# Boeing 727-82C - Type: Aircraft model (FAA registry) - Registry code: 1384026 - Manufacturer (registry): BOEING - Model: 727-82C - 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-727-82c 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 19940721032059I](https://openairdocs.org/incident/19940721032059I), Jul 21, 1994: Boeing 727 (N528PC), Atlanta, GA, Minor damage. Narrative: dennis m. woodlock, ryan int'l employee no. 0662, airframe and powerplant mechanic, was taxiing the airplane for repositioning from the north cargo… ## Service difficulty reports (164, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR DHL2002709004](https://openairdocs.org/sdr/DHL2002709004), Jun 26, 2002: LIGHT. INOPERATIVE. COCKPIT EMERGENCY EXIT LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY SYST, OPS CHECKED GOOD IAW B727 MM 33-50-00. - [SDR DHL2002709003](https://openairdocs.org/sdr/DHL2002709003), Jun 25, 2002: LIGHT. 1) FWD MAIN ENTRY DOOR EMERGENCY EXIT LIGHT VERY DIM.2) R/R EMERGENCY EXIT LIGHT ASSY IAW MM 33-50-00 OPS CK GOOD. - [SDR DHL2002709002](https://openairdocs.org/sdr/DHL2002709002), Jan 15, 2002: ELECTRICAL SYS. MALFUNCTIONED. APU ELECTRICAL TRIPPED OFF. A FEW SECONDS LATER, LEFT PACK TRIP OFF LIGHT ILLUMINATED AND THEN COCKPIT FILLED WITH SMOKE. RAN APU IAW MM 49-00 & JRH 8.1. APU & - [SDR DHL2002709001](https://openairdocs.org/sdr/DHL2002709001), Jan 11, 2002: WINDSHIELD WIPER. OUT OF ADJ. F/O WINDSHIELD WIPER BLADE WILL NOT RUN IN LOW. ADJUSTED F/O'S WIPER IAW 727 MM CHP 30-42-01, OPS CHECK NORMAL AT THIS TIME. - [SDR DHL2001709013](https://openairdocs.org/sdr/DHL2001709013), Sep 15, 2001: FIRE LOOP. OUT OF POSITION. NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3 GROUND FAULT. DEFERRED PER MEL 26-9 CAT-C CONTROL 7094. REPOSITIONED FIRE LOOP AND TESTED IAW 727 MM - [SDR DHL2001709012](https://openairdocs.org/sdr/DHL2001709012), Sep 11, 2001: SWITCH. MALFUNCTIONED. ON FINAL NOSE GEAR INDICATION WENT FROM DOWN AND LOCKED 3 GREEN TO UNSAFE. VISUALLY CONFIRMED GEAR DOWN AND LOCKED. ON FINAL GEAR WENT FROM UNSAFE TO DOWN AND L - [SDR DHL2001709011](https://openairdocs.org/sdr/DHL2001709011), Aug 25, 2001: FIRE LOOP. OUT OF POSITION. NR 1 ENGINE FIRE DETECTOR CIRCUIT AND LIGHT ILLUMINATED. REPOSITIONED FIRE LOOP. OPS CHECKED GOOD IAW DHL 727 MM CH 26-11-00. - [SDR DHL2001709010](https://openairdocs.org/sdr/DHL2001709010), Jul 19, 2001: FIRE LOOP. INOPERATIVE. NR 1 ENGINE FIRE DETECTION SYSTEM WILL NOT TEST NR 1 ENG FIRE WALL TEST INOP. INSTALLED OVERHAULED ENGINE SENSOR LOOP IAW WITH B-M/M 26-11-021 R&R FIRE SENSOR/R - [SDR 2001F00221](https://openairdocs.org/sdr/2001F00221), Jul 4, 2001: HYDRAULIC LINE. LEAKING. TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED - [SDR 2001F00220](https://openairdocs.org/sdr/2001F00220), Jul 4, 2001: HYDRAULIC LINE. LEAKING. TOTAL LOSS OF A SYSTEM HYDRAULICS. COMPLIED WITH EMERGENCY CHECKLIST OF HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED - [SDR 2001F00099](https://openairdocs.org/sdr/2001F00099), Jun 14, 2001: ELEMENT. MALFUNCTIONED. WHEEL WELL FIRE LIGHT ILLUMINATED 4 MINUTES AFTER TAKEOFF. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT WHEEL WELL FIRE SENS - [SDR DHL2001709009](https://openairdocs.org/sdr/DHL2001709009), Jun 14, 2001: AUTOPILOT SYS. MALFUNCTIONED. AT FL350 WITH A/P ENGAGED AND ELEVATOR IN A OR B MODE, A/P PITCHES UP AND WILL NOT HOLD ALTITUDE. (BEGINS ALTITUDE OSCILLATION AND OVER CORRECTS WITH TRIM). AUT - [SDR DHL2001709008](https://openairdocs.org/sdr/DHL2001709008), May 31, 2001: CONTROL HANDLE. BROKEN. GREEN GEAR NOSE LIGHT EXTINGUISHED AND RED GEAR LIGHT ILLUMINATED WITH GEAR LEVER DOWN. ABNORMAL PROCEDURES ACCOMPLISHED. FOUND ARM AND LINKAGE BROKEN AT APEX A - [SDR DHL2001709007](https://openairdocs.org/sdr/DHL2001709007), May 18, 2001: LIGHT. MALFUNCTIONED. LEFT GEAR WARNING LIGHT IN TRANSIT (RED) DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. ALL GEAR LIGHTS TEST ARE NORMAL. MAIN LANDING GEAR LOCK SWITCHES TESTED PER - [SDR DHL2001709006](https://openairdocs.org/sdr/DHL2001709006), May 16, 2001: LIGHT. INOPERATIVE. LT LANDING GEAR INTRANSIT UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. ALL RED LIGHTS GROUND TEST NORMAL. FOUND LT MAIN GEAR RED LIGHT - [SDR DHL2001709005](https://openairdocs.org/sdr/DHL2001709005), Apr 28, 2001: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL DOOR EMER EXIT BATTERIES WITH SERVICABLE. OPS CHECK GOOD IAW MM 33-50-01. - [SDR DHL2001709004](https://openairdocs.org/sdr/DHL2001709004), Apr 18, 2001: CONTROL UNIT. MALFUNCTIONED. ANYTIME THE AUTOPILOT ELEVATOR IS ENGAGED IN A SYSTEM MODE, THE AIRCRAFT PITCHES ERATICALLY UP AND DOWN. R / R PITCH CHANNEL CONTROL IAW MM 22-11-01. SECURITY C - [SDR DHL2001709003](https://openairdocs.org/sdr/DHL2001709003), Apr 17, 2001: AUTOPILOT SYS. MALFUNCTIONED. WITH AUTOPILOT AND ALT HOLD ENGAGED, A/C GAINS ABOUT 300 FT AN HOUR IN BOTH A & B MODE AND WITH AUX 1 NORMAL AND AUX VGS SELECTED. TRANSFERRED ITEM TO DEFERRAL- - [SDR DHL2001709002](https://openairdocs.org/sdr/DHL2001709002), Feb 20, 2001: START VALVE. MALFUNCTIONED. NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED ON TAXI-OUT. SHUT DOWN ENGINE AND CLOSED NR 3 BLEED. REMOVED AND REPLACED NR 3 ENGINE START VALVE (P/N 979254-1-1 - [SDR 20010425AP003](https://openairdocs.org/sdr/20010425AP003), Feb 18, 2001: BULB. BURNED OUT. MAIN CABIN SMOKE DETECTOR HAS 1 BACKGROUND LIGHT INOPERATIVE. REMOVED AND REPLACED ONE BACKGROUND LIGHT IN MAIN CABIN SMOKE DETECTOR INDICATOR ON FLIGHT ENGINEE - [SDR DHL2001709001](https://openairdocs.org/sdr/DHL2001709001), Feb 17, 2001: HARNESS. CHAFED. DURING TAXI-OUT, ENGINE NR 3 START VALVE OPEN LIGHT ILLUMINATED. TROUBLESHOT SYSTEM AND FOUND START VALVE LIGHT SWITCH CANNON PLUG WIRES CHAFING (BARE) AND WITH - [SDR DHL2001709064](https://openairdocs.org/sdr/DHL2001709064), Dec 28, 2000: FAIRING. MISSING. NR 8 FLAP JACKSCREW FAIRING MISSING. TRANS TO DMI 3788. - [SDR DHL2000709063](https://openairdocs.org/sdr/DHL2000709063), Oct 20, 2000: SWITCH. OUT OF ADJ. CONFIGURATION WARNING HORN SOUNDS WITH TAKEOFF POWER APPLIED. COFIGURATIONS NORMAL. ADJUSTED FLAP T/O WARNING SWITCH S 196. TESTED T/O WARNING SYS PER M/M 31-26 - [SDR DHL2000709062](https://openairdocs.org/sdr/DHL2000709062), Sep 23, 2000: CSD. FAILED. NR 1 CSD LOW OIL PRESS LIGHT ILLUM DURING TAXI. RETURNED TO BLOCKS IN TEMP 150 AND RISING. DEFERRED PER MEL 24-1 DMI NR 2496 CAT B PLACARD INSTALLED. THE CSD WA - [SDR DHL200070948D](https://openairdocs.org/sdr/DHL200070948D), Aug 21, 2000: SKIN. DENTED. RIGHT WING L/E SKIN HAS 3 DENTS OVER NR 4 L/E FLAP. REMOVED INNER SKIN FOR ACCESS PER SRM 51-30-2. REWORKED ALL 3 DENTS PER SRM 57-20-1. REINSTALLED INNER SKIN - [SDR DHL200070937C](https://openairdocs.org/sdr/DHL200070937C), Aug 13, 2000: SKIN. DAMAGED. DURING C CHECK INSPECTION, FOUND HOLE IN UPPER SURFACE OF RIGHT INBORD AFT FLAP APPROX 18 INCHES OF NR 6 AFT FLAP FAIRING. INSTALLED DOUBLER PER SRM 51-40-0. SI - [SDR DHL200070958D](https://openairdocs.org/sdr/DHL200070958D), Aug 5, 2000: SKIN. DELAMINATED. LEFT WING O/B TRAILING EDGE FLAP AFT LOWER SURFACE OLD REPAIR IS DELAMINATED. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-0. - [SDR DHL200070949D](https://openairdocs.org/sdr/DHL200070949D), Aug 1, 2000: FITTING. CRACKED. RT WING UPPER FRONT SPAR CORNER FITTING AT RBL 70.5 IS CRACKED. REMOVED UPPER FRONT FITTING PER SRM 51-30-2. INSTALLED NEW FITTING PER SRM 51-30-2. - [SDR DHL200070938C](https://openairdocs.org/sdr/DHL200070938C), Jul 31, 2000: STRUCTURE. CORRODED. DURING D CHECK INSPECTION, FOUND RT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS .050. OUT OF L - [SDR DHL200070936C](https://openairdocs.org/sdr/DHL200070936C), Jul 31, 2000: PANEL. CRACKED. DURING D CHECK INSPECTION, FOUND LT WING LOWER SURFACE PANEL NR 1 JACKSCREW FASTENER HOLE ATTACH TO UPPER FAIRING CRACKED. INSTALLED COMPOSITE REPAIR TO LEFT WI - [SDR DHL200070935C](https://openairdocs.org/sdr/DHL200070935C), Jul 31, 2000: STRUCTURE. CORRODED. DURING D CHECK INSPECTION, FOUND RIGHT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS .050. OUT O - [SDR DHL200070923C](https://openairdocs.org/sdr/DHL200070923C), Jul 23, 2000: BULKHEAD. CRACKED. AFT BULKHEAD BS 1183, BETWEEN RBL 12 TO RBL 26 DITCH PAN HAS CRACK. REMOVED DAMAGED DITCH PAN AND FABRICATED NEW PAN PER SRM 51-10-1, 51-10-2 AND 51-10-2. TREAT - [SDR DHL200070929C](https://openairdocs.org/sdr/DHL200070929C), Jul 22, 2000: BULKHEAD. CRACKED. AFT BULKHEAD FUSELAGE STA 1183 RT LOWER 20 IN FROM RT CORNER FOUND DITCH PAN CRACKED. (BETWEEN RBL 24.7 AND RBL 45.5). REMOVED PAN PER SRM 51-30-2. CLEANED AREA - [SDR DHL200070934C](https://openairdocs.org/sdr/DHL200070934C), Jul 20, 2000: COVER. WORN. NR 2 ENGINE FIREWALL REAR MOUNT LOWER SURFACE FIBERGLASS COVER WORN. REMOVED COVER AND SENT TO FIBERGLASS SHOP FOR REPAIR PER M/M 54-30-0. INSTALLED FIBERGLASS - [SDR DHL200070912C](https://openairdocs.org/sdr/DHL200070912C), Jul 19, 2000: FLOOR PANEL. CORRODED. MAIN CARGO COMPT FLOOR PANEL 1B CORRODED ON TOP AREA. REMOVED UPPER SKIN AND CORROSION FROM FLOOR PANEL PER SRM 51-10-6. MATERAL LOSS WITHIN LIMITS PER SRM 53-3 - [SDR DHL200070930C](https://openairdocs.org/sdr/DHL200070930C), Jul 19, 2000: SKIN. CRACKED. RIGHT WING I/B FLAP MID SECTION CRACK INDICATION (2) AT CUTOUT I/B EXTENSION MECHANISM. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED AT END OF CRACK PER SRM - [SDR DHL200070961D](https://openairdocs.org/sdr/DHL200070961D), Jul 18, 2000: DOOR FRAME. CRACKED. AFT CARGO DOOR UPPER FRAME IS CRACKED AT INNER BLENDING RADIOUS AT 2 LOCATIONS AT FWD AND AFT STOP FITTINGS. REMOVED FASTENERS AT INNER SKIN AND REMOVED UPPER C - [SDR DHL200070905C](https://openairdocs.org/sdr/DHL200070905C), Jul 15, 2000: COVER. BROKEN. RT WING NR 7 L/E SLAT ACTUATOR COVER BROKEN AND MISSING BOLT. REPLACED ANGLES SUPPORTS FROM ACTUATOR COVER PANEL PER SRM 51-40-4 FOR FWD ANGLE AND 51-40-3 FOR A - [SDR DHL200070936D](https://openairdocs.org/sdr/DHL200070936D), Jul 13, 2000: STRINGER. CRACKED. RT W/W STR 18A HAS CRACK AT BS 940 SEEN FROM TOP OF WING. REMOVED FASTENERS FOR ACCESS PER SRM 51-30-2. REPAIRED PER DWG DHL MIA 60-00022H. HFEC INSPECTED AREA - [SDR DHL200070935D](https://openairdocs.org/sdr/DHL200070935D), Jul 13, 2000: FITTING. CORRODED. RT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED RT MLG FWD TRUNNION AS PER SR - [SDR DHL200070928C](https://openairdocs.org/sdr/DHL200070928C), Jul 11, 2000: STRINGER. CORRODED. STRINGER 26R BETWEEN BS 360 AND 380 CORODED. REMOVED TIE FITTING PER SRM 51-30-2. REMOVED DAMAGED SECTION AND INSTALLED STRINGER REPAIRS AT STR 26R BETWEEN BS 3 - [SDR DHL200070919C](https://openairdocs.org/sdr/DHL200070919C), Jul 11, 2000: HOUSING. CRACKED. VERT STAB RT SIDE DUCT HOUSING STA 1307 APPROX HAS SEVERAL CRACKS (DUCT MATES TO VERT STAB FRONT SPAR). CUT OUT DAMAGED AREA PER SRM 51-40-2. INSTALLED EXTERNAL - [SDR DHL200070933C](https://openairdocs.org/sdr/DHL200070933C), Jul 10, 2000: PANEL. FAILED. LOWER FUS FAIRING PANEL AROUND FWD CARGO AIR OUTFLOW VALVE, FS 685 - 700, RBL 10L - 10R, PANEL HAS MANY CORROSION HOLES. REMOVED LOWER FUSELAGE FAIRING PANEL FO - [SDR DHL200070932C](https://openairdocs.org/sdr/DHL200070932C), Jul 10, 2000: FLOORBEAM. CORRODED. CORROSION ON AFT SIDE OF FLOORBEAM AT STA 1130. REMOVED SUB FLOOR AT RT SIDE FROM STA 1130 TO 1160 RBL 25 TO RBL 62 AS PER SRM 51-30-2. REMOVED CORROSION AND FO - [SDR DHL200070931C](https://openairdocs.org/sdr/DHL200070931C), Jul 10, 2000: FLOORBEAM. CORRODED. FWD RT CORNER OF FLOORBEAM AT STA 1130 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. TREATED AND PRIMED AREA PER SRM 51-6-2. FABRIC - [SDR DHL200070926C](https://openairdocs.org/sdr/DHL200070926C), Jul 10, 2000: FRAME. CORRODED. CIRCUMFERENTIAL FRAME FWD WEB CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. DID HFEC INSPECTION PER NDT M/M 51-00-00. - [SDR DHL200070913C](https://openairdocs.org/sdr/DHL200070913C), Jul 10, 2000: FLOOR SUPPORT. BENT. FLOOR SUPPORT ANGLE IS BENT AND CRACKED ON LOWER AFT CARGO COMPT STR 27R BS 1148 - 1166. REMOVED REAR SUPPORT DAMAGED ANGLE PER SRM 51-30-2. FABRICATED AND INST - [SDR DHL200070911C](https://openairdocs.org/sdr/DHL200070911C), Jul 10, 2000: ANGLE. CORRODED. CIRCUMFERENTIAL FRAME REINFORCING ANGLE CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. HFEC INSPECTED CUTOUT PER NDT M - [SDR DHL200070908C](https://openairdocs.org/sdr/DHL200070908C), Jul 10, 2000: SUPPORT BRACKET. CRACKED. NR 5 FLAP TRACK O/B AFT SUPPORT BRACKET CRACKED. REPLACED CRACKED BRACKET PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30-2. - [SDR DHL200070907C](https://openairdocs.org/sdr/DHL200070907C), Jul 10, 2000: FAIRING. CRACKED. NR 4 FLAP TRACK CANOE FAIRING, FWD L/E OF SKIN HAS CRACK IN EXISTING REPAIR. REMOVED AND REPLACED EXISTING REPAIR PER SRM 51-30-2. All 164: https://openairdocs.org/model/boeing-727-82c/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.