# Service difficulty reports: N15948, cancelled Jul 11, 2016

A list on [N15948, cancelled Jul 11, 2016](https://openairdocs.org/deregistered/N15948-2016-07-11.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 97 reports

- [SDR ASOA20131026191](https://openairdocs.org/sdr/ASOA20131026191.md): Duct · cracked · Oct 26, 2013 · N15948 · Emb EMB145EP · Air Distribution System
  > CREW REPORTED PACK 1 AND 2 FAILED IN FLIGHT AND A BAD ODOR AFTER SELECTING. RESET PACK 2 CREW CONTINUED TO DESTINATION WITH PACKS DEACTIVATED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE "Y" DUCT BETWEEN THE PACK VALVE AND DUAL
- [SDR ASOA20130915168](https://openairdocs.org/sdr/ASOA20130915168.md): Light · inoperative · Sep 15, 2013 · N15948 · Emb EMB145EP · Emergency Lighting
  > DURING TESTING, NR 3 EMERGENCY LIGHT FAILED TO ILLUMINATE. MX REPLACED THE LIGHT STRIP, OPS TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR ASOA20130421138](https://openairdocs.org/sdr/ASOA20130421138.md): Skin · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 20R-20L. MX R & R THE SKIN IAW EC5320-01787. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421137](https://openairdocs.org/sdr/ASOA20130421137.md): Stringer · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421136](https://openairdocs.org/sdr/ASOA20130421136.md): Stringer · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421135V](https://openairdocs.org/sdr/ASOA20130421135V.md): Sill · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130210012](https://openairdocs.org/sdr/ASOA20130210012.md): Skin · cracked · Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2R. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.
- [SDR ASOA20130210011](https://openairdocs.org/sdr/ASOA20130210011.md): Skin · cracked · Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.
- [SDR ASOA20120405051](https://openairdocs.org/sdr/ASOA20120405051.md): Connector · broken · Apr 6, 2012 · N15948 · Emb EMB145EP · Light System Wiring
  > DURING MX INSPECTION, LT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120405050](https://openairdocs.org/sdr/ASOA20120405050.md): Connector · disconnected · Apr 5, 2012 · N15948 · Emb EMB145EP · Light System Wiring
  > DURING MX INSPECTION, THE RT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. RESECURRED THE EXIT SIGN INVERTER ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA138](https://openairdocs.org/sdr/C2XA11IA138.md): Dimmer · defective · Jul 2, 2011 · N15948 · Emb EMB145EP · Electrical Power System
  > IAH - FLIGHT 2060, DURING TAXI THE CREW REPORTED A RELAY CLICKING ON THE CAPTAINS SIDE WITH LOTS OF FUMES. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED SWITCH S0019 (DIMMER SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRC
- [SDR C2XA11IA074](https://openairdocs.org/sdr/C2XA11IA074.md): Blade · broken · Apr 21, 2011 · N15948 · Emb EMB145EP · Turbine Section
  > FLIGHT 2031, CREW REPORTED NR 2 ENG LP VIBRATIONS EXCEEDED LIMITS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE NR 2 ENGINE, OPS AND LEAK CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETU
- [SDR C2XA11IA055](https://openairdocs.org/sdr/C2XA11IA055.md): Control Handle · inoperative · Mar 17, 2011 · N15948 · Emb EMB145EP · Landing Gear Selector
  > IAH - FLIGHT 2544, THE CREW REPORTED THAT THE GEAR WAS SLOW TO RETRACT ON DEPARTURE FROM DAL WITH THE ASSOCIATED WARNINGS. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE, OPERATIONALLY
- [SDR C2XA10IA339](https://openairdocs.org/sdr/C2XA10IA339.md): Inverter · inoperative · Dec 17, 2010 · N15948 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT LIGHT AT THE WING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA10IA284](https://openairdocs.org/sdr/C2XA10IA284.md): Warning System · malfunctioned · Nov 4, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - 500 FEET ABOVE THE GROUND THE CREW REPORTED A LANDING GEAR AIR/ GRND FAIL MESSAAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESET THE LANDING GEAR AIR GROUND CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA10IA279](https://openairdocs.org/sdr/C2XA10IA279.md): Proximity Switch · inoperative · Oct 30, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2876, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR C2XA10SH362](https://openairdocs.org/sdr/C2XA10SH362.md): Skin · cracked · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET HEAD FR 78 RT SIDE. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN FR 78 RT SIDE IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH361](https://openairdocs.org/sdr/C2XA10SH361.md): Skin · cracked · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET AT RT SIDE FR 77. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN RT SIDE FR 77 IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH360](https://openairdocs.org/sdr/C2XA10SH360.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 29) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM L-FLANGE AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA10SH359](https://openairdocs.org/sdr/C2XA10SH359.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 29) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER BEAM CROSSBEAM SUPPORT AT FR 29 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS AP
- [SDR C2XA10SH358](https://openairdocs.org/sdr/C2XA10SH358.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 33) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH357](https://openairdocs.org/sdr/C2XA10SH357.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 33) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FR 33 IAW EMB-145 SRM 53-00-10 FIG 202 STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH356](https://openairdocs.org/sdr/C2XA10SH356.md): Yoke · cracked · Oct 25, 2010 · N15948 · Emb EMB145ER · Engine Mount Section
  > SHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH355](https://openairdocs.org/sdr/C2XA10SH355.md): Door Frame · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Structure
  > SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR STRUCTURE CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER STRUCTURE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH354](https://openairdocs.org/sdr/C2XA10SH354.md): Bracket · worn · Oct 25, 2010 · N15948 · Emb EMB145ER · Ailerons
  > SHV - DURING C-CHECK RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) MISSING. MAINTENANCE REMOVED AND REPLACED RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) IAW EMB-145 SRM 51-40-02.
- [SDR C2XA10SH353](https://openairdocs.org/sdr/C2XA10SH353.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FR 49-50 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH352](https://openairdocs.org/sdr/C2XA10SH352.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 58 CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 58 CARBON CROSS MEMBER IAW SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR C2XA10SH351](https://openairdocs.org/sdr/C2XA10SH351.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 44 HAS CORROSION (LEVEL 2 LOCAL) TO CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT FRM 44 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH350](https://openairdocs.org/sdr/C2XA10SH350.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 44 TO CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FR 44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH349](https://openairdocs.org/sdr/C2XA10SH349.md): Beam · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Structure (General)
  > SHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLANGE AT FRAME 54-59 IAW EMB-145 EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH348](https://openairdocs.org/sdr/C2XA10SH348.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM "L" FLANGE AT 49-50 AT CARBON CROSS MEMBER IAW EMB-145 SRM 51-40-02, 53-00-10 AND RESTORED TO ORI
- [SDR C2XA10SH347](https://openairdocs.org/sdr/C2XA10SH347.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 38) CTR OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CTR OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH346](https://openairdocs.org/sdr/C2XA10SH346.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 FLANGE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 19-20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH345](https://openairdocs.org/sdr/C2XA10SH345.md): Floor Support · corroded · Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 38) LT OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRM 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA275](https://openairdocs.org/sdr/C2XA10IA275.md): Proximity Sensor · dirty · Oct 24, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2541, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND THE THRUST REVERSERS WOULD NOT DEPLOY ON LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY TESTED THE THRUST REVERSERS WITH NO DEFECTS. CLEANED
- [SDR C2XA10IA255](https://openairdocs.org/sdr/C2XA10IA255.md): Skin · damaged · Sep 15, 2010 · N15948 · Emb EMB145EP · Rudder, Plate/Skin
  > IAH - FLIGHT 2149, DURING POST FLIGHT INSPECTION THE CREW REPORTED A HOLE IN THE RIGHT LOWER SIDE OF RUDDER II. MAINTENANCE REPLACED THE DAMAGED SECTION OF SKIN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA207](https://openairdocs.org/sdr/C2XA10IA207.md): Module · inoperative · Jul 25, 2010 · N15948 · Emb EMB145EP · Cabin Pressure Control System
  > IAH - FLIGHT 2547, DURING CLIMB THE CREW REPORTED THAT THE AUTO PRESSURIZATION WAS NOT WORKING AND THAT THE EICAS INDICATIONS WERE INTERMITTENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CPAM MODULE,
- [SDR C2XA10IA160](https://openairdocs.org/sdr/C2XA10IA160.md): Indicator · defective · May 23, 2010 · N15948 · Emb EMB145EP · Fuel Quantity Indicator
  > CRP - FLIGHT 2894, DURING CLIMB THE CREW REPORTED THAT THE NUMBER ONE FUEL QUANTITY INDICATOR DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY REPEATER OPERATIONALLY TESTED THE FUEL
- [SDR C2XA10IA133](https://openairdocs.org/sdr/C2XA10IA133.md): Light · out of adjust · Apr 26, 2010 · N15948 · Emb EMB145EP · Emergency Lighting
  > LRD - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW TWELVE TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA126](https://openairdocs.org/sdr/C2XA10IA126.md): Light · inoperative · Apr 22, 2010 · N15948 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA079](https://openairdocs.org/sdr/C2XA10IA079.md): Light · shorted · Feb 22, 2010 · N15948 · Emb EMB145EP · Flight Compartment Lighting
  > IAH - FLIGHT 2720, THE CREW REPORTED, SMELLED ELECTRICAL SMOKE AND CB11 FOR THE COCKPIT READING LIGHTS POPPED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE F/O'S READING LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS. A
- [SDR C2XA10IA045](https://openairdocs.org/sdr/C2XA10IA045.md): Light · inoperative · Jan 29, 2010 · N15948 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT ROW 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA027](https://openairdocs.org/sdr/C2XA10IA027.md): Unknown · odor · Jan 18, 2010 · N15948 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 2372, THE FLIGHT ATTENDANT REPORTED A SMELL OF FUEL IN THE CABIN DURING DESCENT WITH THE SMELL COMING FROM THE WING AREA AND AFT. THE SMELL DISSIPATED AFTER THE RECIRC FAN WAS TURNED OF, AND RETURNED ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHO
- [SDR C2XA09TY119](https://openairdocs.org/sdr/C2XA09TY119.md): Unknown · fumes · Jun 17, 2009 · N15948 · Emb EMB145ER · Air Distribution System
  > THERE WERE SUFFOCATING FUMES AND ODOR REPORTED BY THE GROUND WORKERS COMING FROM THE CARGO BIN. THE CARGO BIN WAS INSPECTED AND FOUND ODOR TO BE RESIDUAL FROM A PASSENGER TRANSPORTING FISH, THERE WAS NO FLUIDS FOUND IN CARGO AND NO MX OR DISCREPANCIES FOUND.
- [SDR C2XA09CL071](https://openairdocs.org/sdr/C2XA09CL071.md): Turbine Wheel · cracked · May 21, 2009 · N15948 · Emb EMB145EP · Turbine Section
  > DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.
- [SDR C2XA09TY063A](https://openairdocs.org/sdr/C2XA09TY063A.md): Connector · loose · Apr 20, 2009 · N15948 · Emb EMB145 · Light System Wiring
  > SEAT 12BC SIDEWALL AFT EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR AND OPS CHECKED GOOD. IAW EMB 145 AMM 33-50-14
- [SDR C2XA08IA042](https://openairdocs.org/sdr/C2XA08IA042.md): Skin · cracked · Jan 29, 2008 · N15948 · Emb EMB145EP · Wing, Plate/Skin
  > IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THE
- [SDR C2XA06IA082](https://openairdocs.org/sdr/C2XA06IA082.md): Wire Harness · disconnected · Jun 2, 2006 · N15948 · Emb EMB145EP · Light System Wiring
  > OKC - FLIGHT 2637, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIGN TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE SIGN, OPERATIONALLY CHECK
- [SDR C2XA06TY006](https://openairdocs.org/sdr/C2XA06TY006.md): Casting · cracked · Jan 10, 2006 · N15948 · Emb EMB145EP · Fuselage Main, Frame
  > MAIN DOOR FRAME STRUCTURE UPPER FWD STOP HOLE IS CRACKED (TOP INBOARD HOLE). REMOVED AND REPLACED CASTING FOR UPPER FWD PAX DOOR STOP IAW EMB 145 SRM 51-40-02.
- [SDR C2XA06TY005](https://openairdocs.org/sdr/C2XA06TY005.md): Floorbeam · corroded · Jan 10, 2006 · N15948 · Emb EMB145EP · Fuselage Main, Floor Beam
  > GALLEY AREA RT OMEGA BEAM CORRODED. BLENDED OUT CORROSION, APPLIED HYSOL, FABRICATED REPAIR DOUBLER, DRILLED COUNTERSANK, ALODINED, PRIMED. INSTALLED PAINT. ALL WORK C/W IAW EMB135/145 SRM 51-10-03, 51-20-03, 51-40-06, 51-40-02 AND 53-21-10 AND CPM 51-21-04

Next page: https://openairdocs.org/deregistered/N15948-2016-07-11/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 n_number = 'N15948' AND deregistration_id = 'N15948-2016-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15948-2016-07-11/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.