# Service difficulty reports: Boeing 737-284

A list on [Boeing 737-284](https://openairdocs.org/model/boeing-737-284.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA021203009](https://openairdocs.org/sdr/CA021203009.md): Actuator · leaking · Nov 30, 2002 · Boeing 737284 · Leading Edge Slat Actuator
  > (CAN) AFTER LANDING, FLIGHT CREW REPORTED THE AIRCRAFT LOST ALL SYSTEM "A" HYDRAULIC PRESSURE AND THE FLUID QUANTITY INDICATION READ ZERO.MAINTENANCE INSPECTION REFEALED THE NR 1 GROUND SPOILER OUTBOARD ACTUATOR ASSEMBLY WAS LEAKING - ACTUATOR CASING CRACKED.
- [SDR AT0100200](https://openairdocs.org/sdr/AT0100200.md): Battery Pack · discharged · Jun 26, 2001 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND EMERGENCY LIGHT INOPERATIVE AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACKS AT M1051 AND M1053 IAW 737 MM 33-51-00.
- [SDR AT0100171](https://openairdocs.org/sdr/AT0100171.md): Socket · broken · May 15, 2001 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND EMERGENCY PATH LIGHT SOCKET BROKEN. REPLACED SOCKET IAW STANDARD WIRING PRACTICES.
- [SDR AT0100119](https://openairdocs.org/sdr/AT0100119.md): Skin · corroded · Mar 11, 2001 · N470AT · Boeing 737284 · Fuselage Main, Plate/Skin
  > FOUND AFT LAV SERVICE PANEL SKIN AT BS 976-1006 CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW B737 53-10-03 FIG 1 AND 53-10-02 FIG 9.
- [SDR AT0000489](https://openairdocs.org/sdr/AT0000489.md): Power Supply · inoperative · Dec 20, 2000 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND FORWARD EXTERNAL EMERGENCY LIGHTS CAME ON WHEN POWER WAS OFF AIRCRAFT AND EMERGENCY SWITCH WAS OFF. REPLACED BATTERY POWER SUPPLY UNIT. IAW B737 MM 33-50
- [SDR AT0000487](https://openairdocs.org/sdr/AT0000487.md): Smoke · detected · Dec 8, 2000 · N470AT · Boeing 737284 · Smoke Detection
  > CLIMBING THRU 110FL THE L1 CAME TO THE COCKPIT TO REPORT SMOKE IN THE CABIN. WE DELCARED AN EMERGENCY AND RETURNED TO ATL. INSPECTED OVERHEAD PSU'S, INCLUDING SEAT ROW 10 WHERE SMOKE WAS DETECTED. PERFORMED SYSTEM OPERATIONAL CHECK WITH BOTH ENGINES RUNNIN
- [SDR CA001122018](https://openairdocs.org/sdr/CA001122018.md): Stator · broken · Nov 7, 2000 · Boeing 737284 · Brake
  > (CAN) DURING THE SERVICE CHECK NR 3 BRAKE TENSION ADJUSTMENT PINS WERE FOUND LOOSE. WHEN CHECKED FURTHER ONE OF THE BRAKE STATORS HAD BROKEN AND THERE WERE MULTIPLE PIECES FOUND CONTAINED INSIDE THE WHEEL. NR 3 BRAKE WAS REPLACED AND NR 3 MAIN WHEEL ASSEMBLY D
- [SDR AT0000450](https://openairdocs.org/sdr/AT0000450.md): Insert · worn · Oct 21, 2000 · N470AT · Boeing 737284 · Turbine Engine Oil System
  > LOST OIL QUANTITY IN NR 1 ENGINE DURING CRUISE. INSTALLED NEW INSERT IN GEARBOX AT OIL PRESSURE DIFFERENTIAL LINE.
- [SDR AT0000422](https://openairdocs.org/sdr/AT0000422.md): Light · missing · Sep 26, 2000 · N470AT · Boeing 737284 · Emergency Lighting
  > DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND EMERGENCY PATH LIGHT STRIP MISSING AT ROW 10. REMOVED AND REPLACED EMERGENCY PATH LIGHT STRIP AND ASSEMBLY IAW MM 33-21-27.
- [SDR CA001016007](https://openairdocs.org/sdr/CA001016007.md): Indicator · split · Sep 21, 2000 · Boeing 737284 · Trailing Flap Position Indicating System
  > (CAN) ON APPROACH FLIGHT CREW WERE UNABLE TO EXTEND THE FLAPS PAST 5 UNITS DUE TO AN ASYMMETRY INDICATION. AN UNEVENTFUL FLAPS 5 LANDING WAS CARRIED OUT. MAINTENANCE INSPECTED THE TRAILING EDGE FLAPS WITH NO FAULTS FOUND. THE PROBLEM WAS TRACED TO THE INDICATO
- [SDR AT0000299](https://openairdocs.org/sdr/AT0000299.md): Light · inoperative · May 31, 2000 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW 737 MM 33-51-81.
- [SDR AT0000161](https://openairdocs.org/sdr/AT0000161.md): Battery Pack · discharged · Apr 1, 2000 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND FORWARD OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. CORRECTIVE ACTION: R&R BATTERY PACK. IAW B737 MM 3351.
- [SDR AT0000160](https://openairdocs.org/sdr/AT0000160.md): Lens · missing · Mar 28, 2000 · N470AT · Boeing 737284 · Emergency Lighting
  > FOUND EMERGENCY PATH LIGHTING TO HAVE ONLY TWO RED LIGHTS AT OVER WING EXIT. CORRECTIVE ACTION: INSTALLED 2 ADDITIONAL LIGHTS AT OVER WING EXIT. IAW 737 MM 33-50
- [SDR AT0000209](https://openairdocs.org/sdr/AT0000209.md): Plate · cracked · Mar 2, 2000 · N470AT · Boeing 737284 · Fuselage Miscellaneous Structure
  > FOUND FORWARD BAGGAGE SCUFF PLATE CRACKED. REMOVED SCUFF PLATE, TIG WELDED, AND INSTALLED SCUFF PLATE IAW EA PD37-53-034, 737 SRM 52-31-00, 51-30-01, AND 737 MM 12-31-1.
- [SDR AT0000130](https://openairdocs.org/sdr/AT0000130.md): Skin · dented · Feb 28, 2000 · N470AT · Boeing 737284 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE DENT AT BS 424 AND AT SKIN LAP STR 14R BEYOND.125 LIMITS. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW 737 SRM 53-30-03, 51-10-01, AND 51-30-02.
- [SDR AT0000131](https://openairdocs.org/sdr/AT0000131.md): Seat Track · corroded · Feb 27, 2000 · N470AT · Boeing 737284 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN FLOOR TRACK HAS PITTED CORROSION FROM BS 927 - 947. REMOVED CORROSION FROM CABIN FLOOR TRACK, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW 737 SRM 53-10-01, 51-30 -2, 51-30-5, 51-30-8, 51-10-2, 51-20-4, 51-10-1 PART 4.
- [SDR CA000301010](https://openairdocs.org/sdr/CA000301010.md): Window · cracked · Feb 14, 2000 · Boeing 737284 · Flight Compartment Windows
  > (CAN) DURING CRUISE CAPTAINS SLIDING WINDOW DELAMINATED AND CRACKED. WINDOW AND HEAT CONTROLLER REPLACED.
- [SDR CA000301009](https://openairdocs.org/sdr/CA000301009.md): Coffeemaker · overheated · Feb 11, 2000 · Boeing 737284 · Buffet/Galleys
  > (CAN) DURING CLIMB CREW REPORTED SMELL OF SMOKE IN BACK OF MAIN CABIN, A/C RETURNED. COFFEEMAKER OVERHEATED AND REPLACED.
- [SDR AT9900886](https://openairdocs.org/sdr/AT9900886.md): Wire · broken · Dec 10, 1999 · N470AT · Boeing 737284 · Light System Wiring
  > EMERGENCY PATH LIGHTING IN FORWARD CABIN INOPERATIVE. RE-SPLICED BROKEN WIRE UNDER E-PATH WIRE COVERS.
- [SDR CA991229060](https://openairdocs.org/sdr/CA991229060.md): Structure · cracked · Dec 1, 1999 · Boeing 737284 · Passenger/Crew Doors
  > (CAN) DURING INSP OF FWD ENTRY DOOR A CRACK WAS FOUND IN THE LOWER 1/3 OF DOOR NEAR DOOR CENTERLINE BETWEEN RIVETS. A/C FERRIED FOR REPAIR.
- [SDR AT9900465](https://openairdocs.org/sdr/AT9900465.md): Indicator · defective · Jun 26, 1999 · N470AT · Boeing 737284 · Fuel Flow Indicating
  > AT FLIGHT LEVEL 250 AT 1.6 ENGINE PRESSURE RATIO AT FUEL FLOW 3000 NR 2 ENGINE ROLLED BACK TO PLUS 500 FUEL FLOW, SHUT ENGINE DOWN AND AIR STARTED NORMALLY. RAN NORMAL TO LAND. REMOVED AND REPLACED NR 2 FUEL FLOW INDICATOR AND OPS CHECKED GOOD IAW MM 28-40.
- [SDR AT9900001](https://openairdocs.org/sdr/AT9900001.md): Wire · damaged · Jan 5, 1999 · N470AT · Boeing 737284 · Light System Wiring
  > DURING LAYOVER CHECK, FOUND EMERGENCY PATH LIGHTING AT ROW 10 DEF BROKEN. REPAIRED DAMAGED WIRES PER B737 STANDARD WIRING MANUAL 20-10-13.
- [SDR VJ9800612](https://openairdocs.org/sdr/VJ9800612.md): Boost Pump · malfunctioned · Nov 18, 1998 · N470AT · Boeing 737284 · Fuel Boost Pump
  > EN ROUTE, NR 2 TANK FUEL BOOST PUMP POPPED FWD AND AFT CIRCUIT BREAKER. FLIGHT CREW ELECTED TO DIVERT INTO MEM. SUMPED FUEL TANK AND NO WATER FOUND, REMOVED AND REPLACED FWD BOOST PUMP AT NR 2 TANK. LEAK CHECKED GOOD AND RAN ENGINES, FUEL SYSTEM CHECKED NOR
- [SDR VJ9800571](https://openairdocs.org/sdr/VJ9800571.md): Skin · corroded · Oct 12, 1998 · N470AT · Boeing 737284 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER STRINGER 27R AT STA 727-727A CORRODED. REMOVED CORROSION IAW SRM 53-30-1, TRIMMED OUT SKIN AND FABRICATED FILLER AND DOUBLER IAW B737 SRM 53-30-3. ALODINED, PRIMED AND INSTALLED REPAIR IAW B737 SRM 51-10-2, 51-20-11, 53-30-3 AND 51-30-2.
- [SDR VJ9800592](https://openairdocs.org/sdr/VJ9800592.md): Skin · corroded · Oct 9, 1998 · N470AT · Boeing 737284 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE I/B TAIL DOOR SKIN CORRODED. LOSS ON SKIN AT 3RD RIB FROM FWD PART OF COWL OUT OF LIMIT IAW B737 SRM 54-30-1. CUT OUT AND FABRICATED REPAIR DOUBLER, DRILLED, DEBURRED AND INSTALLED IAW B737 SRM 54-10-3. TREATED ALL BLENDED AREAS IAW B737 SRM 51-
- [SDR VJ9800537](https://openairdocs.org/sdr/VJ9800537.md): Bushing · corroded · Oct 6, 1998 · N470AT · Boeing 737284 · Trailing Edge Flaps
  > LT WING O/B FLAP I/B TRACK PITTED WITH CORROSION ON AFT SPAR MOUNT SURFACE AND I/B BOLT HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED NEW BUSHINGS AND SHIM IAW B737 SRM 51-10-6, MM 20-10-71 AND AIRTRAN EO 981765.
- [SDR VJ9800544](https://openairdocs.org/sdr/VJ9800544.md): Hinge · corroded · Sep 30, 1998 · N470AT · Boeing 737284 · Landing Gear Doors
  > TOP SIDE LT MLG DOOR HINGE CASTING CORRODED. REMOVED AND INSTALLED NEW CASTING, TRIMMED SKIN 2 INCHES, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW B737 SRM 51-30-2, 51-40-4, MM 32-13-11.
- [SDR VJ9800543](https://openairdocs.org/sdr/VJ9800543.md): Stringer · corroded · Sep 30, 1998 · N470AT · Boeing 737284 · Fuselage Main, Longeron/Stringer
  > RT BELLY SKIN HAS CORROSION BULGE BETWEEN FASTENERS AT BS 741, S28R. REMOVED AND REPLACED STRINGER S27R FROM BS 727-840 IAW B737 SRM 51-30-2, 51-10-1.
- [SDR VJ9800536](https://openairdocs.org/sdr/VJ9800536.md): Bulkhead Angle · cracked · Sep 29, 1998 · N470AT · Boeing 737284 · Fuselage Main, Bulkhead
  > ATTACH ANGLE VERTICAL LEG ON SHEAR BEAM AT BS 664, S18R CRACKED BETWEEN THREE FASTENERS AND SHEAR BEAM AT BS 664, S18AL CRACKED IN RADIUS AT BULKHEAD ATTACH POINT. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW B737 SB 53-1066, REPAIR KIT 65C29228-29. REMO
- [SDR VJ9800294](https://openairdocs.org/sdr/VJ9800294.md): Light · inoperative · Aug 25, 1998 · N470AT · Boeing 737284 · Emergency Lighting
  > L-2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED L-2 DOOR PORTABLE EMERGENCY LIGHT IAW BMM 33-51-101.
- [SDR ZZDA5228197](https://openairdocs.org/sdr/ZZDA5228197.md): Door · not latched · Dec 8, 1997 · N470AT · Boeing 737284 · Electrical/Electronic Compartment Doors
  > DURING CLIMB OUT OF FLT 930, CREW UNABLE TO PRESSURIZE THE AIRCRAFT. ALL DOOR LIGHTS CHECKED OUT EXTINGUISHED. ALL CHECK LISTS PERFORMED. EQUIPMENT DOOR ILLUMINATED, APPROXIMATELY 8,000 FEET. RETURNED TO MCO. PERFORMED LOW APPROACH AND SMOOTH SOFT LANDIN
- [SDR ZZDA5324397](https://openairdocs.org/sdr/ZZDA5324397.md): Skin · damaged · Oct 26, 1997 · N470AT · Boeing 737284 · Cargo/Baggage Doors
  > AFTER FLT NR 704 FROM MCO/DAY, THE FORWARD CARGO PIT DOOR WILL NOT OPEN. THE DOOR HANDLE WILL UNLOCK. THE MECHANIC AND A RAMP AGENT WERE ABLE TO OPEN THE DOOR ENOUGH TO MOVE THE BAGS OFF THE DOOR ALLOWING IT TO OPEN COMPLETELY. AFTER THE DOOR WAS OPEN, THE
- [SDR VSTA9609004](https://openairdocs.org/sdr/VSTA9609004.md): Power Supply · inoperative · Sep 23, 1996 · N310VA · Boeing 737284 · Engine Fuel Distribution
  > NO FUEL FLOW AND NR 2 ENGINES BAD POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY, OPS CHECKED GOOD.
- [SDR 96ZZZX4710](https://openairdocs.org/sdr/96ZZZX4710.md): Fitting · corroded · Aug 22, 1996 · N310VA · Boeing 737284 · Leading Edge Slat Actuator
  > DURING SB INSPECTION OF NR 1 AND NR 5 LEADING EDGE SLAT ACTUATOR SUPPORT FITTINGS, FITTINGS WERE REMOVED TO REPLACE ATTACH HARDWARE. CORROSION WAS FOUND AT BOTH POSITIONS SEVERE ENOUGH TO REQUIRE REPAIR. SUBSEQUENT INSPECTION UNDER REMAINING FITTINGS REVEALE
- [SDR VSTA9602002](https://openairdocs.org/sdr/VSTA9602002.md): Switch · failed · Feb 22, 1996 · N310VA · Boeing 737284 · Engine Cranking
  > NR 1 ENGINE WOULD NOT START. FOUND BAD SWITCH IN THROTTLE QUAD. REMOVED AND REPLACED START SWITCH IN QUAD.
- [SDR 96ZZZX3287](https://openairdocs.org/sdr/96ZZZX3287.md): Fitting · cracked · Sep 28, 1995 · N310VA · Boeing 737284 · Rudder Structure
  > TUS - MAINTENANCE REPORT OF RUDDER ATTACH POINT WEB ASSEMBLY BEING CRACKED UPON INSPECTION FOR RUDDER INSTALLATION (RUDDER ATTACH POINT NR 2). UPON INSPECTION, FOUND MAINTENANCE PROCEDURES FOR REMOVAL OF RUDDER WERE NOT STRICTLY ADHERED TO. THE REMOVAL CALLS
- [SDR 96ZZZX327](https://openairdocs.org/sdr/96ZZZX327.md): Fitting · cracked · Sep 28, 1995 · N310VA · Boeing 737284 · Rudder Structure
  > ON AM OF SEPTEMBER 28, 1995, MX REPORT OF RUDDER ATTACH POINT WEB ASSY BEING CRACKED UPON INSPECTION FOR RUDDER INSTALLATION. (RUDDER ATTACH POINT NR 2). UPON FURTHER INVESTIGATION, FOUND MX PROCEDURES FOR REMOVAL OF RUDDER WERE NOT STRICTLY ADHERED TO. THE

## 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 = '737284'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-284/reports

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