# Service difficulty reports: Boeing 727-2J7

A list on [Boeing 727-2J7](https://openairdocs.org/model/boeing-727-2j7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 117 reports

- [SDR PCSA2009021801](https://openairdocs.org/sdr/PCSA2009021801.md): Smoke Detector · dirty · Feb 18, 2009 · N128NA · Boeing 7272J7 · Smoke Detection
  > CREW LOG ITEM, CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. BABY CHICKS WERE TRANSPORTED IN POSITIONS 3-7. MAINTENANCE CLEANED THE SMOKE DETECTORS FROM POSITION 2-7 AND THE SYSTEM TESTED NORMAL IAW THE MM. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR PCSA2009012801](https://openairdocs.org/sdr/PCSA2009012801.md): Smoke Detector · false activation · Jan 27, 2009 · N128NA · Boeing 7272J7 · Smoke Detection
  > CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT. MX REPLACED NR1 AND NR3 SMOKE DETECTORS.
- [SDR PCSA2009012701](https://openairdocs.org/sdr/PCSA2009012701.md): Smoke Warning · false activation · Dec 31, 2008 · N128NA · Boeing 7272J7 · Smoke Detection
  > CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, RAN ALL APPROPRIATE CHECKS, FALSE INDICATION, CONTINUED FLIGHT. MX PERFORMED AN OPS TEST OF THE SMOKE DETECTION SYS AND FOUND GOOD IAW THE MM.
- [SDR PCSA2008121801](https://openairdocs.org/sdr/PCSA2008121801.md): Smoke Detector · dirty · Dec 18, 2008 · N128NA · Boeing 7272J7 · Smoke Detection
  > ON DESCENT, MAIN CABIN SMOKE DETECTOR LIGHT ILLUMINATED. NO EVIDENCE OF SMOKE DISCOVERED. MX DISCOVERED NR 1 SMOKE DETECTOR DIRTY. THE DETECTOR WAS CLEANED AND THE SYS TESTED NORMAL.
- [SDR PCSA2008103101](https://openairdocs.org/sdr/PCSA2008103101.md): Garlock Seal · leaking · Oct 31, 2008 · Boeing 7272J7 · Turbine Engine Oil System
  > ENGINE 2 OIL TEMPERATURE RED BAND INDICATION, OIL QUANTITY NORMAL 3 GALLONS, ENGINE INSTRUMENT PARAMETERS NORMAL. ENGINE SHUT DOWN PER ALTERNATE AND ABNORMAL PROCEDURES. WINDMILL AFTER SHUTDOWN 20 MINUTES, OIL PRESSURE 15 PSI. DIVERTED TO SDQ AND PERFORMED
- [SDR 2008040101](https://openairdocs.org/sdr/2008040101.md): Warning System · malfunctioned · Apr 1, 2008 · N128NA · Boeing 7272J7 · Smoke Detection
  > AMERIJET FLIGHT 8110 FROM TSSJ TO KMIA - MAIN CARGO COMPARTMENT SMOKE WARNING CAME ON IN CRUISE FLIGHT. VISUALLY CHECKED FALSE WARNING. ON ARRIVAL KMIA THE MAIN CARGO SMOKE DETECTION SYSTEM WAS OPERATIONALLY TESTED AND NO DEFECTS WERE FOUND.
- [SDR C7WA200400082](https://openairdocs.org/sdr/C7WA200400082.md): Switch · intermittent · Mar 30, 2005 · N128NA · Boeing 7272J7 · Leading Edge Slat Position Indicating System
  > NR 2 KRUGER FLAP EXTEND LIGHT REMAINED ON AFTER TAKEOFF. REMOVED AND REPLACED NR 2 KRUGER FLAP SWITCH IAW MM.
- [SDR C7WA200400037](https://openairdocs.org/sdr/C7WA200400037.md): Skin · cracked · Jun 30, 2004 · N128NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED STRINGER 21 LEFT STATION 1233. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3. REPAIR DOUBLER, FABRICATED FROM 2024-T3,.080 BY 8 BY 7. (M)
- [SDR C7WA200400034](https://openairdocs.org/sdr/C7WA200400034.md): Hinge · cracked · Jun 30, 2004 · N128NA · Boeing 7272J7 · Cargo/Baggage Doors
  > FOUND MAIN CARGO DOOR UPPER AFT HINGE SECTION CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AEI MM CHAPTER 52 PAGE 15. (M)
- [SDR C7WA200400035](https://openairdocs.org/sdr/C7WA200400035.md): Skin · corroded · Jun 30, 2004 · N128NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CORRODED STRINGER 27 RIGHT STATION 500. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 6. REPAIR DOUBLER FABRICATED FRAME 2024-T3,.050 BY 31.25 BY 18. (M)
- [SDR C7WA200400036](https://openairdocs.org/sdr/C7WA200400036.md): Skin · corroded · Jun 30, 2004 · N128NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CORRODED STRINGER 17 LT STATION 1183. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3A. REPAIR DOUBLER FABRICATED FROM 2024-T3,.080 BY 17 BY 11.80. (M)
- [SDR C7WA200400033](https://openairdocs.org/sdr/C7WA200400033.md): Pcu · leaking · Jun 5, 2004 · N128NA · Boeing 7272J7 · Elevator Control System
  > IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT.6 GALLONS. FOUND LT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LT ELEVATOR PCU IAW MM. OPS AND LEAK CHECK GOOD.
- [SDR C7WA200400049](https://openairdocs.org/sdr/C7WA200400049.md): Pcu · leaking · Jun 5, 2004 · N128NA · Boeing 7272J7 · Elevator Control System
  > IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT.6 GALLONS. FOUND LEFT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LEFT ELEVATOR PCU IAW B727 MM 27-30-81, OPS AND LEAK CHECK GOOD. (M
- [SDR C7WA200300049](https://openairdocs.org/sdr/C7WA200300049.md): Pin · broken · Nov 14, 2003 · N128NA · Boeing 7272J7 · Power Indicating System
  > REJECTED TAKEOFF, NR 3 EPR UNRELIABLE AT TAKEOFF POWER READS LOW. SEEMS TO READ NORMAL AT CRUISE POWER. FOUND WIRE NOT CONNECTED TO PIN NR 3 AT EPR GAUGE CANNON PLUG. INSTALLED NEW PIN AND RECONNECTED WIRE IAW WIRING STANDARD PRACTICE CH 20 EPR READS NORMAL
- [SDR C7WA200200042](https://openairdocs.org/sdr/C7WA200200042.md): Line · leaking · Mar 28, 2003 · N128NA · Boeing 7272J7 · Hydraulic System, Main
  > LOST SYSTEM A HYDRAULIC. ENGINE NR 1 PUMP LOW PRESSURE LIGHT FOLLOWED BY FLUID LOSS IN FLIGHT. REMOVED AND REPLACED TWO EACH HYDRAULIC LINES, P/N 65-17844-250 AND 65-17844-17, LEAK CHECK GOOD. (M)
- [SDR C7WA200200041](https://openairdocs.org/sdr/C7WA200200041.md): Control Panel · shorted · Mar 14, 2003 · N128NA · Boeing 7272J7 · Autopilot System
  > WHEN ENGAGING AUTOPILOT, CRUISE STABILIZER TRIMS TO THE FULL NOSE DOWN POSITION. WITH AUTOPILOT DISCONNECTED, AFTER LEVEL OFF AT FL350, AN ELECTRICAL OVERHEAT ODOR STARTED TO FILL THE COCKPIT. CHECKLIST PERFORMED, ODOR STOPPED. REMOVED AND REPLACED RIGHT EL
- [SDR C7WA200200031](https://openairdocs.org/sdr/C7WA200200031.md): Connector · broken · Oct 16, 2002 · N128NA · Boeing 7272J7 · Air Data Computer
  > DURING FLIGHT, THE NR 1 ALTIMETER FLAG CAME IN VIEW AND STAYED. DIVERTED FLIGHT TO YIP. FOUND PIN 16 ON TOP PLUG OF AIR DATA COMPUTER BROKE. REPAIRED WIRE IAW MM CHAPTER 20. PERFORMED BITE TEST IAW MM 34-12-0 IAW BOEING MM 34-12-0. REF C7WA200200030 - AIR
- [SDR C7WA200200030](https://openairdocs.org/sdr/C7WA200200030.md): Adc · failed · Oct 16, 2002 · N128NA · Boeing 7272J7 · Air Data Computer
  > AIRCRAFT DEPARTED YIP AT 23:52Z AND HAD AIR DATA INSTRUMENT FAILURE CLIMBING THRU 5000FT. AIRCRAFT RETURNED TO YIP AND MADE OVERWEIGHT LANDING.
- [SDR C7WA20020029](https://openairdocs.org/sdr/C7WA20020029.md): Pitot Tube · obstructed · Oct 15, 2002 · N128NA · Boeing 7272J7 · Pitot/Static System
  > REJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND FOUND INSPECT BLOCKAGE FROM FIRST OFFICERS PITOT TUBE. REMOVED BLOCKAGE CHECKED SYSTEM IAW MM 34-11-31. (M)
- [SDR C7WA200200029](https://openairdocs.org/sdr/C7WA200200029.md): Pitot Tube · obstructed · Oct 15, 2002 · N128NA · Boeing 7272J7 · Pitot/Static System
  > REJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND REMOVED INSECT BLOCKAGE FROM F/O PITOT SYSTEM IAW MM 34-11-31.
- [SDR COOSDR020214](https://openairdocs.org/sdr/COOSDR020214.md): Structure · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Ailerons
  > RIGHT WING, OUTBOARD AILERON TRAILING EDGE (PN 65-21766-66)(SN BN-26) WITH DELAMINATION.
- [SDR COOSDR020210](https://openairdocs.org/sdr/COOSDR020210.md): Skin · corroded · Jul 1, 2002 · N128NA · Boeing 7272J7 · Trailing Edge Flaps
  > LEFT WING, OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN120) UPPER SKIN AND HONEYCOMB CORE SECTION CORRODED.
- [SDR COOSDR020209](https://openairdocs.org/sdr/COOSDR020209.md): Skin · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > LEFT WING SPOILER NR 7 (PN 65-17348-74) (SN 7888K) LOWER SKIN WITH DELAMINATION.
- [SDR COOSDR020208](https://openairdocs.org/sdr/COOSDR020208.md): Skin · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > RIGHT WING SPOILER NR 9 (PN 65-17348-74) (SN 9087K) LOWER SKIN WITH DELAMINATION.
- [SDR COOSDR020207](https://openairdocs.org/sdr/COOSDR020207.md): Structure · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Aileron Tabs
  > LEFT WING, OUTBOARD AILERON TAB (PN 65-21726-33) TMC 189 WITH DELAMINATION.
- [SDR COOSDR020206](https://openairdocs.org/sdr/COOSDR020206.md): Skin · corroded · Jul 1, 2002 · N128NA · Boeing 7272J7 · Trailing Edge Flaps
  > LEFT WING, INBOARD AFT FLAP (PN 65-21634-79)(SN BN147) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR02205](https://openairdocs.org/sdr/COOSDR02205.md): Skin · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > LEFT WING, SPOILER NR 5, (PN 65-17348-75), (SN 1781P) WITH DELAMINATION AT UPPER SKIN AND LOWER SKIN.
- [SDR COOSDR02204](https://openairdocs.org/sdr/COOSDR02204.md): Skin · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > LEFT WING, SPOILER NR 4, (PN 65-17347-42), (SN TC-248) WITH DELAMINATION AT UPPER SKIN.
- [SDR COOSDR020203](https://openairdocs.org/sdr/COOSDR020203.md): Panel · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Wing Main, Frame Structure
  > RIGHT WING, TRAINLING EDGE - LOWER FIX PANEL (PN 65216522) DELAMINATED.
- [SDR COOSDR020202](https://openairdocs.org/sdr/COOSDR020202.md): Structure · corroded · Jul 1, 2002 · N128NA · Boeing 7272J7 · Trailing Edge Flaps
  > RIGHT WING, INBOARD AFT FLAP (PN 65-21634-92) (SN BN480) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR02200](https://openairdocs.org/sdr/COOSDR02200.md): Panel · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Wing, Plate/Skin
  > RIGHT WING, TRAILING EDGE - LOWER PANEL (PN 6521652616) DELAMINATED.
- [SDR COOSDR02197](https://openairdocs.org/sdr/COOSDR02197.md): Panel · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Wing, Plate/Skin
  > RIGHT WING, TRAILING EDGE-UPPER PANEL (PN 6521657242) DELAMINATED.
- [SDR COOSDR02196](https://openairdocs.org/sdr/COOSDR02196.md): Structure · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > RIGHT WING, SPOILER NR 14, (PN 651734757), SN 9126S WITH DELAMINATION.
- [SDR COOSDR02195](https://openairdocs.org/sdr/COOSDR02195.md): Structure · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > RIGHT WING, SPOILER NR 8 (PN 651734866A) WITH DELAMINATION.
- [SDR COOSDR02194](https://openairdocs.org/sdr/COOSDR02194.md): Structure · delaminated · Jul 1, 2002 · N128NA · Boeing 7272J7 · Spoilers
  > RIGHT WING, SPOILER NR 10, PN 65-17348-75, SN 4268H WITH DELAMINATION.
- [SDR COOSDR02193](https://openairdocs.org/sdr/COOSDR02193.md): Angle · cracked · Jul 1, 2002 · N128NA · Boeing 7272J7 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR (PER STC NO SA1797SO) UPPER JAMB, FORWARD AND AFT CORNER ANGLE CRACKED.
- [SDR 2001F00272](https://openairdocs.org/sdr/2001F00272.md): Control Valve · failed · Jul 23, 2001 · N553NA · Boeing 7272J7 · Compressor Bleed Valve
  > ON FLT 748 - FPO-CVG - TAKEOFF ROLL, NR 2 ENGINE STALLED DURING ACCELERATION THROUGH 70 KTS. PARAMETERS WERE OBSERVED TO RECOVER TO NORMAL. HOWEVER, NR 2 ENGINE ACCESS DOOR LIGHT ILLUMINATED, TAKEOFF ABORTED. REMOVED AND REPLACED NR 2 PRBC VALVE, OPERATION
- [SDR 2001F00271](https://openairdocs.org/sdr/2001F00271.md): Latch · broken · Jul 23, 2001 · N553NA · Boeing 7272J7 · Engine Cowling System
  > FLT 1 - FLL - ON DEPARTURE CLIMB-OUT, NR 2 ENGINE ACCESS DOOR ILLUMINATED. AIRCRAFT RETURNED TO FLL. INSPECTED AND FOUND BROKEN LATCH ON NR 2 ENGINE ACCESS DOOR. REMOVED AND REPLACED LATCH ASSEMBLY PER MM 71-10-00. OPERATION CHECKED NORMAL. AIRCRAFT RETUR
- [SDR 20001120SH021](https://openairdocs.org/sdr/20001120SH021.md): Skin · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Wing, Plate/Skin
  > LOWER RIGHT CENTER WING SKIN, STA 830, RBL 10 ABOVE RIGHT SECONDARY HEAT EXCHANGER, AREA OF BLISTERING CORROSION, AFTER CORROSION REMOVAL, FOUND TO BE EXCEEDING SRM LIMITS (57-30-1 FIG 4). SERVICE ORDER NR 109003 OPS NR 21556. TIMCO RED NR S00316. FOUND DUR
- [SDR 20001120SH020](https://openairdocs.org/sdr/20001120SH020.md): Skin · cracked · Nov 20, 2000 · N129NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FASTENER HOLE CRACKED BS 250.60 BELOW STR 19R. SERVICE ORDER NR 109003 OPS NR 21920. TIMCO RED NR S00370. FOUND DURING C-CHECK. TIMCO OSODA NR T50R383Y. (X)
- [SDR 20001120SH019](https://openairdocs.org/sdr/20001120SH019.md): Skin · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAD A BULGE AT BS 1053 BETWEEN STR 26R AND STR 27R, STR 27R AFT END CORNER CRACKED IN RADIUS. SERVICE ORDER NR 109003. OPS NR 21098. RED NR S00320. CORROSION CAUSED CRACKS IN STRINGERS. FOUND DURING C-CHECK. TIMCO OSCODA NR T50R383
- [SDR 20001120SH018](https://openairdocs.org/sdr/20001120SH018.md): Spoiler · delaminated · Nov 20, 2000 · N129NA · Boeing 7272J7 · Spoilers
  > NR 10 SPOILER PANEL DELAMINATED UPPER SURFACE FORWARD INBOARD CORNER. SERVICE ORDER NR 109003 OPS TT 21,326 HOURS. TIMCO RED S00313. FOUND DURING C-CHECK. TIMCO OSCODA NR T50R383Y. (X)
- [SDR 20001120SH017](https://openairdocs.org/sdr/20001120SH017.md): Structure · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Fuselage Miscellaneous Structure
  > COCKPIT LEFT OUTBOARD CHORD CORRODED STA 252 LBL 52 WL 226. SERVICE ORDER NR 109003 OPS NR 21160. TIMCO RED NR S00327. FOUND DURING C-CHECK. TIMCO OSOCDA NR T50R383Y. (X)
- [SDR 20001120SH016](https://openairdocs.org/sdr/20001120SH016.md): Door Frame · cracked · Nov 20, 2000 · N129NA · Boeing 7272J7 · Fuselage Main, Structure
  > FORWARD CARGO DOOR CUT-OUT CRACKED, 0.50 INCH, LOWER AFT CORNER BETWEEN S25R AND S26R, BS 620.00. SERVICE ORDER NR 109003 OPS NR 21137. TIMCO RED NR S00328. FOUND DURING C-CHECK. TIMCO OSCODA NR T50R383Y. (X)
- [SDR 20001120SH015](https://openairdocs.org/sdr/20001120SH015.md): Skin · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Wing, Plate/Skin
  > CENTER WING SECTION STA 830, LOWER SKIN, LOWER SURFACE, CORROSION S-3C TO S-5C, LBL 27 TO LBL 32. CORROSION REMOVAL EXCEEDED SRM LIMITS. SERVICE ORDER NR 109003 OPS NR 20895. TIMCO RED NR S00311. FOUND DURING C-CHECK. TIMCO OSODA NR T50R383Y. (X)
- [SDR 20001120SH014](https://openairdocs.org/sdr/20001120SH014.md): Structure · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZERS - CENTER SECTION REAR SPAR UPPER FAILSAFE STRAP, CORROSION BLEND-OUT NEAR LEFT AND RIGHT STABILIZER STA 32.08 TOP SURFACE EXCEEDED CORROSION REMOVAL LIMITS. SERVICE ORDER NR 109003 OPS NR 20932 AND 20864 TIMCO RED NR S00330. FOUND DU
- [SDR 20001120SH013](https://openairdocs.org/sdr/20001120SH013.md): Flap Track · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Wing, Control Surface Attach Fittings
  > FOUND DURING C-CHECK, NR 4 AND NR 5 FLAP TRACK MOUNTING PAD MATING SURFACES/BOLT HOLES, CORRODED. SERVICE ORDER NR 109003 OPS NR 20507 AND 2062D TIMCO RED NR S00307. HOLE EXCEEDED THE LIMITS PER SB 727-57-0178 REV PARA B AND PARA H PART IV AND FIG 3, REF/B/.
- [SDR 20001120SH012](https://openairdocs.org/sdr/20001120SH012.md): Angle · corroded · Nov 20, 2000 · N129NA · Boeing 7272J7 · Fuselage Main, Structure
  > FOUND DURING C-CHECK, NOSE LANDING GEAR PRESSURE DECK CHORD ANGLE CORRODED, STA 342 RBL 13, VERTICAL LEG WL 180. REF: TIMCO OSCODA NR T50R383Y. SERVICE ORDER NR 109003. OPS NR 20645, RED-S00324. TIMCO OSCODA NR T50R383Y. (X)
- [SDR 2000ZZZM63](https://openairdocs.org/sdr/2000ZZZM63.md): Nr 3 Disk · failed · Nov 30, 1999 · N128NA · Boeing 7272J7 · Turbine Engine Compressor Section
  > FLT 312 - KCLT-KMIA - AFTER TAKEOFF EPR DECREASED AND EGT INCREASED. RETARDED THROTTLE TO CONTROL EGT WHEN VIBRATION WAS NOTICED AND EXPERIENCED COMPRESSOR STALL. WHEN THROTTLE RETURNED TO IDLE, EGT CONTINUED TO CLIMB. PERFORMED ENGINE INFLIGHT SHUTDOWN PRO
- [SDR 98ZZZM5](https://openairdocs.org/sdr/98ZZZM5.md): Air Distribution · odor · Nov 26, 1997 · N128NA · Boeing 7272J7 · Air Distribution System
  > FLT 230 - DTW-LRD - FLIGHT DIVERTED TO HDY, STRONG SMELL OF ELECTRICAL SMOKE. NO VISIBLE SMOKE, SEEMED TO BE AROUND FE PANEL. INSPECTED FE PANEL AND ADJACENT AREAS, P-6 PANEL, STAB TRIM C/B FOR ABNORMAL SMELL AND EXCESSIVELY HOT COMPONENTS. NONE FOUND. INS

Next page: https://openairdocs.org/model/boeing-727-2j7/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 = '7272J7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2j7/reports

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