# Boeing 727-25 - Type: Aircraft model (FAA registry) - Registry code: 1384006 - Manufacturer (registry): BOEING - Model: 727-25 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-jet - Seats: 134 - Weight class: 20,000 lb and over - Cruise speed: 435 mph - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-25 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 (10) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB BFO90IA028](https://openairdocs.org/ntsb/BFO90IA028), Feb 17, 1990: Boeing B-727-29 (N902TS), Washington, DC, incident, minor damage. Probable cause: THE ACCIDENT WAS FATIGUE FAILURE OF THE RIGHT MAIN LANDING GEAR SUPPORT LINK SHAFT BECAUSE OF OVERTORQUE. - [NTSB MIA77FA089](https://openairdocs.org/ntsb/MIA77FA089), Sep 21, 1977: Boeing 727 (N8130N), Daytona Beach, FL, no damage - [NTSB IAD71II014](https://openairdocs.org/ntsb/IAD71II014), Oct 22, 1970: Boeing 727 (N8104N), Charlotte, NC, incident, no damage - [NTSB MIA69I0072](https://openairdocs.org/ntsb/MIA69I0072), May 1, 1969: Boeing 727 (N8139N), Nashville, TN, incident, minor damage - [NTSB NYC67A0175](https://openairdocs.org/ntsb/NYC67A0175), Jun 9, 1967: Boeing 727 (N8145N), Massena, NY, no damage - [NTSB DIA67I0021](https://openairdocs.org/ntsb/DIA67I0021), Jun 2, 1967: Boeing B-727 (N8133N), Washington, DC, incident, minor damage - [NTSB NYC67A0160](https://openairdocs.org/ntsb/NYC67A0160), May 15, 1967: Boeing 727 (N8144N), Philadelphia, PA, no damage - [NTSB NYC66I0142](https://openairdocs.org/ntsb/NYC66I0142), May 20, 1966: Boeing 727 (N8145N), East Boston, MA, incident, no damage - [NTSB CHI66I0008](https://openairdocs.org/ntsb/CHI66I0008), Jul 16, 1965: Boeing 727 (N8118N), Chicago, IL, incident, minor damage - [NTSB UNK64X2587](https://openairdocs.org/ntsb/UNK64X2587), Jul 1, 1964: Boeing 727 (N8108N), W Palm Beach, FL, incident, minor damage ## FAA accident and incident reports (29) 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 19990506020269I](https://openairdocs.org/incident/19990506020269I), May 6, 1999: Boeing 727J4 (N505FE), Baltimore, MD, Minor damage. Upon landing pilot reported aircraft shook violently from nose gear area. Aircraft cleared active and called for company maintenance personnel. Found nose gear… - [Incident 19990209011869I](https://openairdocs.org/incident/19990209011869I), Feb 9, 1999: Boeing 72725 (N155FE), Minneapolis, MN. Faulty nose gear indication with gear lever in the down positiion. Recycled gear and got three gear green lights, however unsafe horn sounded when throttle was… - [Incident 19980623038199I](https://openairdocs.org/incident/19980623038199I), Jun 23, 1998: Boeing 72725 (N506FE), Indianapolis, IN. (-5) Fire bell sounded during taxi, no associated lites. Shut down #1 engine after fire dept. Noted smoke from left engine. 5 min. Later fire bell sounded with… - [Incident 19980127017169I](https://openairdocs.org/incident/19980127017169I), Jan 27, 1998: Boeing 72725 (N510FE), Richmond, VA. Contained compressor failure at cruise possibly disk. Landed number two engine out with no further incident. - [Incident 19960521021289I](https://openairdocs.org/incident/19960521021289I), May 21, 1996: Boeing 727100 (N154FE), North Platte, NE. Narrative: on may 21, 1996, approximately 1705 CDT, Boeing 727-100, N154FE, operating as fed-x flight 3438 from memphis, TN (mem), to great falls, mt (gtf),… - [Incident 19951107039689I](https://openairdocs.org/incident/19951107039689I), Nov 7, 1995: Boeing 72725 (N507FE), Wichita, KS. Buffet vibrations en route. Right yoke not level. Te flaps loose. Replaced carriage plates and bushings. - [Incident 19950525022549I](https://openairdocs.org/incident/19950525022549I), May 25, 1995: Boeing 727100 (N8104N), Des Moines, IA. Smoke in cockpit en route. Declared emergency. Diverted to dsm. Defective ballast for cockpit lights. - [Incident 19940716030949I](https://openairdocs.org/incident/19940716030949I), Jul 16, 1994: Boeing 727 (N280NE), Galena, AK, Minor damage. Cargo shifted on climbout. Minor damage to sidewalls of fuselage. Cargo strap broke. - [Incident 19930720028929I](https://openairdocs.org/incident/19930720028929I), Jul 20, 1993: Boeing 72725 (N502FE), Nashville, TN, Minor damage. Fumes in cockpit. Diverted to Nashville. Landed safely. Evacuated aircraft. First officer overhead speaker shorted. - [Incident 19921022049009I](https://openairdocs.org/incident/19921022049009I), Oct 22, 1992: Boeing 72725 (N290NE), Eugene, OR. Part of engine nacelle of 727 found beside runway. Traced to eisa. Found NR3 engine blowout panel missing from 209NE - [Incident 19920831041329I](https://openairdocs.org/incident/19920831041329I), Aug 31, 1992: Boeing 72725 (N708DH), Houston, TX, Minor damage. Right main NR3 and NR4 and left main NR1 tires blew on rollout. Brakes locked up. Replaced brake antiskid unit. - [Incident 19910409015559I](https://openairdocs.org/incident/19910409015559I), Apr 9, 1991: Boeing 72725 (N509FE), Ft Lauderdale, FL. Lost a system hydraulic fluid on climb. Dumped fuel. Returned. Found a leaking outboard trailing edge flap valve. - [Incident 19901227060969I](https://openairdocs.org/incident/19901227060969I), Dec 27, 1990: Boeing 72725 (N156FE), Syracuse, NY. Lost a system hydraulic pressure inflight. Landed safely. Fluid leaking at NR3 slat actuator. - [Incident 19891122059839I](https://openairdocs.org/incident/19891122059839I), Nov 22, 1989: Boeing 72725 (N506FE), Portland, ME. Flaps malfunctioned on approach. Made a go around. Landed safely. Replaced flap position indicator. - [Incident 19870706043789I](https://openairdocs.org/incident/19870706043789I), Jul 6, 1987: Boeing 72725 (N8141N), Kansas City, MO. Engine oil temperature higher than normal. Engine shut down. Aircraft landed safely. Suspect fuel heat valve failed - [Incident 19851120064819I](https://openairdocs.org/incident/19851120064819I), Nov 20, 1985: Boeing 72725 (N8105N), Philadelphia, PA. Loss of power on nr 1 and nr 3 engines. Diverted.engines operated normally at decreased power. Cause undetermined. - [Incident 19830209007759I](https://openairdocs.org/incident/19830209007759I), Feb 9, 1983: Boeing 72725 (N8104N), Atlantic City, NJ. All generators dropped off. Crew went to essential power. Found a failed generator and constant speed drive. - [Incident 19811120080209I](https://openairdocs.org/incident/19811120080209I), Nov 20, 1981: Boeing 72725 (N8105N), Atlanta, GA, Substantial damage. Torando hit airport, 11 aircraft and 300 passengers involved. Minor injury to one ramp person. Substantial damage. - [Incident 19810616042699I](https://openairdocs.org/incident/19810616042699I), Jun 16, 1981: Boeing 72725 (N8114N), San Antonio, TX. Hydraulic system a dropped to zero quantity. Found right flap motor case drain cracked. Replaced motor and pump. - [Incident 19801127080599I](https://openairdocs.org/incident/19801127080599I), Nov 27, 1980: Boeing 72725 (N8108N), Pittsburgh, PA. High engine temp and fire warning light after takeoff. Found a hole in the cas near a bleed duct. - [Incident 19800717060959I](https://openairdocs.org/incident/19800717060959I), Jul 17, 1980: Boeing 72725 (N8117N), Washington, DC, Minor damage. Taxiing aircraft struck wing tip of parked aircraft. - [Incident 19791212047299I](https://openairdocs.org/incident/19791212047299I), Dec 12, 1979: Boeing 72725 (N8104N), Boston, MA. Had difficulty extending nose gear. Replaced lock actuator PN77AC222 and side plates, washed, lubricated. - [Incident 19790822032179I](https://openairdocs.org/incident/19790822032179I), Aug 22, 1979: Boeing 72725 (N8139N), Atlanta, GA. Missed approach made due to turbulence. Engines were changed due to operation at red line from missed appr point. - [Incident 19790415008219I](https://openairdocs.org/incident/19790415008219I), Apr 15, 1979: Boeing 72725 (N8141N), Boston, MA. "A" system hydraulic failure due to leaking gear actuating cylinder - [Incident 19790302010409I](https://openairdocs.org/incident/19790302010409I), Mar 2, 1979: Boeing 72725 (N8141N), Houston, TX. Lost hydraulic system a due to blown flap actuator seal. Also found damage to compressor fan blades. - [Incident 19790206004549I](https://openairdocs.org/incident/19790206004549I), Feb 6, 1979: Boeing 72725 (N8104N), Pittsburgh, PA. Crew unable to control pressurization, found ruptured duct. - [Incident 19790113001829I](https://openairdocs.org/incident/19790113001829I), Jan 13, 1979: Boeing 727 (N8130N), Miami, FL, Minor damage. Aft cargo door sliding fairing separated from aircraft on landing. - [Incident 19781225020629I](https://openairdocs.org/incident/19781225020629I), Dec 25, 1978: Boeing 727 (N8133N), Pittsburgh, PA. Flight reported stuck slat. Landed ok., replaced a switch. - [Incident 19780607044909I](https://openairdocs.org/incident/19780607044909I), Jun 7, 1978: Boeing 72725 (N8111N), Boston, MA. Flight returned due to hydraulic problem. #2 hydraulic pump pressure line was leaking. ## Service difficulty reports (827, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 07FDEA01038](https://openairdocs.org/sdr/07FDEA01038), Mar 21, 2007: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT (BEAM ) HAS CORROSION FS 620, LBL 35. FABRICATED REPAIR ANGLES PER DWG SR27-53-033 AND MAE TRAVELER T7/669736 CUT OUT DAMAGED AREA IAW DWG S - [SDR 02FDEA00565](https://openairdocs.org/sdr/02FDEA00565), Aug 7, 2002: DOOR FRAME. CRACKED. AFT FRAME OF FWD CARGO DOOR CUT OUT CRACK AT THE TIP DOOR STOP FITTING BETWEEN STR 19R - 20R. REMOVED AND REPLACED ANGLE & FILLER ON AFT FRAME PER EA 7-5310-658 - [SDR 02FDEA00567](https://openairdocs.org/sdr/02FDEA00567), Aug 6, 2002: SKIN. DAMAGED. NUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 580 & 600, STR 23R TO STR 26R. - [SDR DHL2002708009](https://openairdocs.org/sdr/DHL2002708009), Jul 12, 2002: BUTTON. BROKEN. SMOKE DETECTION SYSTEM NR 2 TEST BUTTON BROKE OFF DURING TEST. REPAIRED TEST BUTTON COVER IAW BMM 20-60-01. - [SDR DHL2002708008](https://openairdocs.org/sdr/DHL2002708008), Jun 8, 2002: FIRE LOOP. OUT OF POSITION. NR 1 FIRE PROTECTION DETECTOR LIGHT ON. REPOSITIONED FIRE LOOP NR 1 ENG, OPS CHECKED GOOD IAW M/M 26-11-00. - [SDR DHL2002708007](https://openairdocs.org/sdr/DHL2002708007), Jun 5, 2002: FIRE LOOP. OUT OF POSITION. ENG NR 1 FIRE DETECTION GROUND FAULT LIGHT FLASHES IN FLIGHT. REPOSITIONED ENG NR 1 FIRE LOOP AND REMOVED AND REPLACED NR 1 GROUND FAULT LENS COVER WITH NEW LEN - [SDR DHL2002708006](https://openairdocs.org/sdr/DHL2002708006), May 14, 2002: WINDSHIELD WIPER. OUT OF ADJUST. CAPTAIN'S SIDE WINDSHIELD WIPER DOES NOT FUNCTION IN THE LOW POSITION THE WIPER DOES NOT HAVE ADEQUATE RANGE OF MOTION TO KEEP THE UPPER PORTION OF THE WINDSHIE - [SDR DHL2002708005](https://openairdocs.org/sdr/DHL2002708005), Apr 15, 2002: POWER SUPPLY. NOT SEATED. APU FIRE DETECT SYS WILL NOT TEST. RESEATED APU FIRE WARNING POWER SUPPLY. OPS GOOD IAW MM 26-15-0. - [SDR DHL2002708004](https://openairdocs.org/sdr/DHL2002708004), Mar 30, 2002: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE IN TEST. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CK NORMAL IAW B727 MM 33-50-1. - [SDR DHL2002708003](https://openairdocs.org/sdr/DHL2002708003), Mar 26, 2002: TRANSMISSION. FAILED. CAPTAIN WINDSHIELD WIPER IS INOP. REMOVED AND REPLACED WINDSHIELD WIPER TRANSMISSION IAW B-M/M 30-42-11, OPS CHECK GOOD. - [SDR DHL2002708002](https://openairdocs.org/sdr/DHL2002708002), Jan 28, 2002: LIGHT. INOPERATIVE. FWD ENTRY EMERGENCY EXIT LIGHT INOP IN TEST POSITION (ON POSITION). REMOVED AND REPLACED FWD ENTRY WAY EMERGENCY EXIT LIGHT ASSY IAW M/M 33-5-00. OPS CHECK SERV - [SDR DHL2002708001](https://openairdocs.org/sdr/DHL2002708001), Jan 27, 2002: GLARE SHIELD. OUT OF POSITION. F/O'S SLIDING WINDOW IS BINDING AGAINST GLARE SHIELD WHEN TRYING TO OPEN WINDOW. REPOSITIONED GLARE SHIELD AT F/O'S SLIDING WINDOW. OPS CHECK SERVICEABLE PER B7 - [SDR DHL2001708016](https://openairdocs.org/sdr/DHL2001708016), Dec 18, 2001: WINDSHIELD WIPER. OUT OF ADJ. F/O WINDSHIELD WIPER DOES NOT WORK ON HALF SPEED. RUNS SLOW ON 3/4 SPEED.ADJUSTED WIPER TENSION PER 727 MM CHAPTER 30-42-01, OPS CK SATISFACTORY. - [SDR DHL2001708014](https://openairdocs.org/sdr/DHL2001708014), Nov 28, 2001: FIRE LOOP. OUT OF POSITION. NR 2 ENGINE GROUND DET LIGHT ON DIM. OPENED COWLING, CLEARED FIRE LOOP FROM COWLING, CLOSED COWLING AND OP TEST NORMAL PER MM 26-00. - [SDR DHL2001708015](https://openairdocs.org/sdr/DHL2001708015), Nov 24, 2001: SKIN. CRACKED. LEFT WING INBOARD AILERON UPPER SURFACE HAS 2 CRACKS 5.5 INCHES APART. OUTBOARD CRACK APPROX 2.25 INCHES LONG, INBOARD APPROX 2 INCHES. REMOVED EXISTING I/B AIL - [SDR 01FDEA00931](https://openairdocs.org/sdr/01FDEA00931), Oct 26, 2001: HYDRAULIC SYSTEM. LEAKING. A-SYS QUANTITY DECREASING. SERVICED A-HYD SYS, NO LEAKS NOTED. OK FOR SERVICE. - [SDR DHL2001708013](https://openairdocs.org/sdr/DHL2001708013), Oct 4, 2001: FIRE LOOP. OUT OF POSITION. 1) NR 1 GROUND DETECTOR CIRCUIT ILLUMINATED IN FLIGHT.2) REPOSITIONED NR 1 ENGINE LOOP-NO FAULTS NOTED.OPS CK SATISFACTORILY PER MM 26-11-000.THIS CLEARS DMI 72 - [SDR DHL2001708012](https://openairdocs.org/sdr/DHL2001708012), Aug 30, 2001: CONTROL VALVE. FAILED. LT MAIN GEAR BRAKE DRAGGING ON TAXI OUT. TAXI BACK TO GATE PER PHONE PATCH. MX FLT CONT CVG LT MAIN BRAKE FIRE THERMAL DISCHARGED TIRE 1 TIRE 2 FIRE LAST OVER 4 - [SDR DHL2001708010](https://openairdocs.org/sdr/DHL2001708010), Jul 22, 2001: FIRE LOOP. GROUNDED. NR 1 FIRE PROTECTION DET CIRCUIT GRD LIGHT ILLUMINATED IN FLT. FOUND ON ENG NR 1 FIRE PROTECTION LOOP WAS GROUNDING ON ENGINE COWLING, REPOSITIONED LOOP IAW B72 - [SDR DHL2001708009](https://openairdocs.org/sdr/DHL2001708009), Jul 21, 2001: FIRE LOOP. OUT OF POSITION. ENGINE NR 1 DETECTOR CIRCUIT GRD WAS ILLUMINATED ON TAXI OUT FROM MCO. FOUND NR 1 ENG LOOP TOUCHING A BRACKET. REPOSITIONED LOOP. SYS NOW OPS CHECK NORMAL PER M - [SDR DHL2001708008](https://openairdocs.org/sdr/DHL2001708008), Jul 7, 2001: ACTUATOR. IN WINGS LEVEL DESCENT @ 280 KNOTS IAS SPEED BRAKE DEPLOYMENT CAUSES AIRCRAFT TO ROLL TO THE RIGHT. STOWING SPEED BRAKE CAUSES AIRCRAFT TO ROLL ABRUPTLY LEFT 15 - [SDR DHL2001708007](https://openairdocs.org/sdr/DHL2001708007), Jul 6, 2001: CONTROLLER. MALFUNCTIONED. WHEN DEPLOYING FLIGHT SPOILERS AIRCRAFT ROLLS RT, WHEN STOWING FLIGHT SPOILERS AIRCRAFT ROLLS ABRUPTLY TO THE RT. INSPECTED ALL SPOILERS FOR DELAM, NONE NOTED. - [SDR DHL2001708006](https://openairdocs.org/sdr/DHL2001708006), Jun 21, 2001: COMPUTER. FAULTY. DURING CRUISE FLT ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. ELEVATOR FEEL DIFF PRESSURE LIGHT STAYED ILLUMINATED. REPLACED EL - [SDR DHL2001708005](https://openairdocs.org/sdr/DHL2001708005), Jun 21, 2001: RECEIVER. UNSERVICEABLE. RADAR PAINTS GROUND CLUTTER AT 6 DEG TILT UP, WHEN TURNING PAINTS GROUND.CORRECTIVE ACTION - R&R RADAR RT PER M/M 34-41-01 OPS CK NORMAL. STATUS-CLOSED. - [SDR DHL2001708003](https://openairdocs.org/sdr/DHL2001708003), May 23, 2001: STUD. MISSING. PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL. SHUTDOWN WHEN OIL PRESSURE STARTED TO DECREASE. ENGINE OIL PRESS/TEMP GOOD UNTIL TOUCHDOWN. PERFORMED ABNORMAL - [SDR DHL2001708004](https://openairdocs.org/sdr/DHL2001708004), May 18, 2001: ENGINE. UNSERVICEABLE. REMOVED AND REPLACED ENG FOR EXCESSIVE OIL CONSUMPTION. REF W/O 600003170. REMOVED NR 1 ENG AND REPLACED PER DHL 727 TASK MANUAL MANUAL 71-01-03 THRU 71-01-18. - [SDR DHL2001708002](https://openairdocs.org/sdr/DHL2001708002), Mar 16, 2001: GEARBOX. LEAKING. NR 1 ENGINE LOST OIL QUANTITY AND PRESSURE IN FLIGHT. COMMENCED ENGINE SHUTDOWN AT INDICATION OF LOW OIL PRESSURE. T/S SYSTEM. REMOVED AND REPLACED N2 GEARBOX I - [SDR 01FDEA00106](https://openairdocs.org/sdr/01FDEA00106), Feb 10, 2001: LIGHT. INOPERATIVE. NR 3 ENG REVERSER LIGHT ILLUM. REMOVED AND REPLACED REVERSER ACTUATOR COVERS. NEED SOCKET MPN 04-1011-003. ALL CKS GOOD. ALL PNLS REINSTALLED. AC OK FOR SERVICE - [SDR DHL2001708001](https://openairdocs.org/sdr/DHL2001708001), Jan 11, 2001: ALTIMETER. UNSERVICEABLE. ALTIMETER SPLIT BETWEEN CAPT AND F/O'S POSITION BY 70 FEET.INSTALLED SERVO-PNUMATIC ALTIMITER IN CAPTS POSITION PER M/M 34-11-0,OPS CHK GOOD. - [SDR DHL2000708027](https://openairdocs.org/sdr/DHL2000708027), Dec 21, 2000: SENSOR. DAMAGED. AFTER T/O NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED,ABNORMAL PROCEDURES COMPLIED WITH. PLACED NR 3 ENGINE MODULATING VALVE ON DEFERRAL PER DHL MEL 36-11, DMI 36 - [SDR 00FDEA00888](https://openairdocs.org/sdr/00FDEA00888), Dec 19, 2000: SWITCH. FAILED. 00-367 LEFT MAIN GEAR IND UNSAFE LEFT MAIN GEAR DOOR CAME ON AND WENT OUT. R&R LH MLG DOWN LOCK POSITION SWITCH PER MM 32-61-21. OPS CK PER MM 32-61-21. - [SDR CA001122010](https://openairdocs.org/sdr/CA001122010), Nov 9, 2000: RESTRICTOR VALVE. FAILED. (CAN) ON DESCENT INTO YEG THE NR 1 ENGINE OIL PRESSURE BEGAN FLUCTUATING BETWEEN 0-35 PSI. IMMEDIATELY FOLLOWING THIS INDICATION THE LOW OIL PRESSURE BYPASS LIG - [SDR CA001019010](https://openairdocs.org/sdr/CA001019010), Sep 21, 2000: RIB. CRACKED. (CAN) DURING A ROUTINE A CHECK IT WAS NOTICED THAT THE NR 8 SLAT ACTUATOR MOUNT WAS CRACKED AT THE ROD END ATTACH POINT. SLAT WAS REMOVED AND MOUNT BRACKETS AND - [SDR DHL200070806C](https://openairdocs.org/sdr/DHL200070806C), Sep 20, 2000: PANEL. CRACKED. VERT STAB RT LWR SLIDING SEAL TRACK AREA LWR FIX PANEL HAS 2 CRACKS. REMOVED AND REPLACED PANEL PER SRM 55-30-2. ALODINED AND PRIMED PER SRM 51-10-2. - [SDR DHL200070812C](https://openairdocs.org/sdr/DHL200070812C), Sep 14, 2000: PANEL. CRACKED. PANEL NR 3429 I/B LARGE PANEL RADIOUS CORNER CRACK PROGRESSIVE BEYOND STOP DRILL HOLE. CUT OUT DAMAGED AREA AT PANEL PER SRM 51-40-1. INSTALLED DOUBLER REPAIR P - [SDR DHL2000708020](https://openairdocs.org/sdr/DHL2000708020), Sep 14, 2000: PANEL. CRACKED. PANEL 5512 MOUNT HOLE CRACK. REPLACED PANEL 12 X 25 INCH PER SRM 51-30-2. - [SDR DHL200070809C](https://openairdocs.org/sdr/DHL200070809C), Sep 13, 2000: FLANGE. CRACKED. NR 9 L/E SLAT I/B TRACK O/B MOUNT AFT FLANGE IS CRACKED. ROUTED OUT CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-3. TREATED AND PRIMED PER SRM - [SDR DHL2000708012](https://openairdocs.org/sdr/DHL2000708012), Sep 13, 2000: STRUCTURE. DAMAGED. OUTBOARD FLAP T/E HONEYCOMB DETERIORATING. REPAIRED PER SRM 51-40-1. SIZE OF REPAIR 10 X 3 INCH. - [SDR DHL2000708005](https://openairdocs.org/sdr/DHL2000708005), Sep 13, 2000: RIB. CRACKED. LEFT WING LEADING EDGE SLAT RIB AFT FLANGE IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-50-3. SIZE OF REPAIR 8 X 2 INCH. - [SDR DHL200070802C](https://openairdocs.org/sdr/DHL200070802C), Sep 12, 2000: STRINGER. CORRODED. EVIDENCE OF CORROSION AT S 23R BETWEEN BS 480 AND 500. REMOVED FASTENERS AND CUT OUT SECTION OF STR 23RT BETWEEN STA 480 AND 500 PER SRM 53-10-3. INSTALLED STR - [SDR DHL200070808C](https://openairdocs.org/sdr/DHL200070808C), Sep 11, 2000: RIB. CRACKED. RT WING NR 4 6 L/E SLAT O/B TRACK I/B MOUNT RIB AFT FLANGE IS CRACKED AT HORIZ NUT PLATE STRAP UPPER ANGLE. REMOVED FASTENERS AT NR 6 SLAT O/B TRACK I/B RIB PER - [SDR DHL200070807C](https://openairdocs.org/sdr/DHL200070807C), Sep 11, 2000: FITTING. DAMAGED. FWD CARGO COMPT RT SIDE BS 480 STATIC PORT FITTINGS PROTECTOR PANEL HAS BROKEN LUG AND MISSING FASTENER. INSTALLED NEW COVER PROTECTOR PER SRM 53-10-2. ALODINED - [SDR DHL200070805C](https://openairdocs.org/sdr/DHL200070805C), Sep 11, 2000: STRINGER CLIP. CORRODED. FWD BAGGAGE COMPT S-20L AT BS 500 WHERE CLIP ATTACHED TO STRINGER HAS A PIN HOLE AND SUSPECTED CORROSION. CUT OUT DAMAGED AREA PER SRM 53-10-3. TREATED AND PRIM - [SDR DHL2000708024](https://openairdocs.org/sdr/DHL2000708024), Sep 11, 2000: LATCH. CRACKED. FWD CARGO DOOR UP LOCK LATCH BRACKET LATCH CRACK. REPLACED LATCH PER SRM 51-10-2. MATERIAL USED 10 X 20 INCH. - [SDR DHL2000708021](https://openairdocs.org/sdr/DHL2000708021), Sep 11, 2000: ANGLE. SHEARED. SKIN BULGING, FASTENERS SHEARED ANGLE CORRODED AT TAIL SKID RIGHT SIDE STATION 1203. REPAIR PER B727 SRM 51-40-3, 51-30-2, 53-30-2. SIZE OF REPAIR 20 X 10 INCH. - [SDR DHL2000708006](https://openairdocs.org/sdr/DHL2000708006), Sep 11, 2000: WEB. CRACKED. STA 294.5 STR 15L HORIZONTAL WEB HAS CRACK GOING BEYOND STOP DRILL. REPLACED HORIZONTAL WEB PER SRM 53-10-1. - [SDR DHL2000708019](https://openairdocs.org/sdr/DHL2000708019), Sep 9, 2000: PRESSURE PANEL. CRACKED. NOSE WHEEL WELL CEILING WEB PANEL SHOW CRACKS RUNNING FROM BS 268.5 AND LBL 20. INSTALLED 13 X 19 INCH DOUBLER PER B727 SRM 51-30-2. - [SDR DHL2000708007](https://openairdocs.org/sdr/DHL2000708007), Sep 9, 2000: ANGLE. CRACKED. FUSELAGE LOWER EXTERIOR BS 610 RT SIDE FAIRING PANEL ANGLE SUPPORT SHOWS CRACKS. INSTALL ANGLE SUPPORT. SIZE OF REPAIR 35 X 1 X 4 INCH. - [SDR DHL200070813C](https://openairdocs.org/sdr/DHL200070813C), Sep 8, 2000: WEB. CRACKED. MCD INTERNAL UPPER ROW OF LIGHTENING HOLES LOWER ROW NR 11 HOLE HAS A CRACK. TRIMMED OUT CRACK PER SRM 51-40-2. INSTALLED DOUBLER PER SRM 51-40-2. ALODINED AND - [SDR DHL200070810C](https://openairdocs.org/sdr/DHL200070810C), Sep 8, 2000: ANGLE. CRACKED. MAIN CARGO DOOR FWD EDGE LWR SECTION, SMALL SECTION OF LINING CRACKED. INSTALLED NEW ATTCH ANGLE AT MCD FWD EDGE LWR SECTION PER SRM 51-10-1. TREATED AND PRIMED All 827: https://openairdocs.org/model/boeing-727-25/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.