Aircraft Report for n280fe



Registration History for n280fe





N-Number Make Model Serial Location Description Time
N280FE BOEING 767-300F 66253 MEMPHIS, TN Aircraft registered to FEDERAL EXPRESS CORP, airworthiness date 2021-10-14, expiration date 2024-10-31, serial number 66253. 2021-10-19
N280FE BOEING 727-233 22347 MEMPHIS, TN Aircraft registered to FEDERAL EXPRESS CORPORATION, airworthiness date 1991-09-05, serial number 22347. 2012-02-01
N280FE BOEING 727-233 22347 MEMPHIS, TN Aircraft registered to FEDERAL EXPRESS CORPORATION, airworthiness date 1991-09-05, expiration date 2015-02-28, serial number 22347. 2012-02-01
N280FE BOEING 767-300F 66253 RENTON, WA Aircraft registered to BOEING COMPANY, serial number 66253. 2021-06-30

Service Difficulty Reports for n280fe




















































































N-Number Make Model Serial Description Time
N280FE BOEING 767 During INSP/MAINT - FOUND LH MLG FWD DOOR STOP SHIMS TO HAVE MIGRATED. REPLACED LH MLG FWD DOOR STOP SHIMS REF 767 SRM 51-20-12 AND 51-20-11. 2022-05-03
N280FE BOEING 727233 During INSP/MAINT - CAPTAINS SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN ON PILOT'S SLIDING WINDOW IAW MM 56-12-011-5. OPS CHECK OF PILOT'S SLIDING WINDOW COMPLIED WITH IAW MM 26-12-011-5. OPS CHECK NORMAL. ACFT OK TO CONTINUE. ADJUSTED GUIDE PIN ONPILOT'S SLIDING WINDOW IAW MM 56-12-011-5. OPS CHECK OF PILOT'S SLIDING WINDOW COMPLIED WITH IAW MM 26-12-011-5. OPS CHECK NORMAL. ACFT OK TO CONTINUE. FINAL CLOSED. 2011-10-24
N280FE BOEING 727233 During INSP/MAINT - CAPTIANS SLIDING WINDOW WILL NOT CLOSE. ADJUSTED CAPT'S SLIDING WINDOW. ADJUSTMENT ROD IAW MM REF 56-12-011-5-0. OPSCHECKED GOOD. OK FOR FLIGHT. 2011-10-13
N280FE BOEING 727233 During INSP/MAINT - FWD PIT, CORROSION ON OTBD SIDE OF VERTICAL STIFFENER AT BS 740, BETWEEN STRINGERS 26L AND 25L. REMOVED AND REPLACEDDAMAGED CHORD WITH NEW PART IAW DWG 65-15940, SRM 51-30-5 AND SRM 51-30-2. 2009-05-05
N280FE BOEING 727233 During INSP/MAINT - ANGLE AT BS 740 AND STRINGER'S 27L TO 28L IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED ANGLEAND FABRICATED A NEW ONE, HEAT TREATED TO T6 CONDITION AND INSTALLED IAW SRM 53-10-1, 51-10-6, 51-30-2 AND DWG 69-43695. 2009-05-05
N280FE BOEING 727233 During INSP/MAINT - RIGHT AFT OVERWING HATCH LOWER SKIN CHAFED ON THE EDGE. BURNISHED AREA AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER USING 2024T-3 .063 PO NR 9008186 DIMS 12 INCH BY 5 INCH AND FILLER USING 2024T-3 .050 PO NR 9008452 DIMS 1 INCH BY 1 INCH AND INSTALLED REPAIR PARTS IAW SRM 52-00-2, 52-00-3, 51-10-2 AND 51-30-2. 2009-05-04
N280FE BOEING 727233 During INSP/MAINT - AFT CARGO COMPARTMENT, FUSELAGE SKIN IS CORRODED NEXT TO STRINGER 29 L AT BS 1145 FOUND CORROSION OUT OF LIMITS IAW SRM53-30-1, CUT OUT DAMAGED AREA. REMOVED PREVIOUS REPAIR AND U CHANNEL IAW SRM 51-30-2 FIG 3. CUT OUT DAMAGED AREA IAW SRM 53-30-2 FABRICATED DOUBLER REPAIR AND FILLERS IAW SRM 53-30-3 FIG 3. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-30-3 2009-04-29
N280FE BOEING 727233 During INSP/MAINT - NR 7 SLAT TRAILING EDGE CHORD IS CRACKED AT INBD UPSTOP PAD REMOVED PANEL FOR ACCESS IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA DIM 29 1/2 INCH IAW B727 SRM 51-40-4. FABRICATED REPAIR PARTS FROM BAC 1514-1559 PO NR 2903470 DIM 29 1/2 INCH AND SPLICE 11 1/2 INCH, ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4, CLOSED PANELS IAW B727 SRM 51-30-2. 2009-04-28
N280FE BOEING 727233 During INSP/MAINT - CORROSION ON SEAT TRACK STA 783-804 LBL 25. REMOVED CORROSION ON SEAT TRACK AND FOUND OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK SECTION USING BAC1506-1108 PO NR 29034128 DIMS 110 INCH BY 4 INCH AND INSTALLEDIAW SRM 51-30-2 AND DWG 65-16279. 2009-04-27
N280FE BOEING 727233 During INSP/MAINT - LEFT INBOARD MIDFLAP LOWER TRAILING EDGE CHORD CRACKED AT WBL100. CUT OUT DAMAGED AREA DIM 48 INCH, FABRICATED NEW CHORD, SPLICE ANGLE AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 57-50-2 AND 51-30-2. 2009-04-27
N280FE BOEING 727233 During INSP/MAINT - LT WING L/E CAVITY NR 1 SLAT ACT ATTACH BRACKETS HAVE BOTH INSIDE PLATES CRACKED. REMOVED 2 EA WEB AND STEEL DOUBLERS ON NR 1 SLAT ACTUATOR. BRACKETS IAW EA 7-5750-126809. FABRICATED 2 EA WEBS & STEEL DOUBLERS IAW EO 7-5750-126809 HEAT TREAT WEBS FROM "O" TO T-6 CONDITION IAW FAS ER 2-32653-801 REV A, CADMIUM PLATED STEEL DOUBLERS IAW SOPM. 20-42-05 ALODINED AND PRIMED PARTS IAW SRM 51-10-2 INSTALLED WEBS AND DOUBLERS IAW EA 7-5750-126809 2009-04-23
N280FE BOEING 727233 During INSP/MAINT - NR 5 SLAT OUTBD LOWER SURFACE IS DAMAGED ROUTED OUT EDGE IAW SRM 51-10-1. AREA FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG2. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR IAW SRM 57-50-3 FIG 1. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 57-50-3 FIG 1 CLOSED PANEL IAW SRM 51-30-2. 2009-04-22
N280FE BOEING 727233 During INSP/MAINT - MAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT OUTER FLANGE, LBL 45 STA 640-680. FABRICATED NEW SEAT TRACK SECTIONFROM BAC1520-792 PO NR 9006020 APPROX LENGTH 18 FT IAW SRM 53-10-5 FIG 1 AND 53-10-5. TREATED AND PRIMED REPAIR PARTSIAW SRM 51-10-2. INSTALLED NEW SEAT TRACK USING EXISTING GOOD CONDITION SPLICES IAW SRM 53-10-5 FIG 1, 51-30-2 AND FX 727 PF SRM 53-10-5. 2009-04-22
N280FE BOEING 727233 During INSP/MAINT - FWD PIT, FWD SIDE OF BS 720 STRINGER 28 LEFT CORRODED. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1, CUT OUT DAMAGED SECTION IAW SRM 53-10-1 FIG 1, FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW SRM 51-30-2 2009-04-22
N280FE BOEING 727233 During INSP/MAINT - FWD PIT STA 720 STRINGER 28L SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-6, AREA FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA IAW SRM 53-30-2 FIG 1, FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 53-10-2, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2009-04-22
N280FE BOEING 727233 During INSP/MAINT - NR 2 SLAT LOWER TRAILING EDGE CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD CUT OUT DAMAGED AREA DIM 25 5/8 INCH IAW SRM 51-10-1. FABRICATED ANGLE SECTION FROM BAC 1514-1559 PO NR 8307196 DIM 25 5/8 INCH AND SPLICE FROM BAC 1514-1559 PO NR 8307196 DIM 11 1/2 INCH IAW SRM 57-50-2 AND 51-40-4. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-40-4. 2009-04-21
N280FE BOEING 727233 During INSP/MAINT - FWD CARGO COMPARTMENT, CORROSION ON INTERCOSTAL AT BS 580 BETWEEN STRINGERS 28R AND 27R REMOVED INTERCOSTAL IAW B727 SRM51-30-2. REMOVED CORROSION ON SKIN IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1. FABRICATED INTERCOSTAL. CUT OUT DAMAGED AREA ON SKIN DIM 4 INCH BY 7/8 INCH IAW SRM 53-30-3. FABRICATED DOUBLER REPAIR IAW SRM 53-30-2 FIG 1 AND53-30-3 FIG 1. ALODINED AND PRIMED DOUBLER AND INTERCOSTAL IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1.INSTALLED INTERCOSTAL IAW SRM 51-30-2. 2009-04-20
N280FE BOEING 727233 During INSP/MAINT - AFT AIRSTAIR AREA - LOWER RT TORQUE BOX LIGHTNING HOLE HAS 2 STOP-DRILLED CRACKS AT BS 1243 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED 2 EA DOUBLERS IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. ALODINED AND PRIMED PARTS AND AREA IAWSRM 51-10-2. INSTALLED REPAIR DOUBLERS IAW SRM 51-40-2 2009-04-17
N280FE BOEING 727233 During INSP/MAINT - PROTRUDING DENT, EXTERIOR SKIN OF C-3 DOOR, TOP OF DOOR BETWEEN RIBS, BS 1110 CHECKED DENT LIMITS AND FOUND OUT OF LIMITS IAW SRM 52-00-2. CUT OUT DAMAGED AREA IAW SRM 52-00-3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-3 FIG 3. TREATED ANDPRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 52-00-3 AND 51-30-2. 2009-04-14
N280FE BOEING 727200 During CLIMB - S/O REPERTED HEARING A SLIGHT POP PASSING 2000FT AFTER RIGHT PACK WAS TURNED ON.NORMAL INDICATION RIGHT PACK MATCHED LEFT PACK TEMP BUT AIR MIX VALVE STAYED COLD ON RIGHT PACK.CABIN STARTED A HIGHER THAN NORMAL CLIMB 71500 FT/MIN IN MANPRESSURIZATION WITH OUTFLOW CLOSED CABIN STILL CLIMBED AT 1500 FT/MIN TRIED TO PRESSURIZE ACFT FOUND NR 2 PACK ISNOT PUTTING OUT ANY AIR OPENED SEVERAL NR 2 PACK ACCESS PANELS VERIFIED INOP RT FWD PACK VALVE. R & R SAME IAW 727-200 AMM 21-55-071-4. OPS CHECK NORMAL PERFORMED EXCESSIVE CABIN PRESSURE LEAK TEST IAW 727 -200 JRH. WITHIN LIMITS. OKTO CONTINUE. CHANGED LT FLOW CONTROL VALVE PRECAUTIONARY IAW 727-200AMM 36-12-061-4. OPS CHECK NORMAL. OK TO CONTINUE 2007-04-19
N280FE BOEING 727200 During CLIMB - NR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WINDMILLING. OIL QTY 3 GALS ENGINE FAILED WITH A LOUD BANG AND SPARKS REPORTED TRAILING AIRCRAFT BY TOWER. VISUAL INSPECTION OF ENGINE REVEALED PARTS OF COMPRESSOR BLADES IN TAIL PIPE. TURBINE WHEEL AND C1 FAN BLADES VISUALLY CK OK BUT 2,3, 4 COMPRESSOR WHEELS ARE BADLY DAMAGED. UNABLE TO TURN FAN BY HAND. WILL REQUIRE NR 2 ENGINE CHANGE. INSPECTION OFINLET DUCT SHOWS NO MISSING VORTEX GENERATORS. THIS WAS A CONTAINED FAILURE, THE ENGINE WAS REMOVED AND REPLACED. 2007-01-23
N280FE BOEING 727233 During CLIMB - ON CLIMB-OUT WHEN FLAP HANDLE WAS RAISED FROM 5 DEG TO 2 DEG, OBSERVED THE INBD FLAP GAUGE STOPPED AT 3/4 DEG. INBD FLAPS INDICATOR REMAINED AT 3-4 DEG FOR LNDG. QRH ACCOMPLISHED. INSP ALL FLAPS AND DISCOVERED LT INBD FLAP INBD JACKSCREW FAIRING END RETAINING NUT AND CAP MISSING, ALLOWING FAIRING TO SHIFT OUT OF POSITION AND LODGED BETWEEN JACKSCREW ANDFUSELAGE STOPPING FLAPS FROM FULLY RETRACTING. REPLACED CAP AND NUT REF IPC 57-30-00-46, PER MM 27-51-022. OPS CKS OK. 2006-12-21
N280FE BOEING 727200 During NOT REPORTED - MAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED TOP SIDE BS 620 LBL 10. REMOVED DAMAGED UPPER TEE IAW B 727 SRM 53-10-8 FIG. 3. FABRICATED AND INSTALLED REPAIR PARTS IAW B 727 SRM 53-10-8 FIG. 3. 2006-10-24
N280FE BOEING 727233 During NOT REPORTED - MAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED BODY STATION 680 BUTT LINE 0 RBL 55. REMOVED CORRODED FLOORBEAM TEESTA 680 IAW B727 SRM 53-10-8. 2006-10-17
N280FE BOEING 727233 During INSP/MAINT - RT WING FALSE SPAR FASTENERS LOOSE AT NR 5 FLAP TRACK ATTACH AREA REMOVED DAMAGED ANGLE AND WEB, FABRICATED NEW WEB SECTION, DOUBLER AND ANGLE SECTION WITH SPLICE ANGLES IAW DWG. SR 27-57-038 REV C. AND EA 7-5750-102761. ALL PARTS ALODINEDAND PRIMERED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW DWG SR27-57-038 REV C AND EA7-5750-102761. 2006-10-16
N280FE BOEING 727233 During INSP/MAINT - LT WING NR 4 FLAP TRACK FALSE SPAR ATTACH FITTING CRACKED AND SEVERAL FASTENERS LOOSE. FABED NEW WEB SECTION, DOUBLER, ANGLE, AND SPLICES; AND INSTALLED IAW DWG SR27-57-038 REV C AND EA 7-5750-102761, (WING SPOILER SUPPORT BEAM-REPAIR) EA ATTACHED TO SNRM N00846 OP WO 0034040. SEE SDR 06-3627. 2006-10-16
N280FE BOEING 727200 During INSP/MAINT - FLOORBEAM AT STA. 720A RBL 18-22 HAS CORROSION ON UPPER CAP. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3 THIS IS A MAJOR REPAIR. 2005-08-01
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK STA 344-480 RBL 45 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2005-08-01
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK STA 690-740 IS CORRODED LBL 24. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-22
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK LBL 45 690-740 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-22
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK LBL 45 STA 480-690 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-20
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK BL 0 STA 600-720 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-20
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK 344-480 RBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-20
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK BL 0 STA 480-600 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-20
N280FE BOEING 727200 During INSP/MAINT - SEAT TRACK RBL 45 STA 740-757 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2005-07-20
N280FE BOEING 727200 During INSP/MAINT - MAIN CARGO DOOR, DOOR HINGE LUG MINOR GOUGE REPAIR BS 616.5. COMPLIED WITH EA 7-5230-75124 DOOR - MAIN CARGO DOOR DOORHINGE LUG MINOR GOUGE REPAIR FS 616.5 AT MAE. 2004-04-06
N280FE BOEING 727200 During INSP/MAINT - LEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709. 2004-04-06
N280FE BOEING 727200 During CLIMB - MAIN CARGO DOOR LIGHT ILLUMINATED AIRBORNE. RETURNED TO DLH. LANDING OK AND PRESSURIZATION OK. FOUND SHORT IN LIGHT IN VENTRAL DOOR STAIR HANDLE AFT COMPARTMENT ON A/C. REPAIRED AS REQUIRED. OPS CHECK NORMAL. 2003-10-10
N280FE BOEING 727200 During CRUISE - LEVEL FL 190 280 KTS OCN LT TURB MAIN CARGO DOOR WARNING LIGHT ILLUMINATED STEADY THEN WENT DIM AND EXTINGUISHED AFTER 30 SEC AS WE COMPLIED WITH RED TABS. CHECKED OPERATION AND INDICATION OF MAIN CARGO DOOR, ONLY DISCREPANCY NOTED WAS INCORRECT ADJUSTMENT OF THE NR3 AND NR 5 OVERCENTER PROXIMITY SWITCHES. LATCHES ALIGNED WITH WHITE STRIPES IAW MM, DOWNSEQUENCE SWITCH WITHIN ADJUSTMENT. ADJUSTED NR 3 AND NR 5 OVERCTR. PROX SWITCHES IAW B727MM 52-34-009-5 PARA. 1 F.(1). MAIN CARGO DOOR OPERATES AND INDICATES NORMAL. 2003-09-17
N280FE BOEING 727200 During CLIMB - DURING FLAP RETRACTION L/E FLAP AMBER LIGHT REMAINED ILLUMINATED 26 S/O PANEL SHOWED 237 L/E SLAT NOT RETRACTED. REMOVED AND REPLACED BOTH RETRACT & EXTEND SWITCHES ON NR 7 SLAT ACTUATOR IAW 727-200 M/M 27-82-011-4. TESTED AS PER SAME REFER. OPS CHECKS GOOD. STOWED JUMPER IS IN S/O'S DESKTOP. 2003-08-20
N280FE BOEING 727233 During INSP/MAINT - MAIN CABIN DOOR UPPER CUTOUT SILL BEAM CRACKED AT BS 606 BETWEEN STR 2L & 3L. REMOVED AND REPLACED BEAM PER EA 7-5310-33368. 2001-09-27
N280FE BOEING 727233 During INSP/MAINT - LT WING LEAD EDGE RIB CRACKED FOR ACTUATOR ROD END CUTOUTS FOR NR 2 SLAT WS 640, WBL 540. REMOVED AND REPLACED RIBS PERSRM 57-30-4. 2001-09-26
N280FE BOEING 727233 During INSP/MAINT - CORROSION ON LT AFT TERMINAL PIN BS 870. REMOVED AND REPLACED TERMINAL PIN PER 57-41-001-4. 2001-09-26
N280FE BOEING 727233 During INSP/MAINT - RT NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTENING HOLE BS 291, WL 156, RBL 18. REMOVED AND REPLACED WEB PER SRM 51-20-1. 2001-09-25
N280FE BOEING 727233 During INSP/MAINT - CORROSION ON CARGO TRACK NR 6 AT BS 420 TO 440. REMOVED AND REPLACED TRACK PER SRM 53-10-5. 2001-09-25
N280FE BOEING 727233 During INSP/MAINT - UPPER O/B SKIN PANEL CRACKED ON NR 3 PYLON BS 1203 AT WL 240. REMOVED AND REPLACED PANEL PER SRM 51-20-1. 2001-09-25
N280FE BOEING 727233 During INSP/MAINT - RT WING NR 5 SLAT ACTUATOR ATTACH RIBS CRACKED WS 408 AND 411, WBL 320 AND 322. ROUTED OUT CRACKS PER SRM 57-50-1. 2001-09-25
N280FE BOEING 727233 During INSP/MAINT - STR 28R CRACKED AT BS 704. REMOVED AND REPLACED STR PER SRM 53-30-3. 2001-09-12
N280FE BOEING 727233 During INSP/MAINT - MAIN CABIN CARGO TRACK CRACKED AT BS 615 BL 0. REMOVED AND REPLACED TRACK PER SRM 53-10-5. 2001-09-12
N280FE BOEING 727233 During INSP/MAINT - NOSE WHEEL WELL SIDE PANEL WEB ABOVE LT FWD NLG DOOR CRACKED BS 234-236, WL 168. REMOVED AND REPLACED WEB PER SRM 51-20-1. 2001-09-12
N280FE BOEING 727233 During INSP/MAINT - RT FAIRING SUPPORT BRACKET CRACKED AT BS 720 AT STR 28R. REMOVED AND REPLACED BRACKET PER SRM 51-40-3. 2001-09-12
N280FE BOEING 727233 During INSP/MAINT - FLANGE ON RT FWD TERMINAL PIN CRACKED BS 740. REMOVED AND REPLACED PIN PER MM 57-41-001-4. 2001-09-12
N280FE BOEING 727233 During INSP/MAINT - N 1494 LH WING L/E RIB CRACKED FOR ACTUATOR ROD END CUT-OUTS FOR #2 SLAT AT WS 640, WBL 540. R&R RIBS PER SRM 57-30-4. 2001-09-10
N280FE BOEING 727233 During INSP/MAINT - N 1481 RH NOSE WHEEL WELL SHELF WEB CRACKED AT LIGHTNING HOLE BS 291, WL 156, RBL 18. R&R WEB PER SRM 51-20-1. 2001-09-10
N280FE BOEING 727233 During INSP/MAINT - N 925 UPR O/B SKIN PANEL CRACKED ON #3 PYLON BS 1203 AT WL 240. R&R PNL PER SRM 51-20-1. 2001-09-10
N280FE BOEING 727233 During INSP/MAINT - A .5 INCH CRACK AND CORROSION ON SKIN AT BS 680-720 AT STR 28R. 2001-08-30
N280FE BOEING 727233 During INSP/MAINT - N00108 DURING ROUTINE INSPECTION - DISCOVERED SUPPORT FITTING FOR NOSE LANDING GEAR DOOR ACTUATOR RODS TO BE CORRODED.S/D COMING ***** 2001-08-22
N280FE BOEING 727233 During CRUISE - DURING CRUISE SYS HYD QUANTITY READ ZERO, PRESS ZERO TOO. RED TAB PROC PUMPS TURN OFF 20 MIN. FOUND FLAP PWR UNIT HYDMOTOR LEAKING FROM TOP OF MOUNTING FLANGE AT FLAP PWR UNIT GEARBOX. REMOVED AND REPLACED FLAP HYD MOTOR IN REF TO 727-200 MM 27-51-062-4. OPS AND LEAK CK GOOD. REMOVED AND REPLACED BOTH 1 & 2 HYD CASE DRAIN FILTER PER MM 29-11-062-. OPSGOOD. 2001-03-29
N280FE BOEING 727233 During CLIMB - 00-330 UPON FLAP RETRACTION AFT T/O, NR 4 LEADING EDGE DEVICE FAILED TO RETRACT. R&R PER B727 MM 27-81-032-4. 2001-01-11
N280FE BOEING 727233 During UNKNOWN - 98-0157 STA-DAY - MASTER FIRE WARNING LIGHTS AND BELL ANNUNCIATED WITH NO OTHER INDICATIONS. WARNING SYSTEMS CHECKED OK ON ENGINE, SMOKE, AND APU, NO FAULTS. 10,000 FEET 300 KTS. COULD NOT DUPLICATE ENGINE, APU AND SMOKE DETECTION SYSTEM CHECKS GOOD ON GROUND. CLEANED AND CHECKED CONNECTION AT R421 RECTIFIER AS PRECAUTION PER WIRING DIAGRAM MANUAL 49-41-01. NO HISTORY. 1998-06-26
N280FE BOEING 727233 During CLIMB - AFTER T/O, DURING FLAP RETRACTION FROM 2 DEG TO UP, AMBER LEADING FLAPS LIGHT REMAINED ON, NR 3 SLAT AMBER LIGHT IND INTERMEDIATE POS, A-SYS HYD QTY OBSERVED AT ZERO. RED TAB CKLT ACCOMPLISHED. SAFETY WIRE BROKEN ON A FLUID S/O VALVES ANDGPWS FLAP. UNEVENTFUL LANDING AT STL, GEAR PINNED AND TOWED TO PARKING. SAFETY WIRE BROKEN ON ALT FLAP SW. ZERO QTYAND PRESS. *S/D* REMOVED AND REPLACED NR 1 AND 2 'A' SYS HYD PUMP, REMOVED AND REPLACED NR 1 AND 2 HYD PUMP CASE DRAINFILTERS, REMOVED AND REPLACED NR 3 L/E SLAT ACT, REMOVED AND REPLACED 'A' HYD RETURN FILTER ASSY. OPS AND FUNCTIONAL CHECKS NORMAL, REMOVED GEAR PINS. 1998-05-29
N280FE BOEING 727233 During INSP/MAINT - FORWARD CABIN FLOOR BEAM STA 344 HAS CORROSION BOTH TOP AND BOTTOM OF TOP FLANGE AT NUTPLATE HOLES LBL 30 - RBL 15 (MARKED TOP AND BOTTOM). REMOVED CORROSION PER MM 51-10-6. OUT OF LIMITS AT LBL 4, 12, AND 22 PER 53-10-8 FIG 9. INSTALLED SPLICE ANGLES PER FEDEX DRAWING NR SR27-53-007. 1996-10-10
N280FE BOEING 727233 During CLIMB - DURING CLIMB, ENGINEER NOTICED A-SYS HYD DECREASING, PERFORMED IMMEDIATE ACTION, A-SYS KEPT DECREASING. PERFORMED HYD LEAK CKLIST AND RETURNED TO MEM. RAN WITH FLUID SHUT-OFF VALVES CLOSED FOR 15 MINS. FOUND RIGHT O/B MOTOR SEAL BLOWN, REPLACED MOTOR AND A-SYS PRESS FILTERS, NO CONTAMINATION FOUND. A/C WILL REQ ALL HYD SYS TO BE BLEED, RESVC, AND LEAK CKA-SYS FILTERS AND O/B FLAP DRIVE MOTOR. RAN ENG, LEAK CK'D, OPS CK'D A-SYS AND FLAP DRIVE SYS. SVC A-SYS TO 5 GALLONS, OK FOR SERVICE. 1995-10-26
N280FE BOEING 727233 During INSP/MAINT - DAMAGED STR CLIP STA 520 27414 IN THE FWD CARGO BAY. REMOVED DAMAGED STR CLIP IAW FEDEX SRM 51-30-2. FABRICATED STR CLIP IAW FEDEX SRM 51-20-1. REPLACED STR CLIP IAW FEDEX 51-30-2 AND 51-10-1. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - TWO LIGHTNING STRIKES BS 220, 227 STR 24R. REPAIRED LIGHTNING STRIKES IAW FEDEX SRM 51-10-2, 51-30-2, 53-30-3 AND FEDEXMM 51-20-2 SEALED FRAYING REPAIR PER FEDEX SRM 51-20-4. INSTALLED FASTENERS PER FEDEX SRM 51-30-2 PRIMMERED PER FEDEXMM 51-20-151. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - LIGHTNING STRIKE IN SKIN AS BS 195, 199 ABOVE STR 24R, BS 261, 271 STR 24R. REPAIRED LIGHTNING STRIKES AT BS 271, STR 24R PER FEDEX SRM 53-30-3, FIG 5 AT BS 195, 199, 261 PER FEDEX SRM 53-30-3. ALODINED PRIMERED PER MM FEDEX SRM 52-20-151WET SEALED PER FEDEX SRM 51-20-4. FASTENERS INSTALLATION PER FEDEX SRM 51-30-2. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - NR 4 FLAP TRACK EMITTING RUST FROM SPOILER SUPPORT BEAM. REMOVED L/W I/B FLAP, REMOVED AND REPLACED NR 4 FLAP TRACK REINSTALLED L/W I/B FLAP AND FUNCTIONALLY TESTED ALL WORK DONE IAW FEDEX MM 27-51-1, 27-51-31, SRM 51-30-2 OHM 57-40-01. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - RT UPPER T-CHORD AT THE FRONT SPAR OF THE VERTICAL FIN FROM FIN STA 242-210 IS CRACKED. REPLACED T-CHORD AT FRONT SPARVERTICAL FIN. PER FEDEX SRM 51-10-1, 51-30-2. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - FWD ENTRY DOOR, LOWER GATE BEAM CRACKED 2 INCHES ON FWD SIDE ADJACENT TO STOP PINE FITTING 1 P/N 50-7945-238. REMOVED AND REPLACED FWD ENTRY DOOR LOWER GATE BEAM. ALL WORK DONE IAW FEDEX 51-30-2. 1994-11-07
N280FE BOEING 727233 During INSP/MAINT - DENT AND GOUGE AT BS 1273 BETWEEN STR 19R AND 20R. REPAIRED FUSELAGE SKIN AS PER FEDEX SRM 53-30-03. 1994-11-07
N280FE BOEING 727233 During CRUISE - 30 MINUTES AFTER TAKEOFF NR 3 OIL FILTER BYPASS LIGHT CAME ON. OIL PRESS WAS NORMAL AT ABOUT 45 PSI WHICH CORRESPONDEDWITH NR 1 AND 2 OIL PRESS. ALL OTHER INDICATIONNS WERE NORMAL. THE ENGINE WAS SHUTDOWN PER CHECKLIST AND CREW LANDED SAFELY. ENGINE WINDMILLED FOR APPROX 40 MINUTES. NR 3 ENGINE REMOVED AND REPLACED DUE TO METAL FOUND IN OIL FILTER. 1993-09-09
N280FE BOEING 727233 During INSP/MAINT - DAMAGED STRINGER CLIP AT STA 500, STR 27 L/H. REPLACED STRINGER CLIP REF SRM 51-20-1, 51-30-2. 1993-07-12
N280FE BOEING 727233 During CLIMB - DURING CLIMB-OUT OF MEM NR 3 LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON. RETARDED NR 3 THRUST LEVER, OIL PRESSURE ANDTEMP WERE NORMAL. ACCOMPLISHED ENGINE SHUTDOWN AND LANDED MEM WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 3ENG LOW OIL PRESSURE SWITCH. 1993-07-07
N280FE BOEING 727233 During CLIMB - AT 8000 FEET CLIMBING OUT OF MEM, THE NR 3 LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON. RETARDED THROTTLE AT IDLE, ACCOMPLISHED ENGINE SHUTDOWN CHECK LIST. RETURNED TO MEM AND LANDED UNEVENTFUL. REMOVED AND REPLACED IAW OIL PRESSURE SWITCH. OPS AND LEAK CHECK OK. 1993-07-07
N280FE BOEING 727233 During APPROACH - SJU - FLIGHT 644 - ON SHORT FINAL, FIRE BELL AND NR 3 MAIN CARGO SMOKE LIGHT CAME ON. SECOND OFFICER TURNED SMOKE CONTROL ON AND TWO MINUTES LATER LIGHT WENT OUT. MAINTENANCE COULD NOT DUPLICATE PROBLEM. NR 3 SMOKE DETECTOR CHECKS GOOD. 1992-03-16
N280FE BOEING 727233 During DESCENT - OAK - FLT 0550 - IN REFERENCE TO CREW REPORT OF SMOKE SMELL AT INITIAL DESCENT. NO EVIDENCE OF BURNED ODOR UPON ARRIVAL. INSPECTED AIRCRAFT AIR CONDITIONING SYSTEM AND ENGINE PRECOOLER VALVES. ALL OPERATE NORMALLY THIS STATION. AIRCRAFTIS SAFE FOR CONTINUED SERVICE. 1992-08-18
N280FE BOEING 727233 During CRUISE - LOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLT ABOUT 5 MIN. AFTER CLOSING ENGINE 2 RIGHT BLEED VALVE. RAN CHECKLIST AND LIGHT WENT OUT IN 30 SEC. FOUND AIR LEAK IN AFT AIRSTAIR AIR DUCT. TIGHTENED UP CLAMP AND STOPPED LEAK. GROUND CHECKS OK. 1993-09-17
N280FE BOEING 727233 During INSP/MAINT - DAMAGED STR CLIP AT STA 560, STR 27L IN THE FWD CARGO BAY. REMOVED AND REPLACED DAMAGED STR CLIP IAW FEDEX MM 51-20-7,51-10-2, 51-20-151. 1994-06-13
N280FE BOEING 727233 During INSP/MAINT - DAMAGED STR CLIP STA 520 STR 27L IN THE FWD CARGO BAY. REMOVED DAMAGED STR CLIP IAW FEDEX SRM 51-30-2, FABRICATED STR CLIP IAW FEDEX SRM 51-20-1, REPLACED STR CLIP IAW FEDEX SRM 51-30-2 AND 51-10-1. MFG P/N NR 7075-T6. 1994-06-20
N280FE BOEING 727233 During INSP/MAINT - LIGHTNING STRIKE DISCHARGE POINT BS 252, STR 24R REPAIRED LIGHTNING STRIKE AT BS 252, STR 24R PER FED EX SRM 53-30-3, ALODINED PER FED ES SRM 51-10-2, PRIMERED PER FED EX MM 51-20-151. SEALED REPAIR PER FEDEX SRM 51-20-4. FASTENERS INSTALLATION PER FEDEX SRM 51-30-2. 1994-06-27
N280FE BOEING 727233 During INSP/MAINT - STRINGER 27 L/H AT STA 500 IN THE FORWARD CARGO BAY IS GOUGED. CUTOUT DAMAGED SECTION, FABRICATED FILLER AND STRINGER SPLICE AS REQUIRED, ALODINED, PRIMERED, AND PAINTED PARTS. INSTALLED REPAIR. WORK DONE PER FEDEX SRM 51-30-2, 53-10-2,53-10-32, 51-10-2. 1994-06-27
N280FE BOEING 727233 During INSP/MAINT - DAMAGED STRINGER CLIP AT STA 580, STR 27 L/H IN THE FWD CARGO BAY. REMOVED DAMAGED STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. 1994-06-27
N280FE BOEING 727233 During INSP/MAINT - CORROSION (71C208-02) ON FRAME AT STA 720C 3 INCHES INBOARD OF STRINGER 28 R/H, WL 140 IN THE FWD CARGO BAY. CUTOUT ANDREMOVED DAMAGE, INSTALLED A DOUBLER. ALL WORK ACCOMPLISHED IAW FEDEX SRM 51-20-3, 53-10-2, 51-10-2, 51-30-2, MM 51-20-2. 1994-06-27

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Aircraft Lookup allows anyone to quickly search public datasets published by various aviation administrative services as well as marketplaces and other private aviation data providers in the United States. These datasets provide valuable insight into the history and maintenance record of any aircraft registered in the US. When you provide an N-Number above, we cross reference historical SDR, FAA, and NTSB datasets to identify any relevant records related to that N-Number.

As you may be aware, N-Numbers are not connected to an aircraft for the life of that aircraft - N-Numbers may be deregistered, and re-registered to completely different aircraft. For that reason, please confirm that the details of any search result correspond to the make and model you intended to pull records for.

SDR, FAA, and NTSB databases are provided as follows:

The Service Difficulty Reports (SDR) dataset is defined as "[t]he reports submitted by certificate holders and certificated repair stations, known as service difficulty reports (SDR's), provide the FAA with airworthiness statistical data necessary for planning, directing, controlling, and evaluating certain assigned safety-related programs." This data is, in its raw form, a tab-delimited file with encoded field headers.

The FAA Registration dataset is fairly straightforward - it is a listing of current registrations (along with addresses, aircraft serial number, and other basic metadata) at any point in time. The registration data is a comma delimited file that has named fields at the top of each file. The FAA provides historical data on their site for the previous few years.

The FAA Accident/Incident dataset covers a range of accidents and incidents that may or may not overlap with NTSB data. Typically, more significant crashes are covered by NTSB data while less significant crashes are more comprehensively covered by the FAA Accident/Incident data, which will frequently include minor events like gear-up landings and so forth. The data provided by the FAA is in a tab-delimited file with encoded field headers.

The NTSB investigation dataset is distinct from the FAA dataset. While the number of accidents or incidents they cover are less numerous, the depth at which they are covered is significantly deeper when reported by the NTSB. While each record from the NTSB contains incredible amounts of metadata related to people responsible for the flight, prevailing meteorological conditions at the time of flight, and passengers aboard, this aircraft lookup tool only provides basic summary data. The full dataset is provided as a series of Microsoft access file databases on the NTSB site.