# Boeing 727-82 - Type: Aircraft model (FAA registry) - Registry code: 1384029 - Manufacturer (registry): BOEING - Model: 727-82 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-jet - Seats: 134 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-82 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19960705024769I](https://openairdocs.org/incident/19960705024769I), Jul 5, 1996: Boeing 72782 (N357NE), Bergamo, IT, Minor damage. Narrative: express one international, inc. (eisa), aircraft 357NE, a Boeing 727-82 departed cia (ciampino, italy) at 19:21 local time. During the post flight… ## Service difficulty reports (103, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR ASAA2016010814695](https://openairdocs.org/sdr/ASAA2016010814695), Jan 8, 2016: WARNING MESSAGE. FALSE ACTIVATION. FMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL. - [SDR ASAA2016010714700](https://openairdocs.org/sdr/ASAA2016010714700), Jan 7, 2016: FMC. MALFUNCTIONED. WHILE AT CRUISE FLIGHT, CAPTS ND SHOWED A "VTK" WITH A FAILURE OF THE MAP. BOTH CDU'S HAD NO "FMC" DISPLAYED. QRH ACCOMPLISHED. BEFORE MOVING THE FMC SELECT SWI - [SDR ASAA2016010714694](https://openairdocs.org/sdr/ASAA2016010714694), Jan 7, 2016: WARNING MESSAGE. FALSE ACTIVATION. FMC DISAGREE ON CAPT & F/O ND ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC DISAGREE NO LONGER DISPLAYED. - [SDR EISA20000154](https://openairdocs.org/sdr/EISA20000154), Sep 28, 2000: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT OVER MAIN ENTRY INOP. REMOVED AND REPLACED EXIT LIGHT IAW M/M 33-50-10. OPS CHECK GOOD. - [SDR EISA20000149](https://openairdocs.org/sdr/EISA20000149), Sep 22, 2000: INDICATOR. FALSE INDICATION. NR 3 ENGINE OIL TEMP HIGH, CAUTION BAND AT LOW POWER SETTINGS, AIR TURNBACK TO AUS. REMOVED AND REPLACED NR 3 ENGINE OIL TEMP BULB AND OIL TEMP INICATOR, RAN EN - [SDR EISA20000143](https://openairdocs.org/sdr/EISA20000143), Sep 4, 2000: FLANGE. CORRODED. SKIN ATTACH FLANGE OF FRAME AT STA 361 STR 23R CORRODED. REMOVED FLANGE, FABRICATED, LOCATED, ALODINED, PRIMED AND INSTALLED IAW B727 DRAWING 65-18420, B727 SRM - [SDR EISA20000142](https://openairdocs.org/sdr/EISA20000142), Sep 4, 2000: SPLICE. CORRODED. CORROSION ON STR 27R AT STA 360. FABRICATED STR SPLICE, LOCATED, ALODINED, PRIMED AND INSTALLED STR SPLICE IAW B727 DRAWING 65-18420, B727 SRM 51-10-2 AND 51-30 - [SDR EISA20000141](https://openairdocs.org/sdr/EISA20000141), Sep 4, 2000: SPLICE. CORRODED. STR 24R FROM STA 360 TO STA 330 HAS CORROSION. FABRICATED STR SPLICE, ALODINED, PRIMED, AND INSTALLED IAW B727 DRAWING 65-18420, B727 SRM 51-10-2, 51-30-2 AND 5 - [SDR EISA20000140](https://openairdocs.org/sdr/EISA20000140), Sep 4, 2000: FLANGE. CRACKED. ATTACH FLANGE OF FRAME CRACKED AT STA 344 STR 22R. REMOVED ATTACH FLANGE OF FRAME, FABRICATED, LOCATED, ALODINED, PRIMED AND INSTALLED FLANGE IAW B727 DRAWING 6 - [SDR EISA20000139](https://openairdocs.org/sdr/EISA20000139), Sep 4, 2000: ATTACH ANGLE. CORRODED. STA 350 STR 25R ATTACH ANGLES CORRODED. REMOVED ATTACH ANGLES, FABRICATED, ALODINED, PRIMED AND INSTALLED ATTACH ANGLES IAW B727 SRM 51-10-2, 51-30-2 AND 53-10- - [SDR EISA20000138](https://openairdocs.org/sdr/EISA20000138), Sep 4, 2000: SPLICE. CORRODED. STA 350, STR 25R EXFOLIATED APPROX 10 INCHES. FABRICATED, ALODINED, PRIMED, AND INSTALLED STR SPLICE IAW B727 DRAWING 65-18420, B727 SRM 51-10-2 AND 51-30-2. - [SDR EISA20000137](https://openairdocs.org/sdr/EISA20000137), Sep 4, 2000: DOUBLER. BULGED. SKIN EXTERIOR BULGED AND FASTENERS PULLED AT STA 345 TO STA 350. FABRICATED DOUBLER, FILLER, SHEAR TIES AND ANGLES. ALODINED, PRIMED AND INSTALLED DOUBLER, FILL - [SDR EISA20000135](https://openairdocs.org/sdr/EISA20000135), Sep 3, 2000: SWITCH. MISALIGNED. AFTER TAKEOFF, NOSE GEAR DOOR LIGHT ILLUMINATED. CYCLED GEAR, NO HELP. AIR TURNBACK TO (INT). CLEANED AND ADJUSTED NOSE LANDING GEAR DOOR SWITCH IAW M/M 32-62-1 - [SDR EISA20000134](https://openairdocs.org/sdr/EISA20000134), Sep 3, 2000: OUTFLOW VALVE. LEAKING. AFTER TAKEOFF, AIRCRAFT WILL NOT PRESSURIZE, FL 310 CABIN AT 9200 FT, DIFF PRESSURE 5.4 PSI OUTFLOW VALVE CLOSED. MANUAL PRESSURE CONTROL AT FULL INCREASE, NO H - [SDR EISA20000144](https://openairdocs.org/sdr/EISA20000144), Aug 31, 2000: SKIN. MISDRILLED. FOUND MISDRILLED HOLES ON LT SIDE 950 FITTING LT EXTERIOR FUSELAGE. FABRICATED AND INSTALLED DOUBLERS AND TRIPLERS IAW B727 SRM 51-10-2, 51-20-4, TIMCO REO W000 - [SDR 20000058](https://openairdocs.org/sdr/20000058), Jul 18, 2000: GASPER FAN. SEIZED. SMOKE IN THE COCKPIT DETECTED, UNSCHEDULED LANDING IN (LFK). GASPER FAN FOUND SEIZED UP, MEL''D CATEGORY D.07-20-2000. REMOVED AND REPLACED GASPER FAN PER M/M 2 - [SDR EISA2000004](https://openairdocs.org/sdr/EISA2000004), Jan 4, 2000: VALVE. MALFUNCTIONED. NR 2 ENGINE FUEL HEAT VALVE OPENED IN THE CLOSED POSITION, OIL TEMP WAS IN YELLOW BAND FOR 15 MINUTES. SHUT DOWN ENGINE. - [SDR CA990323018](https://openairdocs.org/sdr/CA990323018), Mar 12, 1999: SWITCH. FAILED. (CAN) LEADING EDGE POSITION ANNUNCIATOR, INDICATOR NO LIGHTS ON SLAT NR 7 WITH NR 7 EXTENDED. PILOTS LE GREEN AND AMBER INDICATION SERVICEABLE. DEFERRED FOR PAR - [SDR CA990323017](https://openairdocs.org/sdr/CA990323017), Mar 10, 1999: GCU. ARCING. (CAN) NR 1 GENERATOR'S CIRCUIT BREAKER TRIPPED, GCU RECEPTACLE ARCING. RECEPTACLE AND GCU REPLACED. - [SDR CA990330034](https://openairdocs.org/sdr/CA990330034), Mar 9, 1999: GCU. FAILED. (CAN) NR 1 GENERATOR FIELD BREAKER TRIPPED. NR 1 GENERATOR AC CONTROL BREAKER TRIPPED. ELECTRICAL FAULT PANEL ALL LIT UP. GENERATOR CONTROL UNIT REPLACED. - [SDR CA990223016](https://openairdocs.org/sdr/CA990223016), Feb 3, 1999: BRACKET. BROKEN. (CAN) INBOARD FLAPS WOULD NOT RETRACT TO LESS THAN 1.5 DEGREES. FOUND RIGHT INBOARD FLAP FAIRING FORWARD BEARING SUPPORT BRACKET BROKEN. - [SDR CA981216013](https://openairdocs.org/sdr/CA981216013), Nov 24, 1998: FRAME. DAMAGED. (CAN) SEVERAL BELT FRAMES OPPOSITE MAIN CARGO DOOR RT STA 500 TO STA 620 DAMAGED, SUSPECT DUE TO IMPROPER PALLET LOADING. PART TC: 35,055. - [SDR CA981216012](https://openairdocs.org/sdr/CA981216012), Nov 16, 1998: PANEL. CORRODED. (CAN) NOSE WHEELWELL AFT TOP PANEL/INTERIOR WEB AFT OF STA 294 TO STA 310 CORRODED. PART TC: 53,055. - [SDR CA980525002](https://openairdocs.org/sdr/CA980525002), Apr 16, 1998: HINGE. BROKEN. (CAN) MAIN CARGO DOOR UPPER AFT HINGE BROKEN AT 7 SEGMENTS, REPLACED. PART TC: 3,211. - [SDR EISA97206](https://openairdocs.org/sdr/EISA97206), Oct 8, 1997: PACKING. DETERIORATED. NOSE GEAR DOOR LIGHT ILLUMINATED ON GROUND. RE-PACKED NOSE GEAR STRUT AND SWING GEAR. OPS CHECK OK PER MM. (X) - [SDR EISA97166](https://openairdocs.org/sdr/EISA97166), Jul 22, 1997: AURAL WARN BOX. MALFUNCTIONED. AT BRU, FIRE WARNING BELL INOP. REPLACED AURAL WARNING BOX. (M) - [SDR EISA97152](https://openairdocs.org/sdr/EISA97152), Jun 22, 1997: CONNECTOR. LOOSE. NLG DOWN AND LOCK (GREEN) LIGHT INOPERABLE ON FORWARD CENTER INSTRUMENT PANEL. REMOVED AND REINSTALLED CONNECTOR AT LOCK SWITCH. (X) - [SDR EISA97119](https://openairdocs.org/sdr/EISA97119), Jun 13, 1997: SMOKE DETECTOR. CONTAMINATED. CARGO SMOKE LIGHT ON IN BOTH CLIMB AND CLIMB DESCENT. REMOVED MOISTURE WITH NITROGEN, OPS CHECK GOOD. (M) - [SDR EISA97006](https://openairdocs.org/sdr/EISA97006), Jan 23, 1997: BALL GUIDES. MISSING. AFTER TAKEOFF, FLAP RETRACTION FLAP GAUGE INDICATED SPLIT FLAP ON OUTBOARD GAUGE LESS THAN 2 DEGREES. INSTALLED JACKSCREW BALL GUIDES ON OUTBOARD TIE FLAP NR 7 - [SDR EISA96148](https://openairdocs.org/sdr/EISA96148), Sep 16, 1996: CONNECTOR. BROKEN WIRE. NR 2 ENGINE GENERATOR CSD 'IN' TEMP PEGGED HIGH. TROUBLESHOT AND FOUND BROKEN WIRE AT PIN 2 OF CONNECTOR D4392 BEHIND F/E PANEL. REPAIRED WIRE AND OPS CHECKED G - [SDR EISA96143](https://openairdocs.org/sdr/EISA96143), Aug 17, 1996: PACK VLV. INOPERATIVE. AFTER TAKEOFF EXCESSIVE RATE OF CLIMB, RIGHT PACK TEMP AT 30 DEGREES, THE RIGHT MIX VALVE STUCK IN FULL COLD. REPLACED RIGHT PACK VALVE, SYSTEM OPS CHECK GOOD. - [SDR EISA96101](https://openairdocs.org/sdr/EISA96101), Jul 4, 1996: FAIRING. MISSING. POST FLIGHT INSPECTION SHOWED, THE AFT CARGO MOVEABLE FAIRING WAS MISSING. REPLACED AFT CARGO DOOR MOVEABLE FAIRING AND RIGGED IAW MM 52-33-0. OPS CHECK GOOD. ( - [SDR EISA95388](https://openairdocs.org/sdr/EISA95388), Oct 12, 1995: BULKHEAD. CRACKED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A 2 INCH CRACK WAS FOUND AT BS 242, 1 INCH CRACK AT BS 250, 1 INCH CRACK AT BS 251 ON N.W.W LEFT PRES - [SDR EISA95332](https://openairdocs.org/sdr/EISA95332), Oct 9, 1995: SKIN. DELAMINATED. REMOVE BAD FASTENERS UPPER RIGHT AFT FUSELAGE FROM BS 1183 TO BS 1464. REMOVED, FABRICATED AND INSTALLED TWO SKIN PANELS ONE WAS 19 INCHES BY 33 INCHES, AND THE - [SDR EISA95331](https://openairdocs.org/sdr/EISA95331), Oct 9, 1995: STIFFENER. CORRODED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE HORIZONTAL ATTACH STIFFENER FOR AFT AIR STAIR OVERHEAD LIGHT AT BS 1335 IN AIR STAIR HAS CORROSION - [SDR EISA95304](https://openairdocs.org/sdr/EISA95304), Sep 29, 1995: S-DUCT. CRACKED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE S-DUCT AT RIB NR 1 STAINLESS STEEL REPAIR HAS WORKING FASTENERS, 45 EACH. DURING REMOVAL OF FASTE - [SDR EISA95334](https://openairdocs.org/sdr/EISA95334), Sep 23, 1995: HINGE FITTING. CORRODED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING NR 3 KRUGER FLAP INBOARD HINGE FITTING WAS FOUND WITH CORROSION. REMOVED AND REPLACED T - [SDR EISA95370](https://openairdocs.org/sdr/EISA95370), Sep 19, 1995: RIBS. MISMANUFACTURED. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 LEADING EDGE SLAT HAS THREE RIBS WITH LOWER SURFACE FLANGES PREVIOUSLY TRIMMED BEYOND .100 - [SDR EISA95351](https://openairdocs.org/sdr/EISA95351), Sep 19, 1995: L-ANGLE. CRACKED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT INBOARD FLAP TRAILING EDGE AFT LOWER SPAR (L-ANGLE EXTRUSION) IS CRACKED 1.5 INCHES LONG. S - [SDR EISA95292](https://openairdocs.org/sdr/EISA95292), Sep 18, 1995: RIVETS. MISSING. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT AFT EMERGENCY EXIT HATCH HAS TWO MISSING FASTENERS (RIVETS) AND TWO DRILL OFF FASTENERS ON U - [SDR EISA95335](https://openairdocs.org/sdr/EISA95335), Sep 17, 1995: SKIN. CRACKED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING LEADING EDGE WAS FOUND CRACKED ON THE INNER SKIN APPROXIMATELY WS 171.5 IN AREA OF NR 3 - [SDR EISA95374](https://openairdocs.org/sdr/EISA95374), Sep 16, 1995: FITTING. CORRODED. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, WEB SUPPORT FITTING ON RIGHT WING LEADING EDGE CAVITY CORRODED APPROXIMATELY WS 173. REMOVED WEB SUPP - [SDR EISA95369](https://openairdocs.org/sdr/EISA95369), Sep 16, 1995: BRACKET. CORROSION. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, NR 2 KRUGER FLAP AREA OF WING LEADING EDGE HAS CORROSION ON RIB ATTACH FITTING APPROXIMATELY WS 200 - [SDR EISA95362](https://openairdocs.org/sdr/EISA95362), Sep 16, 1995: SKIN. DAMAGED. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 SLAT HAS EXCESSIVE MATERIAL REMOVED FROM UPPER SKIN IN AREA OF INBOARD SLAT HOOK FORWARD M - [SDR EISA95359](https://openairdocs.org/sdr/EISA95359), Sep 14, 1995: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, HEADS GROUND OFF HI-LOCS AND EXCESSIVE MATERIAL WAS REMOVED FROM NR 3 SLAT SKIN. REMOVED FASTENERS - [SDR EISA95333](https://openairdocs.org/sdr/EISA95333), Sep 14, 1995: FRAME. BROKEN. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, TWO FRAME WEBS WERE FOUND TO BE CRACKED AND BROKEN VSS 1365.5R AND 1387.5R. REMOVED CRACKED AND BROKE - [SDR EISA95377](https://openairdocs.org/sdr/EISA95377), Sep 13, 1995: ANGLE. CORROSION. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION BEYOND LIMITS NR 2 SLAT ATTACH ANGLE IAW 51-10-6 100 PERCENT METAL REMOVAL WAS FOUND. FABRI - [SDR EISA95325](https://openairdocs.org/sdr/EISA95325), Sep 13, 1995: SPLICE PLATE. CRACKED. UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT BS 870 SPLICE PLATE BELOW 5-9 WAS FOUND CRACKED BETWEEN FASTENER HOLES. REMOVED CRACKED SPL - [SDR EISA95360](https://openairdocs.org/sdr/EISA95360), Sep 12, 1995: ACCESS PANEL. CORRODED. DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT MAIN LANDING GEAR, FORWARD TRUNNION ACCESS PANEL AROUND MOUNTING HOLES. REMOVED DAMAGED AR - [SDR EISA95324](https://openairdocs.org/sdr/EISA95324), Sep 12, 1995: FLUX VLV HARNESS. TOO SHORT. DURING F.O.M., THE LENGTHENING OF FLUX VALVE HARNESS WAS REQUIRED TO RELOCATE A BRACKET IAW B727 MM 34-21-0. (M) All 103: https://openairdocs.org/model/boeing-727-82/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.