# Service difficulty reports: Boeing 737-282

A list on [Boeing 737-282](https://openairdocs.org/model/boeing-737-282.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 303 reports

- [SDR TSAA0821016](https://openairdocs.org/sdr/TSAA0821016.md): Fan · failed · Mar 13, 2008 · N824AL · Boeing 737282 · Air Distribution Fan
  > FLIGHT 93 OGG - HNL - THE CREW NOTED AN UNPLEASANT BURNING ODOR IN THE CABIN DURING FLIGHT WITH NO SMOKE PRESENT. THE ODOR DECREASED WITH ENGINES AT LOWER THROTTLE SETTINGS. THE AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLAC
- [SDR TSAA0853003](https://openairdocs.org/sdr/TSAA0853003.md): Bulkhead · cracked · Jan 8, 2008 · N824AL · Boeing 737282 · Fuselage Main, Bulkhead
  > WHILE PERFORMING ECO 1822 PART I (REFERENCE AD 93-08-08 AND AD 90-06-02) A CRACK WAS DISCOVERED ON THE LT BULKHEAD BS 1156 ALONG THE LAST ROW OF RIVETS APPROX WL 272-275. REPAIRED CRACK IN ACCORDANCE WITH ECO 1822 PART II (S/B 737-53-1-86 R3).
- [SDR TSAA0721046](https://openairdocs.org/sdr/TSAA0721046.md): Sensor · failed · Aug 15, 2007 · N824AL · Boeing 737282 · Cabin Temperature Control System
  > NON-ETOPS FLIGHT 63 HNL-LIH, DURING CLIMB, THE CREW NOTED LOUD NOISE AND ICE EMANATING FROM THE AIR CONDITIONING SYSTEM. THE CREW ATTEMPTED TO CONTROL THE NOISE AND ICE BY SELECTING A WARMER TEMPERATURE WITH NO CHANGE IN CONDITION. THE NOISE WAS DISRUPTIVE T
- [SDR TSAA0675112](https://openairdocs.org/sdr/TSAA0675112.md): Control Valve · failed · Nov 24, 2006 · N824AL · Boeing 737282 · Engine Bleed Air System
  > FLT 206 HNL-OGG: DURING TAKEOFF ROLL, NR 1 ENGINE EPR WOULD NOT INCREASE ABOVE 1.53 WITH MORE THAN A TWO THROTTLE KNOB WIDTH SPLIT AND EGT RISING TO 580 DEGREES. NR 2 ENGINE STABILIZED AT 1.89 EPR AND EGT AROUND 530 DEGREES. TAKEOFF WAS ABORTED AROUND 80 KNO
- [SDR TSAA0632094](https://openairdocs.org/sdr/TSAA0632094.md): Uplock · dirty · Nov 2, 2006 · N824AL · Boeing 737282 · Landing Gear Position and Warning
  > AFTER TAKEOFF, THE RT MLG DID NOT RETRACT. CREW CYCLED THE LANDING GEAR LEVER AND WAS ABLE TO RETRACT THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE RT MLG UPLOCK SENSOR AND PERFORMED THE MAIN LANDING GEAR EXTENSION AND RETR
- [SDR TSAA0672088](https://openairdocs.org/sdr/TSAA0672088.md): Nose Bullet · loose · Oct 16, 2006 · N824AL · Boeing 737282 · Engine (Turbine/Turboprop)
  > NON-ETOPS FLT 281: CLIMBING THRU 16,000 FEET WITH THE ENGINE ANTI-ICE ON, THE CREW HEARD A LOUD BANGING SOUND COMING FROM THE LT SIDE OF THE AIRCRAFT. ENGINE INDICATIONS WERE NORMAL. THE CREW RETARDED THE NR 1 ENGINE THRUST LEVER AND THE BANGING STOPPED. T
- [SDR TSAA0629060](https://openairdocs.org/sdr/TSAA0629060.md): Hose · failed · Jul 28, 2006 · N824AL · Boeing 737282 · Hydraulic System, Main
  > NON-ETOPS FLT 77 ITO-HNL: DURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED SYSTEM ‘A’ HYDRAULIC FAILURE. THE CREW BROUGHT THE AIRCRAFT TO A STOP, NOTIFIED TOWER, AND PERFORMED THEIR QRH CHECK LIST. THE AIRCRAFT WAS TOWED BY MAINTENANCE TO THE GATE. R & R NO
- [SDR TSAA0652044](https://openairdocs.org/sdr/TSAA0652044.md): Slide · out of position · Jun 6, 2006 · N824AL · Boeing 737282 · Escape Slide
  > NON-ETOPS: FLT 206 HNL - OGG: ON THE GROUND, FWD SVC DOOR EMERGENCY SLIDE ACCIDENTALLY DISLODGED FROM THE DOOR BUT DID NOT INFLATE. REMOVED AND REPLACED FORWARD SERVICE DOOR SLIDE CHUTE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0653002](https://openairdocs.org/sdr/TSAA0653002.md): Skin Panel · cracked · Jan 5, 2006 · N824AL · Boeing 737282 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK LOWER BL-0, BETWEEN S-28L AND R AT BS 370. TWO 1/2 INCH FUSELAGE SKIN CRACKS LOWER BL-0, BETWEEN S-28L AND R AT BS370 AND BS380. MAINTENANCE REPAIRED WITH APPROXIMATELY 40" X 20" SKIN PATCH, FABRICATED DOUBLER)1002024-T3). REPAIR COMPLE
- [SDR BJNA051202](https://openairdocs.org/sdr/BJNA051202.md): Power Supply · inoperative · Dec 7, 2005 · N789TM · Boeing 737282 · Emergency Lighting
  > LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT, INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. (K)
- [SDR BJNA051201](https://openairdocs.org/sdr/BJNA051201.md): Connector · dirty · Dec 2, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ILLUMINATED 2 TIMES ON DESCENT. CLEANED THE CONNECTORS ON THE COCKPIT REMOVABLE EMERGENCY EXIT LIGHT, SYSTEM CHECKS NORMAL. (K)
- [SDR TSAA0532055](https://openairdocs.org/sdr/TSAA0532055.md): Tire · failed · Nov 11, 2005 · N824AL · Boeing 737282 · Tire
  > DURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE FOUND HOLE IN LT NOSEWHEEL AND BOTH TIRES FLAT. REMOVED AND REPLACED BOTH NOSEWHEEL TIRES, INSPE
- [SDR BJNA051101](https://openairdocs.org/sdr/BJNA051101.md): Landing Gear · unknown · Nov 9, 2005 · N233TM · Boeing 737282 · Main Landing Gear
  > AFTER TAKEOFF, RETRACTED LANDING GEAR AND 3 RED LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GEAR DOWN AND UP, 3 GREEN LIGHTS WHEN DOWN, 3 RED LIGHTS WHEN UP. LANDED WITH 3 GREEN LIGHTS. PERFORMED LANDING GEAR ACCY MODULE TEST IAW AMM, COULD NOT DUPLICATE ON
- [SDR TSAA0532050](https://openairdocs.org/sdr/TSAA0532050.md): Anti-Skid Sys · deactivated · Oct 20, 2005 · N824AL · Boeing 737282 · Brake Anti-Skid Section
  > ON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED.
- [SDR BJNA050301](https://openairdocs.org/sdr/BJNA050301.md): Battery Pack · discharged · Mar 16, 2005 · N233TM · Boeing 737282 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE RIGHT OVERWING EXIT LIGHT BATTERY IAW 33-51-21. (M)
- [SDR BJNA050203](https://openairdocs.org/sdr/BJNA050203.md): Battery Pack · discharged · Feb 27, 2005 · N233TM · Boeing 737282 · Emergency Equipment
  > CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M)
- [SDR TSAA0552009](https://openairdocs.org/sdr/TSAA0552009.md): Warning Light · false indication · Feb 25, 2005 · N824AL · Boeing 737282 · Door Warning System
  > FLT 211, OGG-HNL, FORWARD CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KTS. RETURNED TO GATE. MAINTENANCE OPENED AND CLOSED THE FORWARD CARGO DOOR AND CHECKED LOCKS FOR SECURITY. OPS CHECK OK AND LIGHTS CHECK GOOD. IN HNL, FWD
- [SDR BJNA05022](https://openairdocs.org/sdr/BJNA05022.md): Light · inoperative · Feb 14, 2005 · N789TM · Boeing 737282 · Emergency Lighting
  > FORWARD CABIN FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED SECTION OF TRACK LIGHTING, OPERATIONAL CHECKS OK. (M)
- [SDR BJNA05021](https://openairdocs.org/sdr/BJNA05021.md): Engine · failed · Feb 11, 2005 · N344TM · Boeing 737282 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. ENGINE TOTAL TIME 550207, TOTAL CYCLES 52176. SINCE
- [SDR BJNA050104](https://openairdocs.org/sdr/BJNA050104.md): Battery Pack · discharged · Feb 2, 2005 · N233TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE AFT RT SERVICE DOOR (R2) EMERGENCY EXIT ESCAPE SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REOMVED AND REPLACED THE BATTERY PACK FOR THE AFT RT SERVICE DOOR (R2 EMERGENCY EXIT SLIDE LIGHT IAW MM. EMERGENCY EXIT L
- [SDR BJNA050103](https://openairdocs.org/sdr/BJNA050103.md): Line · leaking · Jan 26, 2005 · N344TM · Boeing 737282 · Turbine Engine Oil System
  > NR 1 ENGINE LOST ENGINE OIL QUANTITY AND ILLUMINATED THE LOW OIL PRESSURE LIGHT. ENGINE WAS SHUTDOWN AND WIND MILLED APPROX 20 MIN. INSPECTION FOUND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED AND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH LINE LEA
- [SDR BJNA050102](https://openairdocs.org/sdr/BJNA050102.md): Battery Pack · discharged · Jan 21, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOR ILLUMINATE. MAINTENANCE DISCOVERED THAT THE BATTERIES WERE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIG
- [SDR TSAA0527002](https://openairdocs.org/sdr/TSAA0527002.md): Sensor · defective · Jan 16, 2005 · N824AL · Boeing 737282 · Leading Edge Slat Position Indicating System
  > FLT 278, HNL-KOA: ON INITIAL TAKEOFF ROLL, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED (NR 4 SLAT) WITH THE CONFIGURATION WARNING HORN. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP EXTEND SENSOR. OPS CHECK OK PER
- [SDR 2005F00029](https://openairdocs.org/sdr/2005F00029.md): Stringer · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > IG CORROSION ON SRTINGER 27L AT STATION 950 LBL5)LEVEL2)
- [SDR 2005F00028](https://openairdocs.org/sdr/2005F00028.md): Stringer · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > STRINGER 23L AT STA 950 BL 10L HAS IG CORROSION(LEV. 2)
- [SDR 2005F00027](https://openairdocs.org/sdr/2005F00027.md): Frame · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Frame
  > IG CORROSION ON FRAME AT BS 285 FROM STRINGER 24L TO STR 28L.
- [SDR 2005F00026](https://openairdocs.org/sdr/2005F00026.md): Support Bracket · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings
  > SUPPORT BRACKET FOR NOSE STEERING BRACKET PULLEYS AT BS 289 STRINGER 26 L AND 27L --IG CIRROSION (LEVEL 2)
- [SDR 2005F00025](https://openairdocs.org/sdr/2005F00025.md): Stringer Clip · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings
  > STRINGER TIES AT STA 947, STR.26L AND 27L -IG CORROSION (LEVEL 2).
- [SDR 2005F00015](https://openairdocs.org/sdr/2005F00015.md): Bracket · corroded · Jan 10, 2005 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings
  > BRACKET AT STA 950 LBL 15 HAS IG CORROSION (LEVEL 2).
- [SDR BJNA050101](https://openairdocs.org/sdr/BJNA050101.md): Bulb · burned out · Jan 8, 2005 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIGHT NOW FUNCTIONS NORMALLY. (K)
- [SDR TSAA0434084](https://openairdocs.org/sdr/TSAA0434084.md): Indicator · inoperative · Dec 22, 2004 · N824AL · Boeing 737282 · Airspeed/Mach Indicator
  > FLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE.
- [SDR BJNA041201](https://openairdocs.org/sdr/BJNA041201.md): Battery Pack · discharged · Dec 15, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > DURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT BATTERY PACK IAW MM. EMERGENCY EXIT LIGHTS NO OPERATE NORMALLY. (K)
- [SDR BJNA041106](https://openairdocs.org/sdr/BJNA041106.md): Bracket · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A BRACKET LOCATED AT STATION 950 LBL 15. REMOVED AND REPLACED CORRODED BRACKET LOCATED AT STATION 950 LBL 15. BRACKET WAS FABRICATED FROM 7075-T6.050. WORK DONE IAW BOEING SRM 51-
- [SDR BJNA041105](https://openairdocs.org/sdr/BJNA041105.md): Stringer Clip · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER TIES AT STATION 967 STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED CORRODED STRINGER TIES OF STRINGER 26L AND STRINGER 27L AT STATION 967. STRINGER TIES WERE FABRICATE
- [SDR BJNA041103](https://openairdocs.org/sdr/BJNA041103.md): Frame · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Frame
  > DURING A SCHEDULED C CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A FRAME RIB AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. CUTOUT CORRODED AREA OF FRAME AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. FABRICATED FILLER AND DOUBLER USING 707
- [SDR BJNA041107](https://openairdocs.org/sdr/BJNA041107.md): Stringer Clip · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Attach Fittings
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON TWO STRINGER TIE OF STRINGER 26L LOCATED AT STATION 947. REMOVED AND REPLACED CORRODED STRINGER TIE OF STRINGERS 26L AT STATION 947. STRINGER TIES WERE FABRICATED FROM 7075-T6.063.
- [SDR BJNA041104](https://openairdocs.org/sdr/BJNA041104.md): Stringer · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 27L AT STATION 950 LBL 5. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 27L AT STATION 950 LBL 5 IAW BOEING SRM CHAPTER 53-10-3. (M)
- [SDR BJNA041101](https://openairdocs.org/sdr/BJNA041101.md): Support Bracket · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Leading Edge Devices
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKET ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO LEADING EDGE SLAT ACT
- [SDR BJNA041102](https://openairdocs.org/sdr/BJNA041102.md): Stringer · corroded · Nov 28, 2004 · N233TM · Boeing 737282 · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 26L STATION 950 BL 10L. REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER 26L AT STATION 950 BL 10L IAW BOEING SRM 53-10-3. (M)
- [SDR BJNA041004](https://openairdocs.org/sdr/BJNA041004.md): Light · inoperative · Oct 12, 2004 · N233TM · Boeing 737282 · Emergency Lighting
  > AFT EMERGENCY TRACK LIGHT AND BOTTOM AFT EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW CMM 33-50-01. OPERATIONAL CHECK OK.
- [SDR BJNA041003](https://openairdocs.org/sdr/BJNA041003.md): Bulb · burned out · Oct 10, 2004 · N344TM · Boeing 737282 · Emergency Lighting
  > LT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AND CLEANED SOCKET IAW AMM 33-51-101.
- [SDR BJNA041001](https://openairdocs.org/sdr/BJNA041001.md): Battery Pack · discharged · Oct 5, 2004 · N233TM · Boeing 737282 · Emergency Lighting
  > LT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD.
- [SDR BJNA041002](https://openairdocs.org/sdr/BJNA041002.md): Battery Pack · discharged · Oct 5, 2004 · N233TM · Boeing 737282 · Emergency Lighting
  > RT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD.
- [SDR BJNA040906](https://openairdocs.org/sdr/BJNA040906.md): Battery Pack · inoperative · Sep 19, 2004 · N233TM · Boeing 737282 · Emergency Lighting
  > FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M)
- [SDR BJNA040905](https://openairdocs.org/sdr/BJNA040905.md): Battery Pack · inoperative · Sep 19, 2004 · N233TM · Boeing 737282 · Emergency Lighting
  > FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M)
- [SDR BJNA040904](https://openairdocs.org/sdr/BJNA040904.md): Battery Pack · inoperative · Sep 19, 2004 · N344TM · Boeing 737282 · Emergency Equipment
  > FOUND CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M)
- [SDR BJNA040907](https://openairdocs.org/sdr/BJNA040907.md): Skin · damaged · Sep 18, 2004 · N789TM · Boeing 737282 · Trailing Edge Flaps
  > FOUND THE LEFT INBOARD FORE FLAP TRAILING EDGE DAMAGED FROM POSSIBLE FOD. REMOVED AND REPLACED THE LEFT INBOARD FORE FLAP IAW THE AMM 27-51-41. (M)
- [SDR TSAA0436069](https://openairdocs.org/sdr/TSAA0436069.md): Bleed Air Sys · malfunctioned · Sep 17, 2004 · N824AL · Boeing 737282 · Pneumatic System
  > FLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUC
- [SDR BJNA040903](https://openairdocs.org/sdr/BJNA040903.md): Battery Pack · ingested · Sep 3, 2004 · N789TM · Boeing 737282 · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M)
- [SDR BJNA040809](https://openairdocs.org/sdr/BJNA040809.md): Floor Support · corroded · Aug 25, 2004 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 12 WITH LEVEL 2 CORROSION. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW BOEING 737 STRUCTURAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2

Next page: https://openairdocs.org/model/boeing-737-282/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 = '737282'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-282/reports

---
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