# Service difficulty reports: Boeing 727-2J0

A list on [Boeing 727-2J0](https://openairdocs.org/model/boeing-727-2j0.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 220 reports

- [SDR DHLA200800088](https://openairdocs.org/sdr/DHLA200800088.md): Engine · malfunctioned · Aug 15, 2008 · N749DH · Boeing 7272J0 · Engine (Turbine/Turboprop)
  > 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 AND IDLE PARAMETERS PER MM CH 71-00-87. PP STOP REMOVED AND SAFTIED. TO EPR 2.07. ACFT WAS GROUN
- [SDR DHL2008F00006](https://openairdocs.org/sdr/DHL2008F00006.md): Fairing · cracked · Jun 27, 2008 · N749DH · Boeing 7272J0 · Trailing Edge Flaps
  > 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.md): Structure · cracked · Jun 27, 2008 · N749DH · Boeing 7272J0 · Trailing Edge Flaps
  > 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 AND PAINTED THEN INSTALLED WITH SEALANT AND NAS1097D6 RIVETS, IAW BOEING 727 SRM 57-60-3. THIS IS
- [SDR DHL2008749012](https://openairdocs.org/sdr/DHL2008749012.md): Stringer · cracked · Feb 4, 2008 · N749DH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > 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.md): Skin · misrepaired · Feb 2, 2008 · N749DH · Boeing 7272J0 · Nacelle/Pylon, Main Frame
  > 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 AREAS. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 54-30-3 FIGURE
- [SDR DHL2008749010](https://openairdocs.org/sdr/DHL2008749010.md): Hinge · gouged · Jan 31, 2008 · N749DH · Boeing 7272J0 · Fuselage, Door Hinge
  > 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 5201B AND SRM 51-30-5. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. INSTALLED IAW MM
- [SDR DHL2008749016](https://openairdocs.org/sdr/DHL2008749016.md): Nose Cowl · cracked · Jan 25, 2008 · N749DH · Boeing 7272J0 · Engine Cowling System
  > 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 51-10-1. FABRICATED NEW DOUBLER REPAIR IAW SRM 51-30-5 AND 54-30-2 FIG 1. ALODINED AND PRIMED RE
- [SDR DHL2008749021](https://openairdocs.org/sdr/DHL2008749021.md): Stringer · corroded · Jan 21, 2008 · N749DH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > 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 NEW REPAIR IAW SRM 51-20-1, 51-20-2, 51-30-2, 53-10-2 FIG 9 AND 53-10-3 FIG 1. CLEANED STRINGER
- [SDR DHL2008749014](https://openairdocs.org/sdr/DHL2008749014.md): Tab · dented · Jan 20, 2008 · N749DH · Boeing 7272J0 · Aileron Tabs
  > 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 APPROXIMATE 2" DIAMETER. FABRICATED FILLER APPROXIMATE 2 INCHES DIAMETER AND DOUBLER APPROXIMATE 5
- [SDR DHL2008749020](https://openairdocs.org/sdr/DHL2008749020.md): Shear Tie · corroded · Jan 18, 2008 · N749DH · Boeing 7272J0 · Fuselage Internal Mounting Structure
  > 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 NEW SHEAR TIE IAW SRM 51-20-1, 51-20-2, 51-30-5 AND 53-10-2 FIG 3. ALODINE AND PRIMED ANGLE IAW S
- [SDR DHL2008749001](https://openairdocs.org/sdr/DHL2008749001.md): Stringer · corroded · Jan 10, 2008 · N749DH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > 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 FLANGE ON SPLICE. REMOVED SPLICE IAW B-727 SRM 51-30-2. FABRICATED NEW SPLICE USING BAC 1498-132
- [SDR GAIA06027OP](https://openairdocs.org/sdr/GAIA06027OP.md): Shutoff Valve · closed · Aug 25, 2006 · N284KH · Boeing 7272J0 · Fuel Selector/Shut-Off Valve
  > 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 SHORTLY AFTERWARD. THE FLIGHT CREW PERFORMED THE ENGINE FAILURE CHECKLIST AND RETURNED. THE AIR
- [SDR GAIA05037OP](https://openairdocs.org/sdr/GAIA05037OP.md): Downlock Switch · inoperative · Dec 15, 2005 · N281KH · Boeing 7272J0 · Landing Gear Position and Warning
  > 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 DOWN AND LOCKED. LANDING AND TAXI IN UNEVENTFUL. CLEANED AND RESEATED DOWNLOCK SWITCH AND (DOWNLOCK
- [SDR GAIA05035OP](https://openairdocs.org/sdr/GAIA05035OP.md): Connector · dirty · Dec 6, 2005 · N281KH · Boeing 7272J0 · Landing Gear System Wiring
  > DURING APPROACH, INITIAL GEAR EXTENSIO, NOSE GEAR INDICATOR (NOT SAFE), AFTER RECYCLE AND A SHORT DELAY INDICATION NORMAL. LANDING WAS MADE WITHOUT INCIDENT. CLEAN AND RESEATED NOSE GEAR CONNECTOR PLUGS. INSPECTED NOSE GEAR AREA. NO DEFECT NOTED. CHECKED
- [SDR DHL2005749021](https://openairdocs.org/sdr/DHL2005749021.md): Stringer · corroded · Nov 2, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > 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 51-30-2 MM 21-20-4 FOR ACCESS. CUT OUT DAMAGED SECTION OF STRINGER 8 1/2 INCHES LONG AT BS 720F + 14 AN
- [SDR DHL2005749017](https://openairdocs.org/sdr/DHL2005749017.md): Rod · cracked · Nov 2, 2005 · N749DH · Boeing 7272J0 · Leading Edge Slat Actuator
  > 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 SRM 51-30-2.
- [SDR DHL2005749016](https://openairdocs.org/sdr/DHL2005749016.md): Bracket · cracked · Nov 2, 2005 · N749DH · Boeing 7272J0 · Leading Edge Devices
  > 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 PO 9001801 DIM 9.15" BY 3.25" BY 1.25" IAW S/B 727-57-0130 REV 3 FIG 1. REMOVED ALUMINUM DOUBLERS F
- [SDR DHL2005749015](https://openairdocs.org/sdr/DHL2005749015.md): Frame · dented · Nov 2, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Frame
  > 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 B727 SRM 51-40-3 FIG 1 AND 53-10-2. TREATED AND PRIMED IAW B727 SRM 51-10-20. INSTALLED REPAIR ANG
- [SDR DHL2005749014](https://openairdocs.org/sdr/DHL2005749014.md): Web · cracked · Nov 2, 2005 · N749DH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > 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 PART MAT USED 7075 T6.040 PO 900505 DIM 19 1/2" BY 3" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 5. TREAT
- [SDR GAIA05029OP](https://openairdocs.org/sdr/GAIA05029OP.md): Light · inoperative · Nov 2, 2005 · N281KH · Boeing 7272J0 · Emergency Lighting
  > 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.md): Frame · dented · Nov 1, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Frame
  > 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 DOUBLER 12" BY 2 1/8" OF 7075 T6.063 PO 9002351 IAW B727 SRM 51-10-2 FIG 3 AND 51-40-3 FIG 1. TREAT
- [SDR DHL2005749011](https://openairdocs.org/sdr/DHL2005749011.md): Torque Box · cracked · Nov 1, 2005 · N749DH · Boeing 7272J0 · Horizontal Stabilizer Structure
  > 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 LWR CORNER IAW BOEING SB 727-53-0094 REV 3 AND COTNEY AEROSPACE ED NR EA204-4 REV IR HFEC VERIFIED
- [SDR DHL2005749010](https://openairdocs.org/sdr/DHL2005749010.md): Cowling · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Engine Cowling System
  > 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 AT 12 O'CLOCK IAW B727 SRM 54-30-3 FIG 2. FABBED FILLER FROM 2024T3.071 SIZE 5 1/4 INCHES BY 5 3/4
- [SDR DHL2005749009](https://openairdocs.org/sdr/DHL2005749009.md): Skin · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Trailing Edge Flaps
  > 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 DOUBLER APPROX 6" DIA FROM.016" 2024-T3 PO NR 9002556 BONDED FILLER AND DOUBLER SEALED AND PRIMED IAW B
- [SDR DHL2005749008](https://openairdocs.org/sdr/DHL2005749008.md): Skin · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > 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 PO NR 9002435 DIM 12 1/2" BY 7 1/2" AND FILLER MAT USE 2024T3.050 PO NR 53081 DIM 12 1/2" BY 6" IAW
- [SDR DHL2005749007](https://openairdocs.org/sdr/DHL2005749007.md): Skin · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > 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 DOUBLER OUT OF 2024T3 0.063 11 1/4" BY 7 1/2" PO NR 53125 IAW B727 SRM 53-30-2 FIG 2 AND SRM 53-30
- [SDR DHL2005749006](https://openairdocs.org/sdr/DHL2005749006.md): Skin · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > 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 DOUBLER 2024T3.090 PO NR 9002435 DIM 5.250" DIA AND FILLER 2024T3.080 PO NR 9002727 DIM.750" D
- [SDR DHL2005749005](https://openairdocs.org/sdr/DHL2005749005.md): Skin · dented · Oct 31, 2005 · N749DH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > 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 19" IAW B727 SRM 53-30-1 FIG 1. CUT OUT DENTED SECTION OF FUSELAGE SKIN SIZE 1" BY 2.550" AT STA
- [SDR DHL2005749004](https://openairdocs.org/sdr/DHL2005749004.md): Skin · dented · Oct 30, 2005 · N749DH · Boeing 7272J0 · Elevator, Plate/Skin
  > 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 DRILLED FASTENERS HOLES IN NEW PANEL ASSY P/N 65-25639-75 PO NR 540027 IAW B727 SRM 51-30-2 FIG 1. T
- [SDR DHL2005749003](https://openairdocs.org/sdr/DHL2005749003.md): Hinge · cracked · Oct 30, 2005 · N749DH · Boeing 7272J0 · Spoilers
  > 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 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM MAT 70-75-T6 071 - PO NR 9002507 DIMS 5 3/4" BY 4 1/4"
- [SDR DHL2005749000](https://openairdocs.org/sdr/DHL2005749000.md): Battery · weak · Sep 29, 2005 · N749DH · Boeing 7272J0 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR ILLUMINATED IN FLIGHT. FOUND BATTERIES WEAK. REPLACED BOTH EMERGENCY EXIT LIGHT BATTERIES AND RESEATED UNIT. OPS CHECKS NORMAL IAW B727 M/M CH 33-50-71. TWO EA P/N 37067-001.
- [SDR DHL2005749001](https://openairdocs.org/sdr/DHL2005749001.md): Link · broken · Aug 19, 2005 · N749DH · Boeing 7272J0 · Landing Gear Door Retract Section
  > WITH GEAR HANDLE IN UP POSITION RED DOOR LIGHTS REMAIN ILLUMINATED WITH MODERATE TO SEVERE VIBRATION. REMOVED AND REPLACED BROKEN DOOR LINK. DOORS OP SERVICEABLE IAW MM 32-35-0 AND 32-22-1 P/N: 69-29527-3.
- [SDR GAIA05022OP](https://openairdocs.org/sdr/GAIA05022OP.md): Bulb · burned out · Aug 11, 2005 · N281KH · Boeing 7272J0 · Emergency Lighting
  > 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.md): Light · illuminated · Apr 4, 2005 · N284KH · Boeing 7272J0 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Mar 25, 2005 · N284KH · Boeing 7272J0 · Emergency Lighting
  > DURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHTS SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AC WAS RETURNED TO SERVICE.
- [SDR GAIA05002OP](https://openairdocs.org/sdr/GAIA05002OP.md): O-Ring · damaged · Jan 18, 2005 · N284KH · Boeing 7272J0 · Turbine Engine Oil System
  > 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 AND REINSTALLED NR 2 ENGINE FUEL PUMP, REPLACED FUEL PUMP GARLOC SEAL AND SHAFT O-RING PACKING.
- [SDR GAIA04175OP](https://openairdocs.org/sdr/GAIA04175OP.md): Downlock Switch · failed · Dec 4, 2004 · N281KH · Boeing 7272J0 · Landing Gear Position and Warning
  > 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 DOWN AND LOCKED. DECLARED EMERGENCY. LANDING AND TAXI IN UNEVENTFUL. TROUBLESHOOT NOSE GEAR INDIC
- [SDR GAIA04171OP](https://openairdocs.org/sdr/GAIA04171OP.md): Gasket · blown · Oct 19, 2004 · N284KH · Boeing 7272J0 · Engine Bleed Air System
  > 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. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASKET AND TIGHTENED CLA
- [SDR GAIA04168OP](https://openairdocs.org/sdr/GAIA04168OP.md): Sequence Valve · cracked · Sep 30, 2004 · N284KH · Boeing 7272J0 · Landing Gear Retraction/Extension System
  > 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 AIRCRAFT RETURNED TO ELP WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND LEFT MLG SEQUENCE VALVE LE
- [SDR C8GA20040021](https://openairdocs.org/sdr/C8GA20040021.md): O-Ring · worn · Sep 24, 2004 · N713AA · Boeing 7272J0 · Hydraulic System, Main
  > 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 ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST, AIR TURN BACK TO KTOL AND LANDED WITHOUT INCIDENT
- [SDR 2004F00407](https://openairdocs.org/sdr/2004F00407.md): Housing · cracked · Sep 11, 2004 · N364PA · Boeing 7272J0 · Hydraulic Filter, Main
  > 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 DIVERTED TO MCO. FOUND B HYDRAULIC SYSTEM CASE DRAIN FILTER HOUSING CRACKED. REPLACED FILTER AND HOUS
- [SDR P9RA20040035](https://openairdocs.org/sdr/P9RA20040035.md): Battery Pack · inoperative · Aug 27, 2004 · N906PG · Boeing 7272J0 · Emergency Lighting
  > 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.md): Bulb · inoperative · Jul 31, 2004 · N906PG · Boeing 7272J0 · Emergency Lighting
  > AIRCRAFT IN MAINTENANCE, R2 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED R2 DOOR EXTERIOR LIGHT IAW MM 335001.
- [SDR DHL2004749005](https://openairdocs.org/sdr/DHL2004749005.md): Overheat Loop · malfunctioned · Jul 14, 2004 · N749DH · Boeing 7272J0 · Overheat Detection
  > 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, OPS CHECKS NORMAL.
- [SDR C8GA20040011](https://openairdocs.org/sdr/C8GA20040011.md): Pitot Line · obstructed · Jul 13, 2004 · N713AA · Boeing 7272J0 · Pitot/Static System
  > 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 THE EPR SYSTEM AND FOUND THE PT-2 INLET OBSTRUCTED. CLEARED OBSTRUCTION BUT EPR READING CONTINUES I
- [SDR RIV2004F00000](https://openairdocs.org/sdr/RIV2004F00000.md): Actuator · leaking · Jul 3, 2004 · N364PA · Boeing 7272J0 · Landing Gear Actuator
  > 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 CHECKLIST ITEMS. THE RT MLG WOULD STILL NOT EXTEND USING THE MANUAL EXTENSION SYSTEM, ( THE GEAR APPEARED
- [SDR GAIA04080OP](https://openairdocs.org/sdr/GAIA04080OP.md): Actuator · inoperative · Jun 16, 2004 · N281KH · Boeing 7272J0 · Leading Edge Slat Actuator
  > 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 WITHOUT INCIDENT. FOUND NR 2 L/E SLAT ACTUATOR INOPERATIVE. REMOVED AND REPLACED ACTUATOR. OPS CHECK G
- [SDR GAIA04078OP](https://openairdocs.org/sdr/GAIA04078OP.md): Wire · broken · Jun 4, 2004 · N281KH · Boeing 7272J0 · Flight Control System Wiring
  > 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 ANOTHER LEFT NOT AS HARD. CREW FOLLOWED FLIGHT CONTROL EMERGENCY PROCEDURE AND RETURNED TO ELP. AN
- [SDR GAIA04071](https://openairdocs.org/sdr/GAIA04071.md): Coupler · malfunctioned · Apr 27, 2004 · N281KH · Boeing 7272J0 · Autopilot System
  > DEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPORT, WHERE A LANDING W
- [SDR P9RA20040010](https://openairdocs.org/sdr/P9RA20040010.md): Cable · out of rig · Apr 9, 2004 · N919PG · Boeing 7272J0 · Nose/Tail Landing Gear
  > 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 WITH LOW TENSION. ADJUSTED PER M/M 32-22. CLEANED AND LUBRICATED NOSE GEAR. OPERATIONALLY CHECKED G

Next page: https://openairdocs.org/model/boeing-727-2j0/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '7272J0'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2j0/reports

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