# Service difficulty reports: Boeing 737-222

A list on [Boeing 737-222](https://openairdocs.org/model/boeing-737-222.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 14 · 657 reports

- [SDR UALA2009010200016](https://openairdocs.org/sdr/UALA2009010200016.md): Light · inoperative · Jan 1, 2009 · N318UA · Boeing 737222 · Emergency Lighting
  > EEL BULLNOSE LIGHT INOP AT 7DEF. RELAMPED, CHECKS OK.
- [SDR 219PA0014](https://openairdocs.org/sdr/219PA0014.md): Proximity Switch · out of adjust · Mar 14, 2004 · N219PA · Boeing 737222 · Door Warning System
  > AFT CARGO DOOR LIGHT CAME ON AT 75 KTS. RTO, NO BRAKES APPLIED, REVERSERS ONLY. ADJUSTED PROXIMITY SWITCH AND OPS CHECKED PER MM 52-10-00.
- [SDR 219PA0013](https://openairdocs.org/sdr/219PA0013.md): Lamp · inoperative · Mar 3, 2004 · N219PA · Boeing 737222 · Emergency Lighting
  > AFT CENTER AISLE EMERGENCY EXIT LIGHTS INOP. RELAMPED AND OPS CHECKS GOOD PER MM 33-51-02.
- [SDR 219PA0012](https://openairdocs.org/sdr/219PA0012.md): Battery Pack · inoperative · Feb 20, 2004 · N219PA · Boeing 737222 · Emergency Lighting
  > BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED OVERWING BATTERY PACKS. OPS CHECKS GOOD PER MM 33-50-00.
- [SDR 219PA0011](https://openairdocs.org/sdr/219PA0011.md): Coupler · damaged · Jan 2, 2004 · N219PA · Boeing 737222 · Autopilot System
  > YAW DAMPER LIGHT STAYS OFF WHEN SWITCHED FROM ON TO OFF. REPLACED YAW DAMPER COUPLER, OPS CHECKS NORMAL PER MM 22-12-01.
- [SDR 219PA0010](https://openairdocs.org/sdr/219PA0010.md): Computer · malfunctioned · Sep 25, 2003 · N219PA · Boeing 737222 · Autopilot System
  > ROLL CHANNEL WILL NOT ENGAGE ON AUTO PILOT AND HEADING SELECT WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED GOOD PER MM 22-11-0.
- [SDR 219PA0009](https://openairdocs.org/sdr/219PA0009.md): Computer · malfunctioned · Sep 18, 2003 · N219PA · Boeing 737222 · Autopilot System
  > AUTO PILOT AILERON WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED NORMAL PER MM 22-11-0.
- [SDR 219PA0008](https://openairdocs.org/sdr/219PA0008.md): Limiter · inoperative · Sep 17, 2003 · N219PA · Boeing 737222 · Autopilot System
  > AUTOPILOT ROLL CHANNEL WILL NOT ENGAGE. REPLACED AILERON FORCE LIMITER IAW MM 22-12-10. OPS CHECKS OK.
- [SDR 219PA0007](https://openairdocs.org/sdr/219PA0007.md): Battery Pack · inoperative · Jun 23, 2003 · N219PA · Boeing 737222 · Emergency Equipment
  > FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED FWD FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT BATTERY PACK PER MM 33-51-21.
- [SDR 219PA0006](https://openairdocs.org/sdr/219PA0006.md): Autopilot Sys · Jan 27, 2003 · N219PA · Boeing 737222 · Autopilot System
  > Elevator channel of auto pilot will not stay engaged. Re-racked A/P pitch control channel unit. Ops chks good IAW MM 22-10-10.
- [SDR 219PA0005](https://openairdocs.org/sdr/219PA0005.md): Light · Jan 24, 2003 · N219PA · Boeing 737222 · Emergency Lighting
  > Emergency light above aft service door inop. Removed and replaced emergency light above aft service door Ref. MM 33-50-09. Ops. chk. good per MM 33-50-01.
- [SDR 219PA0004](https://openairdocs.org/sdr/219PA0004.md): Brake Assy · Oct 30, 2002 · N219PA · Boeing 737222 · Brake
  > #3 Brake dragging. Log page entry, (found heat shield from #3 main wheel lodged in rotor of brake assy. R&R brake IAW MM32-41-41 and R&R #3 wheel IAW MM32-45-11). Upon further investigation, found brake pad separated from brake resulting in damage to wheel a
- [SDR 219PA0001A](https://openairdocs.org/sdr/219PA0001A.md): Brake Assy · damaged · Oct 30, 2002 · N219PA · Boeing 737222 · Brake
  > NR 3 BRAKE DRAGGING. LOG PAGE ENTRY, (FOUND HEAT SHIELD FROM NR 3 MAIN WHEEL LODGED IN ROTOR OF BRAKE ASSY. R&R BRAKE IAW MM32-41-41 AND R&R NR 3 WHEEL IAW MM32-45-11). UPON FURTHER INVESTIGATION, FOUND BRAKE PAD SEPARATED FROM BRAKE RESULTING IN DAMAGE TO W
- [SDR 219PA0003](https://openairdocs.org/sdr/219PA0003.md): Transmitter · Jun 25, 2002 · N219PA · Boeing 737222 · Power Indicating System
  > Lower than normal acceleration at T/O EPR 1.95 Engs do not seem to produce thrust per EPR setting. Inspected PT2 systems on #1 and #2 engines and found both EPR transmitters bad. R&R #1 eng & #2 eng EPR transmitter per MM77-11-07, Ops check of eng paramaters
- [SDR 219PA0002](https://openairdocs.org/sdr/219PA0002.md): Valve · Jun 24, 2002 · N219PA · Boeing 737222 · Fuel Controlling System
  > #2 engine would not produce calculated T/O thrust. T/O discontinued at approx. 60 kts.Verified. R&R'd #2 eng P&D valve IAW M/M73-12-1. Ops & Leak chks good. Also C/W work cardPAS-MF-25, JT8D eng. trim & data plate run. Ops chks good no defects noted
- [SDR 219PA0001](https://openairdocs.org/sdr/219PA0001.md): Generator · May 29, 2002 · N219PA · Boeing 737222 · AC Generation System
  > Rt Generator failed at begining of take-off roll. Reset CSD could not duplicate.
- [SDR 20010503CW010](https://openairdocs.org/sdr/20010503CW010.md): Tire · deflated · Mar 11, 2001 · N135TA · Boeing 737222 · Tire
  > LANDING, NR 4 TIRE DEFLATED. TIRE HAS FLAT SPOT AND HOLE ON TREAD SURFACE FROM SKIDDING DURING LANDING. REMOVED AND REPLACED BURST TIRE INSPECTION WAS PERFORMED. NO FURTHER DISCREPANCIES WERE NOTED.
- [SDR 20001206SH021](https://openairdocs.org/sdr/20001206SH021.md): Actuator · failed · Oct 27, 2000 · N135TA · Boeing 737222 · Entrance Stairs
  > KBUF - SABRES 7 - FORWARD AIRSTAIR DOOR OPERATED CORRECTLY IN STANDBY MODE. ONLY THE NORMAL MODE WAS INOPERATIVE. AIRCRAFT RETURNED TO THE AIRFIELD AND LANDED WITHOUT INCIDENT. AFTER CLOSING THE DOOR USING THE STANDBY MODE, THE AIRCRAFT PRESSURIZED NORMALLY
- [SDR P2E00315](https://openairdocs.org/sdr/P2E00315.md): Lap Joint · cracked · Oct 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LOWER ROW OF LONGITUDINAL LAP JOINT AT BS727 STR 10L FASTENER HOLE WITH CRACK L=0.125 W=0.032 INCH. REPAIRED THE EXTERIOR FUSELAGE LOWER ROW OF LONGITUDINAL LAP JOINT AT BS 727 10L FASTENER HOLE
- [SDR COOSDR000016](https://openairdocs.org/sdr/COOSDR000016.md): Lap Joint · cracked · Oct 26, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE AT BS 727A PLUS 10, STR 10 LT LAP JOINT AREA, LOWER SKIN WITH HOLE CRACKED. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)
- [SDR P2EA00320](https://openairdocs.org/sdr/P2EA00320.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS880-890 STR 25R WITH LEVEL 2 CORROSION L=2.00 W=2.00 D=0.008. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS 880-890 STR 25R IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-2000 AND S
- [SDR P2EA00319](https://openairdocs.org/sdr/P2EA00319.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS893-895 STR 20L WITH LEVEL 2 CORROSION L-2.00 W=2.00 D=0.008. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS 893-895 STR 20L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-200
- [SDR P2EA00318](https://openairdocs.org/sdr/P2EA00318.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS747-749 STR 25L WITH LEVEL 3 CORROSION L-2.00 W=2.00 D=0.009. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS747-749 STR 25L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-2000
- [SDR P2EA00317](https://openairdocs.org/sdr/P2EA00317.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS 747-751 STR 25 RT WITH LEVEL 2 CORROSION L=2.00 W=2.00 D=0.009. REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS747-751 STR 25R IAW BOEING S/B 737-53-A1224 PART III PAR C DATED 8-17-
- [SDR P2EA00316](https://openairdocs.org/sdr/P2EA00316.md): Lap Joint · cracked · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE UPPER ROW OF LONGITUDINAL LAP JOINT AT BS 787 STR 14L FASTENER HOLE WITH CRACK L=O.125 W=0.002. REPAIRED THE EXTERIOR FUSELAGE UPPER ROW OF LONGITUDINAL LAP JOINT AT BS 787 14L FASTENER HOLE IAW BO
- [SDR P2EA00321](https://openairdocs.org/sdr/P2EA00321.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE LAP JOINT AT BS953-961 STR 4L WITH LEVEL 2 CORROSION L=23.00 IN, W=3.0-00 IN, D=0.009 IN REPAIRED THE EXTERIOR FUSELAGE LAP JOINT AT BS953-961 STR 4L IAW BOEING S/B 737-53-A1224 PART III PAR C DATED
- [SDR COOSDR000022](https://openairdocs.org/sdr/COOSDR000022.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FROM BS 880 TO BS 890, STR 25RT, LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN CORROSION. (X)
- [SDR COOSDR000021](https://openairdocs.org/sdr/COOSDR000021.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FROM BS 893 TO BS 895, STR 20 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)
- [SDR COOSDR000020](https://openairdocs.org/sdr/COOSDR000020.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FROM BS 747 TO BS 751, STR 25 RT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CORROSION WAS SKIN FATIGUE. (X)
- [SDR COOSDR000019](https://openairdocs.org/sdr/COOSDR000019.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FROM BS 747 TO BS 749, STR 25 LT, LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X)
- [SDR COOSDR000018](https://openairdocs.org/sdr/COOSDR000018.md): Lap Joint · cracked · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 787, STR 14 LT - LAP JOINT AREA, UPPER ROW WITH HOLE CRACKED. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X)
- [SDR COOSDR000017](https://openairdocs.org/sdr/COOSDR000017.md): Lap Joint · corroded · Oct 25, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FROM BS 930 TO BS 961 STR 4 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X)
- [SDR P2EA00312](https://openairdocs.org/sdr/P2EA00312.md): Skin · cracked · Oct 24, 2000 · N603DJ · Boeing 737222 · Fuselage Main, Plate/Skin
  > DURING SPECIAL INSPECTION SERVICE FOUND THE EXTERIOR FUSELAGE SKIN FROM BS482-484 BETWEEN STR 9L AND 10L WITH CRACK L=0.50 W=0.002. REPAIRED THE EXTERIOR FUSELAGE SKIN FROM BS482-484 BETWEEN STR 9L AND 10L IAW BOEING SRM 53-30-3 FIG 9
- [SDR 20001109SH018](https://openairdocs.org/sdr/20001109SH018.md): Rod End · separated · Oct 14, 2000 · N135TA · Boeing 737222 · Landing Gear Retraction/Extension System
  > UNABLE TO RAISE LANDING GEAR HANDLE AFTER TAKEOFF. ROD END SEPARATED FROM TELEFLEX CABLE AT RT MLG. AIR/GROUND SHIFT CABLE ASSY WAS REPLACED AND GEAR SWING PERFORMED. NO FURTHER DEFECTS NOTED, AND AIRCRAFT WAS RETURNED TO SERVICE. (X)
- [SDR P2EA00226](https://openairdocs.org/sdr/P2EA00226.md): Structure · cracked · Jul 11, 2000 · N603DJ · Boeing 737222 · Passenger/Crew Doors
  > MCI - DURING MAINTENANCE, L1 DOOR CRACKED AT BS 341, WL 284.75. REPAIRED CRACK FROM BS 339 TO BS 344 AND FROM WL 284.75 TO 279.75 IAW SRM 52-00-3 FIG 2. (M)
- [SDR P2EA00210](https://openairdocs.org/sdr/P2EA00210.md): Actuator · unserviceable · Jun 14, 2000 · N603DJ · Boeing 737222 · Drag Control Actuator
  > FLT 414 - MDW - FOUND LOST A SYSTEM HYDRAULIC PRESSURE AND QUANTITY WHILE TAXING TO GATE. REMOVED AND REPLACED THE NR 1 GROUND SPOILER ACTUATOR PER BOEING MM 27-62-10. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M)
- [SDR P2EA00197](https://openairdocs.org/sdr/P2EA00197.md): Warning Light · illuminated · Jun 4, 2000 · N209US · Boeing 737222 · Door Warning System
  > FLT 780 - MYR - FORWARD CARGO DOOR LIGHT ILLUMINATED JUST AFTER TAKEOFF, RETURNED TO FIELD. LANDING UNEVENTFUL. INSPECTED FORWARD CARGO DOOR CONTACT. CLOSED DOOR, FOUND OPERATIONALLY SATISFACTORY. (M)
- [SDR P2EA00163](https://openairdocs.org/sdr/P2EA00163.md): Skin · dented · May 10, 2000 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, FOUND FUSELAGE SKIN AT BS 243 - BS 252.5, BETWEEN WL 170 AND WL 161 RIGHT SIDE, WITH DENT. L= 2.00 FEET, W = 1.50 INCHES, D = 0.063 INCH. REPAIRED FUSELAGE SKIN AT BS 243 - BS 252.5, BETWEEN WL 170 AND WL 161 RIGHT SIDE, IAW SRM 53-30-3
- [SDR P2EA00164](https://openairdocs.org/sdr/P2EA00164.md): Skin · dented · May 10, 2000 · N209US · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING C-CHECK, FOUND FUSELAGE SKIN AT BS 438 - BS 447.5, STR 20 - STR 21 LEFT SIDE, WITH DENT. L = 2.00 FEET, W = 1.00 INCH, D - 0.050 INCH. REPAIRED FUSELAGE SKIN AT BS 438 - BS 447.5, STR 20 - STR 21, LEFT SIDE, IAW SRM 53-30-3, FIG 1. SEE COOPESA W
- [SDR P2EA00119](https://openairdocs.org/sdr/P2EA00119.md): Fitting · stripped · May 10, 2000 · N603DJ · Boeing 737222 · Turbine Engine Reduction Gear
  > PIT - FLT 732 - ON SHORT FINAL, NR 1 ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE FLUCTUATED 35 - 45 PSI, OIL PRESSURE LIGHT FLICKERED ON. UPON LANDING, OIL QUANTITY WAS ZERO, OIL PRESSURE WAS 20 SPI, OIL LIGHT WAS ON. CREW SHUT DOWN NR 1 ENGINE. FOUND L
- [SDR P2EA00188](https://openairdocs.org/sdr/P2EA00188.md): Frame · cracked · May 8, 2000 · N209US · Boeing 737222 · Service Doors
  > SJO - DURING C-CHECK, FOUND THE R-2 DOOR LOWER SECTION, LOWER FRAME WITH CRACK 1.5 INCHES LONG,.002 INCHES WIDE. REPLACED THE R-2 DOOR LOWER SECTION, LOWER FRAME IAW BOEING SRM 51-10-1 PAGE 5 AND 51-30-2 PAGE 1. (M)
- [SDR P2EA00193](https://openairdocs.org/sdr/P2EA00193.md): Skin · worn · May 8, 2000 · N209US · Boeing 737222 · Nacelle/Pylon, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN WITH WEAR LENGTH 10 INCH, WIDTH.25 INCH, DEPTH.025 INCH. REPAIRED THE NR 1 ENGINE NOSE COWL UPPER SECTION SKIN IAW COOPESA EO NR COO-3-54-317-00 DATED MAY 12, 2000. (M)
- [SDR P2EA00184](https://openairdocs.org/sdr/P2EA00184.md): Skin · cracked · May 6, 2000 · N209US · Boeing 737222 · Passenger/Crew Doors
  > SJO - DURING C-CHECK, FOUND R-1 DOOR LOWER HINGE SECTION, BS 306-313 BEAM 5-7 SKIN WITH CRACK LENGTH.50 INCH, WIDTH.002 INCH. REPAIRED R-1 DOOR LOWER HINGE SECTION, BS 306-313 BEAM 5-7, SKIN IAW BOEING SERVICE BULLETIN 737-52-1096. (M)
- [SDR P2EA00186](https://openairdocs.org/sdr/P2EA00186.md): Skin · delaminated · May 4, 2000 · N209US · Boeing 737222 · Air Conditioning Doors
  > SJO - DURING C-CHECK, FOUND THE LEFT AIR CONDITION BAY DOOR WITH DELAMINATED, 25 INCHES IN LENGTH, 14 INCHES WIDE. REPAIRED THE LEFT AIR CONDITION BAY DOOR IAW COOPESA EO NR COO-CMP-3-53-305-00 DATED MAY 10, 2000. (M)
- [SDR P2EA00187](https://openairdocs.org/sdr/P2EA00187.md): Panel · delaminated · May 4, 2000 · N209US · Boeing 737222 · Nacelle/Pylon, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE NR 1 ENGINE PYLON UPPER PANEL WITH DELAMINATED, 14 INCHES IN LENGTH, AND 8 INCHES WIDE. REPAIRED THE NR 1 ENGINE PYON UPPER PANEL IAW COOPESA EO NR COO-CMP-3-57-308-00. (M)
- [SDR P2EA00194](https://openairdocs.org/sdr/P2EA00194.md): Panel · delaminated · May 4, 2000 · N209US · Boeing 737222 · Horizontal Stabilizer, Plate/Skin
  > SJO - DURING C-CHECK, FOUND THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL, P/N 65-52493-2 WITH DELAM LENGTH 63 INCHES, WIDTH 6 INCHES. REPAIRED THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL P/N 65-52493-2 IAW CO
- [SDR P2EA00183](https://openairdocs.org/sdr/P2EA00183.md): Web · worn · May 2, 2000 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, FOUND LOWER FUSELAGE BS 510R, RAM AIR INLET DUCT WEB WITH WEAR 1 INCH IN LENGTH,.50 INCH WIDE,.040 INCH DEEP. REPAIRED LOWER FUSELAGE BS 510R RAM AIR INLET DUCT WEB IAW SRM 51-40-2 FIG 1. (M)
- [SDR P2EA00182](https://openairdocs.org/sdr/P2EA00182.md): Splice · cracked · May 1, 2000 · N209US · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING C-CHECK, FOUND STRINGER 27L SPLICE AT BS 358 LBL 16 WITH CRACK.5 INCHES LONG. REPLACED SPLICE FROM BS 354-366 LBL 16 STRINGER 27L IAW SRM 51-10-1 PAR 5. (M)
- [SDR P2EA00180](https://openairdocs.org/sdr/P2EA00180.md): Structure · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Landing Gear Doors
  > SJO - DURIG C-CHECK, FOUND THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE WITH CRACK 2 INCHES LONG BY.002 INCHES WIDE. REPAIRED THE LEFT MAIN LANDING GEAR CENTER DOOR TRAILING EDGE IAW SRM 51-40-3 FIG 1. (M)
- [SDR P2EA00181](https://openairdocs.org/sdr/P2EA00181.md): Gate · cracked · Apr 28, 2000 · N209US · Boeing 737222 · Passenger/Crew Doors
  > SJO - DURING C-CHECK, FOUND THE R-2 DOOR UPPER GATE SKIN WITH CRACK 1 INCH IN LENGTH,.001 INCH WIDE. REPLACED THE R-2 DOOR UPPER GATE IAW BOEING MM 52-41-11. (M)

Next page: https://openairdocs.org/model/boeing-737-222/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 = '737222'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-222/reports

---
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