# Service difficulty reports: Boeing 737-2E3

A list on [Boeing 737-2E3](https://openairdocs.org/model/boeing-737-2e3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 66 reports

- [SDR CA020321002](https://openairdocs.org/sdr/CA020321002.md): Controller · malfunctioned · Mar 15, 2002 · Boeing 7372E3 · Cabin Pressure Controller
  > (CAN) SHORTLY AFTER TAKEOFF WHILE CLIMING THROUGH 31,000 FT, CREW NOTICED THAT CABIN ALTITUDE READING 9,500 FT. A/C DESCENTED TO 14,000 FT. CREW DONNED OXYGEN MASKS, AS PER QRC FOR RAPID DEPRESSURIZATION & PROCEEDED TO SELECT MANUAL CONTROL ON PRESUURIZATION P
- [SDR CA020131001](https://openairdocs.org/sdr/CA020131001.md): Nut · missing · Jan 30, 2002 · Boeing 7372E3 · Engine Mount Section
  > (CAN) SCHEDULED MAINTENANCE DURING REGULAR SCHEDULED OVERNIGHT MAINTENANCE; AD:99-26-07 (A)(2),INSPECTION OF NR 1 ENGINE AFT MOUNT CONE BOLT SECONDARY SUPPORT, WESTJET ENGINEER FOUND THE SECONDARY SUPPORT NUT, P/N:84821CD-524 MISSING. MAINTENANCE REPLACED THE
- [SDR CA011231004](https://openairdocs.org/sdr/CA011231004.md): Engine · failed · Dec 18, 2001 · Boeing 7372E3 · Turbine Engine Accessory Drive
  > (CAN) FLT NR 22 ON APPROACH INTO EDMONTON (YEG), FLT CREW REPORTED THEY HEARD & FELT VIBRATION FROM PEDESTAL AREA. AFTER DEPLOYMENT OF THRUST REVERSERS ON LANDING ROLL, ENGINE SPOOLED TO 1.4 EPR & THEN FLAMED OUT. ABNORMAL ENGINE SHUTDOWN CHECKLIST CARRIED OU
- [SDR AWXA0002203](https://openairdocs.org/sdr/AWXA0002203.md): Module · failed · Aug 22, 2001 · N138AW · Boeing 7372E3 · Hydraulic System, Auxiliary
  > AIR TURNBACK - FLT 704 - DURING CLIMBOUT OF PHX THE AUTO PILOT DISCONNECTED, YAW DAMPER DISENGAGED AND B-SYSTEM HYDRAULIC PRESSURE WENT TO ZERO. AT THE TIME OF OCCURRENCE THE NR 2 B-SYSTEM ELEC HYD PUMP WAS INOPERATIVE ON MEL 29-2 COND 1 DUE TO LOW PRESSURE.
- [SDR CA010504023](https://openairdocs.org/sdr/CA010504023.md): Bracket · worn · Apr 14, 2001 · Boeing 7372E3 · Elevator Control System
  > (CAN) CAREW REPORTED A VIBRATION IN CLIMB THRU 10,000 FEET THEN RECURRED ON DESCENT. AS THE AIRCRAFT DESCENDS BELOW 10,000 FEET. THE PROBLEM DID NOT OCCUR AFTER THE ELEVATOR TAIL HINE BRACKET WAS REPLACED.
- [SDR AWXA0000501](https://openairdocs.org/sdr/AWXA0000501.md): Skin · cracked · Jul 31, 2000 · N138AW · Boeing 7372E3 · Fuselage Main, Plate/Skin
  > A 2.5 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 767 AND 787 STR 19L. REPAIRED SKIN IAW 737 SRM 53-30-3 FIG 6.
- [SDR AWXA9900500](https://openairdocs.org/sdr/AWXA9900500.md): Wheel · unbalanced · Dec 29, 1999 · N138AW · Boeing 7372E3 · Wheel/Ski/Float
  > EMERGENCY LANDING DECLARED, AT V1 PHX, THE NOSE WHEEL FELT OUT OF BALANCE, SUSPECT FLAT TIRE. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES (LT S/N 3248 TOT 22044, RT S/N 6128 TOT 68142). WHEELS WERE REPLACED 13 NOV 99. A/C ALSO HAS HISTORY OF NLG
- [SDR AWXA9900492](https://openairdocs.org/sdr/AWXA9900492.md): Wire · broken · Dec 23, 1999 · N138AW · Boeing 7372E3 · Light System Wiring
  > EMERGENCY LIGHTS STAY ON INFLIGHT. RESPLICED WIRE AT SEAT 13A, OPS CK GOOD. A/C HAS 4 SDR'S GENERATED FOR EMERGENCY LIGHTING, NONE RELATED.
- [SDR AWXA9900449](https://openairdocs.org/sdr/AWXA9900449.md): Valve · failed · Dec 6, 1999 · N138AW · Boeing 7372E3 · Fuel Transfer Valve
  > NR 1 ENG START SEQUENCE NORMAL THROUGH IDLE, AFTER SEVERAL SECONDS FF SURGED AND ENGINE FLAMED OUT. FOUND NR 1 SPAR VALVE MOTOR NOT OPENING VALVE. REPLACED VALVE AND ACTUATOR LK AND OPS CK GOOD.
- [SDR AWXA9900431](https://openairdocs.org/sdr/AWXA9900431.md): Battery Pack · discharged · Nov 28, 1999 · N138AW · Boeing 7372E3 · Emergency Lighting
  > EMERGENCY LIGHTS OUT LAST 6 SEAT ROWS. REPLACED BATTERY PACK AT ROW 18L. CURRENT HISTORY: SEVERAL WRITE-UPS EXPERIENCED IN LAST FEW FLIGHT HRS.
- [SDR AWXA9900430](https://openairdocs.org/sdr/AWXA9900430.md): Battery Pack · discharged · Nov 27, 1999 · N138AW · Boeing 7372E3 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS REMAIN ON WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACKS AT ROW 3L, 11L, AND 17L.
- [SDR AWXA9900068](https://openairdocs.org/sdr/AWXA9900068.md): Battery · discharged · Mar 1, 1999 · N138AW · Boeing 7372E3 · Emergency Lighting
  > IN MAINTENANCE, RT EMERGENCY OVERWING LIGHT OUT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.
- [SDR AWXA9900033](https://openairdocs.org/sdr/AWXA9900033.md): Wire · failed · Jan 24, 1999 · N138AW · Boeing 7372E3 · Light System Wiring
  > A 3 FOOT SECTION OF CABIN ESCAPE PATH LIGHTS INOP. REPAIRED WIRING.
- [SDR AWXA9800247](https://openairdocs.org/sdr/AWXA9800247.md): Light · inop · Dec 24, 1998 · N138AW · Boeing 7372E3 · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICABLE UNIT, OPS NORMAL.
- [SDR AWXA9800107](https://openairdocs.org/sdr/AWXA9800107.md): Battery Pack · discharged · Apr 17, 1998 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH L2 AND R2 EXTERIOR EMERG EXIT LIGHTS FAIL 4 MIN CAP TEST. REMOVED AND REPLACED BATTERY PACK FOR L2 AND R2 EXTERIOR EMERG EXIT LGHTS, SYSTEM OPS CHECKS GOOD.
- [SDR AWXA9800023](https://openairdocs.org/sdr/AWXA9800023.md): Wire · broken · Jan 15, 1998 · N138AW · Boeing 7372E3 · Light System Wiring
  > D-ROW 6ABC EMERGENCY LIGHT INOP. FOUND BROKEN WIRE STC NR SA3432NM.
- [SDR AWXA9700693](https://openairdocs.org/sdr/AWXA9700693.md): Power Supply · inoperative · Dec 15, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > AFT LEFT AND RIGHT ESCAPE SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CK GOOD. STC NR SA3432NM
- [SDR AWXA9700673](https://openairdocs.org/sdr/AWXA9700673.md): Battery · discharged · Nov 13, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS AT ROW 8 TO 15 INOP. REPLACED BATTERY AT ROW 11A, OPS CHECK GOOD.
- [SDR AWXA9700616](https://openairdocs.org/sdr/AWXA9700616.md): Start Vlv Light · illuminated · Oct 28, 1997 · N138AW · Boeing 7372E3 · Engine Start Valves/Controls
  > ON CLIMBOUT 2000 FT START VALVE LIGHT ILLUMINATED AT CLIMB THRUST APPROX 90 PERCENT N1. CYCLED START VALVE C/B'S, NO HELP. SHUT DOWN ENGINE PER QRH, OVERWEIGHT LANDING DONE VERY SMOOTHLY THOUGH COMPLETED ER 2-80-10-03. SWAPPED START VALVE OPEN INDICATION WI
- [SDR AWXA9700390](https://openairdocs.org/sdr/AWXA9700390.md): Wire · broken · Jul 10, 1997 · N138AW · Boeing 7372E3 · Light System Wiring
  > DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 6 LEFT EMERGENCY LIGHT INOP. REPLACED WIRE. OPS CHECK GOOD.
- [SDR AWXA9700346](https://openairdocs.org/sdr/AWXA9700346.md): Fan · failed · Jun 15, 1997 · N138AW · Boeing 7372E3 · Air Distribution Fan
  > COCKPIT CREW AND CABIN CREW NOTICED BURNING PLASTIC SMELL ON FINAL APPROACH. BURNING SMELL CONTINUED UNTIL WE REACHED THE GATE. NO VISIBLE SMOKE. REMOVED AND REPLACED CABIN CONTROL AUGMENTATION FAN PER MM 21-22-11, PAGE 6.
- [SDR AWXA9700310](https://openairdocs.org/sdr/AWXA9700310.md): Wire · disconnected · May 27, 1997 · N138AW · Boeing 7372E3 · Light System Wiring
  > DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 6L EMERGENCY LIGHT IS INOP. ATTACHED BROKEN WIRES, OPS CHECK GOOD. STC - SA3432NM
- [SDR AWXA9700301](https://openairdocs.org/sdr/AWXA9700301.md): Power Supply · inoperative · May 24, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY LIGHT IS OUT EXTERIOR. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. STC - SA3432NM
- [SDR AWXA9700293](https://openairdocs.org/sdr/AWXA9700293.md): Floorbeam · corroded · May 7, 1997 · N138AW · Boeing 7372E3 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL AREAS OF CORROSION ON FLOORBEAM BS 294, BL 0 TO RBL 55, WL 208. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-9.
- [SDR AWXA9700292](https://openairdocs.org/sdr/AWXA9700292.md): Skin · corroded · May 7, 1997 · N138AW · Boeing 7372E3 · Fuselage Main, Plate/Skin
  > DURING ROUTINE MAINTENANCE CHECK, FOUND PILLOWING SKIN AT BS 727 AT RT KEEL BEAM, WL 148.5. REPAIRED PILLOWING SKIN AND KEEL BEAM PER SRM 53-30-3.
- [SDR AWXA9700223](https://openairdocs.org/sdr/AWXA9700223.md): Power Supply · inoperative · Apr 6, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, STC - SA3432NM.
- [SDR AWXA9700210](https://openairdocs.org/sdr/AWXA9700210.md): Battery · discharged · Apr 1, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY, OPS CHECK OK STC SA3432NM.
- [SDR AWXA9700209](https://openairdocs.org/sdr/AWXA9700209.md): Battery · discharged · Apr 1, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT IN CENTER AISLE INOP. REMOVED AND REPLACED BATTERY OPS CHECK OK STC SA3432NM.
- [SDR AWXA9700065](https://openairdocs.org/sdr/AWXA9700065.md): Battery Pack · discharged · Feb 1, 1997 · N138AW · Boeing 7372E3 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE RT SIDE AFT OF AFT WING TO BODY FAIRING. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECK NORMAL. STC - SA3432NM.
- [SDR AWXA9600768](https://openairdocs.org/sdr/AWXA9600768.md): Bypass Sw Line · leaking · Dec 18, 1996 · N138AW · Boeing 7372E3 · Engine Oil Pressure
  > CAPTAIN CALLED OUTSIDE OF LAS AND INFORMED MX. CONTROL THAT THE NR 2 ENGINE OIL QUANTITY WAS SLOWLY DROPPING AND OIL PRESSURE/TEMPERATURE WERE NORMAL. AIRCRAFT DIVERTED TO LAS. REMOVED AND REPLACED FILTER BYPASS SWITCH LINE, ADDED 10 QTS OIL FOR LOSS, LEAK C
- [SDR AWXA960669](https://openairdocs.org/sdr/AWXA960669.md): Engine · failed · Nov 10, 1996 · N138AW · Boeing 7372E3 · Engine (Turbine/Turboprop)
  > AIR TURNBACK WHEN APPLYING TAKEOFF POWER 1 OR 2 MINOR COMPRESSOR STALLS WERE FELT WITH ALL ENGINE INSTRUMENTS INDICATING NORMAL SO TAKEOFF WAS CONTINUED. AT ABOUT 12,000 FEET, NR 2 ENGINE HAD RAPID COMPRESSOR STALLS AND EGT WAS RED. SHUTDOWN ENGINE. BORESCO
- [SDR AWXA9600669](https://openairdocs.org/sdr/AWXA9600669.md): Turbine · failed · Nov 10, 1996 · N138AW · Boeing 7372E3 · Turbine Section
  > AIR TURNBACK. WHEN APPLYING TAKEOFF POWER 1 OR 2, MINOR COMPRESSOR STALLS WERE FELT WITH ALL ENGINE INSTRUMENTS INDICATING NORMAL SO TAKEOFF WAS CONTINUED. AT ABOUT 12,000 FEET, NR 2 ENGINE HAD RAPID COMPRESSOR STALLS AND EGT WAS RED. SHUTDOWN ENGINE. BORE
- [SDR AWXA960397](https://openairdocs.org/sdr/AWXA960397.md): Yaw Dmp Coupler · malfunctioned · Aug 19, 1996 · N138AW · Boeing 7372E3 · Autopilot System
  > PHX - FLT 2450 - DURING TAKEOFF ROLL, EXPERIENCED TWO SEVERE SIDE JOLTS ABOUT 4-5 SECONDS APART. PER QUALITY CONTROL ALERT BULLETIN NR 95-15 PERFORMED RUDDER PCU LEAK CHECK IAW A8M27001, NO DEFECTS NOTED. PER MX CONTROL CHANGED YAW DAMPNER COUPLER IAW 22-11-
- [SDR AWXA960319](https://openairdocs.org/sdr/AWXA960319.md): Floor Beam · corroded · May 1, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Floor Beam
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 987, LBL TO RBL 45, WL 208. REMOVED CORROSION, OUT OF LIMITS. FABRICATED NEW TOP CHORD PER SRM 51-30-2 AND INSTALLED PER SRM 51-10-2 AND ER 2-53-15-39 (TC-PAN
- [SDR AWXA960318](https://openairdocs.org/sdr/AWXA960318.md): Stringer · corroded · May 1, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 17L, BL 967. FABRICATED AND INSTALLED REPAIR STRINGER PER SRM 53-30-02. (M)
- [SDR AWXA960317](https://openairdocs.org/sdr/AWXA960317.md): Rib · cracked · May 1, 1996 · N138AW · Boeing 7372E3 · Horizontal Stabilizer, Spar/Rib
  > DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STABILIZER L/E RIB CRACKED AT STATON 114.55. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M)
- [SDR AWXA960316](https://openairdocs.org/sdr/AWXA960316.md): Rib · cracked · May 1, 1996 · N138AW · Boeing 7372E3 · Horizontal Stabilizer, Spar/Rib
  > PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STABILIZER L/E RIB CRACKED AT STATION 170.34. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M)
- [SDR AWXA960315](https://openairdocs.org/sdr/AWXA960315.md): Rib · cracked · May 1, 1996 · N138AW · Boeing 7372E3 · Horizontal Stabilizer, Spar/Rib
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STAB L/E RIB CRACKED AT STATION 151.75. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M)
- [SDR AWXA960314](https://openairdocs.org/sdr/AWXA960314.md): Rib · cracked · May 1, 1996 · N138AW · Boeing 7372E3 · Horizontal Stabilizer, Spar/Rib
  > DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STAB L/E RIB CRACKED AT STATION 123.85. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M)
- [SDR AWXA960313](https://openairdocs.org/sdr/AWXA960313.md): Rib · cracked · Apr 30, 1996 · N138AW · Boeing 7372E3 · Wing, Rib/Bulkhead
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND LEFT L/E RIB CRCKED AT WBL 183.4. REPAIRED RIB IAW 51-40-4, 51-10-12 AND 51-30-2. (M)
- [SDR AWXA960312](https://openairdocs.org/sdr/AWXA960312.md): Clevis · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Horizontal Stabilizer Structure
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON LEFT UPPER CHORD ATTACH CLEVIS AND BOTTOM CHORD ATTACH LUG OF HINGE HOUSING. REMOVED CORROSION FROM LEFT UPPER/LOWER LUG CLEVIS.018 INCH,.005 INCH,.013 INCH AND.006 INCH
- [SDR AWXA960311](https://openairdocs.org/sdr/AWXA960311.md): Blkhd Doubler · cracked · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Bulkhead
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD DOUBLER AT BS 1156 CRACKED BETWEEN TWO FASTENERS. STOP DRILLED CRACK, NDI VERIFIED CRACK CONTAINMENT. REPAIRED WIT MOD PER SB 53-1086 R3. (M)
- [SDR AWXA960310](https://openairdocs.org/sdr/AWXA960310.md): Mop Sill · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Miscellaneous Structure
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON RIGHT AFT SERVICE DOOR MOP SILL STATION 957-987, RBL 50, WL 208. REMOVED AND REPLACED MOP SILL PER SRM 51-30-2. (M)
- [SDR AWXA960309](https://openairdocs.org/sdr/AWXA960309.md): Floor Beam · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Floor Beam
  > PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION UNDERSIDE OF FLOOR BEAM AROUND NUT PLATES STATION 947, RBL 48 TO LBL 5, WL 208. FABRICATED REPAIR PARTS AND INSTALLED PER ER 2-53-15-40 (TC-PAN-96-0541RR). (M)
- [SDR AWXA960308](https://openairdocs.org/sdr/AWXA960308.md): Floor Beam · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Floor Beam
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON STATION 1016 FLOOR BEAM UPPER CHORD RBL 5 TO LBL 28, WL 208. FABRICATED REPAIR PARTS AND INSTALLED PER ER 2-53-15-41 (TC-PAN-960551RR). (M)
- [SDR AWXA960307](https://openairdocs.org/sdr/AWXA960307.md): Stringer · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Longeron/Stringer
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON THE STRINGER 26R, BS 1004-1016, RBL 12, WL 148. REMOVED AND REPLACED STRINGER 26 PER SRM 53-10-2. (M)
- [SDR AWXA960306](https://openairdocs.org/sdr/AWXA960306.md): Floor Beam · corroded · Apr 30, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Floor Beam
  > PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION AROUND NUT PLATE HOLE ON FLOOR BEAM STATION 967, WL 208, RBL 28. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-9. (M)
- [SDR AWXA960305](https://openairdocs.org/sdr/AWXA960305.md): Bulkhead Fitting · corroded · Apr 25, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Bulkhead
  > PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD SUPPORT FITTING CORRODED BEYOND LIMITS. REPLACED FITTING PER IAW SCM 51-10-1. (M)
- [SDR AWXA960304](https://openairdocs.org/sdr/AWXA960304.md): Stringer · corroded · Apr 25, 1996 · N138AW · Boeing 7372E3 · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND STRINGER 27L AT BS 1006 CORRODED AT STRINGER CLIP. REMOVED, FABRICATED AND REPLACED REPAIR PARTS PER SRM 53-10-3. (M)
- [SDR AWXA960303](https://openairdocs.org/sdr/AWXA960303.md): Angle · corroded · Apr 25, 1996 · N138AW · Boeing 7372E3 · Fuselage Miscellaneous Structure
  > PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BUTT JOINT SPLICE ANGLE AT BS 1016, BL0 WL 194 IS CORRODED. REMOVED SPLICE ANGLE AT BS 1016, BLO, WL 194. CLEANED AREA, ALODINED, PRIMED AND FABRICATED PART AND INSTALLED PER SRM 51-3

Next page: https://openairdocs.org/model/boeing-737-2e3/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 = '7372E3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2e3/reports

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