SEAT TRACK AT STA 440-680, LBL-45, IAW SRM 53-30-52, AND 51-40-02. CATEGORY "A" . MAJOR REPAIR.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MCD INT FUSE WEB ON S17R BETWEEN STA 980- 1000, HAS CORR. REMOVED WEB IAW SRM 51-40-02. RECEIVED ON TRAV T9/792531, INSTALLED NEW WEB IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.
Part: SUPPORT — CORRODED (BS 365-418) · airframe 63,958 hrs · 20,678 cycles
STA 365-418, RBL 45, SEAT TRACK SUPPORT HAS CORROSION. REMOVED SEAT TRACK SUPPORT IAW SRM 53-00-52. FABRICATED NEW SEAT TRACK SUPPORT IAW SRM 53-10-52. INSTALLED SEAT TRACK SUPPORT. REPAIR NR 3, CATEGORY "A", MAJOR REPAIR.
Part: FRAME — CRACKED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
BS 377 STR 2R FRAME CRACKED, REMOVED DAMAGED FRAME IAW SRM 51-40-02. FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-20 AND SRM 53-00-07, FIG 201. CAT."A", MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 440) · airframe 63,958 hrs · 20,678 cycles
MAIN CABIN FLOORBEAM BS 440, RBL 45-65, TOP CHORD IS CORRODED AROUND FASTENERS HOLES. REMOVED CORROSION IAW SRM 51-10-01. FOUND OUT OF LIMITS PER SRM 53-00-51, DETAIL 3. REMOVED DAMAGED SECTION IAW SRM 53-00-51. FABBED NEW TEE. FABRICATED REPAIR ANGLES AND STRAPS. LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW SRM 51-40-05 AND SRM 53-00-51, REPAIR NR 3 AT BS 440, RBL 45- 65. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,958 hrs · 20,678 cycles
MCD FLOORBEAM AT STA 365, BETWEEN RBL25 AND RBL 70, HAS CORROSION. REMOVED DAMAGE SECTION IAW SRM 53-00-51. FABRICATED NEW CHORD MAT BAC1505-100617/20. INSTALLED REPAIR PARTS AND CHORD IAW SRM 53-00-51, AT STA 365, LBL14- RBL70. REPAIR NR 3 AND CATEGORY A, MAJOR REPAIR.
Part: SUPPORT — CORRODED (BS 365-418) · airframe 63,958 hrs · 20,678 cycles
BS 365-418, RBL 24, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION. REMOVED .022 INCH MATERIAL FROM .071 INCH MATERIAL, OUT OF LIMITS IAW SRM 53-00-52, FIG 101. REMOVED SEAT TRACK SUPPORT. FABRICATED NEW SUPPORT. LOCATED AND DRILLED SUPPORT AND INSTALLED SEAT TRACK SUPPORT IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
STA 418-440, RBL24,SEAT TRACK CORRODED. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK P/N 60-6549124, IAW SRM 53-00-52. INSTALLED SEAT TRACK STA 418-440, RBL 24, IAW SRM 51-40-02. CATEGORY, A, MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,958 hrs · 20,678 cycles
STA 418- 440, RBL-45, SEAT TRACK CORRODED. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK P/N 60-6549124 IAW SRM 53-00-52. INSTALLEED SEAT TRACK STA 418-440, RBL 45, IAW SRM 51-40-02, CATEGORY A, MAJOR REPAIR.