# Boeing 727-2J0 - Type: Aircraft model (FAA registry) - Registry code: 1384045 - Manufacturer (registry): BOEING - Model: 727-2J0 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 · Turbo-jet - Seats: 170 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-727-2j0 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 (1) 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 ATL00LA072](https://openairdocs.org/ntsb/ATL00LA072), Jul 28, 2000: Boeing 727-200 (N364PA), Charleston, SC, minor damage. Probable cause: The pilot's inadequate evaluation of weather information, and his delay in taking remedial action that resulted in the in-flight encounter with severe weather. ## FAA accident and incident reports (8) 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 20040426006049I](https://openairdocs.org/incident/20040426006049I), Apr 26, 2004: Boeing 7272J0 (N281KH), San Francisco, CA. (-23) Crew declared an emergency due to statement entered into logpage 4169-37, with airspeed changes, aircraft yaw changes noticeably. After rudder is… - [Incident 20040117010689I](https://openairdocs.org/incident/20040117010689I), Jan 17, 2004: Boeing 7272J0 (N364PA), Kinston, NC. (-23) On January 17, 2004 on a routine flight from bos to cancun mex at 31000, flight 8510 with 149 passengers and 8 crew members had a forward cargo… - [Incident 20010320004809I](https://openairdocs.org/incident/20010320004809I), Mar 20, 2001: Boeing 7272J0 (N364PA), Belleville, IL, Minor damage. (-23) Upon departure from blv, during landing gear retraction, the crew heard a loud clunk and the nose gear would not fully retract. The gear was extended and… - [Incident 20001122021539I](https://openairdocs.org/incident/20001122021539I), Nov 22, 2000: Boeing 7272J0 (N364PA), Pittsburgh, PA, Minor damage. (-23) On November 22, 2000, a B-727, s/n 21107, registered as N364PA, and operated as "riva" flight #63, landed at "pit" after reporting an anti-skid problem… - [Accident 20000728008539A](https://openairdocs.org/incident/20000728008539A), Jul 28, 2000: Boeing 7272J0 (N364PA), Charleston, SC, No damage. (-23) Pan am flight 164 departed sanford (sfr), FL, at 2053Z destined for pittsburg (pit), PA. While maneuvering between cells 60 miles south fo the cae… - [Incident 20000502019559I](https://openairdocs.org/incident/20000502019559I), May 2, 2000: Boeing 7272J0 (N364PA), Pittsburgh, PA. (-23)While enroute from portsmouth, ma to Pittsburgh, PA over albany, PA, the #3 starter valve light illuminated. The power reduced and the light went out.… - [Incident 19870608046289I](https://openairdocs.org/incident/19870608046289I), Jun 8, 1987: Boeing 727221 (N364PA), New York, NY. The NR1 leading edge flap failed to extend properly. A safe landing was made. Flap actuator was replaced. - [Incident 19840201032219I](https://openairdocs.org/incident/19840201032219I), Feb 1, 1984: Boeing 7272D4 (N362PA), Newark, NJ, Minor damage. Fire warning on gear retraction. Bottles discharged. Possible compressor failure. Crusted ice and snow on airplane. ## Service difficulty reports (220, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR DHLA200800088](https://openairdocs.org/sdr/DHLA200800088), Aug 15, 2008: ENGINE. MALFUNCTIONED. REJECTED TAKEOFF, ENG NR 3 WAS 1.88 EPR WITH BUG OF 2.05. GROSS WEIGHT 173.4, AIR SPEED 70 KTS, PRESS ALTITUDE 2360FT, AIR TEMP 39C. TRIMMED ENG TO CORRECT PP A - [SDR DHL2008F00006](https://openairdocs.org/sdr/DHL2008F00006), Jun 27, 2008: FAIRING. CRACKED. POSSIBLE CRACK AT LOWER AFT SIDE OF NR 8 FLAP TRACK FAIRING. REMOVED AND REPLACED FLAP TRACK FAIRING IAW BOEING 727 MM 27-51-31. OPERATIONAL CHECK OK. (A) - [SDR DHL2008F00005](https://openairdocs.org/sdr/DHL2008F00005), Jun 27, 2008: STRUCTURE. CRACKED. POSSIBLE CRACK ON NR 1 K-FLAP AT BOTTOM INBOARD CORNER. STOP DRILLED CRACK AND FABRICATED DOUBLER FROM 2024-TS 2,375 Z 2,375 X .062 (PO 4-6686) TREATED, PRIMED - [SDR DHL2008749012](https://openairdocs.org/sdr/DHL2008749012), Feb 4, 2008: STRINGER. CRACKED. AFT PIT STRINGER 29L CRACKED AT SPLICE AFT OF BS 950. REMOVED AFT PIT STRINGER 29L, LOCATED AND DRILLED NEW STRINGER. INSTALLED NEW STRINGER IAW SB 727-53-0179. - [SDR DHL2008749011](https://openairdocs.org/sdr/DHL2008749011), Feb 2, 2008: SKIN. MISREPAIRED. NR 2 ENGINE INLET COWL LEADING EDGE PREVIOUS REPAIR AT BS 1089 WL 314 AT 9 O'CLOCK POSITION DOES NOT CONFORM TO AERODYNAMIC SMOOTHNESS REQUIRED FOR CRITICAL ARE - [SDR DHL2008749010](https://openairdocs.org/sdr/DHL2008749010), Jan 31, 2008: HINGE. GOUGED. MAIN CARGO DOOR UPPER AFT MOST HINGE IS GOUGED IN CENTER OF HINGE BS 640. REMOVED DAMAGE IAW AEI MM CHAPTER 52. LOCATED AND DRILLED IAW AEI MM CHAPTER 52 FIG 52 - [SDR DHL2008749016](https://openairdocs.org/sdr/DHL2008749016), Jan 25, 2008: NOSE COWL. CRACKED. DURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE IS BENT OUT AND 1" CRACK. CUT OUT DAMAGE AREA DIMENSION 2" BY .75" IAW SRM - [SDR DHL2008749021](https://openairdocs.org/sdr/DHL2008749021), Jan 21, 2008: STRINGER. CORRODED. DURING C CHECK, CORROSION NOTED ON STRINGER 27R REPAIR CHANNEL, BS 560 TO BS 573. REMOVED FASTENERS IAW SRM 51-30-2. REMOVED CHANNEL IAW SRM 51-30-2. FABRICATED - [SDR DHL2008749014](https://openairdocs.org/sdr/DHL2008749014), Jan 20, 2008: TAB. DENTED. DURING C CHECK, LT WING OUTBOARD AILERON CONTROL TAB HAS A DENT WBL 592 TOP SURFACE. DENTED AREA FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 4, CUT OUT DENTED AREA - [SDR DHL2008749020](https://openairdocs.org/sdr/DHL2008749020), Jan 18, 2008: SHEAR TIE. CORRODED. DURING C CHECK, FRAME SHEAR TIE CORRODED AT BS 720C BETWEEN STRINGERS 28L AND 28R. FOUND CORROSION ON SHEAR TIE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED - [SDR DHL2008749001](https://openairdocs.org/sdr/DHL2008749001), Jan 10, 2008: STRINGER. CORRODED. FORWARD CARGO COMPARTMENT CORROSION ON STRINGER SPLICE, STRINGER 28R BETWEEN BS 680 FRAME. FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 ON UPPER - [SDR GAIA06027OP](https://openairdocs.org/sdr/GAIA06027OP), Aug 25, 2006: SHUTOFF VALVE. CLOSED. DURING CLIMB THE NR 2 ENGINE OIL FILTER BYPASS/LOW PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE TEMPERATURE AND QUANTITY WERE NORMAL. THE NR 2 ENGINE FLAMED OUT - [SDR GAIA05037OP](https://openairdocs.org/sdr/GAIA05037OP), Dec 15, 2005: DOWNLOCK SWITCH. INOPERATIVE. DURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DO - [SDR GAIA05035OP](https://openairdocs.org/sdr/GAIA05035OP), Dec 6, 2005: CONNECTOR. DIRTY. DURING APPROACH, INITIAL GEAR EXTENSIO, NOSE GEAR INDICATOR (NOT SAFE), AFTER RECYCLE AND A SHORT DELAY INDICATION NORMAL. LANDING WAS MADE WITHOUT INCIDENT. CL - [SDR DHL2005749021](https://openairdocs.org/sdr/DHL2005749021), Nov 2, 2005: STRINGER. CORRODED. FWD CARGO PIT BILGE AREA STRINGER 27R CORRODED AT BS 720F +14 MARKED. REMOVED BEACON ANTENNA AND CONTROL AIR DUCT AT BS 720F + 14 AND STR 27R IAW B727 SRM 51-30 - [SDR DHL2005749017](https://openairdocs.org/sdr/DHL2005749017), Nov 2, 2005: ROD. CRACKED. NR 3 SLAT WS 515 AT ACT ROD END ATTACH HAS IB FRAMES CRACKED IN AFT RADIUS. REMOVED AND REPLACED DAMAGED IB RIB PN 65-17294-14 PO NR 540053 ON NR 3 SLAT IAW 727 - [SDR DHL2005749016](https://openairdocs.org/sdr/DHL2005749016), Nov 2, 2005: BRACKET. CRACKED. LT WING NR 2 SLAT ACT MOUNT BRACKET IB SIDE HAS INSIDE PLATE CRACKED. REMOVED FABBED NEW AND INSTALLED NR 2 SLAT ACT I/B MOUNT BRACKET MAT USED BAC 1503-10045 P - [SDR DHL2005749015](https://openairdocs.org/sdr/DHL2005749015), Nov 2, 2005: FRAME. DENTED. FRAME AT STA 970 ABOVE STR 26 LT IS DENTED M/R. CUT OUT DAMAGED AREA 7/8" BY 2 3/4" AND FABBED REPAIR ANGLE FROM 7075 T6 .063 PO 9002351 DIM 4" BY 10 7/8" IAW B - [SDR DHL2005749014](https://openairdocs.org/sdr/DHL2005749014), Nov 2, 2005: WEB. CRACKED. FOUND WEB BETWEEN STA 950E AND 950 D ABOVE STR 26 LEFT IS CRACKED M/R. REMOVED WEB FOR FAB NEW AT STA 950E TO 950D STR 26 LT IAW B727 SRM 51-30-2. FAB`D NEW PAR - [SDR GAIA05029OP](https://openairdocs.org/sdr/GAIA05029OP), Nov 2, 2005: LIGHT. INOPERATIVE. DURING A-CHECK FOUND L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AT L1 DOOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) - [SDR DHL2005749012](https://openairdocs.org/sdr/DHL2005749012), Nov 1, 2005: FRAME. DENTED. FOUND DENT ON FRAME AT BS 500 ABOVE STR 24R. CUT OUT DAMAGED AREA 4 1/8" BY 1 1/8" FROM FRAME ON BS 500 ABOVE STR 24R IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR DOU - [SDR DHL2005749011](https://openairdocs.org/sdr/DHL2005749011), Nov 1, 2005: TORQUE BOX. CRACKED. UPPER TORQUE BOX CRACKED ON LWR FWD RT CORNER BS 1303 WEB (ACCESS THRU VERT STAB PANL 9504). STOP DRILLED 1/2" LONG CRACK ON BS 1303 FRAME WEB AT RBL 22.00 FWD - [SDR DHL2005749010](https://openairdocs.org/sdr/DHL2005749010), Oct 31, 2005: COWLING. DENTED. NR 3 ENG NOSE COWL L/E RING AT 12 O'CLOCK POSITION HAS 2 EA DENTED AREAS. CUT OUT DAMAGED AREA SIZE 5 1/4 INCHES X 5 3/4 INCHES ON NR 3 ENG NOSE COWL L/E RING A - [SDR DHL2005749009](https://openairdocs.org/sdr/DHL2005749009), Oct 31, 2005: SKIN. DENTED. FOUND LT WING I/B AFT FLAP DENTED AT LWR SURFACE. CUT OUT DENTED AREA APPROX 3 INCHES. DIA AT LT INB AFT FLAP LWR SURFACE FABBED FILLER APPROX 3" DIA AND DOUBLE - [SDR DHL2005749008](https://openairdocs.org/sdr/DHL2005749008), Oct 31, 2005: SKIN. DENTED. FOUND DENT RT SIDE FUSELAGE SKIN STA 1263 ABOVE STR 19 R (MARKED). CUT OUT DAMAGED AREA DIM 5" BY 3 1/2 AND FABBED REPAIR DOUBLER FROM MATERIAL USE 2024T3 063 P - [SDR DHL2005749007](https://openairdocs.org/sdr/DHL2005749007), Oct 31, 2005: SKIN. DENTED. FOUND DENT RT SIDE FUSELAGE SKIN STA 1095 ABOVE STR 19R. DENT TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 2" BY 1". FABRICATED REPAIR D - [SDR DHL2005749006](https://openairdocs.org/sdr/DHL2005749006), Oct 31, 2005: SKIN. DENTED. FOUND DENT RT SIDE FUSELAGE SKIN STA 1045 ABOVE STR 20R (MARKED). DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM .750 FABRICATED - [SDR DHL2005749005](https://openairdocs.org/sdr/DHL2005749005), Oct 31, 2005: SKIN. DENTED. FOUND DENT RT SIDE FUSELAGE SKIN STA 1001 BELOW STR 25R. EVALUATED DENT AND FOUND OUT OF LIMITS AND IS LESS THAN 10" FROM A CUTOUT OR SPLICE MINIMUM DISTANCE IS - [SDR DHL2005749004](https://openairdocs.org/sdr/DHL2005749004), Oct 30, 2005: SKIN. DENTED. FOUND LEFT ELEVATOR LOWER SURFACE DENTED 40" I/B FROM O/B TIP. REMOVED LT ELEVATOR LOWER SKIN PANEL AT ELEV STA 173.21 IAW B727 SRM 51-30-2 FIG 9 LOCATED AND DR - [SDR DHL2005749003](https://openairdocs.org/sdr/DHL2005749003), Oct 30, 2005: HINGE. CRACKED. FOUND NR 1 SPOILER 2ND HINGE CUTOUT HAS 1" CRACK. STOP DRILLED CRACK IAW 727 SRM 51-10-1. VERIFIED CRACK TERMINATION IN STOP DRILL HOLE IAW B727 NDT PT 6 51-00- - [SDR DHL2005749000](https://openairdocs.org/sdr/DHL2005749000), Sep 29, 2005: BATTERY. WEAK. EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR ILLUMINATED IN FLIGHT. FOUND BATTERIES WEAK. REPLACED BOTH EMERGENCY EXIT LIGHT BATTERIES AND RESEATED UNIT. OPS CHECK - [SDR DHL2005749001](https://openairdocs.org/sdr/DHL2005749001), Aug 19, 2005: LINK. BROKEN. WITH GEAR HANDLE IN UP POSITION RED DOOR LIGHTS REMAIN ILLUMINATED WITH MODERATE TO SEVERE VIBRATION. REMOVED AND REPLACED BROKEN DOOR LINK. DOORS OP SERVICEABL - [SDR GAIA05022OP](https://openairdocs.org/sdr/GAIA05022OP), Aug 11, 2005: BULB. BURNED OUT. L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED L1 DOOR EMERGENCY EXIT LIGHT. LIGHT OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA05019OP](https://openairdocs.org/sdr/GAIA05019OP), Apr 4, 2005: LIGHT. ILLUMINATED. EMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA05016OP](https://openairdocs.org/sdr/GAIA05016OP), Mar 25, 2005: BATTERY PACK. DISCHARGED. DURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LI - [SDR GAIA05002OP](https://openairdocs.org/sdr/GAIA05002OP), Jan 18, 2005: O-RING. DAMAGED. DURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED - [SDR GAIA04175OP](https://openairdocs.org/sdr/GAIA04175OP), Dec 4, 2004: DOWNLOCK SWITCH. FAILED. DURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DO - [SDR GAIA04171OP](https://openairdocs.org/sdr/GAIA04171OP), Oct 19, 2004: GASKET. BLOWN. DURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. - [SDR GAIA04168OP](https://openairdocs.org/sdr/GAIA04168OP), Sep 30, 2004: SEQUENCE VALVE. CRACKED. FLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE AI - [SDR C8GA20040021](https://openairdocs.org/sdr/C8GA20040021), Sep 24, 2004: O-RING. WORN. FLT 712 FROM TOL TO ONT. AFTER TAKEOFF, THE "A" SYSTEM WHEN TO 1/2 GALLON, RETRACT THE FLAPS TO 5 DEGREES AND THE HYDRAULIC SYSTEM WENT TO ZERO. ACCOMPLISHED AB - [SDR 2004F00407](https://openairdocs.org/sdr/2004F00407), Sep 11, 2004: HOUSING. CRACKED. DURING CHARGER FLT FROM CANCUN-BOS, B HYDRAULIC SYSTEM PRESSURE WENT TO ZERO, BOTH NR 1 AND NR 2 PUMP LOW PRESSURE LIGHTS ON. DUMPED 20,000 LBS OF FUEL AND DIVE - [SDR P9RA20040035](https://openairdocs.org/sdr/P9RA20040035), Aug 27, 2004: BATTERY PACK. INOPERATIVE. AIRCRAFT IN MAINTENANCE. CENTER FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 335001. - [SDR P9RA20040025](https://openairdocs.org/sdr/P9RA20040025), Jul 31, 2004: BULB. INOPERATIVE. AIRCRAFT IN MAINTENANCE, R2 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED R2 DOOR EXTERIOR LIGHT IAW MM 335001. - [SDR DHL2004749005](https://openairdocs.org/sdr/DHL2004749005), Jul 14, 2004: OVERHEAT LOOP. MALFUNCTIONED. LOWER AFT BODY OVERHEAT DOES NOT TEST. RESEATED AND CYCLED SYSTEM POWER ON OVERHEAT DETECTION SYSTEM BOX. REF B727 M/M 26-14-000. TESTED LOWER AFT BODY OVERHEAT - [SDR C8GA20040011](https://openairdocs.org/sdr/C8GA20040011), Jul 13, 2004: PITOT LINE. OBSTRUCTED. DURING TAKE-OFF ROLL, UNABLE TO REACH TARGET TAKE-OFF EPR SETTING ON NR 1 ENGINE. ABORTED TAKE-OFF AND RETURNED TO BLOCKS. UPON RETURNED TO BLOCKS, TROUBLESHOOT - [SDR RIV2004F00000](https://openairdocs.org/sdr/RIV2004F00000), Jul 3, 2004: ACTUATOR. LEAKING. FLIGHT CREW WAS UNABLE TO EXTEND THE RT MLG ON AC. DURING INITIAL APPROACH, THE APPROACH WAS ABORTED AND THE CREW ALLEGEDLY ACCOMPLISHED ALL APPROPRIATE CHECKLI - [SDR GAIA04080OP](https://openairdocs.org/sdr/GAIA04080OP), Jun 16, 2004: ACTUATOR. INOPERATIVE. FLT 716 - FWA-PHX - ON DEPARTURE AFTER RETRACTING FLAPS NOTED NR 2 LED DID NOT RETRACT, PROCEEDED TO CHECK LIST. RETURNED TO FWA WHERE A LANDING WAS MADE WITHOU - [SDR GAIA04078OP](https://openairdocs.org/sdr/GAIA04078OP), Jun 4, 2004: WIRE. BROKEN. FLT 2715 - ELP-DFW-FWA - DURING CLIMB, THE UPPER RUDDER INDICATOR WAS SWINGING BETWEEN MINOR INDICIES. AT 10,000 AGL THE LOWER RUDDER SWUNG HARD LEFT AND THEN A - [SDR GAIA04071](https://openairdocs.org/sdr/GAIA04071), Apr 27, 2004: COUPLER. MALFUNCTIONED. DEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH - [SDR P9RA20040010](https://openairdocs.org/sdr/P9RA20040010), Apr 9, 2004: CABLE. OUT OF RIG. WITH GEAR HANDLE IN THE OFF POSITION WHILE IN LIGHT TURBULENCE, NOSE GEAR LIGHT ILLUMINATED. (PIE TO SYR) CRUISE FLIGHT. FOUND NOSE GEAR WHEEL WELL DOOR CABLES All 220: https://openairdocs.org/model/boeing-727-2j0/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.