# Service difficulty reports: Boeing 727-2A7

A list on [Boeing 727-2A7](https://openairdocs.org/model/boeing-727-2a7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 60 reports

- [SDR EISA20010090](https://openairdocs.org/sdr/EISA20010090.md): Splice · corroded · May 5, 2001 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > STRINGER AT BS 680 27 RIGHT SPLICE IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE, INSTALLED NEW SPLICE IAW SRM 53-10-3, 51-10-2, M/M 51-21-31.
- [SDR EISA20000205](https://openairdocs.org/sdr/EISA20000205.md): Skin · dented · Nov 14, 2000 · N310NE · Boeing 7272A7 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN DENTED BS 1260 TO 1280, STRINGER 21R TO 23R. CORRECTIVE ACTION: REMOVED DENTED AREA, FABRICATED DOUBLER, FILLER, AND STRINGER SPLICE REPAIRS, ALODINED, PRIMED AND INSTALLED, REPAIR DOUBLER, IAW 53-30-3 FIG 3, 53-10-3FIG 1, AND FIG 3, 51-10-2
- [SDR EISA20000204](https://openairdocs.org/sdr/EISA20000204.md): Skin · dented · Nov 14, 2000 · N310NE · Boeing 7272A7 · Entrance Stairs
  > AFT AIRSTAIR SKIN HAS 12 INCH LONG DENT. CORRECTIVE ACTION: REMOVED DENTED AREA, FABRICATED, ALODINED, PRIMED, AND INSTALLED SKIN DOUBLER AND CHANNEL IAW SRM 53-10-3, 52-10-2 FIG. 5, 52-10-1, 51-10-2 AND 51-30-2.
- [SDR EISA20000146](https://openairdocs.org/sdr/EISA20000146.md): Switch · out of adj · Sep 7, 2000 · N310NE · Boeing 7272A7 · Auxiliary Gear (Tail Skid)
  > ON ASCENT TAIL SKID LIGHT ILLUMINATED (AIR TURNBACK). ADJUSTED TAIL SKID SWITCH PER M/M 32-71, OPS CHECK NORMAL.
- [SDR EISA2000014](https://openairdocs.org/sdr/EISA2000014.md): Engine · leaking · Feb 11, 2000 · N310NE · Boeing 7272A7 · Turbine Engine Oil System
  > NR 2 ENGINE LOSING 1 QUART OF OIL EVERY 5-7 MINUTES. IN FLIGHT SHUTDOWN NR 2 ENGINE. UNSCHEDULED LANDING. (M)
- [SDR EISA2000006](https://openairdocs.org/sdr/EISA2000006.md): Valve · damaged · Jan 13, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control System
  > AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT, WENT TO MANUAL AND STANDBY POSITIONS. CABIN KEPT CLIMBING. AIR TURN BACK TO IND. REMOVED AND REPLACED RIGHT PACK VALVE PER MM 21-55. REPLACED CABIN PRESSURE CONTROLLER AND PACK SWITCHES. OPS CHECK OK PER MM 2
- [SDR EISA2000017](https://openairdocs.org/sdr/EISA2000017.md): Valve · damaged · Jan 13, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control System
  > AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT WENT TO MANUAL AND STANDBY POSITIONS. CABIN KEPT CLIMBING. AIR TURN BACK TO IND. REMOVED AND REPLACED RIGHT PACK VALVE PER MM 21-55. REPLACED CABIN PRESSURE CONTROLLER ADN PACK SWITCHES. OPS CHECK OK PER MM 21
- [SDR EISA2000005](https://openairdocs.org/sdr/EISA2000005.md): Controller · failed · Jan 12, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control System
  > PRESSURIZATION INOP, CABIN WAS UNCONTROLLABLE UNABLE TO MAKE CABIN DESCEND A/C ALTITUDE 10,000 CABIN WAS AT 8000 OUTFLOW VALVE CARGO HEAT CLOSED. CABIN STILL UNCONTROLLABLE IN ALL MODES. GROUND OPS TESTED PRESSURIZATION SYSTEM PER MM 21-30. PRESSURIZED TO 5
- [SDR EISA99252](https://openairdocs.org/sdr/EISA99252.md): Engine · lack of lube · Dec 7, 1999 · N310NE · Boeing 7272A7 · Turbine Engine Oil System
  > NR 3 ENGINE SHUT DOWN DUE TO LOW OIL QUANTITY, AND LOW OIL PRESSURE. ENGINE WINDMILLED BELOW TEN PSI OIL PRESSURE FOR ONE HOUR AND TEN MINUTES. (M)
- [SDR EISA99163](https://openairdocs.org/sdr/EISA99163.md): Light · inoperative · Aug 23, 1999 · N310NE · Boeing 7272A7 · Emergency Lighting
  > ON POST FLIGHT, L-1 DOOR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED L-1 EMERGENCY LIGHT PER MM 33-50-0. OPS CHECK GOOD. (M)
- [SDR EISA99158](https://openairdocs.org/sdr/EISA99158.md): Engine · failed · Aug 21, 1999 · N310NE · Boeing 7272A7 · Engine (Turbine/Turboprop)
  > NR 3 ENGINE EGT REACHED RED LINE ON TAKEOFF. REPLACED NR 3 ENGINE. (M)
- [SDR EISA99155](https://openairdocs.org/sdr/EISA99155.md): Light · defected · Aug 20, 1999 · N310NE · Boeing 7272A7 · Emergency Lighting
  > REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM 33-50. OPS CHECK GOOD. (M)
- [SDR EISA99137](https://openairdocs.org/sdr/EISA99137.md): Switch · dirty · Jun 15, 1999 · N310NE · Boeing 7272A7 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS LIGHT WENT FROM GREEN TO AMBER, F/E PANEL LIGHT NORMAL. CLEANED AND RESET L/E SLAT SWITCH. (M)
- [SDR EISA99130](https://openairdocs.org/sdr/EISA99130.md): Indicator · unserviceable · May 22, 1999 · N310NE · Boeing 7272A7 · Trailing Flap Position Indicating System
  > CREW HAD SPLIT FLAP INDICATION, DECLARED EMERGENCY AND MADE 'GO AROUND'. CHECKED FLAP OPERATION, REPLACED OUTBOARD FLAP INDICATOR AND OPS CHECKED OK. (M)
- [SDR EISA99121](https://openairdocs.org/sdr/EISA99121.md): Indicator · failed · May 22, 1999 · N310NE · Boeing 7272A7 · Trailing Flap Position Indicating System
  > CREW HAD SPLIT INDICATOR DECLARED EMERGENCY AND MADE GO AROUND. CHECKED FLAP OPERATION. REPLACED OUTBOARD FLAP INDICATOR AND OPS CHECKED OK. (M)
- [SDR EISA98249](https://openairdocs.org/sdr/EISA98249.md): Light · inoperative · Oct 15, 1998 · N310NE · Boeing 7272A7 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED EMERGENCY LIGHT, OPS CHECK GOOD PER MM 33-50. (M)
- [SDR EISA98223](https://openairdocs.org/sdr/EISA98223.md): Door · leaking · Sep 23, 1998 · N310NE · Boeing 7272A7 · Passenger/Crew Doors
  > UNABLE TO PRESSURIZE DUE TO LEAK IN CREW FORWARD ENTRY DOOR. NO WARNING LIGHTS. AIR TURN BACK TO IND. FOUND L-1 DOOR NOT PROPERLY CLOSED. OPENED AND CLOSED DOOR. PRESSURIZED ON GROUND, OK FOR SERVICE. TT: 69,782:12 HOURS. TC: 46,771. (X)
- [SDR EISA98239](https://openairdocs.org/sdr/EISA98239.md): Frame · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION CARD, FOUND FUSELAGE FRAME CRACKED AT STATION 570. REPAIRED FRAME PER SRM 53-20-2 DOUBLER INSTALLED. (M)
- [SDR EISA98238](https://openairdocs.org/sdr/EISA98238.md): Flange · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF C-ROUTINE CPCP INSPECTION CARD, FOUND CORROSION IN NOSE WHEEL WELL PANEL 3120. CORROSION WAS FOUND ON OUTBOARD FLANGE. REPLACED FLANGE PER SRM 53-10-2 DOUBLER INSTALLED. (M)
- [SDR EISA98237](https://openairdocs.org/sdr/EISA98237.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 344 TO 480 RBL 44. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-1. (M)
- [SDR EISA98236](https://openairdocs.org/sdr/EISA98236.md): Fitting · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Main Landing Gear Attach Section
  > DURING ACCOMPLISHMENT OF C-CHECK, WHILE DOING SCHEDULED GEAR CHANGE LEFT FORWARD TRUNNION FITTING CORRODED. REMOVED AND REPLACED FWD TRUNNION FITTING PER SRM 51-10-1 AND 51-30-2 AND MM 20-80-1. (M)
- [SDR EISA98235](https://openairdocs.org/sdr/EISA98235.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION ON SEAT TRACK STATION 560 RBL 44. REMOVED AND REPLACED DAMAGED AREA OF SEAT RACK PER SRM 53-10-5. (M)
- [SDR EISA98234](https://openairdocs.org/sdr/EISA98234.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 837 RBL 24. REMOVED AND REPLACED DAMAGED AREA OF SEAT TRACK PER SRM 53-10-5. (M)
- [SDR EISA98233](https://openairdocs.org/sdr/EISA98233.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 400 RBL 23. REMOVED SEAT TRACK FABRICATED NEW ONE PER SRM 53-10-5. (M)
- [SDR EISA98232](https://openairdocs.org/sdr/EISA98232.md): Web · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION, FOUND RIGHT WEB AT STATION 870 IN KEELBEAM CRACKED. REMOVED DAMAGED AREA FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-2 FIGURE 4. (M)
- [SDR EISA98231](https://openairdocs.org/sdr/EISA98231.md): Angle · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION CARD, FOUND VERTICAL ATTACH ANGLE AT STATION 870 IN KEELBEAM CRACKED. REMOVED AND REPLACED WITH NEW PART PER SRM 51-10-1. (M)
- [SDR EISA98230](https://openairdocs.org/sdr/EISA98230.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION SEAT TRACK STATION 640 AND RBL 44. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. (M)
- [SDR EISA98229](https://openairdocs.org/sdr/EISA98229.md): Web · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD INSPECTION, A 4 INCH CRACK WAS FOUND AT STATION 870 BULKHEAD AT APPROX BL 10. REPAIRED AREA WITH DOUBLER PER EO 53-98-143-1 AND SRM 51-30-2. (M)
- [SDR EISA98228](https://openairdocs.org/sdr/EISA98228.md): Stringer · missing · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD 53-113-01, A 5 INCH SECTION OF STRINGER 30 WAS MISSING FROM FLOOR AFT CARGO PIT BS 1175. REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER PER SRM 53-10-3. (M)
- [SDR EISA98227](https://openairdocs.org/sdr/EISA98227.md): Frame · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 540 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M)
- [SDR EISA98226](https://openairdocs.org/sdr/EISA98226.md): Frame · cracked · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 560 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M)
- [SDR EISA98225](https://openairdocs.org/sdr/EISA98225.md): Seat Track · corroded · Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK AT STATION 1050 LBL 25. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. (M)
- [SDR EISA98176](https://openairdocs.org/sdr/EISA98176.md): Gearbox · contaminated · Jul 11, 1998 · N310NE · Boeing 7272A7 · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM IND WHILE RETRACTING FLAPS, OUTBOARD FLAPS DID NOT RETRACT FROM 2 DEGREES TO UP. PERFORMED PROCEDURE AND PROBLEM REMAINED. RETURNED TO IND. GENERATED FROM PILOT REPORT. CYCLED FLAPS, FLUSHING ANY POSSIBILITY OF AIR, INSPECTED FLAPS, FLAP
- [SDR EISA98148](https://openairdocs.org/sdr/EISA98148.md): Compressor · stalled · Jun 10, 1998 · N310NE · Boeing 7272A7 · Turbine Engine Compressor Section
  > ON TAKEOFF OUT OF ICT NR 3 ENGINE COMPRESSOR STALLED TRIPPING BOTH PACKS ON CLIMB NR 3 REACHED MAX CONT EGT,.10 EPR, BELOW MAX CLIMB EPR, IN CRUISE ALL ENGINE PARAMETERS NORMAL. ICT TEMP 23 DEGREES CELSIUS WIND 100 AT 7 RUNWAY 19R. GENERATED FROM PILOT REPO
- [SDR EISA98146](https://openairdocs.org/sdr/EISA98146.md): Tire · failed · Jun 10, 1998 · N310NE · Boeing 7272A7 · Tire
  > RIGHT MAIN TIRES BLEW POSSIBLY ON TAKEOFF FROM ICT. ICT TOWER REPORTED RUBBER ON RUNWAY. REPAIRED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES IAW 32-45-1. NR 4 TIRE IS THE TIRE THAT BLEW OUT. (M)
- [SDR EISA98123](https://openairdocs.org/sdr/EISA98123.md): Hose · chafed · Jun 9, 1998 · N310NE · Boeing 7272A7 · Engine Thrust Reverser
  > AFTER TAKEOFF, INDIANAPOLIS (IND) WHILE CLIMBING THROUGH APPROXIMATELY 3,000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL. C/W ENGINE NR 1, THRUST REDUCED, LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE COOLING. RETURNED TO (IND). GENERATED FR
- [SDR EISA98127](https://openairdocs.org/sdr/EISA98127.md): Clamp · loose · May 31, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution System
  > CLIMGING THROUGH 16,000 FEET AT 91 PERCENT N1, GOT A NR 1 STRUT OVERHEAT LIGHT OUT WITH THROTTLE RETARDED. SWAPPED NR 1 AND NR 3 BLEEDS PER AOM WITH NO RECURRENCE IN-FLIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT SYSTEM TO LOOSE CLAMP. TIGHTENED CLAMP.
- [SDR EISA98118](https://openairdocs.org/sdr/EISA98118.md): Clamp · loose · May 24, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution System
  > DURING CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT FOUND 8TH STAGE DUCT CLAMP LOOSE, DUCT MISALIGNED, TIGHTENED AND ALIGNED CAMP, RAN ENGINE. NO LEAKS NOTED. (M)
- [SDR EISA98117](https://openairdocs.org/sdr/EISA98117.md): Clamp · loose · May 24, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution System
  > DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST PER ABNORMAL CHECK LIST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON PNEUMATIC DUCT NR 1 ENGINE. RAN ENGINE, LEAK CHECK GOOD. (M)
- [SDR EISA98067](https://openairdocs.org/sdr/EISA98067.md): Fuel Pump · failed · Mar 24, 1998 · N310NE · Boeing 7272A7 · Engine Fuel Pump
  > AFTER TAKEOFF FROM BDL, NR 2 ENGINE COMPRESSOR STALLED AND FAILED. ACCOMPLISHED APPROPRIATE TWO ENGINE OPERATING CHECKLIST. FLIGHT CONTINUED TO DESTINATION BOS. REMOVED AND REPLACED ENGINE FUEL PUMP IAW PRATT AND WHITNEY MM 73-11-1. OPS LEAK CHECK GOOD IAW
- [SDR EISA97224](https://openairdocs.org/sdr/EISA97224.md): Switch · failed · Nov 15, 1997 · N310NE · Boeing 7272A7 · Leading Edge Slat Position Indicating System
  > DURING CRUISE AT FLT 370, THE L/E FLAPS LGHT ON THE PILOT PANEL ILLUMINATED. POSITION TEST INDICATED AMBER IN TRANSIT LIGHT OR, NR 3 L/E FLAP. PERFORMED EMERGENCY CHECK LIST. L/E FLAP NR 3 REMAINED IN TRANSIT. REMOVED AND REPLACED NR 3 FLAP POSITION SWITCH
- [SDR EISA97205](https://openairdocs.org/sdr/EISA97205.md): Oil Cooler · failed · Oct 9, 1997 · N310NE · Boeing 7272A7 · Engine Oil Cooler
  > NR 2 ENGINE OIL TEMPERATURE IN YELLOW ARC. PRECAUTIONARY SHUT DOWN PER MANUAL. REMOVED AND REPLACED OIL COOLER. (X)
- [SDR EISA97114](https://openairdocs.org/sdr/EISA97114.md): Connector · dirty · Jun 10, 1997 · N310NE · Boeing 7272A7 · Fire Detection
  > WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. CLEANED LOOP CONNECTOR, OPS CHECK GOOD. (M)
- [SDR EISA97111](https://openairdocs.org/sdr/EISA97111.md): Connector · dirty · Jun 7, 1997 · N310NE · Boeing 7272A7 · Fire Detection
  > WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON DURING PUSHBACK EMERGENCY SHUT DOWN PROCEDURES. CLEANED CONNECTORS WITH CONTACT CLEANER AT RT W/W AREA, OPS CHECK C/W PER 26-10-0 OK. (M)
- [SDR EISA96119](https://openairdocs.org/sdr/EISA96119.md): Support Web · cracked · Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous Structure
  > FOUR EACH FLOOR SUPPORT WEBS CRACKED AT AFT BULKHEAD LBL 40 TO RBL 35. FABRICATED AND INSTALLED NEW WEBS PER SRM 51-10-02 AND SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X)
- [SDR EISA96118](https://openairdocs.org/sdr/EISA96118.md): Floor Beam · corroded · Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Main, Floor Beam
  > FLOOR BEAM UNDER LAVATORY FLOOR IS CORRODED. REMOVED DAMAGED FLOOR STRINGER, FABRICATED AND INSTALLED NEW STRINGER PER SRM'S 51-40-04, 51-10-02, AND 51-20-01. TT: 66,991:57 HOURS. TC: 45,084. (X)
- [SDR EISA96117](https://openairdocs.org/sdr/EISA96117.md): Frame · cracked · Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Main, Frame
  > FUSELAGE FORGING AT STA 740 RT, BETWEEN STR 18R AND STR 19R, HAS CRACK EMANATING FROM PREVIOUS STOP DRILL HOLES. INSTALLED REPAIR PER SRM'S 51-30-2, 51-10-04, SB 53-0062 AND BOEING DRAWING 65C 15314.
- [SDR EISA96116](https://openairdocs.org/sdr/EISA96116.md): Actuator Bracket · cracked · Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge Slat Actuator
  > RIGHT WING NR 5 SLAT ACTUATOR ATTACH RIB BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-20-03. TT: 66,991:57 HOURS. TC: 45,084. (X)
- [SDR EISA96115](https://openairdocs.org/sdr/EISA96115.md): Angle · cracked · Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge Devices
  > LEFT WING NR 1 SLAT OUTBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. INSTALLED NEW ANGLE BRACKET PER SRM 51-10-1. TT: 66,991:57 HOURS. TC: 45,084. (X)
- [SDR EISA96114](https://openairdocs.org/sdr/EISA96114.md): Angle · cracked · Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge Devices
  > LEFT WING, NR 1 SLAT, INBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X)

Next page: https://openairdocs.org/model/boeing-727-2a7/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 = '7272A7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2a7/reports

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