# Service difficulty reports: N732DH, cancelled Feb 21, 2013 A list on [N732DH, cancelled Feb 21, 2013](https://openairdocs.org/deregistered/N732DH-2013-02-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SIMA201101802](https://openairdocs.org/sdr/SIMA201101802.md): Sign · broken · Jan 17, 2011 · N732DH · Emb EMB135LR · Emergency Lighting > DURING MAINTENANCE BASE VISIT FOUND THE CABIN OVERHEAD LINER EMERGENCY EXIT SIGN BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN OVERHEAD EMERGENCY EXIT SIGN IAW EMB 135 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT W - [SDR SIMA200702302](https://openairdocs.org/sdr/SIMA200702302.md): Unknown · leaking · Jan 21, 2007 · N732DH · Emb EMB135LR · Turbine Engine Oil System > NR 2 SHUTDOWN DUE TO A LOUD POP FOLLOWED BY ENGINE OIL QUANTITY DROPPING TO 3 QUARTS, ITT IN AMBER RANGE EXCEEDING 930 DEGREES, AIRSPEED 280 KNOTS, FLIGHT LEVEL 350. MULTIPLE EICAS MESSAGES, PUNGENT WHITE SMOKE ENTERED CABIN, DISSIPATED AFTER SHUTDOWN OF NR 2 - [SDR SIMA200427904](https://openairdocs.org/sdr/SIMA200427904.md): Floor Support · corroded · Sep 21, 2004 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT A SECTION OF THE OMEGA BEAM TO REMOVE DAMAGE. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS. REPAIR DOEN IAW EMB 145SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-22-10, FIG 203. (SW21200500268) - [SDR SIMA200427905](https://openairdocs.org/sdr/SIMA200427905.md): Floor Support · corroded · Sep 20, 2004 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20. REMOVED RPREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, REINFORCEMENT PLATE AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142, CHAPTER 53, REV 27) 53-21-10 ITEM 2 FIGURE 2 - [SDR SIMA200426901](https://openairdocs.org/sdr/SIMA200426901.md): Stringer · chafed · Sep 18, 2004 · N732DH · Emb EMB135LR · Fuselage Main, Longeron/Stringer > ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A DATED - [SDR SIMA200426906](https://openairdocs.org/sdr/SIMA200426906.md): Sill · corroded · Sep 17, 2004 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC 2003/145-0818 DATED MARCH 6, 2003, AND AMERICAN EAGEL ENGINEERING TECHNICAL NOTICE EB 53-009. (M) - [SDR SIMA200426905](https://openairdocs.org/sdr/SIMA200426905.md): Floor Support · corroded · Sep 15, 2004 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > DURING AN IMBV INSPECTION, THE FORWARD GALLEY FLOOR DIGITAL WAS FOUND CORRODED. CUT OUT A DAMAGED SECTION FROM EXISTING DIGITAL AND CLEANED AREA. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 AND - [SDR SIMA200426904](https://openairdocs.org/sdr/SIMA200426904.md): Beam · corroded · Sep 15, 2004 · N732DH · Emb EMB135LR · Fuselage Main, Structure > DURING AN IMBV INSPECTION THE GALLEY CENTER BEAM WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMGAED AREA. FABRICATED A U SHAPE DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 PARA 5 FIG 204 SHEET 2. (M) - [SDR SIMA200217322](https://openairdocs.org/sdr/SIMA200217322.md): Frame · bent · Jun 21, 2002 · N732DH · Emb EMB135LR · APU Cowling/Containment > APU COWLING INTERIOR FORWARD FRAME IS BENT ABOVE THE TOP LEFT MOUNT HOLE, RECONTOURED FORWARD FRAME, PERFORMED NDT, NO DEFECTS. DONE IAW SRM AND MFG GST. - [SDR SIMA200217316](https://openairdocs.org/sdr/SIMA200217316.md): Skin · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Main, Plate/Skin > THREE GOUGES BETWEEN FRAMES 15-16, BETWEEN STRINGERS 16L AND 17L. (SUP) BLENDED GOUGES, PERFORMED NDT WITH NO DEFECTS. GOUGES ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200217317](https://openairdocs.org/sdr/SIMA200217317.md): Skin · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Main, Plate/Skin > GOUGE IN FUSELAGE SKIN BETWEEN FRAMES 71 AND 72 AND STRINGERS 16R AND 17R. BLENDED GOUGE, PERFORMED NDT WITH NO DEFECTS. GOUGE ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200217318](https://openairdocs.org/sdr/SIMA200217318.md): Skin · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Passenger/Crew Doors > GOUGE ON FORWARD EDGE OF MAIN DOOR SKIN. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. GOUGED ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200217319](https://openairdocs.org/sdr/SIMA200217319.md): Structure · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > GOUGE BETWEEN JUNCTION 1 AND FRAME 14, ALONG STRINGER 15L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200217320](https://openairdocs.org/sdr/SIMA200217320.md): Structure · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Miscellaneous Structure > GOUGE BETWEEN FRAMES 16-17 BETWEEN STRINGERS 16L AND 17L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200217321](https://openairdocs.org/sdr/SIMA200217321.md): Skin · gouged · Jun 19, 2002 · N732DH · Emb EMB135LR · Wing, Plate/Skin > LEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST. - [SDR SIMA200208712](https://openairdocs.org/sdr/SIMA200208712.md): Fire Warning · false activation · Mar 26, 2002 · N732DH · Emb EMB135LR · Fire Detection > RDU - FLT 4549 - ON CLIMB-OUT, CREW HAD CARGO COMPARTMENT SMOKE WARNING AND DISCHARGED FIRE BOTTLES. DECLARED EMERGENCY AND RETURNED TO RDU. NO FIRE NOTICED. REPLACED CARGO FIRE BOTTLES. PERFORMED SYSTEMS OPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE - [SDR SIMA20011079](https://openairdocs.org/sdr/SIMA20011079.md): Smoke · detected · Apr 17, 2001 · N732DH · Emb EMB135LR · Flight Compartment Equipment > LGA - FLT 4521 - DURING INITIAL POWER UP ON AIRCRAFT WITH BATTERY AND AVIONICS SWITCHES ON, SMOKE WAS OBSERVED POURING OUT OF THE CENTER CONSOLE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED APU START AND RAN ELECTRICAL SYSTEM AND FOUND NO EVIDENCE - [SDR SIMA200102901](https://openairdocs.org/sdr/SIMA200102901.md): Structure · leaking · Jan 29, 2001 · N732DH · Emb EMB135LR · Aircraft Structures > LGA - FLT 4559 - DURING CLIMB, CREW REPORTED A PRESSURIZATION LEAK IN THE FORWARD NOSE GEAR AREA. CABIN PRESSURE STARTED TO CLIMB TO 6 PSI AT 5000 FEET. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK IAW EMB MM 21-31-00 WAS GOOD AND AIRCRAFT ## 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 = 'N732DH' AND deregistration_id = 'N732DH-2013-02-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N732DH-2013-02-21/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.