# Service difficulty reports: Boeing 727-82

A list on [Boeing 727-82](https://openairdocs.org/model/boeing-727-82.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 103 reports

- [SDR ASAA2016010814695](https://openairdocs.org/sdr/ASAA2016010814695.md): Warning Message · false activation · Jan 8, 2016 · N565AS · Boeing 72782 · Flight Management Computing Hardware System
  > FMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.
- [SDR ASAA2016010714700](https://openairdocs.org/sdr/ASAA2016010714700.md): Fmc · malfunctioned · Jan 7, 2016 · N557AS · Boeing 72782 · Flight Management Computing Hardware System
  > 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 SWITCH, THE CAPTS SIDE WAS RESTORED BUT THE F/O SIDE LOST THE MAP DISPLAY. BOTH CDUS DISPLAYED AN "FM
- [SDR ASAA2016010714694](https://openairdocs.org/sdr/ASAA2016010714694.md): Warning Message · false activation · Jan 7, 2016 · N566AS · Boeing 72782 · Flight Management Computing Hardware System
  > 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.md): Light · inoperative · Sep 28, 2000 · N357NE · Boeing 72782 · Emergency Lighting
  > 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.md): Indicator · false indication · Sep 22, 2000 · N357NE · Boeing 72782 · Engine Oil Indicating System
  > 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 ENGINE OPS CHECK GOOD.
- [SDR EISA20000143](https://openairdocs.org/sdr/EISA20000143.md): Flange · corroded · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Main, Frame
  > 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 51-10-2, 51-30-2 AND 53-10-2.
- [SDR EISA20000142](https://openairdocs.org/sdr/EISA20000142.md): Splice · corroded · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > 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 51-30-2.
- [SDR EISA20000141](https://openairdocs.org/sdr/EISA20000141.md): Splice · corroded · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > 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 53-10-3.
- [SDR EISA20000140](https://openairdocs.org/sdr/EISA20000140.md): Flange · cracked · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Main, Frame
  > 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 65-18420, B727 SRM 51-10-2, 51-30-2 AND 53-10-2.
- [SDR EISA20000139](https://openairdocs.org/sdr/EISA20000139.md): Attach Angle · corroded · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Main, Structure
  > 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 53-10-2.
- [SDR EISA20000138](https://openairdocs.org/sdr/EISA20000138.md): Splice · corroded · Sep 4, 2000 · N375NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > 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.md): Doubler · bulged · Sep 4, 2000 · N357NE · Boeing 72782 · Fuselage Main, Plate/Skin
  > SKIN EXTERIOR BULGED AND FASTENERS PULLED AT STA 345 TO STA 350. FABRICATED DOUBLER, FILLER, SHEAR TIES AND ANGLES. ALODINED, PRIMED AND INSTALLED DOUBLER, FILLER, SHEAR TIES AND ANGLES IAW B727 DRAWING 65-18420, B727 SRM.
- [SDR EISA20000135](https://openairdocs.org/sdr/EISA20000135.md): Switch · misaligned · Sep 3, 2000 · N357NE · Boeing 72782 · Landing Gear Position and Warning
  > 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 32-62-11, OPS CHECK GOOD.
- [SDR EISA20000134](https://openairdocs.org/sdr/EISA20000134.md): Outflow Valve · leaking · Sep 3, 2000 · N357NE · Boeing 72782 · Pressure Regulator/Outflow Valve
  > 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 HELP. RESEALED AFFECTED AREAS OF LEAKING. REMOVED AND REINSTALLED OUTFLOW VALVE ON RIGHT SIDE. SE
- [SDR EISA20000144](https://openairdocs.org/sdr/EISA20000144.md): Skin · misdrilled · Aug 31, 2000 · N357NE · Boeing 72782 · Fuselage Main, Plate/Skin
  > 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 W00022 AND B727 SRM 51-10-7.
- [SDR 20000058](https://openairdocs.org/sdr/20000058.md): Gasper Fan · seized · Jul 18, 2000 · N357NE · Boeing 72782 · Air Distribution Fan
  > 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 21-23-1. OPS CHECK NORMAL, THIS CLEARS PLACARD 874.
- [SDR EISA2000004](https://openairdocs.org/sdr/EISA2000004.md): Valve · malfunctioned · Jan 4, 2000 · N257NE · Boeing 72782 · Fuel Heater
  > 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.md): Switch · failed · Mar 12, 1999 · Boeing 72782 · Leading Edge Slat Control System
  > (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 PARTS, OPERATED PER MEL. NR 7 SLAT POSITION SWITCH REPLACED.
- [SDR CA990323017](https://openairdocs.org/sdr/CA990323017.md): Gcu · arcing · Mar 10, 1999 · Boeing 72782 · AC Generation System
  > (CAN) NR 1 GENERATOR'S CIRCUIT BREAKER TRIPPED, GCU RECEPTACLE ARCING. RECEPTACLE AND GCU REPLACED.
- [SDR CA990330034](https://openairdocs.org/sdr/CA990330034.md): Gcu · failed · Mar 9, 1999 · Boeing 72782 · AC Generation System
  > (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.md): Bracket · broken · Feb 3, 1999 · Boeing 72782 · Trailing Edge Flaps
  > (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.md): Frame · damaged · Nov 24, 1998 · Boeing 72782 · Fuselage Main, Frame
  > (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.md): Panel · corroded · Nov 16, 1998 · Boeing 72782 · Fuselage Main, Plate/Skin
  > (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.md): Hinge · broken · Apr 16, 1998 · Boeing 72782 · Fuselage, Door Hinge
  > (CAN) MAIN CARGO DOOR UPPER AFT HINGE BROKEN AT 7 SEGMENTS, REPLACED. PART TC: 3,211.
- [SDR EISA97206](https://openairdocs.org/sdr/EISA97206.md): Packing · deteriorated · Oct 8, 1997 · N357NE · Boeing 72782 · Nose/Tail Landing Gear Strut/Axle
  > 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.md): Aural Warn Box · malfunctioned · Jul 22, 1997 · N357NE · Boeing 72782 · Central Warning
  > AT BRU, FIRE WARNING BELL INOP. REPLACED AURAL WARNING BOX. (M)
- [SDR EISA97152](https://openairdocs.org/sdr/EISA97152.md): Connector · loose · Jun 22, 1997 · N357NE · Boeing 72782 · Landing Gear Position and Warning
  > 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.md): Smoke Detector · contaminated · Jun 13, 1997 · N357NE · Boeing 72782 · Smoke Detection
  > 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.md): Ball Guides · missing · Jan 23, 1997 · N357NE · Boeing 72782 · Trailing Edge Flap Control System
  > 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 AND NR 8 JACKSCREWS PER MM 27-52-1, OPS CHECK OK. (M)
- [SDR EISA96148](https://openairdocs.org/sdr/EISA96148.md): Connector · broken wire · Sep 16, 1996 · N357NE · Boeing 72782 · Engine Oil Temperature
  > 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 GOOD AND ENGINE RUN. (M)
- [SDR EISA96143](https://openairdocs.org/sdr/EISA96143.md): Pack Vlv · inoperative · Aug 17, 1996 · N357NE · Boeing 72782 · Cabin Cooling System
  > 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. (M)
- [SDR EISA96101](https://openairdocs.org/sdr/EISA96101.md): Fairing · missing · Jul 4, 1996 · N357NE · Boeing 72782 · Cargo/Baggage Doors
  > 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. (M)
- [SDR EISA95388](https://openairdocs.org/sdr/EISA95388.md): Bulkhead · cracked · Oct 12, 1995 · N357NE · Boeing 72782 · Fuselage Main, Bulkhead
  > 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 PRESS BULKHEAD. STOP DRILLED CRACKS. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B727 SRM 51-40-2 AND
- [SDR EISA95332](https://openairdocs.org/sdr/EISA95332.md): Skin · delaminated · Oct 9, 1995 · N357NE · Boeing 72782 · Fuselage Main, Plate/Skin
  > 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 SECOND ONE WAS 24 INCHES BY 30 INCHES IAW B727 SRM 53-30-2 AND 53-30-3. (M)
- [SDR EISA95331](https://openairdocs.org/sdr/EISA95331.md): Stiffener · corroded · Oct 9, 1995 · N357NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > 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. CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B727 51-40-4. (M)
- [SDR EISA95304](https://openairdocs.org/sdr/EISA95304.md): S-Duct · cracked · Sep 29, 1995 · N357NE · Boeing 72782 · Nacelle/Pylon Structure
  > 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 FASTENERS AND REPAIR FOUND CRACK HAD EXCEEDED LENGTH OF REPAIR. REMOVED SECTION WITH CRACK. FORMED AND
- [SDR EISA95334](https://openairdocs.org/sdr/EISA95334.md): Hinge Fitting · corroded · Sep 23, 1995 · N357NE · Boeing 72782 · Leading Edge Devices
  > 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 THE NR 3 KRUGER FLAP INBOARD HINGE FITTING IAW B727 MM 27-81-0. (M)
- [SDR EISA95370](https://openairdocs.org/sdr/EISA95370.md): Ribs · mismanufactured · Sep 19, 1995 · N357NE · Boeing 72782 · Leading Edge Devices
  > 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 INCH LIMIT. FABRICATED THREE REPAIR ANGLES IAW B727 SRM CH 57-50-3 PO NR 60733 7075-0 X.040 HEAT
- [SDR EISA95351](https://openairdocs.org/sdr/EISA95351.md): L-Angle · cracked · Sep 19, 1995 · N357NE · Boeing 72782 · Trailing Edge Flaps
  > 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. STOP DRILLED CRACK. FABRICATED AN L-ANGLE REPAIR AND INSTALLED IAW B727 SRM 51-40-4. (M)
- [SDR EISA95292](https://openairdocs.org/sdr/EISA95292.md): Rivets · missing · Sep 18, 1995 · N357NE · Boeing 72782 · Emergency Exits
  > 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 UPPER LEFT AND RIGHT CORNERS BY UPPER LATCH ROLLERS (MARKED). REMOVED AND INSTALLED NEW FASTENERS IA
- [SDR EISA95335](https://openairdocs.org/sdr/EISA95335.md): Skin · cracked · Sep 17, 1995 · N357NE · Boeing 72782 · Wing, Plate/Skin
  > 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 D-FLAP. CUT OUT CRACKED SECTION. FABRICATED FILLERS, SPACERS, COVERS, L-ANGLE, AND SPLICE ANGLES
- [SDR EISA95374](https://openairdocs.org/sdr/EISA95374.md): Fitting · corroded · Sep 16, 1995 · N357NE · Boeing 72782 · Wing Miscellaneous Structure
  > 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 SUPPORT FITTING IAW SRM B727 51-10-1. FAB NEW SUPPORT FITTING IAW SRM B727 51-10-1. ALODINED AND PRIM
- [SDR EISA95369](https://openairdocs.org/sdr/EISA95369.md): Bracket · corrosion · Sep 16, 1995 · N357NE · Boeing 72782 · Wing Miscellaneous Structure
  > 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. REPAIRED WEB PER 51-40-2 B727 SRM, FASTENERS PER 51-30-2 B727 SRM, CORROSION INHIBITOR PER 51-10-
- [SDR EISA95362](https://openairdocs.org/sdr/EISA95362.md): Skin · damaged · Sep 16, 1995 · N357NE · Boeing 72782 · Leading Edge Devices
  > 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 MOUNTING SCREW. FABRICATED REPAIR WITH 2024T3 X.090 TRAV NR 1A-720 PO NR 605687 APPROX 4.5 INCHES B
- [SDR EISA95359](https://openairdocs.org/sdr/EISA95359.md): Skin · damaged · Sep 14, 1995 · N357NE · Boeing 72782 · Leading Edge Devices
  > 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 AND CLOSED OUT PANELS TO F.O.M. REPAIR. FABRICATED REPAIR 5 INCHES BY 6.5 INCHES FROM 2024T3-.080
- [SDR EISA95333](https://openairdocs.org/sdr/EISA95333.md): Frame · broken · Sep 14, 1995 · N357NE · Boeing 72782 · Vertical Stabilizer, Spar/Rib
  > 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 BROKEN WEBS. FABRICATED AND INSTALLED TWO WEBS IAW B727 SRM 51-40-2. (M)
- [SDR EISA95377](https://openairdocs.org/sdr/EISA95377.md): Angle · corrosion · Sep 13, 1995 · N357NE · Boeing 72782 · Leading Edge Devices
  > 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. FABRICATED NEW ATTACH ANGLE, ALODINED AND PRIMED AND INSTALLED NEW BRACKET IAW B727 SRM 51-10-1, 51-10-2
- [SDR EISA95325](https://openairdocs.org/sdr/EISA95325.md): Splice Plate · cracked · Sep 13, 1995 · N357NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > 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 SPLICE PLATE. FABRICATED AND INSTALLED NEW PLATE IAW B727 SB 53-0194 AND AD 91-24-11. (M)
- [SDR EISA95360](https://openairdocs.org/sdr/EISA95360.md): Access Panel · corroded · Sep 12, 1995 · N357NE · Boeing 72782 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT MAIN LANDING GEAR, FORWARD TRUNNION ACCESS PANEL AROUND MOUNTING HOLES. REMOVED DAMAGED AREA IAW B727 SRM 53-30-3. FAB NEW REPAIR IAW SRM B727 53-30-3. PRIMED AND ALODINED REPAIR IAW SRM
- [SDR EISA95324](https://openairdocs.org/sdr/EISA95324.md): Flux Vlv Harness · too short · Sep 12, 1995 · N357NE · Boeing 72782 · Attitude and Direction Data System
  > DURING F.O.M., THE LENGTHENING OF FLUX VALVE HARNESS WAS REQUIRED TO RELOCATE A BRACKET IAW B727 MM 34-21-0. (M)

Next page: https://openairdocs.org/model/boeing-727-82/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 = '72782'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-82/reports

---
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.